puddlejumper
Unemployed /Contract User
- Joined
- Nov 26, 2001
- Posts
- 305
My company has managed to get ourselves into a situation and I'd like to get the opinions of some of you on the board. We had an overhaul done by a reputable shop on a PT-6. This engine was on the MORE program with about 4700 hrs since new, about 4300 CSN and 200 hrs since HSI. It was installed as original equipment on a 1978 Cheyenne II. Since the overhaul, this engine has exhibited intermittent torque and fuel flow fluctuations. We've had several other problems since overhaul, including oil leaks and a FCU/responsiveness problem at high-altitude fields. The overhaul included a 3600 hour factory warranty.
After several visits to the overhaul facility and a power section tear-down and torque indicator system re-work, a loaner has been installed. This loaner engine was manufactured in 1999, it has 1025 TSN and something like 800 CSN. It's life as a loaner has been fairly easy from what I could tell by looking at the logs. Ours is the third aircraft it's been installed on. The only problem I could find was a loose oil line connection which resulted in a precautionary in-flight shutdown with the oil pressure never reaching the red-line. (I know this only because it happened on our aircraft as a loaner while our engine was being overhauled).
My question is, what issues would you all address if this loaner engine is offered to us instead of trying to go through reinstalling our original engine? This first-run engine will be up for hot section 1000 hrs earlier. Does this make our engine worth more? All SBs were complied with during the overhaul. I don't think there is any real cycle limited components in our original engine (nothing less than like 12,000 cycles to go), but I'll need to look into that.
This has been our company's first turbine overhaul and also my first. I personally would have suggested securing the service of a professional to assist and advise before and during the overhaul process, but the decisions were already made before I was hired. My company is into engineering and I believe they thought they could handle it all on their own. I'd appreciate any and all thoughts on this matter. If anyone would like more details, feel free to PM me. Thanks!
-PJ
After several visits to the overhaul facility and a power section tear-down and torque indicator system re-work, a loaner has been installed. This loaner engine was manufactured in 1999, it has 1025 TSN and something like 800 CSN. It's life as a loaner has been fairly easy from what I could tell by looking at the logs. Ours is the third aircraft it's been installed on. The only problem I could find was a loose oil line connection which resulted in a precautionary in-flight shutdown with the oil pressure never reaching the red-line. (I know this only because it happened on our aircraft as a loaner while our engine was being overhauled).
My question is, what issues would you all address if this loaner engine is offered to us instead of trying to go through reinstalling our original engine? This first-run engine will be up for hot section 1000 hrs earlier. Does this make our engine worth more? All SBs were complied with during the overhaul. I don't think there is any real cycle limited components in our original engine (nothing less than like 12,000 cycles to go), but I'll need to look into that.
This has been our company's first turbine overhaul and also my first. I personally would have suggested securing the service of a professional to assist and advise before and during the overhaul process, but the decisions were already made before I was hired. My company is into engineering and I believe they thought they could handle it all on their own. I'd appreciate any and all thoughts on this matter. If anyone would like more details, feel free to PM me. Thanks!
-PJ