Boeing 737 - Page 122

737 Operations Manual
Performance Inflight -
Advisory Information
737-400/CFM56-3_23.5K
Copyright © The Boeing Company. See title page for details.
PI.22.2 D6-27370-400E-TBCE
ADVISORY INFORMATION
Advi sory In formati on
Non-Normal Configuration Landing Distance
Dry Runway
LANDING DISTANCE AND ADJUSTMENTS (FT)
REFERENCE
DISTANCE
FOR 48000 KG
LANDING WEIGHT
WT ADJ
PER 2000 KG
ABOVE/BELOW
48000 KG
ALTITUDE ADJ
PER 1000 FT
ABOVE S.L.
LANDING CONFIGURATION
APPROACH
SPEED
ONE ENGINE
INOPERATIVE
VREF15 2900 200 / -90 190
ANTI-SKID INOPERATIVE VREF40 3920 110/-110 90
HYDRAULIC SYSTEM A
INOPERATIVE
(FLAPS 15)
VREF15 3450 150 / -100 190
HYDRAULIC SYSTEM A
INOPERATIVE
(FLAPS 30)
VREF30 3280 100/-90 130
HYDRAULIC SYSTEM A
INOPERATIVE
(FLAPS 40)
VREF40 3190 90/-90 130
HYDRAULIC SYSTEM B
INOPERATIVE
(FLAPS 15)
VREF15 3200 210 / -100 200
HYDRAULIC SYSTEMS
A & B INOPERATIVE
(MANUAL REVERSION)
VREF15 5120 210 / -170 260
LEADING EDGE
ASYMMETRY OR
FAILURE
VREF15+5 3030 200 / -80 200
TRAILING EDGE
FAILURE
(FLAPS LESS THAN 1)
VREF40+40 3480 250 / -120 250
TRAILING EDGE
FAILURE
(FLAPS GREATER THAN 1
AND LESS THAN 15)
VREF40+30 3200 210 / -110 210
FLAPS UP VREF40+55 3950 300 / -160 340
JAMMED STABILIZER VREF15 2820 180 / -80 160
Actual (unfactored) distances are shown
Includes distances from 50 ft above threshold (1000 ft of air distance)
Assumes maximum manual braking and maximum reverse thrust when available on operating engines.
June 07, 2002