THE NEW PIPER AIRCRAFT, INC.
PA-32-301FT / 301XTC
MAINTENANCE MANUAL
PAGE 5
Jun 1/03
4G21
57-40-00
(14) 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.
(15) 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.
(16) Check the rigging and control cable tension of the ailerons and flaps. (Refer to 27-10-00,
Rigging and Adjustment; and 27-50-00, Wing Flap Controls, Rigging and Adjustment.)
(17) Service and refill the brake system with hydraulic fluid in accordance with 12-10-00, Brake
System, Filling. Bleed the system as given in 32-40-00, Bleeding Brakes, and check for fluid
leaks.
(18) Service and fill the fuel system in accordance with 12-10-00, Fuel System, Filling. Open the
fuel valve and check for leaks and flow.
(19) Check the operation of all electrical equipment, and pitot system.
(20) Remove the airplane from the jacks.
(21) Install the cockpit trim panel assembly, spar box carpet, the front and back seats, and wing butt
rubber molding.
(22) Replace all the access plates and panels on the wing involved.
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