Boeing 737 - 600/700/800/900. Operations Manual (1997 year)

Performance Dispatch

Landing

FAA

Category B Brakes

Boeing 737 Operations Manual

Landing

Landing Climb Limit Weight

Valid for approach with Flaps 15 and landing with Flaps 30 or 40

Based on engine bleed for packs on and anti-ice off

AIRPORT

LANDING CLIMB LIMIT WEIGHT (1000 LB)

OAT

AIRPORT PRESSURE ALTITUDE (FT)

°F

°C

1000

2000

3000

120

136.7

131.7

126.8

115

140.5

135.5

130.3

125.4

110

144.2

139.0

133.8

128.8

105

148.1

142.6

137.3

132.2

100

152.2

146.5

141.0

135.7

156.1

150.5

144.7

139.3

160.2

154.4

148.6

142.9

163.7

158.4

152.6

146.7

163.9

160.7

156.6

150.6

164.1

160.9

157.7

154.4

164.3

161.1

157.9

154.6

164.5

161.2

158.0

154.7

164.6

161.4

158.2

154.9

164.8

161.6

158.3

155.0

165.0

161.7

158.5

155.2

-40

166.3

163.1

159.9

156.6

With engine bleed for packs off, increase weight by 2800 lb.

With engine anti-ice on, decrease allowable weight by 500 lb.

With engine and wing anti-ice on, decrease weight by 2700 lb.

When operating in icing conditions during any part of the flight with forecast landing temperature below

10°C, decrease weight by 13800 lb.

PD.22.2

Performance Dispatch

FAA

Landing

Category B Brakes

Boeing 737 Operations Manual

Quick Turnaround Limit Weight

Flaps 40

AIRPORT

LIMIT WEIGHT (1000 LB)

OAT

AIRPORT PRESSURE ALTITUDE (FT)

°F

°C

1000

2000

3000

120

160.0

156.7

153.5

100

163.2

159.8

156.5

153.3

166.5

163.0

159.6

156.3

169.9

166.4

162.9

159.5

173.4

170.0

166.4

162.9

-7

177.0

173.6

170.1

166.5

-18

180.0

177.2

173.8

170.4

-20

-29

180.0

177.7

174.3

-40

180.0

178.3

Increase weight by 1600 lb per 1% uphill slope. Decrease weight by 2400 lb per 1% downhill slope.

Increase weight by 4100 lb per 10 knots headwind. Decrease weight by 17000 lb per 10 knots tailwind.

After landing at weights exceeding those shown above, adjusted for slope and wind, wait at least 62 minutes

and check that wheel thermal plugs have not melted before executing a takeoff.

As an alternate procedure, ensure that each brake pressure plate temperature, without artificial cooling, is

less than 425°F as follows: No sooner than 10 and no later than 15 minutes after parking, measure each

brake pressure plate surface temperature at a minimum of two points per brake by an accurate method

(using a Doric Microtemp 450 hand held thermometer or equivalent, hold temperature probe in place for 20

seconds or until reading stabilizes). If each measured temperature is less than 425°F, immediate dispatch is

allowed; otherwise the required minimum ground wait period of 62 minutes applies.

PD.22.3

FAA

Category B Brakes

Boeing 737 Operations Manual

Performance Dispatch

Chapter PD

Text

Section 23

Text

Introduction

This chapter contains self dispatch performance data intended primarily

for use by flight crews in the event that information cannot be obtained

from the airline dispatch office. The takeoff data provided is for a single

takeoff flap at max takeoff thrust. The range of conditions covered is

limited to those normally encountered in airline operation. In the event of

conflict between the data presented in this chapter and that contained in the

approved Airplane Flight Manual, the Flight Manual shall always take

precedence.

Takeoff

The maximum allowable takeoff weight will be the least of the Field,

Climb and Obstacle Limit Weights as determined from the tables shown.

Tire and Brake Energy Limits are not shown as they are not limiting for the

range of conditions shown in this chapter.

Field Limit Weight - Slope and Wind Corrections

These tables for dry and wet runways provide corrections to the field

length available for the effects of runway slope and wind component along

the runway. Enter the appropriate table with the available field length and

runway slope to determine the slope corrected field length. Next enter the

appropriate table with slope corrected field length and wind component to

determine the slope and wind corrected field length.

Field and Climb Limit Weight

Tables are presented for selected airport pressure altitudes and runway

conditions and show both Field and Climb Limit Weights. Enter the

appropriate table for pressure altitude and runway condition with “Slope

and Wind Corrected Field Length” determined above and airport OAT to

obtain Field Limit Weight. Also read Climb Limit Weight for the same

OAT. Intermediate altitudes may be interpolated or use next higher

altitude. When finding a maximum weight for a wet runway, the dry

runway limit weight must also be determined and the lower of the two

weights used.

PD.23.1

Performance Dispatch

Text

FAA

Category B Brakes

Boeing 737 Operations Manual

Obstacle Limit Weight

The Reference Obstacle Limit Weight table provides obstacle limit

weights for reference airport conditions based on obstacle height above the

runway surface and distance from brake release. Enter the adjustment

tables to adjust the reference Obstacle Limit Weight for the effects of

OAT, pressure altitude and wind as indicated. In the case of multiple

obstacles, enter the tables successively with each obstacle and determine

the most limiting weight.

