Flash Cards
1
Q
Min crew
A
One pilot
2
Q
Passenger seating limitations
A
Part 91 says 15
3
Q
Flight load factor limit with flaps up
A
3.1 positive and 1.24 negative
4
Q
Flight load limit with flaps down
A
2 positive and 0 negative
5
Q
Altitude limitation using aviation gasoline with standby fuel pumps operative
A
35k ft
6
Q
Altitude limitation using aviation gasoline with either standby fuel pump inoperative
A
Flight prohibited
7
Q
Altitude limitation using aviation gasoline without cross feed capability
A
20k ft
8
Q
Max operating altitude normal operation
A
35k ft
9
Q
Maximum operating altitude if yaw damper system is inoperative
A
5k ft
10
Q
Maximum allowable takeoff weight
A
15k lbs or as limited by takeoff climb requirements or tire speed or takeoff field length
11
Q
Maximum landing weight
A
15k lbs or as limited by max landing weight to achieve climb requirements or max landing distance with flaps down
12
Q
Max ramp weight
A
15100 lbs
13
Q
Max zero fuel weight
A
12500 lbs
14
Q
Max weight in baggage compartment
A
550 lbs
15
Q
One engine inoperative best angle of climb Vxse
A
125 kias
16
Q
One engine inoperative best rate of climb Vyse
A
125 Kias
17
Q
One engine inoperative enroute climb Emergency air speed
A
125 kias
18
Q
Air minimum control speed Vmca with flaps up
A
94 kias
19
Q
Air minimum control speed Vmca with flaps approach
A
93 kias
20
Q
Emergency descent speed
A
184 kias
21
Q
Maximum range glide speed
A
135 kias
22
Q
Max demonstrated crosswind
A
20 kias
23
Q
Max demonstrated wind components for coupled approaches with a cross wind
A
32 kias
24
Q
Max demonstrated wind components for coupled approaches with a tailwind
A
14 kias
25
Maneuvering speed Va
184 kias
26
Max flap extended speed Vfe approach
202 kias
27
Max flap extended speed Vfe full down
158 kias
28
Max landing gear operating speed Vlo extension
184 kias
29
Max landing gear operating speed Vlo retraction
166 kias
30
Max landing gear extended speed Vle
184 kias
31
Max operating speed Vmo in knots and Mach number
263 kias and .58 Mach
32
Aircraft height
14 ft 4 in
33
Aircraft length
46 ft 8 in
34
Aircraft wingspan
57 ft 11 in
35
Aft facing seats
Seat back of each occupied aft facing seat must be in upright position with headrest fully extended for takeoff and landing
36
The pilot and Co pilot air data computers must be what for takeoff
Operative
37
The multi function display must be what prior to engine start
Operational
38
The pilot PFD and MFD and Co pilots PFD must be installed and operational in what mode for takeoff
Normal
39
AHRS 1 and 2 must be what for takeoff
Operative
40
Operating in the composite mode is limited to what and what conditions
Training and display failure
41
Auto pilot coupled intercept angle for back course
70 degrees
42
Autopilot max coupled intercept angle for NAV/LOC
Less than 90 degrees
43
During what type of operations a pilot must be seated at the controls with seat belt and shoulder harness fastened
Autopilot
44
When must an autopilot preflight check be conducted
Must be conducted and found satisfactory prior to each flight on which auto pilot is to be used
45
Min autopilot engage height after takeoff
400 ft
46
Min autopilot use height during cruise
1000 ft
47
Min autopilot use height during approach
79 ft AGL
48
Min autopilot use
| Height during steep approach
160 ft AGL
49
When must the auto pilot and yaw damper not be used
During takeoff and landing
50
Operation of the auto pilot with a what is prohibited
Pitch trim malfunction
51
When Should you not manually override the autopilot
During normal flight
52
Below X volts, battery must be recharged or replaced with battery indicating at least 20 volts before connecting external power
20
53
External power amps limit momentary
1000 amps
54
External power amps limit continuous
300 amps
55
External power volt range
28 to 28.4
56
Generator load limit in flight up to 34k ft
100%
57
Generator load limit in flight above 34k ft
95%
58
Generator load limit on the ground with N1 from 62 to 70%
75%
59
Generator load limit on the ground with N1 from 70 to 100%
100%
60
Min battery volts for battery start
23 VDC
61
Starter limits
30 seconds on and 5 min off
30 seconds on and 5 min off
30 seconds on and 30 min off
62
Do not put any fuel in the blank tanks unless the blank tanks are full
Don’t put fuel in the aux tanks unless the mains are full
63
For fuel system don’t takeoff if fuel quantity gauges indicate blank arc or less than blank lbs in each wing system
Yellow arc or less than 265 lbs in each wing
64
Fuel cross feed is permitted only when blank
