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80 Cards in this Set
- Front
- Back
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Max Engine SHP
Takeoff EMER and Max Continuous |
850 (takeoff, emer, max cont)
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Torque Limits
Takeoff, EMER, Continuous Transient When Prop below 1600 |
100% (Takeoff, EMER, MAX CONT)
123% (5 seconds) 49% (below 1600 Prop RPM) |
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Torque limit applies to ____ to _____ propeller RPM (N2). Below _____ RPM, torque is limited to ______.
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1600-2000;
1600; 49% |
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Maximum Observed TGT
(Takeoff; Emer Condition; Max Reverse) |
750
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Max Continuous TGT
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725
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Max TGT at LOW IDLE
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660
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Max TGT at START
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1000 (5 seconds)
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Max Transient TGT
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850
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Max Gas Generator RPM (N1)
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101.5% (Takeoff,Emer,Cont)
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Min N1 at LOW IDLE
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52%
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Max Transient N1
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102.6% (10 seconds)
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Max N1 in MAX REVERSE
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88%
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Max Prop RPM (N2)
Takeoff, EMER, CONT |
2000
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Max Transient Prop RPM (N2)
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2200 (5 seconds)
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Max Prop RPM (N2) in MAX REVERSE
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1900
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Oil Press/Temp Limits for Takeoff, EMER and Continuous
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105-135 (press); 10-99 (temp)
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Oil Press/Temp limits Continuous Operations
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105-135 (P); 10-99 (T)
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Oil Press/Temp limits in High Idle
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85-135 (P); -40-99 (T)
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Oil Press/Temp limits in LOW IDLE
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60 (MIN P); -40-99 (T)
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Oil Temp Min on START
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-40
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TRANSIENT Oil Temp range
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100-104 (5 minutes)
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Oil Press/Temp Limits in REVERSE
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105-135 (P); 0-99 (T)
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Oil Press Limit during extremely cold starts
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200 P
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Above 72% N1 Normal Takeoff and Continuous Press/Temp up to 21,000 ft
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105-135 (P); 60-71 (T)
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Acceptable oil fluctuations above 21,000ft
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10 PSIG
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Do not exceed ____ Torque when oil pressure is below ___.
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49%; 85 PSI
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Takeoff limits are limited to ____ minutes
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5 minutes
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Approximate N1 at HIGH IDLE
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70%
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High TGT at Ground IDLE may be corrected by ________ and/or ________.
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reducing accessory load; increasing N1 RPM
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MAX REVERSE time limit
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1 minute
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For every ____deg C below _____deg C ambient temp, reduce max allowable N1 by ____.
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5.6; -48; 1.6
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Max generator load during ground ops
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85%
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With generator load at 70% OR LESS, what is the min N1 RPM for ground ops?
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52% (w/o AC)
61% (w/AC) |
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Engine ice vanes shall be retracted above what temp?
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15 deg C
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Total usable fuel
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544 gallons
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Starter limits
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40 sec on; 60 seconds off
40 sec on; 60 seconds off 40 sec on; 30 minutes off |
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Blade angles are measured at the _____ in station: Feathered = _____ degrees
Reverse = _____degrees |
measured at 30 in station
90 deg (feathered) -9 (reverse) |
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Prop speeds above ______
indicate failure of _____ |
2000; primary governor
2080; both prim. and overspeed gov |
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Torque is limited to _____ for sustained ops above 2000 RPM. Sustained prop RPM above ______is prohibited.
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81%; 2080
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Normal TGT
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400-750
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Normal Torque
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20-100
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Normal Prop
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1600-2000
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Normal Oil Pressure
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85-135 (85-105 is yellow for operations below 21000ft)
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Normal Oil Temp
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10-99 deg C
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Normal Prop De-ice ammeter
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14-18
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Normal Pneumatic Pressure
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12-20 PSI
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Normal Cabin Pressure Differential
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0-6.1 PSI
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Vmca
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86 (minimum SE control speed)
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Full Flap operating range
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75-146 (157 D model)
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One engine inop best rate of climb (Vyse)
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121
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Max a/s with flaps at 40%
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200
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Max gear extended speed
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181
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Max speed to retract gear
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163
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Max design maneuvering speed
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181
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Vne (max operating speed)
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259
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Prop prohibited range during ILS
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1750-1850 RPM
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When operating above _______ a _____ min supply of oxygen is required for each person. Above 25,000....
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13,000ft; 10
masks for each person must be coupled to the outlet and immediately available |
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Vsse
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Safe SE inoperative speed
104 KIAS |
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Do not use controls abruptly above
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181 KIAS
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Turbulent air penetration speed
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170 KIAS
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Max T/O and land wgt
Max ramp weight Max Zero fuel weight |
12500
12590 10400 |
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Max tire speed
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136 knots
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Max seat weight
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250 fwd, 170 back facing
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Max cabin baggage area weight (C)
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150
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Aft cabin baggage area max weight
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350
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Airstair door weight
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300
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Max sink rate at touchdown
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600 FPM (12,500lbs)
500 FPM (above 12,500) |
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Do not _____ above ____ degrees C.
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brake deice; 15
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Time limit on brake deice
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10 MIN
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Min N1 for simultaneous brake deice and surface deice systems
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85
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Minimum ambient temp for surface deice system
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-40 C
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landing gear cyclying limits
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no more than 5 in 20 minutes
10-15 minutes between 20 minute groupings no more than 10 cycles within 1 hour |
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Altitude and cabin pressure differential limit with cracked windshield
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25,000ft and between 2.0 to 4.6 PSI
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Usable fuel limit
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544 gallons
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Maximum fuel imbalance
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1000 lbs
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If above 12.5k lbs limits
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- paved runways
- at/above 18k ft - cabin press rate of descent <1500 fpm - log time and altitude in 781 - Takeoff <14k lbs - Vne 216 - NO AUTOPILOT - total ferry tank fuel not >240 gal |
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Max flap extension speed
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200 kts
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Max speed for flaps full
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146 (C) 157 (D)
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Max speed to extend gear
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163
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Min speed for practice engine out
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104
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