Enroute

Long Range Cruise Maximum Operating Altitude

These tables provide the maximum operating altitude in the same manner

as the FMC. Maximum altitudes are shown for a given cruise weight and

maneuver capability. Note that this table considers both thrust and buffet

limits, providing the more limiting of the two. Any data that is thrust

limited is denoted by an asterisk and represents only a thrust limited

condition in level flight with 100 ft/min residual rate of climb. Flying

above these altitudes with sustained banks in excess of approximately 15°

may cause the airplane to lose speed and/or altitude. The altitudes shown

in the table are limited to the maximum certified altitude of 41000 ft.

Long Range Cruise Trip Fuel and Time

Long Range Cruise Trip Fuel and Time tables are provided to determine

trip time and fuel required to destination.

To determine trip fuel and time for a constant altitude cruise, first enter the

Ground to Air Miles Conversion table to convert ground distance and

enroute wind to an equivalent still air distance for use with the Reference

Fuel and Time tables. Next, enter the Reference Fuel and Time table with

air distance from the Ground to Air Miles Conversion table and the desired

altitude and read Reference Fuel and Time Required. Lastly, enter the Fuel

Required Adjustment table with the Reference Fuel and the planned

landing weight to obtain the adjustment to the fuel required at the planned

landing weight.

Long Range Cruise Step Climb Trip Fuel and Time

The Long Range Cruise Step Climb Trip Fuel and Time tables are provided

to determine trip time and fuel required to destination when flying a step

climb profile. Step climb profiles are based on 4000 ft step climbs to keep

the flight within 2000 ft of the optimum altitude for the current cruise

weight. To determine trip fuel and time, enter the Ground to Air Miles

PD.23.2

Performance Dispatch

FAA

Text

Category B Brakes

Boeing 737 Operations Manual

Conversion table and determine air distance as discussed above. Then

enter the Trip Fuel and Time Required table with air distance and planned

landing weight to read trip fuel. Continue across the table to read trip time.

Short Trip Fuel and Time

These tables are provided to determine trip fuel and time for short

distances or alternates. Obtain air distance from the table using the ground

distance and wind component to the alternate. Enter the Trip Fuel and Time

Required table with air distance and read trip fuel required for the expected

landing weight, together with time to alternate at right. For distances

greater than shown or other altitudes, use the Long Range Cruise Trip Fuel

and Time tables.

Holding Planning

This table provides total fuel flow information necessary for planning flaps

up holding and reserve fuel requirements. Data is based on the FMC

holding speed schedule which is the higher of the maximum endurance and

flaps up maneuver speeds. As noted, the fuel flow is based on flight in a

racetrack holding pattern. For holding in straight and level flight, reduce

table values by 5%.

Crew Oxygen Requirements

Tables are provided to determine the minimum dispatch oxygen pressure

for protective breathing equipment used by the flight crew. Enter the

number of crew plus observers using oxygen and read the minimum

cylinder pressure required for the appropriate bottle temperature and size.

These pressures provide sufficient oxygen for 15 minutes of protective

breathing for each flight crew member plus 10% contingency at 8000 ft

cabin pressure altitude. Route specific analysis is necessary to determine

if additional oxygen pressure is needed to meet supplemental oxygen

requirements.

Net Level Off Weight

The Net Level Off Weight table is provided to determine terrain clearance

capability in straight and level flight following an engine failure.

Regulations require terrain clearance planning based on net performance

which is the gross (or actual) gradient performance degraded by 1.1%. In

addition, the net level off pressure altitude must clear the terrain by

1000 ft.

To determine the maximum weight for terrain clearance, enter the table

with required net level off pressure altitude and expected ISA deviation to

obtain weight. Adjust weight for anti-ice operation as noted below the

table.

PD.23.3

Performance Dispatch

Text

FAA

Category B Brakes

Boeing 737 Operations Manual

Extended Range Operations

Regulations require that flights conducted over a route that contains a

point further than one hour’s time at

“normal one engine inoperative

speed” from an adequate diversion airport comply with rules set up

specifically for “Extended Range Operation with Two Engine airplanes.”

This section provides reserve fuel planning information for the "Critical

Fuel Scenario" based on two engine operation at Long Range Cruise as

well as single engine operation at Long Range Cruise.

Long Range Cruise Critical Fuel Reserves

Enter the Ground to Air Miles Conversion table with forecast wind and

ground distance to diversion airport from critical point to obtain air

distance. Now enter the Critical Fuel table with air distance and expected

weight at the critical point and read required fuel. Apply the noted fuel

adjustments as necessary. Regulations require a

5% allowance for

performance deterioration unless a value has been established by the

operator for inservice deterioration.

As noted below each table, the fuel required is the greater of the two engine

fuel and the single engine fuel. This fuel is compared to the amount of fuel

normally onboard the airplane at that point in the route. If the fuel required

by the critical fuel reserves exceeds the amount of fuel normally expected,

the fuel load must be adjusted accordingly.

Landing

Tables are provided for determining the maximum landing weight as

limited by field length or climb requirements for a single landing flap.

Maximum landing weight is the lowest of the field length limit weight,

climb limit weight, or maximum certified landing weight.

Landing Field Limit Weight

Obtain wind corrected field length by entering the Wind Corrected Field

Length table with field length available and wind component along the

runway. Now enter the Field Limit Weight table with wind corrected field

length and pressure altitude to read field limit weight for the expected

runway condition.

Landing Climb Limit Weight

Enter the table with airport OAT and pressure altitude to read landing

climb limit weight. Apply the noted adjustments as required.

