5 & 9's Flashcards
1
Q
Airspeed - Minimum for Reverse
A
40 KIAS
2
Q
Airspeed - Vmca Flaps Approach
A
98 KIAS
3
Q
Airspeed - Vmca Flaps Up
A
101 KIAS
4
Q
Airspeed - Vsse Intentional One Engine INOP
A
135 KIAS
5
Q
Airspeed - Vyse
A
135 KIAS
6
Q
Airspeed - Vx
A
135 KIAS
7
Q
Airspeed - Maximum Glide Range
A
135 KIAS
8
Q
Airspeed - Vy
A
135 KIAS
9
Q
Airspeed - Minimum Icing below 15,000 lbs
A
140 KIAS
10
Q
Airspeed - Minimum Icing 15,000-16,500 lbs
A
150 KIAS
11
Q
Airspeed - Vfe Full Down
A
158 KIAS
12
Q
Airspeed - Vlo Retraction
A
164 KIAS
13
Q
Airspeed - Vb Turbulence Penetration
A
170 KIAS
14
Q
Airspeed - Va Flaps Up
A
182 KIAS
15
Q
Airspeed - Vlo Extension
A
182 KIAS
16
Q
Airspeed - Vfe Approach
A
202 KIAS
17
Q
Airspeed - Maximum for Effective Windshield De-Icing
A
226 KIAS
18
Q
Airspeed - Vmo Below 24,000 ft
A
245 KIAS
19
Q
Airspeed - Mmo Above 24,000 ft
A
.58 Mach
20
Q
Torque - Applicable within Range (1,000 - 1,700 RPM)
A
0-100%
21
Q
Torque - Max TQ (Props below 1,000 RPM)
A
62%
22
Q
Torque - Max TQ (Props above 1,700 RPM)
A
96%
23
Q
Torque - Inadvertent Excursions (_ minutes)
A
102%; 7 minutes
24
Q
Torque - Transient (__ seconds)
A
156%; 20 seconds
25
Turbine Tach (N1 Speed) - Minimum Low Idle
62%
26
Turbine Tach (N1 Speed) - Normal Operating Range
62-104%
27
Turbine Tach (N1 Speed) - Max
104%
28
ITT - Max Low Idle
750
29
ITT - Max Reverse
760
30
ITT - Recommended Cruise Climb
785
31
ITT - Max Cruise/Takeoff/Continuous
820
32
ITT - Transient (__ seconds)
850; 20 seconds
33
ITT - Max Starting (_ seconds)
1,000; 5 seconds
34
Oil Temp - Minimum Starting
-40C
35
Oil Temp - Normal Operating Range/Max Reverse
0C-99C
36
Oil Temp - Max Low Idle
-40C-110C
37
Oil Temp - Takeoff/Max Continuous/Cruise Climb
0C-110C
38
Oil Temp - Max Transient (__ minutes)
99C-110C; 10 minutes
39
Oil Temp - Recommended for Fuel Heater Ops at T/O
55C
40
Oil Pressure - Minimum Low Idle
60 psi
41
Oil Pressure - Caution Range (TQ limited __%)
60-90 psi; 62%
42
Oil Pressure - Normal Operating Range
90-135 psi
43
Oil Pressure - Max Starting
200 psi
44
Props (N2 RPM) - Minimum Idle Speed
1,050 RPM
45
Props (N2 RPM) - Normal Operating Range
1,450-1,700 RPM
46
Props (N2 RPM) - Max Reverse
1,650 RPM
47
Props (N2 RPM) - Max
1,700 RPM
48
Props (N2 RPM) - Inadvertent Excursions (_ minutes)
1735 RPM; 7 minutes
49
Props (N2 RPM) - Transient (__ seconds)
1,870 RPM; 20 seconds
50
Autofeather
Must be operable for all flights and must be armed for takeoff, climb, approach, and landing.
