Airworthiness Directive

AD 98-26-17 63 FR 70641 Active

Federal Aviation Administration · 14 CFR part 39

FR document
98-33689
Amendment
39-10960
Published
1998-12-22
Effective
1999-02-05
Models covered
1
Last live check
2026-10-03
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AD

98-26-17

FR doc 98-33689 · 63 FR 70641

AD 98-26-17Published 1998-12-22Effective 1999-02-05

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 accomplishing both a routine visual inspection and either a detailed visual inspection or x-ray inspection of the main landing gear (MLG) bay auxiliary spar booms for cracks or fuel leaks on both the left and right sides…

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to all British Aerospace Jetstream Model 3201 airplanes. This AD requires accomplishing both a routine visual inspection and either a detailed visual inspection or x-ray inspection of the main landing gear (MLG) bay auxiliary spar booms for cracks or fuel leaks on both the left and right sides of the airplane. This AD also requires obtaining and incorporating repair procedures for the MLG bay auxiliary spar where fuel leaks or cracks are found. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for the United Kingdom. The actions specified by this AD are intended to prevent wing failure caused by cracks or fuel leaks in the area of the MLG bay auxiliary spar booms, which could result in loss of control of the airplane.

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All British Aerospace Jetstream 31/32 directives

Applies to 1 model in our index