13.10
13.10
Continued from previous page
----------------------------DEFERRED ITEMS ------------------------------
==> APPROACH
Altimeters . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ___
ALTERNATE FLAPS master
switch (230 knots maximum) . . . . . . . . . . . . . . . . . . . . . . ARM
Note: Asymmetry protection is not provided when the
alternate flap extension system is used.
Flap lever . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Set
During flap extension, set flap lever to next desired flap
position.
ALTERNATE FLAPS position
switch (230 knots maximum) . . . . . . . . . . . . . . . . . . . . .DOWN
Hold down to extend flaps to 15 on schedule. As flaps are
extending, slow to respective maneuvering speed.
Release switch if trailing edge flap asymmetry is detected
during extension.
Note: The LE FLAPS TRANSIT light will remain illuminated
until the flaps approach the flaps 10 position.
Note: On speed tape equipped airplanes, operation within
the lower yellow airspeed band may be needed until
the LE FLAPS TRANSIT light extinguishes.
Continued on next page
June 3, 2005
737 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
13.11
13.11
Continued from previous page
----------------------------DEFERRED ITEMS ------------------------------
==> LANDING
Landing gear lever . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
Manual gear extension handles . . . . . . . . . . . . . . . . . . . . . Pull
[The uplock is released when the handle is pulled to its limit. The related
red landing gear indicator light illuminates, indicating uplock release.]
Wait 15 seconds after the last manual gear extension handle
is pulled:
Landing gear lever . . . . . . . . . . . . . . . . . . . . . . . . . . .DOWN
ENGINE START switches . . . . . . . . . . . . . . . . . . . . . . . . CONT
Landing gear. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .DOWN
Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 15, green light
Condition: The standby hydraulic LOW PRESSURE light
illuminated indicates output pressure of the standby
pump is low.
Note: With a loss of hydraulic system A and B, the rudder is
inoperative.
Condition: The standby hydraulic LOW QUANTITY light
illuminated indicates low quantity in the standby
hydraulic reservoir.
STANDBY HYDRAULIC LOW PRESSURE
STANDBY HYDRAULIC LOW QUANTITY
June 3, 2005
737 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
13.12
13.12
Intentionally
Blank
June 3, 2005
737 Flight Crew Operations Manual
Non-Normal Checklists Chapter NNC
Landing Gear Section 14
Copyright © The Boeing Company. See title page for details.
TOC.14.1
Table of Contents
NNAC.N14T NIoSn-KNoIDrm aIlN COhecPkElisRtsA-LTanIdVinEg G e.a r. . . . . . . . . . . . . . . . . . . . . . . . . . . . 14.1
AUTO BRAKE DISARM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14.1
BRAKE PRESSURE INDICATOR ZERO PSI . . . . . . . . . . . . . . . 14.1
GEAR LEVER WILL NOT MOVE UP AFTER
TAKEOFF . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14.2
LANDING GEAR LEVER JAMMED IN THE UP
POSITION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14.5
< LANDING GEAR LEVER JAMMED IN THE UP
POSITION > . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14.8
MANUAL GEAR EXTENSION . . . . . . . . . . . . . . . . . . . . . . . . . 14.12
PARTIAL OR GEAR UP LANDING . . . . . . . . . . . . . . . . . . . . . 14.14
WHEEL WELL FIRE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14.16
June 3, 2005
737 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
TOC.14.2
Non-Normal Checklists -
Landing Gear
Intentionally
Blank
June 3, 2005
737 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
14.1
14.1
NNC.14 Non-Normal Checklists-Landing Gear
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