B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-50-00-866-008 Extension of the Flaps on the Ground
27-50-00-866-009 Retraction of the Flaps on the Ground
CMM 575512 (for corrective action)
CMM 575513 (for corrective action)
CMM 575514 (for corrective action)
CMM 575515 (for corrective action)
CMM 575516 (for corrective action)
CMM 575517 (for corrective action)
57-55-11-000-001 Removal of the Flap Track Fairings Nos. 2, 3 and 4
(for corrective action)
57-55-11-400-001 Installation of the Flap Track Fairings Nos. 2, 3 and
4 (for corrective action)
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
57-55-11-991-019 Fig. 601
**ON A/C 301-399,
57-55-11-991-019-A Fig. 601A
**ON A/C ALL
3. Job Set-up__________
Subtask 57-55-11-941-067
A. Safety Precautions
(1)
Put warning notices in the cockpit to tell persons not to operate the flaps or slats.
(2)
Put the safety barriers in position.
Subtask 57-55-11-860-067
B. Aircraft Maintenance Configuration
(1)
Extend the flaps fully (Ref. TASK 27-50-00-866-008).
(2)
Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER is installed on the flap/slat control lever.
(3)
Put the access platform in position below the applicable flap, zone 581(681) or 587(687).
Subtask 57-55-11-865-066
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/FLP/CTL AND/MONG/SYS2 8CV Q21
4. Procedure
_________
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
(Ref. Fig. 601/TASK 57-55-11-991-019)
**ON A/C 301-399,
(Ref. Fig. 601A/TASK 57-55-11-991-019-A)
**ON A/C ALL
CAUTION : BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING
_______
EDGE:
-
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS.
-
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS.
-MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.
Flap Track Fairing - Lateral Movement
Figure 601/TASK 57-55-11-991-019
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 57-55-11Page 604 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
R Flap Track Fairing - Lateral Movement
R Figure 601A/TASK 57-55-11-991-019-A
R 1EFF : 301-399, 1 57-55-11 Page 605
1 1 May 01/04
1 1
1CES 1
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
Subtask 57-55-11-220-060
A. Check of the Flap Track Fairing Lateral Movement
(1) Measure the lateral movement of each movable fairing as follows:
(a)
Move the fairing (with a hand force of between 23 kg (51 lb) and 27 kg (60 lb)) to the left.
(b)
Put a straight edge in a vertical position against the flap trailing edge adjacent to the fairing. Make sure you do not move the straight edge.
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