Steve:
Ok guys, just got home from a 4 day, here is what I discussed with a Lord Engineer regarding the difference between the -2 and the -4 mounts for a continental engine, disclaimer, this is not FAA approved data, but is from the manufacturer. The -2 unit is used on the 520 in the Viking. Also, this info is not for the O-470 in the 14-19-2, my conversation was about the 14-19-3, 3A and the Viking with the IO520.
From: Snyder, Paul J \(Grandview\)
Date: 01/09/08 10:06:04
To: Dan & Lori Schultz
Subject: RE: J-7518-4, J-7518-2 mounts
Good morning Dan,
Dimensionally, the J-7518-2 and the J-7518-4 are identical, with the exception of the rib in the elastomer section of the sandwiches used in the -4. The difference is primarily the compression springrate.
The J-7518-2 compression springrate is approximately 5300 lbs/inch while the J-7518-4 compression springrate is approximately 8000 lbs/inch. Both kits are used in the same semi-focalized arrangement on the aircraft, with the same offset for torque. The average weight of the Continental O-470 engine is about 430 lbs, so each mount is supporting approximately 108 lbs.
108 lbs of weight on the J-7518-4 will deflect the mount approximately 0.014 inches. 108 lbs on the J-7518-2 will deflect the mount about 0.020 inches. Over time, the sag for the J-7518-2 kit will probably exceed the -4 kit, but vibration isolation will be improved which is probably why Bellanca went with the J-7518-2 kits.
I see no performance reasons not to recommend using the J-7518-2 in place of the J-7518-4 and you may, in fact, see an improvement in vibration isolation. Let me know if you need anything else.
Very best regards,
Paul J. Snyder
Aerospace and Defense Technical Support
LORD Corporation
PH (814)868-5424 ext 6611
FAX (814)860-3535
http://www.lord.com