Piper ARCHER III - Power Plant Limitations

2.7 POWER PLANT LIMITATIONS
(a) Number of Engines 1
(b) Engine Manufacturer Lycoming
(c) Engine Model No. O-360-A4M
(d) Engine Operating Limits
(1) Takeoff Power
limit (BHP) 180
(2) Takeoff Engine
Speed (RPM) 2700
(3) Maximum Oil Temperature 245F
(4) Oil Pressure
Minimum (red line) 25 PSI
Maximum (red line) 115 PSI
(5) Fuel Pressure
Minimum (red line) 0.5 PSI
Maximum (red line) 8 PSI
(6) Fuel (AVGAS ONLY)
(minimum grade) 100 or 100LL
Aviation Grade
(7) Number of Propellers 1
(8) Propeller Manufacturer Sensenich
(9) Propeller Model 76EM8S14-0-62
(10)Propeller Diameter
Minimum 76 IN.
Maximum 76 IN.
(11)Propeller Tolerance (static RPM
at maximum permissible throttle
setting at sea level) Not above 2340 RPM
at ISA conditions Not below 2240 RPM
NOTE: Reference aircraft maintenance manual
for test procedure to determine approved static
RPM under non-standard conditions.
2.7 POWER PLANT LIMITATIONS
(a) Number of Engines 1
(b) Engine Manufacturer Lycoming
(c) Engine Model No. O-360-A4M
(d) Engine Operating Limits
(1) Takeoff Power
limit (BHP) 180
(2) Takeoff Engine
Speed (RPM) 2700
(3) Maximum Oil Temperature 245F
(4) Oil Pressure
Minimum (red line) 25 PSI
Maximum (red line) 115 PSI
(5) Fuel Pressure
Minimum (red line) 0.5 PSI
Maximum (red line) 8 PSI
(6) Fuel (AVGAS ONLY)
(minimum grade) 100 or 100LL
Aviation Grade
(7) Number of Propellers 1
(8) Propeller Manufacturer Sensenich
(9) Propeller Model 76EM8S14-0-62
(10)Propeller Diameter
Minimum 76 IN.
Maximum 76 IN.
(11)Propeller Tolerance (static RPM
at maximum permissible throttle
setting at sea level) Not above 2340 RPM
at ISA conditions Not below 2240 RPM
NOTE: Reference aircraft maintenance manual
for test procedure to determine approved static
RPM under non-standard conditions.
SECTION 2
PA-28-181, ARCHER III LIMITATIONS
SECTION 2
PA-28-181, ARCHER III LIMITATIONS
ISSUED: JULY 12, 1995 REPORT: VB-1611
2-3
ISSUED: JULY 12, 1995 REPORT: VB-1611
2-3