Airworthiness Directive

AD 98-13-03 63 FR 33532 Active

Federal Aviation Administration · 14 CFR part 39

FR document
98-15884
Amendment
39-10591
Published
1998-06-19
Effective
1998-08-03
Models covered
1
Last live check
2026-10-03
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AD

98-13-03

FR doc 98-15884 · 63 FR 33532

AD 98-13-03Published 1998-06-19Effective 1998-08-03

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 repetitively inspecting the main landing gear (MLG) hinge fitting, support angles, and attachment bolts on British Aerospace H.

Full official abstract

This amendment supersedes Airworthiness Directive (AD) 82-20- 04 R1, which currently requires repetitively inspecting the main landing gear (MLG) hinge fitting, support angles, and attachment bolts on British Aerospace H.P. 137 Mk1 and Jetstream series 200 airplanes, and repairing or replacing any part that is cracked beyond certain limits. This AD requires installing improved design MLG fittings, as terminating action for the repetitive inspections that are currently required by AD 82-20-04 R1, and will incorporate the Jetstream Model 3101 airplanes into the Applicability of the AD. The Federal Aviation Administration's policy on aging commuter-class aircraft is to eliminate or, in certain instances, reduce the number of certain repetitive short-interval inspections when improved parts or modifications are available. The actions specified by this AD are intended to prevent structural failure of the MLG caused by fatigue cracking, which could result in loss of control of the airplane during landing operations.

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All British Aerospace Jetstream 31/32 directives

Applies to 1 model in our index