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96-12-23: Wing Stall Fence Height

FAA order 96-12-23 is an airworthiness directive in force since July 31, 1996. The FAA's subject line: Wing Stall Fence Height. It names Cessna 150, Cessna 152, Cessna A150, Cessna A152: about 9,912 aircraft on the U.S. register today across them, though an order usually covers particular versions or serial numbers rather than every one. System: airframe structure.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
Cessna Aircraft Company
Models
150, 150A, 150B, 150C, 150D, 150E, 150F, 150G, 150H, 150J, 150K, 150L, 150M, 152, A150K, A150L, A150M, A152
On this site
Cessna 150 7,995 registered
Cessna 152 1,637 registered
Cessna A150 232 registered
Cessna A152 48 registered

Dates and paperwork

In force since
July 31, 1996
Docket
95-CE-14-AD
Status
Current
The FAA's document
Read the order on the FAA's site

The FAA's summary their words, unchanged

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.

The order itself the regulatory text, as published

Show the full text (3,284 characters)
96-12-23 THE CESSNA AIRCRAFT COMPANY: Amendment 39-9666; Docket No. 95-CE- 14-AD. \n\n\tApplicability: The following airplane models (all serial numbers), certificated in any category, that have a Bush Conversions, Inc., Short Takeoff and Landing (STOL) kit incorporated in accordance with Supplemental Type Certificate (STC) SA1371SW: \n\n\n150\n150A\t\n150B \n150C\n150D\t\n150E \n150F\n150G\n150H \n150J\n150K\nA150K \t\n150L\nA150L\n150M\nA150M \n152\nA152 \n\t\n\tNOTE 1: This AD applies to each airplane identified in the preceding applicability provision, regardless of whether it has been modified, altered, or repaired in the area subject to the requirements of this AD. For airplanes that have been modified, altered, or repaired so that the performance of the requirements of this AD is affected, the owner/operator must request approval for an alternative method of compliance in accordance with paragraph (d) of this AD. The request should include an assessment of the effect of the modification, alteration, or repair on the unsafe condition addressed by this AD; and, if the unsafe condition has not been eliminated, the request should include specific proposed actions to address it. \n\n\tCompliance: Required within the next 100 hours time-in-service after the effective date of this AD, unless already accomplished. \n\n\tTo prevent the airplane operator from entering a stall condition because of improper wing stall fence height, which, if not detected and corrected, could result in loss of control of the airplane, accomplish the following: \n\n\t(a)\tMeasure the height of the wing stall fence at its trailing edge to ensure that the height does not exceed 1.28 inches. (See Figure 1 of this AD). \n\n\t(b)\tIf the wing stall fence height exceeds 1.28 inches, prior to further flight, install a smaller fence in accordance with instructions obtained from the Wichita Aircraft Certification Office (ACO), FAA, 1801 Airport Road, Mid-Continent Airport, Wichita, Kansas 67209. \n\n\tNOTE 2: Mid-America Drawing No. 1001 (part of STC SA1371SW) is included as Figure 1 of this AD for reference purposes. \n\n\t(c)\tSpecial flight permits may be issued in accordance with sections 21.197 and 21.199 of the Federal Aviation Regulations (14 CFR 21.197 and 21.199) to operate the airplane to a location where the requirements of this AD can be accomplished. \n\n\t(d)\tAn alternative method of compliance or adjustment of the compliance times that provides an equivalent level of safety may be approved by the Manager, Wichita ACO, 801 Airport Road, Mid-Continent Airport, Wichita, Kansas 67209. The request shall be forwarded through an appropriate FAA Maintenance Inspector, who may add comments and then send it to the Manager, Wichita ACO. \n\n\tNOTE 3: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Wichita ACO. \n\n\t(e)\tFigure 1 of this AD may be obtained from the Wichita ACO at the address specifiedin paragraph (d) of this AD; and may be examined at the FAA, Central Region, Office of the Assistant Chief Counsel, Room 1558, 601 E. 12th Street, Kansas City, Missouri 64106. \n\n\t(f)\tThis amendment becomes effective on July 31, 1996. \n\nAD 96-12-23 FIGURE 1

Related safety bulletins advice on the same designs, not orders

2025-12-222025-11 · RUDDER CONTROL SYSTEM
2018-11-21SW-18-31 · NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM
2017-05-11CE-17-12 · Horizontal Stabilizer Elevator Attach Points
2015-10-09CE-16-03 · VERTICAL TAIL Aft Fin Attachment Fitting
2012-01-25CE-12-14 · Three Alternative Methods of Compliance for AD 2011-10-09

Source: FAA Dynamic Regulatory System, airworthiness directives. The FAA's document is the authority; the register counts are this site's, from the FAA register of October 8, 2026. Connections as data: /graph/directive/96-12-23.json · aircraft systems.