Brainscape's Knowledge GenomeTM

Browse over 1 million classes created by top students, professors, publishers, and experts.


See full index

MC-12 Study Guide > 5 & 9 > Flashcards

5 & 9 Flashcards

1
Q

Environmental System Smoke or Fumes

A
  1. Crew oxygen masks — EMERG and on.

2. MIC switches — OXY.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q

Vy

A

135 KIAS

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
3
Q

Gear cycle limits

A
  1. 6 cycles at one cycle every 5 min.

2. 15 minutes rest after 6 cycles

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

L or R BLEED AIR FAIL annunciator illuminated

A
  1. BLEED AIR VALVES switch (affected

engine) — PNEU and ENVIR OFF.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
5
Q

Min Sustained Icing ≤ 15,000lbs (AWR)

A

140 KIAS

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q

Climb Speeds

A

135 KIAS SL to 35,000 ft

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
7
Q

ITT Limits (-60 Engines)

A 
750C	Max. low idle 
760C	Max. reverse 
785C	Cruise climb 
820C	Max cruise 
820C	Takeoff / max. continuous 
850C	Transient (20 sec)
870C       Throttle Push (5 Min, TQ 100% MAX during engine failure)
1000C 	Max. transient starting (5 sec)
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
8
Q

Door Unlock Warning Annunciator Illuminated

A
  1. All occupants — Seated with seatbelts

securely fastened.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
9
Q

Pneumatic Boot limit

A

No operations below –40c

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q

Engine Malfunction During Final Approach

A
  1. POWER — As required.

2. LANDING GEAR CONTROL — Recheck DOWN

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
11
Q

Propeller de-ice ammeter limits

A

26-32 amps Normal Range

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
12
Q

MC-12V VMO MX-15 extended (and >1,500 AGL)

A

180

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
13
Q

Max. Windshield de-icing

A

226 KIAS

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
14
Q

LIMITATIONS ON THE USE OF AV GAS (CONT.)

  1. Maximum altitudes when using AVGAS:
    a. Both Standby Fuel Pumps Operative - _______ feet
    b. Either Standby Fuel Pump ________ - Flight Prohibited
    c. Climbs without Crossfeed Capability - ________ feet
A

LIMITATIONS ON THE USE OF AVIATION GASOLINE CONT’D

  1. Maximum altitudes when using AVGAS:
    a. Both Standby Fuel Pumps Operative - 35,000 feet
    b. Either Standby Fuel Pump Inoperative - Flight Prohibited
    c. Climbs without Crossfeed Capability - 20,000 feet
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
15
Q

Engine Fire In Flight (Identified)

A
  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.
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
16
Q

The propeller autofeather system must be ________ for all flights and must be armed for ______, ______, ______, and ________.

A

The propeller autofeather system must be operable for all flights and must be armed for takeoff, climb, approach and landing.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
17
Q

Autopilot Limitations

A
  1. During AP ops, pilot must be seated at the controls w/ seatbelt/shoulder harness fastened
  2. Satisfactory preflight check conducted prior to each flight autopilot is to be used
  3. Min engagement after takeoff 400’ AGL
  4. Min use during cruise 1,000 AGL
  5. Min height during approach, 79’ AGL
  6. Min height during steep approach, 160’ AGL
  7. Max airspeed, Vmo
  8. AP/YD must not be used for takeoff/landing
  9. Operation w/ pitch trim malfunction is prohibited.
  10. Do not manually override during flight
  11. Max coupled intercept angle, NAV/LOC <90 degrees, Back course 70 degrees
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
18
Q

Oil Temperature Limits (-60 Engines)

A

-40 to 110 C Starting, Low idle
0 to 99 C Normal
99 to 110 C Max transient (10 Min.)
110 C Max
55 C Rec. for fuel heater ops at T/O

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
19
Q

VLO (Retraction)

A

164 KIAS

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
20
Q

Propeller limitations - N2 rpm (-60 Engines)

A 
400-1050	Avoid during ground operations
1050 	        Minimum Idle 
1450-1700 	Normal operating range 
1650         	Max. Reverse 
1700	        Max. 
1735	                (7 minutes)
1870 	        Transient (20 sec)
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
21
Q

Turbine Tachometer (N1 speed) limits

A

62% Min. Low Idle
104% Max.
104% Max. Transient

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
22
Q

VFE

A

158 KIAS

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
23
Q

Unscheduled Electric Elevator Trim

A
  1. Airplane attitude — Maintain using
    elevator control.
  2. AP/TRIM MASTER switch — Depress
    fully and hold.
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
24
Q

VB (Turbulence Penetration)

A

170 KIAS

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
25
Q

Fuselage Fire

A
  1. Fight the fire.

