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Lear 75 > LJ75 Phase IIIA Limitations > Flashcards

LJ75 Phase IIIA Limitations Flashcards

1
Q

Max Ramp Weight (MRW)

A

21,750 LB

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2
Q

Max Takeoff Weight (MTOW)

A

21,500 LB

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3
Q

Max Landing Weight (MLW)

A

19,200 LB

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4
Q

Max Zero Fuel Weight (MZFW)

A

16,(5)00 LB

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5
Q

Minimum Flight Weight (MFW)

A

14,000 LB

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6
Q

CG

A

3.5% (16,260) to 19.5% (21,750) fwd / 28% aft

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7
Q

Vmo

A

330

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8
Q

Mmo

A

Mach .81

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9
Q

Mmo (Mach trim inoperative and AP disengaged)
- Above FL420

A

Mach 0.78 (marked)

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10
Q

Mmo (Mach trim inoperative and AP disengaged)
- FL234 - FL420

A

Mach .76 to .78 (Marked)

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11
Q

Standby Vmo / Mmo
- Below FL220

A

331 KIAS

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12
Q

Standby Vmo / Mmo
- Above FL220

A

330 KIAS / M.81
(AP & Mach Trim Off lims not shown)

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13
Q

Vlo / Vle

A

200 / 260

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14
Q

VFE (Flaps 8°)

A

250

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15
Q

VFE (Flaps 20°)

A

200

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16
Q

VFE (Flaps 40°)

A

150

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17
Q

V MCG

A

105 (APR On or Off)

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18
Q

V MCA

A

107 (8°) / 107 (20°)

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19
Q

V MCL

A

110 (8°) / 102 (40°)

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20
Q

Max Field Elevation for Takeoff

A

14,000’

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21
Q

Max Tailwind

A

10k’ and below - 10 kts
12k’ - 5 kts
14k’ - 0 kts

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22
Q

Takeoff and landings on ________ Surfaces Only

A

Paved

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23
Q

Standing Water Limitation

A

3/4”

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24
Q

HI FLOW Must be ____ for takeoff

A

OFF

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25
Q

Max Fuel imbalance for takeoff

A

200 lbs

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26
Q

Rudder Boost must be ___ for takeoff

A

ON

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27
Q

APR must be _______ for takeoff

A

armed per chart

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28
Q

Engine Sync must be ________ for takeoff

A

OFF

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29
Q

ADC & AHRS must be ________ for takeoff

A

Onside

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30
Q

All displays must be ________ for takeoff

A

Operational

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31
Q

Max Altitude

A

51,000’

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32
Q

Max landing elevation

A

14,000’

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33
Q

Max tailwind when landing up to 14,000’

A

10 kts

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34
Q

The aircraft must be _________ for landing

A

Unpressurized

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35
Q

Max fuel imbalance for landing

A

200 lbs

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36
Q

Min turn-around time

A

15 minutes between touchdown and TO thrust

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37
Q

Does the min turn-around time apply to touch & go landings?

A

No

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38
Q

Load Factors (Flaps UP)

A

-1 - 2.9 Gs

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39
Q

Load Factors (Flaps Down)

A

0 - 2 Gs

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40
Q

Prohibited Maneuvers

A
  • Aerobatics
  • Intentional stalls above 18,000’
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41
Q

Flaps and Gear must not be extended above…

A

18,000’

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42
Q

Seat belts & shoulder harness must be worn during

A

Takeoff and Landing

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43
Q

FWD Partition Door must be open for…

A

Taxi, Takeoff, and Landing (if installed)

44
Q

Aircraft must be warmed to ______ before start

A

> -23°c

45
Q

The aircraft is considered cold soaked on the ground at ________ or less

A

-23°c

46
Q

The cabin temp must be ______ or warmer prior to takeoff.

A

-15°c

47
Q

ADC must be ________ for takeoff

A

onside

48
Q

AHRS must be ________ for takeoff

A

onside, prohibited > N, S Latitudes

49
Q

AP & FD must be _____ for takeoff

A

OFF

50
Q

It is permissible to overpower the AP.

A

False

51
Q

AP min use height for climb, en route, descent

A

1,000’ AGL

52
Q

AP min use height on approach

A

180’ AGL

53
Q

Max glide slope angle for CAT I approaches

A

3.77°

54
Q

Max/min Delta P

A

+9.9 psid to -.5 psid

55
Q

Do not land with the cabin _________.

A

pressurized

56
Q

When must HI FLOW be OFF?

