737 Operations Manual
Performance Inflight - Chapter PI
Advisory Information Section 12
737-300/CFM56-3_22K
FAST-Doc PI/PD Template 9/1/99
Copyright © The Boeing Company. See title page for details.
D6-27370-400E-TBCE PI.12.1
PI.12 Performance Inflight --Advisory Information
ADVISORY INFORMATION
Advi sory In formati on
Autobrake Landing Distance
Reference Landing Distance (FT)
Landing Distance Adjustments (FT)
Slippery Runway Landing Distance
Reference Landing Distance (FT)
Landing Distance Adjustments (FT)
AUTOBRAKE
SETTING
APPROACH SPEED (KIAS)
100 110 120 130 140 150 160
1 4500 5300 6100 6930 7850 8850 9950
2 3800 4440 5080 5730 6450 7240 8100
3 3200 3680 4150 4650 5220 5840 6500
MAX 2500 2760 3010 3280 3600 4000 4500
Actual (unfactored) distances are shown.
Landing distance required includes 1000 ft of air distance.
The distances are valid with or without reverse thrust and for any flap.
If entering with ground speed, ignore adjustments.
AUTOBRAKE
SETTING
ALTITUDE ADJUSTMENT
PER 1000 FT ABOVE SEA LEVEL
TAILWIND ADJUSTMENT
PER 10 KTS
TEMP ADJUSTMENT
PER 10°C ABOVE ISA
1 250 1100 300
2 200 900 250
3 140 650 200
MAX 80 400 100
BRAKING CONFIGURATION
REPORTED BRAKING ACTION
DRY GOOD MEDIUM POOR
MAX MANUAL BRAKING 2525 3445 4495 5625
AUTOBRAKE SETTING 2 4495 4955 5280 5940
AUTOBRAKE SETTING 3 3165 3840 4575 5625
MAX AUTOBRAKE SETTING 2625 3445 4495 5625
CONDITIONS ADJUSTMENTS
WEIGHT
PER 5000 KG BELOW 48,000 KG -150 -245 -375 -510
PER 5000 KG ABOVE 48,000 KG 525 490 525 605
AIRPORT
PRESSURE
ALTITUDE
PER 1000 FT ABOVE SEA LEVEL 130 150 150 165
WIND
PER 10 KTS HEADWIND -80 -150 -245 -345
PER 10 KTS TAILWIND 835 885 1035 1475
APPROACH
SPEED
PER 10 KTS ABOVE VREF 510 475 445 425
SLOPE
PER 1% DOWNHILL SLOPE 35 80 195 445
PER 1% UPHILL SLOPE -35 -35 -115 -260
REVERSE
THRUST
1 REVERSER INOPERATIVE 35 150 410 805
2 REVERSERS INOPERATIVE 115 560 1770 4890
MAXIMUM REVERSE THRUST 0 0 -35 -100
Actual (unfactored) distances are shown.
Landing Distance Required Includes 1000 ft of Air Distance.
Based on flaps 40, VREF40 approach speed.
Includes 2 engine detent reverse thrust.
June 07, 2002
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