Airworthiness directives › 2010-12-04
AD 2010-12-04 Airworthiness Directives; PILATUS Aircraft Ltd. Model PC-7 Airplanes
Makes named: pilatus. Models named: PC-7. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
This AD applies to Model PC-7 airplanes, all serial numbers, certificated in any category.
Compliance
Unless already done, do the following actions: (1) Within the next 120 days after July 13, 2010 (the effective date of this AD), perform a visual inspection of the forward bonding points and the terminal lugs on the left and right lower longerons between fuselage frames 1 and 1A for signs of corrosion. Do the inspection following paragraphs 3.C.(1), (2), and (3) of PILATUS PC-7 Service Bulletin No. 53-007, dated January 5, 2010. (2) If any signs of corrosion are found during the inspection required in paragraph (f)(1) of this AD, prior to further flight, perform corrective actions in accordance with the Accomplishment Instructions in paragraph 3.D of PILATUS PC-7 SB No. 53-007, dated January 5, 2010. If the corrosion damage is out of limits, record the values; apply to PILATUS for a repair scheme at: PILATUS AIRCRAFT LTD., Customer Service Manager, CH-6371 STANS, Switzerland; telephone: +41 (0) 41 619 62 08; fax: +41 (0) 41 619 73 11; and implement the repair scheme. Note 1: The Federal Office of Civil Aviation (FOCA), which is the airworthiness authority for Switzerland, will work with PILATUS in reviewing the results of the initial inspection as specified in PILATUS PC-7 Service Bulletin No. 53-007, dated January 5, 2010. From this, a repetitive inspection requirement or other action may be established. The FAA will evaluate any such action and determine whether further rulemaking is necessary. FAA AD Differences Note 2: This AD differs from the MCAI and/or service information as follows: No differences. Other FAA AD Provisions (g) The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, Standards Office, 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: Doug Rudolph, Aerospace Engineer, FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329-4059; fax: (816) 329-4090. 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. (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. (3) Reporting Requirements: For any reporting requirement in this AD, under the provisions of the Paperwork Reduction Act (44 U.S.C. 3501 et seq. ), the Office of Management and Budget (OMB) has approved the information collection requirements and has assigned OMB Control Number 2120-0056. Related Information (h) Refer to MCAI FOCA AD HB-2010-001, dated February 12, 2010; and PILATUS PC-7 Service Bulletin No. 53-007, dated January 5, 2010, for related information. Material Incorporated by Reference (i) You must use PILATUS PC-7 Service Bulletin No. 53-007, dated January 5, 2010, 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 PILATUS AIRCRAFT LTD., Customer Service Manager, CH-6371 STANS, Switzerland; telephone: +41 (0) 41 619 62 08; fax: +41 (0) 41 619 73 11; Internet: http://www.pilatus-aircraft.com. (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. (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. Issued in Kansas City, Missouri, on May 27, 2010. Steven W. Thompson, Acting Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. 2010-13400 Filed 6-7-10; 8:45 am] BILLING CODE 4910-13-P
Required actions
Unless already done, do the following actions: (1) Within the next 120 days after July 13, 2010 (the effective date of this AD), perform a visual inspection of the forward bonding points and the terminal lugs on the left and right lower longerons between fuselage frames 1 and 1A for signs of corrosion. Do the inspection following paragraphs 3.C.(1), (2), and (3) of PILATUS PC-7 Service Bulletin No. 53-007, dated January 5, 2010. (2) If any signs of corrosion are found during the inspection required in paragraph (f)(1) of this AD, prior to further flight, perform corrective actions in accordance with the Accomplishment Instructions in paragraph 3.D of PILATUS PC-7 SB No. 53-007, dated January 5, 2010. If the corrosion damage is out of limits, record the values; apply to PILATUS for a repair scheme at: PILATUS AIRCRAFT LTD., Customer Service Manager, CH-6371 STANS, Switzerland; telephone: +41 (0) 41 619 62 08; fax: +41 (0) 41 619 73 11; and implement the repair scheme. Note 1: The Federal Office of Civil Aviation (FOCA), which is the airworthiness authority for Switzerland, will work with PILATUS in reviewing the results of the initial inspection as specified in PILATUS PC-7 Service Bulletin No. 53-007, dated January 5, 2010. From this, a repetitive inspection requirement or other action may be established. The FAA will evaluate any such action and determine whether further rulemaking is necessary. FAA AD Differences Note 2: This AD differs from the MCAI and/or service information as follows: No differences. Other FAA AD Provisions (g) The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, Standards Office, 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: Doug Rudolph, Aerospace Engineer, FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329-4059; fax: (816) 329-4090. 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. (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. (3) Reporting Requirements: For any reporting requirement in this AD, under the provisions of the Paperwork Reduction Act (44 U.S.C. 3501 et seq. ), the Office of Management and Budget (OMB) has approved the information collection requirements and has assigned OMB Control Number 2120-0056. Related Information (h) Refer to MCAI FOCA AD HB-2010-001, dated February 12, 2010; and PILATUS PC-7 Service Bulletin No. 53-007, dated January 5, 2010, for related information. Material Incorporated by Reference (i) You must use PILATUS PC-7 Service Bulletin No. 53-007, dated January 5, 2010, 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 PILATUS AIRCRAFT LTD., Customer Service Manager, CH-6371 STANS, Switzerland; telephone: +41 (0) 41 619 62 08; fax: +41 (0) 41 619 73 11; Internet: http://www.pilatus-aircraft.com. (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. (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. Issued in Kansas City, Missouri, on May 27, 2010. Steven W. Thompson, Acting Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. 2010-13400 Filed 6-7-10; 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.
- Bring your existing list in from a spreadsheet Paste the rows straight out of Excel. Headers like C/W Date and N/A are read for you.
- A copy that works when this does not One file. No internet, no login, no this software running. For the morning something has to be produced and the computer is not cooperating.
- $5 a month, or $50 a year Up to 50 aircraft on either.
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