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-1 numbers chp2
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sufficient battery voltage for start
23.5 VDC
Minimum main gear strut extension
2.0 inches
Minimum nose gear strut extension
2.5 inches
– delay between ejections w/ISS in both
0.37 second
LOW AOA (amber donut)
10.5 units
– HIGH AOA (green chevron)
18 units
PMU limit for start
121 degrees C
use HIGH IOAT START procedure
80 degrees C
– max ITT for auto start
130 degrees C
time for STARTER SWITCH MANUAL to cool IOAT or clear residual fuel
20 seconds
stay clear area from aircraft with engine running
3 feet
– idle with PMU off during overspeed gov check
67% N1
– NP at approximately 30% torque during overspeed gov check
100%
NP limit with PMU off during overspeed gov check
100 ± 2%
max amps limit for T/O
+50 amps
degrees nose up for rotation
8-10
climbout pitch attitude
10-15 degrees NH
pitch and speed for obstacle clearance climb
15 degrees nose high and 140 KIAS
check OBOGS and defog
10,000 feet
increase in ITT w/defog on at any PCL setting
40 degrees C
– ITT limit as controlled by PMU
820 degrees C
pressure differential above 18,000 feet MSL
3.6 ± 0.2 psi
max fuel imbalance for pre-stall, spinning and aerobatic checks
50 lbs
power and descent rate desired for enroute descent
200-250 KIAS and 4000 fpm
speed on instrument approach before configuring and during missed approach
150 KIAS
speed on instrument final w/gear and flaps T/O
110 KIAS
check oil within how many min after landing
30 min
max time to apply power to pitot/AOA heating elements on ground
10 sec
min volume of MIL 85470 ice inhibitor to be added to fuel (½ pint/50 gal)
0.1-0.15%
max slope approved for fueling
3 degrees
time limit for LH and RH single point refueling precheck valves to shut
10 seconds
wind speed to consider hangaring A/C
80 knots
– max nose wheel deflection while towing
80 degrees
Author
C17FLYR
ID
62478
Card Set
-1 numbers chp2
Description
-1 numbers chp2
Updated
2011-02-10T00:51:32Z
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