AD 2006-01-11 R1
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Cessna Aircraft Company | 208 | Airworthiness Directives; The Cessna Aircraft Company Models 208 and 208B Airplanes |
| aircraft | Cessna Aircraft Company | 208B | Airworthiness Directives; The Cessna Aircraft Company Models 208 and 208B Airplanes |
Unsafe Condition
Failure of the cargo pod and landing gear fairings due to ice accumulation could result in structural failure or separation of the fairings, leading to loss of airplane control.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Install pilot assist handles and deicing boots on the cargo pod and landing gear fairings. Revise the Pilot's Operating Handbook (POH) and FAA-approved Airplane Flight Manual (AFM) with specified changes.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
before further flight
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Cessna Aircraft Company Models 208 and 208B airplanes
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Cargo pod and landing gear fairings
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - 2006-01-11 R1 (Correction).pdf Copy URL Document Versions Feedback DetailsAttachments/Public Comments AD Number: 2006-01-11 R1 Document Type: AD Final Rules Docket Number: FAA-2005-21275 Subject Heading: Airworthiness Directives; The Cessna Aircraft Company Models 208 and 208B Airplanes Subject: Cargo pod and landing gear fairings Status: Current Citation: Federal Register: May 16, 2006 (Volume 71, Number 94) Citation Publish Date: 05/16/2006 Effective Date: 02/22/2006 Make: Cessna Aircraft Company Model: 208 | 208B Product Type: Aircraft Product Subtype: Small Airplane Affected AD: Superseded AD: 2006-01-11 Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: CORRECTION: [Federal Register: May 16, 2006 (Volume 71, Number 94); Page 28420; www.access.gpo.gov/su_docs/aces/aces140.html] CORRECTION: [Federal Re... ...Show more Automatic Zoom Actual Size Page Fit Page Width 50% 75% 100% 125% 150% 200% 300% 400% 125% of 11 1 [Federal Register: May 16, 2006 (Volume 71, Number 94)] [CORRECTIONS] [Page 28420] From the Federal Register Online via GPO Access [wais.access.gpo.gov] [DOCID:fr16my06-150] ––––––––––––––––––––––––––––––––––– 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 Correction In rule document 06-2546 beginning on page 13538 in the issue of Thursday, March 16, 2006, make the following correction: §39.13 [Corrected] On page 13540, in §39.13, in the table, under the heading ''Actions,'' in entry (4), in the third line, ''(600 SHP) or equipped'' should read ''(600 SHP) or equivalent, and equipped''. [FR Doc. C6-2546 Filed 5-15-06; 8:45 am] BILLING CODE 1505-01-D 2 [Federal Register: May 16, 2006 (Volume 71, Number 94)] [Rules and Regulations] [Page 28250] From the Federal Register Online via GPO Access [wais.access.gpo.gov] [DOCID:fr16my06-4] ––––––––––––––––––––––––––––––––––– 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. ––––––––––––––––––––––––––––––––––– 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
Document Text
Show stored source text (verify against official source)
AD Final Rules - 2006-01-11 R1 (Correction).pdf Copy URL Document Versions Feedback DetailsAttachments/Public Comments AD Number: 2006-01-11 R1 Document Type: AD Final Rules Docket Number: FAA-2005-21275 Subject Heading: Airworthiness Directives; The Cessna Aircraft Company Models 208 and 208B Airplanes Subject: Cargo pod and landing gear fairings Status: Current Citation: Federal Register: May 16, 2006 (Volume 71, Number 94) Citation Publish Date: 05/16/2006 Effective Date: 02/22/2006 Make: Cessna Aircraft Company Model: 208 | 208B Product Type: Aircraft Product Subtype: Small Airplane Affected AD: Superseded AD: 2006-01-11 Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: CORRECTION: [Federal Register: May 16, 2006 (Volume 71, Number 94); Page 28420; www.access.gpo.gov/su_docs/aces/aces140.html] CORRECTION: [Federal Re... ...Show more Automatic Zoom Actual Size Page Fit Page Width 50% 75% 100% 125% 150% 200% 300% 400% 125% of 11 1 [Federal Register: May 16, 2006 (Volume 71, Number 94)] [CORRECTIONS] [Page 28420] From the Federal Register Online via GPO Access [wais.access.gpo.gov] [DOCID:fr16my06-150] ––––––––––––––––––––––––––––––––––– 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 Correction In rule document 06-2546 beginning on page 13538 in the issue of Thursday, March 16, 2006, make the following correction: §39.13 [Corrected] On page 13540, in §39.13, in the table, under the heading ''Actions,'' in entry (4), in the third line, ''(600 SHP) or equipped'' should read ''(600 SHP) or equivalent, and equipped''. [FR Doc. C6-2546 Filed 5-15-06; 8:45 am] BILLING CODE 1505-01-D 2 [Federal Register: May 16, 2006 (Volume 71, Number 94)] [Rules and Regulations] [Page 28250] From the Federal Register Online via GPO Access [wais.access.gpo.gov] [DOCID:fr16my06-4] ––––––––––––––––––––––––––––––––––– 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. ––––––––––––––––––––––––––––––––––– 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
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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