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G550 > Limits > Flashcards

Limits Flashcards

1
Q

Max engine ground start TGT?

Time limit?

A

700

Momentary

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2
Q

Max engine air start relighting TGT?

Time limit?

A

850

Momentary

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3
Q

Max engine takeoff LP

HP

TGT

Time limit

A

101.1

99.6

900

5 mins. Two engine, 10 mins. Single engine

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4
Q

Max continuous LP

HP

TGT

Time limit

A

101

98.9

860

Unrestricted

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5
Q

Max engine over speed LP

HP

TGT

TIME LIMIT

A

101.5

99.8

905

20 seconds

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6
Q

Max reverse thrust LP

TIME LIMIT

A

70

30 seconds

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7
Q

Max Zero fuel weight

A

54,500

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8
Q

Max ramp weight

A

91,400

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9
Q

Max takeoff weight

A

91,000

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10
Q

Max landing weight

A

75,300

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11
Q

Fuel imbalance for takeoff

A

1,000 lbs

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12
Q

Fuel imbalance in-flight

A

2,000 lbs

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13
Q

Max fuel

A

41,300 lbs

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14
Q

Aircraft length

A

96’ 5”

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15
Q

Aircraft wingspan

A

93’ 6”

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16
Q

Aircraft height

A

25’ 11”

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17
Q

Aircraft nosewheel to MLG

A

45’

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18
Q

MLG width

A

14’ 4”

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19
Q

Elevator width

A

35’ 2”

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20
Q

When HMG is in operation, speed brakes may be used provided operation is ?

A

Slow operation, approx 3 seconds for full range movement

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21
Q

Do not operate HMG when normal AC power is available, except?

A

For L or R ESS DC bus failure

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22
Q

Max cabin diff for taxi/takeoff/landing

A

0.3 PSID

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23
Q

Max cabin pressure diff

A

10.48 PSID

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24
Q

When aircraft is static on the ground, stabilized engine operation in the keep out zone of what LP RPM, is prohibited.
Any accel-decel through this band must not exceed 10 seconds.

A

66 to 80% RPM

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25
Q

Max ZFW

A

54,500 lbs

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26
Q

Max ramp weight

A

91,400 lbs

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27
Q

Max takeoff

A

91,000 lbs

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28
Q

Max landing

A

75,300

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29
Q

Max fuel imbalance for takeoff

A

1,000 lbs

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30
Q

Max fuel imbalance in-flight

A

2,000 lbs

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31
Q

Max fuel load

A

41,300 lbs

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32
Q

Max TGT prio to ground start

A

150 deg. C

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33
Q

When the HMG is in operation, speed brakes may be used provided operation is ? (Approx. ? seconds for full range movement

A

Slow, 3 seconds

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34
Q

Max cabin pressure diff

A

10.48 PSID

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35
Q

Max cabin press diff taxi/takeoff/land

A

0.3 PSID

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36
Q

Keep out zone

A

66-80% while static, on the ground. Any accel/decel must not exceed 10 seconds.

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37
Q

Takeoff in ? Control mode is prohibited

A

Alt

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38
Q

X-wind above 20 knots, accel to takeoff power, fan speed limited to <?% until a fwd speed of ? Knots

A

66%

20 knots

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39
Q

Add ? Feet to required field length for slam takeoff

A

600’

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40
Q

X-wind >20 kts, forward speed >20 kts, a ? Acceleration is required.

