IFS OPS LIMITS RED Flashcards
0
Q
Min. Engine out airspeed to sustain windmilling prop
A
60
1
Q
Forced landing final approach airspeed (flaps LDG)
A
55
2
Q
Forced landing final approach airspeed (flaps T/O)
A
60
3
Q
Forced landing final approach airspeed (flaps CRUISE)
A
64
4
Q
Best glide airspeed (1764 lbs) (L/D max)
A
73
5
Q
Vfe (flaps LDG) (max airspeed with flaps extended)
A
78
6
Q
Vfe (flaps TO) (max airspeed with flaps extended)
A
100
7
Q
Va (1764 lbs) (no abrupt mvmts, over stress conditions occur)
A
106
8
Q
Vno (max structural cruising speed)
A
118
9
Q
Force propellor to windmill if stopped, starter inop
A
137
10
Q
Vne (never exceed airspeed)
A
164
11
Q
Max permissible bank angle for steep turns
A
60 degrees
12
Q
Voltmeter green arc (volts)
A
12.5 - 16.1
13
Q
Usable fuel (US gal)
A
24.0
14
Q
Max takeoff weight (lbs)
A
1764
