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Gulfstream 650 > G650ER Memory Flash Cards > Flashcards

G650ER Memory Flash Cards

1
Q

Length, height, and wingspan

A

Length: 99’ 9”
Height: 25’ 7”
Span: 99’ 7”

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2
Q

Maximum Weights

Zero Fuel
Ramp
Takeoff
Landing

A

Max Zero Fuel: 60,500 Lbs
Max Ramp: 104,000 Lbs
Max takeoff: 103,600
Max Landing: 83,500

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3
Q

Max Passengers

A

19
(Depending on floor plan)

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4
Q

Minimum taxi strip for 180° turn?

A

62 feet.

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5
Q

Landing light auto extinguish altitude?

A

18,000 feet; however, pulse mode can operate at altitudes up to 51,000 feet.

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6
Q

Cruising Altitudes?
Initial
Max

A

Initial FL 410
Max FL 510

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7
Q

Range

A

7,000 NM at Mach .85
7,500 NM at Mach .85, with ASC 014

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8
Q

High speed cruise

A

Mach .90

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9
Q

Internal baggage door altitude restriction?

A

Shall remain closed above 40,000’

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10
Q

Max fuel weight?

A

44,200 Lbs.
48,200 Lbs with ASC 014

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11
Q

Max approved airport altitude?

A

15,000’

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12
Q

Max runway slope for takeoff and landing operations?

A

± 2%

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13
Q

Max tailwind component for takeoff

A

10 Knots

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14
Q

Max demonstrated crosswind for takeoff and landing?

A

28 knots

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15
Q

Max crosswind component approved for takeoff and landing when airport field elevation is 10,000’ or above?

A

25 Knots

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16
Q

When may autothrottles be used?

A

From takeoff to landing

Prohibited on Single Engine Approaches

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17
Q

Limitation for ground operation of landing lights

A

10 Minutes

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18
Q

Turbulent Air Penetration Speed

A

10,000’ or above:

270 Knots/.85 Mach

______________________

Below 10,000’:

240 Knots

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19
Q

Max operating speed

A

.925 Mach

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20
Q

Don’t operate weather radar within____ ft. of refueling ops or within ___ of ground personnel?

A

50’, 11

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21
Q

Autopilot Minimum engage height?

A

200’ AGL

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22
Q

Autopilot minimum disengage height from an ILS or LPV approach?

A

80’ AGL

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23
Q

Autopilot minimum disengage height for all other operations?

A

200’ AGL

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24
Q

Maximum demonstrated altitude loss for coupled go-around?

A

50’

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25
Q

Use of autopilot during single engine go-around?

A

Not approved

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26
Q

When can VGP mode not be used

A

VGP mode cannot be used during circling approaches and cannot be armed if preview mode is active.

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27
Q

When is a VOR Approach mode prohibited?

A

If VOR station overflight is required during any portion of the intermediate or final approach segments, excluding the missed approach point

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28
Q

APU generator electrical load?

A

Can deliver 100% (40 KVA)
Electrical power on the ground or in flight from sea level to 45,000’

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29
Q

Max Flap Extended Speed

A

10° = 250 Knots
20° = 220 Knots
39° = 190 Knots

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30
Q

Max operating altitude for extending Flaps to 10° or to 20° or flying with the Flaps extended to 10° or 20°

A

25,000 ‘ MSL

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31
Q

Max Operating Altitude for extending landing Flaps (39° down) or flying with landing Flaps extended

A

20,000’ MSL

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32
Q

When is use of speedbrakes prohibited?

A

Not approved with flapa set at 39° or Landing Gear extended in flight

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33
Q

Ground spoiler restrictions for touch and go landing?

A

GND SPLR must be OFF and manual spoiler landing distances must be taken into account

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34
Q

Restrictions when operating in other than NORMAL MODE?

A
  1. MAX Speed - 285 Knots/ .90 Mach
  2. Crosswind for Landing - 10 Knots
  3. Flight inti known icing cinditions prohibited
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35
Q

Max deflection of flight controls should be confined to speeds below……

A

206 Knots

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36
Q

Max speed if any primary flight control surface or speedboats panel is failed due to a component malfunction (s) or Hydraulic System Failure

A

Do not exceed 285 Knots, .90 Mach

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37
Q

Max tire speed?

A

195 Knots

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38
Q

Max operating altitude for extending landing gear or flying with the landing gear extended?

A

20,000’ MSL

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39
Q

Max speed for extending or retracting the landing gear?

A

225 Knots

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40
Q

Max speed for flying with the landing gear extended?

A

250 Knots

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41
Q

Max speed for extending rhe landing gear using rhe alternate system?

A

175 Knots

42
Q

Max nose wheel and pedal steering authority?

A

Nose wheel steering ± 80°

Pedal steering ± 7°

If tiller steering fails, rudder pedal steering authority automatically increases to ± 16°

43
Q

Max cabin pressure differential permitted for taxi, takeoff or landing?

A

.30 PSI

44
Q

Max normal differential pressure

A

10.69 PSI

45
Q

Part 91 rules for O2 mask donning?

A

Above FL350, pilot must mask if other pilot leaves the cockpit

Above FL410 one Pilot must mask

46
Q

Part 135 rules for donning O2?

A

Above FL250 pilot must mask if other pilot leaves the cockpit

Above FL350 one pilot must mask

47
Q

What altitude is prolonged operation with passengers on O2 NOT recommended?

A

Above 25,000’

48
Q

Single Pack Restrictions?

A

Maintain at or below 48,000’ for remainder of flight

49
Q

Apulia starter duty cycle?