One engine is inoperative
65
Max fuel imbalance
300 lbs
66
Total useable fuel
3611 lbs
67
Each main fuel tank quantity useable
1273 lbs
68
Each aux fuel tank quantity useable
533 lbs
69
Operation of either engine with its corresponding fuel pressure annunciator (L FUEL PRESS LO or R FUEL PRESS LO) illuminated is limited to blank hours before overhaul or replacement of engine driven fuel pump (windmill time doesn’t count)
10 hours
70
Engine anti ice shall be on in ambient temperatures of blank or below when flight free of visible moisture can’t be assured
5 degrees Celsius
71
The left and right engine anti ice shall be off for takeoff operations in ambient temperatures above blank
10 degrees Celsius
72
Min ambient temperature for operation of de icing boots
-40 degrees Celsius
73
Min airspeed for sustained icing flight
140 kias (no flaps except takeoff and landing)
74
Prop de ice ammeter normal operating range
26 to 32 amps
75
Brake de ice temp operation limit
Not above 15 degrees Celsius
76
Landing gear cycle limits
1 cycle every five minutes for 6 cycles followed by 15 min cool down
77
Cabin differential pressure gauge green arc
0 to 6.6 psi
78
Cabin differential pressure gauge red arc
6.6 psi to end of scale
79
The CABIN ALTITUDE light illuminates when
Cabin altitude is above 10k ft
80
CABIN ALTITUDE HI lights illuminates when
Cabin altitude above 12000 ft
81
Above what altitude do oxygen masks automatically deploy
12500 ft
82
Pressure where CABIN DIFF HI light illuminates
6.9 PSID
83
Outside air temperature limit up to 25k ft PA
ISA plus 37 degrees Celsius
84
Outside air temperature limit above 25k ft PA
ISA plus 31 degrees Celsius
85
Engine model number and type
PT6A-60A, turbo prop
86
Propeller type
```
Constant speed
Full feathering
Reversing
Counter weighted
Hydraulically actuated
```
87
When must Auto feather be armed
Takeoff and climb and approach and landing
88
Engine torque for takeoff
100% (102% for 7 minutes)
89
Engine torque max continuous
100% (102% for 7 minutes)
90
Engine torque transient
156% (limited to 20 seconds)
91
Engine torque below 1000 RPM N2
62%
92
Engine max ITT during start
1000 degrees Celsius for 5 seconds
93
Engine max ITT at idle
820 degrees Celsius
94
Engine max ITT max continuous
820 degrees Celsius
95
Engine max ITT max cruise
820 degrees Celsius
96
Engine max ITT cruise climb
785 degrees Celsius
97
Engine max ITT max reverse
760 degrees Celsius
98
Engine max ITT transient
850 degrees Celsius for 20 seconds
99
Engine gas generator (%N1) at idle
62% min
100
Engine gas generator (%N1) at takeoff
104%
101
Engine gas generator (%N1) max continuous
104%
102
Engine gas generator (%N1) cruise climb
104%
103
Engine gas generator (%N1) max cruise
104%
104
Engine gas generator (%N1) transient
104%
105
Engine prop RPM (N2) at idle
1050 min
106
Engine prop RPM (N2) at takeoff
1700 (up to 1735 for 7 minutes)
107
Engine prop RPM (N2) max continuous
1700 (up to 1735 for 7 minutes)
108
Engine prop RPM (N2) at cruise climb
1700 (up to 1735 for 7 minutes)
109
Engine prop RPM (N2) at max cruise
1700 (up to 1735 for 7 minutes)
110
Engine prop RPM (N2) at max reverse
1650
111
Engine prop RPM (N2) transient
1870 for 20 seconds
112
Engine oil pressure starting
0 to 200 psi
113
Engine oil pressure at idle
60 psi min
114
Engine oil pressure at takeoff
90 to 135 psi
115
Engine oil pressure at max continuous
90 to 135 psi
116
Engine oil pressure at cruise climb
90 to 135 psi
117
Engine oil pressure at max cruise
90 to 135 psi
118
Engine oil pressure at max reverse
90 to 135 psi
119
Engine oil pressure transient
200 psi
120
Engine oil temperature starting
-40 degrees Celsius minimum
121
Engine oil temperature idle
-40 to 110 degrees Celsius
122
Engine oil temperature takeoff
0 to 110 degrees Celsius
123
Engine oil temperature max continuous
0 to 110 degrees Celsius
124
Engine oil temperature cruise climb
0 to 110 degrees Celsius
125
Engine oil temperature max cruise
0 to 110 degrees Celsius
126
Engine oil temperature max reverse
0 to 99 degrees Celsius
127
Engine oil temperature transient
0 to 110 degrees Celsius
128
Engine oil temperature min for fuel heat at takeoff
55 degrees Celsius (recommended)
129
Range of primary Governor
1450 to 1700 RPM
130
Over speed Governor governs to x RPM
1768 RPM
131
Why should power lever not be lifted in flight
Leads to nose down pitch and descent rate that could lead to aircraft damage or injury to personnel
132
When must the rudder boost be operational
All phases of flight
133
Max wind any direction
50 kts