2. Land as soon as possible if fire continues

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
26
Q

Fuel System Limits

A 
300 lbs. Max. Imbalance 
265 lbs. Min. in each main for takeoff 
10 hrs.  Max. with fuel press light 
775 gal Max usable fuel quantity ER
IF fuel in aux.’s - mains must be full (Main and Aux full before filling)
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
27
Q

G load limitations

A

Flaps Up -1.21 to +3.01

Flaps Down 0.0 to +2.0

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
28
Q

Throttle Push

A

870 degrees for 5 min. This values is limited to 5 min in the event of an engine failure. Torque not to exceed 100%.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
29
Q

ICING LIMITATIONS:

  1. ENGINE ANTI-ICE, LEFT and RIGHT, shall be ON for operation in ambient temperatures of __°C or below when flight free of ___________ cannot be assured.
  2. ENGINE ANTI-ICE, LEFT and RIGHT, shall be OFF for take-off operations in ambient temperatures of above +__°C.
A

ICING LIMITATIONS:

  1. ENGINE ANTI-ICE, LEFT and RIGHT, shall be ON for operation in ambient temperatures of +5°C or below when flight free of visible moisture cannot be assured.
  2. ENGINE ANTI-ICE, LEFT and RIGHT, shall be OFF for take-off operations in ambient temperatures of above +10°C.
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
30
Q

AUTOPILOT MISTRIM [E] OR [A]

A
  1. Flight controls — Hold firmly (control
    forces may exceed 25 pounds).
  2. Autopilot — Disengage.
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
31
Q

Pneumatic Pressure Limits

A

12-20 psi Normal Operating Range

20 psi Max

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
32
Q

Propeller Failure (Above 1768 RPM)

A
  1. POWER lever (affected engine) — IDLE.

2. PROP lever (affected engine) — FEATHER.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
33
Q

Rudder Boost

A

Must be operational for all flights

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
34
Q

Yaw Damp System

A

19,000 Max Alt Inop (Dual Strakes)
Greater than above, Must be On Except for:
Takeoff and Landing (check REL)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
35
Q

Max Operating Altitude

A

35,000 feet

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
36
Q

MEK ~ DC POWER (%) ~ MEK

A 
Ground Ops:
55 Max (55-70% N1)
In Flight:
100 Max (Sea Level - 34,000 MSL)
95 Max (Above 34,000 MSL)
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
37
Q

Spins

A
  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 pullout.
38
Q

MEK ~ ITT Limits ~ MEK

A 
840 Cruise Climb
840 Mac Cruise
850 Takeoff
840 Max Continuous
870 Transient (20 seconds)
39
Q

Temperature Limits

A

ISA +37 Max SL to 25000’

ISA +31 Max above 25000’

40
Q

Brake de-ice limitations (Don’t use)

A
  1. Above 15 C

2. More than 10 min. w/wheels retracted

41
Q

LIMITATIONS ON THE USE OF AVIATION GASOLINE
1. Operation is limited to _____ hours between
engine overhauls.
2. Operation is prohibited if either standby fuel
pump is ___________.
3. Crossfeed capability is required for flight above
_________ feet pressure altitude (FL____).

A

LIMITATIONS ON THE USE OF AVIATION GASOLINE
1. Operation is limited to 150 hours between
engine overhauls.
2. Operation is prohibited if either standby fuel
pump is inoperative.
3. Crossfeed capability is required for flight above
20,000 feet pressure altitude (FL200).

42
Q

Max Zero Fuel Weight (VaDER)

A

13430 lbs

43
Q

VSSE (Intentional One Engine Inop)

A

135 KIAS

44
Q

Generator Load W/OAT greater than 10 deg C.

