Engine Data Pertinent To Thrush Aircraft Inc Installation - Thrush Aircraft S2RHG-T65 TURBO THRUSH Maintenance Manual

THRUSH AIRCRAFT, INC – MODEL S2RHG-T65 TURBO THRUSH
It is important that each nut be moved the same amount to
ensure that the nuts are not moved out of the relationship with
each other.
Do not perform ground testing of the propeller if the wind
exceeds 5 MPH. If any wind at all is present, head the aircraft
to a crosswind.

ENGINE DATA PERTINENT TO THRUSH AIRCRAFT INC INSTALLATION

Low (Ground) Idle
High (Flight) Flight Idle
Fuel Boost Pump Pressure
(Electric & Engine Driven)
Max Reverse
Prop Test (O/S Governor)
Max Propeller RPM
Hydraulic Low Pitch Stop
ENGINE LIMITS CHART (PT6A-65AG SHOWN), for pertinent engine instrument
marking see chapter 8, Figure 1a through 1d.
POWER SETTING
Takeoff
Max. Continuous
Minimum Idle
Starting
Acceleration
(Transient)
Maximum Reverse
4-28
AIRCRAFT MAINTENANCE MANUAL
**CAUTION**
**CAUTION**
TORQUE ITT
SHP
(PSI) ** (°C)
810
1300 † 48.03‡
810
1220†† 45.07‡‡
****
750
*******
1000*
60.98 870*
900 760
-60AG ...........................62.5% +1%, -0% NG
-45A, -45B, -45R ................... 59% ± 1% NG
-65B, -65AR, -65AG ............... 59% ± 1% NG
69% Ng
20 +/-1 psig
8-10 psi
1,598 ± 20 RPM
1,700 RPM
Check in accordance with 1600 RPM NP
(%) NP
NG (RPM)
104 1700
***
104 1700
56
200 maximum
104 1870
1650
OIL OIL
PRESSURE TEMP.
(PSIG) (°C)
90 to 135 0 to 110
90 to 135 0 to 110
60 minimum -40 to 110
-40
minimum
-40 to 110
40 to 200
*****
0 to 110
90 to 135
******
Effective: 5/05/04