287,000 kg

286,000 kg

224,300 kg

223,000

209,200 kg

116,600 kg

• N1 110%
• N2 110%

872c

585c

• 2 start attempts
• 10 min rest
• 2 start attempts
• 1 hour rest

Throttle........Idle

• Do not operate on a DRY windshield.
• Do not operate at HIGH speed for more than 30 min.

Auto ground spoilers must be operative for T/O

Except when aircraft operation is based on auto ground spoilers inoperative Appendix

ENG ANTI-ICE switches must be turned on when An ICE DETECTED alert is Displayed from the ice detection system.

And

• Any time icing conditions are expected.
• Ice is expected when the air temperature is at or below 6*c and either moisture is visible or outside temp and dew point are within 3*c of each other.

When on the OAT on the ground for takeoff is at or below 6*c and visible moisture is present.

In flight Total air temperature (TAT) IS AT OR BELOW 6*C and visible moisture is present.

Flashing, cargo, fire Agent, discharge switch...push

ENGINE 2 Throttle....................................IDLE

• Oxygen mask...........On/100%
• Outflow valve........... verify closed

WARNING: Establish control of the aircraft through pitch / thrust relationship. Disregard all alerts and warnings, except stick shaker, until after the aircraft is stabilized and safe operations achieved.

• AFS OVRD and FD switches............OFF
• Aircraft pitch/thrust:
• FLAPS AND/OR SLATS EXTENDED:........10* AND 90% N1
• FLAPS AND SLATS UP:.........................4* AND 90% N1

• Throttles.....................................MCT
• Flaps (unless on final)...............up
• Speed(U O F)..........Driftdown or UP/RET Vmin +30

If a second engine fails on final and the gear is down.

• FLAPS.......................................... 28*
• Speed........................................... Flaps 28 Vref +5
• GPWS switch .............................. FLAP OVRD

• ENG IGN OVRD Switch....................... OVRD ON
• ADG...................................................... DEPLOY

The windshield ANTI-ICE selector SHOULD be in High only for the duration of moderate to heavy icing.

Two___channels must be operative for takeoff and must originate from a COMMON flight control computer.

Anti-skid must be operative for Take OFF.

Except when the aircraft operation is based on the Anti-skid inoperative Appendix.

USED only in the zero degree flat configuration with or without flaps extended.

9.1 psi

.5 PSI

Unpressured flight must be conducted with the cabin pressure control in MANUAL and the outflow valve between 1/2 to 2/3 open.

• Maximum lateral fuel imbalance between
• Tank 1 and Tank 3 is 1100 kg

Ballast fuel may only be loaded into:

• *Main tank 2
• *Upper aux tank
• *Tail tank

Ballast fuel may not be loaded in more than one tank at the same time.

Tank 2 is limited to a maximum of 11,300 kg.

• Fuel density must be within the range of:
• .72 to .85 kg/Lt.........fuel temp -40c to 50c

When CG is equal to or forward of 22% MAC:

MTOGW must be reduced by 1134 kg For each .01 kg/Lt of fuel density below .78 kg/Lt when the CG is equal to or forward of 22% MAC.

System 3 minimum hydraulic quanity for dispatch:

6 gallons

Do not interconnect 2 or more active engine pneumatic supply systems.

Use of reverse thrust is prohibited in flight

Ignition OVRD should be used for flame out protection during severe turbulence and/or heavy rain.

• Max N1 RPM 117.5%
• Max N2 RPM 112.5%

• 750c no time limit
• 750c - 870c 40 seconds

Log book entry is required when EGT exceeds 750c during start

925c

960c 5 min

9.5 PSID

• 160c cont
• 160c - 175c 15 min

• Two 5 min starts with 2.5 min cooling each time
• Then 10 min break for an additional 5 min start

• Normally reengagement should be made when N2 below 20%.
• In an emergency, reengagement may be made when N2 is as high as 30%.
• DO NOT ENGAGE STARTER When N2 is above 30%

Test