PD.23.4

FAA

Category C Brakes

Boeing 737 Operations Manual

Performance Dispatch

Chapter PD

Takeoff

Section 30

Takeoff

Takeoff Field Corrections -ff

Dry Runway

Slope Corrections

FIELD LENGTH

SLOPE CORRECTED FIELD LENGTH (M)

AVAILABLE

RUNWAY SLOPE (%)

(M)

-2.0

-1.5

-1.0

-0.5

0.0

0.5

1.0

1.5

2.0

1200

1230

1220

1210

1200

1190

1170

1160

1140

1400

1450

1440

1430

1410

1400

1370

1350

1320

1300

1600

1670

1650

1640

1620

1600

1560

1530

1490

1450

1800

1900

1870

1850

1820

1800

1750

1700

1650

1600

2000

2120

2090

2060

2030

2000

1940

1880

1820

1760

2200

2340

2310

2270

2240

2200

2130

2060

1980

1910

2400

2560

2520

2480

2440

2400

2320

2230

2150

2060

2600

2790

2740

2690

2650

2600

2500

2410

2310

2220

2800

3010

2960

2900

2850

2800

2690

2590

2480

2370

3000

3230

3170

3120

3060

3000

2880

2760

2640

2520

3200

3450

3390

3330

3260

3200

3070

2940

2810

2680

3400

3680

3610

3540

3470

3400

3260

3120

2970

2830

3600

3900

3820

3750

3670

3600

3450

3290

3140

2980

3800

4130

4050

3970

3880

3800

3630

3470

3300

3140

4000

4370

4280

4190

4090

4000

3820

3650

3470

3290

4200

4610

4510

4410

4300

4200

4010

3820

3630

3440

4400

4850

4740

4630

4510

4400

4200

4000

3800

3600

4600

5090

4970

4850

4720

4600

4390

4180

3960

3750

4800

5330

5200

5070

4930

4800

4580

4350

4130

3900

5000

5570

5430

5290

5140

5000

4760

4530

4290

4060

Wind Corrections

SLOPE CORR'D

SLOPE & WIND CORRECTED FIELD LENGTH (M)

FIELD LENGTH

WIND COMPONENT (KTS)

(M)

-15

-10

-5

1200

880

990

1090

1200

1260

1320

1390

1470

1400

1050

1170

1280

1400

1460

1530

1610

1690

1600

1220

1350

1470

1600

1670

1740

1820

1910

1800

1390

1530

1660

1800

1870

1950

2040

2130

2000

1560

1700

1850

2000

2080

2160

2250

2350

2200

1720

1880

2040

2200

2280

2370

2470

2570

2400

1890

2060

2230

2400

2490

2580

2680

2790

2600

2060

2240

2420

2600

2690

2790

2900

3010

2800

2230

2420

2610

2800

2900

3000

3110

3230

3000

2400

2600

2800

3000

3100

3210

3330

3460

3200

2570

2780

2990

3200

3310

3420

3540

3680

3400

2730

2960

3180

3400

3510

3630

3760

3900

3600

2900

3130

3370

3600

3720

3840

3970

4120

3800

3070

3310

3560

3800

3920

4050

4190

4340

4000

3240

3490

3750

4000

4130

4260

4410

4560

4200

3410

3670

3940

4200

4330

4470

4620

4780

4400

3570

3850

4120

4400

4540

4680

4840

5000

4600

3740

4030

4310

4600

4740

4890

5050

5220

4800

3910

4210

4500

4800

4950

5100

5270

5440

5000

4080

4390

4690

5000

5150

5310

5480

5660

PD.30.1

Performance Dispatch

Takeoff

FAA

Category C Brakes

Boeing 737 Operations Manual

Takeoff

Takeoff Field & Climb Limit Weights - Dry Runway

Flaps 5

Sea Level Pressure Altitude

FIELD LIMIT WEIGHT (1000 KG)

CORR'D FIELD

OAT

LENGTH (M)

°C

-40

°F

-40

108

115

122

1400

63.2

58.2

57.8

57.4

57.3

57.1

56.9

56.7

52.7

51.4

50.1

1600

68.3

62.9

62.5

62.1

61.9

61.7

61.5

61.3

57.0

55.6

54.2

1800

73.1

67.2

66.8

66.4

66.2

66.0

65.8

65.5

61.0

59.4

57.9

2000

77.7

71.3

70.9

70.4

70.2

70.0

69.8

69.5

64.6

62.9

61.3

2200

81.8

75.1

74.6

74.2

73.9

73.7

73.4

73.2

67.9

66.2

64.4

2400

85.7

78.6

78.1

77.6

77.4

77.1

76.8

76.6

71.0

69.2

67.3

2600

86.2

81.8

81.3

80.8

80.5

80.3

80.0

79.7

73.9

72.0

70.0

2800

86.2

84.9

84.4

83.8

83.6

83.3

83.0

82.7

76.7

74.7

72.7

3000

86.2

86.0

85.7

85.5

79.2

77.1

75.0

3200

86.2

81.4

79.2

77.1

3400

86.2

83.5

81.3

79.1

3600

86.2

85.5

83.3

81.0

3800

86.2

85.2

82.9

4000

86.2

84.7

4200

86.2

4400

86.2

4600

86.2

CLIMB LIMIT

82.5

81.9

81.8

81.6

81.5

81.4

73.5

71.0

68.5

WT (1000 KG)

1000 FT Pressure Altitude

FIELD LIMIT WEIGHT (1000 KG)

CORR'D FIELD

OAT

LENGTH (M)

