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Maximum Takeoff and Landing Tailwind Component
10 kts
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Maximum Speeds
340kts / .82Mach
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Turbulence penetration speed
280 kts / .76 M
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Maximum operating altitude
41,000ft
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Maximum cabin differential pressure (relief valves)
9.1 psi
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With engine bleed air switches ON, DO NOT operate the air conditioning packs,
In High for takeoff, approach, or landing.
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Engine TAI must be on when icing conditions exist or are anticipated, except
during climbs and cruise below -40C SAT.
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Engine anti-ice must be on prior to and during descent
in all icing conditions, including temperatures below -40C
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Icing conditions exist when
OAT on the ground and for takeoff, or TAT in-flight is 10C 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 crystals)
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Icing conditions also exist when
the OAT on the ground and for takeoff is 10C or below when operation 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.
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Do not rely on airframe visual icing cures 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 damage
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Do not use wing anti-ice as a substitute for
ground de-icing /anti-icing and inspection procedures which are necessary to comply with operating rules
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Do not operate wing anti-ice on the ground
when the OAT is above 10C
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Do not engage the autopilot on takeoff below
500ft agl
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For single channel operation, the autopilot shall not remain engaged below
50ft agl
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For non-precision approaches, the autopilot must be disengaged no lower than
the applicable minimums minus 50ft.
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Use of aileron trim with the autopilot engaged is
Prohibited
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The Autopilot/flight director system has been certified for Cat II and IIIa Automatic Approach and Landing operations
However, the FAA allows certain IIIa equipped aircraft with fail passive systems to fly to a minimum of 600RVR (IIIb on the charts). This FAA approval for Airtran is stated in Ops Spec C060 (CatIII). All approaches below Cat I will be flown using autoland with the Capt as the PF.
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Crosswind
20kts (15kts for lower than Cat I mins)
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Max taxi weight
155,000lbs
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Max takeoff weight
154,500lbs
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Zero fuel wight
120,500lbs
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Do not use VHF-3 for ATC comm
with ACARS operational
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Do not use HF-1 during
fueling, defueling or near fuel spills
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Maximum and minimum engine limits are marked by
a red line
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Engine cautionary range is marked by
an amber arc
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Normal operating range is marked by
a white arc.
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EGT limits
- Takeoff: Red Line 5 minutes (950 deg)
- Max Continuous Thrust: Amber Arc (925 deg)
- Starting: Red Line (725 deg)
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Minimum Oil Pressure
- 13 psi
- If oil pressure is in the yellow band with takeoff thrust set, do not takeoff.
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Maximum Oil Temperature
- 155 deg C
- Max continuous operation is 140 deg C. Operation between 140C and 155C is limited to 45 minutes.
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Engine RPM
- N1 104.0% (104.7% 20 seconds)
- N2 105.0%
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Engine ignition must be on for operation in
heavy rain.
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Starter duty cycle
Limit each start attempt to a maximum of 2 nimutes
A minimum of 10 seconds is required between start attempts
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Intentional selection of reverse thrust in flight
is prohibited
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Takeoff with EEC's in the Alternate mode is allowed if
- No Derate or Assumed temperature thrust is used
- Both EEC's are selected to the Alternate mode
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APU bleed + electrical load max altitude
10,000ft
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APU bleed max altitude
17,000ft
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APU electrical load max altitude
41,000ft
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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
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APU bleed valve may be open during engine start but
avoid engine power above idle
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Do not start or shut down APU during
refueling operations
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Do not deploy the speedbrakes in flight at radio altitudes less than
1,000ft
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In flight do not extend the SPEED BRAKE lever
beyond the FLIGHT DETENT.
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QFE selected is
prohibited.
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Do not operate weather radar during
fueling, near fuel spills or people
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Fuel tanks can be loaded individually, simultaneously, or in any sequence. Main wing tanks must be scheduled to be full if
the center wing tanks contains more than 1,000lbs of fuel.
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Allowable lateral imbalance between main tanks 1 and 2 must be scheduled to be
zero
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Random fuel imbalance must not exceed
1000lbs for taxi, takeoff, flight or landing
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Intentional dry running of a center tank pump (low pressure light illuminated) is
Prohibited
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Do not apply brakes until after
touchdown
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Max flap extension altitude is
20,000ft
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Holding in icing conditions with the flaps extended is
Prohibited
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Use of assumed temperature reduced takeoff thrust is prohibited under the following conditions
- Contaminated Runway
- Anti-skid inoperative
- Wind-shear (known or suspected)
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Pilots are authorized to deviate from their current ATC clearance to the extent necessary to comply with
a TCAS II resolution advisory
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