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Global 5000/5500/6000 > Bombardier 5000/6000 Limitations > Flashcards

Bombardier 5000/6000 Limitations Flashcards

1
Q

Max taxi/ramp weight
(6000)

A

99,750 lb

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2
Q

Max takeoff weight

A

99,500

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3
Q

Max Landing weight

A

78,600 lb

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4
Q

Max zero fuel weight

A

26,308 lb

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5
Q

Min flight weight

A

21,863 lb

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6
Q

Min operating empty weight

A

20,412 lb

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7
Q

Buoyancy limitation, when taking off or landing on runways near bodies of water

A

OUTFLOW VLV 2 closed
and
One pac off

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8
Q

Max airport pressure altitude for takeoff and landing

A

10,000’

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9
Q

Max operating altitude

A

51,000’

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10
Q

Max ambient air temp for takeoff and landing

A

+50°C

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11
Q

Min ambient air temp for takeoff and landing

A

-40°C

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12
Q

Cowl anti-ice during takeoff limit

A

Must not be in AUTO.
OFF or ON only

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13
Q

Limit for cowl anti-ice on during flight

A

TAT is 10°C or less in visible moisture (snow, rain, fog, visibility <1 mile)

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14
Q

Limit for cowl anti-ice while on the ground

A

SAT is 10°C or less with contaminated surfaces (snow, ice, standing water or slush)

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15
Q

Define inflight icing conditions

A

TAT 10°C or less with visible moisture, except when SAT is -40°C or below

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16
Q

Minimum engine speed, while in icing conditions

A

76% N2

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17
Q

Maximum runway slope for takeoff and landing

A

+2% uphill
-2% downhill

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18
Q

Maximum tail wind component approved for takeoff and landing

A

10 kts

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19
Q

Minimum flight crew

A

One pilot and one copilot

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20
Q

Maximum number of passengers

A

19

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21
Q

Maximum number of occupants for operation

A

22

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22
Q

Prohibited runway conditions for operations

A

Unprepared surfaces
(i.e. gravel, grass, etc.)

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23
Q

Limitation for operating display units with flight compartment temperatures in excess of 40°

A

Operations greater than 30 minutes are prohibited

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24
Q

Maximum limit for runway threshold, glidepath, angles

A

Approach angles greater than 5.5° are prohibited.

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25
Q

Maximum ITT for start on the ground

A

700°C

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26
Q

Maximum engine ITT for start in flight

A

850°C

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27
Q

Minimum N2 speed during idle

A

58%

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28
Q

Max N2 speed for takeoff

A

99.6%

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29
Q

Max fan speed for takeoff

A

102.0%

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30
Q

Max ITT for takeoff

A

900°C (5 min AIO)

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31
Q

Max continuous N2

A

98.9%

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32
Q

Max continuous fan speed

A

102.0%

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33
Q

Max continuous ITT

A

860°C

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34
Q

Max transient N2 speed

A

99.8% (20 seconds)

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35
Q

Max transient fan speed

A

102.0% (20 seconds)

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36
Q

Max transient ITT

A

905°C (20 seconds)

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37
Q

Time limit for takeoff thrust all engines operating

A

5 min

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38
Q

Time limit for takeoff, thrust, one engine inoperative

A

10 min

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39
Q

Maximum tailwind for engine starts

A

20 kts

40
Q

Maximum crosswind for engine starts

A

35 kts

41
Q

Minimum crank time for engine start with N1 rotation due to tailwind

A

30 seconds with an immediate AUTO start.

42
Q

Thrust limit for taxing when winds exceed 20 kts

A

Minimum only

43
Q

Limitation for Crosswinds during takeoff that exceed 20 kts

A

Do not exceed 66% N1 below 30 KIAS, then TO thrust.