°C

-40

°F

-40

108

115

122

1400

61.5

56.6

56.2

55.9

55.7

55.5

55.4

54.8

51.0

49.7

48.4

1600

66.5

61.2

60.8

60.4

60.3

60.1

59.9

59.3

55.1

53.7

52.4

1800

71.2

65.4

65.0

64.6

64.4

64.2

64.0

63.4

58.9

57.4

56.0

2000

75.6

69.4

69.0

68.5

68.3

68.1

67.9

67.2

62.4

60.8

59.2

2200

79.6

73.1

72.6

72.1

71.9

71.7

71.4

70.7

65.6

63.9

62.2

2400

83.3

76.4

75.9

75.5

75.2

75.0

74.7

74.0

68.6

66.8

65.0

2600

86.2

79.6

79.1

78.5

78.3

78.0

77.8

77.0

71.3

69.5

67.6

2800

86.2

82.6

82.0

81.5

81.2

81.0

80.7

79.9

74.0

72.1

70.1

3000

86.2

85.3

84.8

84.2

83.9

83.6

83.4

82.5

76.4

74.4

72.4

3200

86.2

86.0

85.7

84.8

78.5

76.5

74.4

3400

86.2

80.6

78.4

76.3

3600

86.2

82.5

80.3

78.2

3800

86.2

84.4

82.2

80.0

4000

86.2

84.0

81.7

4200

86.2

85.7

83.4

4400

86.2

85.1

4600

86.2

CLIMB LIMIT

80.6

80.0

79.9

79.8

79.7

79.6

78.5

71.1

68.7

66.3

WT (1000 KG)

With engine bleed for packs off, increase field limit weight by 400 kg and climb limit weight by 1250 kg.

With engine anti-ice on, decrease field limit weight by 200 kg and climb limit weight by 200 kg.

With engine and wing anti-ice on (optional system), decrease field limit weight by 750 kg and climb limit

weight by 1350 kg.

PD.30.2

Performance Dispatch

FAA

Takeoff

Category C Brakes

Boeing 737 Operations Manual

Takeoff

Takeoff Field & Climb Limit Weights - Dry Runway

Flaps 5

2000 FT Pressure Altitude

FIELD LIMIT WEIGHT (1000 KG)

CORR'D FIELD

OAT

LENGTH (M)

°C

-40

°F

-40

108

115

122

1400

60.0

55.0

54.7

54.3

54.2

54.0

53.5

53.0

49.2

48.0

46.8

1600

64.9

59.5

59.1

58.8

58.6

58.4

57.9

57.3

53.3

51.9

50.6

1800

69.4

63.6

63.2

62.8

62.6

62.4

61.9

61.3

56.9

55.5

54.0

2000

73.7

67.4

67.0

66.6

66.4

66.2

65.6

64.9

60.2

58.7

57.2

2200

77.6

71.0

70.5

70.1

69.8

69.6

69.0

68.3

63.3

61.7

60.0

2400

81.2

74.2

73.7

73.3

73.0

72.8

72.1

71.4

66.2

64.4

62.7

2600

84.5

77.3

76.8

76.3

76.0

75.8

75.1

74.3

68.8

67.0

65.2

2800

86.2

80.2

79.6

79.1

78.9

78.6

77.9

77.1

71.4

69.5

67.6

3000

86.2

82.8

82.3

81.7

81.5

81.2

80.5

79.6

73.7

71.8

69.8

3200

86.2

85.1

84.5

84.0

83.7

83.5

82.7

81.8

75.8

73.8

71.8

3400

86.2

86.1

85.9

85.6

84.8

83.9

77.7

75.7

73.6

3600

86.2

86.0

79.6

77.5

75.4

3800

86.2

81.4

79.3

77.1

4000

86.2

83.2

81.0

78.8

4200

86.2

84.9

82.7

80.5

4400

86.2

84.3

82.1

4600

86.2

85.9

83.6

CLIMB LIMIT

78.6

78.0

77.9

77.8

76.9

75.9

68.7

66.4

64.1

WT (1000 KG)

3000 FT Pressure Altitude

FIELD LIMIT WEIGHT (1000 KG)

CORR'D FIELD

OAT

LENGTH (M)

°C

-40

°F

-40

108

115

122

1400

58.1

53.2

52.9

52.6

52.4

52.0

51.6

51.1

47.5

46.3

45.2

1600

62.9

57.6

57.2

56.9

56.7

56.3

55.8

55.3

51.4

50.2

48.9

1800

67.2

61.5

61.1

60.8

60.6

60.1

59.6

59.1

55.0

53.6

52.3

2000

71.3

65.2

64.8

64.4

64.2

63.7

63.2

62.5

58.1

56.6

55.2

2200

75.1

68.6

68.1

67.7

67.5

67.0

66.4

65.8

61.1

59.5

58.0

2400

78.6

71.7

71.3

70.8

70.6

70.0

69.4

68.7

63.8

62.1

60.5

2600

81.8

74.6

74.2

73.7

73.5

72.9

72.2

71.5

66.4

64.6

63.0

2800

84.9

77.4

76.9

76.5

76.2

75.6

74.9

74.2

68.8

67.0

65.3

3000

86.2

80.0

79.5

79.0

78.7

78.1

77.4

76.6

71.1

69.2

67.4

3200

86.2

82.2

81.7

81.1

80.9

80.2

79.5

78.8

73.0

71.1

69.3

3400

86.2

84.3

83.8

83.2

83.0

82.3

81.6

80.8

74.9

72.9

71.1

3600

86.2

85.8

85.2

85.0

84.3

83.6

82.7

76.7

74.7

72.8

3800

86.2

85.5

84.6

78.5

76.4

74.4

4000

86.2

80.2

78.1

76.1

4200

86.2

81.9

79.7

77.6

4400

86.2

83.5

81.3

79.2

4600

86.2

85.1

82.8

80.7

CLIMB LIMIT

76.2

75.7

75.6

75.5

74.8

74.1

73.2

66.4

64.2

62.0

WT (1000 KG)

With engine bleed for packs off, increase field limit weight by 400 kg and climb limit weight by 1250 kg.

