PIPER COMANCHE SERVIC! MANUAL e. Remove the top rollers from the nap brackets. After the top rollers are removed. the nap will swinK iorward allowing access for the removal of the lower relle-s. Remove the nap. -4.-10. R.",ovol Of flop. (PA.2 .... 4OO) a. Remove the access plate to the n.p beUcrank located on the rear·und.r side of the wing. Remove the main lear wheel well splash pan. b. A flap step lock Wlit is located at the rear·inboard portion of the rilht winl. Enter through the wheel well and rele ... the Sprinl t.llsion Ind diAIl,ale the step lock. c. Disconnect the nap control rod at the beUcrank. d.
Under the inboard end of the rilht nap is an access plate to the nip step lock ~tum cable. Back the adjusting nut off the cable end. Remove the top rollers from the nap brackets. The nap will swina forward allowinl access for removal of the lower rollers. I"emove the flap. 4-11. R.",oved Of Wing. a. Remove wing root fairinls. all wing inspection panels. and the bottom fuselale access panel. b. Drain the ga. from the wing to be removed. (Refer to Drminl Fuel System. Section U.) c. Drain the brake lines and reservoir. (Refer to Oraininl Brake System. Section U.) d. Remove the front and r.ar seats. e. Set the aircraft on jacks. (Refer to Jacking. Section Il.) f.
Remove front floorboara and main spar cover panels. g. Disconnect aileron balance cables at IUeron beUcraaks and aUeron control cables at center of fuselale. HaTE The afurm of the aileron bellcrank md splice sleeve of the aUeron concrol cable is marked with red paint to iodicate correct cable hook up. If the bellcrank or cable is not marked. mark before diacon· neeting. Use caution that the correct cables are marked. h. Disconnect nap control cables at center of fuselage. (PA-24-180. PA-24-2S0 and PA·24-260) i. Disconnect nap control cable from within the wing. (PA-24-400) j , Disconnect the fuel lines at the wing butt. k, Disconnect the airspeed lines. 1.
Disconnect gear control cables from retraction :'IIechanism at main gear. .. Disconnect brake line and electrical wiring. n, Arranl. a suitable fuselap and winl support cradle. Remove wina jeks. O. Remove the front and rear spar bolts. Within the fuseille. remove the main spar bolts at the spar splice and side of fuselage. p. Remove the wing. 4-12. Removol Of Em,enna9a. -4.-13. Removal Of Rueleler. a. Remove the tail cone fairing. STRUCTURE ISSUED: 8/18/72 1 El0