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2017-16-03: Wing Spar

FAA order 2017-16-03 is an airworthiness directive in force since August 9, 2017. The FAA's subject line: Wing Spar. It names Piper PA-46 Malibu, Mirage, Matrix and M-Class: about 1,692 aircraft on the U.S. register today, 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-46-600TP
On this site
Piper PA-46 Malibu, Mirage, Matrix and M-Class 1,692 registered

Dates and paperwork

In force since
August 9, 2017
Published
August 9, 2017 (signed July 28, 2017)
Docket
FAA-2017-0759
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. (Piper) Model PA-46-600TP (M600) airplanes. This AD requires inspection of the aft wing spars with repair as necessary. This AD was prompted by a report from Piper of the aft wing spar cracking during wing assembly. We are issuing this AD to address the unsafe condition on these products.

The order itself the regulatory text, as published

Show the full text (4,631 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): 2017-16-03 Piper Aircraft, Inc.: Amendment 39-18980; Docket No. FAA- 2017-0759; Product Identifier 2017-CE-023-AD. (a) Effective Date This AD is effective August 9, 2017. (b) Affected ADs None. (c) Applicability This AD applies to Piper Aircraft, Inc. Model PA-46-600TP (M600) airplanes; serial numbers 4698004 through 4698042; certificated in any category. (d) Subject Joint Aircraft System Component (JASC)/Air Transport Association (ATA) of America Code 5711, Wing Spar. (e) Unsafe Condition This AD wasprompted by a report from Piper Aircraft, Inc. (Piper) of an aft wing spar cracking during wing assembly of one of the affected airplanes. We are issuing this AD to prevent failure of the aft wing spar, which could lead to wing separation with consequent loss of control. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Inspection and Repair Before further flight, inspect the aft wing spars and, before further flight, repair as necessary following FAA-approved procedures obtained from the Atlanta ACO Branch approved specifically for this AD. Use the contact information found in paragraph (j) of this AD. We are coordinating with Piper on the development of inspection and repair procedures to address this unsafe condition. Piper Aircraft, Inc. Service Bulletin No. 1317, dated July 21, 2017 (not incorporated by reference), and Piper Service Bulletin No. 1317A, dated July 26, 2017, contain additional information relatedto this AD. (h) Special Flight Permit A special flight permit is allowed per 14 CFR 39.23 to relocate the airplane to a facility capable of performing the inspection and/ or repair required by paragraph (g) of this AD provided that all criteria in Part II of Piper Service Bulletin No. 1317A, dated July 26, 2017, are adhered to. (i) Alternative Methods of Compliance (AMOCs) (1) The Manager, Atlanta ACO Branch, 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 certification office, send it to the attention of the person identified in paragraph (j) 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. (j) Related Information For more information about this AD, contact William (Dan) McCully, Aerospace Engineer, Atlanta ACO Branch, FAA, 1701 Columbia Avenue, College Park, Georgia [[Page 37174]] 30337; phone: (404) 474-5548; fax: (404) 474-5606; email: william.mccully@faa.gov. (k) 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. (i) Piper Aircraft, Inc. Service Bulletin No. 1317A, dated July 26, 2017. (ii) Reserved. (3) For Piper Aircraft, Inc. 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, Policy and Innovation Division, 901 Locust, Kansas City, Missouri 64106. For information on the availability of this material at the FAA, call (816) 329-4148. It is also available on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2017-0759. (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

2018-11-21SW-18-31 · NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM
2016-12-13CE-17-02 · Cabin Altitude Encoder Alternative Method of Compliance (AMOC) to Airworthiness Directive (AD)...
2015-06-15CE-15-18 · WING SPAR Main Spar Lower Cap Cracks
2014-08-06CE-14-23 · Powerplant; Air Intake
2014-07-14CE-09-13R1 · POWERPLANT - ENGINE MOUNT Cracking at nose landing gear attachment and trunnion attachment

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/2017-16-03.json · aircraft systems.