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procedures have been accomplished, exceeding 270 KIAS is permissible only
until the next application of Type II or Type IV deicing / anti-icing fluids.”
Note:
· Aircraft is restricted to a maximum of 270 KIAS after Type II or Type IV
fluid application. No MACH restriction.
· Flight Plan Release (amended if required) displays 270-knot restriction.
· Restriction remains in effect for all flights until elevator tab surfaces are
cleaned of Type II or Type IV fluids.
· It has been determined that Type I fluid does not affect the flight
controls of the aircraft. If only Type I fluid is used for deicing / antiicing,
the speed restriction is not applicable.
Caution: Flight Crews will evaluate the need to land at the nearest
suitable airport if in-flight vibrations (ELEVATOR TAB LIMIT
CYCLE OSCILLATION) occur as a result of de-icing.
737 Sec. 3 Page 91
Flight Manual Continental Rev. 11/15/02 #41
The Captain will:
· While holding the tiller securely, smoothly and slowly displace the
rudder full travel in each direction, verifying full travel and freedom
of movement. Ensure that the rudder pedals return to the neutral
position and that no abnormal nosewheel steering pressures are
noted unless required by a single engine taxi situation.
The First Officer will:
· Smoothly and slowly displace the control wheel and the control
column full travel in each direction, verifying full travel and freedom
of movement.
· If the aircraft has been deiced and exterior deicing checklist has not been
accomplished:
The control column will be smoothly and slowly cycled from the full
aft to the full forward position a minimum of three times to minimize
the residual fluids in the balance bay during flight.
Speedbrake Lever.....................................................DOWN DETENT (F, C)
The First Officer will:
· Visually confirm that the speedbrake lever is full forward and that
the Captain has physically checked the speedbrake lever is seated
in the down detent.
The Captain will:
· Physically check the speedbrake lever is seated in the down
detent. The speedbrake lever may visually appear to be in the
down detent, but may not be completely stowed. This will cause a
takeoff warning when throttles are advanced for takeoff.
Flaps ......................................................SET ______, GREEN LIGHT (F, C)
This response refers to the flap setting from the ACCULOAD, the flap
position indicator and handle. Verify that the green LE FLAP light is
illuminated. The Captain will also verify the correct flap setting and will
verbally respond “SET ______, GREEN LIGHT.”
Autobrake................................................................................................... RTO
CDU / Airspeed Bugs ...................................................................... SET (F, C)
Verify all required entries are made to the FMC.
· V1, VR, and V2 should be set on the TAKEOFF REF page.
· Insure the departure runway has been selected on the ROUTE page.
· If VNAV is the pitch mode desired for departure insure entry of
appropriate climb restrictions and speed.
Sec. 3 Page 92 737
Rev. 11/15/02 #41 Continental Flight Manual
· Reduced thrust temperature if appropriate is entered on the N1 LIMIT
page.
· Verify that the TAKEOFF REF page shows PREFLIGHT COMPLETE.
>>@ External (White) Airspeed Bugs
Position the white movable reference bugs at V1, VR, and V2 + 15, and VM
Flaps 0 for the appropriate weight, i.e.; 210 knots if 117,000 lbs. or less
and 220 knots if more than 117,000 lbs.
BCD Reference Speed Bugs
Select AUTO on the speed reference selector. When gross weight and
V-speed entries are made on the CDU V1, VR, V2 + 15, and VM Flaps 0
speed bugs will be displayed. If the FMC is inoperative, enter the
V-speeds manually using the speed reference selector.
Airspeed Cursor
Set the airspeed cursor at V2 using the speed selector on the mode control
panel.
Flight Inst (Flow) ................................................................CHECKED (F, C)
· Check that navigation equipment is operating properly.
1. >>@ Ensure that the AUTO-MANUAL switches on the VHF
NAV radios are set as appropriate for the type of departure.
2. BCD Ensure the appropriate position of the TFR switch.
· Verify that the MCP courses, altitude, heading, and V2 speed are set for the
departure.
· Warning flags should be out of view.
· Confirm N1 and airspeed bugs have been set.
· Pitch and roll attitude information on the (E)ADI and standby horizon
　
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