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Gulfstream 550 > General > Flashcards

General Flashcards

0
Q

Maximum tailwind approved for take-off and landing

A

10kts

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1
Q

Maximum slopes approved for take-off and landing

A

+2%(uphill)

-2%(downhill)

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2
Q

Maximum approved airport pressure altitude for take-off and/or landing

A

14500ft

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3
Q

Maximum speeds vs. altitude

A 
300 KCAS             0-12000 ft
340 KCAS     12000-27860 ft
M 0.85           27860-32160 ft
M 0.885         32160-43500 ft
M 0.86           43500-51000 ft
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4
Q

Polar navigation is approved, provided:

A

TRUE heading is selected prior N73 and S60 deg latitude

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5
Q

Maximum operating altitude

A

51000 ft

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6
Q

Maximum operating altitude with yaw damper inoperative

A

45000 ft

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7
Q

Maximum operating altitude with single air-conditioning pack operating

A

48000 ft

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8
Q

Maximum operating altitude for extending or flying with landing gear extended

A

20000 ft MSL

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9
Q

Maximum operating altitude for extending landing flaps (39deg/down) or flying with flaps extended

A

20000 ft MSL

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10
Q

Maximum operating altitude for extending flaps to 10 deg or 20 deg, or flying with flaps extended to 10 or 20 degrees

A

25000 ft MSL

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11
Q

Minimum control speed, Air

A

112 KCAS

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12
Q

Minimum control speed, Landing

A

110 KCAS

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13
Q

Minimum control speed, Ground

A

107 KCAS - see level
86 KCAS - 15000 ft

(Rate 1 kt / 1000 ft)

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14
Q

Maneuvering speed (Va)

A

206 KCAS

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15
Q

Maximum flaps extended speeds - take-off (10deg)

A

250 KCAS

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16
Q

Maximum flaps extended speeds - take-off approach (20deg)

A

220 KCAS

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17
Q

Maximum extended speeds - Down (39 deg):

A

170 KCAS

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18
Q

Maximum landing gear extended speed

A

250 KCAS / 0.70 Mt

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19
Q

Maximum landing gear operation speed, normal operation

A

225 KCAS

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20
Q

Maximum landing gear operation speed, alternate operation

A

175 KCAS

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21
Q

Minimum holding speed

A

160 KCAS

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22
Q

Mach trim / electric elevator trim inoperative speed

A

0.80 Mt

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23
Q

Turbulence penetration speed

A
  • altitude 10000 ft or above - 270 KCAS / 0.80 Mt

- below 10000 ft - 240 KCAS

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24
Q

Maximum tire speed

A

195 KCAS

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25
Q

Maximum speed with the emergency stabilizer trim armed, autopilot engaged and a jammed elevator

A

270 KCAS / 0.80 Mt

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26
Q

Flight load acceleration - flaps up (0 deg)

A

-1 - 2.5g

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27
Q

Flight load acceleration - flaps 10 or 20 deg

A

0 - 2.0g

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28
Q

Flight load acceleration - flaps Down (39 deg)

A

< MAX Landing weight - 0-2.0g

> MAX Landing weight - 0-1.5g

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29
Q

Maximum Zero Fuel Weight

A

52000 lb

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30
Q

Maximum Ramp Weight

A

91400 lb

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31
Q

Maximum Take-Off Weight

A

91000 lb

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32
Q

Maximum Landing Weight

A

75300 lb

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33
Q

Center of Gravity (ZFW)

A

Min 37.5% MAC

Max 45.0% MAC

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34
Q

Maximum fuel imbalance for take-off

A

1000 lb

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35
Q

Maximum fuel imbalance in-flight

A

2000 lb

36
Q

The engine will run stable on suction fuel feed (no boost pumps) below:

A

20000 ft

37
Q

Maximum Cabin Pressure Differential permitted:

A

10.48 psi

38
Q

Maximum Cabin Pressure Differential permitted for take-off and landing

A

0.3 psi

39
Q

Internal baggage door should be closed above:

A

40000 ft

40
Q

If operating on a single ECS pack the access to the baggage compartment is allowed only at or below:

A

45000 ft

41
Q

Time with the internal baggage door open above 40000ft is limited to:

A

5 minutes

42
Q

Maximum Mmo with Mach Trim inoperative:

A

0.80 Mt

43
Q

Single engine autopilot coupled go-around is:

A

Not approved

44
Q

Autopilot minimum engage height:

A

200 ft

45
Q

Autopilot minimum disengage height:

A
  • ILS approach - min 60ft

- LNAV/VNAV approach - max 50 ft below MDA

46
Q

Maximum demonstrated altitude loss in coupled Go-Around:

A

60 ft

47
Q

Use of autothrottle during single engine approach is:

A

Prohibited

48
Q

When Standby Electrical Power System (HMG) is in operation, speed brakes may be used, provided:

A

Operation is slow (approximately 3 seconds for full range movement)

49
Q

Speed brakes extension with flaps at 39 deg or with landing gear extended in flight:

A

Not approved

50
Q

Usable fuel capacity:

A

41300 lb

51
Q

Red “Fuel Tank Temperature” CAS message, when:

A
  • Fuel tank temperature of +54deg C or greater; or

- Fuel tank temperature is -37 deg C or less.

