MC-12W Flashcards
(98 cards)
1
Q
Maneuvering Speed (Va)
A
184
2
Q
Maneuvering Speed ER (Va)
A
182
3
Q
Max Flap Extension/Extended (Vfe) Approach
A
202
4
Q
Max Flap Extension/Extended (Vfe) Full Down
A
158
5
Q
Max Landing Gear Operating Speed (Vlo) Extension
A
184
6
Q
Max Landing Gear Operating Speed (Vlo) Extension ER
A
182
7
Q
Max Landing Gear Operating Speed (Vlo) Retraction
A
166
8
Q
Max Landing Gear Operating Speed (Vlo) Retraction ER
A
164
9
Q
Air Min Control Speed (Vmca) Flaps up
A
94
10
Q
Air Min Control Speed (Vmca) Flaps up ER
A
101
11
Q
Air Min Control Speed (Vmca) Flaps Down
A
93
12
Q
Air Min Control Speed (Vmca) Flaps Down ER
A
98
13
Q
Max Operating Speed (Vmo) To 21,000
A
263
14
Q
Max Operating Speed (Vmo) To 24,000 ER
A
245
15
Q
Max Operating Speed (Vmo) Above 21,000
A
.58M
16
Q
Max Operating Speed (Vmo) Above 24,000 ER
A
.58M
17
Q
Two engine best rate of climb (Vy)
A
140
18
Q
Two engine best rate of climb (Vy) ER
A
135
19
Q
Turbulent Air Penetration
A
170
20
Q
Max airspeed for effective windshield Anti-icing
A
226
21
Q
Min Airspeed for sustainded flight in icing
A
140
22
Q
Intentional One-Engine Inop Speed (Vsse)
A
110
23
Q
Intentional One-Engine Inop Speed (Vsse) ER
A
135
24
Q
One-Engine Inop best angle of climb (Vxse)
A
125
25
One-Engine Inop best angle of climb (Vxse) ER
135
26
One-Engine Inop best rate of climb (Vxse)
125
27
One-Engine Inop best rate of climb (Vxse) ER
135
28
Emergency Descent
184
29
Emergency Descent ER
182
30
Max Range Glide
135
31
Max Ramp Weight
15,100
32
Max Ramp Weight ER
16,600
33
Max T/O Weight
15,000
34
Max T/O Weight ER
16,500
35
Max landing weight
15,000
36
Max landing weight ER
15,675
37
Usable Fuel
3,611
38
Usabel Fuel ER
5,192
39
Planned Recovery Fuel
550
40
Minimum Fuel
400
41
Emergency Fuel
300
42
Min T/O Fuel(per side)
265
43
Max wind (any direction)
50
44
RCR12 and above wind limits
25
45
Max tailwind component
10
46
Max Cabin diff
6.6
47
CABIN DIFF HI
6.9 +-.3
48
CABIN ALTITUDE HI
12,000
49
Torque-T/O,Max Cont, Cruise, Cruise Climb, Throttle Push
100
50
Torque Transient
156 (20sec)
51
ITT Starting
1000 (5sec)
52
ITT Idle
750
53
ITT- T/O, Max cont, Cruise
820
54
ITT Cruise climb
785
55
ITT Transient
850 (20sec)
56
ITT Throttle Push
870 (5min)
57
Min N1 % Idle
62
58
N1 % -T/O,Max Cont, Cruise, Cruise Climb, Transient, Throttle Push
104
59
Min Prop RPM N2 Idle
1050
60
Prop RPM N2 - T/O, Max Cont, Cruise, Cruise Climb, Throttle Push
1700
61
Prop RPM N2 Transient
1870 (20sec)
62
Oil Press (PSI) Starting
0-200
63
Min Oil Press (PSI) Idle
60
64
Oil Press (PSI) - T/O, Max Cont, Cruise, Cruise Climb, Throttle Push
90-135
65
Oil Press (PSI) Transient
200
66
Min Oil Temp Starting
-40
67
Oil Temp Idle
-40-110
68
Oil Temp -T/O,Max Cont, Cruise, Cruise Climb, Transient, Throttle Push
0-110
69
Inadvertent torque excursions up to ________ are time limited to _____ min
102%, 7
70
Sustained prop overspeeds faster than _____ RPM indicate failure of the primary governor.
1700
71
Flight may be continued at propeller overspeeds up to ______ RPM, provided torque is limitied to _____.
1768, 96%
72
Sustained propeller overspeeds faster than _____ RPM indicate failure of both primary governor and the secondary governor and such overspeed are not approved.
1768
73
Inadvertent propeller excurions up to _____ RPM are time limited to _____ min.
1735, 7
74
Oil pressures under ____ psi are undesirable.
90
75
Under emergency conditions, to complete a flight, a lower oil pressure limit of _____ psi is permissible at a reduced power level not to exceed _____% torque.
62
76
Oil pressures below _____ psi are unsage and require that either the engine be shut down or a landing be made at the nearest suitable airport, using the minimum power required to sustain flight.
60
77
Fluctuations of ____psi are acceptable.
+/- 10
78
Starter is limited to ____sec ON, ___ min OFF, ____ON, ___ min OFF, _____sec ON, then ____ min OFF.
30 sec, 5min, 30 sec, 5 min, 30 sec, 30 min.
79
Load Factor (G's) Flaps up
-1.24 to 3.1
80
Load Factor (G's) Flaps up ER
-1.21 to 3.01
81
Load Factor (G's) Flaps Down
0 to 2.0
82
Min Battery for start
23 volts
83
Min Battery to use ext power
20 volts
84
Ext. Power Cart
28-28.4 volts
85
Cart - Sustained/Momentary
300/1000 Amps
86
Landing gear cycles limited to ___ every ____ min. for ____ cycles followed by a ____ min. cool down.
1, 5min, 6, 15min
87
Rudder boost must be ___________ for _________.
Operational, all flights
88
Auto feather must be operable for ________, and must be armed during ________, _______, ________, and _________.
all flights, TO, Climb, Approach, Landing
89
Engine Anti-ice must be ON for operation in ambient temperatures of _____ C or below when flight free of ________ ________ cannot be assured.
+5, visible moisture
90
Engine Anti-ice must be off for takeoff operations when ambient temps exceed________ C.
+10
91
The order in which the fuel tanks must be filled is ________, _________, then __________.
main, Aux, extended range
92
Sustainde flight in icing conditions with flaps extended is prohibited except for_______ and ________.
Approach and landing.
93
Engine Fire on Ground
1. Condition Lever -- Cutoff
2. Firewall Valve -- Close
3. Starter -- Starter Only
4. Extinguisher (if fire warning persists) -- Actuate
94
Emergency Engine Shutdown on Ground
1. Condition Levers -- Cutoff
2. Props -- Feather
3. Firewall Valves --Close
4. Master Switch -- OFF
5. Batt Bus -- Emer OFF
6. ESIS -- OFF
95
Takeoff Abort
1. Power -- Ground Fine
| 2. Brakes -- As Required
96
Engine Failure Takeoff Continued
1. Vr -- Rotate
2. Power -- Max Allowable
3. Gear -- UP
4. Airspeed -- V2 To Accel height (400' AGL min)
5. Prop(Inop engine) -- Verify Feathered
97
Engine Fire / Failure in Flight
1. Condition Lever -- Cutoff
2. Prop -- Feather
3. Firewall valve -- Close
4. Extinguisher (if fire warning persists) -- Actuate
98
Enviromental Smoke / Fumes
1. Oxygen Mask -- Don
2. Mask selector switch -- EMER
3. Mic -- OXY
