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177 Cards in this Set
- Front
- Back
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Vne, 0 - 20,000'
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280 KIAS
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Vne, 20,000' - 25,000'
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245 KIAS
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Airspeed below 10,000' (FAA)
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250 KIAS
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Canopy, emergency open
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250 KIAS
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Canopy, normal open
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240 KIAS
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Turbulent air penetration, clean
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195 KIAS
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Turbulent air penetration, gear and flaps down
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120 KIAS
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Landing gear extension
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150 KIAS
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Landing gear retraction
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120 KIAS
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Maneuvering airspeed
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135 KIAS
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Flap extension
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120 KIAS
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Flap retraction
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>90 KIAS
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Vy (max rate of climb)
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100 KIAS
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Vx (max angle of climb)
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75 KIAS
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Full flap approach airspeed
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90 KIAS
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No flap approach airspeed
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95 KIAS
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G limits up to 280 KIAS
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+4.5/-1.0
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G limits up to 220 KIAS
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+4.5/-2.3
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G limits with flaps down
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+2.0/-1.0
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Max operating altitude
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25,000'
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Max altitude for airstart
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20,000'
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Min altitude for airstart
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1,500'
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Prop RPM, normal
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1800 – 2200 RPM
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Prop RPM, max
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2200 ± 25 RPM
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Overspeed governor
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2332 RPM
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Fuel topping governor
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2398 RPM
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Prop RPM, idle power on ground
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≤1800 RPM
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Torque operating range, normal
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400 – 1015 ft-lbs
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Torque, max continuous
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1015 ft-lbs
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Torque, max allowable
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1015 ft-lbs
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Torque, max torque
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1315 ft-lbs
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Torque, climb
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1015 ft-lbs (695° C)
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Torque, prop overspeed test range
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400 – 500 ft-lbs
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Torque, auto-ignition range
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300 – 180 ft-lbs
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Torque, idle operating
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150 ft-lbs
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Tachometer (N1), Introduce fuel
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12%
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Tachometer (N1), Flameout indication
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10 – 12%
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Tachometer (N1), FCU stuck at min flow (rollback)
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40 – 60%
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Tachometer (N1), Min N1 for flight (report)
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60%
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Tachometer (N1), Idle operating range
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62 – 65%
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Tachometer (N1), Max continuous
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101.5%
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Tachometer (N1), Max acceleration
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102.6%
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ITT, Normal range
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400 – 695° C
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ITT, Max at shutdown w. cond. lever
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610° C
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ITT, Max continuous
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695° C
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ITT, Max acceleration
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825° C
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ITT, Max start
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1090° C / 925° C (2 sec.)
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Oil system capacity
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4.4 Gal
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Oil tank capacity
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2.8 Gal
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Usable oil (upright)
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1.5 Gal
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Usable oil (inverted)
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1 QT
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Oil temp, min starting temp
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-40° C
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Oil temp, normal operating range
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10 – 99° C
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Oil temp, maximum
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100° C
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Oil press, idle operating range
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40 psi min
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Oil press, normal operating range, N1 > 75%
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65 – 85 psi
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Oil press, max oil pressure
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100 psi
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Oil press, max fluctuation
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±5 psi
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Fuel, total capacity
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135 Gal
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Fuel, max useable
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130 Gal
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Fuel, inboard tank qty
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40 Gal
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Fuel, outboard tank qty
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25 Gal
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Fuel, sump tank qty
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1.5 Gal
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Fuel, flow at idle
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≈125 lbs/hr
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Fuel, max imbalance (PEL req'd)
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>200 lbs split OR >100 lbs split with <200 lbs in either tank
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Elect, system rated
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28V DC
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Elect, voltage reg. maint. sys.
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27.0 – 29.5V DC
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Elect, inverter
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115V AC
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Elect, battery (lead acid)
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24V, 24-amp hour
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Elect, generator
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30V, 200 amps
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Max ramp weight
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4,425 lbs
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Max takeoff weight
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4,400 lbs
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Max landing weight
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4,400 lbs
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Max aerobatic weight
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4,300 lbs
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Max zero fuel weight
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3,650 lbs
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Fuselage type
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semi-monocoque
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Fuselage length
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28' 6"
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Fuselage height
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9' 7"
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Wing type
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full cantilever, slotted flap
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Wingspan
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33' 4"
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Aspect ratio
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6.2:1
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Dihedral angle
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7°
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Angle of incidence
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4° at root, 0.9° at tip
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Wing loading
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24.5 lbs/sq. ft
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Prop arc
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7' 6"
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Prop arc ground clearance
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11"
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aileron type
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servo trim tabs
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rudder type
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anti-servo trim tabs
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elevator type
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bobweights and downsprings
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L/Dmax
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9 units
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Rudder shakers (AOA)
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26.5 ± 1/4 units
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Stall (AOA)
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29 – 29.5 units
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Max sink rate at touchdown
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600 FPM
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Air start envelope, SL-20k
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80 – 280 KIAS
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Oxygen system capacity
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1850 psi at 70°F
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Oxygen system normal limits
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1000 – 1850 psi
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Oxygen system volume
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76 cubic feet
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Engine type
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Pratt & Whitney PT6A-25
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Engine flat-rated SHP
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550 SHP (1315 ft-lbs)
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Engine normal operation SHP
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425 SHP (1015 ft-lbs)
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Nose gear turn limits
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±30°
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Main tire pressure
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90 psi ±2
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Nose tire pressure
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70 psi ±2
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Max inverted flight time
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15 sec.
