AD 2004-22-12

final rule
Data completeness: 70%

Airworthiness Directives; MD Helicopters, Inc. Model 600N Helicopters

AD Number
2004-22-12
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2003-SW-51-AD
FR Citation
69 FR 63054

Applicability

TypeManufacturerModelDetails
aircraft MD Various Airworthiness Directives; MD Helicopters, Inc. Model 600N Helicopters

Unsafe Condition

Fatigue life of the fuselage Station 75 control support bracket assembly is shorter than originally analyzed, potentially leading to 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

Replace the control support bracket assembly, part number 369N2608-11, with an airworthy assembly, part number 600N2608-1, by the specified time limits. Revise the Limitations section of the maintenance manual to reflect the reduced life limits.

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

Compliance Time

No later than November 30, 2005, or by the time the helicopter reaches the hours time-in-service (TIS) listed in the chart, whichever occurs first.

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

Affected Aircraft

MD Helicopters, Inc. Model 600N helicopters with serial numbers prefixed by 'RN' and specific numbers listed, or any Model 600N helicopter with a yaw stability augmentation system (YSAS) installed and control support bracket assembly part number 369N2608-11 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

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