Technical data

13773-001

27-10

Page 6 30 Nov 2000

(b) Defuel airplane. (Refer to 12-20)

inch (2.8 mm) and a maximum of 0.200 inch (5.0 mm) clearance when aileron is fully

deflected, trailing edge down. In the area near the aileron actuation arm where there is no

leading edge cover, the minimum shall be 0.125 inch (3.2 mm).

(d) Verify overlap between aileron and wing has a minimum of 0.010 inch (0.25 mm) and a

maximum of 0.125 inch (3.2 mm) clearance. Aileron may be deflected downward 0° - 5° to

achieve upper overlap, and may be deflected upward 0° - 5° to achieve lower overlap.

(e) With ailerons streamlined, verify neutral position gap has a minimum of 0.060" (1.5 mm)

and a maximum of 0.150" (3.8 mm) at the two points closest to the aileron cove. Maximum

gap in other areas must be less than 0.210" (5.3 mm).

(f) Remove passenger seats. (Refer to 25-10)

(g) Remove carpet and access panels CF3C and CF4C. (Refer to 6-00)

(h) Verify aileron control cable tension set to 30.0 - 40.0 lb (13.6 - 18.1 Kg). (Refer to 27-10)

(i) Verify aileron cable at kick-out pulleys do not rub against pulley flange. (Refer to 27-10)

(j) Verify aileron neutral position remains at 0° +/- 1° with control yoke in neutral position.

(k) Verify 12.5° +/- 1° aileron up and down travel. (Refer to 27-10)

(l) Verify upper aileron stops show a 0.035 inch (0.89 mm) gap between stops and pulley

bearings at aileron actuation pulleys under full left or right roll input. (Refer to 27-10)

(m) Verify 6° +/- 1° aileron trim deflection. (Refer to 27-10)

(n) Perform Rudder-Aileron Interconnect Inspection/Check. (Refer to 27-20)

(o) Verify minimum rod end thread engagement of 0.312 inch (0.79 cm).

(p) Verify proper installation of safety wires and cotter pins on all fasteners and engagement

of all jam nuts through complete aileron control system.

(q) Install access panels and carpet. (Refer to 6-00)

(r) Install passenger seats. (Refer to 25-10)

(s) Fuel airplane. (Refer to 12-10)