THRUSH AIRCRAFT INC – T660 TURBO THRUSH
Type
Airfoil Section
Dihedral
C. G. Range (See Airplane Flight Manual for pertinent data)
-Fwd Limit
-Aft Limit
Aileron Travel
-Up
-Down
Flap Travel Down
HORIZONTAL STABILIZER AND ELEVATORS
Span
Elevator Travel
-Up
-Down
Trim Tab Travel
-Up
-Down
Rudder Travel
Rudder Trim Tab Travel
1 – 3
AIRCRAFT MAINTENANCE MANUAL
WING
VERTICAL STABILIZER AND RUDDER
Full Cantilever
Naca 4412
3.50 Degrees
24.5 Inches Aft Of Datum
30.0 Inches Aft Of Datum
(Datum Is The Leading Edge Of The Wing.)
21 Degrees ±1 Degree
17 Degrees ±1 Degree
15 Degrees ±1 Degree
204 Inches (17')
27 Degrees ±1 Degree
17 Degrees ±1 Degree
8 Degrees ±1 Degree
22 Degrees ±1 Degree
22 Degrees ±1 Degree
0 Degrees to Max 8.6 Degrees Trailing Edge
Left
Effective: 12/17/03