Document ID: chunk:federal_register_of_legislation:F2006B02024:body:0
Version: federal_register_of_legislation:F2006B02024
Segment Type: other
Provision Reference: 
Character Range: 0–1127

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Gulfstream (Grumman American/ American Aviation) AA-1 Series Aeroplanes

AD/AA-1/13 Stall and Spin Placards - Installation 8/73

 Applicability: All models.

             Requirement: 1. Install a placard on the instrument panel in full view of the pilot stating "SPINS PROHIBITED".

             2. Install a placard worded as follows, and as applicable on the instrument panel adjacent to the Airspeed Indicator.

         Model AA-1A                 Model AA-1B
     STALL SPEED KTS. IAS.       STALL SPEED KTS. IAS.
               Bank Angle                 Bank Angle
 Condition                   0                         20  40  60   Condition   0   20  40   60
 Flaps Up                    54                         56    62  76    Flaps Up    56   58   64    79
 Flaps Down                  52                         54    59  74    Flaps Down  53   55   61    75
       1500 lbs Power Off          1560 lbs Power Off

 Compliance: Before 5 September 1973.