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NOTE : When removing tab (13) [9], disengage hinge pins (18) from holes (a) located in the small spar of elevator (3). 2. INSTALLATION OF THE ELEVATOR TAB (Figure 401) A. Tools and consumable materials None B. Procedure NOTE : In case of repair, painting or addition of an option to the elevator tab, check elevator balancing - refer to 51-60-00. Pre-MOD. 128 or Kit OPT10 921700 1) Lubricate hinge pins (18) and the hinges - refer to 12-21-03. Post-MOD. 128 or Kit OPT10 921700 CAUTION : DO NOT LUBRICATE HINGE PINS WHICH ARE PROTECTED BY A TEFLON COAT. 1) Wipe hinge pins (18). Check the teflon coat for evenness. Replace the hinge pins if necessary. S / N 1 - 9999 2) Position hinge pins (18) into the hinges. 3) Position tab (13) [9], insert the end of hinge pins (18) into holes (a) located in the small spar of elevator (3). ABAA Validity : S / N 1 - 9999 55-20-02Page 401 (CA) SEP 04 4) Hold tab (13) [9], secure the hinges with screws (2) and washers (1). NOTE : Secure the bonding strap, if installed. Perform electrical bonding procedure - refer to 20-00-12. 5) Secure the tabs with bolt (7), spacer (11), washer (14) and new nut (15). 6) Secure tab rod (10) to levers (12) with bolt (6), spacer (8), washers (4) and (5) and nut (16). 7) Lock with a new cotter pin (17). 8) Make sure all the tools and materials are removed and the work area is clean and free from debris. 9) Check the tab travel - refer to 27-30-03. ABAA Validity : S / N 1 - 9999 55-20-02Page 402 (CA) SEP 04 1 - Washer 2 - Screw 3 - Elevator 4 - Washer 5 - Washer 6 - Bolt 7 - Bolt 8 - Spacer 9 - R.H. tab 10 - Tab rod 11 - Spacer 12 - Lever 13 - L.H. tab 14 - Washer 15 - Nut 16 - Nut 17 - Cotter pin 18 - Hinge pin Elevator tab - Removal / Installation Figure 401 ABAA Validity : S / N 1 - 9999 55-20-02Page 403 (CA) SEP 04 PAGE INTENTIONALLY LEFT BLANK ABAA Validity : S / N 1 - 9999 55 20-02Page 404 (CA) SEP 04 VERTICAL STABILIZER DESCRIPTION AND OPERATION GENERAL The vertical stabilizer has an entirely metal structure. It supports the rudder. It is secured to the rear of the fuselage with : - the front fitting on frame C7, - the lower bearing on frame C8. The lower bearing is also used as a support for rudder hinge ball joint. 2. LOCATION (Figure 1) COMPONENT QTY AREA ACCESS DOOR REFERENCE ABM |
