AD 99-25-08

final rule
Data completeness: 70%

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

AD Number
99-25-08
Status
final_rule
Effective Date
Product Category
aircraft
Docket
99-SW-71-AD
FR Citation
Federal Register: February 15, 2000 (Volume 65, Number ??)

Applicability

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

Unsafe Condition

Stress corrosion cracks in the thruster control cable conduit cap at the telescopic swivel end and relieved area could cause failure of the cap, leading to a fixed thruster condition and subsequent loss of normal anti-torque directional control.

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

Required Actions

Inspect the thruster control cable conduit cap at the telescopic swivel end within 5 hours time-in-service or before further flight after December 31, 1999. Inspect the cap at the relieved area within 100 hours time-in-service or before further flight after February 19, 2000. Replace unairworthy thruster cables if unacceptable cracks are found.

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

Compliance Time

Within 5 hours time-in-service or before further flight after December 31, 1999 (first inspection); within 100 hours time-in-service or before further flight after February 19, 2000 (second inspection)

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

Affected Aircraft

MD Helicopters Inc. Model 500N (serial numbers LN001-LN099) and Model 600N (serial numbers RN003-RN074) helicopters.

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

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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