TABLAS FAA.

GOV
Pág. 1 de 9
Aircraft Type Load on
one main
gear leg
All-up Mass j) (Máximum Apron Mass)
(Operating Mass Empty) Standard Aircraft Tire Pressure
Ib | kg psi kg/cm 2 Mpa Gear

1 2 3 4 5 6 7

Airbus A300M-B2 47.0 174 122

1 304,012 137,897
1.20
2 198,413 89,999 8

Airbus A300M-B2 47.0 186 13.1 1.28

3 315,035 142,898
4 198,413 89,999 8

Airbus LA300M-B4 47.0 - 203 14.3 1.40

5 339,266 153,889 8
6 198,413 89,999

Airbus A300 M - B4 47.0 215 15.1 1 48

7 349,208 158,398
8 -198,413 89,999 8

Airbus A300M-B4 47.0 218 15.3 1 50

9 354,718 160,898
10 198,413 89,999 8

Airbus A300M-B4 47.0 216 15.2 1.49

11 365,741 165,898 8
12 198,413 89,999

Airbus A300M-B4
47.0 168 11.8 1.16
13 (Option-al Landing qear 30.5/60) 365,741 165,898 8
14 198,413 39,999

Airbus A300 - 600 47.5 186 131 1.28

15 365,741 165,898
16 198,413 89,999 10

Airbus A300 -600

47.5 168 11.8 1.16
17 {Optional Landing qear 30,5-601 365,741 165,898
18 198,413 89,999 10

Airbus A300 - 600R 47.5 194 13.6 1.34

19 380,611 172,642
20 198,413 89,999 10

Airbus A300 - 600R

47.5 175 12.3 1.21
21 (Optionat Landing ciear 33,5/.60i 380,611 172.642 10
22 198,413 89,999

Airbus A31 0-200 46.7 179 12.6 1.23

23 291,010 132,000 4
24 168,909 76,616

Airbus A310 -200 46.7 188 13.2 1.30

25 305,561 138,600
26 169,198 76,747 4

Airbus A310 -200 46.6 193 13.6 1.33

27 319,444 »' 44 ,898
28 182,983 83,000 4

Airbus A310 - 30G 47.2 207 14.5 1.43

29 332,672 150,898
30 182,983 83,000 4

Airbus A310 - 300 47.2 215 15.1 1.48

31 348,104 157,898
32 182,983 83,000 4

Airbus A310 -300 47.2 187 13.1 1.29

33 363,636 164,943
34 182,983 83,000 4

Airbus A319-100 46.3 173 12.2 1.19

35 141,975 64;399
36 85,979 38,999 4

Airbus A31 9-1 00 46.0 187 13.1 1 29

37 155,203 70,399
38 85,979 38,999 4

Airbus A31 9-1 00 45.7 200 14.0 1.38

39 167,326 75,898
40 85,979 38,999 4

Airbus A320-1 00 Dual Landing Gear 47.1 186 13.1 1.28

41 145,505 66,000
42 82,019 37,203 4

Airbus A320-1 00 Duaf Landing Gear 47.1 194 13.63 1 34

43 149,914 68:000
44 87,524 39,700 4
 TABLAS FAA.GOV, Página 2 de 9
Airaran Type
All-up Mass j) (Máximum Apron Mass) Load on one Standard Aircraft
(Operating Mass Empty) main gear leg Tire Pressure
Ib kg (%) , psi kg/cm 2 Mpa Gear

