AD 2002-22-51

final rule
Data completeness: 70%

Airworthiness Directives; MD Helicopters, Inc. Model MD900 Helicopters

AD Number
2002-22-51
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2002-SW-50-AD
FR Citation
67 FR 76109

Applicability

TypeManufacturerModelDetails
aircraft MD Various Airworthiness Directives; MD Helicopters, Inc. Model MD900 Helicopters

Unsafe Condition

Cracking or pitting in the main rotor support static mast (mast) that could result in failure of the mast, separation of the main rotor, 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

Remove the main rotor drive shaft, inspect the top 1 inch of the inside diameter of the mast for cracks or pitting, and remove the mast from service if any are found. Remove the main rotor hub assembly and inspect the mast threads for cracks. If a flaw is found in the thread root area and cannot be determined as a crack, perform a magnetic particle inspection (wet fluorescent) for cracks.

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 MD900 helicopters, serial numbers 900-00008 through 900-00110, with a main rotor support static mast (mast), part number 900F2401021-101, installed.

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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