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Engine model

Continental IO-360

Continental Aerospace Technologies

Airworthiness Directives
15
Manufacturer bulletins
7764 Service Bulletins, 13 Service Instructions
Last live check
2026-10-0315 of 15 re-checked, oldest 2026-10-01

Printed from https://aircraftdirectives.com/engine/continental-io-360 · AircraftDirectives restates official FAA and manufacturer records; the official sources named on this sheet control. Not an airworthiness determination.

This page is a reference Record, not an airworthiness or compliance determination. Official FAA and manufacturer sources control over our restatement, subject to governing law. Check applicability, current requirements and incorporated documents before acting. The owner or operator remains responsible for airworthiness and required records under 14 CFR 91.403 and 91.417, as applicable. Terms of Use: /terms.

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Also known as: TSIO-360

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What directives and bulletins apply to the Continental IO-360

The FAA has published 15 Airworthiness Directives that name the Continental IO-360 (Continental Aerospace Technologies), the earliest in 1995 and the newest on 2023-09-21. The index also holds 3 correction notices for an earlier directive. 77 manufacturer bulletins from Continental Aerospace Technologies name this engine too.

Newest

  1. AD 2023-17-04 Airworthiness Directives; Continental Aerospace Technologies, Inc. Engines 2023-09-21
  2. AD 2023-05-16 Airworthiness Directives; Continental Aerospace Technologies, Inc., Reciprocating Engines 2023-03-15
  3. AD 2023-04-08 Airworthiness Directives; Continental Aerospace Technologies, Inc. Reciprocating Engines 2023-02-23

See all 15 directives

The ones owners meet again

  1. AD 2009-02-03 Airworthiness Directives; Lycoming Engines IO, (L)IO, TIO, (L)TIO, AEIO, AIO, IGO, IVO, an... 2009-01-23 Repetitive inspection or action

We index directives by model, not by serial number or N-number; the record page and the official document say which serials apply.

Bulletins that matter

  1. SB SB25-01 Inspection and Replacement of Part No. 652421 Nuts Used to Secure Engine Mount Legs to the... Open the bulletin
  2. SB MSB23-01A Crankshaft counterweights Open the bulletin
  3. SB SB20-03 ENGINE PRESERVATION DURING COVID-19 PANDEMIC Open the bulletin
  4. SB SB19-09 CHAMPION AEROSPACE SLICK SERVICE BULLETIN SB2-19 Open the bulletin
  5. SB SB19-07 CRANKSHAFT END PLAY CHECK Open the bulletin

How to use this page: check the newest directives at every annual, keep the repetitive items on your inspection calendar, and open the official Federal Register text before any work - our summaries are a reading aid, not a determination of compliance.

Airworthiness Directives

15 records · 3 corrections attached · 3 superseded records nested above
ADAD 2023-17-04Continental Aerospace Technologies, Inc. Engines2023-10-26Active
AD

2023-17-04

FR doc 2023-20445 · 88 FR 65120

AD 2023-17-04Published 2023-09-21Effective 2023-10-26

Supersedes 2022-04-04

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

Continental Aerospace Technologies, Inc. Engines

Requires replacing the fiber gasket with a copper gasket or a stainless steel embedded within polytetrafluoroethylene gasket (stainless steel PTFE gasket).

1 AD superseded by this one retired · earliest 2022-02-22
AD

2022-04-04

FR doc 2022-03640 · 87 FR 9435

AD 2022-04-04Published 2022-02-22Effective 2022-03-29

Superseded by 2023-17-04 — see above

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

Continental Aerospace Technologies, Inc. and Continental Motors Reciprocating Engines

Requires replacing the oil filter adapter fiber gasket (fiber gasket) with an oil filter adapter copper gasket (copper gasket).

Full official abstract

Airworthiness Directives; Continental Aerospace Technologies, Inc. and Continental Motors Reciprocating Engines

The FAA is adopting a new airworthiness directive (AD) for certain Continental Aerospace Technologies, Inc. C-125, C145, IO-360, IO-470, IO-550, O-300, O-470, TSIO-360, TSIO-520 series model reciprocating engines and certain Continental Motors IO-520 series model reciprocating engines with a certain oil filter adapter installed. This AD was prompted by reports of two accidents that were the result of power loss due to oil starvation. This AD requires replacing the oil filter adapter fiber gasket (fiber gasket) with an oil filter adapter copper gasket (copper gasket). The FAA is issuing this AD to address the unsafe condition on these products.

Source: Federal Register document 2022-03640, retrieved 2026-08-15 · checked against the live Federal Register record on 2026-10-01

View on Federal Register (opens in a new tab) View this AD in FAA DRS (opens in a new tab) Print AD packet (opens the full Federal Register document in a new tab)
Full official abstract

Airworthiness Directives; Continental Aerospace Technologies, Inc. Engines

The FAA is superseding Airworthiness Directive (AD) 2022-04-04 for certain Continental Aerospace Technologies, Inc. (Continental) Model C-125, C145, IO-360, IO-470, IO-550, O-300, O-470, TSIO-360, and TSIO-520 series engines and certain Continental Motors IO-520 series engines with a certain oil filter adapter installed. AD 2022-04-04 required replacing the oil filter adapter fiber gasket (fiber gasket) with an oil filter adapter copper gasket (copper gasket). This AD was prompted by reports of two accidents that were the result of power loss due to oil starvation. This AD requires replacing the fiber gasket with a copper gasket or a stainless steel embedded within polytetrafluoroethylene gasket (stainless steel PTFE gasket). This AD also revises the applicability to include Continental model engines equipped with an F&M Enterprises, Inc. (F&M) or a Stratus Tool Technologies, LLC (Stratus) oil filter adapter installed. The FAA is issuing this AD to address the unsafe condition on these products.

Source: Federal Register document 2023-20445, retrieved 2026-08-15 · checked against the live Federal Register record on 2026-10-01

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ADAD 2023-05-16Continental Aerospace Technologies, Inc., Reciprocating Engines2023-03-15Active
AD

2023-05-16

FR doc 2023-05339 · 88 FR 15901

AD 2023-05-16Published 2023-03-15Effective 2023-03-15

Supersedes 2023-04-08

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

Continental Aerospace Technologies, Inc., Reciprocating Engines

Requires inspection of the crankshaft assembly for proper installation of the counterweight retaining rings in the counterweight groove, and corrective actions if improper installation is found.

1 AD superseded by this one retired · earliest 2023-02-23
AD

2023-04-08

FR doc 2023-03796 · 88 FR 11383

AD 2023-04-08Published 2023-02-23Effective 2023-02-23

Superseded by 2023-05-16 — see above

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

Continental Aerospace Technologies, Inc. Reciprocating Engines

Requires inspection of the crankshaft assembly for proper installation of the counterweight retaining rings in the counterweight groove, and corrective actions if improper installation is found.

Full official abstract

Airworthiness Directives; Continental Aerospace Technologies, Inc. Reciprocating Engines

The FAA is adopting a new airworthiness directive (AD) for certain Continental Aerospace Technologies, Inc. (Continental) GTSIO- 520-C, -D, -H, -K, -L, -M, -N, and -S; IO-360-A, -AB, -AF, -C, -CB, -D, -DB, -E, -ES, -G, -GB, -H, -HB, -J, -JB, -K, and -KB; IO-470-D, -E, -G, -H, -J, -K, -L, -M, -N, -P, -R, -S, -T, -U, -V, and -VO; IO-520-A, -B, -BA, -BB, -C, -CB, -D, -E, -F, -J, -K, -L, -M, and -MB; IO-550-A, -B, - C, -D, -E, -F, -G, -L, -N, -P, and -R; LTSIO-360-E, -EB, -KB, and -RB; LTSIO-520-AE; O-470-A, -B, -E, -G, -H, -J, -K, -L, -M, -N, -R, -S, -T, and -U; TSIO-360-A, -AB, -B, -BB, -C, -CB, -D, -DB, -E, -EB, -G, -GB, - H, -HB, -JB, -KB, -LB, -MB, -RB, and -SB; TSIO-520-A, -AE, -AF, -B, - BB, -BE, -C, -CE, -D, -DB, -E, -EB, -G, -H, -J, -JB, -K, -KB, -L, -LB, -M, -NB, -P, -R, -T, -UB, -VB, and -WB; TSIO-550-A, -B, -C, -E, -G, -K, and -N; TSIOF-550-K; and TSIOL-550-A, -B, and -C model reciprocating engines. This AD was prompted by a report of a quality escape involving improper installation of counterweight retaining rings in the engine crankshaft counterweight groove during manufacture. This AD requires inspection of the crankshaft assembly for proper installation of the counterweight retaining rings in the counterweight groove, and corrective actions if improper installation is found. The FAA is issuing this AD to address the unsafe condition on these products.

