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Airworthiness Directive

AD 97-25-16 62 FR 65603 Active

Federal Aviation Administration · 14 CFR part 39

Requires a one-time inspection of the tailplane (horizontal stabilizer) leading edges and surrounding area for discrepancies, and corrective action, if necessary.

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FR document
97-32431
Amendment
39-10241
Published
1997-12-15
Effective
1998-01-20
Models covered
1

Last live check: 2026-10-04

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AD

97-25-16

FR doc 97-32431 · 62 FR 65603

AD 97-25-16Published 1997-12-15Effective 1998-01-20

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 a one-time inspection of the tailplane (horizontal stabilizer) leading edges and surrounding area for discrepancies, and corrective action, if necessary.

Full official abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain British Aerospace (Jetstream) Model 4101 airplanes, that requires a one-time inspection of the tailplane (horizontal stabilizer) leading edges and surrounding area for discrepancies, and corrective action, if necessary. This amendment is prompted by the issuance of mandatory continuing airworthiness information by a foreign civil airworthiness authority. The actions specified by this AD are intended to prevent separation of the horizontal stabilizer from the fin, which could lead to reduced controllability of the airplane.

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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