Torque %

during

Takeoff/Max

100%

Torque %

during

Idle

(ground)

3% to 8%

*Allowable torque range with Np stabilized and PCL at IDLE

Torque % 

during

Transient

131% (for 20 secs)

*Torque at 131% is a materials limit. Torque above 102% is indicative of a systems malfunction

ITT°C MAX 

during

Takeoff/MAX

820°C

ITT°C MAX

during 

IDLE

750°C

ITT°C MAX

during 

START

1000°C (for 5secs)

ITT°C

during 

TRANSIENT

870°C (for 20 secs)

N₁% (PMU ON)

during

TAKEOFF/MAX

104% MAX

N₁% (PMU ON)

during

IDLE

60 to 61 (ground)

67 Min (flight 

N₁% (PMU ON)

during

TRANSIENT

104% MAX

Np%* TAKEOFF/MAX

Avoid stabilized ground operations from 62 to 80% N_p

100% MAX

(with PMU OFF, permissible max N_p is 100 ± 2%)

Np%* IDLE

Avoid stabilized ground operations from 62 to 80% N_p

46% to 50% (ground)

Np%* TRANSIENT

Avoid stabilized ground operations from 62 to 80% N_p

102% (for 20 secs)

110% (Permissible at all powers for completion of flight in emergency)

OIL Pressure 

during

TAKEOFF/MAX

90 to 120 psi

(Normal oil pressure during steady state conditions is 90 to 120 psi. Operation at oil pressure less than 90 psi at flight idle or above is indicative of oil system malfunction)

OIL Pressure 

during

IDLE

90 psi (min)

OIL Pressure 

during

START

200 psi (MAX)

OIL Pressure 

during

TRANSIENT

40 to 130 psi

(Operation in this range permitted only during aerobatics or spins, and 15 to 40 psi for 5 seconds with PCL at IDLE)

OIL TEMPºC psi

during 

TAKEOFF/MAX

10ºC to 105ºC

OIL TEMPºC psi

during 

IDLE

-40ºC to 105ºC(ground)

10ºC to 105ºC (flight)

106ºC to 110ºC (for 10 minutes)*

*Acceptable for ground operations at and below 20% torque

OIL TEMPºC psi

during 

START

-40ºC Min

OIL TEMPºC psi

during 

TRANSIENT

106ºC to 110ºC (for 10 minutes)

1. Inverted Stalls

2. Inverted Spins

3. Spins with PCL above IDLE

4. Spins with the landing gear, flaps, or speed brake extended

5. Spins with the PMU OFF

6. Aggravated spins past two turns

7. Spins below 10,000ft PA

8. Spins above 22,000ft PA

9. Abrupt cross-controlled (snap maneuvers)

10. Aerobatic manuevers, spins, or stalls with a fuel imbalance greater than 50 pounds between wings

11. Tail slides

1. Min voltage for battery start: 23.5V

2. Max crosswind for dry runway: 25KT

3. Max crosswind for wet runway: 10KT

4. Max crosswind for icy runway: 5KT

5. Max tailwind component for takeoff: 10KT

Symmetric Clean:  +7.0  to  -3.5 G's

Symmetric Dirty:  +2.5  to   0.0 G's

Asymmetric Clean: +4.7  to  -1.0 G's

Asymmetric Dirty: +2.0  to   0.0 G's

Inverted Flight:          15 sec

Intentional zero G flight: 5 sec

Starter cycle limitation

Starter duty cycle is limited to four 20 sec cycles

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

150 KIAS

MAX operating (V_MO)

MAX MACH (M_MO)

316 KIAS

0.67 MACH

207 KIAS

22.0V

less than 1800 psi

greater than 3500 psi

Less than 110 pounds

(in respective wing)

3.6 ± 0.2 psi

5000 ft 

RIME