Mailing List lml@lancaironline.net Message #51325
From: terrence o'neill <troneill@charter.net>
Sender: <marv@lancaironline.net>
Subject: [LML] LNC2 gear
Date: Fri, 01 May 2009 16:26:59 -0400
To: <lml@lancaironline.net>
Typo one-=line correction to my last on the gar... line 5... correction underlined.
----- Original Message -----
Sent: Thursday, April 30, 2009 18:55
Subject: [LML] LNC2 gear

Here's an interesting quirk of the retract system, I think....
Yesterday, spurred by a helpful LML suggestion to increase the preload in my nose strut, I chocked the mains, weighted the tail, and supported the nose with the nosewheel an inch off the ground, in order to rotate the nosegear up a little in order to get an air chuck on the schroeder valve less than an inch behnd #3 exhaust tube.
So I pushed up the over- -center brace and pushed back the strut which moved back a little... which reisted .... still locked up. So I opened the free-fall valve. Pushed back the nose strut, chucked my new $22. / 300 psi made-in-china strut pump, on, and put in the max. 
Then lowered the nosewheel to over-center lock, lowered the nose, removed the weight on the tail, and observed 3 inches of strut!
So I pulled the plane out to run an engine idle check, and glanced at the right wing, was shocked to see the gear leaning inward about 10 degrees. !
 
I managed to get the jack in place and raise the wing enough to push the gear in place and pull the over-center strut to lock.
Checked the left gear... and found its over-center strut pushed up, unlocked,  too!
Jacked and pulled it down, and then put the plane back in the hangar and ran a retract-extend check -- after putting the free-fall valve back in closed position.
My guess is that with the hydraulic system closed/normal, in pushing the nosegear over-center lock up and pushing back on the nosewheel I also hydraulic-pressured the main cylinders to pull their over-center locks up.
 
So, if this is true, then here's a scenario to consider:
Gear down, no nose green light.
System pump or solenoid CB pops. 
SO, pull the pump CB, gear switch in Down, valve to free-fall.
Still can't get a nose green light. Just the mains.
 
To land, should the free-fall valve be left open,  or moved to closed? 
 
If it is moved to closed, and the nosegear is not locked over-center... will aft pressure on touchdown unlock the mains too, damaging not only the prop/engine but also the gear and fuselage?
 
Terrence
L235/320 N211AL


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