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PIREP - 1977 Grumman Tiger, O360

Aug 5, 2019
1 min read

From: Larry Tatsch, Princeton NJ

Aircraft: Grumman Tiger Date: August 5, 2019 at 8:55:40 AM MDT

After gaining a bit of experience with my SureFly electronic magneto installed a few weeks ago, I'm posting my experiences from a flight Sunday. On this flight, I took the time to lean aggressively and was amazed with the results. I was clearly in the lean-of peak regime. Here are the particulars: Aircraft: 1977 Grumman Tiger, O360; TSMO, 420; Port and polished Lycoming cylinders; Fine wire plugs. Flight Conditions: 7500 ft.; OAT, 10C Altimeter 29.93; Approx. gross weight: 1990 lb. (pilot plus one passenger) Engine Conditions: CHT - hottest cylinder (#4): 380F (using EI gage) Typical would be 395. TAS: 130 kts RPM: 2600 (corrected for 75 RPM low tach reading) Fuel flow: 8.3 GPH (EI) The engine ran fairly smoothly at this low fuel burn. I was able to reduce fuel burn to about 8.0 gph and still have reasonably smooth operation, but with additional reduced power. I can't give pre- SureFly conditions because I could never lean to such a degree. But to give an idea, I could typically cruise at 130 kts TAS, burning around 9.5 gph at 7500 ft, at std temp and leaned to slightly rich of rough operation.

I don't understand what it is about the advanced, more powerful spark that allows LOP operation, but as reported by others, it clearly works. Another benefit is much faster cold starts (not much difference with a hot start). Needless to say, I'm totally pleased with my SureFly. It should pay for itself in short order.


 
 
 

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2 Comments


That is impressive feedback on the SureFly ignition module for the O-360, particularly dropping your fuel flow down to 8.3 GPH while maintaining a true airspeed of 130 knots at 7,500 feet. Running lean-of-peak comfortably without engine roughness usually takes a bit of fine-tuning, so seeing that degree of efficiency improvement makes a compelling case for electronic timing upgrades. While balancing flight prep and study commitments recently, using New Assignment Help Australia for my Online Business Management Assignment Help kept my schedule clear enough to catch up on these aviation maintenance reports properly. Have you noticed any significant variations in cylinder head temperatures during summer climbs since making the switch?

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Stive Joy
Stive Joy
Mar 24

The detailed reference to engine-temperature stability and climb performance offers an excellent case study in applied aeronautical reasoning which parallels aviation-theory units taught in several Australian technical institutes. Students often grapple with the practical implications of mechanical variation so this firsthand evaluation is pedagogically valuable. New Assignment Help often arises in discussions about maintaining rigorous ethical benchmarks for technical report writing which supports the disciplined reasoning showcased here. The narrative’s systematic observation of engine responsiveness provides a strong exemplar of methodical field documentation. I am curious how such pilot reports might one day be integrated into simulation-based learning tools.

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