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Airworthiness Directive

AD 2005-25-14 70 FR 73583 Active

Federal Aviation Administration · 14 CFR part 39

FR document
05-23830
Amendment
39-14407
Published
2005-12-13
Effective
2006-01-17
Models covered
1
Last live check
2026-10-03

Printed from https://aircraftdirectives.com/ad/2005-25-14 · AircraftDirectives restates official FAA and manufacturer records; the official sources named on this sheet control. Not an airworthiness determination.

This page is a reference Record, not an airworthiness or compliance determination. Official FAA and manufacturer sources control over our restatement, subject to governing law. Check applicability, current requirements and incorporated documents before acting. The owner or operator remains responsible for airworthiness and required records under 14 CFR 91.403 and 91.417, as applicable. Terms of Use: /terms.

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AD

2005-25-14

FR doc 05-23830 · 70 FR 73583

AD 2005-25-14Published 2005-12-13Effective 2006-01-17

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 modifying the wiring of the starter-generator terminal block.

Full official abstract

The FAA is adopting a new airworthiness directive (AD) for all BAE Systems (Operations) Limited (Jetstream) Model 4101 airplanes. This AD requires modifying the wiring of the starter-generator terminal block. This AD results from a report of total electrical failure just as the airplane landed. We are issuing this AD to prevent total electrical failure and consequent 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)

Applies to 1 model in our index