1 2 3 4 5 6 7 8

Airbus A320-100 Bogie

47.1 162 11.38 1.12
45 Landing Gear 149,914 68,000
46 • 88,721 40,243 8

Airbus A320-200 Dual

46.9 200 14.0 1.38
47 Landing Gear 162,919 73,899
48 90,366 40,989 4

Airbus A320-200 Bogie

46.9 177 12.43 1.22
49 Landing Gear 162,919 73,899 8
50 90,366 40,989

Airbus A320-200
46.7 200 14.05 1 .38
51 167.328 75,899 4
52 94,797 42,999

Airbus A320-200
46.5 209 14.68 1.44
53 170,635 77,399
v
54 99,206 44, 999 4

Airbus A321-100 47.8 186 13.07

55 172,840 78;399 1.28,
56 103,616 46,999 4

Airbus A321-100
47.3 197 13.84 1 36
57 183,862 83,398 4
58 103,616 46,999

Airbus A321 -100

47.8 202 14.19 1.39
59 188:272 85,399 4
60 103,616 46,999

Airbus A321 -200

47.5 212 14.89 1.46
61 197,090 89,399 4
62 103,616 46,999

Airbus A330-200
47.4 206 14.47 1 42
63 509,040 230,897
64 271,165 122,999 4

Airbus A330-300 Basic 47.55 190' 13.35

65 469,359 212,898 1.31 10
66 275,575 124,999

Airbus A330-300X 47.9 202 14.19 1.39

67 493,610 223,893 10
68 282,189 127,999

Airbus A340-200 48 186 13.07 1.28

69 560,850 254,398
70 330,690 150,000 10

Airbus A340-300 Basic 48 - 189 13.28

71 560,850 254,398 1.30 10
72 330,690 150,000

Airbus A340-300X
48 199 13.98 1.37
73 «'i 590,612 267,897 10
74 -330,690 150,000

ATR 42 Basic Tires 46.2 109 7.66 0.75

75 36,861 16,720 4
76 22,675 10,285

ATR 42 Low-Pressure
46.2 75 5.27 0.52
77 Tires 36,861 16,720 4
78 22,758 10,323

ATR 72 Basic Tires 47.8 114 8.01 0.79

79 47,466 21,530
80 26,896 12,200 4

Avro RJ 70 3) Standard
46.0 119 836 0.32
81 Tires 84,500 38,329
82 49,500 22,453 4

Avro RJ 70 ,) Low
46.0 81 5.69 0.56
83 Pressure Tires 84,500 38,329
84 49,500 22,4^3 4

Avro RJ 70 ,) Low
46.0 76 5.34 0.52 4
85 Pressure Tires 84,500 38,329
86 49,500 22,453

Avro RJ 85 2) Standard
47.1 135 9.48 0.93
87 Tires 93,500 42,411 4
51,300 23,269
88
 TABLAS FAA.GOV
Página 3 de 9
Aircraft Type Load on one
Atl-up Mass ,) (Máximum Apron Mass) main gear leg
(Operatíng Mass Empty) - (%) Standard Aircraft Tire Pressure
Ib \ kg psi kg/cm7 Mpa ruedas

1 2 3 4 5 6 7 8

Avro RJ 85 2) Low
47,1 99 6.95 0.68 4
89 Pressure Tires 93.500 42,411 4
90 51,300 23,269

Avro RJ1002) Standard

47.2 143 10,05 0.99 4
91 Tires 98,000 44,452
92 53,700 24,358

AvroRJ1002) Low
47.2 108 7.59 0.74 4
93 Pressure Ti res • 98,000 44,452
94 53,700 24,358

95 Bae ATP 50,550 22,929 46.5 86 6.04 0.59 4

96 32,000 14,515

Bae 1-11 Series 400 47.5 135 9,48 0.93 4

97 87,500 39,689
98 49,600 22,498

Bae 1-11 Series 475 47.5 83 5.83 057 4

99 98,500 44,679
100 51,700 ^3,451

101 Bae 1-11 Series 500 105,500 47,854 47.5 157 11.03 1.08 4
102 ,t 54,580 24,757

103 Rao 1 OE; And 23,370 10,600 45.5 112 7.87 0.77 4
-104 12,529 5,683

105 Bae 125-600 25,000 11,340 45.5 120 8.43 0.83 2

106 12,529 5,683

Bae 125-800 Low

92 6.46 0.63 2
107 Pressure Tires 25,500 11,567
108 15,500 7,031

Bae 125-800 Standard

130 9.13 0.90 2
109 Tires 27,400 12,428
110 15,500 7,031

Bae14o'-1Q02) Standard
46.0 117 8.22 0.81 4
111 Tires 84,500 38,329
112 49.500 22,453

