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Airworthiness Directive

AD 96-05-06 61 FR 9090 Active

Federal Aviation Administration · 14 CFR part 39

Requires a one-time inspection of the main distribution center for loose or missing attachment hardware, and correction of any discrepancy identified.

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FR document
96-5078
Amendment
39-9532
Published
1996-03-07
Effective
1996-03-22
Models covered
1

Last live check: 2026-08-19

Printed from https://aircraftdirectives.com/ad/96-05-06 · 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

96-05-06

FR doc 96-5078 · 61 FR 9090

AD 96-05-06Published 1996-03-07Effective 1996-03-22

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 main distribution center for loose or missing attachment hardware, and correction of any discrepancy identified.

Full official abstract

This amendment adopts a new airworthiness directive (AD), applicable to all Canadair Model CL-215-1A10 series airplanes. This action requires a one-time inspection of the main distribution center for loose or missing attachment hardware, and correction of any discrepancy identified. This amendment is prompted by a report of total loss of electrical power on one airplane during flight, which was caused by shorting out of the voltage regulator in the main distribution center. The actions specified in this AD are intended to prevent total electrical failure during flight, which could adversely affect the continued safe flight of the airplane.

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All Canadair CL-215 / CL-415 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