51
External Power - Volts
28.0-28.4 volts
52
External Power - Minimum Momentary
1,000 amps
53
External Power - Continuous
300 amps
54
Generator Load - Ground Operations Max (62%-70% N1)
75%
55
Generator Load - Ground Operations Max (70%-100%N1)
100%
56
Generator Load - In-Flight Operations Max (SL-FL___)
100%; SL-FL210
57
Generator Load - In-Flight Operations Max (FL210-FL___)
90%; FL210-FL260
58
Generator Load - In-Flight Operations Max (FL260-FL___)
80%; FL260-FL300
59
Generator Load - In-Flight Operations Max (FL300-FL___)
75%; FL300-FL320
60
Generator Load - In-Flight Operations Max (FL320-FL___)
70%; FL320-FL350
61
Generator Load - In-Flight Operations Single Engine Operations
90%
62
Generator Load - In-Flight Operations VDC Normal
27.5-29.0
63
Starter Limits
30 sec ON; 5 min OFF
30 sec ON; 5 min OFF
30 sec ON; 30 min OFF
64
Weight Limits - Max Ramp
16,600 lbs
65
Weight Limits - Max Takeoff
16,500 lbs
66
Weight Limits - Max Landing
15,675 lbs
67
Weight Limits - Max Zero Fuel
13,000 lbs
68
Weight Limits - Max Baggage Compartment
550 lbs
69
Weight Limits - Air Stair Door
One Person
70
Fuel System - Max Imbalance
300 lbs
71
Fuel System - Min in each main for T/O (yellow arc)
265 lbs
72
Fuel System - Max Usable QTY (___ gal)
5192 lbs; 775 gal
73
Fuel System - Max with FUEL PRES LO Light
10 Hours
74
Fuel System - Tank Fueling Order
Mains full before Aux full before ER
75
Fuel System - Range w/ ER
approx. 2,300 NM/8 hours
76
Fuel System - ER Tanks
236 gal total; 118 gal per side
77
Fuel System - Fuel Crossfeed
Permitted only when one engine is inoperative
78
Gear Cycle Limits
6 cycles (1 up - 1 down) at one every 5 minutes followed by a 15 minute cool-down period
79
G-Load - Flaps UP
3.0- -1.21
80
G-Load Flaps Down
2.0-0
81
Vacuum Gage - SL to 15,000 ft
4.3-5.9 inHg
82
Vacuum Gage - 15,000 to 35,000 ft
2.8 to 4.3 inHg
83
Prop De-Ice - Normal Operating Range
26-32 Amps
84
Rudder Boost
Must be operation for ALL flights
85
Yaw Damp System - Max Altitude INOP
19,000 ft
86
Yaw Damp System - Must be ON above; OFF for __________ & __________
Above 19,000 ft; takeoff & landing
87
Temperature Limits
ISA+37 - SL to 25,000 ft
| ISA+31 - Above 25,000 ft
88
Surface De-Ice
No operations below -40C
| Activate when Ice accumulates a minimum of 1/2 inch
89
Engine Anti-Ice
ON when ambient temperatures are +5C and below in visible moisture
OFF for takeoff in ambient temperatures above +10C
90
Pneumatic Pressure Gage
12-20 psi - Normal Operating Range
| 20 psi - Max
91
Cabin Altimeter/Differential Limits
6.6 Max
92
Max Altitude
35,000 ft
93
Brake De-Ice (if installed)
Don't use above 15C or more than 10 minutes with wheels retracted
94
Autopilot Limits
1. During autopilot operations, a pilot must be seated at the controls with the seat belt and shoulder harness fastened
2. An autopilot preflight check must be completed and found satisfactory prior to each flight on which the autopilot is to be used
3. The autopilot minimum engage height after takeoff is 400 ft AGL
4. The autopilot minimum use height during cruise is 1,000 ft AGL
5. The autopilot minimum use height during approach is 79 ft AGL
6. The autopilot minimum use height during steep approach is 160 ft AGL
7. Maximum airspeed for autopilot operation is unchanged from the airplane maximum speed (Vmo/Mmo)
8. The autopilot and yaw damper must not be used for takeoff and landing
9. Operation of the autopilot system with a pitch trim malfunction is prohibited
10. Do not manually override the autopilot during normal flight
11. The maximum coupled intercept angles are:
NAV/LOC - 90 degrees
Back course - 70 degrees
95
ENGINE FAILURE BEFORE V1 (ABORT)
1) POWER levers - GROUND FINE
| 2) Braking - As required
96
ENGINE FAILURE AFTER V1
1) POWER - Max allowable
2) LANDING GEAR CONTROL handle - UP (positive rate of climb confirmed)
3) Airspeed - Maintain V2 until 400 ft AGL and clear of obstacles
4) Propeller - Verify feathered
5) FLAPS (after Vyse) - UP
97
ENGINE FAILURE DURING FLIGHT BELOW Vmca
1) POWER - Reduce as required to maintain control
| 2) Pitch Attitude - Lower to accelerate above Vmca
98
ENGINE FAILURE DURING FLIGHT
1) AP/YD - Disengage
2) POWER - As required
3) Failed Engine - Identify
4) Propeller - Verify feathered
