Boeing 737 - Page 52

737 Operations Manual
Performance Inflight -
Advisory Information
737-300/CFM56-3_22K
Copyright © The Boeing Company. See title page for details.
PI.12.2 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 160 / -80 140
ANTI-SKID INOPERATIVE VREF40 3920 120/-110 80
HYDRAULIC SYSTEM A
INOPERATIVE
(FLAPS 15)
VREF15 3250 120 / -80 150
HYDRAULIC SYSTEM A
INOPERATIVE
(FLAPS 30)
VREF30 3280 90/-100 130
HYDRAULIC SYSTEM A
INOPERATIVE
(FLAPS 40)
VREF40 3180 100/-90 130
HYDRAULIC SYSTEM B
INOPERATIVE
(FLAPS 15)
VREF15 3050 180 / -80 150
HYDRAULIC SYSTEMS
A & B INOPERATIVE
(MANUAL REVERSION)
VREF15 4900 170 / -150 230
LEADING EDGE
ASYMMETRY OR
FAILURE
VREF15+5 2900 170 / -80 150
TRAILING EDGE
FAILURE
(FLAPS LESS THAN 1)
VREF40+40 3450 250 / -110 190
TRAILING EDGE
FAILURE
(FLAPS GREATER THAN 1
AND LESS THAN 15)
VREF40+30 3200 210 / -100 180
FLAPS UP VREF40+55 3950 310 / -140 230
JAMMED STABILIZER VREF15 2730 150 / -70 130
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