Airworthiness directives › 2009-07-09
AD 2009-07-09 Airworthiness Directives; DORNIER Luftfahrt GmbH Models Dornier 228-100, Dornier 228-101, Dornier 228-200, Dornier 228-201, Dornier 228-202, and Dornier 228-212 Airplanes
Applicability*9
This AD applies to Dornier 228-100, Dornier 228-101, Dornier 228-200, Dornier 228-201, Dornier 228-202, and Dornier 228-212 airplanes, all serial numbers, certificated in any category.
Compliance
Unless already done, do the following actions: (1) Within the next 10 hours time-in-service (TIS) after May 11, 2009 (the effective date of this AD), do the inspection for “unequal aileron steering wheel force” in accordance with paragraphs 2.A.(1) through 2.A.(3) of the ACCOMPLISHMENT INSTRUCTIONS of RUAG Aerospace Defence Technology Dornier 228 Service Bulletin No. SB-228-275, Revision No.: 0, dated October 8, 2008. If any defect is found, before further flight, modify the attachment bracket riveting in accordance with paragraph 2.B. of the ACCOMPLISHMENT INSTRUCTIONS of RUAG Aerospace Defence Technology Dornier 228 Service Bulletin No. SB-228-275, Revision No.: 0, dated October 8, 2008. (2) Within 300 hours TIS after May 11, 2009 (the effective date of this AD), unless accomplished as required per paragraph (f)(1) of this AD, modify the attachment bracket riveting in accordance with paragraph 2.B. of the ACCOMPLISHMENT INSTRUCTIONS of RUAG Aerospace Defence Technology Dornier 228 Service Bulletin No. SB-228-275, Revision No.: 0, dated October 8, 2008. FAA AD Differences Note: 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: Greg Davison, Glider Program Manager, FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329-4130; 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 European Aviation Safety Agency AD No.: 2008-0217, dated December 10, 2008; and RUAG Aerospace Defence Technology Dornier 228 Service Bulletin No. SB-228-275, Revision No.: 0, dated October 8, 2008, for related information. Material Incorporated by Reference (i) You must use RUAG Aerospace Defence Technology Dornier 228 Service Bulletin No. SB-228-275, Revision No.: 0, dated October 8, 2008, 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 RUAG Aerospace Services GmbH, Dornier 228 Customer Support, P.O. Box 1253, 82231 Wessling, Federal Republic of Germany, telephone: +49 (0) 8153-30-2280; fax: +49 (0) 8153-30-3030; E-mail: custsupport.dorner228@ruag.com ; Internet: http://www.ruag.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 March 24, 2009. John Colomy, Acting Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. E9-7071 Filed 4-3-09; 8:45 am] BILLING CODE 4910-13-P
Required actions
Unless already done, do the following actions: (1) Within the next 10 hours time-in-service (TIS) after May 11, 2009 (the effective date of this AD), do the inspection for “unequal aileron steering wheel force” in accordance with paragraphs 2.A.(1) through 2.A.(3) of the ACCOMPLISHMENT INSTRUCTIONS of RUAG Aerospace Defence Technology Dornier 228 Service Bulletin No. SB-228-275, Revision No.: 0, dated October 8, 2008. If any defect is found, before further flight, modify the attachment bracket riveting in accordance with paragraph 2.B. of the ACCOMPLISHMENT INSTRUCTIONS of RUAG Aerospace Defence Technology Dornier 228 Service Bulletin No. SB-228-275, Revision No.: 0, dated October 8, 2008. (2) Within 300 hours TIS after May 11, 2009 (the effective date of this AD), unless accomplished as required per paragraph (f)(1) of this AD, modify the attachment bracket riveting in accordance with paragraph 2.B. of the ACCOMPLISHMENT INSTRUCTIONS of RUAG Aerospace Defence Technology Dornier 228 Service Bulletin No. SB-228-275, Revision No.: 0, dated October 8, 2008. FAA AD Differences Note: 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: Greg Davison, Glider Program Manager, FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329-4130; 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 European Aviation Safety Agency AD No.: 2008-0217, dated December 10, 2008; and RUAG Aerospace Defence Technology Dornier 228 Service Bulletin No. SB-228-275, Revision No.: 0, dated October 8, 2008, for related information. Material Incorporated by Reference (i) You must use RUAG Aerospace Defence Technology Dornier 228 Service Bulletin No. SB-228-275, Revision No.: 0, dated October 8, 2008, 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 RUAG Aerospace Services GmbH, Dornier 228 Customer Support, P.O. Box 1253, 82231 Wessling, Federal Republic of Germany, telephone: +49 (0) 8153-30-2280; fax: +49 (0) 8153-30-3030; E-mail: custsupport.dorner228@ruag.com ; Internet: http://www.ruag.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 March 24, 2009. John Colomy, Acting Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. E9-7071 Filed 4-3-09; 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