C. Removal of Equipment
 (1)
 Remove the access platform(s).

 (2)
 Remove the safety barriers.

 (3)
 Remove the warning notice(s).

 (4)
 Remove the ground support and maintenance equipment, the special and

 standard tools and all other items. R
 1EFF : ALL 1 28-10-00Page 314 1 1 Aug 01/04 1 1 1CES 1 TANKS - DESCRIPTION AND OPERATION

_________________________________
 1. General
_______

R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 A. Description
 There is one fuel tank in each wing (divided into an inner and outer cell) and one in the center wing box. The total usable fuel capacity is 23859 liters (6304 USgal). The usable fuel capacity of each tank is shown in Table 001. The total unusable fuel capacity is 82.1 liters (21.7 USgal). The unusable fuel quantities are shown in Table 002.
 **ON A/C 301-399,
 A. Description There is one fuel tank in each wing and one in the center wing box. The total usable fuel capacity is 23700 liters (6260 USgal). The usable fuel capacity of each tank is shown in Table 001. The total unusable fuel capacity is 89.7 liters (23.8 USgal). The unusable fuel quantities are shown in Table 002.
 **ON A/C ALL
 There are also two vent surge tanks. The vent surge tanks are located in each wing outboard of the wing tank.
 Each tank is a part of the aircraft structure. All the materials used to seal the tanks are fully resistant to all the fuels and the fuel additives.
 1EFF : ALL 1 28-11-00Page 1 1 1 Aug 01/05 1 1 1CES 1R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,

 -----------------------------------------------------------------------------
| FUEL | LH Wing | Center | RH Wing | Total |
 | TANK | inner outer | | inner outer | |
 |----------------|------------------|------------|------------------|---------|
 | VOLUME (liter) | 6925 | 880 | 8250 | 6924 | 880 | 23859 |
 | (USgal) | 1829 | 232 | 2180 | 1829 | 232 | 6302 |
 | WEIGHT (kg) | 5436 | 691 | 6476 | 5435 | 691 | 18729 |
 | (lb) | 11984 | 1523 | 14278 | 11983 | 1523 | 41291 |
 -----------------------------------------------------------------------------SG = 0.785 Usable Fuel Tank Capacities Table 001
 -----------------------------------------------------------------------------
| SYSTEM/FUEL TANK | CAPACITY | WEIGHT |
 | | (liter) (USgal) | (kg) (lb) |
 |-----------------------------------|--------------------|--------------------|
 | ENGINE FEED SYSTEM | 25.6 | 6.8 | 20.1 | 44.3 |
 | VENT SYSTEM | 0.0 | 0.0 | 0.0 | 0.0 |
 | REFUEL SYSTEM | 0.8 | 0.2 | 0.6 | 1.4 |
 | BOTH SURGE TANKS | 0.5 | 0.1 | 0.4 | 0.9 |
 | BOTH WING TANK INNER CELLS | 28.0 | 7.4 | 22.0 | 48.4 |
 | BOTH WING TANK OUTER CELLS | 4.0 | 1.1 | 3.1 | 6.9 |
 | CENTER TANK | 23.2 | 6.1 | 18.2 | 40.1 |
 |-----------------------------------|----------|---------|----------|---------|
 | TOTAL | 82.1 | 21.7 | 64.4 | 142.0 |
 -----------------------------------------------------------------------------SG = 0.785 Unusable Fuel Tank Capacities Table 002
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 28-11-00Page 2 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1

R **ON A/C 301-399,

R -----------------------------------------------------------R | FUEL | LH | CTR | RH | Total |
R | TANK | Wing | (Transfer) | Wing | |
R |----------------|---------|------------|---------|---------|
R | VOLUME (liter) | 7750 | 8200 | 7750 | 23700 |
R | (USgal) | 2047 | 2166 | 2047 | 6260 |
R | WEIGHT (kg) | 6084 | 6437 | 6084 | 18605 |
R | (lb) | 13413 | 14191 | 13413 | 41017 |
R ------------------------------------------------------------R SG = 0.785
R Usable Fuel Tank Capacities
R Table 001

R -----------------------------------------------------------------------------R | SYSTEM/FUEL TANK | CAPACITY | WEIGHT |
R | | (liter) (USgal) | (kg) (lb) |
R |-----------------------------------|--------------------|--------------------|
R | ENGINE FEED SYSTEM | 24.5 | 6.5 | 19.2 | 42.4 |
R | VENT SYSTEM | 0.0 | 0.0 | 0.0 | 0.0 |
R | REFUEL SYSTEM | 0.8 | 0.2 | 0.6 | 1.4 |
R | CENTER TANK TRANSFER SYSTEM | 2.6 | 0.7 | 2.0 | 4.5 |
R | BOTH SURGE TANKS | 0.2 | 0.1 | 0.2 | 0.3 |
R | BOTH WING TANKS | 38.4 | 10.2 | 30.1 | 66.4 |
R | CENTER TANK | 23.2 | 6.1 | 18.2 | 40.1 |
　
中國航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護(hù)手冊 AMM FUEL 燃油1(78)