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Learjet 60 CAE > Limitations > Flashcards

Limitations Flashcards

1
Q

AIRSPEED - Mmo 26,750 to 37,000 feet

A

0.81 M

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2
Q

AIRSPEED - Mmo 37,000 to 43,000 feet

A

0.81 to 0.78 M

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3
Q

AIRSPEED - Mmo 43,000 feet and above

A

0.78 M

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4
Q

AIRSPEED - Mmo Mach Trim inoperative & A/P disengaged

A

0.77 M

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5
Q

AIRSPEED - Vmo up to 8,000 feet

A

300 KIAS

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6
Q

AIRSPEED - Vmo 8,000 to 20,000 feet

A

340 KIAS

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7
Q

AIRSPEED - Vmo 20,000 to 23,000 feet

A

340 to 330 KIAS

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8
Q

AIRSPEED - Vmo 23,000 to 26,750

A

330 KIAS

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9
Q

Vle

A

260 KIAS

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10
Q

Vlo

A

200 KIAS

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11
Q

Vfe (Flaps 8)

A

250 KIAS

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12
Q

Vfe (Flaps 20)

A

200 KIAS

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13
Q

Vfe (Flaps 40)

A

165 KIAS

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14
Q

Vmca (Flaps 8)

A

120 KIAS

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15
Q

Vmca (Flaps 20)

A

110 KIAS

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16
Q

Vmcg (Rudder Boost ON)

A

95 KIAS

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17
Q

Vmcg (Rudder Boost OFF)

A

116 KIAS

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18
Q

Turbulent Air Penetration

A

250 KIAS / 0.73 M

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19
Q

Max Demonstrated Crosswind

A

29 knots

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20
Q

Tailwind Component for T/O & Landing

A

10 knots

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21
Q

Main Tire Limiting Speed (Ground Speed)

A

182 knots

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22
Q

Maximum Pressure Altitude

A

51,000 feet

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23
Q

Runway Water / Slush on Runway

A

3/4 inch (19 mm)

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24
Q

Spoilers Inoperative

A

38,000 feet

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25
Q

Maximum Pressure Altitude T/O & Landing (Temperature)

A

13,700 feet (+50 / -54)

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26
Q

Fuel Load Balance: Takeoff and Landing

A

Balanced within 200 pounds

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27
Q

Fuel Load Balance: En-route

A

Balanced within 500 pounds

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28
Q

Limit Maneuvering Load Factors: Flaps Up

A

+3.0g to -1.0g

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29
Q

Limit Maneuvering Load Factors: Flaps Down

A

+2.0g to 0.0g

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30
Q

Maximum Ramp Weight

A

23,750 pounds

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31
Q

Maximum Certified Takeoff Weight

A

23,500 pounds

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32
Q

Maximum Certified Landing Weight

A

19,500 pounds

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33
Q

Maximu Zero Fuel Weight

A

17,000 pounds

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34
Q

Maximum Takeoff Weight with anti-skid OFF or inoperative

A

18,500 pounds

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35
Q

Aviation Gasoline

A

The use of aviation gasoline is prohibited

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36
Q

Unusable Fuel in Fuselage Tank with Gravity Transfer

A

350 pounds (approx)

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37
Q

“LOW FUEL” Annunciator

A

410 pounds in either wing

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38
Q

Fuel Anti-Icing Additive

A

Anti-icing additive is not a requirement

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39
Q

“L & R FUEL PRESS” annunciators illuminate

A

2.75 psi or less

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40
Q

Fuel Capacity (SPPR)

A

7,800 pounds

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41
Q

Fuel Capacity (over wing refueling)

A

7,910 pounds

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42
Q

What activates the fuel scavenge pumps?

A

Pressing the Lights Test Switch or either wing fuel < 410 pounds

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43
Q

What turns on the standby fuel pumps?

A

START Cycle, Manually Selected or FILL

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44
Q

Maximum Thrust

A

4,600 pounds @ sea level

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45
Q

Maximum Continuous ITT

A

785 degrees

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46
Q

Max Transient ITT (20 SEC)

A

825 degrees

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47
Q

Maximum ITT on Start

A

950 degrees

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48
Q

FADEC will terminate start at _____________?

