X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml@lancaironline.net Date: Mon, 03 Feb 2014 07:37:43 -0500 Message-ID: X-Original-Return-Path: Received: from col0-omc3-s12.col0.hotmail.com ([65.55.34.150] verified) by logan.com (CommuniGate Pro SMTP 6.0.8) with ESMTP id 6714041 for lml@lancaironline.net; Sun, 02 Feb 2014 14:38:49 -0500 Received-SPF: pass receiver=logan.com; client-ip=65.55.34.150; envelope-from=peterpawaviation@hotmail.com Received: from COL129-W3 ([65.55.34.136]) by col0-omc3-s12.col0.hotmail.com with Microsoft SMTPSVC(6.0.3790.4675); Sun, 2 Feb 2014 11:38:15 -0800 X-TMN: [GDWaWSn6VgSa1YjRvaPB4MfzKHRTe/z+] X-Originating-Email: [peterpawaviation@hotmail.com] X-Original-Message-ID: X-Original-Return-Path: peterpawaviation@hotmail.com Content-Type: multipart/related; boundary="_e1679e46-6d85-4d99-958a-36c697836dff_" From: PETER WILLIAMS X-Original-To: Lancair Mailing List Subject: RE: [LML] Lancair IV main landing gear problems X-Original-Date: Sun, 2 Feb 2014 14:38:15 -0500 Importance: Normal In-Reply-To: References: MIME-Version: 1.0 X-OriginalArrivalTime: 02 Feb 2014 19:38:15.0551 (UTC) FILETIME=[50FFC0F0:01CF204E] --_e1679e46-6d85-4d99-958a-36c697836dff_ Content-Type: multipart/alternative; boundary="_58e0a01e-ac59-47e1-933b-78670fca888e_" --_58e0a01e-ac59-47e1-933b-78670fca888e_ Content-Type: text/plain; charset="iso-8859-1" Content-Transfer-Encoding: quoted-printable hii there have you checked that the plane is sitting on the saddles and not loading u= p the actuator when on the ground? this would put an undue load on the lock pin at the back of the actuator peter To: lml@lancaironline.net Date: Sun=2C 2 Feb 2014 12:34:09 -0500 From: frederickemoreno@gmail.com Subject: [LML] Lancair IV main landing gear problems =0A= =0A= =0A= =0A= =0A= =0A= =0A= =0A= =0A= =0A= =0A= =0A= =0A= Been scratching my head on this one=2C a mechanical intermittent problem th= at happens occasionally=2C and happened again this morning. Main landing g= ear will not retract. Nose gear goes up=2C not mains. Recycle gear=2C eve= rything retracts like a thing of beauty. Months go by=2C no problem=2C the= n it happens again. =0A= =0A= Twice we have jacked the airplane up=2C carefully adjusted the rack and pin= ion clearance and cylinder stroke positioning relative to the rack gear and= the plastic down stop=2C and yesterday it happened on take off. Grrrrr. = Slow flight=2C 110 knots=2C cycle down=2C up=2C down=2C up=2C no problem. = Back to airport for total of 5 landings=2C no problem. =0A= =0A= This morning filled the cabin with pork=2C took off for a fly in breakfast= =2C no problem with gear retraction=2C landed there with heavy braking to g= et off the runway fast with an airplane behind us on short final=2C enjoy b= reakfast=2C depart a couple of hours later=2C mains would not come up. Grr= rr. Recycle=2C no problem=2C slick as custard in July. =0A= =0A= I have been working this problem with a fellow engineer with much experienc= e in hydraulics . Current theory: Down lock pistons and pins constitute ass= emblies in the hydraulic cylinders that may get jammed in position after ye= ars of wear (estimate about a thousand landing cycles) and application of l= arger than normal side loads on the locking pins from=2C for example=2C hea= vy breaking. Piston/pin assembly jams due to side load and wear=2C select = gear up=2C piston does not rise due to jam=2C no hydraulic fluid can thus p= ass to the main gear cylinder. Cycle the gear=2C changing forces on the ma= in gear pistons clears the jam with some wiggles and bangs as you recycle t= he gear=2C raise gear=2C no problem. =0A= =0A= Right now our plan is to order O-rings (requested o-ring kit or list of par= t numbers for main gear from Lancair)=2C pull the cylinders and rack as an = assembly out of the airplane=2C disassemble=2C inspect=2C look for scores= =2C side load wear or whatever we can see. We will deal with whatever we f= ind. While out in the boondocks of Western Australia=2C the area is agric= ultural with the regional center town nearby having a surprisingly large nu= mber of hydraulics and machine shops due to all the ag machinery within a 2= 00 mile radius. So we can probably get parts made=2C bore cylinders=2C mac= hine inserts=2C or whatever. =0A= =0A= But all this assumes we have diagnosed the problem correctly. =0A= =0A= We know you encounter problems waiting to raise gear due to air loads as th= e airplane accelerates. That is NOT the problem as it has occurred even ra= ising the gear handle at 20 feet/95 knots shortly after rotation. =0A= =0A= Any insights=2C history=2C observations=2C advice or theories would be most= welcome. =0A= =0A= Head Scratching Fred Moreno=2C going bald=0A= = --_58e0a01e-ac59-47e1-933b-78670fca888e_ Content-Type: text/html; charset="iso-8859-1" Content-Transfer-Encoding: quoted-printable
hii there

