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Airworthiness Directive

AD 98-05-07 63 FR 11112 Active

Federal Aviation Administration · 14 CFR part 39

Requires replacement of the stringer joint pieces at the left side of the fuselage with new, improved parts.

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FR document
98-5345
Amendment
39-10368
Published
1998-03-06
Effective
1998-04-10
Models covered
1

Last live check: 2026-10-04

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AD

98-05-07

FR doc 98-5345 · 63 FR 11112

AD 98-05-07Published 1998-03-06Effective 1998-04-10

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 replacement of the stringer joint pieces at the left side of the fuselage with new, improved parts.

Full official abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain British Aerospace (Jetstream) Model 4101 airplanes, that requires replacement of the stringer joint pieces at the left side of the fuselage with new, improved parts. This amendment is prompted by issuance of mandatory continuing airworthiness information by a foreign civil airworthiness authority. The actions specified by this AD are intended to prevent the fuselage structure at the stringer joint at station 130 on the left side of the airplane from cracking, which could result in rapid decompression of the airplane at the forward fuselage area.

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All British Aerospace Jetstream 41 directives

View on Federal Register (opens in a new tab) View this AD in FAA DRS (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