Piper Arrow IV, Руководство по обслуживанию

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13. Connect the leads to the appropriate posts on the terminal strip and install the washers and nuts. (For
assistance in connecting the electrical lead, refer to the Electrical Schematics in Chapter 91.) Place the clamps
along the electrical harness to secure it in position and install the terminal strip dust cover.
14. Remove the cap from the fuel line and connect it at the fitting located forward of the spar at the wing
butt line.
15. Connect the aileron balance and control cables at the turnbuckles that are located within the fuselage
aft of the spar. After the left balance cable has been inserted through the bracket assembly and connected,
install a cotter pin cable guard into the hole that is provided in the bracket assembly.
16. Connect the flap by placing the flap handle in the full flap position, place the bushing on the outside of
the rod end bearing and insert and tighten bolt.
17. Check the rigging and control cable tension of the ailerons and flaps. (Refer to Rigging and
Adjustment of Ailerons, and Rigging and Adjustment of Flaps, Chapter 27.)
18. Service and refill the brake system with hydraulic fluid in accordance with Servicing Brake System,
Chapter 12. Bleed the system as given in Chapter 32 and check for fluid leaks.
19. Service and fill the fuel system in accordance with Servicing Fuel System, Chapter 12. Open the fuel
valve and check for leaks and flow.
20. Check the operation of all electrical equipment, and pitot static system.
21. Remove the airplane from the jacks.
22. Install the cockpit trim panel assembly, spar box carpet, the front and back seats, and wing butt rubber
molding.
23. Replace all the access plates and panels on the wing involved.
FLIGHT SURFACES.
REMOVAL OF AILERON. (Refer to Figure 57-2.)
1. Disconnect the aileron control rod at the aileron attachment point by removing the nut, washers and
bolt from the rod end bearing. To simplify installation note location of washers removed.
2. Remove the attaching screws, with nuts, from the hinges at the leading edge of the aileron, and remove
the aileron by lowering the inboard end and swinging it forward to allow the balance arm to clear the opening
in the outboard rib.
INSTALLATION OF AILERON. (Refer to Figure 57-2.)
1. Install the balance arm into the opening in the outboard rib by moving the inboard end of the aileron
forward to allow the arm to be inserted through the opening. Move the aileron into place and install attaching
screws and nuts. Ascertain that the aileron is free to move with no interference.
2. Attach the aileron control rod with bolts, washers and nut, dividing the washers so that the aileron is
free to rotate from stop to stop without the control rod binding or rubbing on the opening in the aft spar. Be
certain that the rod end bearing has no side play when tightening the bolt and that the rod does not contact the
side of the bracket.
3. Actuate the aileron controls to insure freedom of movement.
57-50-02
Page 57-09
Revised: August 18, 1980
2K10
PIPER AIRCRAFT
PA-28RT-201 / 201T
MAINTENANCE MANUAL