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Maximum Takeoff and Landing Tailwind Component
10 kts
Maximum speeds - VMO / MMO?
340 / .82
Turbulence Penetration Speed?
280 / .76.
Maximum Operating Altitude?
41,000 ft.
maximum cabin differential pressure?
9.1 psi.
With engine bleed air switches ON, do not operate the air conditioning packs in
HIGH for?
takeoff, approach or landing..
Engine TAI must be on when icing conditions exist or are anticipated-
except during
climb and cruise below -40°C SAT. Engine anti-ice must be on prior to and during
descent in all icing conditions, including temperatures below -40°C SAT.
Icing Conditions exist when the OAT on the ground and for takeoff, or TAT
inflight is 10°C or below and-
visible moisture in any form is present (such as
clouds, fog with visibility of one mile or less, rain, snow, sleet and ice
Icing conditions also exist when the OAT on the ground and for takeoff is
10°C or below when-
operating on ramps, taxiways or runways where surface
snow, ice, standing water, or slush may be ingested by the engines or freeze
on engines or nacelles.
Do not rely on airframe visual icing cues to turn engine anti-ice on-
Delaying the use
of engine anti-ice until ice buildup is visible from the cockpit may result in severe engine
Do not operate wing anti-ice on the ground when-
OAT is above 10 degrees C.
Do not engage the autopilot on takeoff below-
500 feet AGL.
For single channel operation, the autopilot shall not remain engaged below-
50 feet
For non-precision approaches, the autopilot must be disengaged no lower than-
applicable minimums minus 50 feet.
Use of aileron trim with the autopilot engaged is -
approaches below Cat I will be flown-
using autoland with the Capt as the PF.
25 knots
20 knots (15 knots for lower than Category I minimums)
10 knots.
Autoland capability may only be used with -
flaps 30 and 40 with both engines
Max Taxi
Max Takeoff
Max Landing
Max zero fuel
Do not use VHF–3 for ATC communications-
with ACARS operational.
On the ground, limit one engine driven generator operation to -
a maximum of 75 KVA
(215 amps).
Maximum and minimum limits are -
marked by a red line.
Cautionary range is marked by -
an amber arc.
Normal operating range is marked by
a white arc.
Engine ignition must be on for-
operation in heavy rain
Limit each start attempt to a maximum of 2 minutes  A minimum of
10 seconds is required between start attempts.
Intentional selection of reverse thrust in flight is -
Takeoffs with EEC’s in the Alternate mode is allowed if:-
No Derate or Assumed temperature thrust is used, and
Both EEC’s are selected to the Alternate mode.
APU bleed + electrical load: max alt -
10,000 ft.
APU bleed: max alt -
17,000 ft.
APU electrical load: max alt -
41,000 ft.
APU bleed valve must be closed when:
-ground air connected and isolation valve open
- engine no. 1 bleed valve open
- isolation and engine no. 2 bleed valves open.
APU bleed valve may be open during engine start, but -
avoid engine power above
Do not start or shut down APU during -
refueling operations.
Do not deploy the speedbrakes in flight -
at radio altitudes less than 1,000 feet.
In flight, do not extend the SPEED BRAKE lever beyond the -
QFE selection is -
Do not operate weather radar during -
fueling, near fuel spills or people.
Fuel tanks can be loaded individually, simultaneously, or in any sequence. Main
wing tanks must be scheduled to be full if -
the center wing tank contains more than
1,000 pounds of fuel.
Allowable lateral imbalance between main tanks 1 and 2 must be scheduled to be-.
Random fuel imbalance must not exceed -
1000 lbs for taxi, takeoff, flight or
Intentional dry running of a center tank pump (low pressure light illuminated) is-
Do not apply brakes until after -
Max flap extension altitude is -
20,000 ft.
Holding in icing conditions with flaps extended is -
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