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Lear 35 (Flight Safety) > Limitations > Flashcards

Limitations Flashcards

1
Q 
Aeronca thrust reverser:
Circuit breakers in flight?
Touch and go landings?
Full reverse limited to?
Flashing UNLOCK light after stow?
A

Do not pull CBs in flight
No reversers during touch n go’s
Full reverse limited to 60 kts
Flashing UNLOCK after stow = shut down engine

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2
Q

Fuselage fuel transfer

A

Prior to 2,250lbs in wings or limit speed to 325 KIAS

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3
Q

Max landing weight

A

15,300lbs

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4
Q

Va @ 18,300lbs (varies with altitude)

A

206 - 242 kts

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5
Q

Max start attempts

A

6

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6
Q

N1 ultimate overspeed (computer protection)

A

109%

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7
Q

Cabin altitude limiters activate

A

11,500ft +/- 1,500

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8
Q

LOW FUEL light illuminated

A

400-500lbs

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9
Q

Brew masks not approved above cabin altitude of…

A

40,000ft

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10
Q

Fuel remaining in fuselage tank after gravity transfer

A

162lbs

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11
Q

Required climb gradient formula

A

Required climb FT per NM/6,076

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12
Q

Mmo (any BLE missing)

A

M . 77

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13
Q

Max fuel in tip tanks for landing

A

925lbs

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14
Q

GPU amp limits

A

500-1,100 amp

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15
Q

Generator ground limits

A

320amp

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16
Q

Nose wheel steering authority up to 10 kts

A

45degrees

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17
Q

Max fuel in tip tanks prior to fuselage fuel transfer

A

760lbs

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18
Q

Emergency battery duration “STBY”

A

3hr 45min

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19
Q

Max temp for engine start

A

860 C

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20
Q

Generator airborne limits

A

400 amp

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21
Q

Do not operate NAC HEAT for more than…

A

10 sec when OAT > 50 deg F

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22
Q

Conforming oil - type 2

A

Mobil 254

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23
Q

VLo

A

200 KIAS

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24
Q

N2 overspeed (mechanical protection)

A

105%

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25
Q

Max cabin differential

A

10 psi

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26
Q

Alcohol endurance windscreen and radome

A

45min

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27
Q

Max continuous ITT

A

832 C

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28
Q

GPU over-voltage cut-out circuit

A

33volts

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29
Q

Oil reservoir capacity

A

6 qts

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30
Q

Vmca

A

110 KIAS

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31
Q

AVGAS used as EMERGENCY FUEL limits…

A

STBY (BOOST) and JET pumps = “ON”
Max Altitude = 15,000ft
Max 500 gallons per 100 hrs engine operation

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32
Q

Vmcg

A

103 KIAS

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33
Q

Nose wheel steering must be disconnected

A

45 knots

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34
Q

Aux hydraulic pump output

A

0.5 gal/min

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35
Q

VLe

A

260 KIAS

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36
Q

Hydraulic reservoir capacity (including reserve)

A

1.9gal

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37
Q

LOW HYD light turns off

A

1,250 psi or greater

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38
Q

Aux hydraulic pump operation times

A

3 min continuous, 20 min off

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39
Q

Secondary cabin differential relief valve limit

A

9.7 psi

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40
Q

Airborne starter-assist attempts

A

Max 3

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41
Q

Vfe 9-20 degrees

A

185 KIAS (FCN 85-6 = 200 KIAS)

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42
Q 
Dee Howard thrust reverser limits:
When must it be disarmed?
Max crosswind
Full reverse limit
Max N1 when deployed
A

Disarmed immediately after takeoff
20kt demonstrated crosswind
Full reverse limited to above 50kts
Max N1 75% when deployed

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43
Q

Flaps down load factor limit

A

0G to 2G

44
Q

Engine SYNC must be off for…

A

T/O, landing, & single engine ops

45
Q

Emergency bleed air valves activate

A

9,500ft +/- 250

46
Q

Vmo 8,000 and above

A

350 KIAS

47
Q

Passenger masks prolonged use

A

25,000ft or lower

48
Q

Fuel capacity (one recognition light)

A

6,238lbs

49
Q

Oxygen pressure relief valve opens

A

2,700 - 3,000psi

50
Q

N2 ultimate over speed (computer protection)

A

110%

51
Q

Vfe 1-8 degrees

A

200 KIAS

52
Q

Oxygen masks Auto-drop (cabin overhead lights on)

A

14,000ft +/- 750

53
Q

Mmo (mach trim or A/P inop)

A

M . 74

54
Q

Max tire speed

A

182 KIAS

55
Q

Turbulent air penetration

A

M . 73/ 250 KIAS

56
Q

Max Hydraulic pressure

A

1750psi

Ultimate pressure relief at 1700psi

57
Q

What action MAY momentarily disable Anti-skid?

