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This is an RV-4, an Experimental amateur-built aircraft.
I started building this aircraft on Friday, April 13, 1990, and the first flight was May 26, 2008.
Details...
New Lycoming 0-360 (180 hp) with dual P-MAG digital electronic ignitions
New Hartzell constant speed prop
Grand Rapids dual screen "glass panel" system with EFIS, GPS map, and graphic engine monitor.
XM weather
TIS traffic
TruTrak ADI Pilot II digital autopilot with altitude hold
Garmin SL40 Comm with intercom
Garmin GTX 330 transponder with mode S
Garmin 496 GPS
Angle of attack indicator
Oregon Aero seats
Hooker 5 pt harnesses
Vetterman stainless steel exhaust system
Electric flaps with positioning system
Strobes, halogen landing lights,
LED Nav lights and panel lights
Reiff engine preheat system (of course)
All that and only 1014 lbs EW !!
Top speed: 217 MPH at 1300 MSL. Solo climb rate: 2500 FPM
Cruise speed: 200 MPH TAS @ 65% power, 7500 MSL, 7.5 GPH. Range with 1 hr reserve = 3 hrs = 600 mi.
This table is interesting...
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RV-4 |
C-172 |
P-51D |
Gross
Weight |
1500 |
2550 |
12100 |
Wing
area |
110 |
174 |
233 |
HP |
180 |
180 |
1490 |
Wing
loading (lb/sq ft) |
13.6 |
14.7 |
52 |
Power
loading (lb/hp) |
8.3 |
14.2 |
8.1 |
Notice the RV-4 has wing loading similar to a Cessna 172, but a power loading similar to a P-51 Mustang!
See here for more info about the RV-4 model
RV4 going really fast. Note the ground speed on the upper left corner of the Garmin 496 GPS. There may have been a bit of tailwind.
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RV4 in economy mode @ 5 GPH or 34 MPG. 46% power at 19"/1900 RPM IAS 150 MPH, TAS 168 MPH at 7750 ft MSL
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Lycoming O-360 with the Reiff preheat system installed. The main harness runs across the top of the crankcase, and the band heaters are around the cylinders. The oil sump heater is not shown. Note the AC plug just inside the right side cooling air inlet.
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Behind the
instrument panel
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