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C12U CAE Fixed Wing Course > 5 & 9 > Flashcards

5 & 9 Flashcards

1
Q

VFE

A

157 KIAS

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2
Q

SINGLE ENGINE GO AROUND

A
  1. Power – Max allowable
  2. Landing gear control – Up
  3. Flaps – Up
  4. Airspeed – Vyse
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3
Q

EXCESSIVE DIFFERENTIAL PRESSURE (CABIN DIFF HI ANNUNCIATOR ILLUMINATED)

A
  1. Bleed air valve switches – Enviro off
  2. Crew & Pass Oxy Mask – Emer and don
  3. Mic switches – Oxy
  4. Descend – As req
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4
Q

G LOAD LIMITS @ 12,500

A
  • 1.27 to +3.17 Flaps Up

- 1.27 to +2.0 Flaps Down

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5
Q

ENGINE MALFUNCTION BEFORE V1 (ABORT)

A
  1. Power levers – Idle
  2. Braking – As Required.
  3. Reverse Thrust - As Required.
    If insufficient runway remains for stopping:
  4. Condition Levers - Fuel Cutoff.
  5. Fire Pull Handle - Pull.
  6. Master Switch - OFF.
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6
Q

Max X-wind

A

25 KIAS

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7
Q

ENVIRONMENTAL SMOKE OR FUMES

A
  1. Crew Oxygen masks – Emer and don

2. Mic Switches – Oxy

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8
Q

Min Speed aircraft can be trimmed

A

100 KIAS

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9
Q

Max tire speed (High float tires)

A

139 KIAS

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10
Q

ICING LIMITATIONS

A
  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 +15°C.
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11
Q

SPINS

A
  1. Control Column – Full forward, ailerons neutral
  2. Full rudder – opposite direction of spin
  3. Power levers – idle
  4. Rudder – neutralize when rotation stops
  5. Execute a smooth pullout
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12
Q

PRIMARY AND OVERSPEED GOVERNORS FAILED (PR0PS ABOVE 2120 RPM)

A
  1. Power lever (affected engine) – Idle

2. Prop lever (affected engine) – Feather

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13
Q

VLO Retraction

A

163 KIAS

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14
Q

ENGINE MALFUNCTION DURING FLIGHT

A
  1. AP/YD – Disengage
  2. Power – As required
  3. Affected Engine – Identify
  4. Prop lever(affected ENG) – Feather
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15
Q

CLIMB SPEEDS

A

160 KIAS SL-10,000’
140 KIAS 10-20,000’
130 KIAS 20-25,000’
120 KIAS 25-35,000’

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16
Q

VSSE

A

104 KIAS

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17
Q

Vmo (.52 Mmo), Vne, Max diving

A

260 KIAS

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18
Q

EMERGENCY DESCENT

A
  1. Power levers – Idle
  2. Prop levers – High RPM
  3. Flaps (200 KIAS Max) – Approach
  4. Landing Gear Control (181 KIAS Max) – Down
  5. Airspeed – 181 KIAS Max
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19
Q

FUSELAGE FIRE

A
  1. Fight the Fire

2. Land as soon as Possible

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20
Q

Max Ceiling

A

31,000 MSL

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21
Q

Min speed for reverse props

A

40 KIAS

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22
Q

Generator Max Load

A

100% In Flight
85% On Ground (High Idle)
88% Above 31,000 MSL

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23
Q

VLO Extension

A

181 KIAS

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24
Q

VMCA

A

86 KIAS

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25
Q

Va Flaps Up

A

181 KIAS

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26
Q

STARTER LIMITATIONS

A

40 sec on, 60 sec off
40 sec on, 60 sec off
40 sec on, 30 min off

27
Q

LEFT/RIGHT BLEED AIR FAIL ANNUNCIATOR ILLUMINATED

A
  1. Bleed air valve switch (affected engine) – Pneu and enviro off
28
Q

OIL PRESSURE

A 
60 psi		Min
60-85 psi	TQ limited to 49%
85-100 psi Caution below 21,000
100-135 psi	Normal below 21,000
85-135 psi Normal above 21,000 
200 psi           Max starting with cold oil
29
Q

Va Flaps Down

30
Q

FUEL SYSTEM

A 
2550lbs  Full Mains (386 gal)
3600lbs Full Mains/Aux (544 gal)
1000lbs	Max Imbalance
265lbs	Min, each main for takeoff
10hrs	Max w/ Fuel Press Low Light
150 hrs    AVGAS use
31
Q

BRAKE DE-ICE LIMITATIONS

A

Don’t use:

  1. Above 15 C
  2. More than 10 min w/ wheels retracted
32
Q

MAXIMUM GLIDE

A
  1. Landing Gear Control – Up
  2. Flaps – Up
  3. Prop levers – Feather
  4. Airspeed – as req
33
Q

