AD 87-18-12 R1

final rule
Data completeness: 70%

Airworthiness Directives; McDONNELL DOUGLAS HELICOPTER COMPANY (MDHC) (Hughes Helicopter, Inc.) Model 369D, 369E, 369F, and 369FF Helicopters

AD Number
87-18-12 R1
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft MD Helicopters, Inc. 369D Airworthiness Directives; McDONNELL DOUGLAS HELICOPTER COMPANY (MDHC) (Hughes Helicopter, Inc.) Model 369D, 369E, 369F, and 369FF Helicopters
aircraft MD Helicopters, Inc. 369E Airworthiness Directives; McDONNELL DOUGLAS HELICOPTER COMPANY (MDHC) (Hughes Helicopter, Inc.) Model 369D, 369E, 369F, and 369FF Helicopters
aircraft MD Helicopters, Inc. 369F Airworthiness Directives; McDONNELL DOUGLAS HELICOPTER COMPANY (MDHC) (Hughes Helicopter, Inc.) Model 369D, 369E, 369F, and 369FF Helicopters
aircraft MD Helicopters, Inc. 369FF Airworthiness Directives; McDONNELL DOUGLAS HELICOPTER COMPANY (MDHC) (Hughes Helicopter, Inc.) Model 369D, 369E, 369F, and 369FF Helicopters

Unsafe Condition

Possible loss of power to the main rotor due to metal particles in the main transmission, excessive noise or vibration in the main transmission, or vibrations in the aircraft not reducible by main rotor blade tracking and balancing procedures.

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

Required Actions

Perform dye penetrant and visual inspections on the output shaft assembly ring gear carriers per MDHC SIN DN-148.1/EN-36.1/FN-25.1. Remove from service output shafts with bulging/raised surfaces on upper disc or cracks on upper/lower disc surfaces. Install P/N 369D25132-3 ring gear carriers and reidentify main transmission as P/N 369D25100-505 to eliminate repetitive inspections.

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

Compliance Time

Prior to further flight after effective date (January 15, 1988) for helicopters with issues. For others: inspections within 100 hours (if over 200 hours TIS on ring gear carrier) or at 300 hours intervals from last inspection. Compliance required as indicated unless previously done.

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

Affected Aircraft

McDonnell Douglas Helicopter Company (MDHC) Models 369D, 369E, 369F, 369FF with main rotor transmission output shaft assembly ring gear carriers P/N 369D25132-BSC/-5 in main transmission assemblies P/N 369D25100-BSC/-501/-503.

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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