Specifications Flashcards
Takeoff/Max Power Setting
Torque %: 100 max ITT*C: 820 max N1%: 104 max Np%: 100 max Oil Pressure: 90-120 psi Oil Temp (*C): 10-105
Idle Power Setting
Torque %: 1-10 ground ITT*C: 750 max N1%: 60-61 ground/67 min flight Np%: 46-50 ground Oil Pressure: 90psi min Oil Temp (*C): -40-105 ground/ 10-105 flt/106-110 (7)
Start Power Setting
ITTC: 871-1000 (5 sec)
Oil Pressure: 200psi max
Oil Temp (C): -40 min
Transient Power Setting
Torque %: 132 max (20 sec) ITT*C: 821-870 (20 sec) N1%: 104 max Np%: 110 (20 sec) Oil Pressure: 40-130 Oil Temp (*C): 106-110 (10 min)
With Power Management Unit (PMU) OFF, permissible maximum Np is __ +/- __%
100/2
Avoid stabilized ground operation from __ to __ % Np
62/80
Operation in this range permitted only during aerobatics or spins, and __ to __ psi for __ seconds with PCL at IDLE.
15/40/5
Normal oil pressure during steady-state conditions is __ to __ psi.
90/120
Operation at oil pressure less than __ psi at flight idle or above is indicative of oil system malfunction.
90
Torque at __% is a materials limit above which damage to the engine may occur.
132%
Torque above __% is indicative of a system malfunction
102%
Maximum airspeed gear down (V LE) and Flap Down (V FE)
150 KIAS
Max Operating (V MO)
316 KIAS
Max MACH (M MO)
0.67 Mach
Turbulent Air Penetration Speed, Max
207 KIAS
Prohibited Maneuvers
- Inverted stalls
- Inverted spins
3 Spins with PCL above idle - Spins with the landing gear, flaps, or speedbrake ext
- Spins with the PMU off
- Aggravated spins past two turns
- Spins below 10,000 ft pressure alt
- Spins above 22,000 ft pressure alt
- Abrupt cross-controlled (SNAP) maneuvers
- Aero maneuvers, spins, or stalls with a fuel imbalance greater than 50 lbs between wings
- Tail slides
The aircraft has been approved only for transit through ___ ft of ___ ice
5000/light rime
Minimum Battery Voltage
22 volts
Hydraulic Caution
<1800 psi, >3500 psi
Fuel Caution Light
<110 lbs in respective wing tank
Cockpit Pressurization Schedule Limit
3.6 +/- 0.2 psi
Starter duty cycle is limited to four ___ cycles
20 sec
Cooling period after first starter cycle
30 sec
Cooling period after second starter cycle
2 min
Cooling period after third starter cycle
5 min
Cooling period after fourth starter cycle
30 min
Inverted Flight Limit
60 sec
Intentional Zero G Flight Limit
5 sec
Negative G Operations Limit
60 sec
Do not exceed -2.5G for longer than __
30 sec
Min +Gs upright before additional -Gs
60 sec
Symmetric Clean
+7 to -3.5 Gs
Symmetric Gear and Flaps Extended
+2.5 to 0 Gs
Asymmetric Clean
+4.7 to -1 Gs
Asymmetric Gear and Flaps Extended
+2 to 0 Gs
For uncoordinated rolling maneuvers initiated at __ G, the max bank angle change is __ degrees
-1 / 180
Min Voltage for Battery Start
23.5 volts
Max Crosswind for Dry Runway
25 knots
Max Crosswind for Wet Runway
10 knots
Max Crosswind for Icy Runway
5 knots
Max Tailwind Component for Takeoff
10 knots
