737 Operations Manual
Performance Inflight -
Advisory Information
737-300/CFM56-3_22K
Copyright © The Boeing Company. See title page for details.
PI.12.4 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 5500 200 / -190 240
ANTI-SKID INOPERATIVE VREF40 5870 220/-200 145
HYDRAULIC SYSTEM A
INOPERATIVE
(FLAPS 15)
VREF15 5970 230 / -220 280
HYDRAULIC SYSTEM A
INOPERATIVE
(FLAPS 30)
VREF30 5690 210/-220 240
HYDRAULIC SYSTEM A
INOPERATIVE
(FLAPS 40)
VREF40 5370 220/-200 230
HYDRAULIC SYSTEM B
INOPERATIVE
(FLAPS 15)
VREF15 5250 200 / -170 230
HYDRAULIC SYSTEMS
A & B INOPERATIVE
(MANUAL REVERSION)
VREF15 6450 250 / -230 310
LEADING EDGE
ASYMMETRY OR
FAILURE
VREF15+5 5420 200 / -190 260
TRAILING EDGE
FAILURE
(FLAPS LESS THAN 1)
VREF40+40 6050 220 / -190 280
TRAILING EDGE
FAILURE
(FLAPS GREATER THAN 1
AND LESS THAN 15)
VREF40+30 5620 210 / -180 260
FLAPS UP VREF40+55 6850 250 / -220 330
JAMMED STABILIZER VREF15 4970 180 / -170 210
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
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