With engine anti-ice on, decrease field limit weight by 200 kg and climb limit weight by 200 kg.

With engine and wing anti-ice on (optional system), decrease field limit weight by 750 kg and climb limit

weight by 1350 kg.

PD.30.3

Performance Dispatch

Takeoff

FAA

Category C Brakes

Boeing 737 Operations Manual

Takeoff

Takeoff Field Corrections - Wet Runway

Slope Corrections

FIELD LENGTH

SLOPE CORRECTED FIELD LENGTH (M)

AVAILABLE

RUNWAY SLOPE (%)

(M)

-2.0

-1.5

-1.0

-0.5

0.0

0.5

1.0

1.5

2.0

1200

1190

1170

1160

1140

1400

1430

1420

1410

1400

1380

1360

1330

1310

1600

1670

1650

1630

1620

1600

1570

1540

1510

1480

1800

1900

1870

1850

1820

1800

1760

1720

1680

1650

2000

2130

2100

2070

2030

2000

1950

1910

1860

1810

2200

2360

2320

2280

2240

2200

2150

2090

2040

1980

2400

2600

2550

2500

2450

2400

2340

2280

2210

2150

2600

2830

2770

2720

2660

2600

2530

2460

2390

2320

2800

3060

3000

2930

2870

2800

2720

2640

2560

2490

3000

3300

3220

3150

3070

3000

2910

2830

2740

2650

3200

3530

3450

3370

3280

3200

3110

3010

2920

2820

3400

3760

3670

3580

3490

3400

3300

3200

3090

2990

3600

4000

3900

3800

3700

3600

3490

3380

3270

3160

3800

4230

4120

4020

3910

3800

3680

3560

3450

3330

4000

4460

4350

4230

4120

4000

3870

3750

3620

3500

4200

4700

4570

4450

4320

4200

4070

3930

3800

3670

4400

4930

4800

4670

4530

4400

4260

4120

3980

3830

4600

5160

5020

4880

4740

4600

4450

4300

4150

4000

4800

5400

5250

5100

4950

4800

4640

4490

4330

4170

5000

5630

5470

5320

5160

5000

4840

4670

4510

4340

Wind Corrections

SLOPE CORR'D

SLOPE & WIND CORRECTED FIELD LENGTH (M)

FIELD LENGTH

WIND COMPONENT (KTS)

(M)

-15

-10

-5

1200

860

970

1090

1200

1280

1360

1440

1520

1400

1030

1150

1280

1400

1480

1570

1660

1750

1600

1200

1330

1470

1600

1690

1790

1880

1980

1800

1370

1510

1660

1800

1900

2000

2100

2210

2000

1540

1690

1850

2000

2110

2210

2330

2440

2200

1710

1870

2040

2200

2310

2430

2550

2670

2400

1880

2050

2230

2400

2520

2640

2770

2900

2600

2050

2230

2420

2600

2730

2860

2990

3130

2800

2220

2410

2610

2800

2930

3070

3210

3360

3000

2390

2590

2800

3000

3140

3280

3430

3590

3200

2560

2770

2990

3200

3350

3500

3650

3820

3400

2730

2950

3180

3400

3550

3710

3880

4050

3600

2900

3130

3370

3600

3760

3930

4100

4270

3800

3070

3310

3560

3800

3970

4140

4320

4500

4000

3240

3490

3750

4000

4170

4360

4540

4730

4200

3410

3670

3940

4200

4380

4570

4760

4960

4400

3580

3850

4130

4400

4590

4780

4980

5190

4600

3740

4030

4310

4600

4800

5000

5210

5420

4800

3910

4210

4500

4800

5000

5210

5430

5650

5000

4080

4390

4690

5000

5210

5430

5650

5880

PD.30.4

Performance Dispatch

FAA

Takeoff

Category C Brakes

Boeing 737 Operations Manual

Takeoff

Takeoff Field & Climb Limit Weights - Wet Runway

Flaps 5

Sea Level Pressure Altitude

FIELD LIMIT WEIGHT (1000 KG)

CORR'D FIELD

OAT

LENGTH (M)

°C

-40

°F

-40

108

115

122

1400

63.3

57.6

57.2

56.8

56.6

56.4

56.2

55.9

52.0

50.7

49.4

1600

68.3

62.2

61.7

61.3

61.1

60.8

60.6

60.4

56.1

54.7

53.3

1800

72.9

66.3

65.9

65.4

65.2

64.9

64.7

64.5

59.9

58.4

56.9

2000

77.2

70.2

69.7

69.2

69.0

68.7

68.5

68.2

63.4

61.8

60.2

2200

81.2

73.9

73.3

72.8

72.6

72.3

72.0

71.8

66.7

65.0

63.3

2400

85.0

77.3

76.7

76.2

75.9

75.7

75.4

75.1

69.7

67.9

66.2

2600

86.2

80.6

80.0

79.4

79.1

78.8

78.5

78.2

72.6

70.7

68.9

2800

86.2

83.6

83.0

82.4

82.1

81.8

81.5

81.2

75.3

73.4

71.5

3000

86.2

85.6

85.0

84.7

84.4

84.0

83.7

77.7

75.7

73.7

3200

86.2

80.0

77.9

75.9

3400

86.2

82.2

80.1

78.0

3600

86.2

84.3

82.2

80.0

3800

86.2

84.1

81.9

4000

86.2

86.1

83.8

4200

86.2

85.6

4400

86.2

4600

86.2

CLIMB LIMIT

82.5

81.9

81.8

81.6

81.5

81.4

73.5

71.0

68.5

WT (1000 KG)

