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G650 > Limitations > Flashcards

Limitations Flashcards

1
Q

Minimum Crew

A

2

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2
Q

Maximum Number of PAX

A

19

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3
Q

Runway conditions (WET/CONT)

A
  • 25% of the surface being used, is damp irrespective of it being reflective
  • 25% of the surface being used, frost, ice, snow, slush or greater than 1/8 inch (3mm) of water
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4
Q

Slope

A

+/2 deg

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5
Q

Wind limits

A

TWC 10kts
Abnormal flight control laws, 10kts
Above 10 000ft maximum xwind 25kts

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6
Q

High Elevation Airport

A

14500ft or 15000ft

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7
Q

Minimum / Maximum Operating TEMP

A

Minimum temp for Ground ops following prolonged cold soak: -40
Minimum inflight temp: - 54 TAT

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8
Q

Maximum Operating Altitude

A

51 000ft
Single Pack 48 000ft
Landing Gear extension: 20 000ft
Flaps extension: 10 - 20deg, 25 000ft
39/down, 20 000ft

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9
Q

Internal baggage door

A

40 000ft or 45 000ft

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10
Q

VA

A

206kts

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11
Q

Maximum Flap

A

Take off (10) 250KCAS
T/O APP (20) 220KCAS
DOWN (39) 190 KCAS

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12
Q

Vle

A

250 KCAS

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13
Q

Vlo

A

Normal 225 KCAS
Alternate 175 KCAS

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14
Q

Yaw Damper inop speed

A

285 / 0.9m

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15
Q

Turb penetration

A

Above 10 000ft 270KCAS/0.85m
Below 10 000ft 240 KCAS

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16
Q

Maximum Tyre speed

A

195 Kts

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17
Q

Degraded Flight Control Speed

A

285KCAS / 0.9M

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18
Q

Flight Load

A

Flaps 0 -to -1/2.5g
Flaps 10 or 20 - 0 to 2 G
Flaps Down 0 to 1.5G

19
Q

Maximum imbalance

A

For Takeoff - 1000lb
Inflight - 2000lb

20
Q

Auto pilot

A
  1. Minimum engagement of autopilot: 200ft AGL
  2. Minimum disengagement height: 80ft ILS or LPV
  3. Minimum Disengagement height 200ft height
  4. Altitude loss for coupled approach is 50ft
  5. Auto throttle for single engine operations is not permitted for approach or go around
21
Q

TRU load limits

A

Left Main, Left Essential, Right Main, Right Essential - 80%
Aux - 40%

22
Q

Stall protection

A

Is only available in Normal law

23
Q

Speed brakes

A

Not approved with flaps at 39 deg

24
Q

Take off prohibited when not in normal law

A
25
Q

Refueling

A

Pressure refueling:
Right Tank - 10024kg / 22100lbs
Left Tank - 10024kg / 22100lbs
Total - 20048 / 44200lbs

Overwing - 43650 Lbs

26
Q

Hyd failure occurs

A

Within 1 hour after takeoff
- Altitude no to exceed 27 000ft
- Land within 1.5 hours after failure

More than one hour after take off
- Land within 9 hours

27
Q

Wing Anti-icing

A

Wing anti-icing above 41000ft airspeed must be M0.85 of greater
Maximum altitude with one pack inop max altitude 41 000

28
Q

Engine anti-ice must operation

A

On the ground

SAT - 10deg C in visible moisture on the RWY

Less than 1 deg SAT and in visible moisture,
- maximum 60 min accelerate engine to 40%LP pause wait 10 seconds, then idle
- For Takeoff accelerate the engine to 40% LP pause for 2 seconds then take off

For other temps review the setting.

29
Q

Use of Flaps

A

In icing, before selecting the flaps, ensure wing anti-ice is selected on
Minimum speed holding in icing 180 KCAS

30
Q

Autobrakes

A

Low and Medium modes on Contaminated RWYs is not authorized

31
Q

Operation of Landing lights

A

10 minutes on ground

32
Q

IRS during operation

A

Align In motion may cause an extended delay:
- No change in heading
- No change in acceleration
-

33
Q

TCAS RA

A

The autopilot must be off

34
Q

Engine power plant limits

A

TGT 900C above red arc
% LP 102.8 red arc
% HP 100 red arc
Oil temp: 160C - -41C and below red digits
0 - 25 PSI red digits
- 37 and below red digits

35
Q

Engine temperature operating limits

A

Maximum Temps
Ground Start 700 momentary
Air start 850 Momentary
Take off LP102.8 / HP100 / TGT 900 5 minutes
MCT LP102.8 / HP98.7 / TGT 885 unrestricted
Maximum over speed LP 104.3 / HP 101.3 20 Seconds
Maximum over temp 920 20 Seconds
Reverse thrust LP 78.1 30 Seconds

36
Q

Engine Ground Start

A

Max Crosswind Component: 30 kts
Max TWC: 20 kts
TWC 10 kts, maximum HP motoring

37
Q

Engine Fuel Temprature

A

Minimum: -40
Max unrestricted: +140
Max (15min) transient: +165

38
Q

Max Fuel Tank Temperature

A

+54 degrees. C

39
Q

Thrust reverser limit

A

Idle rev by 60 kts
May be used for taxi - no time limit
Deployment every 100 hours
If reverse is used to halt the aircraft then record in the ATL
No backup reverse operations

40
Q

Oil Inlet temperature

A

Minimum for starting -40 deg C
Minimum for takeoff +20 deg C
Maximum Temp +160 deg C

41
Q

Shut down Oil pressure

A

When pressure drops below 25 Psi

42
Q

Starter Duty Cycle

A

3 starter cycles in 3 minutes 15 second break
After 3 cycles 15 min break

43
Q

Turning diameter

A

Turning circle - 114 ft

44
Q

Aircraft dimensions

A

Length - 99.9ft
Wingspan - 99.7

G650 (3 decks)

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