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AtAA Validity : S / N 1 - 433 53-10-01Page 802 (BA) SEP 04 Frames and fittings - Reinforcement of frame C4 Figure 801 AAAA Validity : S / N 1 - 433 53-10 01Page 803 (BA) SEP 04 1 - Frame C4 2 - Shim 3 - Angle bracket 4 - Rivet 5 - Door 6 - Rivet 7 - Rivet 8 - Gusset 9 - Rivet 10 - Doubler 11 - Rivet (see NOTE 1) 12 - Washer (see NOTE 1) 13 - Bulkhead 14 - Rivet (see NOTE 1) 15 - Stiffener 16 - Rivet 17 - Rivet 18 - Bolt 19 - Washer 20 - Nut (see NOTE 1) 21 - Rivet 22 - Lower angle bracket 23 - Support lower side panel 24 - Upper angle bracket 25 - Support upper side panel 26 - Unfolding wedge 27 - Unfolding strip 28 - Angle bracket 29 - Stiffener 30 - Bolt (see NOTE 1) Frames and fittings - Reinforcement of frame C4 Key to Figure 802 WA Validity : S / N 1 - 433 53-10-01Page 804 (BA) SEP 04 Frames and fittings - Reinforcement of frame C4 Figure 802 WA Validity : S / N 1 - 433 53 10-01Page 805 (BA) SEP 04 16) Position gusset (8), counterdrill with a drill No. 20 (dia. 4.1 mm). Remove, deburr then rivet gusset (8) to angle bracket (3) and to the fuselage bottom sheet. 17) Position door (5), counterdrill with a drill No. 20 (dia. 4.1 mm). Remove then deburr door (5). 18) Vacuum-clean the chips inside the fuselage. 19) Make sure all the tools and materials are removed and the work area is clean and free from debris. 20) Rivet door (5) to the cargo compartment floor. 21) If disconnected, reconnect the wing flaps control system - refer to 27-50-00. 22) Check the wing flaps for correct operation - refer to 27-50-01. 23) Make sure all the tools and materials are removed and the work area is clean and free from debris. 24) Install the rear cowling under hull 218A. 25) Install the rear bench - refer to 25-12-00. AAA Validity : S / N 1 - 433 53-10 Page j uN80016 01 (BA) REAR FUSELAGE STRUCTURE DESCRIPTION AND OPERATION 1. GENERAL The rear fuselage structure is a metallic, aluminium alloy structure of semi-monocoque design. The rear fuselage structure consists of : - the frames, - the cross beams and stringers, - the fairings, - the skins, - the fittings. 2. LOCATION (Figure 1) COMPONENT QTY AREA ACCESS DOOR REFERENCE |
