737 Operations Manual
Performance Inflight -
Advisory Information
737-400/CFM56-3_23.5K
Copyright © The Boeing Company. See title page for details.
PI.22.4 D6-27370-400E-TBCE
ADVISORY INFORMATION
Advi sory In formati on
Non-Normal Configuration Landing Distance
Medium Reported Braking Action
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 5700 220 / -210 300
ANTI-SKID INOPERATIVE VREF40 5860 210/-200 175
HYDRAULIC SYSTEM A
INOPERATIVE
(FLAPS 15)
VREF15 6300 260 / -230 330
HYDRAULIC SYSTEM A
INOPERATIVE
(FLAPS 30)
VREF30 5680 220/-210 240
HYDRAULIC SYSTEM A
INOPERATIVE
(FLAPS 40)
VREF40 5380 200/-190 230
HYDRAULIC SYSTEM B
INOPERATIVE
(FLAPS 15)
VREF15 5430 200 / -190 280
HYDRAULIC SYSTEMS
A & B INOPERATIVE
(MANUAL REVERSION)
VREF15 6730 270 / -250 340
LEADING EDGE
ASYMMETRY OR
FAILURE
VREF15+5 5600 220 / -200 310
TRAILING EDGE
FAILURE
(FLAPS LESS THAN 1)
VREF40+40 6050 210 / -190 350
TRAILING EDGE
FAILURE
(FLAPS GREATER THAN 1
AND LESS THAN 15)
VREF40+30 5700 200 / -180 310
FLAPS UP VREF40+55 6850 230 / -220 450
JAMMED STABILIZER VREF15 5100 200 / -180 240
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
To Next Page
Loading...