A

Slam

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41
Q

Max x-wind for takeoff & land

A

28 knots

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42
Q

Once takeoff had commenced, use of tiller >? Knots, is not recommended

A

60 knots

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43
Q

Max x-wind for engine start

A

30 knots

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44
Q

Max tailwind for engine start

A

20 knots

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45
Q

Weather radar, ? Feet from refueling ops

A

300’

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46
Q

Min crew

A

2 pilots

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47
Q

Max pax

A

19

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48
Q

Max occupants

A

22

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49
Q

Slope

A

+2% uphill
-2% downhill

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50
Q

Max eng oil temp

A

160 deg C

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51
Q

Min eng oil temp for start

A

-30 deg C

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52
Q

Min eng oil temp for takeoff power

A

20 deg C

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53
Q

Min Eng oil press for T/O (<72.3 HP)

A

35 PSI <72.3 HP

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54
Q

Min oil press for T/O (>90 Hp)

A

45 PSI >90 HP

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55
Q

Eng oil press continue flight (<72.3 HP)

A

25 PSI <72.3 HP

56
Q

Eng oil press continue flight (>90 HP)

A

35 psi >90HP

57
Q

Engine starter duty limits

A

3, three minute attempts, 15 seconds between each then 15 minutes off

58
Q

The starter may be reengaged at HP RPM speeds up to starter cut out of

A

42% HP RPM

59
Q

All operable fuel boost pumps must be selected “?” for ??? phases of flight unless fuel balancing is in progress

A

On for all

60
Q

Engines will suction feed at or below ? feet

A

20,000’

61
Q

Use of T/R’s for power back is/is not approved?

A

Is not

62
Q

Minimum fuel tank temp

A

-37 deg C

63
Q

Max fuel tank temp

A

+54 deg C

64
Q

10 deg flaps speed

A

250 knots/.60 mt

65
Q

20 deg flaps speed

A

220kcas/.60mt

66
Q

39 deg flaps speed

A

170 kcas/.60 mt

67
Q

Use of speed brakes is/is not allowed with gear down and/or full flaps?

A

Is not

68
Q

Ground spoilers may be inop if ? Is operative! 20 deg flaps are used, and wing anti-ice systems are not used. See MEL

A

Anti-skid

69
Q

If a touch-and-go landing is to be performed, the ground spoiler switch must be ? and manual spoiler landing distances must be taken into account.

A

Off

70
Q

Max landing gear altitude

A

20,000 MSL maximum

71
Q

Normal ops landing gear speed (VLO)

A

225 kcas/.70 mt

72
Q

Normal ops landing gear extended speed (VLE)

A

250 kcas/.70mt

73
Q

Landing gear blowdown speed?
Once gear extended?

A

175kcas
250kcas/.70mt

74
Q

Anti-skid may be inop provided? See MEL

A

Dry rwy, ground spoilers operative, flaps 20, cowl & wing anti-ice not used.

75
Q

Airspeed limit FL290-320

A

0.85

76
Q

Airspeed limit FL320-440

A

0.885

77
Q

Airspeed limit FL440-510

A

0.86

78
Q

Vmo above 8,000’

A

340 kcas

79
Q

Vmo below 8,000

A

300kcas

80
Q

Minimum control airspeed (Vmca)

A

112kcas

81
Q

Minimum control speed landing (Vmcl)

A

110kcas

82
Q

Minimum control speed ground (Vmcg)

A

107kcas at sea level

83
Q

Minimum control speed ground (Vmcg)

A

.86kcas at 15,000’

84
Q

Vmcg decreases linearly at approx. ? Knot per ? Ft from sea level to 15,000

A

1 knot per 1,000’

85
Q

Maneuvering speed (Va)

A

206kcas

86
Q

Turb. Penetration speed (Vb) > 10,000

A

270kcas/.80mt

87
Q

Turb. Penetration speed (Vb) <10,000’

A

240kcas

88
Q

Holding speed in icing conditions

A

160kcas

89
Q

Minimum Mach trim inop.