A
  • Takeoff power selected
  • Landing
  • Anti-Ice operations
  • Flight above 30,000’
57
Q

The ______ /_______ must be onboard (Garmin)

A

Approved Cockpit Reference Guide
Pilot’s Guide

58
Q

All displays must be __________ for takeoff

A

operational

59
Q

Prohibited Garmin Features

A
  • Airspace alerting
  • system clock local time
60
Q

Garmin Advisory (SA) only features

A
  • NEXRAD Wx
  • E-Checklist
  • E-docs
  • Moving Map
  • Synthetic Vision
61
Q

Airspace displayed on map is _________.

A

Allowed, but NO alerting

62
Q

Do not ______ or _______ the DEFAULT crew profile.

A

change or modify

63
Q

How many GTCs can a FMS flight plan be edited at one time?

A

One

64
Q

The use of non-WGS84 waypoints is ________.

A

prohibited

65
Q

Planned / flown GPS/SBAS IAPs must be __________________.

A

in the FMS database

66
Q

Engine sync must be OFF for…

A
  • Takeoff
  • Landing
  • Single Engine Ops
67
Q

Max external power amps

A

1500 A

68
Q

Max generator amps

A

300 continuous, higher transients allowed

69
Q

The Garmin G5000 system clock must be set to ____ time.

A

UTC

70
Q

The use of FMS TOLD is limited to takeoff and landing below _______ feet.

A

10,000

71
Q

The obstacle database includes obstacles ____ ft and higher and the coverage area includes _____ and most of ___________.

A

200; US; Western Europe

72
Q

The use of weather radar ________ mode is prohibited.

A

Altitude compensated Tilt

73
Q

Crew and passenger oxygen masks are not approved for use above _______ cabin altitude.

A

40,000’

74
Q

Prolonged operation of passenger masks above ______ cabin altitude is not recommended.

A

25,000’

75
Q

Hats and earmuff type headsets must be _______ prior to donning crew oxygen masks.

A

removed

76
Q

Rudder boost must be ___ for takeoff.

A

ON

77
Q

Do not ______ spoilers with flaps extended while _______, except as specified in __________.

A

extend; in-flight; EMERGENCY / ABNORMAL PROCEDURES

78
Q

Autospoilers must _______ for takeoff and landing.

A

ARMED

79
Q

Do not arm autospoilers for

A

training maneuvers where engine failure will be simulated above V1 speed or touch and go landings.

80
Q

Engine starter attempts; wait times

A

1; 1 minute
2; 2 minutes
3; 30 minutes

81
Q

Thrust Reverser operation is limited to

A

ground operations on paved surfaces

82
Q

Do not use the thrust reversers to _______ the aircraft.

A

back up

83
Q

The T/R circuit breakers may only be pulled in flight if…

A

directed by checklist procedure

84
Q

Thrust reversers must not be used for _______ landings.

A

touch and go

85
Q

Thrust reversers are limited to ______ when the engines are operating in MAN mode.

A

idle reverse

86
Q

Max tire speed

A

165 kts ground speed

87
Q

Engine computers must be _____ at all times unless _______.

A

ON; directed by checklist procedure

88
Q

Engine type

A

Honeywell TFE731-40BR-1B

89
Q

Engine thrust at sea level

A

3,850 lbs

90
Q

Engine preheat is recommended below ______.

A

-28°c

91
Q

Allow oil temperature to increase above _____ prior to increasing thrust above idle.

A

30°c

92
Q

Takeoff and APR time limit (two engine ops)

A

5 minutes

93
Q

Takeoff and APR time limit (single engine ops)

A

10 minutes

94
Q

Max engine thrust with oil temp < 30°c

A

IDLE

95
Q

Approved fuels

A

JP-5 / JP-8 / JetA & JetA-1 / DEF STAN 91-91 Jet A1 & CAN F-34 (consult AFM)

96
Q

SPPR refueling pressure limit

A

55 psig max

97
Q

SPPR defueling is limited to ______ psig

A

-10

98
Q

Hydraulic fluid type

A

MIL-PRF-5606

99
Q

The APU is limited to ______ operations only.

A

ground

100
Q

Max pressure altitude for APU ops

A

10,000’

101
Q

The APU must be ________ prior to takeoff.

A

shut down

102
Q

APU operation during gravity fill refueling is ________.

A

PROHIBITED

103
Q

APU operation during fluid de-icing / anti-icing is ___________.

A

PROHIBITED

104
Q

Takeoff is ____________with amber APU FAIL CAS displayed.

A

PROHIBITED

105
Q

If the APU automatically shuts down due to an APU failure, a _________________ must be conducted prior to the flight.

A

visual inspection

106
Q

APU start attempts; wait times.

A

1; 1 minute
2; 2 minutes
3; 15 minutes

107
Q

APU generator amp limits

A

300 Amps continuous; higher transient allowed

Lear 75 (2 decks)

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