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Lear 45 Additional Questions > Limitations > Flashcards

Limitations Flashcards

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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
Single point pressure refueling limit
55 psi G
26
Thrust Reverser limitations
• 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
27
Turn Anti-ice on prior to flight and visual moisture in
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
28
Aircraft and components must be warmer than what temperature prior to start?
-23°C
29
Cabin temperature prior to takeoff?
-15°C
30
Mmo Mach trim operative? Mach trim in-operative an auto pilot engaged?
Mach 0.81
31
Mach trim inoperative and auto pilot disengaged? 23,400-FL420 Above FL420? 
M .76-.78 Above FL420 - M.78
32
Vmo
330 kias
33
Vmo standby instruments
325 Kias
34
Mmo Standy Instruments
M 0.75
35
Vlo
200 Kias
36
Vle
260 Kias
37
Vfe Flaps 8 Flaps 20 Flaps 40
250 200 150
38
Vmca Flaps 8 Flaps 20
Vma Flaps 8 - 103 Kias Flaps 20 - 101 Kias
39
Vmcg Rudder boost on, APR On Rudder boost on, APR Off
Vmcg Rudder boost on, APR On. - 102 Kias Rudder boost on, APR off. - 100 Kias
40
Vmcl Flaps 8 Flaps 40
Vmcl Flaps 8 - 105 Kias Flaps 40 - 98 Kias
41
Turbulent air penetration speed
250 Kias or M 0.73 (Whichever is less)
42
Demonstrated crosswind
22 Kias
43
Tailwind component for landing
10 kts
44
Tailwind for landing for takeoff 12,000 feet and below
10 kts
45
Minimum battery voltage to close battery relay on the ground
14 volts
46
Approximate battery voltage
24 volts
47
GPU amp limits
1500 Amps
48
Continuous generator output
300 amps (Higher loads for cross start and battery charging authorized)
49
Maximum main tire speed
165 kts ground speed
50
Main tire pressure
165 psi loaded
51
Nose tire pressure
104 psi loaded
52
Nose will steering authority
60° decreases to 7° at 70 kts
53
Emergency brake accumulator
At least six brake applications
54
Maximum certified Landing Weight exceeded
Perform hard and overweight landing inspection
55
Maximum brake energy weight exceeded
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
What engine do we have? (Modified)
Honeywell TFE 731–20 BR
57
What are the start cycles for the engine?
1st attempt - 1 minute 2nd attempt - 2 minutes 3rd attempt - 30 minutes
58
What is the starting Max ITT?
991°C
59
What is the APR max ITT?
1013°C for five minutes (life of engine) Extra 150 lbs of thrust (3650 lbs total)
60
What is the TO Max ITT?
991°C (5 min max)
61
What is MCT Max ITT?
991°C
62
What is the max MCR ITT?
974°C 
63
Oil level should be checked within how long of shut down?
One hour
64
When should engine sync be off?
• take off • landing • single engine operations
65
APU start cycles
1st attempt- 1 minute 2nd attempt - 2 minutes 3rd attempt - 15 minutes
66
Approve fuels for APU?
Same as approved for Engines…. Jet A, Jet A1, JP-5, JP-8
67
What are the ambient temperature limitations for the APU?
Continuous operation up to an ambient temperature of 125°F * APU fan fails limited to 100°F
68
When can APU be used?
Ground use only at field pressure altitude up to 10,000 feet
69
What is the APU continuous generator limit?
300 Amps (Hire transient loads for cross darts and battery charging are authorized)
70
Can you take off with APU fail Amber CAS message?
No
71
What do you do in the event of APU auto shut down?
Visual inspection prior to flight… Preferably call Maintenance
72
What is the max pressure altitude enroute?
51,000 feet
73
Max takeoff and landing altitude?
14,000 feet
74
Delta P limits
9.9 PSId to -0.5 PSI
75
Cabin altitude caution?
Above 8500 cabin altitude
76
EMER press automatic activation?
Above 9500 cabin altitude (Landing set 8,000 or less)
77
Cabin altitude warning?
Above 10,000 feet cabin altitude (Landing set 8,000 or less)
78
Outflow valve closes?
Above 13,700 Cabin altitude
79
Masks deploy with EMER lights
Above 14,500 feet cabin altitude (Landing set 8,000 or less)
80
Hi Flo must be off for?
• Take off • landing • anti-ice operations • flight above 30,000 feet
81
Can you land with Cabin pressurized?
No
82
Rudder Boost…
Must be on for Takeoff

Lear 45 Additional Questions (3 decks)

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