Source: Federal Register document 2023-03796, retrieved 2026-08-15 · checked against the live Federal Register record on 2026-10-01

View on Federal Register (opens in a new tab) View this AD in FAA DRS (opens in a new tab) Print AD packet (opens the full Federal Register document in a new tab)
Full official abstract

Airworthiness Directives; Continental Aerospace Technologies, Inc., Reciprocating Engines

The FAA is superseding Airworthiness Directive (AD) 2023-04-08 which applied to certain Continental Aerospace Technologies, Inc. (Continental) GTSIO-520-C, -D, -H, -K, -L, -M, -N, and -S; IO-360-A, - AB, -AF, -C, -CB, -D, -DB, -E, -ES, -G, -GB, -H, -HB, -J, -JB, -K, and -KB; IO-470-D, -E, -G, -H, -J, -K, -L, -M, -N, -P, -R, -S, -T, -U, -V, and -VO; IO-520-A, -B, -BA, -BB, -C, -CB, -D, -E, -F, -J, -K, -L, -M, and -MB; IO-550-A, -B, -C, -D, -E, -F, -G, -L, -N, -P, and -R; LTSIO- 360-E, -EB, -KB, and -RB; LTSIO-520-AE; O-470-A, -B, -E, -G, -H, -J, - K, -L, -M, -N, -R, -S, -T, and -U; TSIO-360-A, -AB, -B, -BB, -C, -CB, - D, -DB, -E, -EB, -G, -GB, -H, -HB, -JB, -KB, -LB, -MB, -RB, and -SB; TSIO-520-A, -AE, -AF, -B, -BB, -BE, -C, -CE, -D, -DB, -E, -EB, -G, -H, -J, -JB, -K, -KB, -L, -LB, -M, -NB, -P, -R, -T, -UB, -VB, and -WB; TSIO-550-A, -B, -C, -E, -G, -K, and -N; TSIOF-550-K; and TSIOL-550-A, - B, and -C model reciprocating engines. AD 2023-04-08 required inspection of the crankshaft assembly for proper installation of the counterweight retaining rings in the counterweight groove and, depending on the results of the inspection, corrective actions if improper installation was found. This AD continues to require inspection of the crankshaft assembly for proper installation of the counterweight retaining rings in the counterweight groove, and corrective actions if improper installation is found. Since the FAA issued AD 2023-04-08, operators notified the FAA, and Continental confirmed, that certain affected model reciprocating engines not included in the applicability of AD 2023-04-08 are also affected by the unsafe condition. Additionally, the FAA determined the special flight permit paragraph required revision. This AD was prompted by a report of a quality escape involving improper installation of counterweight retaining rings in the engine crankshaft counterweight groove during manufacture. The FAA is issuing this AD to address the unsafe condition on these products.

Source: Federal Register document 2023-05339, retrieved 2026-08-15 · checked against the live Federal Register record on 2026-10-01

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ADAD 2022-16-03Continental Aerospace Technologies, Inc., Lycoming Engines, and Textron Lycoming/Subsidiary of Textron, Inc. Reciprocating Engines2022-08-15Active
AD

2022-16-03

FR doc 2022-16371 · 87 FR 45633

AD 2022-16-03Published 2022-07-29Effective 2022-08-15

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

Continental Aerospace Technologies, Inc., Lycoming Engines, and Textron Lycoming/Subsidiary of Textron, Inc. Reciprocating Engines

Requires the replacement of affected magneto or inspection of affected magneto and, if no white grease is detected, replacement of magneto components, as applicable, and reassembly of the magneto.

Full official abstract

Airworthiness Directives; Continental Aerospace Technologies, Inc., Lycoming Engines, and Textron Lycoming/Subsidiary of Textron, Inc. Reciprocating Engines

The FAA is adopting a new airworthiness directive (AD) for certain Continental Aerospace Technologies, Inc. GTSIO-520, IO-346, IO- 470, IO-520, IO-550, LTSIO-520, O-470, TSIO-520, and TSIOL-550 series model reciprocating engines, Lycoming Engines AEIO-320, AEIO-360, AEIO- 540, AIO-320, AIO-360, GO-480, GSO-480, HIO-360, HIO-540, IGO-480, IGO- 540, IGSO-480, IGSO-540, IO-320, IO-360, IO-540, LIO-360, LTIO-540, O- 235, O-320, O-360, O-540, TIGO-541, TIO-360, TIO-540, TIO-541, TVO-435, VO-435, and VO-540 series model reciprocating engines, and Textron Lycoming/Subsidiary of Textron, Inc. IO-720 series model reciprocating engines. This AD was prompted by a report of a manufacturing quality escape of improperly lubricated roller bearings installed in certain magnetos, which may result in overheating and magneto seizure. This AD requires the replacement of affected magneto or inspection of affected magneto and, if no white grease is detected, replacement of magneto components, as applicable, and reassembly of the magneto. The FAA is issuing this AD to address the unsafe condition on these products.

Source: Federal Register document 2022-16371, retrieved 2026-08-14 · checked against the live Federal Register record on 2026-10-02

View on Federal Register (opens in a new tab) View this AD in FAA DRS (opens in a new tab) Print AD packet (opens the full Federal Register document in a new tab)
ADAD 2013-21-02Lycoming Engines and Continental Motors, Inc. Reciprocating Engines2013-11-13Active
AD

2013-21-02

FR doc 2013-25342 · 78 FR 64394

AD 2013-21-02Published 2013-10-29Effective 2013-11-13

Supersedes 2012-24-09

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

Lycoming Engines and Continental Motors, Inc. Reciprocating Engines

Requires removing certain HET turbochargers from service before further flight.

1 AD superseded by this one retired · earliest 2012-12-05
AD

2012-24-09

FR doc 2012-29472 · 77 FR 72203

AD 2012-24-09Published 2012-12-05Effective 2012-12-20

Superseded by 2013-21-02 — see above

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

Lycoming Engines and Continental Motors, Inc. Reciprocating Engines

Requires removing the affected turbochargers from service before further flight.

1 correction to this AD FAA · 2013-01-14

Correction published 2013-01-14

Issued by
Federal Aviation Administration
Published
2013-01-14
Document
Federal Register 2013-00525 · Final rule; correction

The FAA is correcting an airworthiness directive (AD) that published in the Federal Register. That AD applies to Lycoming Engines TSIO-540-AK1A, and Continental Motors, Inc. TSIO-360-MB, TSIO-360-SB, and TSIO-360-RB reciprocating engines, with certain Hartzell Engine Technologies (HET) turbochargers, model TA0411, part number 466642- 0001; 466642-0002; 466642-0006; 466642-9001; 466642-9002; or 466642- 9006, or with certain HET model TA0411 turbochargers overhauled or repaired since August 29, 2012. The Summary paragraph and the Applicability paragraph list an incorrect engine model for Lycoming Engines. This document corrects those errors. In all other respects, the original document remains the same.

A correction restates part of an AD that was published incorrectly. It is not an additional requirement and it does not change the AD number or its effective date.

Source: Federal Register document 2013-00525, retrieved 2026-08-15

Read this correction on Federal Register (opens in a new tab)
Full official abstract

Airworthiness Directives; Lycoming Engines and Continental Motors, Inc. Reciprocating Engines

We are adopting a new airworthiness directive (AD) for Lycoming Engines TSIO-540-AK1A, and Continental Motors, Inc. TSIO-360- MB, TSIO-360-SB, and TSIO-360-RB reciprocating engines, with certain Hartzell Engine Technologies (HET) turbochargers, model TA0411, part number (P/N) 466642-0001; 466642-0002; 466642-0006; 466642-9001; 466642-9002; or 466642-9006, or with certain HET model TA0411 turbochargers overhauled or repaired since August 29, 2012. This AD requires removing the affected turbochargers from service before further flight. This AD was prompted by a report of a turbocharger turbine wheel that failed a static strength test at its manufacturing facility. We are issuing this AD to prevent turbocharger turbine wheel failure, reduction or complete loss of engine power, loss of engine oil, oil fire, and damage to the airplane.

