Today's Message Index:
----------------------
1. 04:48 AM - Re: Tech: Annual Headache (Harry Merritt)
2. 04:52 AM - Re: panama jim (Bill Bow)
3. 08:31 AM - Re: whereabouts (Frits Abbing)
4. 03:28 PM - Re: Tech: Annual Headache (Todd Hindmarsh)
5. 04:39 PM - Re: Tech: Annual Headache (YOURTCFG@aol.com)
Message 1
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| Subject: | Re: Tech: Annual Headache |
--> Commander-List message posted by: "Harry Merritt" <avtec2@bellsouth.net>
I Have
Harry
321 267-3141
----- Original Message -----
From: Todd Hindmarsh
To: commander-list@matronics.com
Sent: Tuesday, February 25, 2003 5:35 PM
Subject: Commander-List: Tech: Annual Headache
--> Commander-List message posted by: "Todd Hindmarsh" <todd@inpnet.org>
Hi Everyone,
I have several Q's so be patient with me. All are for a '58 680.
Capt. JimBob - How much is the No AD Prop change?
Can we get away from the Bell crank AD? If so how much does it cost?
For Harry and/or Morris and/or Tylor:
We need a Tach Generator, and a Generator for the left engine.
Also a DME Antenna.
Our co-pilot Attitude Indicator is starting to act up. Does anyone have one
of those?
Having a prop AD that has to go to the factory, a bell crank AD and a wing
spar AD all at once isn't all that much fun.:-)
Thanks in advance everyone,
Todd
N6229B
Message 2
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--> Commander-List message posted by: "Bill Bow" <bowing74@earthlink.net>
> I want to come pick up my airplane tomorrow or Thu. latest.....maybe I can
> have some lunch/coffee with you & Morris!
>
> /John
I know Morris, you mean doughnuts.
bilbo
Message 3
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--> Commander-List message posted by: Frits Abbing <fritsabbing@yahoo.com>
Hi Barry,
You came up with 2,680FL for sale and I received also
that message. Are you able to sort out which ones are
here to be looked at?
I am in contact with the guy. You need registration
for that?
Thanks,
Frits Abbing
http://taxes.yahoo.com/
Message 4
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| Subject: | Tech: Annual Headache |
--> Commander-List message posted by: "Todd Hindmarsh" <todd@inpnet.org>
Thanks JB. What props specifically does the STC require?
What "Bellcrank" AD??
14 CFR Part 39 Aileron Bellcrank Casting
AD 57-09-01
57-09-01 AERO COMMANDER: Applies to All Model 680 Aircraft.
Compliance required not later than the next 3 hours of flight or May 15,
1957, whichever occurs first and at 100-hour intervals thereafter.
As a result of finding cracks in the aileron bellcrank casting in the
vicinity of the aileron push-pull rod attach bolt, the following action is
considered necessary unless already accomplished.
Inspect, using dye penetrant or fluorescent methods, all aileron bellcrank
castings P/N 3510005 on bellcrank assembly P/N 4510004-401 and 402 for
cracks in upper or lower lugs to which the aileron push-pull rod attaches.
Remove rod to make the inspection, replace all castings found defective and
reattach push-pull rod, making certain no clearance exists between casting
lugs and rod-end bearing inner race before tightening bolt. Use shim washers
to eliminate clearance. The 100-hour reinspection of casing P/N 3510005 may
be discontinued upon installation of revised casting under development by
Aero Design. (Aero Design Service Bulletin No. 41, dated April 19, 1957,
provides a sketch of the part and defines the area to be inspected.)
This AD covers the same inspection required by CAA telegraphic instructions
dated April 25, 1957.
Message 5
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| Subject: | Re: Tech: Annual Headache |
--> Commander-List message posted by: YOURTCFG@aol.com
In a message dated 2/26/2003 4:15:53 PM Pacific Standard Time,
todd@inpnet.org writes:
> 57-09-01 AERO COMMANDER: Applies to All Model 680 Aircraft.
>
> Compliance required not later than the next 3 hours of flight or May 15,
> 1957, whichever occurs first and at 100-hour intervals thereafter.
>
> As a result of finding cracks in the aileron bellcrank casting in the
> vicinity of the aileron push-pull rod attach bolt, the following action is
> considered necessary unless already accomplished.
>
> Inspect, using dye penetrant or fluorescent methods, all aileron bellcrank
> castings P/N 3510005 on bellcrank assembly P/N 4510004-401 and 402 for
> cracks in upper or lower lugs to which the aileron push-pull rod attaches.
> Remove rod to make the inspection, replace all castings found defective and
> reattach push-pull rod, making certain no clearance exists between casting
> lugs and rod-end bearing inner race before tightening bolt. Use shim washers
> to eliminate clearance. The 100-hour reinspection of casing P/N 3510005 may
> be discontinued upon installation of revised casting under development by
> Aero Design. (Aero Design Service Bulletin No. 41, dated April 19, 1957,
> provides a sketch of the part and defines the area to be inspected.)
>
HI TODD.You must be kidding. Your airplane was never changed?? I suggest
going to a salvage yard and buying a bellcrank, that will end the AD. Yours
is the first and only airplane that I have heard of that has an old belcrank.
jb
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