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Max zero G flight time
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Transient only
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Max vertical flight, nose up
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15 sec.
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Max vertical flight, nose down
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3 sec.
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Max knife edge, wings vertical
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3 sec.
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Max crosswind, no flap
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22 knots
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Max crosswind, full flap
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15 knots
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Min. bailout altitude, Day VMC
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1200'
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Min. bailout altitude, Night/IMC
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2000'
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Min. bailout altitude, out of control flight
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5000'
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Starter
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28V, 800 amps
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Starter time limits
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40/60, 40/60, 40/30 minutes
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Prohibited Maneuvers (6)
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1. Night formation flights (except in emergencies)
2. Inverted flight above 220 KIAS 3. Inverted stall maneuvers 4. Intentional inverted spins 5. Intentional spins with flaps and/or gear extended 6. Intentional spins with prop feathered |
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Downwind Airspeed
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100 KIAS
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VFR/Overhead Break Airspeed
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170 KIAS
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Full Flap LDG Airspeed
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85 KIAS
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No Flap LDG Airspeed
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95 KIAS
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Best Maneuvering Speed
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135 KIAS
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Recommended Bailout Airspeed
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90 – 120 KIAS
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Max range torque
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580 ft-lbs
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Max endurance torque
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420 ft-lbs
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Fuel flow, normal operation
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~335 lbs/hr
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Fuel type
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JP5
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Oil press, dynamic maneuvers
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10 psi for 5 sec.
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G limit, gear down
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+1.5/-0.0
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Weight limit, crew + luggage
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450 lbs
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Max total wind
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25 knots
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Engine stages
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3 axial, 1 centrifugal
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Engine compression ratio
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7:1
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Engine reduction ratio
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15:1
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Compressor turbine RPM
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37,000 RPM (N1)
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Power Turbine RPM
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33,000 RPM (N2)
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Blade angle, feathered
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87.5°
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Blade angle, Idle/low pitch
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17.5°
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Blade angle, beta
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-5°
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Oil type/designators
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MIL-L-23699 or Exxon 2380
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At _____ oil pressure, prop goes to FTHR
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10 psi
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temp at which oil cooler bypass valve fully closed
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71ºC
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temp at which oil cooler bypass fully open
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60ºC
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minimum wait time after refueling before taking samples
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30 minutes
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number of snap drains
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5 total; 2 per wing, 1 on sump
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primary fuel boost pump pressure
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800 psi
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time limit for unboosted fuel ops
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10 hours
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ITT, max idle
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660ºC
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Prop RPM, prop overspeed test
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1950-2150 RPM
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A/C high pressure circuit breaker
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380 psi
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A/C low pressure circuit breaker
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3 psi
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bleed air light comes on at what temperature?
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250ºF
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KIAS rotate for obstacle clearance T.O.
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70 KIAS
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KIAS rotate for minimum run T.O.
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60 KIAS
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KIAS for steady state spin
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80-100 KIAS
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basic a/c weight
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2970 lbs
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max forward crew weight
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266 lbs
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max aft crew weight
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250 lbs
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Torque, PEL max
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850 ft-lbs
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N1, starter off
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60%
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N1, norm @ 1015 ft-lbs
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89-93%
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N1, rollback indication
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40-65%
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N1, minimum EPL idle
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65%
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Gear warning system sounds: (4)
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1. gear up/flaps extended
2. gear up/both PCL and EPL < or > 75% 3. gear up/A/C on deck 4. handle/gear don't agree |
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main gear olea
|
3"
|
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nose gear olea
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3-5"
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brake lining limit
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must be >1/10th inch
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nose tire rating
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120 mph
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main tire rating
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190 mph
|
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ailerons neutral at
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2º down
|
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elevator trim tabs neutral at
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4.5º down left/4.5º up right
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flap type
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slot type
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flap extension at 100%
|
30º
|
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flap indicator driven by?
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left flap only
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GPU start required when battery is?
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<22V
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Battery must be replaced when?
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<18V
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minimum battery voltage during non-GPU start?
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10V
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generator light illuminates when?
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at 25-27.5VDC
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