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Dash 1 chapter 2.csv
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Number of static wicks and placement
17 total
4 on each wing
9 on elevator
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
Do not connect external power with battery voltage below
22.0 V
Connect external power for battery voltage below
23.5 V
LOW AOA (amber donut)
10.5 units
HIGH AOA (green chevron)
18 units
Best cockpit cooling at altitudes below 7500 MSL
Set RAM AIR FLOW switch to OFF
PMU IOAT limit for start
121 C
Indications for IOAT above PMU limit
IOAT and ITT indicated by amber dashes
PMU FAIL annunciator illuminated
Use HIGH IOAT START procedure
80 C
Max ITT for auto start
130 C
Time for STARTER SWITCH MANUAL to cool IOAT or clear residual fuel
20 sec
Aural tones inaudible during engine start until
50% N1
Stay clear area from aircraft with engine running
3 feet
Time between GEN switch ON and AVIONICS MASTER switch ON
10 sec
Minimum idle on ground
60% N1
Prohibited range of stabilized prop speed on the ground
62-80% Np
Idle with PMU off during overspeed gov check
N1 stable between 60 and 70%
Approximate torque setting for overspeed gov check
30%
Np limit with PMU off during overspeed gov check
100 + 2%
Max amps limit for takeoff
+50 amps
Radius for inside gear w/NWS
15.5 feet
0.0 feet w/differential braking
Radius for nose wheel w/NWS
18.0 feet
8.3 feet w/differential braking
Radius for outside gear w/NWS
19.6 feet
8.6 feet w/differential braking
Radius for wingtip w/NWS
33.2 feet
21.0 feet w/differential braking
Minimum separation behind large A/C for wake turbulence avoidance
2 minutes
Setting to check engine instruments for T/O check
25-30% torque
Rotation attitude
7-10 degrees NH
Rotation speed with gusty winds
Half gust factor (up to 10 knots)
Best rate of climb (Vy)
140 KIAS
Increased visibility during climg
160-180 KIAS
Pitch and speed for obstacle clearance climb
15 degrees NH and 140 KIAS
Climb check altitude
10,000 feet
Increase in ITT w/defog on at any PCL setting
40 C
ITT limit as controlled by PMU
820 C
Required pressure differential above 18069 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
Descent rate with speed brake extended and idle power
8000-11000 fpm
Airspeed to break up rudder icing
170 KIAS
Recommended holding speed
120-150 KIAS
Time to allow for correction of attitude errors
1-2 min
Pressurization DUMP before landing at fields above
7500 MSL
Gusty wind threshold and touchdown speeds
Add half gust factor (up to 10 knots)
Normal touchdown speed (depending on flap setting)
75-105 KIAS
Lower nosegear to runway below __ KIAS unless needed to affect stopping distance
80 KIAS
Brake with great caution above this speed
80 KIAS
Time for ITT to stabilize before shutdown
1 min
Max time to apply power to pitot/AOA heating elements on ground
10 seconds
Min volume of MIL 85470 ice inhibitor to be added to fuel
0.5 pint/50 gal
Max slope approved for fueling
3 degrees
Time limit for LH and RH single point refueling precheck valves to shut
10 seconds
Ground power required
28-28.5 VDC
1000 amps for 5 sec
500 amps for 2 min
300 amps continuous
24.0-29.5 V for off-station
Main gear tire pressure (norm)
185 +/- 5 psi
Main gear tire pressure (max)
225+5 psi
Nose gear pressure
120+5 psi
Wind speed to consider hangaring A/C
80 knots
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Author
elitylski
ID
218686
Card Set
Dash 1 chapter 2.csv
Description
Dash 1 ch 2
Updated
2013-05-09T02:36:40Z
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