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Airworthiness Directives (ADs)

CAA-2016-02-003

The aircraft owner or operator shall comply with Airworthiness Directives issued by the CAA or the aeronautics authority of the State of Design (SoD) of the aviation products, appliances and parts, and take all necessary actions thereto.

Issue Date
2016/02/19
Applicability
(1) Model DC-9-11, DC-9-12, DC-9-13, DC-9-14, DC-9-15, and DC-9-15F airplanes. (2) Model DC-9-21 airplanes. (3) Model DC-9-31, DC-9-32, DC-9-32 (VC-9C), DC-9-32F, DC-9-33F, DC-9-34, DC 9 34F, and DC 9 32F (C-9A, C 9B) airplanes. (4) Model DC-9-41 airplanes. (5) Model DC-9-51 airplanes. (6) Model DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), and DC-9-87 (MD-87) airplanes. (7) Model MD-88 airplanes. (8) Model MD-90-30 airplanes.
Model Number
Boeing Model DC-9, MD-88 and MD-90 airplanes.
CAA AD Number
CAA-2016-02-003
Aeronautics Authority of Original AD
FAA
Original AD Number
2016-03-06
Effective Date
2016/03/23
Subject
FUEL - Install Ground Fault Interrupter Relays and Change Fuel Pump System Wiring
Reference Publications (Revision/ATA/SB)
(i) This AD replaces FAA AD 2012-18-05 (CAA-2012-09-006). (ii) Boeing Service Bulletin MD80-28-228, Revision 1, dated August 27, 2015. Boeing Service Bulletin MD90-28-013, Revision 1, dated August 27, 2015. Boeing Twinjet Special Compliance Item Report MDC-92K9145, Revision N, dated June 13, 2014, including Appendices A through D. McDonnell Douglas MD-80 Service Bulletin 28-53, Revision 1, dated April 16, 1992. McDonnell Douglas MD-80 Service Bulletin 28-63, Revision 2, dated April 8, 1992.
Remarks
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CAA-2016-02-003.pdf
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