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- slack and loose rivets on spacers (10) of levers (12). 6) Inspect input rod (13) for : - slack, buckling, cracks, binding and corrosion, - condition of the attachment rivets of rod end assy, - correct tightening of the attachment nuts of the tapped end, - correct safetying of the jam nut of adjustable yoke end (16), - correct safetying of attachment nuts (17) of the input rod with cotter pins. D. Check of the rudder rotational free play (Tables 201 and 202) 1) With rudder pedals blocked, actuate rudder and check that play at trailing edge lower rib is 0.275 in (7 mm) maximum. 2) If play exceeds 0.275 in (7 mm), perform the following operations a) Mark and remove rudder control rods and levers. b) Clean rods and levers with a clean linffree cloth soaked with cleaning agent (TB 11-002). c) Perform a dimensional check of rudder control supports, rods and levers borings - see Tables 201 and 202. d) Replace the defective components or contact the manufacturer for repair. e) Install rudder control rods and levers - refer to 20-00-11. E. Final steps 1) Make sure all the tools and materials are removed and the work area is clean and free from debris. 2) Install inspection doors 235L and 235R. 3) Install baggage compartment bottom door 242 and close baggage compartment door 219. 4) Install the cowling under hull 218. 5) Install engine cowlings - refer to 71-10-01. ABAA Validity : S / N 1 - 9999 27 20 00 Page 210 (CA) SEP 04 6) Install tail cone 222 - refer to 53-20-00. 7) Remove the warning sign prohibiting main switch-breaker operation. ABAA Validity : S / N 1 - 9999 Page 211 27-20-00 (CA) SEP 04 ITEM THEORETICAL DIMENSION MAXIMUM WEAR DIMENSION BORING DECISION ACTION 1 Dia. 0.2362/0.2381 in (6.0/6.048 mm) Dia. 0.2409 in (6.120 mm) 2 3 4 5 Dia. 0.2362/0.2374 in (6.0/6.030 mm) Dia. 0.2381 in (6.048 mm) 6 7 Dia. 0.3543/0.3551 in (9.0/9.022 mm) Dia. 0.3566 in (9.058 mm) 8 Yaw control/nose landing gear interconnection rods and levers ITEM THEORETICAL |
