Airworthiness directives › 2015-02-05
AD 2015-02-05 Airworthiness Directives; The Boeing Company Airplanes
Models named: 717-200, MD-10-10F, MD-10-30F, MD-88, MD-90-30. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
This AD applies to all The Boeing Company airplanes identified in paragraphs (c)(1), (c)(2), and (c)(3) of this AD, certificated in any category. (1) The Boeing Company Model 717-200 airplanes. (2) The Boeing Company Model DC-10-10, DC-10-10F, DC-10-15, DC-10-30, DC-10-30F (KC-10A and KDC-10), DC-10-40, and DC-10-40F airplanes; and Model MD-10-10F and MD-10-30F airplanes. (3) The Boeing Company Model DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), and DC-9-87 (MD-87) airplanes; Model MD-88 airplanes; and Model MD-90-30 airplanes.
Compliance
Comply with this AD within the compliance times specified, unless already done.
Required actions
Within 30 days after the effective date of this AD, revise the maintenance or inspection program, as applicable, by incorporating the information specified in paragraphs (g)(1), (g)(2), or (g)(3) of this AD, as applicable. The initial compliance time for the tasks is within 18 months after the effective date of this AD. (1) For Model 717-200 airplanes; Model DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), and DC-9-87 (MD-87) airplanes; Model MD-88 airplanes; and Model MD-90-30 airplanes: Incorporate Special Compliance Item (SCI) 34-1, “Functional Test of the Captain and First Officer's Altimeter, of Appendix A—“SCIs” to Boeing Report No. MDC-92K9145, “Twinjet Special Compliance Items Report,” Revision M, dated February 5, 2013. (2) For Model DC-10-10, DC-10-10F, DC-10-15, DC-10-30, DC-10-30F (KC-10A and KDC-10), DC-10-40 and DC-10-40F airplanes: Incorporate SCI 34-4, “Functional Test of the Captain and First Officer's Altimeter,” of Appendix A—“SCIs” to Boeing Report No. MDC-02K1003, “Trijet Special Compliance Item Report,” Revision K, dated February 1, 2013. (3) For Model MD-10-10F and MD-10-30F airplanes: Incorporate SCI 34-4, “Functional Test of the Captain and First Officer's Altimeter, of Appendix A—“SCIs” to Boeing Report No. MDC-02K1003, “Trijet Special Compliance Item Report,” Revision K, dated February 1, 2013.
Unsafe condition
This AD was prompted by reports of latent air data transducer degradation. We are issuing this AD to prevent erroneous air data information, which could lead to a mid-air collision within reduced vertical separation minimum (RVSM) airspace.
Affected ADs
None.
Read the original on the Federal Register →
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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