Aircraft Landing Gear Design: Principles and Practices

Chapter 14: Design Data

This chapter provides a summary of data that may be useful to the landing gear designer. It includes tables of information on various aircraft to permit comparative flotation evaluation, tables showing landing gear characteristics and tires used, illustrations of typical landing gears, and detail design data. The tables are self-explanatory and no discussion is therefore provided.

TABLES 14.1 14.8

Table 14.1: Commercial Aircraft Characteristics for Flotation Analysis

Airplane designation

Max gross weight, 1000 lb

Main landing gear

Wheels per strut

Tire size

Inflation pressure, psi

Type [a]

DC-3

28.0

1

170.0 16

50

S

DC-4

82.5

2

15.5 20

82

T

DC-6B

107.0

2

15.5 20

107

T

DC-7C

143.0

2

17 20

127

T

DC-8-63F

358.0

4

44 16

200

TT

DC-9-41

115.0

2

41 15

165

T

DC-10

533.0

4

50 20-20

185

[b]

L-100-30

155.0

2

56 20

105

ST

L-1011

409.0

4

50 20

175

TT

L-188

116.0

2

13.5 16

135

T

L-1049

140.0

2

17.0 20

130

T

B-707-320C

336.0

4

46 16

180

TT

B-720B

235.0

4

40 14

145

TT

B-727-200

173.0

2

49 17

168

T

B-737-200

111.0

2

40 14

145

T

B-747B

775.0

4

46 16

210

DTT

Convair 440

50.0

2

34 9.9

75

T

880

185.0

4

39 13

150

TT

990

253.0

4

41 15

170

TT

A300B4-200

365.7

4

49 17

180

TT

F-27-40

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