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) 2004-19-01, 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: 04-27513
Citation: 69 FR 75236
Amendment: 39-13795
Docket: Docket No. 2003-CE-40-AD
Action: Final rule; correction.
Published: 2004-12-16
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 241 (Thursday, December 16, 2004)]
[Rules and Regulations]
[Page 75236]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 04-27513]


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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) 2004-19-01, 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.

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 2004-19-01, Amendment 39-13795 
(69 FR 55943, September 17, 2004) (as corrected in the publication of 
October 7, 2004 (69 FR 60081), 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 a serial number for Model T337B 
airplanes in the applicability section of AD 2004-19-01. The correct 
serial number range for the affected Model T337B airplanes is 337-0001, 
337-0470, 337-0526 through 337-0568, and 337-0570 through 337-0755. 
This correction is needed to prevent confusion in the field regarding 
the FAA's intent of the AD applicability.

Correction of Publication

    Accordingly, the publication of September 17, 2004 (69 FR 55943), 
of AD 2004-19-01; Amendment 39-13795; which was the subject of FR Doc. 
04-20774 (as corrected in the publication of October 7, 2004 (69 FR 
60081), which was the subject of FR Doc. 04-21814), is corrected as 
follows:


Sec.  39.13  [Corrected]

0
On page 55946, in Sec.  39.13 [Amended], 2., replace paragraph (c)(129) 
with the following text:

``(129) T337B 337-0001, 337-0470, 337-0526 through 337-0568, and 
337-0570 through 337-0755''.

    Action is taken herein to correct this reference in AD 2004-19-01 
and to add this AD correction to Sec.  39.13 of the Federal Aviation 
Regulations (14 CFR 39.13).
    The effective date remains November 1, 2004.

    Issued in Kansas City, Missouri, on December 7, 2004.
Sandra J. Campbell,
Acting Manager, Small Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 04-27513 Filed 12-15-04; 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/2004/12/16/04-27513/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-2004-12-16/pdf/04-27513.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.