THRUSH S2R-T34 Airplane Flight Manual page 7

Thrush Aircraft Inc
Albany, GA
ENGINE LIMITS: PT6A-41AG, -41, -42 (PT6A-41AG shown)
POWER
SHP
SETTING
Takeoff & Max
750
continuous
Max Climb 700
Max Cruise 700
Idle
Starting
Acceleration
Max. Reverse 750
GENERAL NOTE: The operating parameters in this Table are individual limits for each engine
parameters and do not necessarily apply simultaneously.
*These values are time limited to five (5) seconds.
**Time limited to ten (10) minutes at any operating condition.
***Torque limit shown for N
†For PT6A-42 790ºC.
††For PT6A-42 765ºC.
†††For PT6A-42 100 to 135
STARTER: Maximum starter engagement duration is 30 Seconds followed by a 60 Seconds
cool down period. Total of 3 cycles to be followed by 30 minutes starter cool
down.
AIR STARTS: Normal air starts are approved from sea level to 12,000 feet altitude and from 80
MPH to 126 MPH air speed. See the Emergency Procedures in Section III.
PROPELLER: Hartzell Hub Model HC-B3TN-3C (or HC-B3TN-3D) with Blade Model T-10282,
Diameter 102.5 inches maximum, 92.5 inches minimum or optional Blade Model
T-10282 (N) +4, Diameter 106.5 inches maximum, 98.0 inches minimum.
REVERSE POWER: Do not use in flight
P-3 HEATER: Regardless of fuel type used, the P-3 heater switch must be turned on (if installed)
for flight and ground operations when the free air temperature is below 40 Degrees
F.
FAA APPROVED: Jan. 27, 2009
Model S2R-T34
AIRPLANE FLIGHT MANUAL
***
ITT
TORQUE
(ºC)
(PSI)
64.5 750†
60.2 725††
60.2 725†
1000*
68.4* 850
64.5 750
= 1600-2000 RPM.
P
N N
G P
(%) (RPM)
101.5 2000
101.5 2000
2000
50
102.6 2205
101.5 2000
SECTION I
LIMITATIONS
OIL OIL
PRESS. TEMP.
(PSIG) (ºC)
105 to
0 to 99
135†††
105 to
0 to 99
135†††
105 to
0 to 99
135†††
60 Min. -40 to 99
-40 Min.
99 to 104**
105 to
0 to 99
135†††
Revision 4, SECTION I-2