+---------------------------------------------------------------------+
| Value | Content Description |
|--------------|------------------------------------------------------|
R | | 7C.2.306.10 Engine 2 |
R |--------------|------------------------------------------------------|
R | LPT | Selected LPTC Posiiton |
R | X99 | (-10 to 100 %) |
R | | ECU 7C.1.307.01 Engine 1 |
R | | 7C.2.307.10 Engine 2 |
R |--------------|------------------------------------------------------|
R | GLE | Engine Generator Load |
R | 999 | (0 to 100 %) |
R | | SDAC 29.1.077.01 Engine 1 |
R | | 29.2.077.01 |
R | | 29.1.077.10 Engine 2 |
R | | 29.2.077.10 |
R |--------------|------------------------------------------------------|
R | PD | Precooler Inlet Pressure |
R | 99 | (0 to 50 psi) |
R | | BMC 06F.1.143.01 Engine 1 |
R | | 06F.2.143.01 |
R | | 06F.1.142.01 Engine 2 |
R | | 06F.2.142.10 |
R |--------------|------------------------------------------------------|
R | TN | Nacelle Temperature |
R | X99 | (-55 to 300 C) |
R | | NOTE: Negative values are shown with an N in the |
R | | first position. If there are no negative |
R | | values then the value starts at the first |
R | | position. |
R | | FCW 26.1.322.01 Engine 1 |
R | | 26.2.322.01 |
R | | 26.1.322.10 Engine 2 |
R | | 26.2.322.10 |
R |--------------|------------------------------------------------------|
R | PT2 | PT2 Total Air Pressure at Position 2 |
R | 99999 | (0.0 to 25.000 psia) |
R | | ECU 7C.1.131.01 Engine 1 |
R | | 7C.2.131.10 Engine 2 |
R |--------------|------------------------------------------------------|
R | OIQH | Oil Consumption from the previous flight |
R | X999 | (-9.99 to 20.00 qts/h) |
R | | DMU Engine 1 |
R | | Engine 2 |
R |--------------|------------------------------------------------------|
R | VN | FAN Pick Up N1 Track Vibration |
R | 99 | (0.0 to 10.0) |
R 1EFF : 159-199, 210-210, 1 31-37-73Page 39 1 1 May 01/05 1 1 1CES 1 +---------------------------------------------------------------------+
| Value | Content Description |
|--------------|------------------------------------------------------| R | | EVM 3D.1.227.01 Engine 1 | R | | 3D.1.227.10 Engine 2 | R |--------------|------------------------------------------------------| R | VL | TRF Pick Up N1 Vibration | R | 99 | (0.0 to 10.0) If value is 10.0 then 99 is printed. | R | | EVM 3D.1.227.11 Engine 1 | R | | 3D.1.227.00 Engine 2 | R |--------------|------------------------------------------------------| R | PHA | FAN Pick Up Phase Angle | R | 999 | (0 to 360 deg) | R | | EVM 3D.1.226.01 Engine 1 | R | | 3D.1.226.10 Engine 2 | R |--------------|------------------------------------------------------| R | PHT | TRF Pick Up Phase Angle | R | 999 | (0 to 360 deg) | R | | EVM 3D.1.226.11 Engine 1 | R | | 3D.1.226.00 Engine 2 | R |--------------|------------------------------------------------------| R | VC | FAN Pick Up N2 Track Vibration | R | 99 | (0.0 to 4.0) | R | | EVM 3D.1.230.01 Engine 1 | R | | 3D.1.230.10 Engine 2 | R |--------------|------------------------------------------------------| R | VH | TRF Pick Up N2 Track Vibration | R | 99 | (0.0 to 4.0) | R | | EVM 3D.1.230.11 Engine 1 | R | | 3D.1.230.00 Engine 2 | R |--------------|------------------------------------------------------| R | EVM | Engine Vibration Status Word | R | XXXXX | EVM 3D.1.035.01 Engine 1 | R | | 3D.1.035.10 Engine 2 | R |--------------|------------------------------------------------------| R | OIP | Engine Oil Pressure | R | 999 | (0 to 400 psia) | R | | FWC 26.1.317.01 Engine 1 | R | | 26.2.317.01 Engine 2 | R | | 26.1.317.10 Engine 1 | R | | 26.2.317.10 Engine 2 | R |--------------|------------------------------------------------------| R | OIT | Engine Oil Temperature | R | X99 | (-60 to 250 C) | R | | FWC 26.1.316.01 Engine 1 | R | | 26.2.316.01 Engine 2 | R | | 26.1.316.10 Engine 1 |
R 1EFF : 159-199, 210-210, 1 31-37-73Page 40 1 1 May 01/05 1 1 1CES 1
+---------------------------------------------------------------------+
| Value | Content Description |
|--------------|------------------------------------------------------|
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本文链接地址：A320飞机维护手册 AMM 指示/记录系统 5(2)
