(4)
On the upper ECAM DU, on the MEMO page:
-the N WHEEL STEERG DISC indication goes out of view.
(5) Do an EIS stop procedure (Ref. TASK 31-60-00-860-002). Subtask 09-10-00-862-051
F. De-energize the aircraft electrical circuits
(1)
If you energized the aircraft with the tractor (Ref. TASK 24-41-00-862-002).
(2)
If you energized the aircraft with the APU (Ref. TASK 24-41-00-862-002).
(3)
If you energized the aircraft with the engine (Ref. TASK 24-41-00-862-002).
EFF : ALL 09-10-00Page 231 Aug 01/05R CES
TASK 09-10-00-584-003
Towing with the Main Gear from the Front
R NOTE : For aircraft with cabin and/or cargo compartment(s) floor panels
____ R removed, smooth and low-speed towing is recommended.
1. Reason for the Job
__________________
To tow the aircraft with the main landing gear from the front.
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific movable taxiway plates
No specific towing strap
No specific tractor
D23156000 1 PIN
98A09001002000 1 CABLE, TOWING - MLG
98A09003000001 1 BAR - STEERING NOSE WHEEL
98A09003500000 1 CABLE, TOWING - MLG
98D09104000001 2 TOWING ATTACHMENT
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
05-57-00-200-001 Aircraft Stability 09-10-00-584-001 Towing 29-10-00-863-002 Pressurize the Yellow Hydraulic System 29-10-00-864-002 Depressurize the Yellow Hydraulic System 31-60-00-860-001 EIS Start Procedure 31-60-00-860-002 EIS Stop Procedure 32-00-00-481-001 Installation of the Safety Devices on the Landing
Gears
09-10-00-991-004 Fig. 205
09-10-00-991-005 Fig. 206
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
**ON A/C 001-003, 051-052,
09-10-00-991-014 Fig. 210 R **ON A/C 004-049, 053-099, 101-149, 151-199, 201-299, 301-399, 401-499,
09-10-00-991-014-A Fig. 210A
**ON A/C ALL
3. Job Set-up
__________
Subtask 09-10-00-941-051
A. Aircraft Maintenance Configuration
(1)
Only tow the aircraft if the ground conditions let you. If necessary, put down the applicable surface equipment: slopes, movable taxiway plates, etc. Only try to turn if the ground conditions let you.
(2)
Make sure that the safety devices are installed on the landing gears (Ref. TASK 32-00-00-481-001).
(3)
Make sure that the engine cowls are closed.
(4)
On the N/W-steering deactivation electrical-box 5GC:
-set the ground-towing control lever to the towing position.
(5)
Install the PIN (D23156000).
(Ref. Fig. 206/TASK 09-10-00-991-005)
(6)
Do an EIS start procedure (Ref. TASK 31-60-00-860-001).
(7)
On the upper ECAM DU, on the MEMO page:
-the N WHEEL STEERG DISC indication comes into view.
(8)
On the panel 400VU:
R - make sure that the pressure indication on the yellow brake-pressure triple-indicator is correct: 3000 psi (206.8427 bar). The pointer must be in the green range.
-if necessary, pressurize the Yellow hydraulic system (Ref. TASK 29-10-00-863-002).
NOTE : A pressure of 3000 psi (206.8427 bar) lets you operate the
____
brake seven times.
(9) On the panel 110VU:
-set the PARKING BRK control-switch to OFF.
Subtask 09-10-00-210-063
B. Aircraft Stability
(1) Make sure that the aircraft is stable (Ref. TASK 05-57-00-200-001). **ON A/C 001-003, 051-052,
Subtask 09-10-00-480-052
C. Installation of the Towing Attachment and Towing Cable
(Ref. Fig. 210/TASK 09-10-00-991-014)
WARNING : MAKE SURE THAT THE NLG DOWNLOCK SAFETY PIN AND THE TWO DOOR
_______
SAFETY PINS ARE INSTALLED.
(1)
Install the TOWING ATTACHMENT (98D09104000001) on each main landing gear.
(2)
Install the CABLE, TOWING - MLG (98A09001002000) or CABLE, TOWING -MLG (98A09003500000) on the towing fittings.
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