Engine model

Continental O-300

Continental Aerospace Technologies

Airworthiness Directives
5
Manufacturer bulletins
5041 Service Bulletins, 9 Service Instructions
Last live check
2026-10-025 of 5 re-checked, oldest 2026-10-01
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.

Also known as: C145

Save this engine

What directives and bulletins apply to the Continental O-300

The FAA has published 5 Airworthiness Directives that name the Continental O-300 (Continental Aerospace Technologies), the earliest in 1996 and the newest on 2023-09-21. The index also holds 1 correction notice for an earlier directive. 50 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 2022-04-04 Airworthiness Directives; Continental Aerospace Technologies, Inc. and Continental Motors ... 2022-02-22
  3. AD 2011-26-07 Airworthiness Directives; Teledyne Continental Motors (TCM) and Rolls-Royce Motors Ltd. (R... 2011-12-20

See all 5 directives

Bulletins that matter

  1. SB SB00-12A Instructions for Continued Airworthiness (ICAs) for Continental Engine Models Manufactured... Open the bulletin
  2. SB SB20-06 HYDRAULIC LIFTER ASSEMBLIES Open the bulletin
  3. SB SB20-03 ENGINE PRESERVATION DURING COVID-19 PANDEMIC Open the bulletin
  4. SI SIL00-7C OIL GAGE ROD APPLICATION Open the bulletin
  5. SI SIL18-02 APPLICABILITY OF CMI SERVICE DOCUMENTS 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

5 records · 1 correction attached · 1 superseded record nested above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

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

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

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

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

ADAD 94-05-05 R1Teledyne Continental Motors Models C75, C85, C90, C125, C145, O-200, O-300, and GO-300 Series and Rolls-Royce, plc C90, O-200 and O-300 Series Reciprocating Engines1996-02-13Active
AD

94-05-05 R1

FR doc 96-1409 · 61 FR 2708

AD 94-05-05 R1Published 1996-01-29Effective 1996-02-13

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 Models C75, C85, C90, C125, C145, O-200, O-300, and GO-300 Series and Rolls-Royce, plc C90, O-200 and O-300 Series Reciprocating Engines

Requires inspection of the cylinder rocker shaft bosses for cracks, and inspection of the cylinder rocker shaft for looseness and replacement, if necessary, with a serviceable part.

Full official abstract

Airworthiness Directives; Teledyne Continental Motors Models C75, C85, C90, C125, C145, O-200, O-300, and GO-300 Series and Rolls-Royce, plc C90, O-200 and O-300 Series Reciprocating Engines

This amendment revises an existing airworthiness directive (AD), applicable to Teledyne Continental Motors (TCM) Models C75, C85, C90, C125, C145, O-200, O-300, and GO-300 series reciprocating engines, that currently requires inspection of the cylinder rocker shaft bosses for cracks, and inspection of the cylinder rocker shaft for looseness and replacement, if necessary, with a serviceable part. This amendment clarifies that the inspection must be accomplished at the next cylinder removal from the engine or engine overhaul, whichever occurs first, and adds certain Rolls-Royce, plc engines to the AD's applicability. This amendment is prompted by the need to clarify when the inspection must be performed. The actions specified by this AD are intended to prevent engine power loss and engine failure.

Source: Federal Register document 96-1409, retrieved 2026-08-15 · checked against the live Federal Register record on 2026-10-02

Service Bulletins

41 records
SBSB00-12AInstructions for Continued Airworthiness (ICAs) for Continental Engine Models Manufactured Under License by Rolls Royce2021-07-14
SB

SB00-12A

Continental Aerospace Technologies

Issued 2021-07-14

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

Instructions for Continued Airworthiness (ICAs) for Continental Engine Models Manufactured Under License by Rolls Royce

Applies to Continental C-90Continental O-200Continental O-300

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

SBSB20-06HYDRAULIC LIFTER ASSEMBLIES2020-12-14
SB

SB20-06

Continental Aerospace Technologies

Issued 2020-12-14

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (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.

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (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)

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)

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.

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (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.

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (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)

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.

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (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.

