Boeing 737 - PI.32 Performance Inflight -Advisory Information

737 Operations Manual
Performance Inflight - Chapter PI
Advisory Information Section 32
737-500/CFM56-3_20K
FAST-Doc PI/PD Template 9/1/99
Copyright © The Boeing Company. See title page for details.
D6-27370-400E-TBCE PI.32.1
PI.32 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 2475 3315 4280 5315
AUTOBRAKE SETTING 2 4215 4660 4985 5595
AUTOBRAKE SETTING 3 3020 3660 4330 5315
MAX AUTOBRAKE SETTING 2560 3315 4280 5315
CONDITIONS ADJUSTMENTS
WEIGHT
PER 5000 KG BELOW 45,000 KG -150 -245 -360 -490
PER 5000 KG ABOVE 45,000 KG 445 425 445 525
AIRPORT
PRESSURE
ALTITUDE
PER 1000 FT ABOVE SEA LEVEL 130 130 150 165
WIND
PER 10 KTS HEADWIND -80 -150 -230 -345
PER 10 KTS TAILWIND 805 855 1015 1425
APPROACH
SPEED
PER 10 KTS ABOVE VREF 510 475 445 425
SLOPE
PER 1% DOWNHILL SLOPE 35 80 180 425
PER 1% UPHILL SLOPE -35 -35 -100 -245
REVERSE
THRUST
1 REVERSER INOPERATIVE 35 150 375 755
2 REVERSERS INOPERATIVE 50 525 1690 4775
MAXIMUM REVERSE THRUST 0 0 -35 -80
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