Wiring Diagram for Cessna 177

attached using a .257” (F size) drill bit. (3) Place the steel bushing (P/N 2510-202) in the .257" hole and reconnect the aileron control cable as shown in Figure 2-4, Torque AN3-13A bolt to 20-25 in-lb. -AN3-13A AN960-416 -2510-202 Thru Bellcrank AN960-416L -2510-073 MM-3-300 Rod End Bearing -AN970-3 MS20364-1032 Figure 2-4 (4) Verify that the feel of the controls in roll have not changed as this could indicate that a control cable has come off of the pulley. This bolt replacement should be able to be accomplished without re-tensioning the aileron control cables. vi) Assemble Servo Arm (P/N 7200-096) and 60 inch/lb PMA servo (P/N 8100-064 for 12 volt or P/N 8100-065 for 24 volt). (1) Attach the Servo Arm (P/N 7200-096) to the 60 inch/lb PMA servo (P/N 8100-064 for 12 volt or P/N 8100-065 for 24 volt) using the provided 8-32 x 3/8" flat head screws. (2) Use blue threadlocker (Loctite 242 or equivalent) and torque the screws to 18-20 in-lb. vii) Pause the servo installation and move to the Wiring Harness Mounting Instructions viii) Trim the roll wiring harness to length and terminate wiring harness per the Vizion wiring diagram in the Vizion PMA Installation Guide (TruTrak Doc. 166) using Connector Backshell 9 Pin (P/N 2100-010). Rev: E Appendix B C177 8 Vizion Install Formatted: Deleted TRUTRAK THE AUTOPILOT PEOPLE- ix) Install 60 inch/lb PMA servo (P/N 8100-064 for 12 volt or P/N 8100-065 for 24 volt). (1) Attach the electrical connector to the roll servo and secure it in place with the mounting screws. Torque to approximately 2-3 in-lb. (2) Place the servo behind the mounting bracket with the arm oriented between the servo stops as shown in Figure 2-5, Formatted: Deleted | Figure 2-5 (3) Attach the servo to the Cessna 177 Roll Bracket Assembly (P/N 7200- 093) using 3 AN3-3A bolts with MS35333-39 lock washers and blue threadlocker (Loctite 242 or equivalent) torqued to 20-25 in-lb. x) Install Push Rod (1) Fully thread an AN315-4 nut on the CM-3B-14 Rod End Bearing (P/N 2510-052) then thread the push rod (P/N 2520-061) approximately half way on the rod end bearing. (2) Fully thread an AN345-10 nut on the MM-3-300 Rod End Bearing (P/N 2510-051) that is attached to the aileron bellcrank. (3) Thread the push rod (P/N 2520-061) approximately half way on MM- 3-300 Rod End Bearing (P/N 2510-051). (4) Adjust just rod end bearings so that full aileron deflection will move the servo arm equally between the stops built in to the Cessna 177 Roll Bracket Assembly (P/N 7200-093). (5) Attach the inboard end of the push rod assembly to the servo arm as shown in Figure 2-6, Torque AN3-11A bolt to 20-25 in-lb. Rev: E Appendix B C177 0 Vizion Install Deleted Formatted: TRUTRAK THE AUTOPILOT PEOPLE- MA SERV TRUTRAK -AN970-3 -AN3-11A 2X AN960-10- AN960-10 CM-3B-14 Rod End Bearing Figure 2-6 (6) Adjust push rod so that both rod end bearings are threaded evenly. (7) Use blue threadlocker (Loctite 242 or equivalent) and torque the jam nuts to 20-25 in-lb. Verify that both rod ends can move freely throughout full aileron travel. Rev: E Appendix B C177 10 Vizion Install TRUTRAK THE AUTOPILOT PEOPLE- | xi) Figure 2-7 and Figure 