A

Selecting A/C “ON”

58
Q

Nose tire inflation

A

104-114 psi loaded

105 +/-5 unloaded

59
Q

Mmo

A

M . 81

60
Q

Hydraulic fluid reserve (available to aux pump only)

A

0.4gal

61
Q

CAB ALT light (control box reverts to manual)

A

8,750ft +/- 250

62
Q

Max aircraft operating altitude

A

45,000ft

63
Q

Min battery voltage to close battery or GPU relays

A

16 VDC

64
Q

Min and Max oil pressure

A

Min 25psi

Max 55 psi

65
Q

Max T/O weight

A

18,300lbs

66
Q

If any 2 of the 3 Anti-skid lights are illuminated…

A

Nose wheel steering must be disconnected or speed less than 10kts

67
Q

Max oil temp

A

140c

68
Q

Max fuel out of balance with autopilot engaged (FC530)

A

200lbs

69
Q

Cabin altitude horn activates

A

10,100ft +/- 250

70
Q

LOW HYD light illuminated (aux pump off)

A

1,125psi or less

71
Q

Anti-ice on prior to flight in visible moisture…

A 
Takeoff= SAT  < 4.4 degrees C 
In-flight = RAT 10 to -40 degrees C
72
Q

Max tip & wing zero fuel weight

A

13,500lbs

May increase 14,000lbs if 500lbs fuel added to fuselage

73
Q

N1/N2 overspeed (1min)

A

100-103%

74
Q

N1/N2 overspeed (5sec)

A

103-105%

75
Q

Max takeoff and landing altitude

A

10,000ft

76
Q

Conditions to start A/C

A

Ammeters read below 250amps w/both engines running

One ammeter reads below 150amps if one engine running

77
Q

Max water on runway

A

.25” T/O

.75” LDG

78
Q

Emergency battery duration “ON”

A

30min

79
Q

Hydraulic accumulator pre-charge

A

750-850psi

80
Q

Max temp for takeoff (5min)

A

860 C

81
Q

Minimum fuel temp

A

-54c

82
Q

Vmo up to 8,000

A

300 KIAS

83
Q

Brake energy limits

A

ABORTED TAKEOFF checklist

84
Q

Main tires inflation

A

161-171 psi loaded

160psi +/-5 unloaded

85
Q

Engine?

A

TFE-731-2-2B

86
Q

Vfe 21-40 degrees

A

150 KIAS

87
Q

Hydraulic fluid color and type

A

(Red) Mil-H-5606

88
Q

Nose wheel steering authority at 45 knots

A

8 degrees

89
Q

Max ramp weight

A

18,500lbs

90
Q

Flaps up load factor limit

A

-1G to 3G

91
Q

Primary cabin differential relief valve limit

A

9.4 psi

92
Q

Check oil level within…

A

1 hour after shutdown

15 minutes is recommended

93
Q

Prist/Quell 20oz can treats…

A

105-260gals

94
Q

Do we take off or land while the cabin is pressurized?

A

No

95
Q

Drag chute max deploy speed

A

150 KIAS

20 KIAS crosswind

96
Q

Normal oil pressure

A

38-46psi

97
Q

Recommended continuous ITT

A

795 C

98
Q

Wait time between start attempts in minutes

A

1 ,1 ,15 ,1 ,1 ,60

99
Q

Alcohol endurance radome only

A

2hr 9min

100
Q

Min fuel each wing for takeoff or intentional go-around

A

600lbs per wing

101
Q

Tip tanks out of balance for landing (demonstrated)

A

600lbs

102
Q

Max tailwind

A

10 KIAS

103
Q

Demonstrated crosswind

A

24.7 KIAS

104
Q

Fuel remaining in tip tanks when jet pump inop

A

600lbs

105
Q

Max Wing fuel imbalance during ground refueling

A

125gal

106
Q

Max aft baggage weight

A

500lbs

Lear 35 (Flight Safety) (5 decks)

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