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37 Cards in this Set
- Front
- Back
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Minimum control speed Vmca flaps 10 |
64 kias |
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Climb speed Vx flaps 10 |
87 kias |
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Climb speed best rate Vy flaps 0 |
100 kias |
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Climb speed single engine Vyse flaps 10 |
80 kias |
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Flaps extended speed Vfe Flaps 10 Flaps 10-37 |
103 93 |
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Maximum operating speed Vmo |
166 kias to 6700 feet 156 kias 6700-10000 feet 141 kias 10000-15000 feet |
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Maneuvering speed Vp Gust penetration speed Vb |
132 kias |
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Take Off SHP Tq T5 Ng Np Oil Press Oil Temp |
620 shp Tq 50 psi T5 790 c Ng 101.6 % Np 96 % Oil Press 85-105 psi Oil Temp 10-99 c |
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MAX Climb/Cruise SHP Tq T5 Ng Np Oil Press Oil Temp |
585 shp Tq 50 psi T5 740 c Ng 101.6 % Np 91 % Oil Press 85-105 psi Oil Temp 0-99 c |
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MAX Continuous SHP Tq T5 Ng Np Oil Press Oil Temp |
585 shp Tq 50 psi T5 765 c Ng 101.6 % Np 91 % Oil Press 85-105 psi Oil Temp 0-99 c |
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Idle T5 Oil Press Oil Temp |
T5 685 c Oil Press 40 Min Oil Temp -40-99 c |
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Starting T5 Oil |
T5 1090 Oil Temp -40 Min |
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Acceleration Tq T5 Ng Np Oil Press Oil Temp |
Tq 68.4 psi T5 825 c Ng 102.6 % Np 110 % Oil Press 85-105 psi Oil Temp 0-99 c |
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Max Reverse SHP Tq T5 Ng Np Oil Press Oil Temp |
620 shp Tq 50 % T5 790 c Ng 101.6 % Np 91 +-1 % Oil Press 85-105 psi Oil Temp 0-99 c |
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Generator Load Limits |
160 amps on ground OAT greater than 7 c, for cooling 200 amps on ground OAT 7 c or less, for cooling 200 amps in flight any temp generator capacity |
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Starter Limitations |
25 seconds ON, 1 minute OFF, then 25 seconds ON, 1 minute OFF, then 25 seconds ON, followed by 30 minutes off for cooling. |
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Jump Door Limits |
Closed for take off and landing 140 KIAS with door open Door open for use, 140 KIAS Flaps 20 |
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MAX Altitude |
25000 feet 24380 feet both engines operating, 12500 lbs |
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Weights Take Off Landing Zero Fuel |
12500 Take Off 12300 Landing 12300 Zero Fuel |
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Baggage Loads Forward Aft Shelf |
Forward 285 lbs Aft 500 lbs which includes the 150 limit on the shelf |
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Floor Loading |
Cabin 200 lbs sq ft Forward and Rear 100 lbs sq ft |
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Flap Limits Take Off Landing Ice |
10 for take off 20-37 for landing Landing in ice 10 |
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Fuel Capacity Forward Aft |
Forward Tank 1235 pounds / 574 kg Rear Tank 1341 pounds / 608 kg |
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Dimensions Wing Span Length Cabin Height Tail Height |
Wing Span 65 feet (19.8 m) Length 51 feet, 9 inches (15.8 m) Cabin Height 9 feet, 8 inches (2.95 m) Tail Height 19 feet, 9 inches (6.02 m) |
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Describe Electrical System |
The electrical system is a 28 volt, direct current, single wire installation with the airframe used as ground return. The aircraft is entirely 28 volt powered. There are no inverters or fuses. Primary DC power is supplied by two engine-driven starter-generators. A 48-amp-hour battery provides power when the generators are inoperative. Electrical power is distributed through a multiple bus system consisting of left, right, hot battery,and battery/external power busses. |
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Describe Fuel System |
Fuel is contained in forward and aft fuselage tanks located in the lower fuselage beneath the cabin floor. A filler neck and cap for each tank is provided on the left side of the fuselage. Each tank consists of four interconnected flexible rubber cells, one of which is a collector cell (cell number 4 forward and cell number 5 aft) into which fuel is transferred from the other cells through a boost pump operated ejector. The fuel is delivered by boost pumps to the engines. All cells are vented to atmosphere. Each Collector cell contains two boost pumps, a float switch, and a level control valve. Every Cell contains a capacitance probe. |
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Describe FIre Warning and Extinguishing System |
Fire detecting and extinguishing systems are installed in both engine nacelles to provide warning of fire and means to extinguish a fire. Fire detection is by means of detection units in each nacelle, any one of which, if closed by heat, activates a warning light in the fire extinguisher push button of the affected engine. An aural warning, consisting of the word FIRE, is provided concurrent with illumination of either fire warning pushbutton.The system incorporates a test switch for visually checking the operation of the firewarning pushbuttons and the aural warning.
