Airworthiness Directive

AD 98-06-25 63 FR 13491 Active

Federal Aviation Administration · 14 CFR part 39

Requires inspecting the cargo door lower belt frames at the cargo latch receptacles for cracks in the belt frames, repairing any cracks, and reinforcing the cargo door lower belt frames by installing doublers.

FR document
98-6767
Amendment
39-10403
Published
1998-03-20
Effective
1998-04-27
Models covered
1

Last live check: 2026-10-04

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AD

98-06-25

FR doc 98-6767 · 63 FR 13491

AD 98-06-25Published 1998-03-20Effective 1998-04-27

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 inspecting the cargo door lower belt frames at the cargo latch receptacles for cracks in the belt frames, repairing any cracks, and reinforcing the cargo door lower belt frames by installing doublers.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to Fairchild Aircraft Inc. (Fairchild) Models SA226-AT, SA226- TC, SA227-AC, and SA227-AT airplanes. This action would require inspecting the cargo door lower belt frames at the cargo latch receptacles for cracks in the belt frames, repairing any cracks, and reinforcing the cargo door lower belt frames by installing doublers. The AD is the result of a decompression incident during flight caused by fatigue at the bottom of the cargo door on a Fairchild Model SA226- TC. The actions specified by this AD are intended to prevent the failure of the cargo door in flight, which could cause decompression injuries to passengers and substantial structural damage to the airplane.

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All Fairchild SA226/SA227 Metro directives

Applies to 1 model in our index