|
|
|
|
Daniels Web Site
|
Date: 11-14-2016
|
Number of Hours: 1.10
|
Manual Reference: PAP G2
|
Brief Description: PAP - G2 - Flight Controls
|
|
All of the steps in this section passed with some specific notes as follows:
With stabilator at full trailing edge up and trim at full "NOSE UP", distance between center of AST and center of trailing edge of stabilator is 5/8" (spec is 9/16").
With stabilator at full trailing edge up and trim at full "NOSE UP", distance between bottom of rudder and AST push rod is 5/8" (spec is at least 1/4").
With stabilator at full trailing edge down and trim at full "NOSE DN", distance between center of AST and center of trailing edge of stabilator is 3/8" (spec is 3/8").
With stabilator at full trailing edge up and trim at full "NOSE DN", distance between bottom of rudder and AST push rod is 5/8" (spec is at least 1/4").
With trim at full "NOSE DN", stabilator trailing edge up, and rudder full left, horizontal distance between bottom rudder trailing edge and center of AST pushrod is 7-1/8" (spec is 7-1/8"). Diagonal distance is 8" (spec is 7-5/16")
With trim at full "NOSE DN", stabilator trailing edge up, and rudder full right, horizontal distance between bottom rudder trailing edge and center of AST pushrod is 6-3/4" (spec is 7-1/8"). Diagonal distance is 7-1/4" (spec is 7-5/16")
With left flaperon held faired, right flaperon trailing edge is 1/4" below trail position (spec is 1/4"). With approximate 10 pound up force on right flaperon, flaperon flexes 1/2" from trail position (spec is 1/2")
With stick moved full right, less than 1/8 clearance from fuselage skin (spec is 1/8"). Need to trim inboard edge of right flaperon skin to get 1/8" clearance from fuselage skin. Also noticed that LP4-3 rivet on leading edge of flaperon skin rubs against LP4-3 rivet at actuating bracket. May need to use a CS4 rivet at actuating bracket. Left side is OK.
SECTION G2 IS COMPLETE
|
|
Control Cable Attach Points
|
|
Control Cable and Trim Tray Attach Points
|
|
RH Flaperon Trail Position
|
|
|
|
|
|
|
|
|
Copyright © 2001-2024 Matronics. All Rights Reserved. |