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USAPAT Study > G550 Limits > Flashcards

G550 Limits Flashcards

1
Q

Max Speed, use of tiller steering

A

60 Kts

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2
Q

Min. Control Speed Ground (Vmcg) at 15,000 feet

A

86 Kts

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3
Q

Min Control Speed Ground (Vmcg) at Sea Level

A

107 Kts

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4
Q

Min. Control Speed Landing (Vmcl)

A

110 KCAS

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5
Q

Min. Control Speed Air (Vmca)

A

112 KCAS

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6
Q

Min. speed in icing conditions

A

160 KCAS

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7
Q

Max Speed Flaps 39°

A

170 KCAS / .60 MT

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8
Q

Max speed alternate extension of landing gear handle blow down
(emergency gear handle ops)

A

175 KCAS

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9
Q

Max tire speed

A

195.5 KCAS

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10
Q

Max speed with deployed Thrust Reverser

A

200 KCAS

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11
Q

Maneuvering Speed (Va)

A

206 KCAS

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12
Q

Yaw Damp Inop greater than 20k ft
(Minimum speed)

A

Min 210 KCAS

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13
Q

Max Speed Flaps 20°

A

220 KCAS / .60MT

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14
Q

Max Gear Extension Speed (Vlo)

A

225 Knots / 0.70 Mach

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15
Q

Turb. Penetration Speed (Vb) less than 10k ft

A

240 KCAS

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16
Q

Max Gear Extended Operation (Vle)

A

250 Knots/ 0.70 MT

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17
Q

Max Speed Flaps 10°

A

250 KCAS / .60MT

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18
Q

Yaw Damp Inop below 10,000 ft

A

Max 250 KCAS

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19
Q

Yaw Damp Inop above 10,000 ft

A

Max 260 KCAS / 0.80 mach

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20
Q

Turb. Penetration Speed (Vb) above 10,000 ft

A

270 Kts / .80 MT

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21
Q

Vmo below 8,000’ __________
Vmo above 8,000’ __________

A

Vmo below 8,000’ 300 KCAS
Vmo above 8,000’ 340 KCAS

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22
Q

Maximum Mach with Trim Inoperative

A

0.80 mach

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23
Q

Max Speeds at FL

A

Max Speed FL 290-320: 0.85 mach
Max Speed FL 320-440: 0.885 mach
Max Speed FL 440-510: 0.86 mach

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24
Q

Max altitude, APU use during “bleeds off” T/O:

A

5,000 ft

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25
Q

Max Airport Take-Off Elevation

A

14,500 ft

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26
Q

Max altitude Flaps 39° or Gear Extended

A

20,000 ft

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27
Q

Max alt. possible for engine suction fuel feed (without cross flow opened and fuel pump turned on)

A

20,000 ft

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28
Q

Max altitude wind-milling engine airstart

A

25,000 ft

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28
Q

Max altitude Flaps 10° or Flaps 20°

A

25,000 ft

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29
Q

Max altitude APU-assisted engine airstart

A

30,000 ft

(Engine limit is 25k)

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30
Q

Max altitude Anti-Ice AUTO mode works

A

35,000 ft

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31
Q

Max altitude APU guaranteed start

A

39,000 ft

32
Q

Internal baggage door open, above 40,000’

A

5 min limit

33
Q

Max altitude APU may start

A

43,000 ft

34
Q

Internal baggage door open, with only one ECS Pack operational, no entry above _________

A

45,000 ft

35
Q

Max altitude yaw damp inop

A

45,000 ft

36
Q

Max altitude APU operations

A

45,000 ft

37
Q

Max altitude single pack operations

A

48,000 ft

38
Q

Max Operational altitude

A

51,000 ft

39
Q

Max Fuel Imbalance, during takeoff

A

1,000 lbs

40
Q

Max Fuel Imbalance, in-flight

A

2,000 lbs

41
Q

Max Fuel capacity

A

41,300 lbs

42
Q

Max Zero Fuel Weight

A

54,500 lbs

43
Q

Max Landing Weight

A

75,300 lbs

44
Q

Max Takeoff Weight

A

91,000 lbs

45
Q

Max Ramp Weight

A

91,400 lbs

46
Q

Min Engine Fuel Temperature

A

-40° C

47
Q

Min Fuel Tank Temperature

A

-37° C

48
Q

Min Oil Temp for starting engine

A

-30° C

49
Q

Cowl Anti-Ice ON (w/ visible moisture)

A

10° C or below

50
Q

Min cabin temp before cockpit system pwr

A

18°C/65°F

51
Q

Min Oil Temp for T/O Power

A

20° C

52
Q

Fuel Tank Temperature Limits

A

Min -37° C
Max 54° C

53
Q

Max Engine Fuel Temperature

A

140° C

54
Q

Max Residual Engine Temp (TGT) prior to ground start

A

150° C

55
Q

Max Engine Oil Temperature

A

160° C

56
Q

APU Max Start Temperature

A

1,050° C

57
Q

Max tailwind component during takeoff

A

10kts

58
Q

Max tailwind component during engine start _______

For acceleration to takeoff with crosswinds above ____ kts, the fan speed is limited to less than 66 % LP RPM until a forward speed of _______ kts has been reached. Above ______ kts forward speed, a slam acceleration to T/O power is required. Add _______ft to the required field length when using this procedure.

