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-1 number chp 5,6,7,apndx
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– Max turbulence penetration A/S
195 KIAS
– Symmetric Vo
227 KIAS
Asymmetric Vo 5 seconds
177 KIAS
– Max ramp weight
6550
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)
Dry RCR
23
Wet RCR
12
Ice/standing water RCR
5
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
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Author
C17FLYR
ID
62488
Card Set
-1 number chp 5,6,7,apndx
Description
-1 number chp 5,6,7,apndx
Updated
2011-02-10T00:59:48Z
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