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Lear 60 > Lear 60 Ops Limits > Flashcards

Lear 60 Ops Limits Flashcards

1
Q

Airspeed Limits

MMO up to FL370

A

.81 MACH

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2
Q

Airspeed Limits

MMO Mach Trim A/P Inop

A

.77 MACH

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3
Q

Airspeed Limits

VMO up to 8000 ft

A

300 KIAS

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4
Q

Airspeed Limits

VMO 8000 - 20000 ft

A

340 KIAS

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5
Q

Airspeed Limits

SPOILERS INOP

A

38000 FT

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6
Q

Airspeed Limits

VLE

A

260 KIAS

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7
Q

Airspeed Limits

VLO

A

200 KIAS

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8
Q

Airspeed Limits

Vfe (flaps - 8)

A

250 KIAS

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9
Q

Airspeed Limits

Vfe (flaps - 20)

A

200 KIAS

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10
Q

Airspeed Limits

Vfe (flaps - 40)

A

165 KIAS

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11
Q

Airspeed Limits

Vmca Flaps 8

A

120 KIAS

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12
Q

Airspeed Limits

Vmca Flaps 20

A

110 KIAS

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13
Q

Airspeed Limits

Vmcg Rudder Boost On/Off (Inop)

A

95 KIAS/116 KIAS

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14
Q

Airspeed Limits

Turb Air Penetration

A

250 KIAS/ .73 MACH

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15
Q

Airspeed Limits

Max DEMO CROSS WIND

A

29 KIAS

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16
Q

Airspeed Limits

Max CROSS WIND w/o Spoil.

A

25 KIAS

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17
Q

Airspeed Limits

Max TAIL WIND

A

10 KIAS

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18
Q

Airspeed Limits

Max TIRE SPEED

A

182 KIAS

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19
Q

Airspeed Limits

RWY water/slush contamination

A

3/4 in. (19mm)

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20
Q

Weight and Balance

Max RAMP WEIGHT

A

23,750 Pounds

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21
Q

Weight and Balance

Max CERT T/O WEIGHT

A

23,500 Pounds

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22
Q

Weight and Balance

Max CERT LANDING WEIGHT

A

19,500 Pounds

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23
Q

Weight and Balance

Max ZERO FUEL WEIGHT

A

17,000 Pounds

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24
Q

Weight and Balance

Max T/O Without Anti-Skid

A

18,500 Pounds

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25
Q

Load Factors

FLAPS UP

A

+3G TO -1G

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26
Q

Load Factors

FLAPS DOWN

A

+2G TO 0G

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27
Q

Oil System Limits

MAX Oil Temperature

A

143

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28
Q

Oil System Limits

Oil Pressure Green Arc (normal)

A

36 - 80 PSI

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29
Q

Oil System Limits

Check Oil Level after Landing within:

A

10 Minutes of engine shutdown

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30
Q

Oil System Limits

Engine Oil Types

A

Type II/Mobile 254

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31
Q

Oil System Limits

OIL CAPACITY (RESERVOIR)

A

1.95 US GALLONS

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32
Q

Fuel Limits

Fuel Jet A, A-1, B, JP 5/8

A

Fuel Anti-Ice Not Required

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33
Q

Fuel Limits

Max Out of Balance T/O - Land

A

200 Pounds

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34
Q

Fuel Limits

Max Out of Balance Inflight

A

500 Pounds

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35
Q

Fuel Limits

LOW FUEL PRESSURE LIGHT

A

2.75 PSI

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36
Q

Fuel Limits

Low Fuel Light either Wing

A

410 Pounds

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37
Q

Fuel Limits

Fuselage Tank Gravity Transfer Unusable

A

350 Pounds

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38
Q

Fuel Limits

Aviation Gas

A

Prohibited

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39
Q

Power Plant Limitations

Max N1 APR/MCT/MCR and T/O

A

102%

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40
Q

Power Plant Limitations

Max N2 APR/MCT/MCR and T/O

A

102%

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41
Q

Power Plant Limitations

N1/N2 Transient for 20 Seconds

A

104%

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42
Q

Power Plant Limitations

Engine Computer Must Be In Auto

A

Except Emergency

43
Q

Power Plant Limitations

Max Idle N2 Ground/Inflight

A

52% N2/65% N2

44
Q

Power Plant Limitations

APR and TAKEOFF POWER LIMITS

A

5 Minutes

45
Q

ITT LIMITS/BRAKE LIMITS

Max Temperature -Start

A

950 ITT

46
Q

ITT LIMITS/BRAKE LIMITS

Max Transient Temperature(20 Seconds)