44
Q

Maximum crosswind component during start

A

35 kts

45
Q

Max N2 RPM for engine starter engagement

A

42%

46
Q

Engine start limits

A

3 min ON, 15 sec OFF,
3 min ON, 15 sec OFF,
3 min ON, 15 min OFF

47
Q

Maximum wing fuel imbalance during flight

A

1100 lb

48
Q

Maximum wing fuel imbalance during takeoff and landing

A

600 lb

(1100-600 lb depending on remaining fuel)

49
Q

Usable fuel in each main wing tank

A

15,050 lb

50
Q

Usable fuel in auxiliary tank

A

12,700 lb

51
Q

Usable fuel in aft tank

A

2,300 lb

52
Q

Minimum flight planned cruise altitude for center tank fuel to be usable

A

30,000’

53
Q

Limit to consider aft tank fuel usable

A

5500 lb wing fuel,
planned cruise > FL300
500 lb min in Aft tank

54
Q

Minimum fuel for a go-around

A

600 lb
Wings level, max 10° nose up.

55
Q

Minimum engine fuel temperature for takeoff

A

5°C

56
Q

Minimum oil temperature for starting

A

-40°C

57
Q

Minimum oil temperature before accelerating above idol

A

20°C

58
Q

Maximum permissible oil temperature

A

160°C

59
Q

Maximum oil consumption rate per engine

A

.21 US quarts per hour

60
Q

Auxiliary power unit type

A

RE 220

61
Q

Maximum APU rpm

A

106%

62
Q

Maximum operating altitude of the APU

A

45,000’

63
Q

Maximum number of APU starts

A

3 per hour

64
Q

Maximum altitude for starting the APU

A

37,000’

65
Q

Maximum altitude for APU bleed air extraction

A

30,000’

66
Q

Maximum OAT for APU bleeder extraction for air conditioning

A

45°C

67
Q

Maximum slats extended speed

A

225 kts

68
Q

Maximum speed for flaps 16°

A

210 kts

69
Q

Maximum speed for flaps 6°

A

210 kts

70
Q

Maximum speed for flaps 30°

A

185 kts

71
Q

Landing gear operating speed

A

200 kts

72
Q

Landing gear extended speed

A

250 kts/0.7M

73
Q

Maximum altitude for landing gear extended

A

20,000’

74
Q

Tire limit speed

A

183 kts

75
Q

Max turbulence penetration speed

A

300 kts/0.80M

76
Q

Maneuvering limit load factors - slats/flaps retracted

A

-1.0 G to +2.05 G

77
Q

Maneuvering limit load factors - slats/flaps extended

A

0.0 G to +2.0 G

78
Q

Cooling pack discharge temperature range during manual mode operations

A

5°C to 60°C

79
Q

Pack limit during manual mode operations

A

One pack must be selected off

80
Q

Maximum relieve differential pressure on cabin

A

10.73 psi

81
Q

Maximum negative relief differential pressure on cabin

A

-.5 psi

82
Q

Maximum cabin differential pressure during taxi and takeoff

A

0.1 psi

83
Q

Maximum cabin differential pressure during touchdown limit

A

1.0 psi

84
Q

Altitude limit for use of AUX PRESS

A

41,000’

85
Q

Max altitude for EMER DEPRESS

A

15,000’

86
Q

Maximum altitude with a yard damper disengaged 

A

41,000’

87
Q

Minimum speed to set autothrottles on takeoff

A

60 KIAS

88
Q

Minimum altitude for auto pilot engagement after takeoff

A

400’ AGL

89
Q

Minimum altitude for the autopilot during a Cat I ILS or LPV

A

80’ AGL

90
Q

Minimum altitude for auto pilot during a non-precision approach

A

400’ AGL

91
Q

Minimum altitude for auto pilot during a non-precision approach with vertical path reference

A

160’ AGL

92
Q

APU generator load limit

A

40 kVA

93
Q

Maximum altitude for slats/flaps extended

A

18,000’

94
Q

Minimum altitude for flight spoilers

A

300’ AGL

95
Q

Limitations on the use of MAX spoilers

A

Prohibited, except during emergency conditions, or as required by AFM procedures

Global 5000/5500/6000 (4 decks)

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