AD 2003-14-51

final rule
Data completeness: 70%

Airworthiness Directives; MD Helicopters, Inc., Model MD900 Helicopters

AD Number
2003-14-51
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2003-SW-33-AD
FR Citation
68 FR 47211

Applicability

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

Unsafe Condition

Failure of a main rotor blade retention bolt (part number 900R3100001-103), leading to loss of a main rotor blade 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

Before further flight, remove, inspect, and reinstall each bolt. Replace any unairworthy bolt with an airworthy one. Perform visual checks and cam lever force inspections on bolts with 400 or more hours TIS. Disassemble, inspect, and reinstall each airworthy bolt within 30 days for those with 400 or more hours TIS, and before accumulating 400 hours TIS for those with less than 400 hours TIS. Replace any unairworthy bolt with an airworthy one before further flight.

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, all serial numbers, equipped with main rotor blade retention bolts (part number 900R3100001-103).

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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