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

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B02024 In force Legislative Instrument

Legislation content

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.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.