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TABLAS FAA.GOV
Pág. 1 de 9
| |Aircraft Type |All-up Mass j) (Máximum Apron |Load on |Standard Aircraft Tire Pressure| |
| ||Mass) (Operating Mass Empty) |one main | | |
| | | |gear leg || |
| | |Ib | kg | |psi |kg/cm 2|
| | |Ib|kg |(%) , |
| | |Ib \ kg | |psi|
| | |Ib | kg |(%) |psi |kg/cm2 |
| | |Ib \ kg|(%) |psi |kg/cm 2 |
| | |. Ib | kg |(%) |psi |kg/cm 2|
| ||Ib |Kg |(%) |psi |
| | |Ib- | kg |(%) |psi|kg/cm2 |

|
|Ib | kg |
|psi |kg/cm 2 |Mpa |Ruedas | |
|1 |2 3 |4 |6 |6 |7 |8 | |361 |Trident 3E |150,501 |68,266 |45.5 |165 |11.62|1.14 | | |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...
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