R. Item 16: Rudder trim position
R **ON A/C 401-499,
R (Ref. Fig. 006)
R **ON A/C ALL
ITEM (D) The index is normally displayed in cyan and moves along the scale according to the present trim position. It is displayed in amber when both contol systems are faulty as transmitted by the FWC. It is replaced by amber XX when the value for the trim position is not transmitted.
S. Item 17: Rudder position
R **ON A/C 401-499,
R (Ref. Fig. 006)
R **ON A/C ALL
ITEM (A) The rudder symbol is normally displayed in green. It is displayed in amber when the three hydraulic pressures drop below 1450 PSI as transmitted by the SDAC, or when the FWC transmits three LO PRESS for the three hydraulic pressures.
T. Item 18: Rudder hydraulic status
R **ON A/C 401-499,
R (Ref. Fig. 006)
R **ON A/C ALL
ITEM (B)
(1) Case 1 Each one of the three letters G B Y is normally displayed in green.
1EFF : ALL 1 31-67-27Page 15 1 1 Aug 01/05 1 1 1CES 1
(2)
Case 2 They are displayed in amber when there is a low press on the relevant hydraulic system.
(3)
Case 3 They are not displayed when the status for the relevant hydraulic system is transmitted neither by the SDAC nor by the FWC.
U. Item 19: Trimmable horizontal stabilizer position
R **ON A/C 106-149, 303-399, 401-499,
(Ref. Fig. 005)
**ON A/C ALL
(1)
Case 1 The angle The angle which value ranges from -13.5. to +4., and the UP direction (only displayed below -0.09.) are normally displayed in green.
(2)
Case 2 The angle, and the DN (DOWN) direction (only displayed above +0.09.) are normally displayed in green.
(3)
Case 3 The angle and UP are displayed in amber when there is a low pressure on both the yellow system and the green system as transmitted by the SDAC or the FWC.
(4)
Case 4 The angle and DN are displayed in amber when there is a low pressure on both the yellow system and the green system as transmitted by the SDAC or the FWC.
(5)
Case 5 The value and the direction for the stabilizer position are not displayed and replaced by amber XX when the angle is not available.
(6)
PITCH TRIM Title PITCH TRIM is normally displayed in white. It is displayed in amber in case of a THS jam, as transmitted by the FCDC bus.
1EFF : ALL 1 31-67-27Page 16 1 1 Aug 01/05 1 1 1CES 1
V. Item 20: Elevator (left) Refer to the right elevator (item 11, 12, 13 and 14) as the same description applies.
W. Item 21: Trimmable horizontal stabilizer control PITCH TRIM is normally displayed in white. It is dsiplayed in amber when there is a jam as transmitted by the FCDC.
X. Item 22: ELAC operation The letter 1 or 2 is normally displayed in green with the outline part in grey. They are displayed in amber when the relevant computer is faulty as transmitted by the FCDC. The figure is replaced by an amber X whis the outline part grey when the computer status is not transmitted by the FCDC.
Y. Item 23: Aileron indication (left) Refer to the right aileron indication (item 5, 6, 7 and 8) as the same description applies.
1EFF : ALL 1 31-67-27Page 17 1 1 Aug 01/05 1 1 1CES 1 SYSTEM DISPLAY - FUEL PAGE - DESCRIPTION AND OPERATION
______________________________________________________
1. "FUEL Page"
___________ R **ON A/C 106-149, 401-499,
The FUEL Page is described in the following figure with its 25 parameters as
follows:
(Ref. Fig. 001)
Item 1: Left inner cell fuel quantity
Item 2: Left inner cell temperature
Item 3: Left transfer valve
Item 4: Left outer cell temperature
Item 5: Left outer cell fuel quantity
Item 6: Left tank pumps 1 & 2
Item 7: APU fire valve
Item 8: Engine 1 fire valve (or LP valve)
Item 9: Fuel used - Engine 1
Item 10: Engine related number
Item 11: total fuel used
Item 12: Fuel used - Engine 2
Item 13: Engine number
Item 14: Engine 2 fire valve (or LP valve)
Item 15: Fuel Xfeed valve
Item 16: Right tank pumps 2 & 1(n.1 on the left side, n.2 on the right)
Item 17: Right outer cell fuel quantity
Item 18: Right transfer valve
Item 19: Right outer cell temperature
1EFF : ALL 1 31-67-28Page 1 1 1 Aug 01/05 1 1 1CES 1
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM 指示/記錄系統 8(107)
