Technical data

13773-001
27-20
Page 16 31 July 2001
(f) Remove excess slack from interconnect arm to forward clamp by pulling excess bungee
through clamp.
(g) Set roll trim to full left.
(h) Remove excess slack from interconnect arm to aft clamp by pulling excess bungee
through clamp.
(i) Position aileron rigging template on wing.
(j) Verify that steady rudder application will move the ailerons the required travel while also
ensuring that at full aileron trim travel, the bungee does not get tensioned.
(k) Install fuselage floor access panel 3C. (Refer to 6-00)
(l) Install rear passenger compartment carpeting.(Refer to 6-00)
(4) Inspection/Check - Rudder-Aileron Interconnect
(a) Verify interconnect adjustment will meet the requirements of FAR 23.177 or optionally:
1
full left rudder deflection causes 5° minimum, 8° maximum right aileron trailing edge
down.
2
full right rudder deflection causes 5° minimum, 8° maximum left aileron trailing edge
down.
(b) Verify bungee cord ends are folded back upon themselves and securely terminated with
vinyl electrical tape or electrical heat shrink wrap.
(c) Verify positive bungee cord clearance under slack and full cross control movement.
(d) Verify minimum 0.06 inch clearance between interconnect arm and aileron cable turnbuck-
les. Shim arm with washers if necessary to obtain correct clearance.