2-8 show full servo installation Figure 2-7 xii) Reinstall Inspection Covers Figure 2-8 (1) Verify that the roll controls move freely and that there is not contact interference between the mounted roll servo assembly and the aileron controls. (2) Reinstall the inspection covers removed at the beginning of the roll servo installation. Rev: E Appendix B C177 11 Vizion Install Deleted: Deleted: Formatted: Formatted: THE AUTOPILOT PEOPLE- TRUTRAK c) Cessna 177 Vizion Roll IPC 4 B 19 Servo Arm to Pushrod 20 15 TYP 2X) 15 17 6 12 10 2 Parts List B ITEM QTY PART NUMBER DESCRIPTION 1 1 8100-064 (12V Volt) 8100-065 (24 Volt) 8200-128 2 1 7200-096 IR 3 1 4 1 2520-061 5 1 2510-202 6 1 2510-073 7 1 2510-052 15 16 15 16 15 16 15 13 15 13 llel-lelllel༄།]༄།8]རྨུ༐N]ཎྜ 8 1 2510-051 9 3 2500-216 10 1 2500-210 11 1 2500-209 12 1 2500-208 PMA in-lb PMA Servo Cessna 177 Roll Hardware (Includes following items) 2.5" PMA Servo Arm Assembly 7200-093 Rev A or later Cessna 177 Roll Bracket Assy 4.75" Push Rod Tapped 1/4-28 and 10-32 Steel Bushing 250 OD X.199 IDX.195L 250 LX 375 OD X.199 ID Aluminum Spacer CM-3B-14 Small Rod End Bearing MM-3-300 8-32 x 3/8 Flat Head Socket Cap Screw SS AN3-13A AN90-416L AN90-416 13 3 2500-132 AN3-4A Bolt 14 3 2500-081 15 9 2500-076 MS35333-39 Internal Lock Washer AN960-10 16 6 2500-075 AN3-3A 17 1 2500-072 AN3-11A 18 1 2500-055 AN345-10 19 1 2500-054 AN315-4 20 2 2500-047 21 1 2500-042 22 1 1450-133 Not 1 AN970-3 Washer MS20364-1032 C177 Roll Doubler 1450-116 Rev B or later Cessna 177 Roll Drill Jig 22 Shown 14 TYP 3X 16 TYP 3X 2 TYP 3X TRUTRAK FLIGHT SYSTEMS, INC. TITLE C177 Roll IPC SIZE DWG NO REV B Document 238 A SCALE SHEET DRAWN BY REVISION HISTORY None REV DESCRIPTION IR Initial Release A Implemented 1450-133 3 DATE 11/1/2017 11/8/2018 2 APPROVED MATERIAL ZDW ZDW 1 OF 1 TOLERANCE ZDW ENG APPROVAL DATE ZDW 11/1/2017 1 4 Rev: E 12 Appendix B C177 Vizion Install TRUTRAK THE AUTOPILOT PEOPLE- 3) Cessna 177 Pitch Servo Bracket Installation a) Pitch Materials List Qty. Description 1 Cessna 177 Pitch Plate 1 Cessna 177 Pitch Arm Trutrak P/N 1450-112 1450-114 7 MS20364-1032 2 AN970-3 2 AN315-4 1 AN3-10A 1 AN3-7A 14 AN3-3A 10 AN960-10 4 MS35333-39 3 8-32 x 3/8 Flat Head Socket Cap Screw SS 2500-216 2 CM-3B-14 Rod End Bearing 2510-052 5 BSPQ-44 Rivet 1 Microfit 6 Position Cable 1M 6000-063 1 MS-34589-20 1 Servo Arm 7200-091 1 1 1 Cessna 177 Pitch Bracket Assembly Cessna 177 Pitch Push Rod Assembly 60 inch/lb PMA servo OR 60 inch/lb 24 Volt PMA servo OR 7200-092 7200-098 8100-064 8100-065 Rev: E Appendix B C177 13 Vizion Install TRUTRAK THE AUTOPILOT PEOPLE- b) Pitch Servo Bracket Mounting Instructions i) The Cessna 177 pitch servo will be mounted in the rear fuselage at the former location (station 263.0) shown in figure 3-1. Servo Mounting Former Figure 3-1 Vizion Install 14 Rev: E Appendix B C177 TRUTRAK THE AUTOPILOT PEOPLE- ii) Remove bulkhead aft of the baggage compartment. iii) Remove the inspection covers located fore and aft of the servo mounting former (station 263.0) of both sides of the aircraft. (1) Remove the tailcone exposing the upper side of the stabilator. Figure 3-2 Rev: E Appendix B C177 15 Vizion Install