Source: Federal Register document 2012-29472, retrieved 2026-08-15 · checked against the live Federal Register record on 2026-10-01

View on Federal Register (opens in a new tab) Search DRS manually for AD 2012-24-09 (opens in a new tab) Print AD packet (opens the full Federal Register document in a new tab)
Full official abstract

Airworthiness Directives; Lycoming Engines and Continental Motors, Inc. Reciprocating Engines

We are superseding airworthiness directive (AD) 2012-24-09 for Lycoming Engines TIO-540-AK1A, and Continental Motors, Inc. (CMI) TSIO- 360-MB, TSIO-360-SB, and TSIO-360-RB reciprocating engines, with certain Hartzell Engine Technologies (HET) turbochargers, model TA0411, installed. AD 2012-24-09 required removing certain HET turbochargers from service before further flight. This AD also requires removing certain HET turbochargers from service before further flight. This AD was prompted by a report that an additional engine, the CMI LTSIO-360- RB, has the affected HET turbochargers installed. We are issuing this AD to prevent turbocharger turbine wheel failure, reduction or complete loss of engine power, loss of engine oil, oil fire, and damage to the airplane.

Source: Federal Register document 2013-25342, retrieved 2026-08-15 · checked against the live Federal Register record on 2026-10-03

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ADAD 2011-26-07Teledyne Continental Motors (TCM) and Rolls-Royce Motors Ltd. (R-RM) Series Reciprocating Engines2012-01-24Active
AD

2011-26-07

FR doc 2011-32252 · 76 FR 78808

AD 2011-26-07Published 2011-12-20Effective 2012-01-24

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

Teledyne Continental Motors (TCM) and Rolls-Royce Motors Ltd. (R-RM) Series Reciprocating Engines

Requires replacement of certain magnetos if they fall within the specified serial number (S/N) range, inspection of the removed magneto to verify that the stop pin is still in place, and, if the stop pin is not in place…

Full official abstract

Airworthiness Directives; Teledyne Continental Motors (TCM) and Rolls-Royce Motors Ltd. (R-RM) Series Reciprocating Engines

We are superseding an existing airworthiness directive (AD) for certain TCM and R-RM series reciprocating engines. That AD currently requires replacement of certain magnetos if they fall within the specified serial number (S/N) range, inspection of the removed magneto to verify that the stop pin is still in place, and, if the stop pin is not in place, inspection of the engine gear train, crankcase, and accessory case. This new AD corrects the range of S/Ns affected, requires the same replacement and inspections, and adds R-RM C-125, C- 145, O-300, IO-360, TSIO-360, and LTSIO-520-AE series reciprocating engines to the applicability. This AD was prompted by our awareness of an error in the previous AD applicability in the range of magneto S/Ns affected and of the need to include certain engines made by R-RM, under license of TCM. We are issuing this AD to prevent engine failure and loss of control of the airplane due to migration of the magneto impulse coupling stop pin out of the magneto frame and into the gear train of the engine.

Source: Federal Register document 2011-32252, retrieved 2026-08-15 · checked against the live Federal Register record on 2026-10-01

View on Federal Register (opens in a new tab) View this AD in FAA DRS (opens in a new tab) Print AD packet (opens the full Federal Register document in a new tab)
ADAD 2010-11-04Teledyne Continental Motors (TCM) 240, 346, 360, 470, 520, and 550 Series and Rolls-Royce Motors, Ltd. (R-RM) IO-240-A Reciprocating Engines2010-06-16Active
AD

2010-11-04

FR doc 2010-12177 · 75 FR 30290

AD 2010-11-04Published 2010-06-01Effective 2010-06-16

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

Teledyne Continental Motors (TCM) 240, 346, 360, 470, 520, and 550 Series and Rolls-Royce Motors, Ltd. (R-RM) IO-240-A Reciprocating Engines

Requires before further flight, replacing certain part number (P/N) hydraulic lifters.

Full official abstract

Airworthiness Directives; Teledyne Continental Motors (TCM) 240, 346, 360, 470, 520, and 550 Series and Rolls-Royce Motors, Ltd. (R-RM) IO-240-A Reciprocating Engines

The FAA is superseding an existing emergency airworthiness directive (AD) 2009-24-52 that was sent previously to all known U.S. owners and operators of TCM 240, 360, 470, 520, and 550 series reciprocating engines. That AD requires before further flight, replacing certain part number (P/N) hydraulic lifters. This AD results from TCM reporting another occurrence of rapid wear on the face of hydraulic lifters, P/Ns 657913, 657915, and 657916, and from the need to expand the applicability of this AD to include the TCM 346 series reciprocating engines and the R-RM IO-240-A reciprocating engines. We are issuing this AD to prevent excessive hydraulic lifter wear, which can result in loss of engine power and loss of control of the airplane.

Source: Federal Register document 2010-12177, retrieved 2026-08-17 · checked against the live Federal Register record on 2026-10-02

View on Federal Register (opens in a new tab) View this AD in FAA DRS (opens in a new tab) Print AD packet (opens the full Federal Register document in a new tab)
ADAD 2009-02-03Lycoming Engines IO, (L)IO, TIO, (L)TIO, AEIO, AIO, IGO, IVO, and HIO Series Reciprocating Engines, Teledyne Continental Motors (TCM) LTSIO-360-RB and TSIO-360-RB Reciprocating Engines, and Superior Air Parts, Inc. IO-360 Series Reciprocating Engines With Certain Precision Airmotive LLC RSA-5 and RSA-10 Series, and Bendix RSA-5 and RSA-10 Series, Fuel Injection Servos2009-02-09Active
AD

2009-02-03

FR doc E9-1047 · 74 FR 4123

AD 2009-02-03Published 2009-01-23Effective 2009-02-09

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

Lycoming Engines IO, (L)IO, TIO, (L)TIO, AEIO, AIO, IGO, IVO, and HIO Series Reciprocating Engines, Teledyne Continental Motors (TCM) LTSIO-360-RB and TSIO-360-RB Reciprocating Engines, and Superior Air Parts, Inc. IO-360 Series Reciprocating Engines With Certain Precision Airmotive LLC RSA-5 and RSA-10 Series, and Bendix RSA-5 and RSA-10 Series, Fuel Injection Servos

Requires inspecting servo plugs for looseness and damage on fuel injection servos that have a servo plug gasket, part number (P/N) 365533, installed, and if loose, inspecting the servo regulator cover threads for damage…

Full official abstract

Airworthiness Directives; Lycoming Engines IO, (L)IO, TIO, (L)TIO, AEIO, AIO, IGO, IVO, and HIO Series Reciprocating Engines, Teledyne Continental Motors (TCM) LTSIO-360-RB and TSIO-360-RB Reciprocating Engines, and Superior Air Parts, Inc. IO-360 Series Reciprocating Engines With Certain Precision Airmotive LLC RSA-5 and RSA-10 Series, and Bendix RSA-5 and RSA-10 Series, Fuel Injection Servos

The FAA is superseding an existing airworthiness directive (AD) for Lycoming Engines IO, (L)IO, TIO, (L)TIO, AEIO, AIO, IGO, IVO, and HIO series reciprocating engines, TCM TSIO-360-RB reciprocating engines, and Superior Air Parts, Inc. IO-360 series reciprocating engines with certain Precision Airmotive LLC RSA-5 and RSA-10 series fuel injection servos. That AD currently requires inspecting servo plugs for looseness and damage on fuel injection servos that have a servo plug gasket, part number (P/N) 365533, installed, and if loose, inspecting the servo regulator cover threads for damage, inspecting the gasket for damage, reinstalling acceptable parts, and torquing the servo plug to a new, higher torque to maintain the proper clamp-up force between the plug and cover. This AD requires the same inspections, except if the plug is found loose, servo plug gasket, P/N 365533, must be replaced with a new, improved gasket, P/N 2577258. This AD also requires replacement by December 31, 2009, of servo plug gaskets, P/N 365533, manufactured and made available on or after August 22, 2006, as mandatory terminating action to the repetitive inspections required by this AD. This AD also prohibits the installation of any servo plug gasket, P/N 365533. This AD also clarifies the TCM engine model applicability, and adds Bendix RSA-5 and RSA-10 series fuel injection servos to the applicability. This AD results from Precision Airmotive LLC introducing the installation of a new improved servo plug gasket, P/N 2577258, to the affected Precision Airmotive LLC RSA-5 and RSA-10 series, and Bendix RSA-5 and RSA-10 series, fuel injection servos. We are issuing this AD to prevent a lean running engine, which could result in a substantial loss of engine power and subsequent loss of control of the airplane.

