5. Close-up________
R Subtask 28-42-00-862-051-A
R A. Aircraft Configuration
R (1) If you refueled the aircraft with battery power, on the refuel/defuel
R control panel (800VU), put the BATT POWER switch to the NORM
R position.
R (2) If you have external power available, do the EIS stop procedure
R (Ref. TASK 31-60-00-860-002) then de-energize the aircraft electrical
R circuits (Ref. TASK 24-41-00-862-002).
Status Report (BITE)
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
-
THE FLIGHT CONTROLS
-
THE FLIGHT CONTROL SURFACES
-
THE LANDING GEAR AND THE RELATED DOORS
-COMPONENTS THAT MOVE.
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
GEAR.
1. Reason for the Job
__________________
R R Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s)
No specific safety barriers
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
12-11-28-650-003 Pressure Refuel with Automatic Control 24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
from the External Power 28-25-00-650-001 Pressure Defuel 28-25-00-869-001 Fuel Transfer 31-32-00-860-001 Procedure to Get Access to the SYSTEM REPORT/TEST
Menu Page
31-60-00-860-001 EIS Start Procedure
34-10-00-860-002 ADIRS Start Procedure
1EFF : ALL 1 28-42-00Page 504 1 1 May 01/04 1 1 1CES 1
3. Job Set-up
__________
Subtask 28-42-00-941-050
A. Safety Precautions
(1) Put the safety barriers in position.
Subtask 28-42-00-860-050
B. Aircraft Maintenance Configuration
(1)
Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).
(2)
Do the ADIRS start procedure (Ref. TASK 34-10-00-860-002).
(3)
Do the EIS start procedure (ECAM only) (Ref. TASK 31-60-00-860-001), then:
(a)
On the ECAM control panel (CP), push the FUEL pushbutton switch (P/BSW).
(b)
Make sure that the FUEL page shows on the ECAM lower display-unit (DU).
(c)
On the ECAM CP, push the STS P/BSW.
(d)
Make sure that the STATUS page shows on the ECAM lower DU.
(e) Make sure that there are no FUEL messages under MAINTENANCE. R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
Subtask 28-42-00-650-052
C. Fuel Configuration
(1) If it is necessary to do a test of the cadensicon 19QT1(19QT2) or 20QT, refuel the applicable fuel tank to this quantity (Ref. TASK 12-11-28-650-003):
-
the applicable wing tank to 1500 kg (3306.9330 lb) minimum
-
the center tank to 2000 kg (4409.2440 lb) minimum.
1EFF : ALL 1 28-42-00Page 505 1 1 Aug 01/05 1 1 1CES 1 **ON A/C 301-399,
Subtask 28-42-00-650-052-A
C. Fuel Configuration
(1) If it is necessary to do a test of the ultracomps 50QT and 52QT and/or the dualcomp 53QT, refuel the applicable fuel tank to this quantity (Ref. TASK 12-11-28-650-003):
-
the applicable wing tank to 1000 kg (2204.6220 lb) minimum
-
the center tank to 1500 kg (3306.9330 lb) minimum.
**ON A/C ALL
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