PW120 Series Engines
Join Date: Mar 2008
Location: Canada
Age: 63
Posts: 4
Likes: 0
Received 0 Likes
on
0 Posts
Engine driven fuel pumps are typically lubricated with fuel. The boost pumps need to be on to do that. Don't know the 120 but I know Pt6s are only allowed to operate with the boost pumps off for a max of 10 hours. More than that and pump comes off. Boost pumps need to be on even during engine maintenance such as compressor washes. My two bits worth.
Join Date: Jun 2002
Location: Vega Constellation
Posts: 286
Likes: 0
Received 0 Likes
on
0 Posts
The ATR is fitted with PW120 series engines, and I have heard this comment many times.
This is either pure invention, or some procedure carried from another PW engine that is totally unrelated.
There is (was) no such thing in the ATR manuals.
Follow the manufacturer's manuals. If it was causing any damage, they would have included this procedure. It may well be on the PT6, but not on the PW120 series, at least not the ones mounted on ATR aircraft.
This is either pure invention, or some procedure carried from another PW engine that is totally unrelated.
There is (was) no such thing in the ATR manuals.
Follow the manufacturer's manuals. If it was causing any damage, they would have included this procedure. It may well be on the PT6, but not on the PW120 series, at least not the ones mounted on ATR aircraft.
Join Date: Apr 2008
Location: nowhere
Posts: 1
Likes: 0
Received 0 Likes
on
0 Posts
The ATR is fitted with PW120 series engines, and I have heard this comment many times.
This is either pure invention, or some procedure carried from another PW engine that is totally unrelated.
There is (was) no such thing in the ATR manuals.
Follow the manufacturer's manuals. If it was causing any damage, they would have included this procedure. It may well be on the PT6, but not on the PW120 series, at least not the ones mounted on ATR aircraft.
This is either pure invention, or some procedure carried from another PW engine that is totally unrelated.
There is (was) no such thing in the ATR manuals.
Follow the manufacturer's manuals. If it was causing any damage, they would have included this procedure. It may well be on the PT6, but not on the PW120 series, at least not the ones mounted on ATR aircraft.
In addition to what Kiwiconehead has rightfully stated, the aux pumps were procedurally switched on only for takeoff and approach on the -300 (just like they are now on the -400). Between climb check and approach check they were only required to run for some abnormal procedures (typically involving high oil or fuel temperatures).
And the engines ran just fine under this kind of treatment.
Maybe captjns could specify which type he is referring to?
And the engines ran just fine under this kind of treatment.
Maybe captjns could specify which type he is referring to?
Join Date: Oct 2006
Location: Earth
Posts: 93
Likes: 0
Received 0 Likes
on
0 Posts
Based on the terms used in captjns post ie "boost pumps" and "engine speed" (Ng) I think he refers to the PT6 series. Never heard those terms used on the PW120 series, but hey I coud be wrong.
