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FAA orders · airworthiness directive · historical

2009-13-06: Nose baggage door

FAA order 2009-13-06 is an airworthiness directive in force since July 24, 2009. The FAA's subject line: Nose baggage door. It names Piper PA-23 Apache and Aztec, Piper PA-31 Navajo and Chieftain, Piper PA-42: about 2,310 aircraft on the U.S. register today across them, though an order usually covers particular versions or serial numbers rather than every one. System: airframe structure.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
Piper Aircraft Inc.
Models
PA-23, PA-23-160, PA-23-235, PA-23-250, PA-23-250 (Navy UO-1), PA-31, PA-31-300, PA-31-325, PA-31-350, PA-31P, PA-31P-350, PA-31T, PA-31T1, PA-31T2, PA-31T3, PA-42, PA-42-1000, PA-42-720, PA-E23-250
On this site
Piper PA-23 Apache and Aztec 1,316 registered
Piper PA-31 Navajo and Chieftain 935 registered
Piper PA-42 59 registered

Dates and paperwork

In force since
July 24, 2009
Published
June 19, 2009 (signed June 12, 2009)
Docket
FAA-2009-0218
Replaced by
2009-13-06 R1
Status
Historical
The FAA's document
Read the order on the FAA's site

The FAA's summary their words, unchanged

We are adopting a new airworthiness directive (AD) for certain Piper Aircraft, Inc. (Piper) PA-23 series airplanes and all PA-31 and PA-42 series airplanes. This AD establishes life limits for safety- critical nose baggage door components. This AD also requires you to replace those safety-critical nose baggage door components and repetitively inspect and lubricate the nose baggage door latching mechanism and lock assembly. This AD results from several incidents and accidents, including fatal accidents, where the nose baggage door opening in flight was listed as a causal factor. We are issuing this AD to detect and correct damaged, worn, corroded, or non-conforming nose baggage door components, which could result in the nose baggage door opening in flight. The door opening in flight could significantly affect the handling and performance of the aircraft. It could also allow baggage to be ejected from the nose baggage compartment and strike the propeller. This failure could leadto loss of control.

The order itself the regulatory text, as published

Show the full text (5,282 characters)
2009-13-06 Piper Aircraft, Inc.: Amendment 39-15944; Docket No. FAA- 2009-0218; Directorate Identifier 2009-CE-006-AD. \n\nEffective Date \n\n\t(a) This AD becomes effective on July 24, 2009. \n\nAffected ADs \n\n\t(b) None. \n\nApplicability \n\n\t(c) This AD applies to Models PA-23, PA-23-160, PA-23-235, PA- 23-250, PA-23-250 (Navy UO-1), PA-E23-250, PA-31, PA-31-300, PA-31- 325, PA-31-350, PA-31P, PA-31P-350, PA-31T, PA-31T1, PA-31T2, PA- 31T3, PA-42, PA-42-720, and PA-42-1000 airplanes, all serial numbers, that are: \n\t(1) Certificated in any category; and \n\t(2) Equipped with a baggage door in the fuselage nose section (a nose baggage door). \n\nUnsafe Condition \n\n\t(d) This AD results from several incidents and accidents, including some fatal accidents, where the nose baggage door opening in flight was listed as a causal factor. We are issuing this AD to detect and correct damaged, worn, corroded, or non-conforming nose baggage door components, which could result in the nose baggage door opening in flight. The door opening in flight could significantly affect the handling and performance of the aircraft. It could also allow baggage to be ejected from the nose baggage compartment and strike the propeller. This failure could lead to loss of control. \n\nCompliance \n\n\t(e) To address this problem, you must do the following, unless already done: \n\n\nActions\nCompliance\nProcedures\n(1) For all aircraft:\n(i) inspect the nose baggage door assembly for damaged, worn, corroded, or non-conforming components;\n(ii) replace life-limited components specified in the service information; and\n(iii) install or inspect, as applicable, the nose baggage placard following the service information. \n(A) Initially: within 1,000 hours time-in-service (TIS) since all life-limited components were installed new following Piper Aircraft, Inc. Service Bulletin No. 1194A, dated November 10, 2008, or within the next 100 hours TIS after July 24, 2009 (the effective date of this AD), whichever occurs later; and \n(B) Repetitively thereafter: at intervals not to exceed 1,000 hours TIS.\nFollow INSTRUCTIONS: PART I of Piper Aircraft, Inc. Service Bulletin No. 1194A, dated November 10, 2008. As an alternative to using part number 100700-079 placard, you may fabricate a placard (using at least 1/8-inch letters) with the words in figure 1 of this AD and install the placard directly above the nose baggage door handle.\n(2) For all aircraft:\n(i) lubricate and inspect all nose baggage door latching and locking components for damaged, worn, corroded, or non-conforming components; and\n(ii) verify the key can only be removed from the lock assembly in the locked position in accordance with the service instructions.\n(A) Initially: within 100 hours TIS afterJuly 24, 2009 (the effective date of this AD); and\n(B) Repetitively thereafter: at intervals not to exceed 100 hours TIS. \nFollow INSTRUCTIONS: PART II of Piper Aircraft, Inc. Service Bulletin No. 1194A, dated November 10,2008.\n(3) For all aircraft with damaged, worn, corroded, or non-conforming components: repair/replace any damaged, worn, corroded, or non-conforming components.\nBefore further flight after any inspection required in paragraphs (e)(1) and (e)(2) of this AD where any evidence of damaged, worn, or corroded components was found.\nFollow Piper Aircraft, Inc. Service Bulletin No. 1194A, dated November 10, 2008.\n\n\n\n\n\n\nAlternative Methods of Compliance (AMOCs) \n\n\t(f) The Manager, Atlanta Aircraft Certification Office (ACO), FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. Send information to ATTN: Gregory K. Noles, Aerospace Engineer, One Crown Center, 1895 Phoenix Blvd., Suite 450, Atlanta, Georgia 30349; telephone: (770) 703-6085; fax: (770) 703-6097. Before using any approved AMOC on any airplane to which the AMOC applies, notify your appropriate principal inspector (PI) in the FAA Flight Standards District Office (FSDO), or lacking a PI, your local FSDO. \n\nMaterial Incorporated by Reference \n\n\t(g) You must use Piper Aircraft, Inc. Service Bulletin No. 1194A, dated November 10, 2008, to do the actions required by this AD, unless the AD specifies otherwise. \n\t(1) The Director of the Federal Register approved the incorporation by reference of this service information under 5 U.S.C. 552(a) and 1 CFR part 51. \n\t(2) For service information identified in this AD, contact Piper Aircraft, Inc., 2926 Piper Drive, Vero Beach, Florida 32960; telephone: (772) 567-4361; fax: (772) 978-6573; Internet: http:// www.newpiper.com/company/publications.asp. \n\t(3) You may review copies of the service information incorporated by reference for this AD at the FAA, Central Region, Office of the Regional Counsel, 901 Locust, Kansas City, Missouri 64106. For information on the availability of this material at the Central Region, call (816) 329-3768. \n\t(4) You may also review copies of the service information incorporated by reference for this AD at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call (202) 741-6030, or go to: http:// www.archives.gov/federal_register/code_of_federal_regulations/ ibr_locations.html.

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Source: FAA Dynamic Regulatory System, airworthiness directives. The FAA's document is the authority; the register counts are this site's, from the FAA register of October 5, 2026. Connections as data: /graph/directive/2009-13-06.json · aircraft systems.