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FAA orders · airworthiness directive · historical

2003-24-13: Honeywell KAP 140 autopilot computer system

FAA order 2003-24-13 is an airworthiness directive in force since January 20, 2004. The FAA's subject line: Honeywell KAP 140 autopilot computer system. It names Cessna T182 Turbo Skylane, Cessna T206 Turbo Stationair: about 1,993 aircraft on the U.S. register today across them, though an order usually covers particular versions or serial numbers rather than every one. System: flight controls.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
—
Models
172R, 172S, 182S, 182T, 206H, T182T, T206H
On this site
Cessna T182 Turbo Skylane 935 registered
Cessna T206 Turbo Stationair 1,058 registered

Dates and paperwork

In force since
January 20, 2004
Published
December 4, 2003 (signed November 25, 2003)
Docket
2003-CE-28-AD
Replaced by
2004-15-18
Status
Historical
The FAA's document
Read the order on the FAA's site

The FAA's summary their words, unchanged

The FAA adopts a new airworthiness directive (AD) for certain Cessna Aircraft Company (Cessna) Models 172R, 172S, 182S, 182T, T182T, 206H, and T206H airplanes that are equipped with a Honeywell KAP 140 autopilot computer system installed on the center instrument control panel near the throttle. This AD requires you to install an update to the operating software of the KAP 140 autopilot computer system, change the unit's part number, and change the software modification identification tag. This AD is the result of reports of inadvertent and undetected engagement of the autopilot system. We are issuing this AD to prevent unintentionally engaging the KAP 140 autopilot computer system, which could cause the pilot to take inappropriate actions.

The order itself the regulatory text, as published

Show the full text (4,497 characters)
2003-24-13 Cessna Aircraft Company: Amendment 39-13382; Docket No. 2003-CE-28-AD. When Does This AD Become Effective? (a) This AD becomes effective on January 20, 2004. What Other ADs Are Affected by This Action? (b) None. What Airplanes Are Affected by This AD? (c) This AD affects the following airplane models and serial numbers that are: (1) equipped with a KAP 140 autopilot computer system, part number (P/N) 065-00176-2602, P/N 065-00176-5402, or P/N 065-00176- 7702; and (2) certificated in any category; Model Serial No. 172R 17280001 through 17281073, 17281075 through 17281127, and 17281130 172S 172S8001 through 172S9195, 172S9197, 172S9198, and 172S9200 through 172S9203 182S 18280001 through 18280944 182T 18280945 through 18281064, 18281067 through 18281145,18281147 through 18281163, 18281165 through 18281167, and 18281172 T182T T18208001 through T18208109, and T18208111 throughT18208177 206H 20608001 through 20608183, 20608185, 20608187, and 20608188 T206H T20608001 through T20608039, T20608041 through T20608367, T20608369 through T20608379, T20608381, T20608382, and T20608385. What Is the Unsafe Condition Presented in This AD? (d) This AD is the result of reports of inadvertent and undetected engagement of the autopilot system. The actions specified in this AD are intended to prevent unintentionally engaging the KAP 140 autopilot computer system, which could cause the pilot to take inappropriate actions. What Must I Do To Address This Problem? (e) To address this problem, you must do the following: Actions Compliance Procedures (1) Install and update the KC 140 autopilot computer system operating software. Within the next 100 hours time-in-service (TIS) after January 20, 2004 (the effective date of this AD), unless already done. Follow Honeywell Service Bulletin No: KC 140-M1, dated August 2002, as specified in Cessna Service Bulletin SB02-22-01, dated November 25, 2002. (2) Do the following: (i) Change the unit part number by attaching flavor sticker, part number (P/N) 057-02203-0003, on the unit s serial tag;. (ii) Attach an M decal, P/N 057-02984-0501, in front of the unit serial number (this indicates that the unit s P/N has been changed); and (iii) Attach a software mod tag, P/N 057-05287-0301, in place of the old tag to indicate the software change to SW MOD 03/01. Prior to further flight after installing the update to the KC 140 autopilot computer system operating software, unless already done. Follow Honeywell Service Bulletin No: KC 140-M1, dated August 2002, as specified in Cessna Service Bulletin SB02-22-01, dated November 25, 2002. (3) Only install KC 140 autopilot computer systems, P/Ns 065-00176- 2602, 065-00176-5402, and 065- 00176-7702, that have been modified as specified in paragraphs (d)(1) and (d)(2) of this AD). As of January 20, 2004 (the effective date of this AD. Not applicable. (f) You may request a revised flight manual supplement from Cessna or Honeywell at the address specified in paragraph (h) of this AD. May I Request an Alternative Method of Compliance? (g) You may request a different method of compliance or a different compliance time for this AD by following the procedures in 14 CFR 39.13. Send your request to the Manager, Wichita Aircraft Certification Office (ACO), FAA. For information on any already approved alternative methods of compliance, contact Dan Withers, Aerospace Engineer, Wichita Aircraft Certification Office, FAA, 1801 Airport Road, Wichita, Kansas 67209; telephone: (316) 946-4196; facsimile: (316) 946-4107. Does This AD Incorporate Any Material by Reference? (h) You must do the actions required by this AD per Honeywell Service Bulletin No: KC 140-M1, dated August 2002, as specified in Cessna Service Bulletin SB02-22-01, dated November 25, 2002. The Director of the Federal Register approved the incorporationby reference of this service bulletin in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. You may get a copy from Cessna Aircraft Company, Product Support, P.O. Box 7706, Wichita, Kansas 67277; telephone: (316) 517-5800; facsimile: (316) 942-9006 and Honeywell, Business, Regional, and General Aviation, 23500 W. 105th Street, Olathe, Kansas 66061. You may review copies at FAA, Central Region, Office of the Regional Counsel, 901 Locust, Room 506, Kansas City, Missouri 64106; or at the Office of the Federal Register, 800 North Capitol Street, NW., suite 700, Washington, DC.

Related safety bulletins advice on the same designs, not orders

2019-02-12CE-19-01 · Engine Oil and Airplane Hour Meter; Pressure Switch Failure
2018-11-21SW-18-31 · NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM
2013-05-01CE-13-07R1 · Engine Exhaust; Tailpipe V-band Couplings
2012-12-13CE-13-07 · Engine Exhaust; Tailpipe V-band Couplings
2012-08-09CE-12-41 · Flight Controls Loose Glide Screw

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/2003-24-13.json · aircraft systems.