99
ENGINE FAILURE DURING FINAL APPROACH
1) POWER - As required
| 2) Landing gear - confirm down
100
ENGINE FAILURE (SECOND ENGINE)
1) Airspeed - As required
2) POWER lever - IDLE
3) PROP lever - As required
101
MAXIMUM GLIDE
1) LANDING GEAR CONTROL handle - UP
2) FLAPS - UP
3) PROP levers - FEATHER
4) Airspeed - 135 KIAS
102
SINGLE-ENGINE GO AROUND
1) POWER - Maximum allowable
2) LANDING GEAR CONTROL handle - UP
3) FLAPS - UP
4) Airspeed - Vyse
103
L OR R BLEED AIR FAIL ANNUNCIATOR ILLUMINATED
1) BLEED AIR VALVES switch (affected engine) - PNEU & ENVIR OFF
104
EXCESSIVE DIFFERENTIAL PRESSURE (CABIN DIFF HI ANNUNCIATOR ILLUMINATED)
1) BLEED AIR VALVES switches - ENVIR OFF
2) Crew oxygen masks - EMER and don
3) MIC swtich - OXY
4) PASSENGER MANUAL DROP OUT handle - Pull on
5) Descend - As required
105
LOSS OF PRESSURIZATION (CABIN ALTITUDE AND/OR CABIN ALT HI ANNUCIATOR ILLUMINATED)
1) Crew oxygen masks - EMER and don
2) MIC switches - OXY
3) PASSENGER MANUAL DROP OUT handle - Pull on
4) Descend- As required
106
DOOR UNLOCK WARNING ANNUNCIATOR ILLUMINATED
1) All occupants - Seated with seatbelts securely fastened
107
CRACKED CABIN WINDOW
1) Crew oxygen masks - ON
| 2) MIC switches - OXY
108
BOTH DC GEN LIGHTS ILLUMINATED
1) Mission power - Off
2) INSTRUMENT EMERGENCY LIGHTS - ON (if required)
3) Generators - GEN RESETS, then ON
4) Operating generator load meter - Monitor (100% maximum)
5) ECS MODE - OFF
6) COCKPIT/CABIN BLOWER - AUTO
7) Non-essential equipment - Off
109
PRIMARY AND OVERSPEED GOVERNERS FAILED (ABOVE 1768)
1) POWER lever (affected engine) - IDLE
| 2) PROP lever (affected engine) - FEATHER
110
PRIMARY AND OVERSPEED GOVERNERS FAILED (ABOVE 1768 RPM)
1) POWER lever (affected engine) - IDLE
| 2) PROP lever (affected engine) - FEATHER
111
ENGINE/NACELLE FIRE DURING START OR GROUND OPERATIONS
1) PROP levers - FEATHER
2) CONDITION levers - FUEL CUTOFF
3) F/W VALVE PUSH switch - Push to close (CLOSED annunciator illuminated)
4) EXTINGUISHER PUSH switch - PUSH
5) MASTER SWITCH - OFF
6) BATT BUS - EMER OFF
112
ENGINE FIRE IN FLIGHT (IDENTIFIED)
1) POWER lever (affected engine) - IDLE
2) PROP lever (affected engine) - FEATHER
3) CONDITION lever (affected engine) - FUEL CUTOFF
4) F/W VALVE PUSH switch - Push to close (CLOSED annunciator illuminated)
5) EXTINGUISHER PUSH switch - PUSH
113
FUSALAGE FIRE
1) Fight the fire
| 2) Land as soon as possible
114
WING FIRE
1) Perform engine shutdown on affected side
| 2) Land as soon as possible
115
ELECTRICAL SMOKE OR FIRE
1) Crew oxygen masks - EMER and don
| 2) MIC switches - OXY
116
ENVIRONMENTAL SYSTEM SMOKE OR FUMES
1) Crew oxygen masks - EMER and don
| 2) MIC switches - OXY
117
EMERGENCY DESCENT
1) POWER levers - IDLE
2) PROP levers - High
3) Flaps (202 KIAS max) - APPROACH
4) LDG GEAR CONTROL handle (182 KIAS max) - DN
5) Airspeed - 182 KIAS maximum
118
UNSCHEDULED RUDDER BOOST ACTIVIATION
1) AP/TRIM MASTER switch - Press to first detent and hold
2) RUDDER BOOST switch - OFF
3) AP/TRIM MASTER switch - Release
If condition persists
4) YD/AP DISC switch (on flight guidance panel) - Pull down
119
UNSCHEDULED ELECTRIC ELEVATOR TRIM
1) Airplane attitude - Maintain using elevator control
| 2) AP/TRIM MASTER switch - Depress fully and hold
120
AUTOPILOT MISTRIM [E] OR [A]
1) Flight controls - Hold firmly
| 2) Autopilot - Disengage
121
AUTOPILOT MISTRIM [TRIM]
1) Flight controls - Hold firmly
| 2) Autopilot - Disengage
122
UNEXPECTED AUTOPILOT DISENGAGEMENT
1) Aircraft control - Maintain
| 2) Autopilot/trim disconnect switch - Press to first level to cancel horn
123
STALLS (DEPARTURE FROM CONTROLLED FLIGHT)
1) Autopilot and yaw damper - Disengage
2) Aircraft pitch - Apply control to reduce angle of attack
3) Aircraft bank - Wings level
4) POWER - As required
5) Execute a smooth recovery
124
SPINS
1) Autopilot and yaw damper - Disengage
2) Control wheel - Full forward, ailerons neutral
3) Full rudder - Opposite the direction of spin
4) POWER levers - IDLE
5) RUDDER - Neutralize when rotation stops
6) Execute a smooth recovery
125
Throttle Push
Single use emergency power available for single engine operations in high density altitude conditions. 100% TQ with max of 870C ITT at 1,700 RPM for 5 minutes.
