AircraftDirectives
MembershipSign inCreate free account
Menu
Airworthiness Directive

AD 96-12-23 61 FR 29468 Active

Federal Aviation Administration · 14 CFR part 39

FR document
96-14632
Amendment
39-9666
Published
1996-06-11
Effective
1996-07-31
Models covered
1
Last live check
2026-10-02

Printed from https://aircraftdirectives.com/ad/96-12-23 · 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.

Opens your browser's print dialog. Choose “Save as PDF” to export a file. Keyboard: Ctrl+P or Cmd+P.

AD

96-12-23

FR doc 96-14632 · 61 FR 29468

AD 96-12-23Published 1996-06-11Effective 1996-07-31

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 measuring the wing stall fence for maximum height, and installing a smaller fence if the fence exceeds the maximum height of 1.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to Cessna Aircraft Company (Cessna) 150 and A150 series and Models 152 and A152 airplanes that have a Bush Conversions, Inc., Short Takeoff and Landing (STOL) kit incorporated in accordance with Supplemental Type Certificate (STC) SA1371SW. This action requires measuring the wing stall fence for maximum height, and installing a smaller fence if the fence exceeds the maximum height of 1.28 inches. An accident of a Cessna Model 152 airplane where the STOL kit adversely affected the airplane's stall characteristics prompted this action. The actions specified by this AD are intended to prevent the airplane from entering a stall condition because of improper wing stall fence height, which could result in loss of control of the airplane.

More directives for Cessna 150/152

  1. AD 2009-10-09 R2 Airworthiness Directives; Cessna Aircraft Company Airplanes 2011-08-26
  2. AD 2011-10-09 Airworthiness Directives; Cessna Aircraft Company Models 150, 152, 170, ... 2011-05-13
  3. AD 2009-10-09 R1 Airworthiness Directives; Cessna Aircraft Company 150 and 152 Series Air... 2009-11-06
  4. AD 2009-10-09 Airworthiness Directives; Cessna Aircraft Company 150 and 152 Series Air... 2009-05-13
  5. AD 2008-22-18 Airworthiness Directives; Cessna Aircraft Company 150 Series Airplanes 2008-11-04

All Cessna 150/152 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