A

3 Consecutive start attempts, then 1 hour cool down period

50
Q

Apulia Max Start Altitude?

A

39,000’

51
Q

Altitude at which APU can provide starter assist for main engine start?

A

Less than or equal to 30,000’

52
Q

Engine Starter Duty Cycle

A

3 Start Cycles at 3 Minutes each, with 15 seconds cool down between cycles. After 3 start attempts, delay use of starter for 15 minutes.

53
Q

Max Crosswind Component and tailwind component for engine ground start?

A

30 knots crosswind
20 knots tailwind

CAUTION: Tailwind of 10 knots, direction of rotation of LP (fan,) might be reversed. If so, the fuel control switch should not be set to run until the LP indication confirms positive rotation

54
Q

Min Oil Temp for engine start?

A

-40°C

55
Q

Max TGT prior to ground start?

A

150° C

56
Q

Max start TGT?
On ground
In flight

A

On ground: 700°C

In flight: 850°C

57
Q

Starter re-engagement RPM?

A

42% HP

58
Q

Crisswind/ tailwind limits for static operation above idle?

A

Limited to crosswind component of 25 knots and /or tailwind of < 20 Knots

59
Q

Use of takeoff thrust?

A

5 Minutes with all engines operating or 10 for single engine in the event of an engine failure.

60
Q

Max Takeoff TGT?

A

900° C for 5 Minutes

61
Q

Max Continuos TGT?

A

885° C unrestricted

62
Q

Engine suction feed altitude?

A

Below 20,000’, engine will run on suction feed

Above 20,000’, the engine will run erratically and flame out if crossflow valve is not open with at least one boost pump on

63
Q

Speed for canceling reverse thrust?

A

Should be initiated so as to be at reverse idle position by 60 Knots

64
Q

Requirement if reverse thrust is used to bring the airplane to a halt in an emergency?

A

Record and report for maintenance action

65
Q

Use of reverse thrust to power back?

A

Not approved

66
Q

When should you check engine oil?

A

Between 5 Mins- 24 hours after shutdown. If in doubt, run engines at idle for 10 minutes, and re-check oil

67
Q

Temperature at which corner anti-icing required for taxi and takeoff with visible moisture, precipitation, or wet runway present?

A

+10°C

68
Q

When is takeoff prohibited?

A

With frost, icen snow, or slush adhering to the wings, control surfaces,Engine inlets, or other critical surfaces

69
Q

When is auto anti-ice feature inhibited

A

Above FL 350

70
Q

Use of wing and cowl anti-ice

A

Must be selected when entering icing conditions is imminent or immediately upon detection of ice formation on winhs, wingless, or windshield edges

71
Q

Use of Flaps in icing conditions?

A

Restricted to take off, approach and landing only

72
Q

Holding in icing conditions?

A

Flaps up, minimum speed of 180 Knots

73
Q

Max altitude for use of WAI with single bleed?

A

41,000’

74
Q

Minimum airspeed for use of WAI above 41,000?

A

.85 Msch

75
Q

Boost pump operation?

A

All operable boost pumps must be selected on for all phases of flight unless fuel balancing in progress

76
Q

Max Fuel Imbalance

Ground

Flight

A

Ground: 1000 Lbs

Flight: 2000 Lbs

77
Q

Crossflow valve affect on heated fuel return?

A

Heated fuel return ceases when crossflow valve is opened.

78
Q

Minimum Holding speed in Icing

A

180 Knots

79
Q

Maximum G Load Flaps up

A

-1.0 - 2.5 Gs

80
Q

Max G Load with Flaps extended to Flaps 10/20

A

0 to 2.0 Gs

81
Q

Max G Load with Flaps 39

A

0- 1.5 Gs

82
Q

Cabin Pressure where Amber CAS appears

A

10.8 PSI

83
Q

Cabin Pressure where RED CAS Appears

A

11.0 PSI

84
Q

Minimum speed with RAT Deployed for useful energy

A

180 Knots

85
Q

What Engines does the G650ER Have?

A

Rolls Royce
BR700-725A1-12

Rated at 16,900 Lbs of Thrust Per Engine
At Sea Level and ISA+15°C

86
Q

How Long do the EBHA and UPS Batteries last

A

30 Minutes

But can be charged by the RAT above 180 Knots

87
Q

How many NiCad Batteries

A

3- 28V DC Batteries

88
Q

What kind of Batteries are the Mains and EBHA?

A

NiCad 28 V DC Batteries

89
Q

Min oil temp for Take off

A

20° C

90
Q

Speeds for Assisted Air Start (APU)
Or Windmilling

A

Below 250, APU, Apove 250 Windmilling

91
Q

Max Fuel Tank Temp

A

54°C

92
Q

Min Fuel Tank Temp

A

-37° C

93
Q

At what Temp is the heated fuel return activated?

A

0°C or colder

94
Q

When does heated fuel return deactivate?

A

Temps above 10°C

95
Q

When does the Hyd PTU activate?

A

When Left System Pressure drops below 2400 PSI

Right System is above 2850 PSI

And left System fluid qty is above .36 Gal.

96
Q

Engine warmup if Temps less than 1°C

A

Operate Engine at 40% LP for 10 seconds before take off, every 60 Minutes.

97
Q

Operation on freezing fog below -10°C?

A

Prohibited

98
Q

How many start attempts of the APU on Batt Power?

A

2 Start attemps

99
Q

Max Temp for Take Off

A

Isa +35°C

100
Q

Min Temp for Take-off

A

-50°C

Gulfstream 650 (1 decks)

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