Prohibited Maneuvers
1. Tail slides
2. Inverted spins
3. Inverted stalls
4. Aggravated spins > 2 turns
5. Abrupt cross-controlled (snap) maneuvers
6. Aerobatic maneuvers, spins, or stalls while fuel imbalance between wings >50 lbs
7. Spins with PCL above idle
8. Spins with la
Max airspeed with gear down/flaps extended
150 KIAS
Max operating airspeed (mach number)
316 KIAS (0.67 M)
Max turbulence airspeed
207 KIAS
Cooling periods after first/second/third/fourth starter cycle
30 seconds/2 min/5 min/30 min
Starter duty cycle is limited to 4 ____ cycles
20-second
Max allowable time in inverted flight
15 sec
Max allowable time in zero-G flight
5 sec
G force windows for:
1. Symmetric Clean
2. Symmetric Dirty
3. Asymmetric Clean
4. Asymmetric Dirty
1. (+7.0) to (-3.5)
2. (+2.5) to (0)
3. (+4.7) to (-1.0)
4. (+2.0) to (0)
Min voltage for battery start
23.5 V
Max crosswinds for:
1. Dry runway
2. Wet runway
3. Icy runway
1. 25 kts
2. 10 kts
3. 5 kts
Max tailwind for TO
10 kts
Min allowable battery voltage
22.0 V
Hydraulic caution window
<1800 psi
>3500 psi
Fuel caution window
< 110 lbs in respective tank
Cockpit pressurization schedule limit
3.6 (+/-) 0.2 psi
TORQUE %:
1. TO/Max
2. Idle
3. Start
4. Transient
1. 100%
2. 1-10% (ground); allowable torque range with Np stabilized and PCL at idle
3. ---
4. 131% (20 sec); torque at 131% is a material limit above which damage to the engine may occur. Torque above 102% is indicative of a system malfunction.
ITT (Celsius) Max:
1. TO/Max
2. Idle
3. Start
4. Transient
1. 820 �C
2. 750 �C
3. 1000 �C (5 sec)
4. 870 �C (20 sec)
N1 % (N1 values presented for PMU ON. With PMU OFF, N1 may vary from these values):
1. TO/Max
2. Idle
3. Start
4. Transient
1. 104% max
2. 60-61% (ground0; 67% min (flight)
3. ---
4. 104% max
Np% (Avoid stabilized ground operation from 62-80% Np):
1. TO/Max
2. Idle
3. Start
4. Transient
1. 100% (with PMU OFF, permissible maximum Np is 100 +/- 2%)
2. 46-50% (ground)
3. ---
4. 102% (20 sec) or 110% (permissible at all powers for completion of flight in emergency)
Oil Px (psi):
1. TO/Max
2. Idle
3. Start
4. Transient
1. 90-120 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)
2. 90 psi (min)
3. 200 psi (max)
4. 40-130 psi (Operation in th
Oil Temp (Celsius):
1. TO/Max
2. Idle
3. Start
4. Transient
1. 10-105
2. -40-105 (grnd); 10-105 (flt); 106-110 (Acceptable for ground operation at and below 20% torque)
3. -40 (min)
4. 106-110 (10 min)
The aircraft has been approved only for transit through _____ ft of _____ ice.
5000, light rime
With 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. Operation at oil pressure less than _____ psi at flight idle or above is indicative of oil system malfunction.
90, 120, 90
Acceptable for ground operation at and below _____% torque.
20
Torque at _____% is a materials limit above which damage to the engine may occur. Torque above _____ is indicative of a system malfunction.
131, 102