Source: Federal Register document E9-1047, retrieved 2026-08-14 · checked against the live Federal Register record on 2026-10-02

View on Federal Register (opens in a new tab) View this AD in FAA DRS (opens in a new tab) Print AD packet (opens the full Federal Register document in a new tab)
ADAD 2008-08-14Lycoming Engines IO, (L)IO, TIO, (L)TIO, AEIO, AIO, IGO, IVO, and HIO Series Reciprocating Engines, Teledyne Continental Motors (TCM) TSIO-360-RB Reciprocating Engines, and Superior Air Parts, Inc. IO-360 Series Reciprocating Engines With Certain Precision Airmotive LLC RSA-5 and RSA-10 Series Fuel Injection Servos2008-04-29Active
AD

2008-08-14

FR doc E8-7574 · 73 FR 19977

AD 2008-08-14Published 2008-04-14Effective 2008-04-29

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

Lycoming Engines IO, (L)IO, TIO, (L)TIO, AEIO, AIO, IGO, IVO, and HIO Series Reciprocating Engines, Teledyne Continental Motors (TCM) TSIO-360-RB Reciprocating Engines, and Superior Air Parts, Inc. IO-360 Series Reciprocating Engines With Certain Precision Airmotive LLC RSA-5 and RSA-10 Series Fuel Injection Servos

Prompted by eighteen reports of fuel injection servo plugs, part number (P/N) 383493, that had loosened or completely backed out of the threaded plug hole on the regulator cover of the fuel injection servo.

Full official abstract

Airworthiness Directives; Lycoming Engines IO, (L)IO, TIO, (L)TIO, AEIO, AIO, IGO, IVO, and HIO Series Reciprocating Engines, Teledyne Continental Motors (TCM) TSIO-360-RB Reciprocating Engines, and Superior Air Parts, Inc. IO-360 Series Reciprocating Engines With Certain Precision Airmotive LLC RSA-5 and RSA-10 Series Fuel Injection Servos

This document publishes in the Federal Register an amendment adopting emergency airworthiness directive (AD) 2008-06-51 that was sent previously to all known U.S. owners and operators of Lycoming Engines IO, (L)IO, TIO, (L)TIO, AEIO, AIO, IGO, IVO, and HIO series reciprocating engines, TCM TSIO-360-RB reciprocating engines, and Superior Air Parts, Inc. IO-360 series reciprocating engines with certain Precision Airmotive LLC RSA-5 and RSA-10 series fuel injection servos. This AD results from eighteen reports of fuel injection servo plugs, part number (P/N) 383493, that had loosened or completely backed out of the threaded plug hole on the regulator cover of the fuel injection servo. These servo plugs were installed with servo plug gasket, P/N 365533, under the plug hex-head. We are issuing this AD to prevent a lean running engine, which could result in a substantial loss of engine power and subsequent loss of control of the airplane.

Source: Federal Register document E8-7574, retrieved 2026-08-14 · checked against the live Federal Register record on 2026-10-02

View on Federal Register (opens in a new tab) Search DRS manually for AD 2008-08-14 (opens in a new tab) Print AD packet (opens the full Federal Register document in a new tab)
ADAD 2002-13-04Teledyne Continental Motors2002-07-12Active
AD

2002-13-04

FR doc 02-16174 · 67 FR 43230

AD 2002-13-04Published 2002-06-27Effective 2002-07-12

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

Teledyne Continental Motors

Requires the same replacement and inspections and adds TCM C-125 and C145 series reciprocating engines to the applicability, which were inadvertently omitted from the emergency AD.

1 correction to this AD FAA · 2002-07-26

Correction published 2002-07-26

Issued by
Federal Aviation Administration
Published
2002-07-26
Document
Federal Register 02-19035 · Final rule; correction
Corrects
the version published June 27, 2002 at 67 FR 43230

This document makes a correction to Airworthiness Directive (AD) 2000-NE-19 applicable to Teledyne Continental Motors O-300, IO- 360, TSIO-360, and LTSIO-520-AE series reciprocating engines that was published in the Federal Register on June 27, 2002 (67 FR 43230). The superseded AD number was inadvertently omitted from the regulatory information, paragraph 2. of Sec. 39.13 [Amended]. This document corrects that omission. In all other respects, the original document remains the same.

A correction restates part of an AD that was published incorrectly. It is not an additional requirement and it does not change the AD number or its effective date.

Source: Federal Register document 02-19035, retrieved 2026-08-15

Read this correction on Federal Register (opens in a new tab)
Full official abstract

Airworthiness Directives; Teledyne Continental Motors

This amendment supersedes emergency airworthiness directive (AD) 2000-11-51 that was sent previously to all known U.S. owners and operators of Teledyne Continental Motors (TCM) O-300, IO-360, TSIO-360, and LTSIO-520-AE series reciprocating engines. That action required within 10 flight hours after receipt of that AD, replacement of certain magnetos if they fall within the specified serial number range, inspection of the removed magneto to verify that the stop pin is still in place, and, if the stop pin is not in place, inspection of the engine gear train. This amendment requires the same replacement and inspections and adds TCM C-125 and C145 series reciprocating engines to the applicability, which were inadvertently omitted from the emergency AD. This amendment is prompted by reports of engine failures on certain TCM reciprocating engines. The actions specified by this AD are intended to prevent engine failure and loss of control of the airplane due to migration of the magneto impulse coupling stop pin out of the magneto frame and into the gear train of the engine.

Source: Federal Register document 02-16174, retrieved 2026-08-15 · checked against the live Federal Register record on 2026-10-01

View on Federal Register (opens in a new tab) Search DRS manually for AD 2002-13-04 (opens in a new tab) Print AD packet (opens the full Federal Register document in a new tab)
ADAD 2000-23-21Teledyne Continental Motors IO-360, TSIO-360, LTSIO-360, O-470, IO-470, TSIO-470, IO-520, TSIO-520, LTSIO-520, IO-550, TSIO-550, and TSIOL-550 Series Reciprocating Engines2000-12-12Active
AD

2000-23-21

FR doc 00-29496 · 65 FR 70654

AD 2000-23-21Published 2000-11-27Effective 2000-12-12

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

Teledyne Continental Motors IO-360, TSIO-360, LTSIO-360, O-470, IO-470, TSIO-470, IO-520, TSIO-520, LTSIO-520, IO-550, TSIO-550, and TSIOL-550 Series Reciprocating Engines

Requires removing a core sample of material from the propeller mounting flange of certain crankshafts, and sending the core sample to TCM for evaluation.

Full official abstract

Airworthiness Directives; Teledyne Continental Motors IO-360, TSIO-360, LTSIO-360, O-470, IO-470, TSIO-470, IO-520, TSIO-520, LTSIO-520, IO-550, TSIO-550, and TSIOL-550 Series Reciprocating Engines

This amendment supersedes emergency airworthiness directive (AD) 2000-08-51. Emergency AD 2000-08-51 was sent to all known U.S. owners and operators of Teledyne Continental Motors (TCM) IO-360, TSIO- 360, LTSIO-360, O-470, IO-470, TSIO-470, IO-520, TSIO-520, LTSIO-520, IO-550, TSIO-550, and TSIOL-550 series reciprocating engines by individual letters. This amendment requires removing a core sample of material from the propeller mounting flange of certain crankshafts, and sending the core sample to TCM for evaluation. This amendment is prompted by reports of crankshaft failures, and by the addition of additional crankshaft serial numbers (SN) that have been added to the suspect population. The actions specified by this AD are intended to prevent fracture of the crankshaft connecting rod journal, which could result in total engine power loss, in-flight engine failure and possible forced landing.

Source: Federal Register document 00-29496, retrieved 2026-08-15 · checked against the live Federal Register record on 2026-10-01

View on Federal Register (opens in a new tab) View this AD in FAA DRS (opens in a new tab) Print AD packet (opens the full Federal Register document in a new tab)
ADAD 97-26-17Teledyne Continental Motors IO-360, TSIO-360, LTSIO-360, IO-520, LIO-520, TSIO-520, LTSIO-520 Series, and Rolls-Royce plc IO-360 and TSIO-360 Series Reciprocating Engines1998-01-23Active
AD

97-26-17

FR doc 97-33142 · 62 FR 66502

AD 97-26-17Published 1997-12-19Effective 1998-01-23

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

Teledyne Continental Motors IO-360, TSIO-360, LTSIO-360, IO-520, LIO-520, TSIO-520, LTSIO-520 Series, and Rolls-Royce plc IO-360 and TSIO-360 Series Reciprocating Engines

Requires ultrasonic inspection for subsurface fatigue cracks in crankshafts installed in TCM IO-520 and TSIO-520 series engines and replacement of the crankshaft if a crack is found.

1 correction to this AD FAA · 1998-03-09

Correction published 1998-03-09

Issued by
Federal Aviation Administration
Published
1998-03-09
Document
Federal Register 98-5798 · Final rule; correction
Corrects
the version published December 19, 1997 at 62 FR 66502

This document makes a correction to airworthiness directive (AD) 97-26-17 applicable to certain Teledyne Continental Motors (TCM) IO-520 and TSIO-520 engines that was published in the Federal Register on December 19, 1997 (62 FR 66502). The address information for the contact engineer in the For Further Information Contact section and the manufacturer's telephone number in the Addresses section and paragraph (f) of the Compliance Section is incorrect. This document corrects that information. In all other respects, the original document remains the same.

