Global 6500 - Limits Flashcards

1
Q

Buoyancy Limitations

Takeoff on runways near bodies of water &
For takeoff weights above the maximum landing weight…

A

OUTFLOW VLV 2 must be closed and one air-conditioning pack must be shutdown for takeoff.

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2
Q

Buoyancy Limitations

Landing on runways near bodies of water &
For forced / emergency landing at weights above the maximum landing weight…

A

OUTFLOW VLV 2 must be closed and on air-conditioning pack must be shutdown for landing.

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3
Q

Maximum airport pressure altitude for takeoff and landing

A

10,000 feet

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4
Q

Maximum operating altitude

A

51,000 feet

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5
Q

Maximum ambient air temperature approved for takeoff and landing

A

+50° C (122° F)

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6
Q

Minimum ambient temperature approved for takeoff

A

-40° C (-40° F)

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7
Q

During takeoff, use of cowl anti-ice in AUTO mode is __________.

A

Prohibited

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8
Q

The cowl anti-ice system must be ON when the OAT is ____ or colder and visible moisture in any form is present.

A

10° C

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9
Q

During takeoff, use of the wing anti-ice system in AUTO is __________.

A

Prohibited

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10
Q

The wing anti-ice system must be ON for takeoff when the OAT is ____ or colder and visible moisture in any form is present.

A

5° C

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11
Q

The wing anti-ice system must be _____ when in icing conditions, or when ICE is annunciated by the ice detection system.

A

ON

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12
Q

During single bleed operation, the wing anti-ice system must be selected OFF when above _____.

A

41,000 feet

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13
Q

When in icing conditions, the minimum engine speed N2 limit is:

A

7,000 feet pressure altitude and below: 75.5%
14,000 feet pressure altitude and above: 79.0%

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14
Q

The maximum runway slopes approved for takeoff and landing are:

A

+2% uphill
-2% downhill

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15
Q

The maximum tailwind component approved for takeoff and landing:

A

10 knots

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16
Q

Operations from unprepared (i.e. gravel, grass, etc.) runways are _____________.

A

Prohibited

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17
Q

ITT Limits:

A

Start: 700° C (on ground), 850° C (in flight)
Idle: 850° C
Takeoff: 890°C (Takeoff thrust for 5 minutes AEO), 900° C (2 min for takeoff/Go-around only)
Max Continuous: 850° C
20s transient: 915° C

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18
Q

N1 Limits

A

Takeoff: 102.1%
Max Continuous: 102.1%
20s transient: 103.3%
Reverse Thrust: 70.4%

19
Q

N2 Limits

A

Idle: 58.2%
Takeoff: 101.6%
Max Continuous: 99.9%
20s transient: 102.8%

20
Q

Static ground operations in the range of _______ to _______ N1 is prohibited. Acceleration/deceleration thru this range is permitted.

A

66% to 80% N1

21
Q

N1 Fan operation in the caution area range between and is permitted with no limitations.

A

100% and 102.1%

22
Q

Engine operation in FZFG is prohibited.

23
Q

Wind speed limits: Starting

A

Crosswind: 35 knots
Tailwind: 20 knots

24
Q

Wind speed limits: Static Ground

A

Crosswind: 15 knots
Tailwind: 10 knots

25
Q

Wind speed limits: Taxi

A

Crosswind: 35 knots
Tailwind: 20 knots

26
Q

Wind speed limits: Takeoff

A

Crosswind: 20 knots (30 knots with N1 below 66%)
Tailwind: 10 knots

27
Q

Starter Cranking limits: Normal Engine Start

A

3 consecutive cycles of 3 minutes each with 15 seconds cooling between cycles (aka, 3 min on, 15 seconds off)

After 3 attempts, a 15-minute cooling period is required.

28
Q

Fuel Imbalance: On ground

A

Below 20,250lbs of fuel: 1100 lb
Above 20,250lbs of fuel: 600 lb

29
Q

Usable Fuel Load (pressure refuel)

A

Wing: 15,050 lb each
Center: 12,700 lb
Aft: 2,300 lb
Total: 45,100 lb

30
Q

Usable Fuel Load (gravity refuel)

A

Wing: 13,850 lb each
Center: 11,150 lb
Aft: not available

31
Q

Takeoff with engine fuel temperature indications below is prohibited.

32
Q

Fuel crossfeed must be for takeoff and landing.

33
Q

Oil temperature limits:

A

Minimum for starting: -40° C
Minimum before accelerating above idle: +20° C
Maximum permissible: +160° C

34
Q

Oil pressure limits:

A

See FCOM Volume 2 Figure 02-05-7

35
Q

Oil consumption limit is US qt per hour.

36
Q

Operating Speeds: Slat/Flap Extended Speeds

A

Slats extended: 225 KIAS
Flaps 6’b0: 210 KIAS
Flaps 16’b0: 210 KIAS
Flaps 30’b0: 185 KIAS

37
Q

Operating Speeds: Landing gear extension / retraction

38
Q

Operating Speeds: Landing gear extended

39
Q

Flights at altitudes above with the landing gear extended is prohibited.

A

20,000 feet

40
Q

Operating Speeds: Tire Limit Speed

41
Q

Operating Speeds: Turbulence Penetration Speed

A

300 KIAS or 0.80 Mach maximum, whichever is lower

42
Q

Operating Speeds: Minimum Operating Limit Speed

A

Vmca in Takeoff: 88 KIAS
Vmcg: 82 KIAS
Vmcl in landing configuration: 87 KIAS

43
Q

Operating Speeds: RVSM Maximum Cruise Mach Number

44
Q

Maneuvering Limit Load Factors

A

Slats/Flaps retracted: -1.0G to +2.5G
Slats/Flaps extended: 0.0G to +2.0G