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ENGINE & WING ANTI-ICE ON -1.9 -2.0 -2.2 -2.4 -2.6 -2.7 -2.8 -3.0 -3.0
REPORTED
OAT TAT PRESSURE ALTITUDE (FT)
°C °F °C -1000 0 1000 2000 3000 4000 5000 6000 7000 8000
55 131 58 93.1 93.9 93.9 93.9
50 122 53 93.7 94.2 94.2 94.2 94.2 94.2
45 113 48 94.1 94.7 94.6 94.6 94.6 94.6 94.7 94.8 94.6
40 104 43 94.5 95.1 95.1 95.1 95.0 95.1 95.1 95.2 95.1 95.0
35 95 38 95.1 95.5 95.6 95.5 95.5 95.7 95.7 95.7 95.6 95.6
30 86 33 95.1 96.1 96.1 96.0 96.0 96.3 96.2 96.2 96.1 96.0
25 77 28 94.3 95.3 95.8 96.2 96.5 96.7 96.7 96.6 96.5 96.5
20 68 23 93.5 94.5 95.0 95.4 95.9 96.6 97.1 97.2 97.0 96.9
15 59 18 92.7 93.7 94.1 94.6 95.1 95.8 96.3 96.8 97.3 97.5
10 50 13 91.9 92.8 93.3 93.7 94.2 95.0 95.4 96.0 96.4 96.9
5 41 8 91.1 92.0 92.5 92.9 93.4 94.1 94.6 95.1 95.6 96.1
0 32 3 90.3 91.2 91.7 92.1 92.6 93.3 93.7 94.3 94.7 95.2
-10 14 -8 88.5 89.5 90.0 90.4 90.8 91.5 92.0 92.5 93.0 93.4
-20 -4 -18 86.8 87.8 88.2 88.6 89.1 89.8 90.3 90.8 91.2 91.6
-30 -22 -28 85.1 86.0 86.5 86.9 87.3 88.0 88.5 89.0 89.4 89.8
-40 -40 -38 83.3 84.2 84.7 85.1 85.5 86.2 86.6 87.1 87.5 87.9
-50 -58 -48 81.5 82.4 82.8 83.2 83.7 84.3 84.7 85.2 85.6 86.0
BLEED
CONFIGURATION
TAT (°C)
- 60 60
ENGINE BLEED TO PACKS OFF 0.8 1.0
PACKS HIGH - 0.3 - 0.3
WING A/I ALL ENGINES - 1.3 - 1.6
WING A/I 1 ENGINE INOP - 2.2 - 2.7
June 3, 2005
737 Flight Crew Operations Manual
Performance Inflight -
General
737-300/CFM56-3_22K
Copyright © The Boeing Company. See title page for details.
PI.20.26
Flight With Unreliable Airspeed / Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
Climb
Flaps Up, Set Max Climb Thrust
Cruise
Flaps Up, Adjust %N1 for Level Flight
Descent
Flaps Up, Set Idle Thrust
Holding
Flaps Up, Adjust %N1 for Level Flight
PRESSURE ALTITUDE (FT)
(SPEED)
WEIGHT (1000 KG)
32 34 44 54 64
35000 PITCH ATT 6.5 6.5 6.0 5.5 5.5
(.73M) V/S (FT/MIN) 3100 2800 1800 1000 300
30000 PITCH ATT 7.0 6.5 6.0 5.5 5.5
(.73M) V/S (FT/MIN) 3900 3600 2500 1700 1100
25000 PITCH ATT 7.0 6.5 6.0 6.0 6.0
(280 KIAS) V/S (FT/MIN) 3700 3500 2500 1800 1300
20000 PITCH ATT 8.5 8.5 7.5 7.0 7.0
(280 KIAS) V/S (FT/MIN) 4600 4300 3100 2300 1800
15000 PITCH ATT 10.5 10.0 9.0 8.0 8.0
(280 KIAS) V/S (FT/MIN) 5400 5100 3800 2900 2200
10000 PITCH ATT 13.0 12.0 10.5 9.5 9.0
(280 KIAS) V/S (FT/MIN) 6300 5900 4400 3400 2700
5000 PITCH ATT 15.0 14.5 12.0 11.0 10.0
(280 KIAS) V/S (FT/MIN) 7100 6700 5000 3900 3100
SEA LEVEL PITCH ATT 17.5 17.0 14.0 12.5 11.5
(280 KIAS) V/S (FT/MIN) 7900 7400 5600 4400 3500
PRESSURE ALTITUDE (FT)
(SPEED)
WEIGHT (1000 KG)
34 38 42 46 50 54
30000 PITCH ATT 2.0 2.0 2.5 3.0 3.0 3.5
(.73M) %N1 79 79 80 81 82 83
10000 PITCH ATT 2.0 2.0 2.5 3.0 3.0 3.5
(280 KIAS) %N1 65 65 66 66 67 68
PRESSURE ALTITUDE (FT)
(SPEED)
WEIGHT (1000 KG)
34 38 42 46 50 54
30000 PITCH ATT -3.5 -3.0 -2.5 -2.0 -1.5 -1.0
(.73M) V/S (FT/MIN) -4200 -3800 -3600 -3400 -3300 -3200
20000 PITCH ATT -2.5 -2.0 -1.0 -0.5 0.0 0.0
(280 KIAS) V/S (FT/MIN) -2900 -2600 -2500 -2300 -2200 -2100
10000 PITCH ATT -2.5 -2.0 -1.5 -1.0 -0.5 0.0
(280 KIAS) V/S (FT/MIN) -2500 -2300 -2200 -2100 -2000 -1900
PRESSURE ALTITUDE (FT) WEIGHT (1000 KG)
34 38 42 46 50 54
10000
PITCH ATT 4.0 4.5 5.5 5.5 5.5 5.5
%N1 56 57 59 61 63 65
KIAS 210 210 210 215 225 230
June 3, 2005
737 Flight Crew Operations Manual
Performance Inflight -
General
737-300/CFM56-3_22K
Copyright © The Boeing Company. See title page for details.
 PI.20.27
Flight With Unreliable Airspeed / Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
Terminal Area
Adjust %N1 for Level Flight
Final Approach
Gear Down, Adjust %N1 for 3° Glideslope
FLAP POSITION (SPEED) WEIGHT (1000 KG)
32 40 48 56 64
FLAPS UP (GEAR UP)
PITCH ATT 3.5 5.0 6.0 6.5 7.0
%N1
KIAS
52
210
55
210
58
210
62
220
65
230
FLAPS 1 (GEAR UP)
PITCH ATT 4.0 5.5 6.5 7.0 7.5
%N1
KIAS
55
190
57
190
60
190
64
200
67
210
FLAPS 5 (GEAR UP)
PITCH ATT 3.5 4.5 6.0 6.5 6.5
%N1
KIAS
55
180
58
180
61
180
65
190
68
200
FLAPS 15 (GEAR DOWN)
PITCH ATT 3.5 5.5 7.5 8.0 8.0
%N1
KIAS
61
　
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