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Airworthiness Directive packet

AD 2004-19-01

Airworthiness Directives; Cessna Aircraft Company 120, 140, 140A, 150, F150, 170, 172, F172, FR172, P172D, 175, 177, 180, 182, 185, A185E, 190, 195, 206, P206, U206, TP206, TU206, 207, T207, 210, T210, 336, 337, and T337 Series Airplanes

1 · Quick read — prepared by AircraftDirectives

Our plain-language summary — not the regulation

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…

AD number
2004-19-01
Federal Register document
04-21814
Citation
69 FR 60081
Amendment
39-13795
Docket
Docket No. 2003-CE-40-AD
Action
Final rule; correction.
Published
2004-10-07
Effective
2004-11-01
Effective (as stated in the rule)
The effective date of this AD remains November 1, 2004.
Issued by
Transportation Department, Federal Aviation Administration
Regulation
14 CFR 39
Applies to these models (in our index)
Cessna 140, Cessna 150/152, Cessna 170, Cessna 172, Cessna 175 Skylark, Cessna 177 Cardinal, Cessna 180, Cessna 182, Cessna 185 Skywagon, Cessna 195 Businessliner, Cessna 206, Cessna 210 Centurion, Cessna 336/337 Skymaster

2 · Official Federal Register document — government source, verbatim

Reproduced unedited from the Federal Register
[Federal Register Volume 69, Number 194 (Thursday, October 7, 2004)]
[Rules and Regulations]
[Page 60081]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 04-21814]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 2003-CE-40-AD; Amendment 39-13795; AD 2004-19-01]
RIN 2120-AA64


Airworthiness Directives; Cessna Aircraft Company 120, 140, 140A, 
150, F150, 170, 172, F172, FR172, P172D, 175, 177, 180, 182, 185, 
A185E, 190, 195, 206, P206, U206, TP206, TU206, 207, T207, 210, T210, 
336, 337, and T337 Series Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule; correction.

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SUMMARY: 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.

DATES: The effective date of this AD remains November 1, 2004.

FOR FURTHER INFORMATION CONTACT: Gary D. Park, Aerospace Engineer, FAA, 
Wichita Aircraft Certification Office, 1801 Airport Road, Room 100, 
Mid-Continent Airport, Wichita, Kansas 67209; telephone: (316) 946-
4123; facsimile: (316) 946-4107.

SUPPLEMENTARY INFORMATION:

Discussion

    On September 8, 2004, FAA issued AD 2004-19-04, Amendment 39-13795 
(69 FR 55943, September 17, 2004), which applies to certain 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. This AD supersedes AD 86-26-04 with a new AD that requires 
you to inspect and, if necessary, modify the pilot/co-pilot upper 
shoulder harness adjusters that have certain Cessna accessory kits 
incorporated.

Need for the Correction

    The FAA incorrectly referenced the AD number as 2004-19-04. The 
correct AD number is AD 2004-19-01. This correction is needed to ensure 
that the correct AD number is entered in the logbook and to eliminate 
misunderstanding in the field.

Correction of Publication

0
Accordingly, the publication of September 17, 2004 (69 FR 55943), of 
Amendment 39-13795; AD 2004-19-04, which was the subject of FR Doc. 04-
20774, is corrected as follows:


Sec.  39.13  [Corrected]

0
On page 55945, in section 39.13 [Amended], replace 2004-19-04 with 
2004-19-01.
    Action is taken herein to correct this reference in AD 2004-19-04 
and to add this AD correction to section 39.13 of the Federal Aviation 
Regulations (14 CFR 39.13).
    The effective date remains November 1, 2004.

    Issued in Kansas City, Missouri, on September 23, 2004.
David R. Showers,
Acting Manager, Small Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 04-21814 Filed 10-6-04; 8:45 am]
BILLING CODE 4910-13-P

Sources. Section 1 is written by AircraftDirectives from the record below and is a reading aid only. Section 2 is the United States Government's own text, reproduced without edit.

Federal Register: https://www.federalregister.gov/documents/2004/10/07/04-21814/airworthiness-directives-cessna-aircraft-company-120-140-140a-150-f150-170-172-f172-fr172-p172d-175

Official PDF: https://www.govinfo.gov/content/pkg/FR-2004-10-07/pdf/04-21814.pdf

Packet generated 2026-08-18 08:12 UTC.

This packet is not an airworthiness determination and not legal or maintenance advice. AircraftDirectives reproduces official records and condenses their wording for easier reading. It does not decide, certify or imply whether any aircraft, engine, appliance or part is airworthy, compliant, affected by this directive, or eligible for return to service. No inspection, approval, or determination of any kind is performed or implied by this document.

Section 1 is a reading aid, not the rule. It is our own plain-language condensation, written to help a reader find the relevant directive quickly. It is NOT a substitute for the regulation, it may omit conditions, exceptions, compliance times, alternative methods of compliance (AMOCs) and applicability limits, and it has no legal force whatsoever. Only the official text governs. Where Section 1 and Section 2 differ in any respect, Section 2 - and the official source it was retrieved from - controls absolutely.

Responsibility remains with the owner/operator. Under 14 CFR §91.403 and §91.417 the owner or operator is responsible for maintaining airworthiness and for required records; under §39.7 no person may operate a product to which an airworthiness directive applies except in accordance with that directive. Determining applicability to a specific serial number and configuration, and performing or supervising any required action, is the responsibility of the owner/operator and appropriately certificated personnel.

Accuracy and currency. Section 2 was retrieved at the time stamped above and is reproduced without edit; Federal Register material is a work of the United States Government. Directives are amended, corrected and superseded over time, and this sheet is a snapshot, not a live record - it does not update after printing. Re-check the official sources before acting on it. This packet is provided without warranty of any kind, express or implied, including fitness for a particular purpose. We do not sell parts and have no commercial interest in any action a directive may require.

AircraftDirectives · AD 2004-19-01 · Section 1 is our plain-language reading aid; Section 2 is the official Federal Register text and controls where the two differ. Not an airworthiness determination — 14 CFR §91.403 / §91.417 responsibility remains with the owner/operator. Retrieved 2026-08-18 08:12 UTC.