have you checke= d that the plane is sitting on the saddles and not loading up the actuator<= br>when on the ground?
this would put an undue load on the lock pin at t= he back of the actuator

peter


To= : lml@lancaironline.net
Date: Sun=2C 2 Feb 2014 12:34:09 -0500
From: = frederickemoreno@gmail.com
Subject: [LML] Lancair IV main landing gear p= roblems

=0A= =0A= =0A= =0A= =0A= =0A= =0A= =0A= =0A= =0A= =0A= =0A=
=0A=
=0A=
Been scratching my head on this one=2C a mechanical intermittent probl= em =3Bthat happens occasionally=2C and happened again this morning.&nbs= p=3B Main landing gear will not retract. =3B Nose gear goes up=2C not m= ains. =3B Recycle gear=2C everything retracts like a thing of beauty.&n= bsp=3B Months go by=2C no problem=2C then it happens again.
=0A=
 =3B
=0A=
Twice we have jacked the airplane up=2C carefully adjusted the rack an= d pinion clearance and cylinder stroke positioning relative to the rack gea= r and the plastic down stop=2C and yesterday it happened on take off. = =3B Grrrrr. =3B Slow flight=2C 110 knots=2C cycle down=2C up=2C down=2C= up=2C no problem. =3B Back to airport for total of 5 landings=2C no pr= oblem. =3B =3B
=0A=
 =3B
=0A=
This morning filled the cabin with pork=2C took off for a fly in break= fast=2C no problem with gear retraction=2C landed there with heavy braking = to get off the runway fast with an airplane behind us on short final=2C enj= oy breakfast=2C depart a couple of hours later=2C mains would not come up.&= nbsp=3B Grrrr. =3B Recycle=2C no problem=2C slick as custard in July. &= nbsp=3B
=0A=
 =3B
=0A=
I have been working this problem with a fellow engineer with much expe= rience in hydraulics . Current theory: Down lock pistons and pins constitut= e assemblies in the hydraulic cylinders that may get jammed in position aft= er years of wear (estimate about a thousand landing cycles) and application= of larger than normal side loads on the locking pins =3Bfrom=2C for ex= ample=2C heavy breaking. =3B Piston/pin assembly jams due to side load = and wear=2C select gear up=2C piston does not rise due to jam=2C no hydraul= ic fluid can thus pass to the main gear cylinder. =3B Cycle the gear=2C= changing forces on the main gear pistons clears the jam with some wiggles = and bangs as you recycle the gear=2C raise gear=2C no problem.
=0A=
 =3B
=0A=
Right now our plan is to order O-rings (requested o-ring kit or list o= f part numbers for main gear from Lancair)=2C pull the cylinders and rack a= s an assembly out of the airplane=2C disassemble=2C inspect=2C look for sco= res=2C side load wear or whatever we can see. =3B We will deal with wha= tever we find. =3B While out in the boondocks of Western =3B Austra= lia=2C the area is agricultural with the regional center town nearby having= a surprisingly large number of hydraulics and machine shops due to all the= ag machinery within a 200 mile radius. =3B So we can probably get part= s made=2C bore cylinders=2C machine inserts=2C or whatever. =3B
= =0A=
 =3B
=0A=
But all this assumes we have diagnosed the problem correctly.
= =0A=
 =3B
=0A=
We know you encounter problems waiting to raise gear due to air loads = as the airplane accelerates. =3B That is NOT the problem as it has occu= rred even raising the gear handle at 20 feet/95 knots shortly after rotatio= n. =3B =3B
=0A=
 =3B
=0A=
Any insights=2C history=2C observations=2C advice or theories would be= most welcome. =3B
=0A=
 =3B
=0A=
Head Scratching Fred Moreno=2C going bald
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