[Autopilot/Flight Director System] # Do not engage the autopilot for takeoff
below 400 feet AGL
[Autopilot/Flight Director System] # Do not use LVL CHG...
on final approach below 1,000 feet AFE.
[Fuel] Center tank fuel qty (lbs)
28,973 lbs
[Engines and APU] # With APU bleed maximum altitude
17,000 ft
[Engines and APU] # Reverse Thrust
Intentional selection of reverse thrust in flight is prohibited
[Anti–Ice, Rain] # Engine Anti-Ice System - engine anti-ice system must be ON during all ground and flight operations when Icing Conditions exist or are anticipated, except...
during climb and cruise when Static Air Temperature (SAT) is below -40°C
[Engines and APU] Normal operating range is marked by...
a white arc.
[TCAS] Do not use the look-ahead terrain alerting and terrain display functions:
Within 15 nm of takeoff, approach or landing at an airport not contained in the GPWS terrain database
Which winds should be used for tailwind computations
Peak gust wind velocity.
[Engines and APU] APU bleed valve must be closed when:
• Ground air connected and isolation valve open
• Engine no. 1 bleed valve open
• Isolation valve and engine no. 2 bleed valve open
APU bleed valve may be open during engine start, but avoid engine power above idle
[Fuel] # Center tank fuel pumps must not be “ON” unless
personnel are available in the flight deck to monitor low pressure lights
[Engines and APU] Engine Ignition When flight in moderate or heavy rain, hail or sleet is encountered or anticipated except on short final when landing is assured the engine start switches must be set to
FLIGHT and a minimum of 45% N1 must be maintained
When crosswinds exceed 20 kts - which type of takeoff should be used?
Rolling takeoff
[RVSM] maximum allowable IN FLIGHT difference between Captain and First Officer altitude displays for RVSM operations.
200 feet
[Engines and APU] # Maximum Continuous EGT
925º C
[Weight Limits] Maximum Landing Weight
146,300 lbs
[Fire Protection] Aircraft must land within...
60 minutes after initial discharge of lower cargo fire suppression system.
[Engines and APU] Maximum N1 RPM
104%
[RVSM] maximum allowable ON THE GROUND altitude display differences for RVSM - [5,001 feet to 10,000 ft, Capt vs 10,000]
60 feet
[Engines and APU] Engine Ignition - engine start switches must be set to FLIGHT and a minimum of 45% N1 must be maintained
When flight in moderate or heavy rain, hail or sleet is encountered or anticipated except on short final when landing is assured
[Landing Gear] # Operation with assumed temperature reduced takeoff thrust is not permitted with...
anti-skid inoperative
Maximum flight operating latitude
82 North and 82 South *
[Fuel] Defueling or transferring fuel with passengers on board is
prohibited.
Flight Maneuvering Load Acceleration Limits Flaps Up
+2.5g to -1.0g
[Engines and APU] # Reduced Thrust - Use of assumed temperature reduced thrust procedures is not allowed when:
• The runway is contaminated with standing water, ice, slush, or snow
• With anti-skid inoperative
• With EEC is in Alternate mode
• The probability of windshear exists
[Flight Controls] # Avoid rapid and large alternating control inputs, especially...
in combination with large changes in pitch, roll, or yaw (e.g., large side slip angles) as they may result in structural failure at any speed, including below VA
[Flight Controls] # Do not deploy the speedbrakes in flight at
radio altitudes less than 1,000 feet.
[Fuel] Center tank fuel pumps must be “OFF” when:
• Center tank fuel is < 5,000 pounds and aircraft is readied for initial taxi
• Center tank fuel reaches approximately 1,000 pounds during climb
• Center tank fuel reaches 3,000 pounds during descent and landing
[Fuel] # Minimum fuel temperature
fuel freeze point of the fuel being used +3° C or –43° C, whichever is higher.
# Maximum Takeoff and Landing Tailwind Component
15 knots