A

1000 degrees ITT or < 200 degrees ITT after 15 seconds

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49
Q

Maximum time APR or Thrust Levers in T/O position

A

5 mins

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50
Q

Engine idle speed (ground)

A

52% N2 (PMA powers FADEC @ 52%)

51
Q

Engine idle speed (in-flight)

A

65% N2

52
Q

Engine Computers / Annunciators

A

Engine Computers must be in AUTO MODE and annunciators must be extinguished

53
Q

Starter Limits

A

After Start attempt: Wait:
1 3 mins
2 15 mins
3 30 mins

54
Q

Hydraulic AUX PUMP Usage (0.5 GAL per minute)

1000 - 1125 psi

A

3 minutes ON, 20 minutes OFF

55
Q

Normal Hydraulic Pressure

A

1500 psi

56
Q

Hydraulic Pressure Relief Valve

A

Opens at 1750 psi

57
Q

GEAR AIR & BRAKE AIR Pressure

A

1800 - 3000 psi (Nitrogen or Dry Air)

58
Q

Hydraulic Accumulators

A

2 Accumulators
1 for Thrust Reversers
1 for rest of the hydraulic system
750 psi (MINIMUM), 850 psi (PRECHARGE)

59
Q

Hydraulic Fluid Type

A

MIL-5606

60
Q

“L & R HYDR PRESS” Annunciators illuminate at what psi?

A

150 psi from respective engine driven pump (2)

61
Q

Secondary Flight Controls are _________?

A

Electrically controlled & hydraulically actuated (FLAPS, SPOILERONS, and AUTOSPOILERS)

62
Q

Oil Capacity Per Engine

A

1.95 gallons

63
Q

Check Oil Level

A

10 minutes after shutdown

64
Q

Type of Oil

A

Type II oils conforming to Pratt and Whitney Canada PWA521

65
Q

“L & R OIL PRESS” Annunciator illuminates at ________?

A

Less than 20 psi

66
Q

What drives the accessory gear box?

A

Tower Shaft

67
Q

Minimum Fuel required for APU / from which fuel tank

A

100 pounds / Left fuel tank

68
Q

When does the APU shut down in the event of a fire?

A

At first indication of a fire

69
Q

How would you detect an APU fire during a walk-around?

A

By a horn from the left main wheel well

70
Q

How can an APU fire be extinguished?

A

Automatically from 10-17 seconds of fire indication or manually pressing FIRE button on APU control panel

71
Q

Primary Power is from what?

A

Two engine -driven START/GENERATORS RATED TO 30 VCD, 400 AMPS

72
Q

Secondary Power

A

Two 24-volt lead acid, NICAD or Concorde (MAINT FREE) batteries

73
Q

AC Power (What Converts 28VDC to 115 AC)

A

Two 115-volt, solid-state inverters

74
Q

GPU Limitations

A

500-1500 amps, regulated to 28 VDC, over-voltage protection at 32 VDC

75
Q

Generator Limits

A

325 amps ground operations, 400 amps flight operations

76
Q

Emergency Battery Duration

A

EMER BAT 1 = 3.1 hours

EMER BAT 2 = 99.2 hours

77
Q

What types of circuit breakers are installed?

A

Thermal and magnetic.

All A/C circuit breakers are magnetic.

78
Q

How are emergency bus items identified on the circuit breaker panel?

A

Red ring around the circuit breaker

79
Q

How are AC items identified on the circuit breaker panel?

A

White ring around the circuit breaker

80
Q

Maximum Cabin Altitude

Unless Landing 8000 feet PA or Higher

A

8,000 feet +/- 250 feet

81
Q

Maximum Cabin Altitude

Cabin Outflow Valves Close

A

13,700 feet +/- 500 feet

82
Q

Maximum Differential Pressure

A

9.8 psig

83
Q

When does the “PRESS SYS” annunciator illuminate?

A

AUTOMATIC MODE - 8,600 feet +/- 250 feet

MANUAL MODE - 8,750 feet +/- 250 feet

84
Q

When does the “EMER PRESS” annunciator illuminate?

A

9,500 feet +/- 250 feet

85
Q

When does the cabin altitude warning horn and (if installed) CABIN HI annunciator activate?

A

10,100 feet +/- 250 feet

86
Q

Passenger Oxygen Masks automatically deploy when?

A

14,500 feet +/- 250 feet cabin altitude

87
Q

What mode must be used for takeoff and landing above 8,000 feet PA?

A

AUTO (All cautions and warnings reset to 14,500 feet except cabin altitude limiters)

88
Q

What fire extinguishing agent is used?

