-
– Max turbulence penetration A/S
195 KIAS
-
-
Asymmetric Vo 5 seconds
177 KIAS
-
-
Max zero fuel weight
5500
-
– Max descent rate at touchdown
780 fpm
-
– Min / Max Pilot weight (Nude) for ejection seat
103 - 245 lbs
-
Min / Max Pilot weight (with equipment) for ejection seat
121- 271 lbs
-
utilize half lateral stick inputs or less performing sustained elevated G rolls
>180 KIAS
-
sink rate at best glide, clean
1100 to 1300 fpm
-
best glide, gear down, flaps/SB up
105 KIAS
-
sink rate at best glide w/gear down
1500 fpm
-
– zero thrust power setting
4 to 6% torque
-
full right rudder and full right aileron may not prevent a left roll off at stall
>60% torque
-
altitude loss during six turn, steady-state spin
4500’
-
nose high pitch for best spin entry
15° to 20°
-
per turn, stabilized spin
2 - 3 seconds, 400’ to 500’, 120 KIAS, 18 AOA
-
– aggravated spin
70° nose down, 280°/second turn
-
altitude loss for spins
500’/turn, 1500’ to 200’ dive recovery
-
Recommended turbulence/t–storm penetration airspeed
180 KIAS
-
Windshear T/O
VROT + (up to)10
-
– Windshear approach
VAPP + (up to) 10
-
Approach/landing speed with ice accumulation on aircraft
VAPP + 10(min)
-
Windshear recovery
15° pitch/110 KIAS min/10.5 AOA max/PCL MAX
-
Operations in visible moisture should be avoided within what temps
5° C/41° F (or below)
-
hydroplaning can occur
<0.1 inch of slush or water
-
– nose tire hydroplane
>85 knots
-
– main tire hydroplane
>115 knots
-
In what temp will Power-up of the digital instruments may shorten instrument service life
<-21° C (-6° F)
-
– Remove battery
-29° C (-20° F)
-
-
-
-
Maximum brake energy absorption capability
3.96 Million Foot-lbs
-
Max abort speed reaction time
6 seconds (3 sec decision/3 sec application)
-
Airspeed increase during 6 second reaction at max abort speed
20 knots
|
|
