Mahindra GIPPSAERO GA8-TC 320 - Power Plant Limitations and Instrument Markings

C01-01-08 5 Feb 2009 Page 2-3
Section 2
Model GA8-TC 320 Limitations
2.4. POWER PLANT LIMITATIONS
2.4.1. Engine
Manufacturer: Lycoming Engines
652 Oliver Street
Williamsport, Pennsylvania, 17701, USA
Model: Lycoming TIO-540-AH1A
2.4.2. Engine Limitations
MAXIMUM
TEMPERATURES
PRESSURE LIMITS (See Notes)
FUEL OIL
Cyl
Head
TIT Oil Min Max Min Max
Alternate
Take-Off
2500 40 in Hg
Sea Level to
5000 ft
260°C
(500°F)
899°C
(1650°F)
118°C
(245°F)
186 kPa
(27 psi)
448 kPa
(65 psi)
379 kPa
(55 psi)
654 kPa
(95 psi)
Normal
Take-Off
(300 BHP)
2500 38 in Hg
5000 ft to
12,000 ft
(critical
altitude)
260°C
(500°F)
899°C
(1650°F)
118°C
(245°F)
186 kPa
(27 psi)
448 kPa
(65 psi)
379 kPa
(55 psi)
654 kPa
(95 psi)
Maximum
Continuous
(300 BHP)
2500 38 in Hg
Sea Level
to 12,000
ft (critical
altitude)
260°C
(500°F)
899°C
(1650°F)
118°C
(245°F)
186 kPa
(27 psi)
448 kPa
(65 psi)
379 kPa
(55 psi)
654 kPa
(95 psi)
NOTES:
Other limits are as follows:
1. Minimum fuel pressure at idle: 83 kPa (12 psi).
2. Minimum oil pressure at idle: 173 kPa (25 psi)
3. Maximum oil pressure at start: 793 kPa (115 psi)
2.4.3. Fuel Grade
Avgas 100/100LL, Avgas 100/130
NOTE:
For fuel tank capacities refer to paragraph 2.12 Fuel Limitations
RPM
POWER
MANIFOLD
PRESSURE
PRESSURE
ALTITUDE