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Airworthiness Directive

AD 2004-19-01 69 FR 55943 Active

Federal Aviation Administration · 14 CFR part 39

Requires you to inspect and, if necessary, modify the pilot/co-pilot upper shoulder harness adjusters that have certain Cessna accessory kits incorporated.

Federal Register (opens in a new tab)

FR document
04-20774
Amendment
39-13795
Published
2004-09-17
Effective
2004-11-01
Models covered
13

Last live check: 2026-08-19

Printed from https://aircraftdirectives.com/ad/2004-19-01 · 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

2004-19-01

FR doc 04-20774 · 69 FR 55943

AD 2004-19-01Published 2004-09-17Effective 2004-11-01

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 inspect and, if necessary, modify the pilot/co-pilot upper shoulder harness adjusters that have certain Cessna accessory kits incorporated.

Supersedes an earlier directive that is not in our index. See the official text.

Published in the Federal Register as AD 2004-19-04; the FAA corrected the number to AD 2004-19-01 in a later notice, listed with this record. The printed number still reaches this page.

2 corrections to this AD FAA · 2004-12-16

Correction published 2004-10-07

Issued by
Federal Aviation Administration
Published
2004-10-07
Document
Federal Register 04-21814 · Final rule; correction
Corrects
the version published September 17, 2004 at 69 FR 55943

This document makes a correction to Airworthiness Directive (AD) 2004-19-04, which was published in the Federal Register on September 17, 2004 (69 FR 55943), and applies to certain Cessna Aircraft Company (Cessna) 120, 140, 140A, 150, F150, 170, 172, F172, FR172, P172D, 175, 177, 180, 182, 185, A185E, 190, 195, 205, 205A, 206, P206, P206E, TP206A, TU206, TU206E, U206, U206E, 207, T207, 210, T210, 336, 337, and T337 series airplanes. We incorrectly referenced the AD number as AD 2004-19-04. The correct AD number is 2004-19-01. This action corrects the regulatory text.

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 04-21814, retrieved 2026-08-14

Read this correction on Federal Register (opens in a new tab)

Correction published 2004-12-16

Issued by
Federal Aviation Administration
Published
2004-12-16
Document
Federal Register 04-27513 · Final rule; correction
Corrects
the version published September 17, 2004 at 69 FR 55943

This document makes a correction to Airworthiness Directive (AD) 2004-19-01, which was published in the Federal Register on September 17, 2004 (69 FR 55943), and applies to certain Cessna Aircraft Company (Cessna) 120, 140, 140A, 150, F150, 170, 172, F172, FR172, P172D, 175, 177, 180, 182, 185, A185E, 190, 195, 205, 205A, 206, P206, P206E, TP206A, TU206, TU206E, U206, U206E, 207, T207, 210, T210, 336, 337, and T337 series airplanes. We incorrectly referenced a serial number for the affected Model T337B airplanes in the applicability section as 37-0570. The correct serial number is 337-0570. This action corrects the applicability section of AD 2004-19-01, Amendment 39- 13795.

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 04-27513, retrieved 2026-08-14

Read this correction on Federal Register (opens in a new tab)
Full official abstract

The FAA adopts a new airworthiness directive (AD) that will supersede AD 86-26-04, which applies to certain Cessna Aircraft Company (Cessna) 120, 140, 140A, 150, F150, 170, 172, F172, FR172, P172D, 175, 177, 180, 182, 185, A185E, 190, 195, 205, 205A, 206, P206, P206E, TP206A, TU206, TU206E, U206, U206E, 207, T207, 210, T210, 336, 337, and T337 series airplanes. AD 86-26-04 currently requires you to inspect and, if necessary, modify the pilot/co-pilot upper shoulder harness adjusters that have certain Cessna accessory kits incorporated. This AD is the result of reports that additional airplanes have the same unsafe condition and the manufacturer revised the service information to add these airplanes and correct the part number of the shoulder harness adjusters. Consequently, this AD retains the actions of 86-26-04, adds additional airplanes to the applicability section of this AD, and incorporates the revised service information. We are issuing this AD to prevent slippage of the pilot/co-pilot shoulder harness, which could result in failure of the shoulder harness to maintain proper belt length adjustment and tension. Such failure could result in pilot/co- pilot injury.

More directives for Cessna 140

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  2. AD 2004-15-18 Airworthiness Directives; Cessna Aircraft Company Models 172R, 172S, 182... Effective 2004-09-12
  3. AD 2003-24-13 Airworthiness Directives; Cessna Aircraft Company Models 172R, 172S, 182... Effective 2004-01-20

All Cessna 140 directives

View on Federal Register (opens in a new tab) Search DRS manually for AD 2004-19-01 (opens in a new tab) Print AD packet (opens the full Federal Register document in a new tab)

Applies to 13 models in our index