A correction restates part of an AD that was published incorrectly. It is not an additional requirement and it does not change the AD number or its effective date.

Source: Federal Register document 98-5798, retrieved 2026-08-15

Read this correction on Federal Register (opens in a new tab)
Full official abstract

Airworthiness Directives; Teledyne Continental Motors IO-360, TSIO-360, LTSIO-360, IO-520, LIO-520, TSIO-520, LTSIO-520 Series, and Rolls-Royce plc IO-360 and TSIO-360 Series Reciprocating Engines

This amendment supersedes an existing airworthiness directive (AD), applicable to certain Teledyne Continental Motors (TCM) IO-520 and TSIO-520 series reciprocating engines, that currently requires ultrasonic inspection for subsurface fatigue cracks in crankshafts installed in TCM IO-520 and TSIO-520 series engines and replacement of the crankshaft if a crack is found. This amendment adds a requirement to remove crankshafts manufactured using the airmelt process and replace them with crankshafts manufactured using the vacuum arc remelt (VAR) process, incorporates new ultrasonic inspection criteria in the AD, adds engine series TCM IO-360, TSIO-360, LTSIO-360, IO-520, LIO- 520, TSIO-520, LTSIO-520 and Rolls-Royce, plc IO-360 and TSIO-360 to the applicability, and revises the economic impact analysis. This amendment is prompted by reports of crankshaft failures due to subsurface fatigue cracking on engines that had been inspected in accordance with the current AD. The actions specified by this AD are intended to prevent crankshaft failure and subsequent engine failure.

Source: Federal Register document 97-33142, retrieved 2026-08-15 · checked against the live Federal Register record on 2026-10-02

View on Federal Register (opens in a new tab) View this AD in FAA DRS (opens in a new tab) Print AD packet (opens the full Federal Register document in a new tab)
ADAD 95-08-10Teledyne Continental Motors (TCM) Model TSIO-360 and LTSIO-360 Engines1995-07-10Active
AD

95-08-10

FR doc 95-15151 · 60 FR 32581

AD 95-08-10Published 1995-06-23Effective 1995-07-10

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

Teledyne Continental Motors (TCM) Model TSIO-360 and LTSIO-360 Engines

Requires replacement of the suspect turbocharger check valves prior to further flight, and prohibits special flight permits.

Full official abstract

Airworthiness Directives; Teledyne Continental Motors (TCM) Model TSIO-360 and LTSIO-360 Engines

This document publishes in the Federal Register Airworthiness Directive (AD) 95-08-10 that was sent previously to all known U.S. owners and operators of Teledyne Continental Motors (TCM) Model TSIO- 360 E, EB, F, FB, G, GB, KB, LB, MB, and Model LTSIO-360 E, EB, and KB reciprocating engines by individual letters. This AD requires replacement of the suspect turbocharger check valves prior to further flight, and prohibits special flight permits. This amendment is prompted by three reported engine failures caused by incorrectly assembled turbocharger oil outlet check valves, resulting in an improperly expanded rivet that held the check valve flapper assembly together as one unit. The actions specified by this AD are intended to prevent complete engine failure due to an incorrectly assembled turbocharger oil outlet check valve.

Source: Federal Register document 95-15151, retrieved 2026-08-15 · checked against the live Federal Register record on 2026-10-01

View on Federal Register (opens in a new tab) View this AD in FAA DRS (opens in a new tab) Print AD packet (opens the full Federal Register document in a new tab)

Service Bulletins

64 records
SBSB25-01Inspection and Replacement of Part No. 652421 Nuts Used to Secure Engine Mount Legs to the Crankcase2025-03-10
SB

SB25-01

Continental Aerospace Technologies

Issued 2025-03-10

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

Inspection and Replacement of Part No. 652421 Nuts Used to Secure Engine Mount Legs to the Crankcase

Applies to Continental IO-360Continental IO-520Continental IO-550Continental O-470

Source: Continental Aerospace Technologies, retrieved 2026-08-16 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBMSB23-01ACrankshaft counterweights2023-02-13
SB

MSB23-01A

Continental Aerospace Technologies

Issued 2023-02-13

Manufacturer document

Manufacturer's own classification: “Mandatory Service Bulletin”. The manufacturer's classification is not an FAA requirement.

Manufacturer document; legal obligations depend on applicable requirements.

Crankshaft counterweights

Applies to Continental IO-360Continental IO-520Continental IO-550Continental O-470

Source: Continental Aerospace Technologies, retrieved 2026-08-16 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBSB20-03ENGINE PRESERVATION DURING COVID-19 PANDEMIC2020-04-13
SB

SB20-03

Continental Aerospace Technologies

Issued 2020-04-13

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

ENGINE PRESERVATION DURING COVID-19 PANDEMIC

Applies to Continental C-85Continental C-90Continental E165/E185/E225Continental IO-360Continental IO-520Continental IO-550Continental O-200Continental O-300Continental O-470

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBSB19-09CHAMPION AEROSPACE SLICK SERVICE BULLETIN SB2-192019-12-13
SB

SB19-09

Continental Aerospace Technologies

Issued 2019-12-13

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

CHAMPION AEROSPACE SLICK SERVICE BULLETIN SB2-19

Applies to Continental IO-360Continental IO-520Continental IO-550Continental O-200Continental O-470

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBSB19-07CRANKSHAFT END PLAY CHECK2019-12-10
SB

SB19-07

Continental Aerospace Technologies

Issued 2019-12-10

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

CRANKSHAFT END PLAY CHECK

Applies to Continental IO-360Continental IO-520Continental IO-550Continental O-200Continental O-470

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBCSB19-01AFUEL (PRIMER) DIVERTER VALVE ASSEMBLY2019-12-05
SB

CSB19-01A

Continental Aerospace Technologies

Issued 2019-12-05

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

FUEL (PRIMER) DIVERTER VALVE ASSEMBLY

Applies to Continental IO-360

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBSB19-02ACHAMPION AEROSPACE SLICK SERVICE BULLETIN SB1-192019-04-22
SB

SB19-02A

Continental Aerospace Technologies

Issued 2019-04-22

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

CHAMPION AEROSPACE SLICK SERVICE BULLETIN SB1-19

Applies to Continental IO-360Continental IO-520Continental IO-550Continental O-200Continental O-470

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBSB17-06CONNECTING ROD BOLT, (P/N 655959) AND CRANKCASE CLEARANCE INSPECTION2017-10-20
SB

SB17-06

Continental Aerospace Technologies

Issued 2017-10-20

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

CONNECTING ROD BOLT, (P/N 655959) AND CRANKCASE CLEARANCE INSPECTION

Applies to Continental IO-360

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBSB17-04CONTINENTAL MOTORS IGNITION SYSTEMS SERVICE BULETIN SB6702017-09-29
SB

SB17-04

Continental Aerospace Technologies

Issued 2017-09-29

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

CONTINENTAL MOTORS IGNITION SYSTEMS SERVICE BULETIN SB670

Applies to Continental IO-360Continental IO-520Continental IO-550Continental O-200Continental O-300Continental O-470

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBSB17-05CONTINENTAL MOTORS IGNITION SYSTEMS SERVICE BULLETIN SB643C2017-09-29
SB

SB17-05

Continental Aerospace Technologies

Issued 2017-09-29

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

CONTINENTAL MOTORS IGNITION SYSTEMS SERVICE BULLETIN SB643C

Applies to Continental IO-360Continental IO-520Continental IO-550Continental O-200Continental O-300Continental O-470

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBSB13-4CANEROID EQUIPPED FUEL PUMPS2016-11-07
SB

SB13-4C

Continental Aerospace Technologies

Issued 2016-11-07

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

ANEROID EQUIPPED FUEL PUMPS

Applies to Continental IO-360Continental IO-550

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBCSB97-10BPISTON PIN PLUG WEAR2016-07-27
SB

CSB97-10B

Continental Aerospace Technologies

Issued 2016-07-27

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

PISTON PIN PLUG WEAR

Applies to Continental E165/E185/E225Continental IO-360Continental IO-520Continental IO-550Continental O-470

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBCSB98-1CINTAKE AND EXHAUST VALVE INSPECTION.2016-07-27
SB

CSB98-1C

Continental Aerospace Technologies

Issued 2016-07-27

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

INTAKE AND EXHAUST VALVE INSPECTION.

