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80 Cards in this Set

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