A

30% with Air Conditioner ON

50% with Air Conditioner OFF

45
Q

Engine Malfunction During Flight

A
  1. AP/YD — Disengage.
  2. POWER — As required.
  3. Failed engine — Identify.
  4. Propeller — Verify feathered. If propeller
    does not autofeather, perform manual
    feather.
46
Q

MMO (Above 24,000 feet)

A

.58 mach

47
Q

VMO (Below 24,000 feet)

A

245 KIAS

48
Q

VYSE

A

135 KIAS

49
Q

Torque Limits

A

0 – 100% Normal operating range (1000-1700 rpm)
96% Max. TQ, props above 1700 RPM
102% Transient 7 minutes
156% Max transient (20 Sec)

50
Q

Cabin altimeter and differential limitation

A

6.6 psig Max cabin differential

51
Q

VA (Flaps Up) - Maneuvering Speed

A

182 KIAS

52
Q

Engine Malfunction (Second Engine)

A
  1. Airspeed — As required.
  2. POWER lever — IDLE.
  3. PROP lever — As required.
53
Q

EXCESSIVE DIFFERENTIAL PRESSURE (CABIN DIFF HI ANNUNCIATOR ILLUMINATED)

  1. _____________________________
  2. _____________________________
  3. _____________________________
  4. _____________________________
  5. _____________________________
A

EXCESSIVE DIFFERENTIAL PRESSURE (CABIN DIFF HI ANNUNCIATOR ILLUMINATED)

  1. Bleed air valve switches – Enviro off
  2. Crew Oxygen Mask – Emer and don
  3. Mic switches – Oxy
  4. Passenger Manual Dropout Handle – Pull on
  5. Descend – As required
54
Q

DC Power Ground Operation Limits (-60 Engines)

A

75% Max. (62% - 70% N1)

100% Max. (70% - 100% N1)

55
Q

Emergency Descent

A
  1. POWER levers — IDLE.
  2. PROP levers — HIGH RPM.
  3. FLAPS (202 KIAS max) — APPROACH.
  4. LDG GEAR CONTROL handle (182
    KIAS max) — DOWN.
  5. Airspeed — 182 KIAS maximum.
56
Q

Vx

A

135 KIAS

57
Q

External Power Limits

A

28.0 - 28.4 volts normal
1000 volts momentary
300 volts continuous

58
Q

Engine Malfunction After V1

A
  1. POWER — Maximum allowable.
  2. LANDING GEAR CONTROL handle— UP
    (after positive rate of climb confirmed).
  3. Airspeed — Maintain V2 TO 400 FT AGL and clear of obstacles.
  4. Propeller — Verify feathered. If propeller
    does not autofeather, perform manual
    feather.
  5. FLAPS (after VYSE) — UP.
59
Q

Single – Engine Go Around

A
  1. POWER — Maximum allowable.
  2. LANDING GEAR CONTROL handle — UP.
  3. FLAPS — UP.
  4. Airspeed - Vyse.
60
Q

MEK ~ Turbine Tach (N1) % ~ MEK

A

55% Min Ground Idle
64% Min Flight Idle
104% Max
104% Max Transient

61
Q

Cracked Cabin Window

A
  1. Crew oxygen masks — ON.

2. MIC switches — OXY.

62
Q

Gyro Suction Gage limits

A
  1. 3 to 5.9 in. Normal SL to 15,000 ft

2. 8 to 4.3 in. Normal 15,000 to 35,000 ft

63
Q

Unscheduled Rudder Boost Activation

A
  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.
64
Q

Wing Fire

A
  1. Perform engine shutdown on affected side.

2. Land as soon as possible.

65
Q

Oil Pressure Limits

A

60 psi Minimum low idle
60-90 psi Caution Range (Torque limited to 62%)
90-135 psi Normal operating
200 psi Max. Starting

*Note: Oil pressure below 60 psi is unsafe and requires engine shutdown or landing at nearest suitable airport. Fluctuations of +/- 10 psi are acceptable.

66
Q

LOSS OF PRESSURIZATION (CABIN ALT OR CABIN ALT HI ANNUNCIATOR ILLUMINATED)

  1. _____________________________
  2. _____________________________
  3. _____________________________
  4. _____________________________
A

LOSS OF PRESSURIZATION (CABIN ALT OR CABIN DIFF HI ANNUNCIATOR ILLUMINATED)

  1. Crew Oxygen masks – Emer and don
  2. Mic Switches – Oxy
  3. Passenger Manual Dropout Handle – Pull On
  4. Descend – As required
67
Q

ER Fuel Quantity

A

118 gal per side, 236 total
775 gal (5192 lbs.) with main, aux, and ER full
Range approx. 2300NM, 8hrs endurance

68
Q

AUTOPILOT TRIM FAIL [TRIM]

A
  1. Flight controls — Hold firmly.

