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Found Loose Cylinder Bolt



 
 
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  #1  
Old February 16th 04, 11:11 PM
Greg Hopp
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Default Found Loose Cylinder Bolt

On preflight I noticed a little oil seeping around the bolt on the
pilot's front cylinder (Superior Milleniums). This is on a '67 C150
w/ the Continental O200. I grabbed the bolt and turned it @ 2 1/2
times until it was finger tight against the cylinder.

Partner and I have grounded the plane. The gents hanging out at the
FBO say, put a wrench on her and fly the darn thing. We'd prefer to
stay safe, legal and alive.

Anyone else experience this and what am I in for? Thanks folks.

Greg
  #2  
Old February 16th 04, 11:32 PM
Jay Honeck
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Partner and I have grounded the plane. The gents hanging out at the
FBO say, put a wrench on her and fly the darn thing. We'd prefer to
stay safe, legal and alive.

Anyone else experience this and what am I in for? Thanks folks.


Were all the bolts lose, or just one?
--
Jay Honeck
Iowa City, IA
Pathfinder N56993
www.AlexisParkInn.com
"Your Aviation Destination"


  #3  
Old February 17th 04, 03:10 PM
Greg Hopp
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"Jay Honeck" wrote in message news: Were all the bolts lose, or just one?

As for what we could visualize, just the one bolt appears loose. The
mechanic who installed the jugs has said: "I torqued them to
specification and have the paperwork to prove my wrench is correct."
He has advised us to tighten it up and see if will seat and stay
tight.

If not, the engine comes apart to helicoil the receiving end for the
thru bolt, is what I'm told.

Greg Hopp
  #4  
Old February 17th 04, 11:47 PM
Habah Fongoula
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The torque should have been checked after 25 or 50 hours. Your
mechanic should have specified this. Instead he throws meaningless
certifications at you. If he's studious enough to have his wrenches
checked, why didn't he tell you about retorquing, or even use a bit of
torque seal on the nuts? In any event, stop crying, have the cylinder
retorqued (all the nuts/bolts) use torque seal and have them rechecked
and torqued in 25 hours.

On 17 Feb 2004 07:10:45 -0800, (Greg Hopp) wrote:

"Jay Honeck" wrote in message news: Were all the bolts lose, or just one?

As for what we could visualize, just the one bolt appears loose. The
mechanic who installed the jugs has said: "I torqued them to
specification and have the paperwork to prove my wrench is correct."
He has advised us to tighten it up and see if will seat and stay
tight.

If not, the engine comes apart to helicoil the receiving end for the
thru bolt, is what I'm told.

Greg Hopp


  #5  
Old February 16th 04, 11:24 PM
jls
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Default


"Greg Hopp" wrote in message
om...
On preflight I noticed a little oil seeping around the bolt on the
pilot's front cylinder (Superior Milleniums). This is on a '67 C150
w/ the Continental O200. I grabbed the bolt and turned it @ 2 1/2
times until it was finger tight against the cylinder.

Partner and I have grounded the plane. The gents hanging out at the
FBO say, put a wrench on her and fly the darn thing. We'd prefer to
stay safe, legal and alive.

Anyone else experience this and what am I in for? Thanks folks.

Greg


Yeah, use a torque wrench and tighten it to its lower or middle torque limit
and go fly. Check the torque on the rest of the nuts too. You should be
tightening a nut instead of a bolt. There are two sets of torque values on
those nuts because they go on bolts (or studs) of two different diameters.
AN5 and AN6? You're probably going to have to use a special wrench for the
torque wrench to connect to, but there should be plenty of those around to
borrow. There are here.


  #6  
Old February 16th 04, 11:55 PM
Ben Jackson
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Default

In article ,
Greg Hopp wrote:
On preflight I noticed a little oil seeping around the bolt on the
pilot's front cylinder (Superior Milleniums).


A guy across the hanger row from me lost a cylinder in flight on a
relatively new (60-70 hour) engine. Looking at the studs it appeared
that one bolt had been lose and backed off, allowing the other 3 to
shear off. I'd be looking at what kind of damage might have happened
to the adjacent studs while the bolt was loose.

--
Ben Jackson

http://www.ben.com/
  #7  
Old February 16th 04, 11:58 PM
Dave Stadt
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Default


"Ben Jackson" wrote in message
news:jMcYb.46366$uV3.92300@attbi_s51...
In article ,
Greg Hopp wrote:
On preflight I noticed a little oil seeping around the bolt on the
pilot's front cylinder (Superior Milleniums).


