performance 737

737-600 performance summary

COPYRIGHT 2006 THE BOEING COMPANY

Basic Maximum1

Passengers (FC/EC)

Cargo m3 (ft3)

110 (8/102)

20.4 (720)

110 (8/102)

20.4 (720)

Engines

Boeing-equivalent thrust/flat-rated temperature lb/F CFM56-7B18/3

18,400/86

CFM56-7B22/3

22,000/86

Maximum taxi weight kg (lb)

Maximum takeoff weight kg (lb)

Maximum landing weight kg (lb)

Maximum zero fuel weight kg (lb)

Operating empty weight kg (lb)

Fuel capacity L (U.S. gal)

56,470 (124,500)

56,240 (124,000)

54,650 (120,500)

51,480 (113,500)

37,340 (82,330)

26,020 (6,875)

66,220 (146,000)

65,990 (145,500)

54,650 (120,500)

51,700 (114,000)

37,340 (82,330)

26,020 (6,875)

Design range (MTOW, full passenger payload) nmi (km) 1,280 (2,370) 3,150 (5,830)

Cruise Mach 0.785 0.785

Takeoff field length (SL, 30C, MTOW) m (ft)

Initial cruise altitude (MTOW, ISA + 10C) ft

Engine-out altitude capability (MTOW, ISA + 10C) ft

Landing field length (MLW) m (ft)

Approach speed (MLW) kias

1,615 (5.310)

41,000

22,900

1,335 (4,380)

125

1,880 (6,180)

39,800

17,300

1,335 (4,380)

125

Fuel burn/seat

500 nmi kg (lb)

1,000 nmi kg (lb)

26.7 (58.9)

46.8 (103.2)

26.6 (58.7)

46.7 (103.0)

Typical mission rules. Two-class seating. Data does not reflect Tech Insertion.

1 Highest optional weight.



Basic Maximum1

Passengers (FC/EC)

Cargo m3 (ft3)

126 (8/118)

27.3 (964)

126 (8/118)

27.3 (964)

Engines


19,700/86

CFM56-7B26/3

26,100/86







60,550 (133,500)

60,320 (133,000)

58,050 (128,000)

54,650 (120,500)

38,410 (84,690)

26,020 (6,875)

70,300 (155,000)

70,080 (154,500)

58,600 (129,200)

55,200 (121,700)

38,410 (84,690)

26,020 (6,875)

Design range (MTOW, full passenger payload) nmi (km) 1,560 (2,885) 3,380 (6,255)







1,645 (5,410)

41,000

20,100

1,415 (4,650)

129

1,675 (5,500)

38,400

16,900

1,425 (4,690)

130

Fuel burn/seat

500 nmi kg (lb)

1,000 nmi kg (lb)

23.7 (52.3)

41.5 (91.4)

23.6 (52.1)

41.4 (91.2)

Typical mission rules. Two-class seating. Data does not reflect Tech Insertion. With optional winglets.


737-700ER Performance summary

737-PS-2012 10/6/06 DR/GG COPYRIGHT 2006 THE BOEING COMPANY

737-700ER 737-700ER

4 auxiliary tanks 9 auxiliary tanks

Passengers BC

Cargo m (ft)

48

14.0 (494)

48

5.2 (183)

Engines

Boeing equivalent thrust/flat-rated temperature lb/F

CFM56-7B24/3

23,700/86

CFM56-7B26/3

26,100/86







71,900 (158,500)

71,670 (158,000)

60,780 (134,000)

57,150 (126,000)

40,310 (88,860)

33,610 (8,880)

77,790 (171,500)

77,560 (171,000)

60,780 (134,000)

57,150 (126,000)

40,990 (90,380)

40,530 (10,707)

Design range (MTOW, full passenger payload) nmi (km)

Cruise Mach

Takeoff field length (SL, 86F, MTOW) m (ft)

Initial cruise altitude capability (MTOW, ISA + 10C) ft (m)



4,865* (8,853)*

0.777

1,745 (5,730)

38,000 (11,580)

1,475 (4,840)

132

5,675 (10,510)

0.779

2,080 (6,840)

36,300 (11,050)

1,475 (4,840)

132

Fuel burn/seat

1,000 nmi kg (lb)

3,000 nmi kg (lb)

101.2 (223.2)

289.1 (637.3)

102.1 (225.0)

292.3 (644.4)

Typical mission rules. Auxiliary fuel tanks are optional. 737-700ER with optional winglets. Data does not reflect CFM Tech Insertion engines.

* Fuel volume limited.

