Boeing 737 - Page 317

737 Operations Manual
Non-Normal Checklists -
Engines, APU
Copyright © The Boeing Company. See title page for details.
D6-27370-400E-TBCE NNC.7.21
Continued from previous page
If additional go–around thrust is desired, below 10,000 feet
configure the pressurization system for a no engine bleed
landing:
ISOLATION VALVE SWITCH . . . . . . . . . . . . . . . . . . . CLOSE
ENGINE No. 1 BLEED AIR SWITCH . . . . . . . . . . . . . . . .OFF
APU BLEED AIR SWITCH . . . . . . . . . . . . . . . . . . . . . . . . .ON
Do not open the APU bleed valve if the engine fire
warning switch remains illuminated.
LEFT PACK SWITCH . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO
ENGINE No. 2 BLEED AIR SWITCH . . . . . . . . . . . . . . . .OFF
ALTIMETERS AND
INSTRUMENTS . . . . . . . . . . . . . . . . . . . . . SET & X–CHECKED
N1 AND IAS BUGS . . . . . . . . . . . . .CHECKED & SET, VREF 15
GROUND PROXIMITY FLAP
INHIBIT SWITCH. . . . . . . . . . . . . . . . . . . . . . . . . .FLAP INHIBIT
GO–AROUND PROCEDURE . . . . . . . . . . . . . . . . . . . . REVIEW
Accomplish normal go–around procedure except:
• Use flaps 1
• Maintain VREF 15 + 5 knots to flap retraction altitude
• Limit bank angle to 15 degrees until reaching VREF 15
+ 15 knots or minimum maneuver speed
• Accelerate to flaps 1 maneuvering speed prior to flap
retraction.
---------------------------- DEFERRED ITEMS ------------------------------
==> LANDING
ENGINE START
SWITCH (operating engine) . . . . . . . . . . . . . . . . . . . . . . . . .ON
RECALL. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKED
SPEED BRAKE . . . . . . . . . . . . . . . . . . ARMED, GREEN LIGHT
LANDING GEAR . . . . . . . . . . . . . . . . . . . . . . .DOWN, 3 GREEN
FLAPS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 15, GREEN LIGHT
June 07, 2002