A

825 ITT

47
Q

ITT LIMITS/BRAKE LIMITS

Max Contiuous/ REC

A

785 ITT

48
Q

ITT LIMITS/BRAKE LIMITS

Brake Energy Exceeded Limit

A

20 Minute / Visual inspection

49
Q

ITT LIMITS/BRAKE LIMITS

GEAR / BRAKE AIR PRESSURE

A

1800-3000 PSI

50
Q

HYDRAULIC and ELECTRICAL SYSTEM LIMITS

Pressure Relief Valve Opens

A

1750 PSI

51
Q

HYDRAULIC and ELECTRICAL SYSTEM LIMITS

Accumulator Pre Charge

A

750 - 850 PSI

52
Q

HYDRAULIC and ELECTRICAL SYSTEM LIMITS

Hydraulic Fluid for Aux. Pump

A

.4 GAL

53
Q

HYDRAULIC and ELECTRICAL SYSTEM LIMITS

Emergency Air Pressure

A

1800 - 3000 PSI

54
Q

HYDRAULIC and ELECTRICAL SYSTEM LIMITS

Auxiliary Hyd Pump

A

3 min. on / 20 min. off

55
Q

HYDRAULIC and ELECTRICAL SYSTEM LIMITS

BATTERIES

A

24 VDC

56
Q

HYDRAULIC and ELECTRICAL SYSTEM LIMITS

ENGINE GENERATORS

A

28 VDC

57
Q

HYDRAULIC and ELECTRICAL SYSTEM LIMITS

GENERATOR GROUND LIMIT

A

325 AMPS

58
Q

HYDRAULIC and ELECTRICAL SYSTEM LIMITS

GENERATOR AIRBORNE LIMIT

A

400 AMPS

59
Q

HYDRAULIC and ELECTRICAL SYSTEM LIMITS

EMERGENCY BATT 1
EMERGENCY BATT 2

A
  1. 1 HRS

99. 2 HRS

60
Q

PRESSURIZATION LIMITS

Press switches from auto to Man (Press SYS and Fault Lights).

If in Manual Mode

A

8,600’ +/-250’

8,750’ +/-250’

61
Q

PRESSURIZATION LIMITS

Emergency Pres SYS Activates
Auto Shed and Emer Pres Lights

A

9,500 +/- 250’

62
Q

PRESSURIZATION LIMITS

Cabin Alt Hi Light/Horn (mute)

A

10,100’ +/- 250’

63
Q

PRESSURIZATION LIMITS

Cab Alt Lim Limits Cabin to

A

13,700’ +/- 500’

64
Q

PRESSURIZATION LIMITS

O2 Masks Drop/Emer Lights On

A

14,500’ +/- 750’

