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
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…
[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.