-
Takeoff/Max
TORQUE %
ITT °C MAX
N1 %
NP %
OIL PRESSURE psi
OIL TEMP °C
- TORQUE % - 100 MAX
- ITT °C MAX - 820
- N1 % - 104
- NP % - 100
- OIL PRESSURE psi - 90 TO 120
- OIL TEMP °C - 10 TO 105
-
Idle
TORQUE %
ITT °C MAX
N1 %
NP %
OIL PRESSURE psi
OIL TEMP °C
- TORQUE % - 3 to 8%
- ITT °C MAX - 8750
- N1 % - 60 to 61 (ground), 67 min (flight)
- NP % - 46 to 50 (ground)
- OIL PRESSURE psi - 90 min
- OIL TEMP °C - -40 to 105 (ground), 10 to 105 (flight), 106 to 110
-
Start
TORQUE %
ITT °C MAX
N1 %
NP %
OIL PRESSURE psi
OIL TEMP °C
- TORQUE % - ---
- ITT °C MAX - 1000 (5 sec)
- N1 % - ---
- NP % - ---
- OIL PRESSURE psi - 200 MAX
- OIL TEMP °C - -40 min
-
Transient
TORQUE %
ITT °C MAX
N1 %
NP %
OIL PRESSURE psi
OIL TEMP °C
- TORQUE % - 131 (20 sec)
- ITT °C MAX - 870 (20 sec)
- N1 % - 104
- NP % - 102 (20 sec), 110
- OIL PRESSURE psi - 40 to 130
- OIL TEMP °C - 106 to 110 (10 mins)
-
TORQUE LIMITS
TAKEOFF/MAX
IDLE
START
TRANSIENT
- TAKEOFF/MAX 100 MAX
- IDLE 3 TO 8% (GROUND)
- -- Allowable torque range with Np stabilized and PCL at IDLE.
- START ---
- TRANSIENT 131 (20 sec)
- -- Torque at 131% is a materials limit above which damage to the engine may occur. Torque above 102% is indicative of a system malfunction.
-
ITT °C MAX
TAKEOFF/MAX
IDLE
START
TRANSIENT
- TAKEOFF/MAX 820
- IDLE 750
- START 1000 (5 sec)
- TRANSIENT 870 (20 sec)
-
N1 %
TAKEOFF/MAX
IDLE
START
TRANSIENT
- N1 % - N1 values presented for PMU ON. With PMU OFF, N1 may vary from these values.
- TAKEOFF/MAX 104 MAX
- IDLE 60 to 61 (ground), 67 MIN (flight)
- START ---
- TRANSIENT 104 MAX
-
NP %
TAKEOFF/MAX
IDLE
START
TRANSIENT
- NP % - Avoid stabilized ground operation from 62 to 80 % NP.
- TAKEOFF/MAX 100 MAX
- -- With PMU OFF, permissible maximum NP is 100 +/- 2 %.
- IDLE 46 to 50 (ground)
- START ---
- TRANSIENT 102 (20 sec),
- 110 -- Permissible at all powers for completion of flight in emergency.
-
OIL PRESSURE psi
TAKEOFF/MAX
IDLE
START
TRANSIENT
- TAKEOFF/MAX 90 to 120
- -- 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.
- IDLE 90 MIN
- START 200 MAX
- TRANSIENT 40 to 130
- -- Operation in this range permitted only during aerobatics or spins, and 15 to 40 psi for 5 seconds with PCL at IDLE.
-
OIL TEMP °C
TAKEOFF/MAX
IDLE
START
TRANSIENT
- TAKEOFF/MAX 10 to 105
- IDLE -40 to 105 (ground), 10 to 105 (flight),
- 106 to 110
-- Acceptable for ground operation at and below 20% torque. - START -40 MIN
- TRANSIENT 106 to 110 (10 Minutes)
-
MAXIMUM AIRSPEED GEAR DOWN (VLE) & FLAP DOWN (VFE)
150 KIAS
-
MAX OPERATING (VMO)
316 KIAS
-
-
TURBULENT AIR PENETRATION SPEED, MAXIMUM:
207 KIAS
-
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 FIRST STARTER CYCLE
30 min
-
Prohibited Maneuvers
- Inverted Stalls
- Inverted Spins
- Spins with PCL above IDLE
- Spins with the LANDING GEAR, FLAPS, or SPEEDBRAKE extended
- Spins with the PMU off
- Aggravated spins past two turns
- Spins below 10,000 feet Pressure Altitude
- Spins above 22,000 feet Pressure Altitude
- Abrupt Cross-Controlled (SNAP) maneuvers
- Aerobatic maneuvers, Spins, or Stalls with Fuel Imbalance greater than 50 pounds between the wings
- Tail Slides
-
The aircraft has been approved only for transit through _____ feet of ____ ice.
5000 feet of Light Rime Ice
-
Minimum Battery Voltage
22.0 Volts
-
-
Fuel Caution Light
<110 Pounds in respective wing tank
-
Cockpit Pressurization Schedule Limit
3.6 +/- 0.2 PSI
-
Inverted Flight Limitation
15 seconds
-
Intentional Zero G Flight
5 sec
-
Acceleration Limitation
Symmetric Clean
+7.0 to -3.5 Gs
-
Acceleration Limitation
Symmetric Gear and Flaps Extended
+2.5 to 0.0 Gs
-
Acceleration Limitation
Asymmetric Clean
+ 4.7 to -1.0 Gs
-
Acceleration Limitation
Asymmetric Gear & Flaps Extended
+2.0 to 0.0 Gs
-
Acceleration Limitation
For uncoordinated rolling maneuvers initiated at ___ Gs, the maximum bank angle change is ___ Degrees.
-
Min Voltage for Battery Start
23.5 Volts
-
Max crosswind for dry runway
25 KTS
-
Max crosswind for wet runway
10 KTS
-
Max Crosswind for icy runway
5 KTS
-
Max tailwind component for takeoff
10 KTS
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