Bae 146-1 00 2) Low

46.0 77 5.41 0.53 4
113 Pressure Tires 84,500 38,329
114 49,500 22,453

115 Bae 146-200 2) 93,500 42,411 4

47.1 133 9.34 0.92
Standard Tires
116 51,300 -23,269

Bae 1 46-200 2) Low 4

47.1 95 6,67 0.65
117 Pressure Ji res 93,500 42,411
118 51,300 23,269

Bae 146-300 2) Standard

47.2 137 9.62 0.94 4
119 Tires 95,500 43,318
120 53,700 24,358

121 Bae 146-300 2) Low 95,500 43,318 47.2 99 6.95 0.68 4

<22 Pressure Tires 53,700 24,358

123 Bae 748 46,500 21,092 43.6 • 86 6.04 0.59 4

124 26,859 12,183

125 B707-120B 258,000 117,027 46.7 170 11.94 1.17 8

126 127,500 57,833

127 B707-320B 328,000 148,778 46.0 180 12.64 1 ?A 8

128 142,780 64,764

129 B707-320C (Freigther) 336,000 152,407 46.7 180 12.64 1.24 8

130 135,503 61,463

TABLAS FAA.GOV
Página 4 de 9
Aircraft Type AIl-up Mass -j) (Máximum Apron Mass) Load on one
(Operating Mass Empty) main gear ieg Standarc 1 Aircraft Tire Pressure
Ib | kg (%) psi kg/cm2 Mpa RUEDAS

1 2 3 4 5 6 7 8
 B707-320C (Convertible) 46.7 180 12.64 1 24 8
131 336,000 152,407
132 148,303 67,269

133 B707-320/420 316,000 143,335 46.0 180 12.64 1.24 8

134 142,600 64.682

135 B720 229,999 104,326 47.4 145 10.20 1 00 4

136 110,800 50,258

137 B720B 234,999 106,594 46.4 145 10.20 1.00 4

138 115,000 52.163

139 B727-100 170,000 ' 77,111 45.2 165 11.59 1.14

140 87,695 39,778
4

141 B727-100C 161,000 73,028 45.4 158 11.10 1.09

142 87,598 39,734
4
B727-200 (Standard) 46.2 167 11,73 1.15 4
143 173,000 78,472
144 . 97,649 44,293

D 46.7 148 10.40

145 B727-200 185,800 84,278 1.02 4
146 97,599 44,270

147 B727 (Advanced) 191,000 86,636 46.6 148 10.40 1.02 4

148 97,768 44,347

149 B727 (Advanced) 197700 89,675 46.4 167 11.73 1 15

150 98,040 44,470
4

151 B727 (Advanced)' 210,000 95,255 ,16.1 167 11.73 1.15

152 100,700 45,677
4

153 B737-100 / 97,800 44,361 46.2 133 9.34 092

154 57,190 25,941
4

155 B737-200 100,800 45,712 46.4 138 9.69 0.95

156 57,190 25,941
4

157 B737-200 116,000 52,617 45.5 160 11.24 1.10

158 60,170 27,293
4

159 B737-200 116,000 52,617 45.5 91 6.39 0.63 4

160 60,170 27,293

B737-200/200C
46.4 168 11.80 1 16 4
161 (Advanced) 117,500 53.297
162 63,749 28,916

B737-200/200C •
46.3 178 12.50 1.23 4
163 (Advanced) 125,000 ..56,699
164 61.438 27,868

B737-200 (Advanced) 46.0 183 12.86 1.26 4

165 128,600 58,332
166 64,238 29,138

167 B737-300 135,500 61,462 45.9 165 11.59 1.14 4

168 ,72,500 32,885

169 B737-300 135,500 61,462 45.9 195 13.70 1.34 4

170 72,500 32,885

171 B737-400 143,000 64,864 46.9 209 14.68 1.44 4

172 72,000 32,659

173 B737-400 (HGW) 150,500 68,266 46.9 185 13.00 1 27 4

174 72,000 32,659

B737-500 Standard Tire

46.1 14)4 13.63 1 34 4
175 Pressure 134,000 60,781
176 72,000 32.659

TABLAS FAA.GOV
Página 5 de 9
Aircraft Type All-up Mass (Máximum Apron Mass) (Operating Load on one f.
Mass Empty) main gear leg Standard Aircraft Tire Pressure
Ib \ kg (%) psi kg/cm 2 Mpa
Ruedas
1 2 3 4 5 6 7 8

