AD 2001-26-13

final rule
Data completeness: 80%

Airworthiness Directives; Pilatus Aircraft Ltd. Model PC-7 Airplanes

AD Number
2001-26-13
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2001-CE-30-AD
FR Citation
67 FR 1286

Applicability

TypeManufacturerModelDetails
aircraft Pilatus Aircraft Ltd Airworthiness Directives; Pilatus Aircraft Ltd. Model PC-7 Airplanes

Unsafe Condition

Insufficient clearance between the temperature-control lever mechanism and the landing-gear emergency-extension cable could result in damage to the emergency landing gear extension cable, or the cable could get caught on the temperature control lever.

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

Required Actions

Inspect the landing-gear emergency-extension cable for damage and replace if necessary; verify the correct installation of the bowden-cable conduit clamp and correct if necessary; modify the temperature-control lever mechanism.

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

Affected Aircraft

Pilatus Aircraft Ltd. Model PC-7 airplanes.

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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