Boeing 737 - Page 188

737 Operations Manual
Performance Inflight -
Advisory Information
737-500/CFM56-3_20K
Copyright © The Boeing Company. See title page for details.
PI.32.2 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 2800 150 / -80 150
ANTI-SKID INOPERATIVE VREF40 3840 110/-110 90
HYDRAULIC SYSTEM A
INOPERATIVE
(FLAPS 15)
VREF15 3270 90 / -90 160
HYDRAULIC SYSTEM A
INOPERATIVE
(FLAPS 30)
VREF30 3220 90/-90 130
HYDRAULIC SYSTEM A
INOPERATIVE
(FLAPS 40)
VREF40 3150 80/-90 130
HYDRAULIC SYSTEM B
INOPERATIVE
(FLAPS 15)
VREF15 3100 150 / -90 160
HYDRAULIC SYSTEMS
A & B INOPERATIVE
(MANUAL REVERSION)
VREF15 4800 130 / -150 210
LEADING EDGE
ASYMMETRY OR
FAILURE
VREF15+5 2950 150 / -70 160
TRAILING EDGE
FAILURE
(FLAPS LESS THAN 1)
VREF40+40 3520 210 / -110 200
TRAILING EDGE
FAILURE
(FLAPS GREATER THAN 1
AND LESS THAN 15)
VREF40+30 3260 190 / -90 170
FLAPS UP VREF40+55 4000 260 / -140 260
JAMMED STABILIZER VREF15 2760 140 / -70 140
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