737 Operations Manual
Performance Inflight -
Advisory Information
737-500/CFM56-3_20K
Copyright © The Boeing Company. See title page for details.
D6-27370-400E-TBCE PI.32.5
ADVISORY INFORMATION
Advi sory In formati on
Non-Normal Configuration Landing Distance
Poor 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 7250 290 / -270 370
ANTI-SKID INOPERATIVE VREF40 7340 290/-270 240
HYDRAULIC SYSTEM A
INOPERATIVE
(FLAPS 15)
VREF15 7360 300 / -280 380
HYDRAULIC SYSTEM A
INOPERATIVE
(FLAPS 30)
VREF30 6800 270/-260 290
HYDRAULIC SYSTEM A
INOPERATIVE
(FLAPS 40)
VREF40 6410 240/-240 280
HYDRAULIC SYSTEM B
INOPERATIVE
(FLAPS 15)
VREF15 6570 260 / -240 310
HYDRAULIC SYSTEMS
A & B INOPERATIVE
(MANUAL REVERSION)
VREF15 7800 270 / -300 360
LEADING EDGE
ASYMMETRY OR
FAILURE
VREF15+5 6750 270 / -250 340
TRAILING EDGE
FAILURE
(FLAPS LESS THAN 1)
VREF40+40 7650 280 / -270 390
TRAILING EDGE
FAILURE
(FLAPS GREATER THAN 1
AND LESS THAN 15)
VREF40+30 7120 260 / -250 330
FLAPS UP VREF40+55 8640 310 / -300 480
JAMMED STABILIZER VREF15 6200 240 / -230 290
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...
