AD 2011-14-05

final rule
Data completeness: 70%

Airworthiness Directives; MD Helicopters, Inc. Model MD900 Helicopters

AD Number
2011-14-05
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2011-0695
FR Citation
76 FR 41662

Applicability

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

Unsafe Condition

Incorrectly inserted flanged bushings in the main rotor lower hub assembly (lower hub) can result in local corrosion, leading to fatigue cracking.

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

Required Actions

Visually inspect the lower hub for a crack. If a crack is found, replace the lower hub with an airworthy lower hub before further flight. Perform an eddy current inspection of the lower hub if necessary.

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

Compliance Time

Within 100 hours time-in-service (TIS) or during the next annual inspection, whichever occurs first, unless the inspection was done within the last 200 hours TIS.

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

Affected Aircraft

MD Helicopters, Inc. Model MD900 helicopters with lower hubs having serial numbers beginning with 5009 (e.g., 5009-XXXX).

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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