TrackAD

Airworthiness directives › 2011-05-10

AD 2011-05-10 Airworthiness Directives; BAE Systems (Operations) Limited Model ATP Airplanes; BAE Systems (Operations) Limited Model HS 748 Airplanes

2011-03-25
2011-03-10
—
—
Airframe
—

Models named: ATP, HS 748 series 2A, series 2B. Read the applicability below — it usually turns on serial or part numbers too.

Applicability*9

This AD applies to all BAE Systems (Operations) Limited Model ATP airplanes and BAE Systems (Operations) Limited Model HS 748 series 2A and series 2B airplanes; certificated in any category.

Compliance

You are responsible for having the actions required by this AD performed within the compliance times specified, unless the actions have already been done. Inspection and Corrective Action (g) Within 90 days after the effective date of this AD: Do a detailed inspection of the aileron and rudder tab piano hinge pins to determine that each piano hinge pin is 0.120 inch (3.00 mm) shorter than the piano hinge at each end; and that the piano hinge ends have been pinched sufficiently to prevent the piano hinge migrating from the piano hinge, in accordance with the Accomplishment Instructions of BAE Systems (Operations) Limited Service Bulletin ATP-27-090, dated April 14, 2009; or BAE Systems (Operations) Limited Service Bulletin HS748-27-136, dated April 14, 2009, as applicable. (1) If any piano hinge pin is not 0.120 inch (3.00 mm) shorter than the piano hinge at each end, before further flight, cut to size, in accordance with Accomplishment Instructions of BAE Systems (Operations) Limited Service Bulletin ATP-27-090, dated April 14, 2009; or BAE Systems (Operations) Limited Service Bulletin HS748-27-136, dated April 14, 2009; as applicable. (2) If any piano hinge pin is not pinched sufficiently to prevent the piano hinge migrating from the piano hinge, before further flight, pinch the hinge, in accordance with Accomplishment Instructions of BAE Systems (Operations) Limited Service Bulletin ATP-27-090, dated April 14, 2009; or BAE Systems (Operations) Limited Service Bulletin HS748-27-136, dated April 14, 2009; as applicable. FAA AD Differences Note 1: This AD differs from the MCAI and/or service information as follows: No differences Other FAA AD Provisions (h) The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, International Branch, ANM-116, Transport Airplane Directorate, 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: Todd Thompson, Aerospace Engineer, International Branch, ANM-116, Transport Airplane Directorate, FAA, 1601 Lind Avenue, SW., Renton, Washington 98057-3356; phone: 425-227-1175; fax: 425-227-1149. Information may be e-mailed to: 9-ANM-116-AMOC-REQUESTS@faa.gov. 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. The AMOC approval letter must specifically reference this AD. (2) Airworthy Product: For any requirement in this AD to obtain corrective actions from a manufacturer or other source, use these actions if they are FAA-approved. Corrective actions are considered FAA-approved if they are approved by the State of Design Authority (or their delegated agent). You are required to assure the product is airworthy before it is returned to service. Related Information (i) Refer to Mandatory Continuing Airworthiness Information (MCAI) EASA Airworthiness Directive 2010-0035, dated March 04, 2010; BAE Systems (Operations) Limited Service Bulletin ATP-27-090, dated April 14, 2009; and BAE Systems (Operations) Limited Service Bulletin HS748-27-136, dated April 14, 2009; for related information. Material Incorporated by Reference (j) You must use BAE Systems (Operations) Limited Service Bulletin ATP-27-090, dated April 14, 2009; or BAE Systems (Operations) Limited Service Bulletin HS748-27-136, dated April 14, 2009; as applicable; to do the actions required by this AD, unless the AD specifies otherwise. (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. (2) For service information identified in this AD, contact BAE Systems (Operations) Limited, Customer Information Department, Prestwick International Airport, Ayrshire, KA9 2RW, Scotland, United Kingdom; telephone +44 1292 675207; fax +44 1292 675704; e-mail RApublications@baesystems.com; Internet http://www.baesystems.com/Businesses/RegionalAircraft/index.htm. (3) You may review copies of the service information at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington. For information on the availability of this material at the FAA, call 425-227-1221. (4) You may also review copies of the 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/code_of_federal_regulations/ibr_locations.html. Issued in Renton, Washington, on February 22, 2011. Kalene C. Yanamura, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 2011-5115 Filed 3-9-11; 8:45 am] BILLING CODE 4910-13-P

Read the original on the Federal Register →

You just looked this one up by hand

TrackAD holds all 12,278 of them and matches them against the aircraft you actually look after — airframe, engine, propeller and appliances in one pass — then works out what falls due and when.

Look round a real shop first Start free

The demonstration shop is eleven real aircraft with a year of work behind them. No account needed.

The directive text above is reproduced from the Federal Register, a work of the United States government and in the public domain. The separation into applicability, compliance and required actions is TrackAD's.*1