A

0.80mt

90
Q

Tire speed limit

A

195.5 kts

91
Q

Yaw damp inop >10,000’ ft max

A

260kcas/.80

92
Q

Yaw damp inop. <10,000’ max

A

250kcas

93
Q

Yaw damps inop. >20,000 ft. minimum

A

210kcas

94
Q

Yaw damp inop. <20,000’

A

See chart AOM Vol 1

95
Q

Max airport operating altitude

A

14,500

96
Q

Max airport with HLFE system fitted

A

15,000

97
Q

Max operating altitude

A

51,000

98
Q

Single pack operations

A

48,000

99
Q

Internal baggage door open

A

Above 40,000 ft for 5 mins

100
Q

Internal baggage door open with one Pack

A

One ECS PACK, no entry >45,000 ft

101
Q

Maximum yaw damp inop altitude

A

45,000

102
Q

APU max operating altitude

A

45,000’

103
Q

APU guaranteed start altitude

A

39,000
(May start up to 43,000)

104
Q

APU Electrical load

A

100% sea level up to 45,000’

105
Q

APU may be used for starter assisted air starts below ? Feet. However, max altitude for an engine air start is ? Feet.

A

30,000
25,000

106
Q

APU max start TGT

A

1,050

107
Q

APU max running TGT

A

732

108
Q

APU max rotor speed

A

106%

109
Q

Continuous operation of the APU starter when powered by airplane batteries:

? consecutive start attempts followed by a ? hour cooldown

A

3 consecutive start attempts followed by a 1 hour cooldown

110
Q

Continuous operation of APU starter when powered by external DC cart:

Max of ? start attempts with a ? minute cool down between each attempt. ? hour cool down after 3rd attempt
Successful consecutive starts limited to ? at ? minute intervals per start

A

Max of 3 start attempts with a 15 minute cool down between each attempt. 1 hour cool down after 3rd attempt.

Successful consecutive starts limited to 6 at 10 minute intervals per start

111
Q

What conditions do we turn on Cowl anti-ice ?

A

SAT 10 deg. C or below and visible moisture

112
Q

When do we turn on wing anti-ice?

A

Icing conditions are imminent or immediately upon detection

113
Q

Max engine fuel temp

A

140 C

114
Q

Fuel temp up to ? for a max of ? minutes is permissible

A

165 C , 15 mins

115
Q

Minimum engine fuel temp

A

-40 C

116
Q

Speed brakes are not allowed when landing gear is ? and/or ?

A

Gear extended and/or full flaps

117
Q

Flaps 0 flight load

A

-1 to 2.5

118
Q

Flaps 10 or 20 flight load

A

0 to 2.0 up to max takeoff weight

119
Q

Flaps 39 flight load < 75,300 lbs

A

0 to 2.0

120
Q

Flaps 39 flight load > 75,300 lbs

A

0 to 1.5

121
Q

Do not operate HMG when normal ? power is available, except as provided for in L or R ? failure.

A

AC

ESS DC bus failure

122
Q

With a single nine inop, select ? Only as the TCAS operating

A

TA only

123
Q

Mach trim inop

A

.80 MT maximum

124
Q

Autopilot minimum engage height on takeoff

A

200’ AGL

125
Q

Autopilot minimum disengage height for ILS, MLS, or LPV approach

A

60’ AGL

126
Q

Autopilot minimum disengage height for MDA/DA from LNAV approach

A

50’ below MDA/DA

127
Q

Autopilot minimum demonstrated altitude loss for coupled go-around

A

60’

128
Q

Auto-throttles are available from takeoff to landing except?

A

Single engine approach

129
Q

Minimum flight crew

A

Pilot and copilot

130
Q

Maximum passengers

A

19

131
Q

Max occupants

A

22

132
Q

Max slope for takeoff and landing

A

+2% uphill and -2% downhill

133
Q

APU ? Ground ops are prohibited

A

Ground

134
Q

APU use in flight prohibited except the following

A

Dual engine failure
Dual generator failure
Single engine failure
Single generator failure

135
Q

The APU may be operated in-flight for the purpose of “bleeds off” takeoff, up to a max of ? Ft

A

5,000’ AGL

136
Q

Dispatch is ? Premiered with any engine generator inop

A

Not

G550 (2 decks)

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