AD 2002-13-05

final rule
Data completeness: 70%

Airworthiness Directives; MD Helicopters, Inc. Model 369D, 369E, 369F, and 369FF Helicopters

AD Number
2002-13-05
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2001-SW-40-AD
FR Citation
67 FR 43227

Applicability

TypeManufacturerModelDetails
aircraft MD Various Airworthiness Directives; MD Helicopters, Inc. Model 369D, 369E, 369F, and 369FF Helicopters

Unsafe Condition

Bolts of inadequate grip length were specified to attach the tail rotor gearbox to the tailboom, which could lead to loss of the tail rotor gearbox and subsequent loss of control of the helicopter.

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

Required Actions

Inspect the part number (P/N) of the bolts attaching the tail rotor gearbox to the tailboom. Replace any bolt with inadequate grip length with an airworthy bolt. Determine the number of bolt threads protruding from each nutplate and add an additional washer if more than four threads protrude.

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

Compliance Time

Before further flight.

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

Affected Aircraft

MD Helicopters, Inc. Model 369D, 369E, 369F, and 369FF helicopters with a tailboom modified according to Aerometals Supplemental Type Certificate (STC) SH5055NM or SH4801NM.

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

Source: Official FAA Source ↗

Retrieved: Apr 6, 2026

Rights: U.S. Government Public Domain

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