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2017-02-06: Electrical Power/Electrical Power System Wiring

FAA order 2017-02-06 is an airworthiness directive in force since February 22, 2017. The FAA's subject line: Electrical Power/Electrical Power System Wiring. It names Piper PA-31 Navajo and Chieftain: about 935 aircraft on the U.S. register today, though an order usually covers particular versions or serial numbers rather than every one. System: electrical power.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
Piper Aircraft Inc.
Models
PA-31P-350, PA-31T, PA-31T1, PA-31T2, PA-31T3
On this site
Piper PA-31 Navajo and Chieftain 935 registered

Dates and paperwork

In force since
February 22, 2017
Published
February 7, 2017 (signed January 18, 2017)
Docket
FAA-2017-0045
Status
Current
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. Models PA-31T, PA-31T1, PA-31T2, PA-31T3, and PA- 31P-350 airplanes. This AD requires repetitive detailed visual inspections of the wiring below the main circuit breaker panel for proper clearance and evidence of damage and rerouting or replacing wires and/or parts as necessary. This AD was prompted by a fatal accident where evidence of thermal damage in this area was found. We are issuing this AD to correct the unsafe condition on these products.

The order itself the regulatory text, as published

Show the full text (5,680 characters)
Adoption of the Amendment Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows: PART 39--AIRWORTHINESS DIRECTIVES 0 1. The authority citation for part 39 continues to read as follows: Authority: 49 U.S.C. 106(g), 40113, 44701. Sec. 39.13 [Amended] 0 2. The FAA amends Sec. 39.13 by adding the following new airworthiness directive (AD): 2017-02-06 Piper Aircraft, Inc.: Amendment 39-18785; Docket No. FAA- 2017-0045; Directorate Identifier 2017-CE-002-AD. (a) Effective Date This AD is effective February 22, 2017. (b) Affected ADs None. (c) Applicability This AD applies to Piper Aircraft, Inc. Models PA-31T, serial numbers (SN) 31T-7400002 through 31T-8120104; PA-31T1, SNs 31T- 7804001 through 31T-8304003 and SNs 31T-1104004 through 31T-1104017; PA-31T2, SNs 31T-8166001 through 31T-8166076 and 31T-1166001 through 31T-1166008; PA-31T3, SNs 31T-8275001 through31T-8475001 and 31T- 5575001; and PA-31P-350, SNs 31P-8414001 through 31P-8414050; certificated in any category. (d) Subject Joint Aircraft System Component (JASC)/Air Transport Association (ATA) of America Code 2497, Electrical Power/Electrical Power System Wiring. (e) Unsafe Condition This AD was prompted by a fatal accident where evidence of thermal damage in the area below the main circuit breaker panel was found. We are issuing this AD to detect and correct rubbing/chafing of wiring with other wires, adjacent structure, and/or flammable fuel lines, which could lead to electrical arcing and possible inflight fire in an area that is not accessible by the crew. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Inspection (1) Within 30 days after February 22, 2017 (the effective date of this AD) and repetitively thereafter at intervals not to exceed 12 calendar months, do a detailed visual inspection of the wiring in the area below the main circuit breaker panel using mirrors, a suitable light source, and other equipment (small cameras, borescopes, and magnification, etc.,) as needed to do the visual inspection of the area. Follow paragraphs 1, 2, and 3 of the Instructions section of Piper Aircraft, Inc. Service Bulletin No. 1301, dated January 6, 2017. Note 1 to paragraph (g)(1) of this AD: You may begin the repetitive inspections before 12 calendar months after the initial inspection to coincide the repetitive inspection with the annual inspection. (2) If any damage and/or rubbing or chafing is found during any of the inspections required in paragraph (g)(1) of this AD, before further flight, reroute, rework, or replace any wires as specified in paragraphs 2 and 3 of the Instructions section of Piper Aircraft, Inc. Service Bulletin No. 1301, dated January 6, 2017. (3) Perform a functional test after any inspection required by this AD as specified in paragraph 4 of the Instructions section of Piper Aircraft, Inc. Service Bulletin No. 1301, dated January 6, 2017. (4) The Summary section of Piper Aircraft, Inc. Service Bulletin No. 1301, dated January 6, 2017, states to contact the Factory Authorized Piper Service Facility to make arrangements for compliance with the service bulletin. Any appropriately licensed mechanic may do the work of this AD. Please note that to receive any warranty credit from Piper, the work may need to be done at the Factory Authorized Service Facility. (h) Alternative Methods of Compliance (AMOCs) (1) 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. In accordance with 14 CFR 39.19, send your request to your principal inspector or local Flight Standards District Office, as appropriate. If sending information directly to the manager of the ACO, send it to the attention of the person identified in paragraph (i) of this AD. (2) Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the local flight standards district office/certificate holding district office. (i) Related Information For more information about this AD, contact Bryan Long, Aerospace Engineer, FAA, Atlanta Aircraft Certification Office, 1701 Columbia Avenue, College Park, Georgia 30337; phone: (404) 474-5578; fax: (404) 474-5606; email: bryan.long@faa.gov. (j) Material Incorporated by Reference (1) The Director of the Federal Register approved the incorporation by reference (IBR) of the service information listed in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51. (2) You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise. [[Page 9501]] (i) Piper Aircraft, Inc. Service Bulletin No. 1301, dated January 6, 2017. (ii) Reserved. (3) For service information identified in this AD, contact Piper Aircraft, Inc., Customer Service, 2926 Piper Drive, Vero Beach, Florida 32960; telephone: (877) 879-0275; fax: none; email: customer.service@piper.com; Internet: www.piper.com. (4) You may view this referenced service information at the FAA, Small Airplane Directorate, 901 Locust, Kansas City, Missouri 64106. For information on the availability of this material at the FAA, call (816) 329-4148. (5) You may view this service information that is incorporated by reference 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/cfr/ibr-locations.html.

Related safety bulletins advice on the same designs, not orders

2016-12-16CE-17-05 · Electrical Power/Electrical Power System Wiring
2013-12-12CE-14-07 · WING SPAR Main Spar Lower Cap Cracks
2008-01-09CE-08-11 · Landing Gear
2006-01-20CE-06-22 ·
2004-09-13CE-04-86 ·

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 7, 2026. Connections as data: /graph/directive/2017-02-06.json · aircraft systems.