A guy across the hanger row from me lost a cylinder in flight on a
relatively new (60-70 hour) engine. Looking at the studs it appeared
that one bolt had been lose and backed off, allowing the other 3 to
shear off. I'd be looking at what kind of damage might have happened
to the adjacent studs while the bolt was loose.


What kind of engine only has three studs/bolts holding the cylinder on?
OBTW nuts go on studs not bolts.


--
Ben Jackson

http://www.ben.com/



  #8  
Old February 17th 04, 12:29 AM
jls
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Posts: n/a
Default


"Dave Stadt" wrote in message
...

"Ben Jackson" wrote in message
news:jMcYb.46366$uV3.92300@attbi_s51...
In article ,
Greg Hopp wrote:
On preflight I noticed a little oil seeping around the bolt on the
pilot's front cylinder (Superior Milleniums).


A guy across the hanger row from me lost a cylinder in flight on a
relatively new (60-70 hour) engine. Looking at the studs it appeared
that one bolt had been lose and backed off, allowing the other 3 to
shear off. I'd be looking at what kind of damage might have happened
to the adjacent studs while the bolt was loose.


What kind of engine only has three studs/bolts holding the cylinder on?
OBTW nuts go on studs not bolts.


There would be six nuts holding each of four cylinders down on an O-200
Continental, the standard engine on a Cessna 150. IIRC, 2 are AN5 and 4
are AN6, i. e., the stud diameters are 5/16" and 3/8" respectively. I
watch my nuts, you should pardon the expression. They have anti-sabotage
paint on them and palnuts are even better. Torque is often not enough to
hold them from backing off, and they certainly do not have (and are not
supposed to have) lockwashers under them.



--
Ben Jackson

http://www.ben.com/





  #9  
Old February 16th 04, 11:55 PM
Tina Marie
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Default

In article , Greg Hopp wrote:
Partner and I have grounded the plane. The gents hanging out at the
FBO say, put a wrench on her and fly the darn thing. We'd prefer to
stay safe, legal and alive.


Don't just crank it down with a wrench! In general, every bolt connecting
everything to your engine has a proper torque. A lot of those torque settings
are way lower then you'd think, and you can overtorque things easily.

With that said, you have two choices he

A) Put a torque wrench on it, tighten it and then fly it. Torque
settings are in the Lycoming Direct Drive Overhaul Manual (~$17 for a
reprint from Aircraft Spruce, or find the equivalent Continental
publication). Check it every few hours.

B) Take it to your A&P. He will pull out his torque wrench, his copy
of the Lycoming Direct Drive Overhaul Manual, tighen it, and tell you
to check it every few hours.

It's up to you.

Tina Marie
Tripacer N3653P
--
http://www.tripacerdriver.com "...One of the main causes
of the fall of the Roman Empire was that, lacking zero, they had no way
to indicate successful termination of their C programs." (Robert Firth)
  #10  
Old February 17th 04, 03:37 AM
Orval Fairbairn
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Posts: n/a
Default

In article ,
Tina Marie wrote:

In article , Greg Hopp wrote:
Partner and I have grounded the plane. The gents hanging out at the
FBO say, put a wrench on her and fly the darn thing. We'd prefer to
stay safe, legal and alive.


Don't just crank it down with a wrench! In general, every bolt connecting
everything to your engine has a proper torque. A lot of those torque settings
are way lower then you'd think, and you can overtorque things easily.

With that said, you have two choices he

A) Put a torque wrench on it, tighten it and then fly it. Torque
settings are in the Lycoming Direct Drive Overhaul Manual (~$17 for a
reprint from Aircraft Spruce, or find the equivalent Continental
publication). Check it every few hours.

B) Take it to your A&P. He will pull out his torque wrench, his copy
of the Lycoming Direct Drive Overhaul Manual, tighen it, and tell you
to check it every few hours.

It's up to you.

Tina Marie
Tripacer N3653P


According to my Lycomung Overhaul Manual, the cylinder torque settings
a

1/2" base nuts: 600 in-lb (50 ft-lb)

3/8" base nuts: 300 in-lb (25 ft-lb)

Tightening sequence: (1/2" first)

On the O-235, tighten as if you have 1/2" bolts, too

1/2" 3/8"

4 1 4 1

3 2 3 2
 




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