AD 2007-09-51

final rule
Data completeness: 70%

Airworthiness Directives; MD Helicopters, Inc., Model 369, YOH-6A, 369A, OH-6A, 369H, 369HM, 369HS, 369HE, 369D, 369E, 369F, and 369FF Helicopters

AD Number
2007-09-51
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2007-28449
FR Citation
72 FR 33642

Applicability

TypeManufacturerModelDetails
aircraft MD Various Airworthiness Directives; MD Helicopters, Inc., Model 369, YOH-6A, 369A, OH-6A, 369H, 369HM, 369HS, 369HE, 369D, 369E, 369F, and 369FF Helicopters

Unsafe Condition

Tail rotor blade root fitting failure due to a machining defect causing a sharp transition in the tapered end of the bore, which can lead to blade 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

Remove each affected tail rotor blade assembly, inspect the bore of the tail rotor blade root fitting using a bright light, replace any blade assembly that does not have a smooth radius, and identify each airworthy tail rotor blade assembly with the applicable helicopter model.

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 369, YOH-6A, 369A, OH-6A, 369H, 369HM, 369HS, 369HE, 369D, 369E, 369F, and 369FF helicopters, with tail rotor blade part numbers 369A1613, 369D21606, 369D21613, 369D21615, or 421-088 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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