David-aviator
Well Known Member
For those interested in real world climb numbers concerning RV-7A, gather 'round. I just landed and this is what I wrote down.
First off, here are the starting points.
OAT 81F, SL pressure 29.74, airport elevation 630'.
Aircraft gross weight = 1512 lbs, CG @ 83.2", take off fuel = 39.3 gallons.
Climb power from take off was wide open throttle. Rather than try to guess a best climb speed for the conditions, I decided to let the engine decide that. After take off, when rpm hit 2400-2500, climb was initiated at 110-115 KIAS. I maintained 2400-2500 rpm all the way up to level off. Also, the engine was leaned using the target EGT technique from a lead provided by hevans7a last evening. I used 1300F. Max CHT in the climb was 407F, oil temp never hit 180.
The Dynon timer was started as power came up for take off. Here's what happened.
Out of 2000 MSL - 1:31 minutes (913 fpm)
Out of 4000 MSL - 3:00 minutes (1123 fpm)
Out of 6000 MSL - 4:43 minutes (1130 fpm)
Out of 8000 MSL - 6:26 minutes (1142 fpm)
Level at 10,000 MSL - 8:27 minutes (1104 fpm)
The rates of climb have the airport elevation factored in and it must be noted - time is from standing still on the runway - conservatively one could subtract at least 30 seconds if times were measured from the initiation of the climb at 110 KIAS. I should have noted that time but did not. If it were as much as a minute, it would make a huge difference. Average rate to 10 grand would be 1252 fpm.
Density altitude at level off 11,810'
Fuel at level off = 37.2 (2.1 gallons burned to 10,000')
Total time of the flight 17:48 by the Dynon timer. Fuel remaining at shut down = 36.5 gallons (3.8 gallons up and down)
For sure a light weight RV-4 with 180hp and a CS prop will do much better. But all in all, it isn't that bad for 1500 lb + airplane on a relatively warm day with a fixed pitch prop.
First off, here are the starting points.
OAT 81F, SL pressure 29.74, airport elevation 630'.
Aircraft gross weight = 1512 lbs, CG @ 83.2", take off fuel = 39.3 gallons.
Climb power from take off was wide open throttle. Rather than try to guess a best climb speed for the conditions, I decided to let the engine decide that. After take off, when rpm hit 2400-2500, climb was initiated at 110-115 KIAS. I maintained 2400-2500 rpm all the way up to level off. Also, the engine was leaned using the target EGT technique from a lead provided by hevans7a last evening. I used 1300F. Max CHT in the climb was 407F, oil temp never hit 180.
The Dynon timer was started as power came up for take off. Here's what happened.
Out of 2000 MSL - 1:31 minutes (913 fpm)
Out of 4000 MSL - 3:00 minutes (1123 fpm)
Out of 6000 MSL - 4:43 minutes (1130 fpm)
Out of 8000 MSL - 6:26 minutes (1142 fpm)
Level at 10,000 MSL - 8:27 minutes (1104 fpm)
The rates of climb have the airport elevation factored in and it must be noted - time is from standing still on the runway - conservatively one could subtract at least 30 seconds if times were measured from the initiation of the climb at 110 KIAS. I should have noted that time but did not. If it were as much as a minute, it would make a huge difference. Average rate to 10 grand would be 1252 fpm.
Density altitude at level off 11,810'
Fuel at level off = 37.2 (2.1 gallons burned to 10,000')
Total time of the flight 17:48 by the Dynon timer. Fuel remaining at shut down = 36.5 gallons (3.8 gallons up and down)
For sure a light weight RV-4 with 180hp and a CS prop will do much better. But all in all, it isn't that bad for 1500 lb + airplane on a relatively warm day with a fixed pitch prop.