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Learjet 45 > General (3/18/2024) > Flashcards

General (3/18/2024) Flashcards

1
Q

Max Ramp Weight

(LR45 Modified)

A

21,750 lbs

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2
Q

Max Certified Takeoff Weight

(LR45 Modified)

A

21,500 lbs.

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3
Q

Minimum Flight Weight

(LR45 Modified, LR45 Not Modified)

A

14,000 lbs.

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4
Q

Max Zero Fuel Weight

(LR45 Modified)

A

16,500 lbs.

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5
Q

Max Certified Landing Weight

(LR45 Modified, LR45 Not Modified, LR40)

A

19,200 lbs.

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6
Q

V MO

A

330 KIAS

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7
Q

M MO

A

.81M

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8
Q

MMO with Mach Trim Inop. & A/P Engaged

A

.81M

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9
Q

MMO with Mach Trim Inop. & A/P Disengaged

A

23,400 to 42,000 FT: .76 -.78 M

Above 42,000 FT: .78 M

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10
Q

STANDBY INSTRUMENTS

A

VMO 325 KIAS

MMO .75M

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11
Q

VLE

A

260 KIAS

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12
Q

VLO

A

200 KIAS

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13
Q

VFE Flaps 8º

A

250 KIAS

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14
Q

VFE Flaps 20º

A

200 KIAS

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15
Q

VFE Flaps 40º

A

150 KIAS

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16
Q

VMCA Flaps 8°

A

103 KIAS (Minimum control speed in flight at which the aircraft can be controlled with a maximum bank of 5 degrees, if one engine fails, the other engine remaining at takeoff power (takeoff flap setting, gear retracted))

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17
Q

VMCA Flaps 20°

A

101 KIAS????? (Minimum control speed in flight at which the aircraft can be controlled with a maximum bank of 5 degrees, if one engine fails, the other engine remaining at takeoff power (takeoff flap setting, gear retracted))

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18
Q

VMCG - Rudder Boost On, APR On

A

102 KIAS (Minimum speed, on the ground during takeoff, at which the aircraft can be controlled by the use of primary flight controls only, after a sudden failure of the critical engine, the other engine remaining at takeoff power.)

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19
Q

VMCG - Rudder Boost On, APR Off

A

100 KIAS (Minimum speed, on the ground during takeoff, at which the aircraft can be controlled by the use of primary flight controls only, after a sudden failure of the critical engine, the other engine remaining at takeoff power.)

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20
Q

VMCL Flaps 8°

A

105 KIAS (Minimum control speed in flight at which the aircraft can be controlled with a maximum bank of 5 degrees, if one engine fails, the other engine remaining at takeoff power (approach flap setting))

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21
Q

VMCL Flaps 40°

A

98 KIAS (Minimum control speed in flight at which the aircraft can be controlled with a maximum bank of 5 degrees, if one engine fails, the other engine remaining at takeoff power (approach flap setting))

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22
Q

Turbulent Air Penetration Speed

A

250 KIAS or .73M

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23
Q

Max Pressure Altitude – Takeoff and Landing

A

14,000 FT

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24
Q

Max Pressure Altitude Enroute

A

51,000 FT

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25
Q

Max Tailwind ≤ 12,000 FT

A

10 KTS

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26
Q

Max Water/Slush On Runway

A

.75 IN

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27
Q

Min Turn-Around Time

A

15 Minutes

28
Q

Max Fuel Imbalance

A

200 lbs

29
Q

Load Factor – Flaps UP

A

+2.9g to -1g

30
Q

Load Factor – Flaps Down

A

+2g to 0g

31
Q

EICAS or MFD

A

SUMRY or FLT Page for Takeoff and Landing

32
Q

Flaps and Gear - Max Altitude for Extension

A

18,000 FT

33
Q

Autopilot Minimum Altitudes

A
  1. Climb, Enroute, Descent ……………………. 500FT AGL
  2. LNAV Only…………………………………………400FT AGL
  3. LNAV/VNAV ……………………………………….300FT AGL
  4. LPV or DA………………………………………….200FT AGL
34
Q

Pressurization Delta P

A

9.9 to -0.5 psid

35
Q

Engine Sync Required Off

A
  1. Takeoff
  2. Landing
  3. Single – Engine Operations
36
Q

Wing/Stab Heat On

A

2 Minutes Before Takeoff Thrust

37
Q

Anti-Ice On

A

+10°C to -40°C and Visible Moisture

38
Q

MAX ITT APR

BR and AR Engines

A

BR- 1013°C
AR- 963°C

39
Q

MAX ITT T/O

BR and AR Engines

A

BR- 991°C
AR- 941°C

40
Q

Max ITT MCT

BR and AR Engines

A

BR- 991°C
AR- 916°C

41
Q

Max ITT MCR temperature

BR and AR Engines

A

BR- 974°C
AR- 900°C

42
Q

Max Start temperature

BR and AR Engines

A

BR- 991°C
AR- 941°C

43
Q

Oil Pressure (Normal Operating Range)

A

50 to 100 psi

44
Q

Oil Pressure (Starting)

A

125 psi

45
Q

Oil Temperature (Normal Operating Range)

A

30°C to 127°C

46
Q

Oil Temperature (Min for Starting)

A

-28ºC

47
Q

Oil Temperature > 30,000FT

A

140ºC

48
Q

APU Limitations (6 items)

A
  • 300 Amps Max APU Generator
  • Ground Use Only
  • Off During De-icing and Gravity Refueling
  • No Dispatch With APU FAIL CAS
  • Starter Cooling: 1 Min, 2 Mins, 15 Mins
  • 30 Seconds Between Stop and Off
49
Q

GPU Max Amps

A

1500 Amps

50
Q

Generator Limit

A

300 Max Continuous Amps

51
Q

Spoiler Deployment Prohibited

A

Flaps more than 0°

52
Q

Starter On Limit

A

1 Minute

53
Q

Starter Cooling

A

• 1 Minute
• 2 Minutes
• 30 Minutes

54
Q

Thrust Reverser Limitations (5 items)

A
  • Paved Surface
  • No Backing
  • No Use During Touch and Go’s
  • Max Thrust Only Above 40 KTS
  • Ground Use Only
55
Q

Tire Speed Limit. Tire pressure. Blowout temp (main only)

Nose and main

A

Nose: 182 KTS, 105 to 115 psi
Main: 165 KTS, 165 psi, > 390 F

56
Q

Hydraulic Fluid

A

MIL-H-5606

57
Q

Radar Off Near People

A

9 FT (this is what the AFM says)

58
Q

Radar Off Near Large Metal

A

100 FT

59
Q

Engine Idle Prior to Cutoff (Ground)

A

1 Minute

60
Q

What type of oil is used on the LR45?

A

Type II

61
Q

Oil Level Check

A

Within 1 Hour of Shutdown
(Preferably Within 15 Minutes After Shutdown)

62
Q

Max Baggage Compartment

A

500 lbs

63
Q

Best glide

A

160 KIAS

64
Q

Driftdown Speed

A

170-200 KIAS

65
Q

Demonstrated crosswind (not a limitation)

A

22 knots

Learjet 45 (11 decks)

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