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60 Cards in this Set
- Front
- Back
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Max ramp weight?
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17,230 lbs.
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Max take off weight?
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17,120 lbs.
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Max landing weight?
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16,765 lbs.
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Max zero fuel weight?
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15,165 lbs.
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Forward section / aft. cargo max weight?
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1,000 lbs.
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Aft section / aft cargo max weight?
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630 lbs.
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Max weight in closet?
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250 lbs.
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Max weight on closet rod? (if installed)
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100 lbs.
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Floor load limit?
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100 lbs. per sq. ft.
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Va
Maneuvering speed? |
178 KIAS
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V Lo
Max landing gear operating speed? |
Extension 180 KIAS
Retraction 180 KIAS |
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V Le
Max landing gear extended speed? |
180 KIAS
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V mca
Air minimum control speed? Flaps 0 Flaps 17 |
Flaps 0......92 KIAS
Flaps 17....92 KIAS |
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V mo
Max operating speed Sea level to 13,200ft? 13,200 to 25,000ft? |
Sea level to 13,200ft.....248 KIAS
13,200 to 25,000ft........248-195* KIAS * .48 Mach |
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Limitations on the use of aviation gasoline?
4 items. |
150hrs. between engine overhauls.
Prohibited if either standby pump inop. Prohibited above 18,000ft. Standby pump must be ON for takeoff and landing. |
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Maximum Usable Fuel
Total Gallons? Pounds? |
665.4 gallons
4,484 lbs. |
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Maximum Usable Fuel
Each main tank Gallons? Pounds? |
240.5 gallons
1,621 lbs. |
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Maximum Usable Fuel
Each aux tank Gallons? Pounds? |
92.2 gallons
621 lbs. |
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Max fuel imbalance?
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200 lbs.
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Time limit for "L or R Fuel Press LO"
annunciator? |
10hrs before overhaul or replacement.
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Engine model number?
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PT6A-67D
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Max starting ITT
Temp? Time? |
1000 C
5 seconds. |
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Propeller diameter?
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110.0 inches.
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Maximum cabin differential pressure?
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5.1 psi.
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Landing gear cycle limit?
Cycles? Time limit? |
3 cycles.
2 minutes between first two cycles and 5 minutes each additional cycle. |
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Maximum airspeed for effective windshield anti-icing?
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223 KIAS
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Min. temperature for operation of deicing boots?
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-40 C
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Min. airspeed for sustained level flight in icing conditions is?
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160 KIAS
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Engine anti-ice for operations in ambient temperatures of?
2 items. |
+5 C or below and visible moisture.
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L or R FUEL PRES LO
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Fuel pressure less than 10 psi
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L or R OIL PRES
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Oil pressure below 60 psi
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L or R BL AIR FAIL
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EVA tubing has detected a rupture in the bleed air line or the system is off.
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CAB ALT HI
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Cabin altitude exceeds 10,000ft
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L or R ENVIR FAIL
2 Items. |
Bleed air overtemp (500 F) or overpressure (44 psi) in environmental system.
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L or R AC BUS
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AC bus has inoperative inverter or
L or R AC bus is not powered |
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A/P TRIM FAIL
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Out of trim or no trim command with autopilot on.
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LAVATORY SMOKE
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Smoke in lavatory (if installed)
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(Annunciator)
CABIN DOOR |
Cabin entry door is open or not secure.
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(Annunciator)
CARGO DOOR |
Cargo door is open or not secure.
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ARM EMER LITES
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Emergency light controls disarmed.
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CABIN DIFF HI
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Cabin differential exceeds 5.25 psi.
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A/P FAIL
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A failure has occurred in the selected APC-65 computer.
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L or R DC GEN
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Generator is off line.
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L or R FW VALVE
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Fuel valve has not reached the selected position.
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L or R ENG ICE FAIL
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Ice vane has not reached selected position.
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L or R FIRE LOOP
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Engine fire detection sense loop is open.
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L or R NO FUEL XFR
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No fuel transfer from auxiliary to main tank.
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L or R FUEL QTY
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Less than 324 pounds of usable fuel remaining in respective tank.
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L or R COL TANK LOW
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Less than 53 pounds of usable fuel remaining in respective tank.
(8 minutes cruise at 400lbs/hr.) |
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L or R BK DI OVHT
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EVA tubing has sensed bleed air leak in break de-ice line.
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L or R PITOT HEAT
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Pitot tube not receiving enough power to prevent icing or is not turned on.
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One-Engine-Inoperative
Best Angle-of-Climb (Vxse) |
122 kts
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One-Engine-Inoperative
Best Rate-of-Climb (Vyse) |
128 kts
(Decrease 2 knots per 5000 feet) |
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One-Engine-Inoperative
En Route Climb (Venr) |
123 kts
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Emergency Decent
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180 kts
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Maximum Range Glide
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140 kts
Glide Ratio: 2.0 nautical miles for every 1000ft of altitude. Decrease by .13 nautical miles for each 10 kts of headwind. |
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Fuel gages in yellow arc
Pounds? |
363 lbs.
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Torque Meter - Green Arc
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0 ft-lbs to 3750 ft-lbs
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Torque Meter - Yellow Arc
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3750 ft-lbs to 3950 ft-lbs
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Torque Meter - Red Arc
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3950 ft-lbs
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