Boeing 737 - PI.22 Performance Inflight -Advisory Information

737 Operations Manual
Performance Inflight - Chapter PI
Advisory Information Section 22
737-400/CFM56-3_23.5K
FAST-Doc PI/PD Template 9/1/99
Copyright © The Boeing Company. See title page for details.
D6-27370-400E-TBCE PI.22.1
PI.22 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 1200 350
2 200 950 300
3 140 700 200
MAX 80 400 150
BRAKING CONFIGURATION
REPORTED BRAKING ACTION
DRY GOOD MEDIUM POOR
MAX MANUAL BRAKING 2660 3660 4825 6055
AUTOBRAKE SETTING 2 4840 5330 5695 6400
AUTOBRAKE SETTING 3 3380 4100 4890 6055
MAX AUTOBRAKE SETTING 2770 3660 4825 6055
CONDITIONS ADJUSTMENTS
WEIGHT
PER 5000 KG BELOW 52,000 KG -150 -245 -375 -510
PER 5000 KG ABOVE 52,000 KG 490 445 475 560
AIRPORT
PRESSURE
ALTITUDE
PER 1000 FT ABOVE SEA LEVEL 150 150 165 195
WIND
PER 10 KTS HEADWIND -100 -165 -260 -375
PER 10 KTS TAILWIND 885 935 1085 1540
APPROACH
SPEED
PER 10 KTS ABOVE VREF 540 490 460 460
SLOPE
PER 1% DOWNHILL SLOPE 35 80 215 510
PER 1% UPHILL SLOPE -35 -35 -130 -295
REVERSE
THRUST
1 REVERSER INOPERATIVE 35 165 445 885
2 REVERSERS INOPERATIVE 130 590 1805 4775
MAXIMUM REVERSE THRUST 0 0 -35 -115
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