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MC-12 Study Guide > 5 & 9 > Flashcards

5 & 9 Flashcards

(90 cards)

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1
Q

Environmental System Smoke or Fumes

A
  1. Crew oxygen masks — EMERG and on.

2. MIC switches — OXY.

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2
Q

Vy

A

135 KIAS

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3
Q

Gear cycle limits

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

2. 15 minutes rest after 6 cycles

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4
Q

L or R BLEED AIR FAIL annunciator illuminated

A
  1. BLEED AIR VALVES switch (affected

engine) — PNEU and ENVIR OFF.

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5
Q

Min Sustained Icing ≤ 15,000lbs (AWR)

A

140 KIAS

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6
Q

Climb Speeds

A

135 KIAS SL to 35,000 ft

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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)
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8
Q

Door Unlock Warning Annunciator Illuminated

A
  1. All occupants — Seated with seatbelts

securely fastened.

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9
Q

Pneumatic Boot limit

A

No operations below –40c

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10
Q

Engine Malfunction During Final Approach

A
  1. POWER — As required.

2. LANDING GEAR CONTROL — Recheck DOWN

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11
Q

Propeller de-ice ammeter limits

A

26-32 amps Normal Range

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12
Q

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

A

180

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13
Q

Max. Windshield de-icing

A

226 KIAS

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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
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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.
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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.

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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
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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

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19
Q

VLO (Retraction)

A

164 KIAS

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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)
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21
Q

Turbine Tachometer (N1 speed) limits

A

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

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22
Q

VFE

A

158 KIAS

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23
Q

Unscheduled Electric Elevator Trim

A
  1. Airplane attitude — Maintain using
    elevator control.
  2. AP/TRIM MASTER switch — Depress
    fully and hold.
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24
Q

VB (Turbulence Penetration)

