THRUSH AIRCRAFT, INC – MODEL S2R-G10
AIRCRAFT MAINTENANCE MANUAL
Page 7-2 Effective: 03/26/2010
EMPENNAGE........................................................................................................15
EMPENNAGE REMOVAL................................................................................15
EMPENNAGE INSTALLATION ........................................................................15
Horizontal Stabilizer..........................................................................................15
Figure 7-9: Empennage Exploded View.....................................................16
Figure 7-10: Stabilizer Attachment to Fuselage .........................................17
VERTICAL STABILIZER ..................................................................................17
WINGS...................................................................................................................18
WING REMOVAL .............................................................................................18
WING INSTALLATION .....................................................................................19
Figure 7-11: Wing Spar Inboard Splice ......................................................20
Figure 7-12: Wing Spar Splice ...................................................................22
Figure 7-13: Attach Angle Mounting to Spar Web......................................23
WING INSTALLATION WHEN ATTACH ANGLES ARE REPLACED..............24
Figure 7-14: Attach Angle Mounting to Fuselage Frame............................25
Table 7-1: CONTROL SYSTEM TROUBLESHOOTING CHART...................27
AILERON SYSTEM..........................................................................................27
FLAP SYSTEM ................................................................................................27
RUDDER SYSTEM ..........................................................................................28
ELEVATOR SYSTEM ......................................................................................28
ELEVATOR SYSTEM (Continued)...................................................................29
ELEVATOR TRIM SYSTEM.............................................................................29
FLIGHT CONTROL STATIC BALANCE LIMITS.............................................30
TABLE 7-2: Static Balance Limits ...............................................................30
For example, 29” x 3.45# = 100 #” (55.2 oz/16 = 3.45#) .................................30
For example, 16” x 3.31# = 53 #” (53 oz/16 = 3.31#) ......................................30
For example, 21.1” x 1.96# = 41.4 #” (31.4 oz/16 = 1.96#) .............................30
Table 7-3: Wing Splice Fittings Torque Chart..............................................31
To Next Page
Loading...