Applies to Continental C-85Continental C-90Continental E165/E185/E225Continental IO-360Continental IO-520Continental IO-550Continental O-200Continental O-300Continental O-470

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBSB08-4AFUEL INJECTION SYSTEM CONTAMINATION2016-07-27
SB

SB08-4A

Continental Aerospace Technologies

Issued 2016-07-27

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

FUEL INJECTION SYSTEM CONTAMINATION

Applies to Continental IO-360Continental IO-520Continental O-470

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBSB95-7AMANIFOLD VALVE COVER INSPECTION2016-06-20
SB

SB95-7A

Continental Aerospace Technologies

Issued 2016-06-20

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

MANIFOLD VALVE COVER INSPECTION

Applies to Continental IO-360Continental IO-520Continental IO-550

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBCSB14-1ACYLINDER BARREL FIN INSPECTION2016-06-16
SB

CSB14-1A

Continental Aerospace Technologies

Issued 2016-06-16

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

CYLINDER BARREL FIN INSPECTION

Applies to Continental IO-360

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBCSB95-4AINTAKE VALVE GUIDE SEAL P/N 646678 INSPECTION2016-06-16
SB

CSB95-4A

Continental Aerospace Technologies

Issued 2016-06-16

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

INTAKE VALVE GUIDE SEAL P/N 646678 INSPECTION

Applies to Continental IO-360

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBSB99-8BENGINE FUEL INJECTION SYSTEM PRESERVATION2016-06-16
SB

SB99-8B

Continental Aerospace Technologies

Issued 2016-06-16

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

ENGINE FUEL INJECTION SYSTEM PRESERVATION

Applies to Continental IO-360Continental IO-520Continental IO-550

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBSB15-5CHAMPION AEROSPACE SLICK SERVICE LETTER SL NO. 4300/6300-74-20-0012015-10-06
SB

SB15-5

Continental Aerospace Technologies

Issued 2015-10-06

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

CHAMPION AEROSPACE SLICK SERVICE LETTER SL NO. 4300/6300-74-20-001

Applies to Continental IO-360Continental IO-520Continental IO-550Continental O-470

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBMSB96-10BCRANKSHAFT ULTRASONIC INSPECTION2015-08-10
SB

MSB96-10B

Continental Aerospace Technologies

Issued 2015-08-10

Manufacturer document

Manufacturer's own classification: “Mandatory Service Bulletin”. The manufacturer's classification is not an FAA requirement.

Manufacturer document; legal obligations depend on applicable requirements.

CRANKSHAFT ULTRASONIC INSPECTION

Applies to Continental IO-360Continental IO-520Continental IO-550Continental O-470

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBCSB08-3CTHROTTLE AND MIXTURE CONTROL LEVERS2013-07-17
SB

CSB08-3C

Continental Aerospace Technologies

Issued 2013-07-17

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

THROTTLE AND MIXTURE CONTROL LEVERS

Applies to Continental C-85Continental C-90Continental E165/E185/E225Continental IO-360Continental IO-520Continental IO-550Continental O-200Continental O-300Continental O-470

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBMSB00-6DSLICK SERVICE BULLETIN SB1-00C2010-11-19
SB

MSB00-6D

Continental Aerospace Technologies

Issued 2010-11-19

Manufacturer document

Manufacturer's own classification: “Mandatory Service Bulletin”. The manufacturer's classification is not an FAA requirement.

Manufacturer document; legal obligations depend on applicable requirements.

SLICK SERVICE BULLETIN SB1-00C

Applies to Continental IO-360Continental O-300

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBMSB94-8DMAGNETO TO ENGINE TIMING2010-02-17
SB

MSB94-8D

Continental Aerospace Technologies

Issued 2010-02-17

Manufacturer document

Manufacturer's own classification: “Mandatory Service Bulletin”. The manufacturer's classification is not an FAA requirement.

Manufacturer document; legal obligations depend on applicable requirements.

MAGNETO TO ENGINE TIMING

Applies to Continental C-85Continental C-90Continental E165/E185/E225Continental IO-360Continental IO-520Continental IO-550Continental O-200Continental O-300Continental O-470

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBMSB09-8AINSPECTION AND REMOVAL OF CERTAIN TCM ENGINE HYDRAULIC LIFTERS2009-12-04
SB

MSB09-8A

Continental Aerospace Technologies

Issued 2009-12-04

Manufacturer document

Manufacturer's own classification: “Mandatory Service Bulletin”. The manufacturer's classification is not an FAA requirement.

Manufacturer document; legal obligations depend on applicable requirements.

INSPECTION AND REMOVAL OF CERTAIN TCM ENGINE HYDRAULIC LIFTERS

Applies to Continental IO-360Continental IO-520Continental IO-550Continental O-470

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBSB09-14CRANKSHAFT CORROSION TREATMENT2009-10-29
SB

SB09-14

Continental Aerospace Technologies

Issued 2009-10-29

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

CRANKSHAFT CORROSION TREATMENT

Applies to Continental C-85Continental C-90Continental E165/E185/E225Continental IO-360Continental IO-520Continental IO-550Continental O-200Continental O-300Continental O-470

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBSB06-5CRANKSHAFT OIL TRANSFER TUBE INSPECTION AND REPLACEMENT2006-05-25
SB

SB06-5

Continental Aerospace Technologies

Issued 2006-05-25

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

CRANKSHAFT OIL TRANSFER TUBE INSPECTION AND REPLACEMENT

Applies to Continental E165/E185/E225Continental IO-360Continental IO-520Continental IO-550Continental O-300Continental O-470

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBSB05-9SLICK SERVICE BULLETIN SB1-88B2005-10-17
SB

SB05-9

Continental Aerospace Technologies

Issued 2005-10-17

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

SLICK SERVICE BULLETIN SB1-88B

Applies to Continental C-85Continental C-90Continental E165/E185/E225Continental IO-360Continental IO-520Continental IO-550Continental O-200Continental O-300Continental O-470

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBSB04-10PISTON POSITION MARKING2004-10-26
SB

SB04-10

Continental Aerospace Technologies

Issued 2004-10-26

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

PISTON POSITION MARKING

Applies to Continental C-85Continental C-90Continental E165/E185/E225Continental IO-360Continental IO-520Continental IO-550Continental O-200Continental O-300Continental O-470

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBCSB04-5ATELEDYNE CONTINENTAL MOTORS IGNITION SYSTEMS CRITICAL SERVICE BULLETIN CSB665A2004-08-20
SB

CSB04-5A

Continental Aerospace Technologies

Issued 2004-08-20

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

TELEDYNE CONTINENTAL MOTORS IGNITION SYSTEMS CRITICAL SERVICE BULLETIN CSB665A

Applies to Continental C-85Continental C-90Continental E165/E185/E225Continental IO-360Continental IO-520Continental IO-550Continental O-200Continental O-300Continental O-470

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBCSB02-8TELEDYNE CONTINENTAL MOTORS IGNITION SYSTEM CRITICAL SERVICE BULLETIN CSB664.2002-09-06
SB

CSB02-8

Continental Aerospace Technologies

Issued 2002-09-06

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

TELEDYNE CONTINENTAL MOTORS IGNITION SYSTEM CRITICAL SERVICE BULLETIN CSB664.

Applies to Continental C-85Continental C-90Continental E165/E185/E225Continental IO-360Continental IO-520Continental IO-550Continental O-200Continental O-300Continental O-470

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBSB02-7TELEDYNE CONTINENTAL MOTORS IGNITION SYSTEM SERVICE BULLETIN SB663.2002-06-28
SB

SB02-7

Continental Aerospace Technologies

Issued 2002-06-28

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

TELEDYNE CONTINENTAL MOTORS IGNITION SYSTEM SERVICE BULLETIN SB663.

Applies to Continental IO-360

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBSB01-5STARTER ADAPTER BEVEL GEAR INSPECTION2001-10-18
SB

SB01-5

Continental Aerospace Technologies

Issued 2001-10-18

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

STARTER ADAPTER BEVEL GEAR INSPECTION

Applies to Continental IO-360

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBMSB00-5DCRANKSHAFT MATERIAL INSPECTION.2001-10-17
SB

MSB00-5D

Continental Aerospace Technologies

Issued 2001-10-17

Manufacturer document

Manufacturer's own classification: “Mandatory Service Bulletin”. The manufacturer's classification is not an FAA requirement.

Manufacturer document; legal obligations depend on applicable requirements.

CRANKSHAFT MATERIAL INSPECTION.

