COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Cessna 150, F150, 152 & F152 Series Aeroplanes
AD/CESSNA 150/36
Amdt 1
Wing Flap Operating System 5/81
All models 150 M with S/Nos. 15078506 to 15079405 and F150 with S/Nos.
F15001339 to F15001428;
All models A150 M with S/Nos. A1500685 to A1500734 and FRA150 with S/Nos. FRA1500312 to FRA1500336;
All models 152 with S/Nos. 1527940 to 15283354 and F152 with S/Nos. F15201429 to F15201683;
All models A152 with S/Nos. A1520433 and A1520735 to A1520867, and FA152 with S/Nos. FA1520337 to FA1520357.
Modify the wing flap operating system by installing a Cessna P/N 0560037-1 flap follow-up cable clamp and associated hardware in accordance with instructions in Cessna SIL’s SE79-16 and SE79-16 (Supplement No. 1) and Cessna SK 172-60A.
SB Reims Aviation No. 21 and Bureau Veritas Consigne De Navigabilite 81- 46-1MP(A) and, FAA AD 80-06-03 Amendment 39-3713 refer.
1. For aeroplanes which have achieved 1000 hours time in service; unless already accomplished, within 100 hours time in service after 30 June 1981.
2. All other aeroplanes; before achieving 1000 hours time in service unless already accomplished.
The modification is required to prevent possible sudden unexpected retraction of the left wing flap. This amendment adds aeroplanes of Reims manufacture to the applicability list.