Boeing 737 - Non-Normal Configuration Landing Distance

737 Operations Manual
Performance Inflight -
Advisory Information
737-300/CFM56-3_22K
Copyright © The Boeing Company. See title page for details.
D6-27370-400E-TBCE PI.12.5
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 7330 310 / -280 330
ANTI-SKID INOPERATIVE VREF40 7410 290/-280 200
HYDRAULIC SYSTEM A
INOPERATIVE
(FLAPS 15)
VREF15 7400 310 / -290 360
HYDRAULIC SYSTEM A
INOPERATIVE
(FLAPS 30)
VREF30 6900 270/-280 290
HYDRAULIC SYSTEM A
INOPERATIVE
(FLAPS 40)
VREF40 6490 280/-260 280
HYDRAULIC SYSTEM B
INOPERATIVE
(FLAPS 15)
VREF15 6650 260 / -250 300
HYDRAULIC SYSTEMS
A & B INOPERATIVE
(MANUAL REVERSION)
VREF15 7930 340 / -300 380
LEADING EDGE
ASYMMETRY OR
FAILURE
VREF15+5 6800 280 / -250 330
TRAILING EDGE
FAILURE
(FLAPS LESS THAN 1)
VREF40+40 7600 310 / -280 360
TRAILING EDGE
FAILURE
(FLAPS GREATER THAN 1
AND LESS THAN 15)
VREF40+30 7100 290 / -250 340
FLAPS UP VREF40+55 8600 340 / -310 420
JAMMED STABILIZER VREF15 6250 250 / -240 270
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