52
Q

Amber “Fuel Tank Temperature” CAS message is displayed when

A

Fuel tank temperatures are -35 deg C to -36 deg C

53
Q

Maximum hydraulic reservoir quantities (pressurized) are

A
  • left hydraulic system: 4.8 gal

- right hydraulic system: 1.6 gal

54
Q

Left and Right hydraulic system accumulator pre-charge is

A

1200 psi at 21 deg C, +/- 25 psi for each 5 deg C difference in temperature from 21 deg C

55
Q

Automatic anti-ice is inhibited above:

A

35000 ft

56
Q

Holding in icing condition is limited to ……. Flaps only.

A

0 deg (up)

57
Q

All RA and TA aural messages (TCAS) are inhibited at a radio altitude of

A

Less than 500 ft +/- 100 ft climbing and descending.

58
Q

The APU may be used for starter-assisted main engine starts below

A

30000 ft

59
Q

Maximum permissible APU EGT:

A
  • Start: 1050 deg C,

- Running: 732 deg C.

60
Q

Maximum APU rotor speed

A

106%

61
Q

APU starter limitations, when powered by airplane batteries

A
  • max 3 consecutive start attempts;

- 1 hour cool down period.

62
Q

APU starter limitations, when powered by an external DC cart

A
  • max 3 consecutive start attempts;
  • 15 minutes cool down between start attempts;
  • 1 hour cool down perid.
63
Q

The APU generator can deliver 100% (40 KVA) electrical power on the ground or in flight (altitude?)

A

Sea level to 45000 ft

64
Q

APU is guaranteed to start at or below

A

39000 ft (possible start from 39000 ft to 43000 ft)

65
Q

APU operations limitation (altitude)

A

45000 ft

66
Q

Max TGT during powerplant ground start

A

700 deg C (momentary)

67
Q

Max TGT during airstart (relight)

A

850 deg C (momentary)

68
Q

Max TGT (powerplant) during take-off

A

900 deg C (5 min - all engines, 10 min - single engine)

69
Q

Max continuous powerplant TGT

A

860 deg C (unrestricted)

70
Q

Max powerplant overspeed

A

Max LP 101.5%
Max HP 99.8%
(20 sec)

71
Q

Max powerplant TGT overtemperature

A

905 deg C (20 sec)

72
Q

Max LP reverse thrust

A

Max LP 70.0% (30 sec)

Above 60 kts IAS

73
Q

Maximum crosswind component for ground start

A

30 kts

74
Q

Maximum tailwind component for engine ground start

A

20 kts

75
Q

Prefered method of engine airstart

A
  1. Automatic

2. Manual starter assist / Windmill airstart

76
Q

Take-off in alternate control mode:

A

Prohibited

77
Q

Minimum engine fuel temperature

A

-40 deg C

78
Q

Maximum engine fuel temperature

A

Unrestricted: +140 deg C.

Transient (15 min): +165 deg C.

79
Q

Maximum fuel tank temperature

A

+54 deg C

80
Q

Limitation on continuous (airstart) ignition

A

No limitation on duty cycle time

81
Q

Minimum oil inlet temperature for starting

A

-30 deg C

82
Q

Minimum oil inlet temperature for take-off power

A

+20 deg C

83
Q

Maximum oil inlet temperature

A

+160 deg C

84
Q

The engine must be shut down when oil pressure drops below

A

25 psi

85
Q

Minimum engine oil pressure for power setting below 72.3 % HP

A
  • for take-off - 35 psi;

- to complete the flight - 25 psi.

86
Q

Minimum engine oil pressure with power setting above 90.0 % HP

A
  • for take-off - 45 psi;

- to complete the flight - 35 psi.

87
Q

Engine starter duty cycle:

A
  • 3 start cycles with a max 3 min per start cycle;
  • 15 seconds delay between start cycles;
  • 15 min delay after 3 start cycles
88
Q

The starter may be reengaged at HP RPM speeds up to

A

42% HP RPM

Gulfstream 550 (1 decks)

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