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C12U CAE Fixed Wing Course > C12 U1 - Ch 5 - Limits Test > Flashcards

C12 U1 - Ch 5 - Limits Test Flashcards

1
Q

TQ Limits:

Normal Operating Range

A

20-100%

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2
Q

TQ Limits:

Maximum

A

100%

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3
Q

TQ Limits:

Max Transient (5 Seconds)

A

123%

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4
Q

TQ Limits:

Max w/PROP > 2000 RPM

A

81%

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5
Q

TQ Limits:

Max w/PROP < 1600 RPM

A

49%

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6
Q

TQ Limits:

Max w/Oil Press < 85 PSI

A

49%

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7
Q

Turbine Gas Temperature (TGT) Limits

Normal Operating Range

A

400-800* Celcius

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8
Q

Turbine Gas Temperature (TGT) Limits

Takeoff & Max Continuous

A

800* Celcius

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9
Q

Turbine Gas Temperature (TGT) Limits

Normal Climb/Cruise

A

770* Celcius

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10
Q

Turbine Gas Temperature (TGT) Limits

Max Reverse (1 Minute)

A

750* Celcius

1 Minute

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11
Q

Turbine Gas Temperature (TGT) Limits

Max Starting

A

1000* Celcius

5 Seconds

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12
Q

Turbine Gas Temperature (TGT) Limits

Max Low Idle

A

750* Celcius

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13
Q

Turbine Tachometer (N1) Speed

Takeoff & Max Continuous

A

101.5

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14
Q

Turbine Tachometer (N1) Speed

Transient & Time Limit

A

102.6

10 Seconds

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15
Q

Turbine Tachometer (N1) Speed

Max Below -48* C

A

100.1

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16
Q

Turbine Tachometer (N1) Speed

Minimum Low Idle

A

56

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17
Q

Propeller Tachometer (N2) RPM

Normal Operating Range

A

1600-2000 RPM

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18
Q

Propeller Tachometer (N2) RPM

Maximum

A

2000 RPM

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19
Q

Propeller Tachometer (N2) RPM

Max Transient

A

2200 RPM

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20
Q

Propeller Tachometer (N2) RPM

Max Reverse

A

1900 RPM

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21
Q

Oil Pressure PSI Limits

NORMAL below 21K Feet

A

100-135 PSI

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22
Q

Oil Pressure PSI Limits

NORMAL Above 21K Feet

A

85-135 PSI

23
Q

Oil Pressure PSI Limits

CAUTION below 21K Feet

A

85-100 PSI

24
Q

Oil Pressure PSI Limits

Minimum Low IDLE PSI

A

60 PSI

25
Q

Oil Temperature Limits (*C)

Takeoff & Max Continuous

A

0 - 99* Celcius

26
Q

Oil Temperature Limits (*C)

Starting Limit

A

-40* Celcius

27
Q

Oil Temperature Limits (*C)

Low Idle Range

A

-40 - 99* Celcius

28
Q

Oil Temperature Limits (*C)

Transient and Time Limit

A

99 - 104* Celcius

5 Minutes

29
Q

Pneumatic Pressure

Normal Range

A

12-20 PSI

30
Q

Pneumatic Pressure

Maximum

A

20 PSI Maximum

31
Q

Propeller Deicer Ammeter

A

14-18 Amperes Normal Operations

32
Q

Starter Limitations

A

40 sec on - 60 sec off

40 sec on - 60 sec off

40 sec on - 30 min off

33
Q

Aircraft Weight Limitations

Max Ramp
Max GTOW
Max Landing
Max Zero Fuel

A

14,090 lb. Max Ramp

14,000 lb. Max GTOW

12,500 lb. Max Landing

11,000 lb. Max Zero Fuel

34
Q

Cabin Altimeter and Differential Pressure

A

0-6.1 PSID Normal Range

6.1 PSID Maximum

35
Q

Brake deice system shall not be operated, except to test, at ambient temperatures above _______ * C.

A

15* Celcius

36
Q

Maintain ________% N1 or higher during simultaneous operations of the brake deice and surface deice.

A

85% N1

37
Q

Is Brake Deice use allowed during single engine operations?

