Published 2006-05-16 · Federal Register document 06-4424
Airworthiness Directives; The Cessna Aircraft Company Models 208 and 208B Airplanes
Publication summary
This document makes a correction to Airworthiness Directive (AD) 2006-01-11 R1, which published in the Federal Register on March 16, 2006 (71 FR 13538), and applies to all The Cessna Aircraft Company (Cessna) Models 208 and 208B airplanes. AD 2006-01-11 R1 requires the installation of a pilot assist handle and deicing boots on the cargo pod and landing gear fairings; and the incorporation of changes to the Pilot's Operating Handbook (POH) and FAA-approved Airplane Flight Manual (AFM). Current language in paragraph (e)(4) of AD 2006-01-11 R1 regarding the placard requirement inadvertently states: "You may insert a copy of this AD into the appropriate sections of the POH to comply with this action." This does not meet the intent of the AD. This document corrects that paragraph by removing the language referenced above.
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Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:20.745856+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2006-8d787f8b35bc8016
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- results[157]
- Raw source SHA-256
- 8d787f8b35bc80165a417cea66de09cd32a1700face13759db364c607e405963
Correction notice · separate source edition
Recorded publication clauses
- AD identifier printed in this edition
- 2006-01-11 R1
- Effective date printed in this edition
- Unknown
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Find all recorded historical references to AD 2006-01-11 R1 · 0 printed reference observations in this pinned collection.
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Observation revision: whole-ad-publication-clause-observations-1.0.1. Text SHA-256: 9dd1f763af37be3cfb0ce92bf8144e8e11998b1ccbf9efcf1963bbc468aaa027. Source manifest: d0b44d78faa55874df111ff631d240838276a1f1801cbc8433c006d5f5dd9e54.
Official source · 2006-05-16
Publication text
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Read the complete official publication text
[Federal Register Volume 71, Number 94 (Tuesday, May 16, 2006)]
[Rules and Regulations]
[Page 28250]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 06-4424]
[[Page 28250]]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2005-21275; Directorate Identifier 2005-CE-28-AD;
Amendment 39-14515; AD 2006-01-11 R1]
RIN 2120-AA64
Airworthiness Directives; The Cessna Aircraft Company Models 208
and 208B 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) 2006-01-11 R1, which published in the Federal Register on March
16, 2006 (71 FR 13538), and applies to all The Cessna Aircraft Company
(Cessna) Models 208 and 208B airplanes. AD 2006-01-11 R1 requires the
installation of a pilot assist handle and deicing boots on the cargo
pod and landing gear fairings; and the incorporation of changes to the
Pilot's Operating Handbook (POH) and FAA-approved Airplane Flight
Manual (AFM). Current language in paragraph (e)(4) of AD 2006-01-11 R1
regarding the placard requirement inadvertently states: ``You may
insert a copy of this AD into the appropriate sections of the POH to
comply with this action.'' This does not meet the intent of the AD.
This document corrects that paragraph by removing the language
referenced above.
DATES: The effective date of this AD (2006-01-11 R1) remains February
22, 2006.
FOR FURTHER INFORMATION CONTACT: Robert P. Busto, Aerospace Engineer,
Wichita Aircraft Certification Office, FAA, 1801 Airport Road, Wichita,
Kansas 67209; telephone: (316) 946-4157; facsimile: (316) 946-4107.
SUPPLEMENTARY INFORMATION:
Discussion
On March 10, 2006, the FAA issued AD 2006-01-11 R1, Amendment 39-
14515 (71 FR 13538, March 16, 2006), which applies to all Cessna Models
208 and 208B airplanes. AD 2006-01-11 R1 requires the installation of a
pilot assist handle and deicing boots on the cargo pod and landing gear
fairings; and the incorporation of changes to the Pilot's Operating
Handbook (POH) and FAA-approved Airplane Flight Manual (AFM). Current
language in paragraph (e)(4) of AD 2006-01-11 R1 regarding the placard
requirement inadvertently states: ``You may insert a copy of this AD
into the appropriate sections of the POH to comply with this action.''
This does not meet the intent of the AD.
Need for the Correction
This correction is needed to not allow a method of compliance that
was inadvertently included in the AD and does not address the unsafe
condition.
Correction of Publication
0
Accordingly, the publication of March 16, 2006 (71 FR 13538), of
Amendment 39-14515; AD 2006-01-11 R1, which was the subject of FR Doc.
06-2546, is corrected as follows:
Sec. 39.13 [Corrected]
On page 13540, in Sec. 39.13 [Amended], in paragraph (e)(4), in
the Procedures column, remove the following text:
``You may insert a copy of this AD into the appropriate sections
of the POH to comply with this action.''
Action is taken herein to correct this reference in AD 2006-01-11
R1 and to add this AD correction to Sec. 39.13 of the Federal Aviation
Regulations (14 CFR 39.13).
The effective date remains February 22, 2006.
Issued in Kansas City, Missouri, on May 5, 2006.
Kim Smith,
Manager, Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. 06-4424 Filed 5-15-06; 8:45 am]
BILLING CODE 4910-13-P
Why this text is shown
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- Text SHA-256
- 9dd1f763af37be3cfb0ce92bf8144e8e11998b1ccbf9efcf1963bbc468aaa027
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