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G550 > Limitations > Flashcards

Limitations Flashcards

0
Q

Dimensions
Length?
Height?
Wingspan?

A

Length 96’5”
Height 25’11”
Wingspan 93’6”

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1
Q 
MAXIMUM WEIGHTS
     Ramp?
     Takeoff?
      Zero Fuel?
      Landing?
A

Ramp - 91,400
Takeoff - 91,000
Zero Fuel - 54,500
Landing - 75,300

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2
Q

What is the minimum taxi strip width to make a 180 degree turn?

A

62’

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3
Q

Runway slope limitations

A

+/- 2 %

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4
Q

Usable fuel capacity

A

41,300 lbs

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5
Q

Maximum fuel imbalance:

  • Takeoff?
  • Flight?
A

Takeoff - 1000 lbs

Flight - 2000 lbs

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6
Q

When is the use of speed brakes prohibited?

A
  • Flaps 39

- Gear down in flight

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7
Q

Tire speed limit

A

195.5 kts ground speed

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8
Q

Maximum speed for extension of the landing gear (Vlo)

A

Vlo - 225 kcas/ .70 Mach

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9
Q

The APU is guaranteed to start below ______feet?

A

39,000’

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10
Q

Maximum altitude for engine airstart?

A

25,000’

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11
Q

Maximum speed for landing gear extended flight? (Vle)

A

Vle 250 kcas / .70 mach

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12
Q

Maximum permitted cabin pressure differential in flight?

A

10.48 psi

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13
Q

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

A

0.3 psi

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14
Q

Maximum crosswind and tailwind for engine start?

A

crosswind - 30 kts

tailwind - 20 kts

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15
Q

Use cowl anti-ice for taxi and takeoff when SAT is ___°C or below in visible moisture.

A

+10°C

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16
Q

When is automatic cowl and wing anti-ice inhibited during takeoff and climb out?

A
  • Below 1500 AGL

- Above 35,000’ MSL

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17
Q

Thrust reversers should be at idle by ____ kts.

A

60 kts

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18
Q

Turbulent air penetration speed

A
  • Above 10,000’ – 270 kts / 0.80 MT

- Below 10,000’ – 240 kts

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19
Q

Maximum cabin window ground time?

A

10 minutes

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20
Q

Minimum bleed air pressure for engine start.

A

40 psi

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21
Q

Maximum and minimum fuel tank temperature?

A

max – +54°C

min – -35° to -36°C

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22
Q

Maximum TGT to initiate engine ground start?

A

150° C

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23
Q

Maximum RPM for the APU?

A

106%

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24
Q

Maximum running TGT for the APU?

A

732°C

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25
Q

Radar operating limitations

A
  • not within 300’ of refueling ops

- not within 49’ of ground personal

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26
Q

Maximum Altitudes for:
Flaps 10° or 20°
Flaps 39°
Gear extended

A

Flaps 10° or 20° 25,000’
Flaps 39° 20,000’
Gear Extended 20,000’

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27
Q

Minimum battery voltage to start the APU?

A

22 volts

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28
Q

Maximum charge for the main batteries?

A

38 amps

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29
Q

Maximum Landing Field Elevation

A

14,500’

30
Q

Maximum speed for alternate extension of the landing gear. (Operation of the emergency gear handle)

A

175 kcas / 0.70 MT

31
Q

What cabin altitude will cause the passenger oxygen masks to drop?

A

14,750 (+/- 250’) cabin altitude

32
Q

Maximum tailwind for landing

A

10 knots

33
Q

Maximum Demonstrated Crosswind

A

28 knots

34
Q

Occupant Limit

A

22 total
19 pax
3 crew

35
Q

Maximum Reverse time limit:

A

30 seconds

36
Q

Maximum Flap Extended Speed (Vfe) for:

  • 10° Flaps
  • 20° Flaps
  • 39° Flaps
A

Flaps 10° - 250 kcas
Flaps 20° - 220 kcas
Flaps 39° - 170 kcas

37
Q

Maximum and minimum engine fuel temperature:

A
  • 40°C / 140°C

* fuel temp up to 165°C for 15 minutes is allowed

38
Q

When do you need an evacuation specialist?

A

10 or more passengers

39
Q

Thrust reverser deploy in flight speed

A

200 knots

40
Q

Maximum altitude for single pack operations.

A

48,000’

41
Q

Maximum altitude to enter the baggage compartment single pack.

A

45,000’

42
Q

APU maximum operating altitude.

A

45,000’

*100% electrical load capability at 45,000’

43
Q

Maximum demonstrated altitude lose for a coupled go-around.

A

60’

44
Q

HMG limitations

A
  • Do no operate the HMG when normal AC power is available

- Move speed brakes slowly (3 seconds to full)

45
Q

Limit baggage door open to 5 minutes above _____ feet.