65
Q

PRESSURIZATION LIMITS

Max Differential Pressure

A

9.8 PSI

66
Q

PRESSURIZATION LIMITS

Max Operation Manual Mode

A

8,000 Feet

67
Q

PRESSURIZATION LIMITS

Freon Cooling System T/O and Land

A

OFF or Cabin Manual Mode Full COLD

68
Q

STARTER DUTY CYCLE
Failure After 1st Attempt

Failure After 2nd Attempt

Failure After 3rd Attempt

A

3 Minutes

15 Minutes

30 Minutes

69
Q

STARTER DUTY CYCLE

GPU MIN/MAX AMPS

A

500 AMPS - 1500 AMPS

70
Q

STARTER DUTY CYCLE

GPU CONNECTED TO AIRCRAFT

A

1 BATTERY ON

71
Q

STARTER DUTY CYCLE

GPU REQ Ambient Temp

A

0 c and Below

72
Q

FIRE PROTECTION/OXYGEN

Fire-Extinguisher Agent

A

Halon

73
Q

FIRE PROTECTION/OXYGEN

Fire Bottle Gauge Pressure

A

600 psi @ 70 f

74
Q

FIRE PROTECTION/OXYGEN

OKYGEN PRESSURE

A

1550 to 1850 psi

75
Q

FIRE PROTECTION/OXYGEN

Crew masks not approved above cabin altitude

A

40,000 Feet

76
Q

FIRE PROTECTION/OXYGEN

Passenger masks not sufficient above cabin altitude

A

34,000 Feet

77
Q

FIRE PROTECTION/OXYGEN

Prolonged passenger usage not recommended above cabin altitude

A

25,000 Feet

78
Q

OPERATIONAL LIMITS

MAX Altitude

A

51,000 Feet

79
Q

OPERATIONAL LIMITS

Temperature

A

+50 c / -54 c

80
Q

OPERATIONAL LIMITS

MAX Takeoff Altitude (PA)

A

13,700 Feet

81
Q

OPERATIONAL LIMITS

MAX Depth of Water or Slush on Runway

A

3/4 inch

82
Q

OPERATIONAL LIMITS

Do Not Takeoff or Land with the:

A

Cabin Pressurized

83
Q

ANTI ICE

Takeoff: Anti Ice On prior to flight into visible moisture and SAT

A

10 c or Below NAC HEAT - ON

84
Q

ANTI ICE

In Flight: Anti Ice On prior to flight into visible moisture and RAT

A

10 c or Below NAC HEAT - ON

85
Q

ALCOHOL LIMITS

Type of Alcohol

A

Methanol O-M-232

86
Q

ALCOHOL LIMITS

Reservoir Capacity

A

2.35 Gallons

87
Q

ALCOHOL LIMITS

System Duration Windshield Only

A

45 Minutes

88
Q

ANTI ICE LIMITATIONS

NACELLE HEAT ENGINES (OFF) MAX

A

5 Seconds Max

89
Q

ANTI ICE LIMITATIONS

NACELLE HEAT SAT +15C (OAT) MAX

A

30 Seconds Max

90
Q

ANTI ICE LIMITATIONS

IN-FLIGHT NACELLE HEAT REQUIRED

A

10c/ -40c 2 Minutes Prior to Entering Icing

91
Q

ANTI ICE LIMITATIONS

Wing Stab Heat (AMPS/LGT/ITT)

A

5 Seconds Max before Self shutoff/ If test failed 3 Minute wait before retest.

92
Q

ANTI ICE LIMITATIONS

Windshield Heat Light GND/AIR

WSHLD
OV HT

A

250C/ 345C

93
Q

ANTI ICE LIMITATIONS

MAX N1 Nacelle Heat Usage

A

65% N1

94
Q

ANTI ICE LIMITATIONS

Static Discharge Wicks

A

19 Installed / 14 Required

95
Q

THRUST REVERSER LIMITATIONS

MAX CONTINUOUS OPERATION

A

5 Minutes

96
Q

THRUST REVERSER LIMITATIONS

NOSE GEAR

A

Ground Contact

97
Q

THRUST REVERSER LIMITATIONS

HYDRAULICALLY ACTIVATED

A

ELECTRONICALLY CONTROLLED

98
Q

THRUST REVERSER LIMITATIONS

LIMITED TO IDLE

A

Below 50 KIAS

99
Q

THRUST REVERSER LIMITATIONS

T/R USE TO BACK UP AIRCRAFT

A

PROHIBITED

100
Q

THRUST REVERSER LIMITATIONS

PAVED SURFACE

A

Required

101
Q

MISCELLANEOUS LIMITATIONS

Center of Gravity

A

-4% to 25% MAC

102
Q

MISCELLANEOUS LIMITATIONS

NO INTENTIONAL STALLS

A

Above 18,000 Feet

103
Q

MISCELLANEOUS LIMITATIONS

Operational Trim Checks

A

First Flight

104
Q

MISCELLANEOUS LIMITATIONS

YAW DAMPER USED DURING T/O AND LANDING

A

DO NOT USE

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