W DOC AIRBUS | MMEL OPS PROC

LGCIU 2 LH L/G Shock Absorber Proximity Detector

32-32-03ALGCIU 2 LH L/G Shock Absorber Proximity Detector
Applicable to: -
- General Information
SYSTEMS
CONSEQUENCES
PROCEDURES
PITOTS(on ground)
The CAPT pitot is set to the high heating level when the EXT PWR pb-sw is set to OFF.
Keep the EXT PWR pb-sw set to ON until engine start.
AVNCS VENT(on ground)
  • The system remains in the closed circuit configuration
  • (If Installed) The ground cooling system is inoperative.
  • Time limitations on ground for ELEC PWR supply:
    • OAT ≤ 42 °C: No limitation
    • OAT = 53 °C: 3 h
    • OAT = 61 °C: 30 min
  • Check that the air conditioning system is operative.
ADIRU and AVNCS VENT alert(on ground)
The horn and the light are inoperative.
HYD alerts(on ground)
The BLUE ELEC PUMP FAULT light and the YELLOW ENG 2 PUMP FAULT light come on when engines are off.
(If Installed) TPIS(on ground)
The WHEEL TYRE LO PR alert threshold is set to flight level.
LIGHTS(on ground)
(If Installed) The strobe lights are not inhibited.
On ground, set the STROBE sw to OFF.
On ground, with flaps retracted, the logo lights do not come on.
ELEC(on ground)
When only the APU generator or GPU supplies the aircraft, the main galleys are not supplied.
ENG 2(on ground)
The FADEC supply is continuously on.
The automatic start abort is inoperative.
Use the MAN START procedure. Refer to FCOM
The minimum idle is inoperative.
Refer to OpsProc Minimum Idle on Ground
When FLX TO selected, MCT thrust is set.
Use the TOGA for takeoff.
The thrust Reverser is inoperative.
Refer to OpsProc Thrust Reverser
(If Installed) The BUMP function is inoperative.
Do not use the BUMP function.
SLATS(on ground)
The slats are slow from 1 to 0.
AIR COND(on ground)
The air conditioning pack 1 ram air inlet does not close
CARGO DOOR
Only the manual control is operative.
WATER SERVICING(on ground)
The preselect water servicing is inoperative.
RECORDERS(on ground)
The CVR test and the CVR erase functions are inoperative.
The CVR and the DFDR do not stop after engine shutdown.
ECAM(in flight and on ground)
  • On the WHEEL SD Page, the landing gear position indications associated with the LGCIU 2 are displayed XX.
  • The L/G LGCIU 2 FAULT alert is displayed on the EWD.
32-32-03ALGCIU 2 LH L/G Shock Absorber Proximity Detector
Applicable to: -
- General Information
SYSTEMS
CONSEQUENCES
PROCEDURES
PITOTS(on ground)
The CAPT pitot is set to the high heating level when the EXT PWR pb-sw is set to OFF.
Keep the EXT PWR pb-sw set to ON until engine start.
AVNCS VENT(on ground)
  • The system remains in the closed circuit configuration
  • (If Installed) The ground cooling system is inoperative.
  • Time limitations on ground for ELEC PWR supply:
    • OAT ≤ 42 °C: No limitation
    • OAT = 53 °C: 3 h
    • OAT = 61 °C: 30 min
  • Check that the air conditioning system is operative.
ADIRU and AVNCS VENT alert(on ground)
The horn and the light are inoperative.
HYD alerts(on ground)
The BLUE ELEC PUMP FAULT light and the YELLOW ENG 2 PUMP FAULT light come on when engines are off.
(If Installed) TPIS(on ground)
The WHEEL TYRE LO PR alert threshold is set to flight level.
LIGHTS(on ground)
(If Installed) The strobe lights are not inhibited.
On ground, set the STROBE sw to OFF.
On ground, with flaps retracted, the logo lights do not come on.
ELEC(on ground)
When only the APU generator or GPU supplies the aircraft, the main galleys are not supplied.
ENG 2(on ground)
The FADEC supply is continuously on.
The automatic start abort is inoperative.
Use the MAN START procedure. Refer to FCOM
The minimum idle is inoperative.
Refer to OpsProc Minimum Idle on Ground
When FLX TO selected, MCT thrust is set.
Use the TOGA for takeoff.
The thrust reverser is inoperative.
Refer to OpsProc Thrust Reverser
The (If Installed) BUMP function is inoperative.
Do not use the BUMP function.
SLATS(on ground)
The slats are slow from 1 to 0.
AIR COND(on ground)
The air conditioning pack 1 ram air inlet does not close.
CARGO DOOR
Only the manual control is operative.
WATER SERVICING(on ground)
The preselect water servicing is inoperative.
RECORDERS(on ground)
The CVR test and the CVR erase functions are inoperative.
The CVR and the DFDR do not stop after engine shutdown.
ECAM(in flight and on ground)
  • On the WHEEL SD Page, the landing gear position indications associated with the LGCIU 2 are displayed XX.
  • The L/G LGCIU 2 FAULT alert is displayed on the EWD.
"WTRUIB" 2025