THRUSH S2R-H80 - Section 1: Limitations; Aircraft Limits and Specifications

S2R-H80 Single & Dual Cockpit
AIRPLANE FLIGHT MANUAL
AFM H8001 SINGLE & DUAL COCKPIT Revision B Page 1
FAA APPROVAL DATE: 3/19/2015
SECTION 1 LIMITATIONS:
1.1. POWERPLANT LIMITS:
ENGINE : General Electric Model GE-H80-100
FUEL: JET A 1 acc. To AST< D 1655 89 or DERD 2494
 JET A acc. to ASTMD 1655 89
FUEL
CAPACITY: 230 US Gallons
OILS :
 AERO SHELL TURBINE OIL 500 acc. to MIL L 23699C
 AERO SHELL TURBINE OIL 560 acc. to MIL L 23699C
 MOBILE JET OIL II acc. to MIL L 23699C
 Synthetic oil B3V acc. to TJU 38 101295 85
 EASTMAN TURBO OIL 2380
 CASTROL 599
 ROYCO TURBINE OIL
The purity of filled oil should meet the max. grade 8 in accordance with NAS 1638
standard or max. grade 11 in accordance with GOST 17216-71 standard.
POWER SETTING
SHP
TORQUE
%
ITT
(°C)
(%) N
G
N
P
(RPM)
OIL
PRES.
(PSIG)
OIL TEMP
(°C)
Takeoff –
(5 minute limit)
800
100
780
101.5
2080
26 to 39
+20 to 85
Maximum Continuous
800
100
750
100.1
2080
26 to 39
+20 to 85
Climb
800
100
750
100.1
2080
26 to 39
+20 to 85
Ground Idle
550
57-60
18
minimum
+20 to 85
Starting
730
26 to 39
-20 to 85
Acceleration
106*
780
102.5*
2140*
26 to 39
+20 to 85
Maximum Reverse
710
96
1900
26 to 39
+20 to 85
Emergency Governor
800
100
780
101.5
2080
26 to 39
+20 to 85
*Short term overshoot. – 5 Seconds Maximum.