B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-42-00-861-001 Energize the Ground Service Network from the External Power 24-42-00-862-001 De-energize the Ground Service Network Supplied from the External Power
27-51-00-820-005 Adjustment of the Flap Rigged Position (With the R Sharks Fin) (OBSOLETE) REPLACED BY 27510082000800 AND R 27510082000900
27-54-45-400-002 Installation of the Torque Shaft 6204CM(6254CM) 31-32-00-860-006 Procedure to Get Access to the SYSTEM REPORT/TEST F/CTL Page 32-12-00-010-001 Open the Main Gear Doors for Access
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
32-12-00-410-001 Close the Main Gear Doors after Access
**ON A/C 001-049, 051-061, 101-103, 201-203, 301-399,
27-50-00-991-006 Fig. 202 R **ON A/C 062-099, 104-149, 151-199, 204-299, 401-499,
27-50-00-991-006-A Fig. 202A
**ON A/C ALL
3. Job Set-up
__________
Subtask 27-50-00-941-061
A. Safety Precautions
(1)
Make sure that the safety barriers are in position.
(2)
Make sure that the warning notice is in position on the panel 114VU to tell persons not to operate the flap/slat controls.
Subtask 27-50-00-860-062
B. Aircraft Maintenance Configuration
(1)
Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER is attached to the flap/slat control lever on the panel 114VU.
(2)
Make sure that the applicable MLG door is open (Ref. TASK 32-12-00-010-001).
(3)
Make sure that the GROUND LOCK SLEEVE is installed on the applicable main gear door actuator.
(4)
Make sure that the access platform is in position in the MLG bay.
(5)
Make sure that the torque shaft assy 6204CM(6254CM) is removed.
(6)
Make sure that the ground service network is energized (Ref. TASK 24-42-00-861-001).
Subtask 27-50-00-865-066
C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 6CV B07 121VU FLIGHT CONTROLS/WTB/FLP/SYS2 12CV P20 121VU FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 8CV Q21 122VU FLIGHT CONTROLS/WTB/FLP/SYS1 10CV S07
4. Procedure
_________
**ON A/C 001-049, 051-061, 101-103, 201-203, 301-399,
(Ref. Fig. 202/TASK 27-50-00-991-006)
R **ON A/C 062-099, 104-149, 151-199, 204-299, 401-499,
(Ref. Fig. 202A/TASK 27-50-00-991-006-A)
**ON A/C ALL
Subtask 27-50-00-866-058
A. Manual Retraction of the Flaps with Pneumatic Wrench
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE
_______ CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE.
(1)
Fully retract the flaps with the ADAPTOR-DRIVE, SLAT (AND FLAP) (98D27804001000) and the pneumatic right-angle wrench.
(2)
Install the PIN RIGGING-FLAPS (TRACK 1) (98D27504005000) at the track 1 rigging pin position. This will set the flaps to the zero degree position.
(3)
Remove the pneumatic right-angle wrench from the ADAPTOR-DRIVE, SLAT (AND FLAP).
Installation of the Flap Rigging Pin at Track 1
Figure 202/TASK 27-50-00-991-006
R 1EFF : 001-049, 051-061, 101-103, 201-203, 1 27-50-00Page 227 1301-399, 1May 01/05 1 1 1CES 1
Installation of the Flap Rigging Pin at Track 1 Figure 202A/TASK 27-50-00-991-006-A
R 1EFF : 062-099, 104-149, 151-199, 204-299, 1 27-50-00Page 228 1401-499, 1Aug 01/05 1 1 1CES 1
(4) Remove the ADAPTOR-DRIVE, SLAT (AND FLAP) from the right angle gearbox 6203CM (6253CM).
Subtask 27-50-00-866-060
B. Manual Retraction of the Flaps without Pneumatic Wrench WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE
_______ CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE.
(1)
Fully retract the flaps with the BAR-TURNING.
(2)
Install the PIN RIGGING-FLAPS (TRACK 1) at the track 1 rigging pin position. This will set the flaps to the zero degree position.
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