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Airworthiness Directive

AD 96-10-01 61 FR 19813 Superseded

Federal Aviation Administration · 14 CFR part 39

Revised by AD 96-10-01 R1Federal Register (opens in a new tab)FAA DRS (opens in a new tab)

FR document
96-10913
Amendment
39-9606
Published
1996-05-03
Effective
1996-06-10
Models covered
1

Last live check: 2026-08-19

Printed from https://aircraftdirectives.com/ad/96-10-01 · 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

96-10-01

FR doc 96-10913 · 61 FR 19813

AD 96-10-01Published 1996-05-03Effective 1996-06-10

Revised by 96-10-01 R1

Supersedence is read from the Federal Register text of the newer AD — the FAA publishes no structured field for it — and names only ADs held in our index.

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 complete landing light support replacement.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to certain The New Piper Aircraft, Inc. (Piper) Models PA-28- 140, PA-28-150, PA-28-160, and PA-28-180 airplanes. This action requires a complete landing light support replacement. This AD action is prompted by reports of two accidents and two incidents resulting from the landing light retainer support seal breaking apart and entering the carburetor. The actions specified by this AD are intended to prevent the landing light retainer support seal from being ingested by the updraft carburetor, which, if not detected and corrected, could result in rough engine operation or possible engine failure and loss of control of the airplane.

More directives for Piper PA-28

  1. AD 2024-10-04 Airworthiness Directives; Piper Aircraft, Inc. Airplanes Effective 2024-06-06
  2. AD 2020-26-16 Airworthiness Directives; Piper Aircraft, Inc. Airplanes Effective 2021-02-16
  3. AD 2020-24-05 Airworthiness Directives; Piper Aircraft, Inc. Airplanes Effective 2020-12-28
  4. AD 2018-07-03 Airworthiness Directives; Piper Aircraft, Inc. Effective 2018-04-20
  5. AD 2018-02-05 Airworthiness Directives; Piper Aircraft, Inc. Effective 2018-02-07

All Piper PA-28 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