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

SBSB09-6AVOLARE’ CARBURETORS, LLC SB-5 REV A SERVICE BULLETIN2009-06-19
SB

SB09-6A

Continental Aerospace Technologies

Issued 2009-06-19

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

VOLARE’ CARBURETORS, LLC SB-5 REV A SERVICE BULLETIN

Applies to Continental C-85Continental C-90Continental O-200Continental O-300Continental O-470

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

SBSB09-3AVOLARE CARBURETORS, LLC SERVICE BULLETIN SB-2 REVISION A, REQUIRED REPLACEMENT OF FOAM FLOATS AND HOLLOW FLOATS2009-04-24
SB

SB09-3A

Continental Aerospace Technologies

Issued 2009-04-24

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

VOLARE CARBURETORS, LLC SERVICE BULLETIN SB-2 REVISION A, REQUIRED REPLACEMENT OF FOAM FLOATS AND HOLLOW FLOATS

Applies to Continental C-85Continental C-90Continental O-200Continental O-300Continental O-470

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

SBSB09-2VOLARE CARBURETORS, LLC SB1 SERVICE BULLETIN2009-03-17
SB

SB09-2

Continental Aerospace Technologies

Issued 2009-03-17

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

VOLARE CARBURETORS, LLC SB1 SERVICE BULLETIN

Applies to Continental C-85Continental C-90Continental O-200Continental O-300Continental O-470

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

SBSB08-1ROCKER SHAFT INSPECTION AND REPLACEMENT2008-02-05
SB

SB08-1

Continental Aerospace Technologies

Issued 2008-02-05

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

ROCKER SHAFT INSPECTION AND REPLACEMENT

Applies to Continental O-200Continental O-300

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (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.

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (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.

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (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.

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (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.

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (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.

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (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.

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (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.

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (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)

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)

SBCSB96-1STARTER GEAR AND CLUTCH ASSEMBLY P/N 6535751996-03-01
SB

CSB96-1

Continental Aerospace Technologies

Issued 1996-03-01

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

STARTER GEAR AND CLUTCH ASSEMBLY P/N 653575

Applies to Continental O-200Continental O-300

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (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.

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (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.

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (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.

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (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.

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

SBM92-8APPLICATION OF 4-1/6″ DIAMETER CYLINDER ASSEMBLIES1992-05-29
SB

M92-8

Continental Aerospace Technologies

Issued 1992-05-29

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

APPLICATION OF 4-1/6″ DIAMETER CYLINDER ASSEMBLIES

Applies to Continental C-85Continental C-90Continental O-200Continental O-300

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

SBM92-5PRECISION AIRMOTIVE CORPORATION MANDATORY SERVICE BULLETINS #MSA-1 REV. 1 AND MSA-2 REV. 11992-02-28
SB

M92-5

Continental Aerospace Technologies

Issued 1992-02-28

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.

PRECISION AIRMOTIVE CORPORATION MANDATORY SERVICE BULLETINS #MSA-1 REV. 1 AND MSA-2 REV. 1

Applies to Continental C-85Continental C-90Continental O-200Continental O-300Continental O-470

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (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.

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (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.

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (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.

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (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.

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (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.

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

SBM77-19INTAKE AND EXHAUST ROCKER ARM IDENTIFICATION AND APPLICATION1977-08-12
SB

M77-19

Continental Aerospace Technologies

Issued 1977-08-12

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

INTAKE AND EXHAUST ROCKER ARM IDENTIFICATION AND APPLICATION

Applies to Continental C-85Continental C-90Continental O-200Continental O-300

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (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.

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (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.

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

SBM73-13REAMING AND BUSHING ROCKER SHAFT BOSSES1973-07-10
SB

M73-13

Continental Aerospace Technologies

Issued 1973-07-10

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

REAMING AND BUSHING ROCKER SHAFT BOSSES

Applies to Continental C-85Continental C-90Continental O-200Continental O-300

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

SBM73-12MARVEL-SCHEBLER CARBURETOR BULLETIN A1-731973-06-08
SB

M73-12

Continental Aerospace Technologies

Issued 1973-06-08

Manufacturer document

Manufacturer document; legal obligations depend on applicable requirements.

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (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.

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

Service Instructions

9 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.

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (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.

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (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.

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (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.

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (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.

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (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.

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (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.

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (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.

Source: Continental Aerospace Technologies, retrieved 2026-09-01 · manufacturer page (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.

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

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