Airworthiness Directive

AD 95-11-17 60 FR 28529 Active

Federal Aviation Administration · 14 CFR part 39

FR document
95-13120
Amendment
39-9250
Published
1995-06-01
Effective
1995-07-19
Models covered
1
Last live check
2026-10-03
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AD

95-11-17

FR doc 95-13120 · 60 FR 28529

AD 95-11-17Published 1995-06-01Effective 1995-07-19

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 airplane electrical system and revising the emergency procedures section of the Airplane Flight Manual (AFM) on certain Jetstream Aircraft Limited (JAL) Jetstream Models 3101 and 3201 airplanes.

Full official abstract

This amendment supersedes Airworthiness Directive (AD) 90-13- 12, which currently requires modifying the airplane electrical system and revising the emergency procedures section of the Airplane Flight Manual (AFM) on certain Jetstream Aircraft Limited (JAL) Jetstream Models 3101 and 3201 airplanes. This action retains the requirements of AD 90-13-12 for those airplanes that do not have modified inverters installed and the inverted transfer function restored. The Federal Aviation Administration (FAA) has determined that installing modified inverters along with restoring the inverter transfer function corrects the problems in the power supply addressed by AD 90-13-12. The actions specified by this AD are intended to prevent alternating current system failures, which, if not detected and corrected, could result in damage to the airplane navigational systems.

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All British Aerospace Jetstream 31/32 directives

Applies to 1 model in our index