AD 2010-18-52

final rule
Data completeness: 70%

Airworthiness Directives; MD Helicopters, Inc. Model MD900 Helicopters

AD Number
2010-18-52
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2010-1126
FR Citation
75 FR 69862

Applicability

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

Unsafe Condition

Crack in the main rotor hub near the flex beam bolt hole locations, which could lead to hub failure 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

Visually inspect the main rotor hub for a crack, paying particular attention to the area of the 5 flex beam bolt hole locations. If a crack is found, replace the unairworthy hub with an airworthy hub before further flight. Report the finding to the Los Angeles Aircraft Certification Office within 10 days of finding the crack.

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

Compliance Time

Within 4 hours time-in-service

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

Affected Aircraft

MD Helicopters, Inc. Model MD900 helicopters with part numbers 900R2101008-103, -105, and -107.

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

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.