LIMITATIONS (Global Express & Global XRS)

Question 1

Max Take Off Weight

MTOW

Answer 1

Classic & XRS -

99500 pounds

98000

96000

95000

93500

5000 -

92500

89700

88700

87700

Question 2

Max Ramp Weight

MRW

Answer 2

Classic & XRS -

99750 pounds

98250

96250

95250

93750

**5000 - **

92750

89950

88950

87950

Question 3

Max Landing Weight

MLW

Answer 3

78600 pounds

Question 4

Max Zero Fuel Weight

MZFW

Answer 4

56000 pounds

Question 5

Minimum Operating Empty Weight

Answer 5

Classic & XRS - 45000 pounds

5000 - 48000

Question 6

Max Takeoff/Landing Pressure Altitude

Answer 6

10000’

13700’ IAW Supplement 20

Question 7

Max Operating Altitude

Answer 7

51000’

Question 8

Max Ambient Air Temp for Takeoff/Landing

Answer 8

+50°C (+122°F) at Sea Level

see AFM page 02-04-2

Question 9

Min Ambient Air Temp for Takeoff

Answer 9

-40°C (-40°F)

Question 10

Icing Conditions

Answer 10

In flight at TAT 10°C (50°F) or below, and visible moisture in any form, except when SAT -40°C or below

Question 11

COWL Anti Ice

Ground

Answer 11

During Takeoff use of AUTO mode is PROHIBITED.

Must be ON when OAT is 10°C or below with visible moisture, or on contaminated runway.

Question 12

COWL Anti Ice

Flight

Answer 12

Must be ON when in icing conditions, or when ICE is annunciated.

Question 13

WING Anti Ice

Ground

Answer 13

During Takeoff use of AUTO mode is PROHIBITED.

Must be ON when OAT is 5°C or below with visible moisture, or on contaminated runway.

When Type II or IV fluids are used, must be ON, if required, just prior to thrust increase for takeoff.

Question 14

WING Anti Ice

Flight

Answer 14

Must be ON when in icing conditions, or when ICE is annunciated.

Do not hold in icing conditions with slats extended.

Minimum engine speed of 76% N2.

Question 15

Max runway slopes for Takeoff/Landing

Answer 15

+2% uphill and -2% downhill

Question 16

Max Tailwind for Takeoff/Landing

Answer 16

10 knots

Question 17

Max Tailwind for a HUD/CAT II approach

Answer 17

11 knots

Question 18

Approach with glide-path angle > 4.5°

Answer 18

PROHIBITED

Question 19

Approach with glide-path angle > 3.5°

Answer 19

IAW Supplement 29 (see AFM)

Question 20

Frost adhering to underside of wing

Answer 20

Takeoff is permitted if it was caused by cold soaked fuel IAW FCOM Vol 1 Chap 7.

Question 21

Max ITT Start

Ground

Flight

Answer 21

700° (ground)

850° (flight)

Question 22

Min N2 idle

Answer 22

58.0%

Question 23

Max ITT Idle

Answer 23

860°

Question 24

Max ITT Takeoff

Answer 24

900°

Takeoff thrust for 5 minutes with all engines, takeoff thrust for 10 minutes with engine failure

Question 25

Max ITT Continuous

Answer 25

860°

Question 26

Max ITT 20 seconds

Answer 26

905°

Question 27

Min N2 Idle

Answer 27

58.0%

Question 28

Static ground operation

Answer 28

66% to 80% N1 is PROHIBITED except for reverse thrust.

Question 29

Max N2 Takeoff

Answer 29

99.6%

Question 30

Max N2 Continuous

Answer 30

98.9%

Question 31

Max N2 20 seconds

Answer 31

99.8%

Question 32

Max N1 Takeoff

Answer 32

102.0%

Question 33

Max N1 Continuous

Answer 33

102.0%

Question 34

Max N1 20 seconds

Answer 34

102.5%

Question 35

Max N1 Reverse thrust

Answer 35

70.0% (30 seconds)

Question 36

Minimum Oil temp for starting engines

Answer 36

-40°C

Question 37

Minimum Oil temp before accelerating above idle

Answer 37

+20°C

Question 38

Max engine Oil temp

Answer 38

+160°C

Question 39

Max Oil Consumption per engine

Answer 39

.21 quarts per hour max

Question 40

Oil Replenishment

Answer 40

PROHIBITED when OAT less/equal to -12°C

Question 41

Shut down or Start abort Oil pressure

Answer 41

25 psi minimum