B737-500LowTire Pressure 46.1 164 11.52 1.13

177 134,000 60,781
178 72,000 32,659 4
 B737-600 45.83 . 180 12.64 1.24
179 145,000 65,771
180 80,000 36,287 4

B737-700 45.35 193 13.56 1.33

181 155,000 70,307 4
182 80,000 36,287

B737-800 46.79 204 14.33 1.41

183 174,700 79,243 4
184 100,000 45,359

1 41
B737-900 48.27 204 14.33
185 174,700 79,243 4
186 100,000 45,359

B737-BBJ 45.86 204 14.33

187 171,500 77,791 1 41 4
188 100,000 45,359

B747-100 23.4 218 15.31 1 50

189 713,000 323,412 16
190 358,000 162,386

B747-100B 23.1 226 15.88 1.56

191 738,000 334.752 16
192 381,479 173,036

B747-100B 23.1 191 13.42 1.32

193 753,000 341555 16
194 378,908 171,870

16
B747-100BSR 24.1 151 10.61 1.04
195 523,000 237,229
196 362,755 164,543

B747-SP 22.9 . 189 13.28 1.30

197 663,500 300,959 16
198 325,658 147,716

- B747-SP 21.9 203 14.26 1.40

199 703,010 318,880
200 326,275 147,996 16

B747-200B 23.6 199 13.98 1 .37

201 778,000 352,895
202 381,148. 172,886 16

B747-200C 23.1 189 13.28 1.30

203 823,000 373,307
204 367,619 166,749 16

205 836,000 379,204 139

B747-200F 22.7 202 14.19
206 345,337 156,642 16

B747-300 22.7 189 13.28 1.30

207 836,000 379,204 16
208 385,500 174,860

B747-400 23.4 205 14.40 1.41

209 873,000 395,987 16
210 390,000 176,901

B757-200 *> 45.2 170 11.94 1.17

211 -240,965 109,300 8
212 125,66? 57,000

B757-200 (HGW) 46.2 181 12.72 1.25

213 251,000 113,852 8
214 130,000 58,967

B767-200 46.3 190 13.35 1.31

215 317,025 143,800 8
216 175,929 79,800

B767-200ER "- 46.4 190 13.35 1.31

217 388,000 175,994 8
218 200,000 90,719

B767-300 46.3 175 12.29 1.21

219 351,858 159,600
220 188,936 85,700 . 8

B767-300ER 46.0 200 14.05 1.38

221 409,000 185,519 8
222 200,000 90,719

TABLAS FAA.GOV Pág. 6 de 9

AirÜraft Type

All-up Mass (Máximum Apron Mass) (Operating Load on one Standard Aircraft Tire
Mass Empty) main gear leg Pressure
. Ib | kg (%) psi kg/cm 2 Mpa Ruedas

