THRUSH AIRCRAFT, INC – MODEL S2RHG-T65 TURBO THRUSH
The Thrush Aircraft Inc Turbo Thrush is designed especially for agricultural flying. It is a
monoplane featuring a full cantilever low wing and all metal construction. The design and
construction of the airframe components assure all structural integrity, flight safety, and
minimum maintenance requirements. The Turbo Thrush is designed for the highest crash
load factors in the industry. Safety and reliability of operation and maximum pilot crash
protection are proven and effective features of the design. The high strength overturn
structure is a proven design. The fuselage and overturn structure, constructed throughout
of chrome-moly steel tubing, is immensely strong in the cockpit area.
For further information related to this manual, please contact our Product Support
Manager at(229) 883-1440 extension 524.
Wing Span Extended Tip
Overall Length
Height To Top Of Canopy
Main Gear Tread
Main Gear To Tail Wheel
Type
Airfoil Section
Dihedral
C. G. Range (See Airplane Flight Manual for pertinent data)
Forward Limit
Aft Limit
Datum
Aileron Travel
-Up
-Down
Flap Travel Down
1-2
AIRCRAFT MAINTENANCE MANUAL
GENERAL DESCRIPTION
CONTACT INFORMATION
PRINCIPAL DIMENSIONS
GENERAL
WING
47.5 feet
33.33 feet
10.0 feet
9.35 feet
19.71 feet
Full Cantilever
NACA 4412
3.50 Degrees
Forward Limit at 7600 pounds and below is
22.5 inches aft of datum.
Forward Limit at 10500 pounds is 26 inches
aft of datum with straight line variations to
7600 pounds at 22.5 inches.
29.0 Inches Aft Of Datum
28.0 inches for dual cockpit
Datum Is The Leading Edge Of The Wing.
21 Degrees ±1 Degree
17 Degrees ±1 Degree
15 Degrees ±1 Degree
Effective: 9/16/05