Hey guys,
I would like to get your thoughts on a recent incident I had.
Airplane in question - late 1970's PA-28 with a 160hp engine (1700 SMOH).
We were flying out of an airport last week where the density altitude was about 5500 ft and the TOW was about 200 below the MTOW. W & B was well within limits.
During the takeoff roll (and after having leaned the aircraft during the run-up) I felt that the airplane is a bit under powered and that the engine is sounding rough.
During the climb-out we experienced frequent RPM drops of about 100-150 RPM's and again, roughness from the engine (I have about 10-12 hours on this specific airplane in the last 3 week so I am well familiar with how the engine sounds during normal flight). Having deemed the airplane incapable of continuing the flight safely, I made a decision to return to the departure airport about 15 minutes after the departure.
We had maintenance done on the airplane that same day and the A&P found nothing wrong with the plane. After receiving an ear full from the flight school for not completing the flight, we got up the following morning and headed back to the airport for another attempt.
The second time, density altitude was about 3200 ft and the TOW again well below MTOW. During the climb-out I felt again that the engine is running a little rough, but the performance was better thanks to the lower density altitude. We made it safely to 10,500 ft, our cruising altitude (where the density altitude was about 13,000 ft enroute).
I had selected a route of flight which took us over airports, which later turned out to be a smart move. During cruise, I again felt that the engine was running rough and making unusual noises.
About an hour and a half into the flight at 10,500 ft, we experienced an engine out. The power failure was immediate, but luckily we were about 10 nm from an airport. We established best glide and began troubleshooting the problem. Nothing seemed to make a difference. We went over the emergency checklist, again no difference. At about 6000 ft (a few minutes into the glide) the engine fired back up after playing with the power setting. Not wanting to take any more risks, we kept the engine pretty much on idle the entire way down and continued with the landing.
A few days later, the flight school went to pick up the airplane. They brought a maintenance guy who deemed the airplane completely airworthy and flew it back home. I, of course, again received an ear full for not being a good enough pilot to determine that high density altitude was the cause of our problems. I am not entirely sure how density altitude could be the cause of this, especially an hour and a half into the cruise and after having switched the tanks every 30 minutes.
Any intake on this would be greatly appreciated - thanks!
I would like to get your thoughts on a recent incident I had.
Airplane in question - late 1970's PA-28 with a 160hp engine (1700 SMOH).
We were flying out of an airport last week where the density altitude was about 5500 ft and the TOW was about 200 below the MTOW. W & B was well within limits.
During the takeoff roll (and after having leaned the aircraft during the run-up) I felt that the airplane is a bit under powered and that the engine is sounding rough.
During the climb-out we experienced frequent RPM drops of about 100-150 RPM's and again, roughness from the engine (I have about 10-12 hours on this specific airplane in the last 3 week so I am well familiar with how the engine sounds during normal flight). Having deemed the airplane incapable of continuing the flight safely, I made a decision to return to the departure airport about 15 minutes after the departure.
We had maintenance done on the airplane that same day and the A&P found nothing wrong with the plane. After receiving an ear full from the flight school for not completing the flight, we got up the following morning and headed back to the airport for another attempt.
The second time, density altitude was about 3200 ft and the TOW again well below MTOW. During the climb-out I felt again that the engine is running a little rough, but the performance was better thanks to the lower density altitude. We made it safely to 10,500 ft, our cruising altitude (where the density altitude was about 13,000 ft enroute).
I had selected a route of flight which took us over airports, which later turned out to be a smart move. During cruise, I again felt that the engine was running rough and making unusual noises.
About an hour and a half into the flight at 10,500 ft, we experienced an engine out. The power failure was immediate, but luckily we were about 10 nm from an airport. We established best glide and began troubleshooting the problem. Nothing seemed to make a difference. We went over the emergency checklist, again no difference. At about 6000 ft (a few minutes into the glide) the engine fired back up after playing with the power setting. Not wanting to take any more risks, we kept the engine pretty much on idle the entire way down and continued with the landing.
A few days later, the flight school went to pick up the airplane. They brought a maintenance guy who deemed the airplane completely airworthy and flew it back home. I, of course, again received an ear full for not being a good enough pilot to determine that high density altitude was the cause of our problems. I am not entirely sure how density altitude could be the cause of this, especially an hour and a half into the cruise and after having switched the tanks every 30 minutes.
Any intake on this would be greatly appreciated - thanks!