THRUSH AIRCRAFT, INC – MODEL S2RHG-T65 TURBO THRUSH
AIRCRAFT MAINTENANCE MANUAL
1-2
Effective: 9/16/05
GENERAL DESCRIPTION
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.
CONTACT INFORMATION
For further information related to this manual, please contact our Product Support
Manager at(229) 883-1440 extension 524.
PRINCIPAL DIMENSIONS
GENERAL
Wing Span Extended Tip
47.5 feet
Overall Length
33.33 feet
Height To Top Of Canopy
10.0 feet
Main Gear Tread
9.35 feet
Main Gear To Tail Wheel
19.71 feet
WING
Type Full
Cantilever
Airfoil Section
NACA 4412
Dihedral 3.50
Degrees
C. G. Range (See Airplane Flight Manual for pertinent data)
Forward Limit
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.
Aft Limit
29.0 Inches Aft Of Datum
28.0 inches for dual cockpit
Datum
Datum Is The Leading Edge Of The Wing.
Aileron Travel
-Up
21 Degrees ±1 Degree
-Down
17 Degrees ±1 Degree
Flap Travel Down
15 Degrees ±1 Degree
