Brainscape's Knowledge GenomeTM

Browse over 1 million classes created by top students, professors, publishers, and experts.


See full index

Lear 45/45XR > Operation limitations > Flashcards

Operation limitations Flashcards

1
Q

Maximum Pressure Altitude

TAKEOFF

A

14,000 ft

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q

Max Tailwind Component

Non SB 45-72-1

A

10 knots

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
3
Q

Max Tailwind Component
12,000 ft and below
(SB 45-72-1)

A

10 knots

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

Max Tailwind Component
Above 12,000 ft
(SB 45-72-1)

A

0 knots

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
5
Q

Max Pressure Altitude En Route

A

51,000 ft

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q

Max Fuel Imbalance En Route

45-002 thru 45-258 and 45-260, not modified by 45-28-8

A

500 lbs

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
7
Q

Max Fuel Imbalance En Route

45-259, 45-261 thru 45-2000, and prior modified by 45-28-8

A

200 lbs

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
8
Q

Max Pressure Altitude

Landing

A

14,000 ft

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
9
Q

Max Tailwind

A

10 knots

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q

Landing is limited to ____________ runways.

A

Paved

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
11
Q

Maximum runway contamination depth for FAA and JAA certified aircraft?

A

3/4 Inch (FAA) 1/2 inch (JAA)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
12
Q

Can you land with the cabin pressurized?

A

No, do not land with cabin pressurized.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
13
Q

Max fuel imbalance for landing

A

200 lbs

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
14
Q

EICAS display for landing or takeoff

A

SUMRY or FLT Page

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
15
Q

A minimum of _______ minutes must elapse between landing touchdown and selection of Takeoff thrust for next takeoff.

A

15 min.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
16
Q

Do Not extend flaps above ____________ feet.

A

18,000 ft

17
Q

Do Not extend Gear above __________ feet.

A

18,000 ft

18
Q

No aerobatic maneuvers, including spins are approved.

Intentional stalls are prohibited above _________ ft.

A

18,000 ft

19
Q

Can spoilers be extended with flaps extended?

A

No, do Not extend spoilers with flaps extended

20
Q

When must autospoilers be armed?

A

Takeoff and Landing, except for training maneuvers where engine failure will be simulated above V1 or touch and go landings.

21
Q

Can thrust reverser be used to back up aircraft?

A

NO

22
Q

Can you pull the thrust reverser circuit breaker in flight?

A

No, except as specified in QRH

23
Q

Thrust reverser must not be used during ________ and _______ landings.

A

Touch and go landings

24
Q

Maximum reverse thrust is usable down to ________KIAS.

A

40 KIAS

25
Q

TR’s limited to _______ when in MANUAL mode.

A

IDLE

26
Q

Icing conditions exist when the temperature is between _______ degrees to negative ______ degrees with visible moisture.

A

10 to -40 Celsius

27
Q

When do icing conditions exist for takeoff and on the ground?

A

10 degrees or below when visible moisture is falling or with snow, slush, ice, or standing water on taxiways or runways and 1 mile or less visibility.

28
Q

The Lear 45 is certified under FAR part 25. What category?

A

Transport

29
Q

What is the waiting period if two consecutive aborted takeoffs have been made?

A

4-hours. DO NOT attempt a third take off until completion of the waiting period and visual inspection has been performed.

30
Q

What is the definition of Takeoff Decision Speed (V1)?

A

The speed at which a decision to continue takeoff would result in 35ft above RW or a stop and not exceed scheduled takeoff distance.

31
Q

What is the definition of Rotation Speed (Vr)?

A

The speed at which rotation is initiated to obtain takeoff performance.

32
Q

What is the definition of Takeoff Safety Speed (V2)?

A

The actual speed at 35ft above the RW as demonstrated in flight during a single engine climb.

33
Q

What is the limit maneuvering load factor with flaps up?

A

2.9 to -1.0 G’s

34
Q

What is the limit maneuvering load factor with flaps down?

A

2.0 to 0 G’s

35
Q

The acceleration values limit the bank angle in a level coordinated turn to what degree of bank with flaps up?

A

70 degrees of bank

36
Q

The acceleration values limit the bank angle in a level coordinated turn to what degree of bank with flaps down?

A

60 degrees of bank

37
Q

What is the minimum temperature the aircraft and components must be warmed to prior to ground start?

A

-23 degrees C or above.

38
Q

What temperature must the cabin be warmed to prior to takeoff?

A

-15 deg. C.

Lear 45/45XR (9 decks)

Brainscape helps you reach your goals faster, through stronger study habits.
© 2024 Bold Learning Solutions. Terms and Conditions