A

No

38
Q

Max G loading (G’s) at 12,500 lbs (and below)

  • Flaps Up
  • Flaps Down
A

Wing flaps up (-/+) -1.27 to +3.17

Wing flaps down (-/+) -1.27 to +2.0

39
Q

Fuel Limitations

No Takeoff Range

A

0-265 LBS No Takeoff

40
Q

Fuel Limitations

Max Fuel Imbalance

A

1000 lbs

41
Q

Max Alt for ac operations

A

31,000 ft MSL

42
Q

The aircraft shall not be operated when the ambient temperatures are
warmer than International Standard Atmosphere (ISA) ______·C at SL to 25,000
ft or ISA ______ ·C above 25,000 ft PA.

A

The aircraft shall not be operated when the ambient temperatures are
warmer than International Standard Atmosphere (ISA) +37 ·C at SL to 25,000
ft or ISA +31 ·C above 25,000 ft PA.

43
Q

Ice vanes shall be extended for operations in ambient temperature of ______·c or
below when flight free of visible moisture cannot be assured.

A

Ice vanes shall be extended for operations in ambient temperature of +5·c or
below when flight free of visible moisture cannot be assured.

44
Q

Engine ice vanes shall be retracted at ______·C and above for flight operations.

A

Engine ice vanes shall be retracted at +15·C and above for flight operations.

45
Q

Minimum FAT for operation of deicing boots shall be _______ ·c.

A

Minimum FAT for operation of deicing boots shall be -40 ·c.

46
Q

Maximum crosswind component is _____ (KTS) at 90 degrees.

A

Maximum crosswind component is 25 (KTS) at 90 degrees.

47
Q

The pitot heat is limited to ______ minutes during ground operations.

A

The pitot heat is limited to 15 minutes during ground operations.

48
Q

ICING LIMITATIONS (SEVERE):

Use of the _____________ is prohibited when any of
the visual cues specified above exist, or when unusual lateral trim
requirements or autopilot trim warnings are encountered while the airplane
is in icing conditions.

A

Use of the autopilot is prohibited when any of
the visual cues specified above exist, or when unusual lateral trim
requirements or autopilot trim warnings are encountered while the airplane
is in icing conditions.

49
Q

BRAKE DEICE: Brake Deice system shall not be operated, except to test, at ambient temperatures above ____*C.

Maintain ________% N1 or higher during simultaneous operation of the brake deice and surface deice.

A

BRAKE DEICE: Brake Deice system shall not be operated, except to test, at
ambient temperatures above 15*C.

Maintain 85% N1 or higher during
simultaneous operation of the brake deice and surface deice.

50
Q

Hydraulic Landing Gear

Landing gear cycles, a complete retraction and extension, are limited to one every ___ minutes for a total of ____ cycles
followed by a ___ minute cool-down period.

A

Hydraulic Landing Gear. Landing gear cycles, a complete retraction and
extension, are limited to one every 5 minutes for a total of six cycles
followed by a 15 minute cool-down period.

51
Q

ICING LIMITATIONS (TYPICAL):

While in icing conditions, if there is an unexplained ____ % increase of torque needed to maintain airspeed in level flight, a cumulative total of ____ or more inches of ice accumulation on the wing, an unexplained decrease of _____ KIAS, or an unexplained deviation
between pilot and copilot airspeed indicators, the icing environment should be exited as soon as possible. Ice accumulation on the pitot tube assemblies could cause a complete loss of airspeed indication.

A

ICING LIMITATIONS (TYPICAL): While in icing conditions, if there is an
unexplained 30 % increase of torque needed to maintain airspeed in level
flight, a cumulative total of two or more inches of ice accumulation on the
wing, an unexplained decrease of 15 KIAS, or an unexplained deviation
between pilot and copilot airspeed indicators, the icing Evironment should be
exited as soon as possible. Ice accumulation on the pitot tube assemblies
could cause a complete loss of airspeed indication.

52
Q

Gyro Suction

A
  1. 8-4.3 inHg Normal 35,000-15,000

4. 3-5.9 inHg Normal 15,000-Sea Lvl

53
Q

Propeller Limitations

Prop RPM greater than ____ indicates a failure of the _____.

Prop RPM greater than ____ indicates a failure of both _____ and ____.

A

2000; Primary Governor

2120; Primary Governor, Overspeed Governor

C12U CAE Fixed Wing Course (8 decks)

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