Thrush Aircraft S2RHG-T65 TURBO THRUSH Maintenance Manual page 93

THRUSH AIRCRAFT, INC – MODEL S2RHG-T65 TURBO THRUSH
LEGEND:
† 1050 SHP -60AG; 1050 SHP -45A, -45B, -45R; 1100 SHP – 65B
†† 1050 SHP -60AG; 1020 SHP -45A, -45B, -45R; 1100 SHP – 65B
‡ 38.8 PSI -60AG; 38.8 PSI -45A, -45B, -45R; 43.34 PSI – 65B
‡‡ 37.7 PSI -60AG; 37.7 PSI -45A, -45B, -45R; 43.34 PSI – 65B
* Transient Engine Limits are limited to 5 seconds for starting and 20 seconds
during acceleration.
** The Torque Pressure Limits listed above are for NP = 1700 RPM only.
*** -45A, -45B & -45R = 800; -60AG = 820; -65B = 820; - 65AR = 855
**** -45A, -45B & -45R = 800; -60AG = 775; -65AR = 840
***** -45A, -45B & -45R = 99°to 110; -60AG = 0 to 110
****** -60AG = 0 to 104; - 65B = 0 to 99; -65AR = 10 to 105
******* -65B = 700; -65AR = 715
For PT6A-45A, -45B, -45R, -60AG and -65AG, -65AR, -65B with HC-B5MP-
3C/M10876AS or ANS propeller the following applies:
A. 1170 to 1400 RPM Np is prohibited on Ground
B. Stabilized operation below 900 RPM Np is prohibited – Except in feathered
operation from 0 to 400 RPM Np.
Effective: 9/16/05
AIRCRAFT MAINTENANCE MANUAL
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