Limitations; Powerplant Limits; Section 1 Limitations - THRUSH S2R-H80 Flight Manual

1.1.

POWERPLANT LIMITS:

ENGINE
FUEL
:
FUEL
CAPACITY
OILS
:
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
Takeoff –
(5 minute limit)
Maximum Continuous
Climb
Ground Idle
Starting
Acceleration
Maximum Reverse
Emergency Governor
AFM H8001 SINGLE & DUAL COCKPIT Revision B
FAA APPROVAL DATE: 3/19/2015
SECTION 1
: General Electric Model GE-H80-100
JET A 1 acc. To AST< D 1655 89 or DERD 2494
JET A acc. to ASTMD 1655 89

: 230 US Gallons

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
TORQUE ITT
% (°C)
800 100 780
800 100 750
800 100 750
550
730
106* 780
710
800 100 780
*Short term overshoot
S2R-H80 Single & Dual Cockpit
AIRPLANE FLIGHT MANUAL

LIMITATIONS:

N
P
(%) N
G
(RPM)
101.5 2080
100.1 2080
100.1 2080
57-60
102.5* 2140*
96 1900
101.5 2080
. – 5 Seconds Maximum.
OIL
OIL TEMP
PRES.
(°C)
(PSIG)
26 to 39 +20 to 85
26 to 39 +20 to 85
26 to 39 +20 to 85
18
+20 to 85
minimum
26 to 39 -20 to 85
26 to 39 +20 to 85
26 to 39 +20 to 85
26 to 39 +20 to 85
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