Airworthiness Directives (ADs)

Aviation Industry

CAA-2006-04-012A

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: 2008/02/18

Applicability: McDonnell Douglas Model DC-8-11, DC-8- 12, DC-8-21, DC-8-31, DC-8-32, DC-8-33, DC-8-41, DC-8-42, and DC-8-43 Airplanes; Model DC-8F-54 and DC-8F-55 Airplanes; Model DC-8-50, -60, - 60F, -70, and -70F Series Airplanes; Model DC-9-10, -20, -30, -40, and -50 Series Airplanes; Model DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), and DC-9-87 (MD-87) Airplanes; and Model MD-88 Airplanes

Model Number: McDonnell Douglas Model DC-8-11, DC-8- 12, DC-8-21, DC-8-31, DC-8-32, DC-8-33, DC-8-41, DC-8-42, and DC-8-43 Airplanes; Model DC-8F-54 and DC-8F-55 Airplanes; Model DC-8-50, -60, - 60F, -70, and -70F Series Airplanes; Model DC-9-10, -20, -30, -40, and -50 Series Airplanes; Model DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), and DC-9-87 (MD-87) Airplanes; and Model MD-88 Airplanes

CAA AD Number: CAA-2006-04-012A

Aeronautics Authority of Original AD: FAA

Original AD Number: 2008-03-12

Effective Date: 2008/03/11

Subject: To prevent failure of the rudder pedal bracket assembly, which could result in the loss of rudder and braking control at either the captain's or first officer's position.

Reference Publications (Revision/ATA/SB): Supersedes AD 2006-07-25(CAA-2006-04-012). Ref. McDonnell Douglas DC-8 Alert Service Bulletin A27-273R1, R5; McDonnell Douglas DC-9 Alert Service Bulletin A27-307R1; Boeing Alert Service Bulletin DC9-27A307R7

Remarks

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