Applies to Continental IO-360Continental IO-520Continental IO-550

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBCSB01-1FUEL PUMP INSPECTION AND SEAL LEAK TEST2001-04-25
SB

CSB01-1

Continental Aerospace Technologies

Issued 2001-04-25

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

FUEL PUMP INSPECTION AND SEAL LEAK TEST

Applies to Continental IO-360Continental IO-520Continental IO-550

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBSB00-10FUEL PUMP SEAL P/N 649198.2000-12-19
SB

SB00-10

Continental Aerospace Technologies

Issued 2000-12-19

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

FUEL PUMP SEAL P/N 649198.

Applies to Continental IO-360Continental IO-520Continental IO-550Continental O-470

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBSB00-4AAUSTRALIAN AVGAS CONTAMINATION.2000-03-07
SB

SB00-4A

Continental Aerospace Technologies

Issued 2000-03-07

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

AUSTRALIAN AVGAS CONTAMINATION.

Applies to Continental C-85Continental C-90Continental E165/E185/E225Continental IO-360Continental IO-520Continental IO-550Continental O-200Continental O-300Continental O-470

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBSB98-8NUMBER ONE AND THREE CYLINDER INTAKE TUBE MODIFICATION.1998-10-22
SB

SB98-8

Continental Aerospace Technologies

Issued 1998-10-22

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

NUMBER ONE AND THREE CYLINDER INTAKE TUBE MODIFICATION.

Applies to Continental IO-360

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBSB97-15TCM IGNITION SYSTEM SERVICE BULLETIN SB660.1997-12-05
SB

SB97-15

Continental Aerospace Technologies

Issued 1997-12-05

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

TCM IGNITION SYSTEM SERVICE BULLETIN SB660.

Applies to Continental C-85Continental C-90Continental E165/E185/E225Continental IO-360Continental IO-520Continental IO-550Continental O-200Continental O-300Continental O-470

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBCSB96-13IO-360, TSIO-360 AND LTSIO-360 SERIES ENGINE CONNECTING ROD INSPECTION AND REPLACEMENT.1996-11-14
SB

CSB96-13

Continental Aerospace Technologies

Issued 1996-11-14

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

IO-360, TSIO-360 AND LTSIO-360 SERIES ENGINE CONNECTING ROD INSPECTION AND REPLACEMENT.

Applies to Continental IO-360

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBCSB96-8REPLACEMENT OF AIRMELT (NON-VAR) CRANKSHAFTS1996-06-25
SB

CSB96-8

Continental Aerospace Technologies

Issued 1996-06-25

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

REPLACEMENT OF AIRMELT (NON-VAR) CRANKSHAFTS

Applies to Continental IO-360Continental IO-520

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBSB96-4IMPROVED OIL PUMP GEARS AND SUCTION SCREENS1996-04-12
SB

SB96-4

Continental Aerospace Technologies

Issued 1996-04-12

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

IMPROVED OIL PUMP GEARS AND SUCTION SCREENS

Applies to Continental IO-360Continental O-300

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBCSB96-5OIL PUMP DRIVE GEARS, P/N 649506 AND 6496811996-04-11
SB

CSB96-5

Continental Aerospace Technologies

Issued 1996-04-11

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

OIL PUMP DRIVE GEARS, P/N 649506 AND 649681

Applies to Continental IO-360Continental O-300

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBCSB94-1TELEDYNE CONTINENTAL MOTORS IGNITION SYSTEMS SERVICE BULLETIN – NO. CSB6411994-02-01
SB

CSB94-1

Continental Aerospace Technologies

Issued 1994-02-01

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

TELEDYNE CONTINENTAL MOTORS IGNITION SYSTEMS SERVICE BULLETIN – NO. CSB641

Applies to Continental C-85Continental C-90Continental E165/E185/E225Continental IO-360Continental IO-520Continental IO-550Continental O-200Continental O-300Continental O-470

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBMSB93-12VALVE RETAINER KEY INSTALLATION INSPECTION1993-05-12
SB

MSB93-12

Continental Aerospace Technologies

Issued 1993-05-12

Manufacturer document

Manufacturer's own classification: “Mandatory Service Bulletin”. The manufacturer's classification is not an FAA requirement.

Manufacturer document; legal obligations depend on applicable requirements.

VALVE RETAINER KEY INSTALLATION INSPECTION

Applies to Continental IO-360Continental IO-520Continental IO-550Continental O-200Continental O-300Continental O-470

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBM93-10TCM IGNITION SYSTEMS SERVICE BULLETIN NO. 6391993-03-01
SB

M93-10

Continental Aerospace Technologies

Issued 1993-03-01

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

TCM IGNITION SYSTEMS SERVICE BULLETIN NO. 639

Applies to Continental C-85Continental C-90Continental E165/E185/E225Continental IO-360Continental IO-520Continental IO-550Continental O-200Continental O-300Continental O-470

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBM93-8ROCKER ARM TO ROTOCOIL CLEARANCE1993-02-19
SB

M93-8

Continental Aerospace Technologies

Issued 1993-02-19

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

ROCKER ARM TO ROTOCOIL CLEARANCE

Applies to Continental E165/E185/E225Continental IO-360Continental IO-520Continental IO-550Continental O-470

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBM93-4CRANKSHAFT COUNTERWEIGHTS1993-02-12
SB

M93-4

Continental Aerospace Technologies

Issued 1993-02-12

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

CRANKSHAFT COUNTERWEIGHTS

Applies to Continental E165/E185/E225Continental IO-360Continental IO-520Continental IO-550Continental O-470

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBM92-10STARTER ADAPTER1992-08-14
SB

M92-10

Continental Aerospace Technologies

Issued 1992-08-14

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

STARTER ADAPTER

Applies to Continental IO-360Continental IO-520Continental IO-550Continental O-300Continental O-470

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBM92-7CRANKCASE CYLINDER DECK STUDS1992-05-26
SB

M92-7

Continental Aerospace Technologies

Issued 1992-05-26

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

CRANKCASE CYLINDER DECK STUDS

Applies to Continental IO-360Continental IO-520Continental IO-550Continental O-470

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBM92-4R1IO AND L/TSIO360 ROCKER SHAFT STUD INSPECTION1992-02-05
SB

M92-4R1

Continental Aerospace Technologies

Issued 1992-02-05

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

IO AND L/TSIO360 ROCKER SHAFT STUD INSPECTION

Applies to Continental IO-360

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBM91-4PISTON IDENTIFICATION AND PISTON RING APPLICATION BULLETIN1991-02-11
SB

M91-4

Continental Aerospace Technologies

Issued 1991-02-11

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

PISTON IDENTIFICATION AND PISTON RING APPLICATION BULLETIN

Applies to Continental C-85Continental C-90Continental E165/E185/E225Continental IO-360Continental IO-520Continental IO-550Continental O-200Continental O-300Continental O-470

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBM90-13EXHAUST VALVE STEM CORROSION/EROSION1990-07-16
SB

M90-13

Continental Aerospace Technologies

Issued 1990-07-16

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

EXHAUST VALVE STEM CORROSION/EROSION

Applies to Continental C-85Continental C-90Continental E165/E185/E225Continental IO-360Continental IO-520Continental IO-550Continental O-200Continental O-300Continental O-470

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBM89-18EXHAUST GAS TEMPERATURE (E.G.T.) RECOMMENDATIONS FOR STANDARD ENGINES ( LEANING LEAN )1989-08-10
SB

M89-18

Continental Aerospace Technologies

Issued 1989-08-10

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

EXHAUST GAS TEMPERATURE (E.G.T.) RECOMMENDATIONS FOR STANDARD ENGINES ( LEANING LEAN )

Applies to Continental C-85Continental C-90Continental E165/E185/E225Continental IO-360Continental IO-520Continental IO-550Continental O-200Continental O-300Continental O-470

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBM88-4TCM PRO-TECH OIL FILTER1988-01-15
SB

M88-4

Continental Aerospace Technologies

Issued 1988-01-15

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

TCM PRO-TECH OIL FILTER

Applies to Continental IO-360Continental IO-520Continental IO-550Continental O-470

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBM87-23CRANKSHAFT COUNTERWEIGHT IDENTIFICATION AT OVERHAUL1987-11-24
SB

M87-23

Continental Aerospace Technologies

Issued 1987-11-24

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

CRANKSHAFT COUNTERWEIGHT IDENTIFICATION AT OVERHAUL

Applies to Continental E165/E185/E225Continental IO-360Continental IO-520Continental IO-550Continental O-300Continental O-470

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBM87-16SLICK SERVICE BULLETIN SB1-86A1987-08-14
SB

