Airworthiness Directive

AD 2003-24-13 68 FR 67789 Superseded

Federal Aviation Administration · 14 CFR part 39

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.

FR document
03-30075
Amendment
39-13382
Published
2003-12-04
Effective
2004-01-20
Models covered
4

Last live check: 2026-08-19

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.
AD

2003-24-13

FR doc 03-30075 · 68 FR 67789

AD 2003-24-13Published 2003-12-04Effective 2004-01-20

Superseded by 2004-15-18

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 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.

1 correction to this AD FAA · 2003-12-30

Correction published 2003-12-30

Issued by
Federal Aviation Administration
Published
2003-12-30
Document
Federal Register 03-31667 · Final rule; correction
Corrects
the version published December 4, 2003 at 68 FR 67789

This document makes a correction to Airworthiness Directive (AD) 2003-24-13, which was published in the Federal Register on December 4, 2003 (68 FR 67789), and applies to 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. We inadvertently duplicated affected airplane serial numbers and included a serial number that should not be affected by this AD in the applicability section. This action corrects the applicability section of AD 2003-24-13, Amendment 39-13382.

A correction restates part of an AD that was published incorrectly. It is not an additional requirement and it does not change the AD number or its effective date.

Source: Federal Register document 03-31667, retrieved 2026-08-16

Full official abstract

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.

More directives for Cessna 140

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  2. AD 2004-19-01 Airworthiness Directives; Cessna Aircraft Company 120, 140, 140A, 150, F... Effective 2004-11-01
  3. AD 2004-15-18 Airworthiness Directives; Cessna Aircraft Company Models 172R, 172S, 182... Effective 2004-09-12

All Cessna 140 directives

Applies to 4 models in our index