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Pre-takeoff checklist
I own a 2006 turbo 182 and recently had the prop repaired from a leak. The shop fixed the leak but after the repair my plane felt sluggish and I noticed the manifold pressure was not producing the 32" it was supposed to. I took it back to the shop.
They inspected everything and then sent the prop back to the prop shop for inspection. The prop shop said everything was within parameters but they would adjust the pitch to the lower limits. They got it all back together and at 300' msl the shop was able to get 32" of manifold pressure on a runup. I had a test flight done and the airplane would not hold the manifold pressure on climb. At 10,000 ft the manifold pressure was only 21.7" and a climb rate of only 300 fpm.
During the test flight they landed at an airport at approx 3000' msl and a run up performed there only produced 29.7" manifold pressure.
This airplane should be able to hold 32" up to 20000 ft.
What could be the problem?
They inspected everything and then sent the prop back to the prop shop for inspection. The prop shop said everything was within parameters but they would adjust the pitch to the lower limits. They got it all back together and at 300' msl the shop was able to get 32" of manifold pressure on a runup. I had a test flight done and the airplane would not hold the manifold pressure on climb. At 10,000 ft the manifold pressure was only 21.7" and a climb rate of only 300 fpm.
During the test flight they landed at an airport at approx 3000' msl and a run up performed there only produced 29.7" manifold pressure.
This airplane should be able to hold 32" up to 20000 ft.
What could be the problem?