M87-16

Continental Aerospace Technologies

Issued 1987-08-14

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

SLICK SERVICE BULLETIN SB1-86A

Applies to Continental C-85Continental C-90Continental E165/E185/E225Continental IO-360Continental IO-520Continental IO-550Continental O-200Continental O-300Continental O-470

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBM87-8EXHAUST VALVE INSPECTION1987-02-26
SB

M87-8

Continental Aerospace Technologies

Issued 1987-02-26

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

EXHAUST VALVE INSPECTION

Applies to Continental IO-360

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBM83-5SLICK SERVICE BULLETIN 3-821983-03-07
SB

M83-5

Continental Aerospace Technologies

Issued 1983-03-07

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

SLICK SERVICE BULLETIN 3-82

Applies to Continental C-90Continental IO-360Continental IO-520Continental O-200Continental O-470

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBM81-23R1360 SERIES OIL PUMP DRIVE GEAR1982-02-12
SB

M81-23R1

Continental Aerospace Technologies

Issued 1982-02-12

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

360 SERIES OIL PUMP DRIVE GEAR

Applies to Continental IO-360

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBM81-13R1SLICK SERVICE BULLETIN 1-81 (REVISED)1981-07-18
SB

M81-13R1

Continental Aerospace Technologies

Issued 1981-07-18

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

SLICK SERVICE BULLETIN 1-81 (REVISED)

Applies to Continental C-85Continental C-90Continental IO-360Continental IO-520Continental O-200

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBM77-9THRU BOLT CHANGE1977-03-16
SB

M77-9

Continental Aerospace Technologies

Issued 1977-03-16

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

THRU BOLT CHANGE

Applies to Continental IO-360Continental IO-520

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBM75-6R1CONVERSION OF ENGINES FROM ONE MODEL TO ANOTHER1975-06-04
SB

M75-6R1

Continental Aerospace Technologies

Issued 1975-06-04

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

CONVERSION OF ENGINES FROM ONE MODEL TO ANOTHER

Applies to Continental C-85Continental C-90Continental E165/E185/E225Continental IO-360Continental IO-520Continental IO-550Continental O-200Continental O-300Continental O-470

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBM74-18COMPLIANCE WITH SLICK BULLETIN 1-741974-09-16
SB

M74-18

Continental Aerospace Technologies

Issued 1974-09-16

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

COMPLIANCE WITH SLICK BULLETIN 1-74

Applies to Continental C-85Continental C-90Continental E165/E185/E225Continental IO-360Continental IO-520Continental IO-550Continental O-200Continental O-300Continental O-470

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBM64-18FIELD CONVERSION TO TURBOCHARGING OF CONTINENTAL AIRCRAFT ENGINES1968-10-07
SB

M64-18

Continental Aerospace Technologies

Issued 1968-10-07

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

FIELD CONVERSION TO TURBOCHARGING OF CONTINENTAL AIRCRAFT ENGINES

Applies to Continental C-85Continental C-90Continental E165/E185/E225Continental IO-360Continental IO-520Continental IO-550Continental O-200Continental O-300Continental O-470

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)

Service Instructions

13 records
SBSIL00-7COIL GAGE ROD APPLICATION2019-08-07
SI

SIL00-7C

Continental Aerospace Technologies

Issued 2019-08-07

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

OIL GAGE ROD APPLICATION

Applies to Continental C-85Continental C-90Continental E165/E185/E225Continental IO-360Continental IO-520Continental IO-550Continental O-200Continental O-300Continental O-470

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBSIL18-06ASUPERSEDING MAGNETO AND HARNESS APPLICATIONS2019-04-10
SI

SIL18-06A

Continental Aerospace Technologies

Issued 2019-04-10

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

SUPERSEDING MAGNETO AND HARNESS APPLICATIONS

Applies to Continental IO-360Continental IO-520Continental IO-550Continental O-200

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBSIL16-1AOPTIONAL 24V STARTERS2018-05-29
SI

SIL16-1A

Continental Aerospace Technologies

Issued 2018-05-29

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

OPTIONAL 24V STARTERS

Applies to Continental IO-360Continental IO-550

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBSIL18-02APPLICABILITY OF CMI SERVICE DOCUMENTS2018-02-15
SI

SIL18-02

Continental Aerospace Technologies

Issued 2018-02-15

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

APPLICABILITY OF CMI SERVICE DOCUMENTS

Applies to Continental C-85Continental C-90Continental E165/E185/E225Continental IO-360Continental IO-520Continental IO-550Continental O-200Continental O-300Continental O-470

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBSIL04-2ACYLINDER BARREL ULTRASONIC INSPECTION2016-07-27
SI

SIL04-2A

Continental Aerospace Technologies

Issued 2016-07-27

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

CYLINDER BARREL ULTRASONIC INSPECTION

Applies to Continental C-85Continental C-90Continental E165/E185/E225Continental IO-360Continental IO-520Continental IO-550Continental O-200Continental O-300Continental O-470

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBSIL15-9REMOTE MOUNTED OIL COOLERS2015-12-11
SI

SIL15-9

Continental Aerospace Technologies

Issued 2015-12-11

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

REMOTE MOUNTED OIL COOLERS

Applies to Continental IO-360Continental O-200Continental O-300Continental O-470

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBSIL15-8FRONT MOUNTED ALTERNATOR BRACKET ASSEMBLY INSPECTION2015-11-30
SI

SIL15-8

Continental Aerospace Technologies

Issued 2015-11-30

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

FRONT MOUNTED ALTERNATOR BRACKET ASSEMBLY INSPECTION

Applies to Continental IO-360

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBSIL05-3AENGINE SPECIFICATION NUMBERS2014-04-10
SI

SIL05-3A

Continental Aerospace Technologies

Issued 2014-04-10

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

ENGINE SPECIFICATION NUMBERS

Applies to Continental IO-360Continental IO-520Continental IO-550Continental O-200Continental O-300Continental O-470

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBSSI13-5AMPLIFIED OPERATION, MAINTENANCE AND SERVICING REQUIREMENTS FOR CIRRUS SR-20 AIRCRAFT OPERATED BY CIVIL AVIATION FLIGHT UNIVERSITY OF CHINA (CAFUC) ONLY2013-10-03
SI

SSI13-5

Continental Aerospace Technologies

Issued 2013-10-03

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

AMPLIFIED OPERATION, MAINTENANCE AND SERVICING REQUIREMENTS FOR CIRRUS SR-20 AIRCRAFT OPERATED BY CIVIL AVIATION FLIGHT UNIVERSITY OF CHINA (CAFUC) ONLY

Applies to Continental IO-360

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBSID10-4ENGINE MAINTENANCE FOR VOLCANIC ASH CONTAMINATION2010-07-12
SI

SID10-4

Continental Aerospace Technologies

Issued 2010-07-12

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

ENGINE MAINTENANCE FOR VOLCANIC ASH CONTAMINATION

Applies to Continental C-85Continental C-90Continental E165/E185/E225Continental IO-360Continental IO-520Continental IO-550Continental O-200Continental O-300Continental O-470

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBSIL97-1AIRWORTHINESS LIMITATIONS1997-01-03
SI

SIL97-1

Continental Aerospace Technologies

Issued 1997-01-03

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

AIRWORTHINESS LIMITATIONS

Applies to Continental C-85Continental C-90Continental E165/E185/E225Continental IO-360Continental IO-520Continental IO-550Continental O-200Continental O-300Continental O-470

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBSID96-6TCM IGNITION SYSTEMS SERVICE BULLETIN SB653.1996-05-03
SI

SID96-6

Continental Aerospace Technologies

Issued 1996-05-03

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

TCM IGNITION SYSTEMS SERVICE BULLETIN SB653.

Applies to Continental C-85Continental C-90Continental E165/E185/E225Continental IO-360Continental IO-520Continental IO-550Continental O-200Continental O-300Continental O-470

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)
SBSIL93-14CFC WARNING STATEMENT1993-08-24
SI

SIL93-14

Continental Aerospace Technologies

Issued 1993-08-24

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

CFC WARNING STATEMENT

Applies to Continental C-85Continental C-90Continental E165/E185/E225Continental IO-360Continental IO-520Continental IO-550Continental O-200Continental O-300Continental O-470

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (opens in a new tab)

A manufacturer bulletin is not an FAA rule; applicable ADs, binding Airworthiness Limitations or other governing requirements can require compliance; our bulletin content comprises number, title, date and applicability, with manufacturer attribution and a source link; the manufacturer’s document controls over our Record, subject to governing law; bulletin copyright remains with the manufacturer or other rights holder.

View on Continental Aerospace Technologies' site (opens in a new tab)

This page indexes 15 ADs and 77 SBs from primary sources. The FAA may have issued additional directives for this engine that are not yet included.

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