A

170 KIAS

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25
Fuselage Fire
1. Fight the fire. | 2. Land as soon as possible if fire continues
26
Fuel System Limits
``` 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) ```
27
G load limitations
Flaps Up -1.21 to +3.01 | Flaps Down 0.0 to +2.0
28
Throttle Push
870 degrees for 5 min. This values is limited to 5 min in the event of an engine failure. Torque not to exceed 100%.
29
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.
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.
30
AUTOPILOT MISTRIM [E] OR [A]
1. Flight controls — Hold firmly (control forces may exceed 25 pounds). 2. Autopilot — Disengage.
31
Pneumatic Pressure Limits
12-20 psi Normal Operating Range | 20 psi Max
32
Propeller Failure (Above 1768 RPM)
1. POWER lever (affected engine) — IDLE. | 2. PROP lever (affected engine) — FEATHER.
33
Rudder Boost
Must be operational for all flights
34
Yaw Damp System
19,000 Max Alt Inop (Dual Strakes) Greater than above, Must be On Except for: Takeoff and Landing (check REL)
35
Max Operating Altitude
35,000 feet
36
MEK ~ DC POWER (%) ~ MEK
``` Ground Ops: 55 Max (55-70% N1) ``` ``` In Flight: 100 Max (Sea Level - 34,000 MSL) 95 Max (Above 34,000 MSL) ```
37
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 pullout.
38
MEK ~ ITT Limits ~ MEK
``` 840 Cruise Climb 840 Mac Cruise 850 Takeoff 840 Max Continuous 870 Transient (20 seconds) ```
39
Temperature Limits
ISA +37 Max SL to 25000’ | ISA +31 Max above 25000’
40
Brake de-ice limitations (Don't use)
1. Above 15 C | 2. More than 10 min. w/wheels retracted
41
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____).
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
Max Zero Fuel Weight (VaDER)
13430 lbs
43
VSSE (Intentional One Engine Inop)
135 KIAS
44
Generator Load W/OAT greater than 10 deg C.
30% with Air Conditioner ON | 50% with Air Conditioner OFF
45
Engine Malfunction During Flight
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
MMO (Above 24,000 feet)
.58 mach
47
VMO (Below 24,000 feet)
245 KIAS
48
VYSE
135 KIAS
49
Torque Limits
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
Cabin altimeter and differential limitation
6.6 psig Max cabin differential
51
VA (Flaps Up) - Maneuvering Speed
182 KIAS
52
Engine Malfunction (Second Engine)
1. Airspeed — As required. 2. POWER lever — IDLE. 3. PROP lever — As required.
53
EXCESSIVE DIFFERENTIAL PRESSURE (CABIN DIFF HI ANNUNCIATOR ILLUMINATED) 1. _____________________________ 2. _____________________________ 3. _____________________________ 4. _____________________________ 5. _____________________________
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
DC Power Ground Operation Limits (-60 Engines)
75% Max. (62% - 70% N1) | 100% Max. (70% - 100% N1)
55
Emergency Descent
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
Vx
135 KIAS
57
External Power Limits
28.0 - 28.4 volts normal 1000 volts momentary 300 volts continuous
58
Engine Malfunction After V1
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
Single – Engine Go Around
1. POWER — Maximum allowable. 2. LANDING GEAR CONTROL handle — UP. 3. FLAPS — UP. 4. Airspeed - Vyse.
60
MEK ~ Turbine Tach (N1) % ~ MEK
55% Min Ground Idle 64% Min Flight Idle 104% Max 104% Max Transient
61
Cracked Cabin Window
1. Crew oxygen masks — ON. | 2. MIC switches — OXY.
62
Gyro Suction Gage limits
4. 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
Unscheduled Rudder Boost Activation
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
Wing Fire
1. Perform engine shutdown on affected side. | 2. Land as soon as possible.
65
Oil Pressure Limits
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
LOSS OF PRESSURIZATION (CABIN ALT OR CABIN ALT HI ANNUNCIATOR ILLUMINATED) 1. _____________________________ 2. _____________________________ 3. _____________________________ 4. _____________________________
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
ER Fuel Quantity
118 gal per side, 236 total 775 gal (5192 lbs.) with main, aux, and ER full Range approx. 2300NM, 8hrs endurance
68
AUTOPILOT TRIM FAIL [TRIM]
1. Flight controls — Hold firmly. | 2. Autopilot — Disengage.
69
Both D.C. GEN lights illuminated
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
Engine Malfunction Before V1 (Abort)
1. POWER levers — GROUND FINE. | 2. Braking — As required
71
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. BAT BUS — EMER OFF.
72
Maximum Glide (Emergency Procedure)
1. LANDING GEAR CONTROL handle — UP. 2. FLAPS — UP. 3. PROP levers — FEATHER. 4. Airspeed — 135 KIAS
73
Engine Malfunction During Flight Below Vmca
1. POWER — Reduce as required to maintain control. | 2. PITCH ATTITUDE — Lower to accelerate above VMCA.
74
VMCA (Flaps Up)
101 KIAS
75
Airspeed for Maximum Glide range
135 KIAS
76
Minimum for Reverse
40 KIAS
77
Electrical Smoke or Fire
1. Crew oxygen masks — EMERG and don. | 2. MIC switches — OXY.
78
VMCA (Flaps Approach)
98 KIAS
79
DC Power In flight Operation Limits
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
Min Sustained Icing >15,000lbs (AWR)
150
81
Starter limitations
30 sec On 5 min. Off; 30 sec On 5 min. Off; 30 sec On 30 min. Off
82
MEK ~ Oil Temperature ~ MEK
0 to 110 Normal 11 to 115 Max Transient (10 minute) 55 Rec. fuel heater ops at T/O
83
MEK ~ Props (N2) (RPM) ~ MEK
``` * No Min Idle RPM for MEK 1450-1700 Normal 1650 Max Reverse 1700 Max 1870 Max Transient (20 seconds) ```
84
VLO (Extension)
182 KIAS
85
Weight limits (Normal Operations)
``` 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 & G) 550 lbs. Max. Bag Comp Weight One Person Max on Airstair Door ```
86
UNEXPECTED AUTOPILOT DISENGAGEMENT
1. Aircraft Control - Maintain | 2. Autopilot/trim disconnect switch - Press to first level to cancel horn
87
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
88
MEK ~ ABS INOP ANNUNCIATOR ILLUMINATED OR FLASHING WITH BRAKE APPLICATION WHILE ON THE GROUND
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
~MEK~ ABS BRAKES ARE INEFFECTIVE OR PULLING TO ONE SIDE WHILE ON GROUND
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
Passenger Oxygen Auto Deployment system failure (Cabin Alt HI annunciation illuminated and PASS OXYGEN
Passenger Manual drop out handle -pull on

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