AD 62-11-01

final rule
Data completeness: 70%

GENERAL ELECTRIC Models CJ805-3, -3A, and -3B Engines

AD Number
62-11-01
Status
final_rule
Effective Date
Product Category
engine
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
engine General Electric Company CJ805-3 GENERAL ELECTRIC Models CJ805-3, -3A, and -3B Engines
engine General Electric Company CJ805-3A GENERAL ELECTRIC Models CJ805-3, -3A, and -3B Engines
engine General Electric Company CJ805-3B GENERAL ELECTRIC Models CJ805-3, -3A, and -3B Engines

Unsafe Condition

Thrust reverser actuating pump failure causing reverser inoperability and asymmetric power conditions during reverse thrust application on aircraft landing roll.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Replace GE P/N 105R684P5 or 105R684P6 thrust reverser actuating pumps with P/N 105R684P10, or modify existing pumps by reducing pump drive gear width and enlarging pump shaft oil seal vent per GE Service Bulletins (3B)78-1 and (3)78-16, then reidentify as P/N 105R684P10.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

at next engine overhaul

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

General Electric Models CJ805-3, -3A, and -3B engines equipped with GE P/N 105R684P5 or 105R684P6 thrust reverser actuating pumps.

AI-generated summary from the source AD text. Verify against the official source before acting.

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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