1000 FT Pressure Altitude

FIELD LIMIT WEIGHT (1000 KG)

CORR'D FIELD

OAT

LENGTH (M)

°C

-40

°F

-40

108

115

122

1400

61.5

55.9

55.5

55.1

54.9

54.7

54.5

53.9

50.2

49.0

47.7

1600

66.4

60.3

59.9

59.5

59.3

59.1

58.8

58.2

54.2

52.9

51.5

1800

70.9

64.4

63.9

63.5

63.2

63.0

62.8

62.1

57.8

56.4

55.0

2000

75.0

68.1

67.6

67.2

66.9

66.7

66.5

65.8

61.2

59.7

58.2

2200

78.9

71.6

71.1

70.6

70.4

70.1

69.9

69.2

64.3

62.7

61.1

2400

82.6

75.0

74.4

73.9

73.6

73.4

73.1

72.4

67.3

65.6

63.9

2600

86.1

78.1

77.5

77.0

76.7

76.4

76.2

75.4

70.0

68.3

66.5

2800

86.2

81.0

80.5

79.9

79.6

79.3

79.0

78.2

72.7

70.8

69.0

3000

86.2

83.6

83.0

82.4

82.1

81.8

81.5

80.6

74.9

73.0

71.1

3200

86.2

86.1

85.5

84.9

84.6

84.3

83.9

83.0

77.1

75.2

73.2

3400

86.2

85.4

79.3

77.2

75.2

3600

86.2

81.3

79.2

77.2

3800

86.2

83.3

81.1

79.0

4000

86.2

85.2

83.0

80.8

4200

86.2

84.8

82.6

4400

86.2

84.3

4600

86.2

86.0

CLIMB LIMIT

80.6

80.0

79.9

79.8

79.7

79.6

78.5

71.1

68.7

66.3

WT (1000 KG)

With engine bleed for packs off, increase field limit weight by 350 kg and climb limit weight by 1250 kg.

With engine anti-ice on, decrease field limit weight by 150 kg and climb limit weight by 200 kg.

With engine and wing anti-ice on (optional system), decrease field limit weight by 750 kg and climb limit

weight by 1350 kg.

PD.30.5

Performance Dispatch

Takeoff

FAA

Category C Brakes

Boeing 737 Operations Manual

Takeoff

Takeoff Field & Climb Limit Weights - Wet Runway

Flaps 5

2000 FT Pressure Altitude

FIELD LIMIT WEIGHT (1000 KG)

CORR'D FIELD

OAT

LENGTH (M)

°C

-40

°F

-40

108

115

122

1400

59.8

54.2

53.8

53.4

53.2

53.0

52.6

52.1

48.5

47.3

46.1

1600

64.5

58.5

58.1

57.7

57.5

57.3

56.8

56.2

52.3

51.0

49.7

1800

68.9

62.4

62.0

61.5

61.3

61.1

60.6

60.0

55.8

54.5

53.1

2000

72.9

66.0

65.6

65.1

64.9

64.7

64.1

63.5

59.1

57.6

56.1

2200

76.7

69.4

69.0

68.5

68.2

68.0

67.4

66.7

62.1

60.5

59.0

2400

80.3

72.6

72.1

71.6

71.4

71.1

70.5

69.8

64.9

63.3

61.7

2600

83.7

75.7

75.1

74.6

74.3

74.1

73.4

72.7

67.5

65.8

64.1

2800

86.2

78.5

78.0

77.4

77.1

76.9

76.2

75.4

70.1

68.3

66.5

3000

86.2

81.0

80.4

79.8

79.6

79.3

78.5

77.8

72.3

70.4

68.6

3200

86.2

83.4

82.8

82.2

81.9

81.6

80.9

80.1

74.4

72.5

70.6

3400

86.2

85.7

85.1

84.5

84.2

83.9

83.1

82.3

76.4

74.5

72.5

3600

86.2

86.1

85.3

84.5

78.4

76.4

74.4

3800

86.2

80.3

78.2

76.2

4000

86.2

82.1

80.0

77.9

4200

86.2

83.9

81.7

79.6

4400

86.2

85.7

83.4

81.2

4600

86.2

85.1

82.9

CLIMB LIMIT

78.6

78.0

77.9

77.8

76.9

75.9

68.7

66.4

64.1

WT (1000 KG)

3000 FT Pressure Altitude

FIELD LIMIT WEIGHT (1000 KG)

CORR'D FIELD

OAT

LENGTH (M)

