Published 2004-12-16 · Federal Register document 04-27513
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
Publication 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.
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:13.905821+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2004-cb1e1f18d61cac01
- Source row
- results[526]
- Raw source SHA-256
- cb1e1f18d61cac01616802134d899b0c8ce1a9f79716b5ee037f78e4cb53a00a
Correction notice · separate source edition
Recorded publication clauses
- AD identifier printed in this edition
- 2004-19-01
- Effective date printed in this edition
- Unknown
This correction is a separate source edition; it is not counted as a new adopted rule.
No adopted-clause structure was recorded for this source edition. Read the complete text; no applicability conclusion has been inferred.
No replacement link has been established from this edition. The complete historical rule chain and current legal effect remain unknown.
Find all recorded historical references to AD 2004-19-01 · 0 printed reference observations in this pinned collection.
These are observations from one dated publication. Current legal status is unknown; aircraft applicability, installed configuration, compliance and burden require separate evidence. Missing or unparsed conditions remain unknown.
Why these observations are shown
They were extracted offline from the same immutable official HTML source as the complete recorded text. The dated source wording, original text coordinates and exact quote digests are retained. PDF/text agreement and current regulatory effect have not been qualified.
Observation revision: whole-ad-publication-clause-observations-1.0.1. Text SHA-256: 3a47f2d16617cd85daa35ee1a5028e14f8a206c9482d83ad459ddb0ed2dca9c2. Source manifest: b9944728dbc415f2e20d9ec0231f9610e1a9ae0689c5b000adc486228781305b.
Official source · 2004-12-16
Publication text
This is the complete recorded text of this dated publication.
Current legal effect is unknown. Aircraft applicability, installed configuration and compliance require separate evidence. PDF/text agreement has not been evaluated.
Read the complete official publication text
[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]
-----------------------------------------------------------------------
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.
-----------------------------------------------------------------------
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
Why this text is shown
The complete text was extracted from the official GovInfo HTML edition for this publication. Acquired 2026-10-09T04:00:06.242614+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.
Open the captured official edition
- Source SHA-256
- 4a226b51aa87555e5b09fa9ee059468ea7a875cc36369da1b9e6c6dc3ad81d34
- Text SHA-256
- 3a47f2d16617cd85daa35ee1a5028e14f8a206c9482d83ad459ddb0ed2dca9c2
Return to the full metadata catalog · Search complete publication text · Explore retained publication text and evidence
Coverage and limits
These are dated publication metadata, recorded clauses and literal source observations. Word, model-label, header and reference matches do not establish current legal effect, manufacturer/model identity, aircraft applicability, installed configuration or compliance.
The collection uses 33 explicit annual source snapshots. Source captures and operative-text qualifications have separate states. Missing information remains unknown.