AD/F100/31 - Flight Augmentation Computer Replacement
1AD/F100/31 - Flight Augmentation Computer Replacement
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/F100/31 - Flight Augmentation Computer Replacement.
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text
Fokker F100 (F28 Mk 100) Series Aeroplanes
AD/F100/31 Flight Augmentation Computer Replacement 4/99
Applicability: Model F.28 Mk.0100 aeroplanes serial numbers 11244 through 11348 inclusive.
Requirement: 1. Unless previously accomplished replace all Collins Flight Augmentation Computer (FAC) units, part number (P/N) 622-7478-321, with modified units P/N 622-7478- 401 Mod.11 in accordance with Fokker Service Bulletin (SB) F100-22-026 dated 1 July 1991.
- Replace all Collins FAC units, P/N 622-7478-401, with modified units P/N 622-7478-401 Mod.11 in accordance with Fokker SB F100-22-032 dated
2 September 1991.
Note: Netherlands AD 1991-057/4 refers.
Compliance: 1. Prior to 22 December 1999.
- Prior to 22 December 1999.
This Airworthiness Directive becomes effective on 22 April 1999.
Background: The modified computers provide improved fault isolation to allow cross comparison of more signals than previously possible. Problems with stabiliser trim systems during ground testing and nuisance yaw-damper faults during take off have been solved by the incorporation of an additional modification.