°C

-40

°F

-40

108

115

122

1400

57.8

52.3

52.0

51.6

51.4

51.0

50.6

50.2

46.8

45.6

44.5

1600

62.4

56.5

56.1

55.7

55.5

55.1

54.7

54.1

50.5

49.2

48.1

1800

66.6

60.3

59.9

59.5

59.3

58.8

58.3

57.8

53.9

52.5

51.3

2000

70.5

63.8

63.4

62.9

62.7

62.2

61.7

61.1

57.0

55.6

54.3

2200

74.1

67.1

66.6

66.2

65.9

65.4

64.9

64.3

59.9

58.4

57.0

2400

77.6

70.2

69.7

69.2

69.0

68.4

67.8

67.2

62.6

61.0

59.5

2600

80.8

73.1

72.6

72.1

71.8

71.2

70.6

70.0

65.1

63.5

61.9

2800

83.9

75.8

75.3

74.8

74.5

73.9

73.3

72.6

67.5

65.8

64.2

3000

86.2

78.2

77.6

77.1

76.8

76.2

75.6

74.9

69.6

67.9

66.2

3200

86.2

80.5

79.9

79.4

79.1

78.5

77.8

77.1

71.7

69.8

68.1

3400

86.2

82.8

82.2

81.6

81.3

80.7

80.0

79.2

73.6

71.7

70.0

3600

86.2

84.9

84.3

83.7

83.4

82.8

82.0

81.3

75.5

73.6

71.8

3800

86.2

85.7

85.4

84.8

84.0

83.2

77.3

75.4

73.5

4000

86.2

85.9

85.1

79.1

77.1

75.2

4200

86.2

80.8

78.7

76.8

4400

86.2

82.5

80.4

78.4

4600

86.2

84.2

82.0

79.9

CLIMB LIMIT

76.2

75.7

75.6

75.5

74.8

74.1

73.2

66.4

64.2

62.0

WT (1000 KG)

With engine bleed for packs off, increase field limit weight by 350 kg and climb limit weight by 1250 kg.

With engine anti-ice on, decrease field limit weight by 150 kg and climb limit weight by 200 kg.

With engine and wing anti-ice on (optional system), decrease field limit weight by 750 kg and climb limit

weight by 1350 kg.

PD.30.6

Performance Dispatch

FAA

Takeoff

Category C Brakes

Boeing 737 Operations Manual

Takeoff

Takeoff Obstacle Limit Weight

Flaps 5

Sea Level 30°C & Below, Zero Wind

Based on engine bleed for packs on and anti-ice off

Reference Obstacle Limit Weight (1000 KG)

OBSTACLE

DISTANCE FROM BRAKE RELEASE (100 M)

HEIGHT (M)

73.4

79.2

83.0

67.2

72.8

77.1

80.3

82.5

84.1

62.2

67.4

71.6

75.0

77.7

79.8

81.4

82.7

83.7

84.6

85.3

58.4

63.4

67.6

70.9

73.7

76.0

77.9

79.5

80.8

81.8

82.7

55.1

60.1

64.2

67.6

70.5

72.8

74.9

76.6

78.0

79.2

80.3

100

52.4

57.3

61.4

64.8

67.6

70.1

72.2

74.0

75.5

76.9

78.1

120

49.9

54.8

58.9

62.3

65.1

67.6

69.8

71.7

73.3

74.7

76.0

140

47.7

52.6

56.6

60.0

62.9

65.4

67.6

69.5

71.2

72.7

74.0

160

45.7

50.6

54.6

58.0

60.9

63.4

65.6

67.6

69.3

70.9

72.2

180

43.9

48.7

52.7

56.1

59.0

61.6

63.8

65.8

67.6

69.2

70.6

200

42.3

47.0

51.0

54.4

57.3

59.9

62.1

64.1

65.9

67.5

69.0

220

45.4

49.4

52.8

55.7

58.3

60.6

62.6

64.4

66.0

67.5

240

44.0

47.9

51.3

54.2

56.8

59.1

61.1

63.0

64.6

66.1

260

42.6

46.5

49.9

52.8

55.4

57.7

59.8

61.6

63.3

64.8

280

45.2

48.6

51.5

54.1

56.4

58.4

60.3

62.0

63.5

300

44.0

47.3

50.2

52.8

55.1

57.2

59.1

60.8

62.3

Obstacle height must be calculated from lowest point of the runway to conservatively account for runway

slope.

OAT Adjustments

REFERENCE OBSTACLE LIMIT WEIGHT (1000 KG)

OAT (°C)

30 & BELOW

-0.6

-0.7

-0.9

-1.1

-1.3

-1.4

-1.1

-1.5

-1.8

-2.2

-2.5

-2.9

-1.7

-2.2

-2.7

-3.3

-3.8

-4.3

-2.2

-2.9

-3.6

-4.3

-5.0

-5.7

-2.8

-3.6

-4.5

-5.4

-6.2

-7.1

-3.3

-4.3

-5.4

-6.4

-7.4

-8.5

-3.8

-5.0

-6.2

-7.4

-8.6

-9.8

-4.4

-5.7

-7.1

-8.5

-9.8

-11.2

-4.9

-6.4

-8.0

-9.5

-11.0

-12.6

-5.4

-7.1

-8.8

-10.5

-12.2

-13.9

Pressure Altitude Adjustments

OAT ADJUSTED OBSTACLE LIMIT WEIGHT (1000 KG)

ALT (FT)

S.L &

BELOW

1000

-1.5

-1.8

-2.2

-2.5

-2.9

-3.2

2000

-3.0

-3.7

-4.3

-4.9

-5.5

-6.1

3000

-4.1

-5.1

-6.2

-7.3

-8.3

-9.4

PD.30.7

Performance Dispatch

Takeoff

FAA

Category C Brakes

Boeing 737 Operations Manual

Takeoff

Takeoff Obstacle Limit Weight

Flaps 5

Sea Level 30°C & Below, Zero Wind

Based on engine bleed for packs on and anti-ice off

Wind Adjustments

OAT & ALT ADJUSTED OBSTACLE LIMIT WEIGHT (1000 KG)

WIND (KTS)

15 T W

-6.0

-6.2

-6.4

-6.6

-6.9

-7.1

10 T W

-4.0

-4.1

-4.3

-4.4

-4.6

-4.7

5 T W

-2.0

-2.1

-2.2

-2.3

-2.4

10 H W

1.3

1.1

1.0

0.8

0.6

0.5

20 H W

2.6

2.2

1.9

1.6

1.2

0.9

30 H W

3.9

3.4

2.9

2.4

1.9

1.4

40 H W

5.2

4.6

3.9

3.2

2.5

1.8

With engine bleed for packs off, increase weight by 550 kg.

