X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml@lancaironline.net Date: Tue, 23 Mar 2010 16:02:00 -0400 Message-ID: X-Virus-Scanned: clean according to Sophos on Logan.com X-PolluStop-Diagnostic: (whitelisted) X-Orig-Return-Path: justinh@lancair.com X-Orig-Recipients: y/1mPiZUtbQLvIFjMGAgBeTI1B2BZQNEfeLmLIWRMpw= X-PolluStop-Score: 0.00 X-PolluStop: Scanned with Niversoft PolluStop v2.7.2 X-SpamCatcher-Score: 57 [XX] (71%) BODY: contains an image tag with CID (29%) BODY: likely RX content X-Original-Return-Path: Received: from mail.lancair.com ([66.39.173.18] verified) by logan.com (CommuniGate Pro SMTP 5.3.4) with ESMTP id 4176120 for marv@lancair.net; Tue, 23 Mar 2010 14:34:17 -0400 Received-SPF: pass receiver=logan.com; client-ip=66.39.173.18; envelope-from=JustinH@lancair.com X-MimeOLE: Produced By Microsoft Exchange V6.5 Content-class: urn:content-classes:message MIME-Version: 1.0 Content-Type: multipart/related; boundary="----_=_NextPart_001_01CACAB6.E36ED792"; type="multipart/alternative" Subject: Product Improvement Notice - Fork.doc for LML. X-Original-Date: Tue, 23 Mar 2010 11:30:17 -0700 X-Original-Message-ID: <8128CA1601FBCF478DAAAC0917E6CF56CED8A5@lindbergh.lancair.local> X-MS-Has-Attach: yes X-MS-TNEF-Correlator: Thread-Topic: Product Improvement Notice - Fork.doc for LML. Thread-Index: AcrKtuKynef7znmFQ7qkkPVGVVG0tw== From: "Justin Hawkins" X-Original-To: This is a multi-part message in MIME format. ------_=_NextPart_001_01CACAB6.E36ED792 Content-Type: multipart/alternative; boundary="----_=_NextPart_002_01CACAB6.E36ED792" ------_=_NextPart_002_01CACAB6.E36ED792 Content-Type: text/plain; charset="iso-8859-1" Content-Transfer-Encoding: quoted-printable =20 =20 250 SE Timber Avenue, Redmond, Oregon 97756 Phone 541 923-2233 Fax = 541 923-2255 =20 Product Improvement Notice =20 Subject: Landing Gear Forks =20 Date: March 1, 2010 =20 =20 =20 =20 The Legacy RG aluminum main landing gear fork is designed for normal = use, up to nominal expected gross weight on smooth runways. Aluminum was = chosen for the fork in keeping with the Legacy's emphasis on light = weight and performance. Variations in runway surface, aircraft weight, = tire choice, and pilot technique can, in some cases, allow for the = normal flex in the fork to permit contact between the tire tread surface = and the head of the bolts securing the fork to the shock strut. If you = are experiencing this condition it can be addressed in two ways.=20 =20 Option 1: =20 You may change the fork attach bolts from the originally supplied hex = head bolts to a countersunk bolt. Lancair will supply the necessary = hardware needed to make the change at no charge. To modify the fork, you = should use a 5/16 pilot 100=B0 countersink until head is flush = (nominally .133 deep). This change will increase clearance between the = standard tire and the fork by .375" and will also provide a smooth = surface on the fork's inside surface to eliminate tire tread grooving. Hardware to be supplied: 8 x AN960-516 washers 8 x = MS21042-5 nuts 8 x = MS24694-S156 screws 2 x = MS24665-292 cotter pins =20 Option 2: =20 You may elect to replace the aluminum fork with a stiffer steel fork, = incurring an increased aircraft weight of 7.5 pounds. The stiffer steel = forks flex less and may be secured with the original style AN5-14A hex = head bolts. The steel forks, pn# 433-0010 and 433-0011, may be purchased = from Kit Components Inc. at a net cost of $374 each (exchange), = including shipping. The new forks will come to you ready to install with = new bolts, nuts and washers, and axle cotter pin. The charge will be = $1496, which includes a $748 core charge. The $748 core charge will be = refunded to you upon receipt of your aluminum forks when received at = Lancair. You are responsible for shipping costs of returned aluminum = forks. Aluminum forks must be received within 45 days after steel forks = are shipped for refund. =20 It is the responsibility of the owner to check all clearances and fit = before flying. =20 To place an order, call Kit Components Inc. at 541-923-2244 or email = michelleg@lancair.com. ------_=_NextPart_002_01CACAB6.E36ED792 Content-Type: text/html; charset="iso-8859-1" Content-Transfer-Encoding: quoted-printable

 

250 SE Timber Avenue, Redmond, = Oregon 97756=A0=A0 Phone 541 923-2233=A0=A0 = Fax 541 923-2255

Product Improvement = Notice

=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0= =A0=A0=A0

Subject: Landing Gear Forks

 

Date:=A0=A0=A0=A0=A0 March 1, 2010

 

=A0=A0=A0=A0=A0=A0=A0 =

 

 

The Legacy RG aluminum main landing gear fork is designed for = normal use, up to nominal expected gross weight on smooth runways. Aluminum was = chosen for the fork in keeping with the Legacy’s emphasis on light weight = and performance. Variations in runway surface, aircraft weight, tire choice, = and pilot technique can, in some cases, allow for the normal flex in the = fork to permit contact between the tire tread surface and the head of the bolts securing the fork to the shock strut.=A0 If you are experiencing this = condition it can be addressed in two ways.

 

Option 1:

 

You may change the fork attach bolts from the originally = supplied hex head bolts to a countersunk bolt. Lancair will supply the necessary = hardware needed to make the change at no charge. To modify the fork, you should = use a 5/16 pilot 100=B0 countersink until head is flush (nominally .133 = deep). This change will = increase clearance between the standard tire and the fork by .375” and will also = provide a smooth surface on the fork’s inside surface to eliminate tire = tread grooving.

=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0 Hardware to be = supplied:=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0 8 x AN960-516 = washers

=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0= =A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0 = =A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0 =A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0 8 x MS21042-5 nuts

=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0= =A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0= =A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0 8 x MS24694-S156 screws

=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0= =A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0= =A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0 2 x MS24665-292 cotter pins

 

Option 2:

 

You may elect to replace the aluminum fork with a stiffer steel = fork, incurring an increased aircraft weight of 7.5 pounds. The stiffer steel = forks flex less and may be secured with the original style AN5-14A hex head = bolts. The steel forks, pn# 433-0010 and 433-0011, may be purchased from Kit Components Inc. at a net cost of $374 each (exchange), including = shipping. The new forks will come to you ready to install with new bolts, nuts and = washers, and axle cotter pin. The charge will be $1496, which includes a $748 = core charge. The $748 core charge will be refunded to you upon receipt of = your aluminum forks when received at Lancair. You are responsible for = shipping costs of returned aluminum forks. Aluminum forks must be received within 45 = days after steel forks are shipped for refund.

 

It is the responsibility of the owner to = check all clearances and fit before flying.

 

To place an order, call Kit Components Inc. = at 541-923-2244 or email michelleg@lancair.com.

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