1 2 3 4 5 6 7 8
 12
B777-200A 47.71 182 12.79 1.25
223 537,000 243,579
224 291,900 132,404

B777-200B 47.49 197 13.84 1.36 12

225 582,000 263,991
226 301 ,400 136,713

B777-200B HGVtf 47.37 201 14/12 1.38 12

227 592,000 268,527
228 301,400 136,713

B777-200B PLUS 46.89 215 15.10 1 48 12

229 634,500 287,805
230 301,400 136,713 -

Caravelle Series 10 46.1 109 7.66 0.75 8

231 114,640 52,000
232 64,010 29,034

Caravelle Series 12 46.0 128 8.99 0.88 8

233 123,370 55.960
234 70,110 31,801

Concorde 48.0 183 12.86 1.26 8

235 408,000 185,066
236 173,500 78,698

CanadairCL44 47.5 162 11.33 1 12 8

237 211,000 95,708
238 89,000 40,370

Canadair Regional Jet 46.6 168 11.80 1.16 4

239 51,251 23,247
240 30,100 '13,653

Convair880M 46.6 150 10.50 1.03 8

241 193,499 87,770
242 88,615 40,195

Convair 990 48.5 186 13.05 1.28 8

243 255,000 115,666
244 120,560 54,685

DC-3 46.8 45 3.16 0.31 2

245 25,199 11,430
246 17,123 7,767

DC-4 46.8 77 5.40 0.53 4

247 73,002 33,113
248 48,667 22,075

DC-8-43 46.5 177 12.43 1.22 8

249 318,000 144,243
250 136,509 61,920

DC-8-55 47.0 139 13.28 1.30 8

251 328,000 148,778
252 138,266 62,716

DC-8-61/71 48.0 189 13.28 1.30 8

253 328,000 148,778
254 152,101 68,992

DC-8-62/72 46.5 187 13.14 1.29 8

255 353,000 160,118
256 143,355 65,025

DC-8-63/73 47.6 194 13.63 1 34 8

257 358,000 162,386
258 158,738 " 72,002

DC-9-15 46.2 130 090 4

259 91,500 41,504 Q 1°
260 49,163 22,300

DC-9-21 47.15 142 9.98 098 4

261 101,000 45,813
262 52,644 23,879

DC-9-32 46.2 152 10.68 1 05 4

263 109,000 49,442
264 56,855 25,789

DC-9-41 46.65 160 11.24 1,10 4

265 115,000 52,163
266 61,335 27,821

DC-9-51 47.0 170 11.94 1 17 4

267 122,000 55,338
268 64,675 29;336

TABLAS FAA.GOV
Página 7 de 9
Aircraft Type

All-up Mass i) (Máximum Apron Mass) Load on one main

(Operafing Mass Empíy) gear ieg Standard Aircraft Tire Pressme
Ib Kg (%) psi kg/cm ' Mpa Ruedas

1 2 3 4 5 6 7 8

10
DC10-10 4715 186 13.07 1.28
269 433,000 196,406
270 240.171 108,940
271 DC10-10 443.001 200,942 4685 190 13.35 1.31
272 232,100 105,279 10

273 DC10-15 458,002 207.746 4665 194 13.63 1 34

274 232,100 105,279 10

275 DC-1 0-30/40 558,000 253,105 37.7 • 170 11.94 1.17

276 266,191 120,742 10

277 DC-1 0-30/40 575,001 260,816 37.6 175 12.29 1.21

278 275,501 124,965 10

279 np m ^nMn 593,002 268,982 37.9 180 12.64 1.24

280 LJ^J- \ U~OUf *4U 275,501 124,965

281 MD-11 605,500 274,651 39.2 ¿05 14.40 1.41

282 279,987 127,000 10

283 MD-81 141,000 63,957 4775 170 11.94 1 17

284 81,460 36,950 4

,285 MD-83/MD-88 150,500 68,266 47.55 184 12.93 1.27

286 81,460 36,950 4

287 MD-83 6í
.161,000 73,028 47.4 195 13.70 1 34
288 83,294 37782 4

289 MD-87 141,000 63,957 47.9 170 11.94 1 17

290 75,062 34,048 4

291 MD-90-30 157,000 71.214 48.22 200 14.05 1.38

292 88,171 39,994 4

293 MD-95-30 ,. 115,000 52,163 4749 168 11 80 1.16

294 68,301 30,981 4

295 DHC7 DASH 7 43,800 19,867 4675 107 7.52 0.74

296 26,000 11,793 2

DASH8Sene100 Standard
47.1 131 9.20 0.90
297 Tires 34,700 15,740
298 22,000 9,97^ 4

DASH 8 Serie 100

47.1 77 5.41 0.53
299 Optional Tires 34.700 15,740
300 22,000 9,979 4

301 Dornier 228-101/201 13.250 6,010 44.2 70 4.92 0.48

302 8.224 3,730 2

303 Dornier 228-202 13,734 6,230 45.1 74 5.20 0.51

304 3,354 3,789 2

305 Dornier 228-212 14,175 6,430 45.1 75 5.27 0.52

306 8.398 .3,809 2

307 Dornier 328-1 00 30,247 13,720 46.2 116 8.15 0.80

308 19,423 8,810 2

309 EMB120RT 25,529 1 1 ,580 47.4 115 808 0.79

310 17,066 7,741 2

311 EMB120ER 26,609 12,070 474 127 8.92 0.87

312 17,213 7,808 2

313 EMB 145 RT 42,549 19,300 47.2 ' 131 9.20 0.90
314 25,573 1 1 ,600 4
 TABLAS FAA.GC
Página 8 de 9
Atrcraft Type
AÍI-up Mass i) (Máximum Apron Load on one
Mass) (Operating Mass Empty) main gear leg Standard Aircraft Tire Pressure
Ib- | kg (%) psi kg/cm2 Mpa Ruedas

1 2 3 4 5 6 7 8

EMB145ER , 47.2 139 9.76 0.96

315 45,635 20,700
316 25,573 , 1 1 ,600 4

317 Fokker 27 Standard Mk 45,000 20,412 47.35 80 5.62 0,55

318 200/400/500/600 25,000 11,340 4

Fokker 27 RFV Mk
47.3 58 4.08 0.40
319 200/400/500/600 45,000 20,412
320 25,000 11,340 4