With engine anti-ice on, decrease weight by 250 kg.

With engine and wing anti-ice on, decrease weight by 1300 kg (optional system).

PD.30.8

FAA

Category C Brakes

Boeing 737 Operations Manual

Performance Dispatch

Chapter PD

Enroute

Section 31

Enroute

Long Range Cruise Maximum Operating Altitude

Max Cruise Thrust

ISA + 10°C and Below

WEIGHT

OPTIMUM

TAT

MARGIN TO INITIAL BUFFET 'G' (BANK ANGLE)

(1000 KG)

ALT (FT)

(°C)

1.20 (33°)

1.25 (36°)

1.30 (39°)

1.40 (44°)

1.50 (48°)

30300

-5

32800*

32100

30700

31600

-8

34400*

33400

32000

33000

-11

35900*

34800

33400

34500

-15

37300*

36200

34900

36000

-18

38700*

37800

36400

37700

-18

40200*

39400

38100

39500

-18

41000

39900

41000

-18

41000

-18

41000

-18

41000

ISA + 15°C

WEIGHT

OPTIMUM

TAT

MARGIN TO INITIAL BUFFET 'G' (BANK ANGLE)

(1000 KG)

ALT (FT)

(°C)

1.20 (33°)

1.25 (36°)

1.30 (39°)

1.40 (44°)

1.50 (48°)

30300

30600*

31600

-3

32900*

32000

33000

-6

34800*

34800

33400

34500

-9

36300*

36200

34900

36000

-13

37800*

37800

36400

37700

-13

39200*

38100

39500

-13

40800*

39900

41000

-13

41000

-13

41000

-13

41000

ISA + 20°C

WEIGHT

OPTIMUM

TAT

MARGIN TO INITIAL BUFFET 'G' (BANK ANGLE)

(1000 KG)

ALT (FT)

(°C)

1.20 (33°)

1.25 (36°)

1.30 (39°)

1.40 (44°)

1.50 (48°)

30300

27500*

31600

30000*

33000

32800*

34500

-3

34900*

34900

36000

-7

36500*

36400

37700

-7

38000*

39500

-7

39500*

41000

-7

41000

-7

41000

-7

41000

*Denotes altitude thrust limited in level flight, 100 fpm residual rate of climb.

PD.31.1

Performance Dispatch

Enroute

FAA

Category C Brakes

Boeing 737 Operations Manual

Enroute

Long Range Cruise Trip Fuel and Time

Ground to Air Miles Conversion

AIR DISTANCE (NM)

GROUND

AIR DISTANCE (NM)

HEADWIND COMPONENT (KTS)

DISTANCE

TAILWIND COMPONENT (KTS)

100

(NM)

100

279

259

241

226

212

200

190

181

173

166

160

554

515

480

450

424

400

382

365

349

335

322

829

771

720

675

636

600

573

548

525

504

485

1103

1027

958

899

847

800

764

732

701

673

648

1376

1282

1197

1123

1059

1000

956

915

877

843

811

1649

1536

1435

1348

1270

1200

1147

1098

1053

1012

974

1921

1791

1673

1571

1482

1400

1339

1282

1229

1181

1138

2192

2044

1911

1795

1693

1600

1530

1465

1405

1351

1301

2463

2297

2148

2019

1904

1800

1721

1648

1581

1520

1465

2733

2550

2386

2242

2115

2000

1913

1832

1758

1690

1628

3003

2803

2622

2465

2326

2200

2105

2016

1934

1859

1791

3272

3054

2859

2688

2537

2400

2296

2200

2111

2029

1955

3540

3306

3095

2911

2748

2600

2488

2384

2287

2199

2119

3807

3556

3330

3133

2959

2800

2680

2568

2464

2369

2282

4074

3807

3566

3356

3169

3000

2871

2752

2641

2539

2446

4340

4057

3801

3578

3380

3200

3063

2935

2817

2709

2610

4606

4306

4036

3800

3590

3400

3255

3119

2994

2879

2774

4870

4555

4270

4021

3801

3600

3446

3303

3171

3049

2938

5134

4803

4504

4243

4011

3800

3638

3487

3347

3219

3102

5397

5051

4738

4464

4221

4000

3830

3671

3524

3389

3266

5659

5298

4971

4685

4431

4200

4021

3855

3701

3559

3430

5920

5544

5204

4906

4641

4400

4213

4038

3877

3729

3594

6181

5790

5437

5127

4851

4600

4404

4222

4054

3899

3758

6440

6035

5669

5347

5061

4800

4596

4406

4230

4069

3921

6699

6280

5901

5568

5271

5000

4787

4589

4406

4238

4085

PD.31.2

Performance Dispatch

FAA

Enroute

Category C Brakes

Boeing 737 Operations Manual

Enroute

Long Range Cruise Trip Fuel and Time

Reference Fuel and Time Required

PRESSURE ALTITUDE (1000 FT)

AIR

DIST

(NM)

FUEL

TIME

FUEL

TIME

FUEL

TIME

FUEL

TIME

FUEL

TIME

(1000 KG)(HR:MIN)(1000 KG)(HR:MIN)(1000 KG)(HR:MIN)(1000 KG)(HR:MIN)(1000 KG)(HR:MIN)

200

1.5