Return-Path: Sender: (Marvin Kaye) To: lml Date: Tue, 07 Oct 2003 23:01:16 -0400 Message-ID: X-Original-Return-Path: Received: from lakemtao04.cox.net ([68.1.17.241] verified) by logan.com (CommuniGate Pro SMTP 4.1.5) with ESMTP id 2627929 for lml@lancaironline.net; Tue, 07 Oct 2003 21:14:51 -0400 Received: from Dan.cox.net ([68.110.224.55]) by lakemtao04.cox.net (InterMail vM.5.01.06.05 201-253-122-130-105-20030824) with ESMTP id <20031008011450.BVJY5790.lakemtao04.cox.net@Dan.cox.net> for ; Tue, 7 Oct 2003 21:14:50 -0400 X-Original-Message-Id: <5.2.0.9.0.20031007200351.00b2aa90@pop.east.cox.net> X-Sender: danobrien@pop.east.cox.net X-Mailer: QUALCOMM Windows Eudora Version 5.2.0.9 X-Original-Date: Tue, 07 Oct 2003 21:14:51 -0400 X-Original-To: lml@lancaironline.net From: Dan O'Brien Subject: Re: Prop for the Super ES Mime-Version: 1.0 Content-Type: text/plain; charset="us-ascii"; format=flowed Dan Newland requested passing on any information learned from Tim Ong about the numbers for the three props tested on the factory's Super ES. I spoke with Tim today, and while he didn't have all of the numbers handy, here is the information that he shared. 1. In high cruise (25-squared), the Hartzell was roughly 3 kts faster than the MT and the Aerocomposites. 2. In climb, the MT and Hartzell were about the same, and both did better than the particular Aerocomposites prop that was tested. However, the Aerocomposites prop that was tested did not develop 2700 RPM on the take-off roll because it was not optimized for the ES. Tim saw no reason to believe that the Aerocomposites would not perform as well as the others if adjustments were made to allow it to develop 2700 RPM. His understanding was that these adjustments would not be difficult to make (consistent with Eugene Long's post in this thread). (It is not difficult to believe that the Aerocomposites would perform well on a 2700 RPM take-off if the reports about its take-off performance on the IV and the Legacy are accurate). 3. The Hartzell is roughly 23 lbs heavier than either composite. 4. There is a noticeable reduction in nose-heaviness when flying with one of the composites rather than the Hartzell. However, this can be offset by: i) putting batteries and if needed other accessories aft; ii) a bigger trim tab; or iii) putting about a 5 lb lead weight way back in the tail. Given two planes that are identical except for the prop, the plane with the Hartzell will be about 28 lbs heavier because of the heavier prop and the 5 lbs of ballast in the tail. But the two planes will feel about the same. 5. The Hartzell is more durable than the composite props, and probably requires less frequent repair on average. However, the Hartzell may be more costly to repair. As Pat Weston noted in his post on this thread, little dings in his MT are builder-repairable (apparently a little glass, some sanding, and paint), so the potential for an increased incidence of "dings" that have to be repaired doesn't have to break the budget. It seems that the composite props need repairs more often than the aluminum prop, but the repairs on the composite prop tend to cost less. Take your pick. The Aerocomposites claims to be more durable than other composite props because of its nickel leading edge. Tim did not have the data to evaluate this claim. I note that every person who responded to my question about props for the Super ES is happy with his prop choice. All three props were represented. Seems to me like we have three good options to satisfy different preferences. :) Dan O'Brien Lancair Super ES