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42 Cards in this Set
- Front
- Back
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Engine Shaft Horsepower
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550
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Compressor Rotational Limits (N1)
Max Takeoff / Max Continuous / Cruise Climb |
101.5%
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Propeller Rotational Limits (2)
Max Takeoff / Max Continuous / Cruise Climb |
2200 rpm
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Approved Fuels
Commercial |
Jet A, Jet A-1, Jet B
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Approved Fuels
Military |
JP-4, JP-5
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Fuel:
System Capacity: Max Usable: |
387 gallons
384 gallons |
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Maximum Ramp Weight
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9,705 pounds
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Maximum Take Off Weight
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9,650 pounds
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Maximum Landing Weight
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9,168 pounds
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Maximum Zero Fuel Weight
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No Structural Limit
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Maximum Rear Baggae Compartment Weight
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350 pounds
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Max Operating Speed
(Vmo) |
208 KIAS
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Maveuvering Speed
(Va) |
169 KIAS
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Maximum Flap Speeds
35% (Approach Flap) 100% (Full Flap) |
178 KIAS
137 KIAS |
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Maximum Landing Gear Speeds
Extension Retraction |
156 KIAS
129 KIAS |
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Air Minimum Control Speed
(Vmca) |
90 KIAS
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Engine Model
|
PT6A - 21
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Starting Limit:
ITT |
1090°C
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Starting Limit:
Oil Temp |
-40°C (min)
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Shaft Horse Power
Take off / Max Continuous / Max Cruise |
550 SHP
(5 Minute limit for takeoff) (Max Continuous is intended for Emergency use) |
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Vxse - One engine inoperative best angle of climb
Vyse - one engine inoperative best rate of climb |
100 KIAS
107 KIAS |
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Emergency Descent
Maximum Range Glide Speed |
156 KIAS
125 KIAS |
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N1 Transient
|
102.6%
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ITT Takeoff/Max Continuous
Cruise |
695°C
635°C |
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Torque-Takeoff, Max Continuous
Torque-Transient |
1315 FT-LBS
1500 FT-LBS |
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Oil Temp - takeoff and max continuous thrust
Oil Pressure - takeoff and max continuous thrust |
10-99°C
80-100 PSI |
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APU Volts need to be _____ and capable to supplying ____amperes at a minimum of 16 DC volts during the start cycle
|
28.25 volts
1000 |
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Starter Limits
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40 seconds on, 60 seconds off, 40 seconds on, 60 seconds off, 40 seconds on, 30 minutes off
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Emergency Engine Fuels
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80 Red, 100 LL Blue, 100 Green, 115/145 Purple
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How much fuel must you have to takeoff?
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You cannot take off with fuel gauges in the yellow arc or if fuel quantity is less than 265 pounds in each wing system
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Fuel pressure Low limitation
|
If a fuel pressure annunciator is Illuminated, flight is limited to 10 hours before overhaul or replacement of the engine driven fuel pump.
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Fuel limits
Boost Pumps |
Boost Pumps must be operation prior to takeoff.
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Prop Speed Limits
- Transient - Reverse - Other |
2420 RPM
2100 RPM 2200 RPM |
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Prop overspeed limits
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max overspeed is 240 RPM limited to 5 seconds. Sustained speeds faster than 2200 RPM indicate failure in the primary governor and sustained speeds faster than 2288 indicate failure in the primary and overspeed governor
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Max Landing Weight
Max Zero Fuel Weight |
9168 lbs
No Structural limitation |
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Max Operating Pressure Altitude Limit
|
30,000 Feet
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Max Outside Air Temperature Limit
|
ISA + 37°C
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Maximum Cabin Differential Pressure
|
4.7 psi
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Landing Gear cycle limits
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1 gear cycle (1 up-1 down) limited to one oevery 3 minutes for a total of 10 cycles followed by a 15 minute cool down period
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Aft facing seats
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must be upright and headrest fully extended for takeoff and landing
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Minimum ambient temperature for operation of deicing boots
minimum airspeed for sustained Icing flight |
-40°C
140 KIAS |
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Icing Limitations
Flight in icing with flaps extended Engine Anti-ince |
Sustained flight in icing with flaps extended is prohibited except for approach and landings
Engine anti-ice shall be ON for operation in temperatures of +5°C or below when in flight free of visible moisture |
