Global 6500 - Limits

Question 1

Buoyancy Limitations

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

Answer 1

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

Question 2

Buoyancy Limitations

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

Answer 2

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

Question 3

Maximum airport pressure altitude for takeoff and landing

Answer 3

10,000 feet

Question 4

Maximum operating altitude

Answer 4

51,000 feet

Question 5

Maximum ambient air temperature approved for takeoff and landing

Answer 5

+50° C (122° F)

Question 6

Minimum ambient temperature approved for takeoff

Answer 6

-40° C (-40° F)

Question 7

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

Answer 7

Prohibited

Question 8

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

Answer 8

10° C

Question 9

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

Answer 9

Prohibited

Question 10

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

Answer 10

5° C

Question 11

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

Answer 11

ON

Question 12

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

Answer 12

41,000 feet

Question 13

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

Answer 13

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

Question 14

The maximum runway slopes approved for takeoff and landing are:

Answer 14

+2% uphill
-2% downhill

Question 15

The maximum tailwind component approved for takeoff and landing:

Answer 15

10 knots

Question 16

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

Answer 16

Prohibited

Question 17

ITT Limits:

Answer 17

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

Question 18

N1 Limits

Answer 18

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

Question 19

N2 Limits

Answer 19

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

Question 20

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

Answer 20

66% to 80% N1

Question 21

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

Answer 21

100% and 102.1%

Question 22

Engine operation in FZFG is prohibited.

Answer 22

< -19° C

Question 23

Wind speed limits: Starting

Answer 23

Crosswind: 35 knots
Tailwind: 20 knots

Question 24

Wind speed limits: Static Ground

Answer 24

Crosswind: 15 knots
Tailwind: 10 knots

Question 25

Wind speed limits: Taxi

Answer 25

Crosswind: 35 knots Tailwind: 20 knots

Question 26

Wind speed limits: Takeoff

Answer 26

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

Question 27

Starter Cranking limits: Normal Engine Start

Answer 27

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.

Question 28

Fuel Imbalance: On ground

Answer 28

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

Question 29

Usable Fuel Load (pressure refuel)

Answer 29

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

Question 30

Usable Fuel Load (gravity refuel)

Answer 30

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

Question 31

Takeoff with engine fuel temperature indications below is prohibited.

Answer 31

5° C

Question 32

Fuel crossfeed must be for takeoff and landing.

Answer 32

OFF

Question 33

Oil temperature limits:

Answer 33

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

Question 34

Oil pressure limits:

Answer 34

See FCOM Volume 2 Figure 02-05-7

Question 35

Oil consumption limit is US qt per hour.

Answer 35

0.2

Question 36

Operating Speeds: Slat/Flap Extended Speeds

Answer 36

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

Question 37

Operating Speeds: Landing gear extension / retraction

Answer 37

200 KIAS

Question 38

Operating Speeds: Landing gear extended

Answer 38

250 KIAS

Question 39

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

Answer 39

20,000 feet

Question 40

Operating Speeds: Tire Limit Speed

Answer 40

196 knots

Question 41

Operating Speeds: Turbulence Penetration Speed

Answer 41

300 KIAS or 0.80 Mach maximum, whichever is lower

Question 42

Operating Speeds: Minimum Operating Limit Speed

Answer 42

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

Question 43

Operating Speeds: RVSM Maximum Cruise Mach Number

Answer 43

0.89

Question 44

Maneuvering Limit Load Factors

Answer 44

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