Specifications

Question 1

Takeoff/Max Power Setting

Answer 1

Torque %: 100 max
ITT*C: 820 max
N1%: 104 max
Np%: 100 max
Oil Pressure: 90-120 psi
Oil Temp (*C): 10-105

Question 2

Idle Power Setting

Answer 2

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)

Question 3

Start Power Setting

Answer 3

ITTC: 871-1000 (5 sec)
Oil Pressure: 200psi max
Oil Temp (C): -40 min

Question 4

Transient Power Setting

Answer 4

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)

Question 5

With Power Management Unit (PMU) OFF, permissible maximum Np is __ +/- __%

Answer 5

100/2

Question 6

Avoid stabilized ground operation from __ to __ % Np

Answer 6

62/80

Question 7

Operation in this range permitted only during aerobatics or spins, and __ to __ psi for __ seconds with PCL at IDLE.

Answer 7

15/40/5

Question 8

Normal oil pressure during steady-state conditions is __ to __ psi.

Answer 8

90/120

Question 9

Operation at oil pressure less than __ psi at flight idle or above is indicative of oil system malfunction.

Answer 9

90

Question 10

Torque at __% is a materials limit above which damage to the engine may occur.

Answer 10

132%

Question 11

Torque above __% is indicative of a system malfunction

Answer 11

102%

Question 12

Maximum airspeed gear down (V LE) and Flap Down (V FE)

Answer 12

150 KIAS

Question 13

Max Operating (V MO)

Answer 13

316 KIAS

Question 14

Max MACH (M MO)

Answer 14

0.67 Mach

Question 15

Turbulent Air Penetration Speed, Max

Answer 15

207 KIAS

Question 16

Prohibited Maneuvers

Answer 16

1. Inverted stalls
2. Inverted spins
   3 Spins with PCL above idle
3. Spins with the landing gear, flaps, or speedbrake ext
4. Spins with the PMU off
5. Aggravated spins past two turns
6. Spins below 10,000 ft pressure alt
7. Spins above 22,000 ft pressure alt
8. Abrupt cross-controlled (SNAP) maneuvers
9. Aero maneuvers, spins, or stalls with a fuel imbalance greater than 50 lbs between wings
10. Tail slides

Question 17

The aircraft has been approved only for transit through ___ ft of ___ ice

Answer 17

5000/light rime

Question 18

Minimum Battery Voltage

Answer 18

22 volts

Question 19

Hydraulic Caution

Answer 19

<1800 psi, >3500 psi

Question 20

Fuel Caution Light

Answer 20

<110 lbs in respective wing tank

Question 21

Cockpit Pressurization Schedule Limit

Answer 21

3.6 +/- 0.2 psi

Question 22

Starter duty cycle is limited to four ___ cycles

Answer 22

20 sec

Question 23

Cooling period after first starter cycle

Answer 23

30 sec

Question 24

Cooling period after second starter cycle

Answer 24

2 min

Question 25

Cooling period after third starter cycle

Answer 25

5 min

Question 26

Cooling period after fourth starter cycle

Answer 26

30 min

Question 27

Inverted Flight Limit

Answer 27

60 sec

Question 28

Intentional Zero G Flight Limit

Answer 28

5 sec

Question 29

Negative G Operations Limit

Answer 29

60 sec

Question 30

Do not exceed -2.5G for longer than __

Answer 30

30 sec

Question 31

Min +Gs upright before additional -Gs

Answer 31

60 sec

Question 32

Symmetric Clean

Answer 32

+7 to -3.5 Gs

Question 33

Symmetric Gear and Flaps Extended

Answer 33

+2.5 to 0 Gs

Question 34

Asymmetric Clean

Answer 34

+4.7 to -1 Gs

Question 35

Asymmetric Gear and Flaps Extended

Answer 35

+2 to 0 Gs

Question 36

For uncoordinated rolling maneuvers initiated at __ G, the max bank angle change is __ degrees

Answer 36

-1 / 180

Question 37

Min Voltage for Battery Start

Answer 37

23.5 volts

Question 38

Max Crosswind for Dry Runway

Answer 38

25 knots

Question 39

Max Crosswind for Wet Runway

Answer 39

10 knots

Question 40

Max Crosswind for Icy Runway

Answer 40

5 knots

Question 41

Max Tailwind Component for Takeoff

Answer 41

10 knots