COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Fuji FA-200 Series Aeroplanes
AD/FA-200/3 Propeller Blade Inspection NK and Operating Restriction
Applicability: All model FA-200-180 with S/Nos. 3 to 75 fitted with McCauley B2D34C53/74E propellers.
Requirement: 1. Visually inspect blades for damage with the aid of a 10 power (2 1/2X) glass for defects such as erosion, scratches, nicks, cracks, etc. Rectify as necessary. After rectification dye penetrant inspect the entire blade from hub to tip.
Note: This work can be performed without removing the propeller from the engine.
2. Install a placard on the instrument panel adjacent to the RPM indicator reading as follows:
“AVOID CONTINUOUS OPERATION WHILE DESCENDING BETWEEN 2250 AND 2250 RPM WITH MANIFOLD PRESSURE SETTINGS BELOW 15 INCHES Hg.”
Note: Fuji SB No. FAS.008 dated 6 December 1969 and McCauley SB No. 76 dated 28 November 1969 also refer.
Compliance: Within 25 hours time in service after 4 March 1970.