A single fire extinguisher bottle is installed in each nacelle. Each bottle, when operated,discharges its contents (bromotriflouromethane, also known as Halon 1301 or CF3Br)through a pipe into the engine accessories compartment. Indication of fire extinguisher bottle discharge is provided in the form of two coloured discs on the inboard side of each nacelle. The detecting units are powered from the left DC bus through FIREDETECTION L and R circuit breakers (positions C11 and D11, respectively), and the extinguisher circuits from the same supply through FIRE EXTINGUISHER L and R circuit breakers (positions C10 and D10, respectively).
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Describe Hydraulics System |
The hydraulic system operates the wing flaps, nose wheel steering, wheel brakes and(if installed) the wheel-skis.
The electric motor-driven hydraulic pump is powered from the left DC bus. It maintains the damping and brake accumulators at a working pressure in response to pressures sensed by the pressure switch. When pressure falls between 150 to 300 PSI below the normal system pressure of 1,500 PSI, the motor-driven pump is energized and pressurizes the accumulators to 1575 ± 50 PSI, at which pressure the pump is deenergized.
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High T5, Hung Start, No Light Up During Start |
1. FUEL LEVER (Affected Engine) -------------------------------------------------------------------- OFF 2. START SWITCH (Affected Engine) -------------------------------------------- HOLD ON/10 SEC |
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Engine Fail Fire Below V1 |
1. POWER LEVERS -------------------------FLIGHT IDLE 2. BRAKES----------------------------------AS REQUIRED 3. PARKING BRAKES -----------------------------------ON 4. PROP LEVERS -----------------------BOTH FEATHER 5. FUEL LEVERS -------------------------------BOTH OFF 6. EMERG FUEL SHUTOFF (Affected Engine) -OFF 7. FIRE DISCHARGE (Affected Engine) -------PUSH 8. BOOST PUMPS (Both Engines) ----------------OFF 9. MASTER SWITCH -----------------------------------OFF 10. EVACUATE THE AIRCRAFT -------AS REQUIRED 11. FIRE EXTINGUISHER -------------USE IF NEEDED |
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ENGINE FAIL/ FIRE/SHUTDOWN IN FLIGHT ABOVE V1 |
1. POWER AND PROP LEVERS (Live Engine) -------------------------------------- MAX POWER 2. FLAPS ------------------------------------AS REQUIRED 3. POWER LEVER (Affected Engine) ------------IDLE 4. PROP LEVER (Affected Engine) --------FEATHER 5. FUEL LEVER (Affected Engine) -----------------OFF 6. EMERG FUEL SHUTOFF (Affected Engine) -OFF 7. FIRE DISCHARGE (Affected Engine) --------------------------- PUSH, IF FIRE CONFIRMED 8. BOOST PUMP (Affected Engine) --------------OFF |
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INFLIGHT PROP REVERSAL/ FEATHER - Blades Latches NOT Fitted |
AFFECTED ENGINE ------------------------SHUTDOWN |
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GENERATOR LIGHT FAILS TO ILLUMINATE AFTER START OR SHUTDOWN |
1. EXTERNAL / BATTERY SWITCH ----------------OFF 2. SHUT DOWN ENGINE |
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SMOKE/FIRE IN COCKPIT/CABIN DURING FLIGHT/ SUSPECTED ELECTRICAL FIRE |
1. RAM AIR -------------------------------------------CLOSE 2. GENERATORS ---------------------------------------OFF 3. BUS TIE ---------------------------------------------OPEN 4. MASTER -----------------------------------------------OFF 5. BLEED AIR --------------------------------------------OFF 6. FIRE EXTINGUISHER ----------------AS REQUIRED 7. VENTILATE CABIN --------------------AS REQUIRED |
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Fuel Low Level/Transfer Warning |
The LOW FUEL LEVEL light will normally come on when 75 pounds remains in the FWD tank, or if 110 pounds remains in the AFT tank. If fuel quantity on affected tank is known to be at or above 330 pounds (during level flight conditions), fuel transfer may have failed in that tank. |
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ELEVATOR CONTROL MALFUNCTION |
If movement of the control column does not produce a corresponding change in pitch attitude, longitudinal control can be managed by using the elevator trim. Engine power should be used to assist in controlling vertical speed and airspeed. |
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AILERON TRIM TAB RUNAWAY |
1. IF NECESSARY, REDUCE SPEED TO RELIEVE CONTROL FORCES If trim tab can be operated by pressing switch: 2. AILERON TRIM SWITCH ------------------------------- PRESS IN APPROPRIATE DIRECTION When control force relieved: 3. AIL TRIM ACT CB (Main Panel) --------------------------------------------------------------------- PULL |