Fokker 28 Mk1 000 High Tire

46,4 100 7.03 0.69
321 Pressure 66,500 30,164
322 35,000 15,876 4

Fokker 28 Mk 1 000 Low Tire

46.4 " 70 4.92 0.48
323 Pressure 66,500 30,164
324 35,000 15,876 4

Fokker 28 Mk 2000 High Tire

46.9 102 7.17 0.70
325 Pressure 65,000 29,484
326 35,000 15,876 4

Fokker 28 Mk 2000 Low Tire

46.9 71 4.99 0,49
327 Pressure 65,000 29,484
328 35,000 15,876 4

Fokker 28 Mk3000/4000 High

46.5 101 7.10 0.70
329 Tire Pressure 73,000 33,112
330 38,000 17,237 4

Fokker 28 Mk3000/4000 Low

46.5 78 5.48 0.54
331 Ti re Pressure 73,000 33,112
332 38,000 17,237 4

333 Fokker 50 High Tire Pressure 45,900 20,820 47.8 85 5.97 0.59

334 27,886 v 12,649 80 5.62 0.55 4

335 Fokker 50 Low Tire Pressure 45,900 20,820 47.8 60 4.22 0 41

336 27,886 12,649 4

337 Fokker 1 00 98,500 44,679 47.8 142 9.98 098

338 53,736 24,374 4

339 HS 125-400 23,369 10,600 45.5 111 7.85 077

340 12,529 5,683 2

341 HS 125-600 25,000 11,340 45.5 120 8.46 0,83

342 12,529 5,683 2

343 HS748 46,500 21,092 43.6 86 6.02 0.59

344 26,859 12,183 4

345 L-1 00-20 155,800 70,670 24.1 105 7.38 0.72

346 75,409 34,205 4

347 L-10Q-30 155,800 70,670 24.2 105 7.38 0.72

348 76,502 34,701 4

349 L-1 011-1 432,000 195,952 47.4 193 13.56 1.33

350 240,000 108,862 8

351 L-1 01 1-1 00/200 468,000 212,281 46.8 175 12.30 1.21
352 244,682 110,986 8

353 L-1 011 -500 498,000 225,889 46.2 184 12.93 1.27
354 . 240,136 108,924 8

41.5 70 4.89 0.48

355 L410UVP-E 14,110 6,400
356 9,579 4.345 2

357 Trídent 1 P 134,835 61,160 46.0 150 10.50 1.03

358 73,200 33,203 2

359 Trident 9P 145,501 65,998 47.0 155 10.91 1.07

360 74,913 33,980 2
 TABLAS FAA.GOV

Página 9 de 9

Load on one main

Aircraft Type gearleg
Alf-up Mass -,) (Máximum Apron Mass) (%)
(Operating Mass Empty) Standard Aircraft Tire Press u re
Ruedas
Ib | kg psi kg/cm 2 Mpa
1 2 3 4 6 6 7 8

Trident 3E 45.5 165 11.62 1.14

361 150,501 68,266
362 86,112 39,060 4

363 VC10-1150 " 334,999 151953 48.3 147 10.30 1.01

364 158,600 71,940 8

365 YS-11A 51,800 23,496 45.11 77 5.41 0.53

366 34,170 15:499 4

367 ANTONOVAn 124-100 864,203 391,996 11.0 149 10.47 1.03

368 379,191 171,998 24

369 IL - 86 461,869 209,501 31.2 128 8.99 0.88

370 244,713 111,000 8

371 IL - 62M 370,377 168,000 47.0 157 11.03 1.08

372 157,410 71400 8

373 IL-62 358,472 162,^00 47.0 157 11.03 1.08

374 146,387 66,400 8

375 IL - 76T 376,991 171,000 23.5 93 6.53 0.64

376 184,747 83,800 8

377 Saab 340B 28,800 13,063 46,5 115 8.08 0.79

378 17,715 8,035 8

379 Saab 2000 50,706 23,000 47.5 165 11.59 1.14

380 30,203 13,700 2

381 TU-134A - 104,940 .47,600 45.6 121 8.50 0.83

382 64,706 '29,350 4

383 TU-154B 216,053 98.000 45.1 135 9.48 0.93

384 117,947 53,500 8

385 Raytheon 1900D 17,059 7,738 47.4 93 6.53 0.64

386 9,460 4,291 2

387 Raytheon 1900C 16,601 7,530 48.7 93 6.53 0.64

388 9,460 4,291 2