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Lear 45 Additional Questions > Limitations > Flashcards

Limitations Flashcards

1
Q

Required crew

A

Pilot and copilot

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2
Q

Seatbelt and shoulder harness required

A

Takeoff and landing

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3
Q

EICAS or MFD for takeoff and landing

A

Summary or flight page

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4
Q

Runway water condition for takeoff and landing

A

3/4 of an inch

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5
Q

Flaps down maneuvering load factor

A

2G – 0G

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6
Q

Do you not extend spoilers with flaps extended no intentional stalls flaps or gear extension above

A

18,000 feet

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7
Q

Auto spoilers armed

A

Takeoff and landing

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8
Q

YAW damp

A

Not required

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9
Q

Hydraulic fluid

A

Red mil spec 5606

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10
Q

ADC and AHRS for takeoff

A

Normal

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11
Q

Auto pilot for takeoff and landing

A

Off

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12
Q

Auto pilot minimum used Heights

A

500 feet AGL – climb enroute or descent

200 feet AGL - approach

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13
Q

Minimum turnaround time

A

15 minutes

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14
Q

Maximum ramp weight

A

21,750 pounds

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15
Q

Maximum certified takeoff weight

A

21,500 pounds

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16
Q

Maximum certified Landing Weight

A

19,200 pounds

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17
Q

Minimum flight weight

A

14,000 pounds

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18
Q

Maximum zero fuel weight

A

16,500 pounds

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19
Q

Maximum aft baggage weight

A

500 pounds

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20
Q

Approved fuel’s

A

Referenced the addendum, But we were taught
Jet-A, Jet A1, JP-5, JP-8

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21
Q

Fuel capacity

A

6062 pounds (904.8 gallons)

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22
Q

Fuselage fuel tank capacity

A

2708 pounds (404.2 gallons)

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23
Q

Wing fuel tank capacity

A

Left 1678 pounds

Right 1676

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24
Q

Fuel balance for All phases of flight

A

200 pounds

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25
Q

Single point pressure refueling limit

A

55 psi G

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26
Q

Thrust Reverser limitations

A

• idle only in Manual mode
• max reverse thrust down to 40 kts
• do not back up the aircraft
• Not used for touch-and-go landings
• Ground operations on paved surfaces

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27
Q

Turn Anti-ice on prior to flight and visual moisture in

A

In flight… One minute prior… +10°C to -40°C and visible moisture

On the ground… Two minutes prior… +10°C and below and visible moisture, 1 mile visibility

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28
Q

Aircraft and components must be warmer than what temperature prior to start?

A

-23°C

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29
Q

Cabin temperature prior to takeoff?

A

-15°C

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30
Q

Mmo Mach trim operative?
Mach trim in-operative an auto pilot engaged?

A

Mach 0.81

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31
Q

Mach trim inoperative and auto pilot disengaged?
23,400-FL420

Above FL420?


A

M .76-.78

Above FL420 - M.78

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32
Q

Vmo

A

330 kias

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33
Q

Vmo standby instruments

34
Q

Mmo Standy Instruments

35
Q

Vlo

36
Q

Vle

37
Q

Vfe

Flaps 8
Flaps 20
Flaps 40

38
Q

Vmca
Flaps 8
Flaps 20

A

Vma

Flaps 8 - 103 Kias

Flaps 20 - 101 Kias

39
Q

Vmcg

Rudder boost on, APR On

Rudder boost on, APR Off

A

Vmcg

Rudder boost on, APR On. - 102 Kias

Rudder boost on, APR off. - 100 Kias

40
Q

Vmcl

Flaps 8
Flaps 40

A

Vmcl

Flaps 8 - 105 Kias

Flaps 40 - 98 Kias

41
Q

Turbulent air penetration speed

A

250 Kias or M 0.73

(Whichever is less)

42
Q

Demonstrated crosswind

43
Q

Tailwind component for landing

44
Q

Tailwind for landing for takeoff 12,000 feet and below

45
Q

Minimum battery voltage to close battery relay on the ground

46
Q

Approximate battery voltage

47
Q

GPU amp limits

A

1500 Amps

48
Q

Continuous generator output

A

300 amps

(Higher loads for cross start and battery charging authorized)

49
Q

Maximum main tire speed

A

165 kts ground speed

50
Q

Main tire pressure

A

165 psi loaded

51
Q

Nose tire pressure

A

104 psi loaded

52
Q

Nose will steering authority

A

60° decreases to 7° at 70 kts

53
Q

Emergency brake accumulator

A

At least six brake applications

54
Q

Maximum certified Landing Weight exceeded

A

Perform hard and overweight landing inspection

55
Q

Maximum brake energy weight exceeded

A

Perform high energy landing or rejected takeoff inspection…

Refer to QRH Red tab 18

then go to

• Aborted T/O AFM 3-44
• brake energy charts 5-144

56
Q

What engine do we have?
(Modified)

A

Honeywell TFE 731–20 BR

57
Q

What are the start cycles for the engine?

A

1st attempt - 1 minute
2nd attempt - 2 minutes
3rd attempt - 30 minutes

58
Q

What is the starting Max ITT?

59
Q

What is the APR max ITT?

A

1013°C for five minutes (life of engine)

Extra 150 lbs of thrust (3650 lbs total)

60
Q

What is the TO Max ITT?

A

991°C (5 min max)

61
Q

What is MCT Max ITT?

62
Q

What is the max MCR ITT?

A

974°C 

63
Q

Oil level should be checked within how long of shut down?

64
Q

When should engine sync be off?

A

• take off
• landing
• single engine operations

65
Q

APU start cycles

A

1st attempt- 1 minute
2nd attempt - 2 minutes
3rd attempt - 15 minutes

66
Q

Approve fuels for APU?

A

Same as approved for Engines….

Jet A, Jet A1, JP-5, JP-8

67
Q

What are the ambient temperature limitations for the APU?

A

Continuous operation up to an ambient temperature of 125°F

  • APU fan fails limited to 100°F
68
Q

When can APU be used?

A

Ground use only at field pressure altitude up to 10,000 feet

69
Q

What is the APU continuous generator limit?

A

300 Amps
(Hire transient loads for cross darts and battery charging are authorized)

70
Q

Can you take off with APU fail Amber CAS message?

71
Q

What do you do in the event of APU auto shut down?

A

Visual inspection prior to flight… Preferably call Maintenance

72
Q

What is the max pressure altitude enroute?

A

51,000 feet

73
Q

Max takeoff and landing altitude?

A

14,000 feet

74
Q

Delta P limits

A

9.9 PSId to -0.5 PSI

75
Q

Cabin altitude caution?

A

Above 8500 cabin altitude

76
Q

EMER press automatic activation?

A

Above 9500 cabin altitude

(Landing set 8,000 or less)

77
Q

Cabin altitude warning?

A

Above 10,000 feet cabin altitude

(Landing set 8,000 or less)

78
Q

Outflow valve closes?

A

Above 13,700 Cabin altitude

79
Q

Masks deploy with EMER lights

A

Above 14,500 feet cabin altitude

(Landing set 8,000 or less)

80
Q

Hi Flo must be off for?

A

• Take off
• landing
• anti-ice operations
• flight above 30,000 feet

81
Q

Can you land with Cabin pressurized?

82
Q

Rudder Boost…

A

Must be on for Takeoff

Lear 45 Additional Questions (3 decks)

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