Airworthiness Directive

AD 2023-04-08 88 FR 11383 Superseded

Federal Aviation Administration · 14 CFR part 39

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.

FR document
2023-03796
Amendment
39-22355
Published
2023-02-23
Effective
2023-02-23
Models covered
4

Last live check: 2026-08-19

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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Superseded by 2023-05-16

Supersedence is read from the Federal Register text of the newer AD — the FAA publishes no structured field for it — and names only ADs held in our index.

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.

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

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.

More directives for Continental IO-360

  1. AD 2023-17-04 Airworthiness Directives; Continental Aerospace Technologies, Inc. Engin... Effective 2023-10-26
  2. AD 2023-05-16 Airworthiness Directives; Continental Aerospace Technologies, Inc., Reci... Effective 2023-03-15
  3. AD 2022-16-03 Airworthiness Directives; Continental Aerospace Technologies, Inc., Lyco... Effective 2022-08-15
  4. AD 2022-04-04 Airworthiness Directives; Continental Aerospace Technologies, Inc. and C... Effective 2022-03-29
  5. AD 2013-21-02 Airworthiness Directives; Lycoming Engines and Continental Motors, Inc. ... Effective 2013-11-13

All Continental IO-360 directives

Applies to 4 models in our index