2. Autopilot — Disengage.

69
Q

Both D.C. GEN lights illuminated

A

MISSION POWER - OFF
INSTRUMENT EMERGENCY LIGHTS - ON (if required)
GENERATORS - GEN RESET, THEN ON IF EITHER GEN WILL RESET
OPERATING GENERATOR LOAD METER - monitor 100% max if neither gen will reset
ECS MODE- off
Cockpit/cabin blower - auto
Non essential equipment - off

70
Q

Engine Malfunction Before V1 (Abort)

A
  1. POWER levers — GROUND FINE.

2. Braking — As required

71
Q

Engine/Nacelle Fire During Start or Ground Operations

A
  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. BAT BUS — EMER OFF.
72
Q

Maximum Glide (Emergency Procedure)

A
  1. LANDING GEAR CONTROL handle — UP.
  2. FLAPS — UP.
  3. PROP levers — FEATHER.
  4. Airspeed — 135 KIAS
73
Q

Engine Malfunction During Flight Below Vmca

A
  1. POWER — Reduce as required to maintain control.

2. PITCH ATTITUDE — Lower to accelerate above VMCA.

74
Q

VMCA (Flaps Up)

A

101 KIAS

75
Q

Airspeed for Maximum Glide range

A

135 KIAS

76
Q

Minimum for Reverse

A

40 KIAS

77
Q

Electrical Smoke or Fire

A
  1. Crew oxygen masks — EMERG and don.

2. MIC switches — OXY.

78
Q

VMCA (Flaps Approach)

A

98 KIAS

79
Q

DC Power In flight Operation Limits

A

100% Max. (Sea Level to 21,000ft MSL)
90% Max. (21,000ft to 26,000ft MSL)
80% Max. (26,000ft to 30,000ft MSL)
75% Max. (30,000ft to 32,000ft MSL)
70% Max. (32,000ft to 35,000ft MSL)
90% Max. (Single Engine all altitudes)

80
Q

Min Sustained Icing >15,000lbs (AWR)

A

150

81
Q

Starter limitations

A

30 sec On 5 min. Off;
30 sec On 5 min. Off;
30 sec On 30 min. Off

82
Q

MEK ~ Oil Temperature ~ MEK

A

0 to 110 Normal
11 to 115 Max Transient (10 minute)
55 Rec. fuel heater ops at T/O

83
Q

MEK ~ Props (N2) (RPM) ~ MEK

A 
* No Min Idle RPM for MEK
1450-1700 Normal
1650 Max Reverse
1700 Max
1870 Max Transient (20 seconds)
84
Q

VLO (Extension)

A

182 KIAS

85
Q

Weight limits (Normal Operations)

A 
16,600    	Max. Ramp Weight
16,500   	Max Takeoff Weight 
15,675	Max Landing Weight
13,430     Max Zero Fuel Weight (VaDER)
13,000    	Max. Zero Fuel Weight (M &amp; G)
550 lbs.  	Max. Bag Comp Weight 
One Person  Max on Airstair Door
86
Q

UNEXPECTED AUTOPILOT DISENGAGEMENT

A
  1. Aircraft Control - Maintain

2. Autopilot/trim disconnect switch - Press to first level to cancel horn

87
Q

STALLS (DEPARTURE FROM CONTROLLED FLIGHT)

A
  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
88
Q

MEK ~ ABS INOP ANNUNCIATOR ILLUMINATED OR FLASHING WITH BRAKE APPLICATION WHILE ON THE GROUND

A
  1. Brakes - Release
  2. Directional control - Maintain using rudder, steering, and if required, reverse thrust.
  3. Autopilot/trim disconnect switch - Press to second detent and hold
  4. Brakes - Apply normally
89
Q

~MEK~ ABS BRAKES ARE INEFFECTIVE OR PULLING TO ONE SIDE WHILE ON GROUND

A
  1. Brakes -Release
  2. Directional control - Maintain using rudder, steering, and if required, reverse thrust.
  3. Autopilot/trim disconnect switch - Press to second detent and hold
  4. Brakes - Apply normally
90
Q

Passenger Oxygen Auto Deployment system failure (Cabin Alt HI annunciation illuminated and PASS OXYGEN

A

Passenger Manual drop out handle -pull on

MC-12 Study Guide (10 decks)

Brainscape helps you reach your goals faster, through stronger study habits.
© 2024 Bold Learning Solutions. Terms and Conditions