ABNORMAL AND EMERGENCY PROCEDURES ECAM ADVISORY CONDITIONS

Question 1

APU OIL QTY
(message LOW OIL LEVEL pulsing)

Answer 1

If there is no oil leak, then the remaining oil quantity allows normal APU operation for about 10 h.

Question 2

CAB PR CAB VERTICAL SPEED V/S > 1 800 ft/min

Answer 2

CPC changeover is recommended: ‐ MODESEL:MAN
‐ Wait 10 s
‐ MODE SEL: AUTO
* If unsuccessful:
‐ MODESEL:MAN
‐ Manual pressure control

Question 3

CAB PR CAB ALTITUDE altitude ≥ 8 800 ft

Answer 3

PACK FLOW: HI
CPC changeover is recommended: ‐ MODESEL:MAN
‐ Wait 10 s
‐ MODE SEL: AUTO
* If unsuccessful:
‐ MODESEL:MAN
‐ Manual pressure control

Question 4

CAB PR ΔP ≥ 1.5 PSI in phase 7

Answer 4

LDG ELEV: ADJUST
* If unsuccessful:
‐ MODESEL:MAN
‐ Manual pressure control

Question 5

ELEC IDG OIL TEMP ≥ 147 °C

Answer 5

Reduce IDG load, if possible (GALLEY or GEN OFF).
If required, restore when the temperature has dropped. Restrict generator use to a short time, if the temperature rises again excessively.

Question 6

ENG OIL PRESS
P < amber threshold value

Answer 6

‐ If the oil pressure indication is amber, continue normal engine operation.
‐ If the oil pressure indication becomes red without the ENG 1(2)
OIL LO PR alert, continue normal engine operation.
In both cases, monitor other engine parameters, particularly oil temperature and oil quantity.

Question 7

ENG OIL PRESS P > 259 PSI

Answer 7

Closely monitor other engine parameters for symptoms of engine malfunction.
If a high oil pressure is not accompanied by other abnormal indications, operate the engine normally for the remainder of flight. Record high oil pressure, and corresponding N2 readings, for maintenance action.

Question 8

ENG OIL TEMP
Oil temperature above the advisory threshold and below the caution threshold.

Answer 8

An increase in oil temperature during normal steady-state operation indicates a system malfunction and should be closely monitored for other symptoms of engine malfunction.
Note: If the OIL TEMP increases at thrust reduction, consider increasing the thrust again in order to attempt to lower the oil temperature.
In addition, an increase in oil temperature could be related to the IDG oil cooling system. To reduce oil temperature, before limits are reached, the following are recommended:
1. Low Speed - Increase engine speed to increase fuel flow and
thereby cool IDG oil.
2. High Speed - Reduce generator load or turn off generator. If the
oil temperature continues to rise, mechanically disconnect IDG.

Question 9

ENG OIL QTY < 1.45 QT

Answer 9

The oil quantity in the tank can decrease at high thrust setting due to the effect of oil gulping. In that case, the indicated oil quantity will increase after thrust reduction.
Monitor the affected engine oil parameters and crosscheck with the other engine - As long as the oil temperature and the oil pressure of the affected engine remain within limits, normal engine operation is not affected.
If the oil quantity continues to decrease, both of the following ECAM alerts can be triggered:
‐ ENG 1(2) OIL LO PR caution
‐ ENG 1(2) OIL LO PR warning.

Question 10

ENG NAC TEMP ≥ 280 °C

Answer 10

Monitor engine parameters and crosscheck with other engine.

Question 11

FUEL Difference between wing fuel quantities greater than 1 500 kg (3 307 lb)

Answer 11

FUEL MANAGEMENT (CHECK)
If a fuel leak is suspected, Refer to ABN-21 Fuel Leak

Question 12

FUEL Fuel temp greater than 45 °C in inner cell, or 55 °C in outer cell

Answer 12

GALLEY (OFF)

Question 13

FUEL Fuel temp lower than -40 °C in inner or outer cell

Answer 13

Consider descending to a lower altitude and/or increasing Mach to increase TAT.

Question 14

OXY CKPT OXY
Pulsing green:
When pressure is < 500 PSI. Amber:
When pressure is < 200 PSI.

Answer 14

If mask is not being used, check if it is correctly stowed.