AD 2014-16-01

final rule
Data completeness: 90%

Airworthiness Directives; MD Helicopters, Inc., Helicopters

AD Number
2014-16-01
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2014-0514
FR Citation
79 FR 45322

Applicability

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

Unsafe Condition

A cracked main rotor upper hub assembly (upper hub) could result in failure of the upper hub 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

Clean the upper hub inspection areas and perform an eddy current inspection of the upper hub for a crack. If a crack is found, replace the upper hub with an airworthy upper hub before further flight.

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

Compliance Time

Within the next 25 hours time-in-service (TIS) or at the next annual inspection, whichever occurs first.

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 900-00140, with main rotor upper hub assembly (upper hub) part number 900R2101006-105, -107, -109, or -111 installed, certificated in any category.

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

Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

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