Return-Path: Received: from pop3.olsusa.com ([63.150.212.2] verified) by logan.com (CommuniGate Pro SMTP 3.5b3) with ESMTP id 841445 for rob@logan.com; Mon, 30 Jul 2001 01:37:23 -0400 Received: from cgpro.iccx.net ([166.93.205.11]) by pop3.olsusa.com (Post.Office MTA v3.5.3 release 223 ID# 0-71866U8000L800S0V35) with ESMTP id com for ; Sun, 29 Jul 2001 15:54:10 -0400 Received: from [166.93.108.146] (HELO Pdjpryan.ruralnet.net) by cgpro.iccx.net (CommuniGate Pro SMTP 3.4.6) with SMTP id 69738031 for lancair.list@olsusa.com; Sun, 29 Jul 2001 14:03:31 -0600 Message-ID: <000e01c11869$5eccd740$926c5da6@Pdjpryan.ruralnet.net> From: "DON & PAT RYAN" To: "LML" Subject: LNC2 GEAR UP Date: Sun, 29 Jul 2001 13:37:53 -0600 MIME-Version: 1.0 Content-Type: text/plain; charset="iso-8859-1" Content-Transfer-Encoding: 7bit X-Mailing-List: lancair.list@olsusa.com Reply-To: lancair.list@olsusa.com <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> Here is what I know at this time regarding my accident with N15EG at the La Junta, CO airport, LHX. The evidence strongly suggest that the gear up circuit must have activated on final AFTER my GUMP check and the wheels are partially retracted when we touch down. The following are the facts pertinent to the accident. FACTS: 1.-The runway markings, gear door damage and lack of damage to the gear leave little doubt that the gear was moving up at the time of touchdown. The inboard main gear doors suffered the most damage and are the last to retract, when the gear opens a sequence valve. 2.-There is little or no damage to the gear. The gear came down, as it should when the hydraulic pressure dump valve was operated while held by the crane used to lift the plane from the trailer. 3.-Before lifting the plane from the trailer, I turned on the master switch, to remove gasoline from the wing tanks using the pumps and forgot to pull the gear circuit breaker. The battery drain was excessive, so I decided to disconnect the battery terminals. In doing so I found that the UP RELAY was very hot to the touch even though the gear switch was in the down position. 4.-The airspeed squat switch and the gear switch in the down position should have prevented any power going to the UP RELAY. The hydraulic motor was not running at this time, but may have been shut off by the pressure switch?! 5.-With the plane on jacks and the inboard gear doors removed, gear retraction tests were run many times. Operation was normal! 6.-The airspeed squat switch had to be bypassed to allow these tests. 7.-The gear, flap, starter, and power wiring passes between the seats and is tie wrapped to the hydraulic lines on the fuselage floor. 8. A pile of chewed up paper towel was found in this console on the floor and around the wiring, (obviously a start of a mouse nest). The wiring will have to be pulled to determine if a short occurred at this point. 9.-Full gear up requires 8.6 sec. The gear was only partially retracted. 10.-Using 7 seconds from activation and a descent rate of 300 to 600 ft/min results in a height above the runway of 35 to 70 feet at activation of gear up. 11.-At an average airspeed of 80 mph for 7 seconds the plane traveled 830 ft. after initiation of the gear up, placing the plane well over the runway. Actual touchdown was 1800 ft from the East end of the runway. (The first 1000' of runway 26 is decidedly uphill and I intended to land past this rise). The runway length is 6852 ft. 12.-Difficulty with the relays has been previously reported. However, no accidents were caused by the reported failures. INITIAL CONCLUSIONS. 1.-At this point in landing, this pilot is certainly not touching anything except the throttle, stick and rudders and is completely focused on the runway. Additionally the airspeed squat switch would have prevented an inadvertent operation of the gear up. It requires 95+ mph to raise the gear. 2.-An electrical failure in either the wiring or the relays caused the gear to retract at a very unfortunate time. Possibly initiated by changes in vibrations from the engine or flaps. 3.-More investigation will require removal of all of the wiring under the center console, disassembly of the relays, and possibly some testing of the hydraulic motor. This will be done. QUESTIONS TO BE ANSWERED: 1.-Can the up gear cycle be initiated by any short from a 12v line to the up relay? 2.-Will the gear down relay pressure switch stay open due to pressure from the movement of the hydraulic cylinders? Thus allowing the gear up cycle to continue. 3.-What happens if current is supplied to both windings of the hydraulic motor. I had thought that this motor would be reversed by reversing polarity, but that doesn't seem to be the case since they have a common ground and both leads have the same resistance to ground. >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML website: http://www.olsusa.com/mkaye/maillist.html LML Builders' Bookstore: http://www.buildersbooks.com/lancair Please send your photos and drawings to marvkaye@olsusa.com. >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>