A

40,000’

46
Q

Engine crosswind takeoff limitation.

A
  • For crosswinds > 20 knots
  • LP is limited to 66% until 20 knots groundspeed, then slam acceleration is required (engage auto throttles)
  • Add 600’ to required field length
47
Q

Maximum altitude for Yaw Damp inop.

A

45,000’

48
Q

Minimum speed for holding in icing conditions

A

160 knots

49
Q

Minimum control speed

  • Vmca (air)
  • Vmcg (ground)
A
  • Vmca 112 kias

- Vmcg 107 kias (at sealevel)

50
Q

Anti-Skid Inop Limitation for takeoff

A

Takeoff with anti-skid inop if:

  1. Dry runway
  2. Ground spoilers operative
  3. 20° Flaps takeoff
  4. No cowl or wing anti-ice
51
Q

Ground Spoiler Inop limitation for takeoff

A

Takeoff with ground spoiler inop if:
1. Anti-skid operative
2 Flaps 20° takeoff
3. No cowl or wing anti-ice

52
Q

Max start TGT for the APU

A

1050°C

53
Q

Max engine TGT on Start
Air?
Ground?

A

Air - 850°C

Ground - 700°C

54
Q

Starter may be re-engaged up to ____ % HP?

A

42% HP

55
Q

Maneuvering Speed

Va

A

206 knots

56
Q

Do not turn off the fuel pumps if the fuel tank temp is below _____?
Why?

A
  • 0°C

- Fuel jelling my cause pumps to fail if they are shut down

57
Q 
---Flight Load Limits---
  Flaps 0°
  Flaps 10° or 20°
  Flaps 39° (Below 75,300 lbs)
  Flaps 39° (Above 75,300 lbs)
A

Flaps 0° — -1.0 to 2.5 G’s
Flaps 10° or 20° — 0 to 2.0 G’s
Flaps 39° < 75,300 lbs — 0 to 2.0 G’s
Flaps 39° > 75,300 lbs — 0 to 1.5 G’s

58
Q

Engine Starter Cycle Limits

A
  • 3 start attempts (3 minutes max per attempt)
  • Delay 15 seconds between cycles
  • After the 3rd cycle, delay use of starter for 15 minutes
59
Q

APU Starter Cycle Limits

A
  • on batteries
    • 3 start attempts then 1 hour cool down
  • on DC power cart
    • 15 minute cool down between start attempts
    • 1 hour cool down after 3rd attempt
  • Limit 6 starts @ 10 minute intervals
60
Q

TR limitations

A
  • Ground use only
  • Allowed for taxi
  • Be at idle by 60 knots upon landing
  • Max 70% during landing rollout
  • Power back not approved
61
Q

Engine Static Run Limitation

A
  • No stabilized engine operation, while on the ground, between 66% to 80% LP.
  • Acceleration or deceleration between must not exceed 10 seconds.
62
Q

Auto Pilot Limitations for takeoff and landing.

A
  • Takeoff - on above 200’ agl
  • Landing - off above 60’ agl
  • IMC VNAV coupled approach off by 300’ agl or 50’ below MDA (whichever is higher)
63
Q

Crew and passenger masks are approved up to what altitude?

A
  • Crew - 40,000’ cabin altitude

- Passenger - 25,000’ cabin altitude

64
Q

Minimum oil temp for takeoff.

A

20°C

65
Q

Minimum oil temp to start the engines.

A

-30°C

66
Q

Maximum oil temp.

A

160°C

67
Q

Minimum oil pressure for takeoff

A
  • > 90% HP 45 psi

- < 72.3% HP 35 psi

68
Q

Engine Limit

Max takeoff

A
  • LP 101.1%
  • HP 99.6%
  • TGT 900°C
  • 5 minute limit (2 engine)
  • 10 minute limit (single engine)
69
Q

Engine Limit

Max Continuous

A
  • LP 101%
  • HP 98.9%
  • TGT 860°C
  • No time limit
70
Q

Engine Limit

Max Overspeed

A
  • LP 101.5%
  • HP 99.8%
  • TGT 905°C
  • 20 second time limit
71
Q

Engine Limit

Max Reverse

A
  • LP 70%

- 30 seconds time limit

72
Q

Yaw Damp Inop Max/Min Speeds

  • Below 10,000’
  • Above 10,000’
  • Below 20,000’
  • Above 20,000’
A
  • Below 10,000’ 250 KCAS Max
  • Above 10,000’ 260 KCAS/0.80 MT Max
  • Below 20,000’ see AOM
  • Above 20,000’ 210 KCAS Minimum

G550 (2 decks)

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