GYRO SUCTION GUAGE LIMITS

A
  1. 3-5.9in Normal, SL-15,000’

2. 8-4.3in Normal, 15,000’ to 35,000’

34
Q

GEAR CYCLE LIMITS

A
  1. 6 Cycles at 1 cycle every 5 min

2. 15 min rest after 6 cycles

35
Q

ELECTRICAL SMOKE OR FIRE

A
  1. Crew Oxygen masks – 100% and don

2. Mic Switches – Oxy

36
Q

Vy (12,500)

37
Q

WING FIRE

A
  1. Peform engine shutdown on affected side

2. Land as soon as possible

38
Q

Max Windshield Deicing

39
Q

YAW DAMP SYSTEM

A

17,000’ Max alt Inop (if not Dual Strakes)

Greater than above must be on except for Takeoff/Landing, Check REL

40
Q

ENGINE FAILURE DURING FINAL APPROACH

A
  1. Power – As req

2. Landing Gear – Recheck down

41
Q

PNEUMATIC BOOT OPERATION

A

No operation below -40 C

42
Q

OIL TEMPERATURE

A

-40 to 99 Starting
99 Max Low Idle
0-99 Normal Op Range/Reverse
99-104 Max Transient (5 Min)

43
Q

Torque Limits

A 
49%		Max TQ, props below 1600 rpm
81%		Max TQ, props above 2000 rpm
20-100%Normal Op Range(1600-2000 rpm)
100%	Max 
123% 	Max Transient (5 secs)
44
Q

LOSS OF PRESSURIZATION (Above 10k Feet)

A
  1. Crew Oxygen masks – 100% and don

2. Mic Switches – Oxy

45
Q

CABIN ALTIMETER AND DIFFERENTIAL LIMITS

A

6.1 psig Max cabin differential

46
Q

PROP DE-ICE AMMETER LIMITS

A

18-24 amps Normal

47
Q

ENGINE MALFUNCTION (SECOND ENGINE)

A
  1. Airspeed – As req
  2. Power lever – Idle
  3. Prop lever – As req
48
Q

ENGINE/NACELLE FIRE DURING START/GROUND OPERATIONS

A
  1. Prop levers – Feather
  2. Condition levers – Fuel Cutoff
  3. F/W pull handle - Pull
  4. Eng Fire Push to ext - Push
  5. Master Switch - Off
49
Q

WEIGHT LIMITS

A 
14,090	Max Ramp
14,000	Max T/O
12,500	Max Landing
11,000	Max ZFW
550         Max baggage
300 		Max Airstair Door
238         Toilet
200 lb/ft2 max loading on seat tracks
100 lb/ft2 max loading on floor areas
50
Q

ENGINE MALFUNCTION AFTER V1

A
  1. Power – Max allowable.
  2. Landing Gear Control – Up (after positive rate of climb confirmed.
  3. Propeller – Verify feathered, if propeller doesn’t autofeather, perform manual feather
  4. Flaps (after Vyse) – Up
51
Q

Vfe Flaps Approach

52
Q

PROPS (N2)

A 
1600-2000rpm	Normal Op Range
1900rpm		        Max Reverse (1 Min)
2000rpm		Takeoff / Max Cont
2200rpm		         Max Transient (5 Sec)
2000-2080rpm      Primary Gov Failure
2120rpm            Fuel Top Gov (106% sel)
53
Q

Vb

54
Q

VYSE

55
Q

Min Airspeed Sustained Icing

56
Q

TGT Limits

A 
400-800	Normal
750C	Max Low Idle / Reverse (1 Min)
770C	Climb / Cruise
800C	Takeoff/Max Continuous
850C      Max Transient
1000C	Max Transient starting (5 secs)
57
Q

PNEUMATIC PRESSURE

A

12-20 psi Normal Op Range
16 psi Max with one bleed air inop
20psi Max

58
Q

TURBINE TACH (N1)

A 
56%		Low Idle
65%        Min A/C
85%        1 ENG Pressurization/De-ice/Boots
88%         Max reverse (1 min)
101.5%	Max
102.6%	Max Transient (10 Sec)
59
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 pull handle - Pull
  5. Eng Fire Push to ext – Push as red
60
Q

Max Speed manual ice vane extension

61
Q

EXTERNAL POWER LIMITS

A

27.5 – 29.0 volts normal
1000 amps momentary
300 amps continuous

62
Q

Min Speed for manual gear extension

63
Q

TEMPERATURE LIMITS

A

ISA +37 Max, SL-25,000’

ISA +31 Max, 25,000’ to 35,000’

C12U CAE Fixed Wing Course (3 decks)

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