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Airworthiness Directive

AD 95-22-04 60 FR 54421 Active

Federal Aviation Administration · 14 CFR part 39

Requires inspections to detect cracking of main landing gear (MLG) axles that have been reworked by chromium plating, and replacement of cracked axles.

Federal Register (opens in a new tab)

FR document
95-25990
Amendment
39-9411
Published
1995-10-24
Effective
1995-11-08
Models covered
1

Last live check: 2026-08-19

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AD

95-22-04

FR doc 95-25990 · 60 FR 54421

AD 95-22-04Published 1995-10-24Effective 1995-11-08

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

Requires inspections to detect cracking of main landing gear (MLG) axles that have been reworked by chromium plating, and replacement of cracked axles.

Full official abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain Canadair Model CL-215-1A10 and CL-215-6B11 series airplanes. This action requires inspections to detect cracking of main landing gear (MLG) axles that have been reworked by chromium plating, and replacement of cracked axles. This amendment is prompted by reports of fatigue cracking found on several MLG wheel axes that had been chromium-plated during rework. The actions specified in this AD are intended to prevent such cracking, which can result in failure of the axle, separation of the wheel from the aircraft, and consequent reduced controllability of the airplane during takeoff or landing.

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All Canadair CL-215 / CL-415 directives

View on Federal Register (opens in a new tab) Search DRS manually for AD 95-22-04 (opens in a new tab) Print AD packet (opens the full Federal Register document in a new tab)

Applies to 1 model in our index