EASA Regulations for Airbus A300

42 airworthiness directives and regulations affecting Airbus A300.

EASA SIB NE-10-37

Aug 2, 2010

General Electric - CF6-80C2 FADEC Fuel Metering Valve Resolver Feedback Faults

The General Electric - CF6-80C2 FADEC Fuel Metering Valve Resolver Feedback Faults Special Airworthiness Information Bulletin (SAIB NE-10-37) informs operators of airplanes equipped with GE CF6-80C2 series turbofan engines about potential engine in-flight shutdowns caused by fuel metering valve feedback faults. This bulletin applies to engines on Boeing 747, 767, Airbus A300, and McDonnell Douglas MD-11 aircraft, except Boeing 747 and 767 airplanes with FADEC software version 8.2.R or later. The bulletin provides guidance to prevent dual-channel faults that can lead to uncommanded engine shutdowns.

Safety Information Bulletin
  • Boeing 747
  • Boeing 767
  • Airbus A300
  • McDonnell Douglas MD-11

EASA SIB 2006-02

Apr 12, 2006

AIRBUS A300 aircraft series B2, B4, C4 and F4, except for the A300-600 series - Non-Conformance of maintenance requiring visual inspection of slat transmission shafts number 21 and asymmetry pick off units - DGAC F Airworthiness Directive No. F-2005-213R1

AIRBUS A300 aircraft series B2, B4, C4 and F4, except for the A300-600 series - Non-Conformance of maintenance requiring visual inspection of slat transmission shafts number 21 and asymmetry pick off units - DGAC F Airworthiness Directive No. F-2005-213R1 is an airworthiness directive issued by the DGAC, the French civil aviation authority. It applies to Airbus A300 aircraft series B2, B4, C4, and F4 and mandates a one-time visual inspection of slat transmission shafts number 21 and asymmetry pick off units to ensure proper connection and functionality.

Airworthiness Directive
  • Airbus A300