AD 2008-22-52

final rule
Data completeness: 80%

Airworthiness Directives; MD Helicopters, Inc. Model 500N and 600N Helicopters

AD Number
2008-22-52
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2008-1244
FR Citation
73 FR 72326
Supersedes
2008-18-52

Applicability

TypeManufacturerModelDetails
aircraft MD Various Airworthiness Directives; MD Helicopters, Inc. Model 500N and 600N Helicopters

Unsafe Condition

Failed adapter tubes may lead to loss of yaw control 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

Turn OFF the Yaw Stability Augmentation System (YSAS) switch. Install a placard limiting airspeed to 100 KIAS or V<INF>NE</INF>, whichever is less. Revise the limitations section of the Rotorcraft Flight Manual (RFM) to reflect the airspeed limitation. Replace adapter tubes without a production date code stamp with airworthy adapter tubes that have a production date code stamp.

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

Compliance Time

Before further flight and within 45 days.

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

Affected Aircraft

MD Helicopters, Inc. Model 500N and 600N helicopters with affected adapter tubes installed.

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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