A

HALON 1301

89
Q

Fire Bottle Pressure Gauge

A

600 psi

90
Q

How do you check the smoke detector (CABIN FIRE)?

A

Press either the Pilot’s or Copilot’s Lights Test Switch

91
Q

Normal Oxygen Pressure Gauge

A

1550-1850 psig

92
Q

Crew and Passenger Oxygen masks are not approved above ___________?

A

Above 40,000 feet cabin altitude

93
Q

Passenger Masks will not provide sufficient oxygen above _________?

A

Above 34,000 feet cabin altitude

94
Q

Prolonged operation with passengers on board is not recommended above _____________?

A

25,000 feet cabin altitude

95
Q

A missing Green Discharge Disc mean _____________?

A

An over pressurization of 2700-3000 psi in the oxygen bottle

96
Q

What are the crew oxygen mask settings?

A

Scott ATO crew masks:
Normal, 100% and Emergency

Puritan Bennett Sweep-On 2000 crew masks:
EMER, 100% and NORM

97
Q

When will the crew oxygen masks deliver 100% oxygen regardless of altitude?

A

Above 35,000 feet cabin altitude

98
Q

Anti-Ice ON in what conditions?

A

10 degrees or below, visibility 1 mile or less with visible moisture of any kind (such as rain, snow, sleet, ice crystals, clouds or fog)

99
Q

Type of alcohol used?

A

Methanol O-M-232

100
Q

Alcohol Reservoir Capacity / Duration?

A

2.35 gallons / 45 minutes

101
Q

Do not operate NAC HT With Associated Engine OFF

A

More than 5 seconds

102
Q

Do not operate NAC HT above 15 degrees

A

More than 30 seconds

103
Q

Do not apply NAC HT with thrust above

A

65% N1 except for takeoff

104
Q

Failed STAB HT On the Ground (Ground Test)

A

Flashing “STAB HT” annunciator

105
Q

Failed STAB HT in-flight

A

Steady “STAB HT” annunciator

106
Q

What System is Lost During Emergency Pressurization?

A

Wing and windshield anti-ice

107
Q

What Anti-Ice Systems are lost during EMER BATT conditions?

A

All anti-ice systems are lost except nacele heat

108
Q

What items are heated with the pitot heat switches?

A

Left switch heats the pilot’s pitot tube and stall vane.
Right switch heats the stand-by pitot tube, copilot’s pitot tube, stall vane, pressurization static port, TAT probe, galley drain and lavatory sink drain.

109
Q

Use of thrust reverse to back up the aircraft is ____________?

A

Prohibited

110
Q

How are the thrust reversers deployed?

A

Electrically controlled and hydraulically actuated?

111
Q

Thrust reverse is limited to idle ______________________

A

Below 50 KIAS

112
Q

Thrust reverse approved for what runways?

A

Paved surfaces only

113
Q

How are thrust reversers stowed during an inadvertent T/R deployment?

A

Automatically via the FADEC

114
Q

The autopilot / flight director system is approved for what ILS approaches?

A

Category I ILS approaches

115
Q

Operation of the autopilot with the red TRIM FAIL light illuminated is __________?

A

PROHIBITED

116
Q

Autopilot pitch and roll axis must not be used for _______________?

A

Takeoff and Landing

117
Q

The minimum altitude for use of the autopilot is ____________?

A

Approach Configuration - 200 feet AGL
En route Configuration - 1000 feet AGL
Minimum Engage Height - 1000 feet AGL

118
Q

How many static wicks are installed and how many wicks are required?

A

19 total and 14 required for flight (Check MEL)

119
Q

No Intentional Stalls

A

Above 18,000 feet

120
Q

Yaw Damper for Takeoff or Landings

A

OFF for takeoff

Optional for landings

121
Q

Check of Trim Systems

A

Required daily before first flight

122
Q

If you exceed brake energy limits?

A

Aircraft must be parked for 20 minutes minimum and a visual inspection of main gear tires, wheel and brakes for condition must be made before next takeoff attempt

123
Q

What prerequisites are needed to follow the Through-Flight Checklist?

A

There has been no change in flight crew personnel.
No maintenance has been performed on the aircraft. Routine line servicing is not considered maintenance.
No more than three (3) hours have elapsed between engine shutdown and engine start.
Extreme weather conditions (heavy precipitation, ice, snow, extreme cold, etc. have not occurred which would change the preflight status of the aircraft.

Learjet 60 CAE (21 decks)

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