A

20kts x4
600 feet

Max tailwind component during engine start 20kts

For acceleration to takeoff with crosswinds above 20 kts, the fan speed is limited to less than 66 % LP RPM until a forward speed of 20 kts has been reached. Above 20 kts forward speed, a slam acceleration to T/O power is required. Add 600 ft to the required field length when using this procedure.

59
Q

Max demonstrated crosswind landing

A

28kts

60
Q

Max crosswind component during engine start

A

30kts

61
Q

Gust Procedure: For winds greater than ___ kts, add ____ the steady state wind plus the entire gust to the VREF speed, up to a maximum addition of ____ kts.

A

Gust Procedure: For winds greater than 10 kts, add 1/2 the steady state wind plus the entire gust to the VREF
speed, up to a maximum addition of 20 kts.

62
Q

In tailwinds greater than ____ kts, the direction of rotation of LP may be initially reversed.

A

In tailwinds greater than 10 kts, the direction of rotation of LP may be initially reversed.

If so, the fuel control switch should not be set to run until the LP indication confirms positive rotation.

63
Q

RADAR Min operational distance from personnel

A

49 ft

64
Q

RADAR Min operational distance from refueling ops

A

300 ft

65
Q

Max cabin press diff (taxi / takeoff / landing) ____ PSID

Red Cabin Differential CAS / Max press diff _____ PSID

A

Max cabin press diff (taxi / takeoff / landing) 0.3 PSID

Red Cabin Differential CAS / Max press diff 10.48 PSID

66
Q

Cabin Pressure LOW CAS Message

A
67
Q

Cabin alt. for oxygen mask deployment

A

14,750 ft +/- 250

68
Q

G550 APU Start Limitations

When powered by batteries, ___ consecutive start cycles followed by ___ hour cool down.

When powered by an external DC power source, a max of __ start attempts with a ___ minute cool down between each attempt. Allow ___ hour cool down after 3rd attempt.

A

When powered by batteries, 3 consecutive start cycles
followed by 1 hour cool down.

When powered by an external DC power source, a max of 3 start attempts with a 15 minute cool down between each attempt. Allow 1 hour cool down after 3rd attempt.

69
Q

G550 Engine Start Limitations

__ start cycles with a maximum of __ minutes per cycle.
Delay 15 seconds between start cycles. After __ start cycles, delay use of the starter for at least ___ minutes.

A

3 start cycles with a maximum of 3 minutes per cycle.
Delay 15 seconds between start cycles. After 3 start cycles, delay use of the starter for at least 15 minutes.

70
Q

Starter may be reengaged at HP RPM speeds up to starter cut out of ___% HP RPM

A

Starter may be reengaged at HP RPM speeds up to starter cut out of 42% HP RPM

71
Q

Rotor Shaft Bow If the engine has been shutdown for more than ___ minutes but less than __ hours:

Crank engine at max HP RPM for 30 seconds before selecting fuel cntrl to run. It is not unusual for peak EVM value above the alert level (0.80) to be seen during start.

Alternatively, the engine may be cranked for a minimum of ___ seconds at max cranking HP RPM, not more than ___ minutes before a normal engine start.

A

Rotor Shaft Bow If the engine has been shutdown for more than 20 minutes but less than 5 hours:

Crank engine at max HP RPM for 30 seconds before selecting fuel cntrl to run. It is not unusual for peak EVM value above the alert level (0.80) to be seen during start.

Alternatively, the engine may be cranked for a minimum of 60 seconds at max cranking HP RPM, not more than 20 minutes before a normal engine start.

72
Q

G550 Time Limitations

Min time, engine idle before shutdown ___ min
Min time, engine idle before takeoff ___ min
Oil QTY checked between __ & ___ min after shutdown

A

G550 Time Limitations

Min time, engine idle before shutdown 3 min
Min time, engine idle before takeoff 5 min
Oil QTY checked between 5 and 30 min after shutdown

73
Q

G550 Distance / Length Limitations

Min taxi strip width capable of 180° turn ___ feet
Length of plane:
Wingspan of plane:
Height of tail above the ground:

A

G550 Distance / Length Limitations

Min taxi strip width capable of 180° turn 62 feet
Length: 96 feet 5 inches
Wingspan: 93 feet 6 inches
Height: 25 feet 11 inches

74
Q

G550 Flight Load Limitations

Flaps 0° _____g to ______g
Flaps 10° or Flaps 20° ____ to ___g (up to Max T/O Wt)
Flaps 39° __ to ____g (below 75,300 lbs)
Flaps 39° __ to ____g (above 75,300 lbs)

A

G550 Flight Load Limitations

Flaps 0° -1g to 2.5g
Flaps 10° or Flaps 20° 0 to 2.0g (up to Max T/O Weight)
Flaps 39° 0 to 2.0g (below 75,300 lbs)
Flaps 39° 0 to 1.5g (above 75,300 lbs)

75
Q

TGT Limits

A

Maximum Ground Starting TGT: 700° Max Relighting (Airstart): 850°
Max Continuous: 860°
Max Takeoff: 900° (5min DE, 10 min SE)
Max Overspeed: 905° (20 seconds)

76
Q

LP% RPM Limits

A

Max Takeoff: 101.1% (5min DE, 10 min SE)
Max Continuous: 101%
Max Overspeed: 101.5% (20 seconds)
Max reverse: 70% (30 seconds)

77
Q

HP% RPM Limits

A

Max Takeoff: 99.6% (5min DE, 10 min SE)
Max Continuous: 98.9%
Max Overspeed: 99.8% (20 seconds)

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