AD/A320/7 - Standby Generator Control Unit (GCU)
1AD/A320/7 - Standby Generator Control Unit (GCU)
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/A320/7 - Standby Generator Control Unit (GCU).
meta-content-style-type: text/css meta-content-type: application/xhtml+xml; charset=utf-8 meta-description: CASA Airworthiness Directive meta-generator: Aspose.Words for .NET 22.10.0 meta-keywords: Issue 5/1990,Aircraft above 5700 kg,Airbus Industrie A319, A320 and A321 Series Aeroplanes,Standby Generator Control Unit (GCU),7 title: Airworthiness Directive - AD/A320/7 - Standby Generator Control Unit (GCU)
?xml version="1.0" encoding="utf-8" standalone="no"?>
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text Airbus Industrie A319, A320 and A321 Series Aeroplanes
AD/A320/7 Standby Generator Control Unit (GCU) 5/90
Applicability: All A320-111, A320-211 and A320-231 aircraft.
Requirement: Action in accordance with Airbus Industrie Service Bulletins A320-24-1022 (mod 21052) and A320-24-1035 (mod 21736).
Note: DGAC AD 89-198-004(B) refers.
Compliance: Prior to 17 December 1990.
Background: Airbus Industrie have advised that the modifications contained in the referenced Service Bulletins are necessary to improve the lightning protection of the GCU in order to prevent malfunction.