737-700ER Performance summary

737-PS-2013 10/6/06 DR/GG COPYRIGHT 2006 THE BOEING COMPANY

737-700ER 737-700ER

3 auxiliary tanks 6 auxiliary tanks

Passengers (FC/EC)

Cargo m (ft)

76 (16/60)

17.9 (633)

76 (16/60)

8.5 (299)

Engines

Boeing equivalent thrust/flat-rated temperature lb/F

CFM56-7B24/3

23,700/86

CFM56-7B26/3

26,100/86







72,350 (159,500)

72,120 (159,000)

60,780 (134,000)

57,150 (126,000)

40,250 (88,730)

31,650 (8,363)

77,790 (171,500)

77,560 (171,000)

60,780 (134,000)

57,150 (126,000)

40,940 (90,270)

37,560 (9,923)

Design range (MTOW, full passenger payload) nmi (km)

Cruise Mach


Initial cruise altitude capability (MTOW, ISA + 10C) ft (m)



4,360* (8,070)*

0.780

1,765 (5,800)

37,800 (11,520)

1,475 (4,840)

132

5,080 (9,405)

0.780

2,080 (6,840)

36,300 (11,050)

1,475 (4,840)

132

Fuel burn/seat

1,000 nmi kg (lb)

3,000 nmi kg (lb)

66.1 (145.8)

190.0 (419.0)

66.8 (147.2)

192.2 (423.8)

Typical mission rules. Auxiliary fuel tanks are optional. 737-700ER with optional winglets. Data does not reflect CFM Tech Insertion engines.

* Fuel volume limited.


Basic Maximum1

Passengers (FC/EC)

Cargo m3 (ft3)

162 (12/150)

44.0 (1,555)

162 (12/150)

44.0 (1,555)

Engines


23,700/86

CFM56-7B27/3B1F

28,400/86







70,760 (156,000)

70,530 (155,500)

65,310 (144,000)

61,680 (136,000)

41,720 (91,990)

26,020 (6,875)

79,240 (174,700)

79,010 (174,200)

66,360 (146,300)

62,730 (138,300)

41,720 (91,990)

26,020 (6,875)

Design range (MTOW, full passenger payload) nmi (km) 1,970 (3,645) 3,065* (5,675)*







2,025 (6,650)

38,300

16,600

1,630 (5,360)

141

2,230 (7,330)

35,900

14,900

1,655 (5,440)

142

Fuel burn/seat

500 nmi kg (lb)

1,000 nmi kg (lb)

20.5 (45.1)

36.2 (79.7)

20.5 (45.2)

36.2 (79.7)

Typical mission rules. Two-class seating. Data does not reflect Tech Insertion. With optional winglets.

*Fuel volume limited.


737-900ER performance summary

Basic

Maximum1 One auxiliary

tank1

Two auxiliary

tanks1

Passengers (FC/EC)

Cargo m3 (ft3)

180 (12/168)

51.6 (1,824)

180 (12/168)

51.6 (1,824)

180 (12/168)

47.4 (1,674)

180 (12/168)

44.9 (1,585)

Engines

Boeing-equivalent thrust/flat-rated temperature lb/F

CFM56-

7B26/3

26,100/86

CFM56-

7B27/3B1F

28,400/86

CFM56-

7B27/3B1F

28,400/86

CFM56-

7B27/3B1F

28,400/86







74,610 (164,500)

74,380 (164,000)

67,720 (149,300)

64,090 (141,300)

43,890 (96,780)

26,020 (6,875)

85,360 (188,200)

85,130 (187,700)

71,350 (157,300)

67,720 (149,300)

43,890 (96,780)

26,020 (6,875)

85,360 (188,200)

85,130 (187,700)

71,350 (157,300)

67,720 (149,300)

44,380 (97,860)

27,970 (7,390)

85,360 (188,200)

85,130 (187,700)

71,350 (157,300)

67,720 (149,300)

44,530 (98,190)

29,660 (7,837)

Design range (MTOW, full passenger payload) nmi (km) 1,795 (3,325) 2,795* (5,175)* 2,995* (5,545)* 3,175* (5,885)*

Cruise Mach 0.790 0.791 0.791 0.791






2,010 (6,590)

36,800

16,700

1,540 (5,050)

138

2,675 (8,770)

34,000

12,200

1,610 (5,270)

141

2,675 (8,770)

34,000

12,200

1,610 (5,270)

141

2,675 (8,770)

34,000

12,200

1,610 (5,270)

141

Fuel burn/seat

500 nmi kg (lb)

1,000 nmi kg (lb)

19.7 (43.5)

35.2 (77.5)

19.7 (43.5)

35.2 (77.5)

19.8 (43.7)

35.4 (78.0)

19.9 (43.8)

35.4 (78.1)

Typical mission rules. Two-class seating.

With optional winglets.


Auxiliary fuel tanks are an optional feature.

*Fuel volume limited.

737-900ER performance summary


performance 737

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