Cessna 210 charging problem

Nathan Young wrote in message . ..
On Thu, 08 Jul 2004 03:53:23 GMT, "John Clonts"
wrote:

I am now able to reproduce my charging problem.

Engine off, Bat and Alt on:
Bus voltage: 24.8
Supply to Voltage Regulator: 22.6
Voltage Regulator Output to Alt Field: 21.6

I'm thinking maybe I should rig a jumper from Bus to the Voltage regulator
to see if the problem has to do with that 2.2v drop through the "Alt/Reg" 5A
circuit breaker, the Alt side of the master switch, and the Overvoltage
relay.

John, I didn't see your original charging problem, so cannot comment
on that, but will make a few general comments on this post.

21.6 Volts seems like a high field voltage to drive the alternator.
What kind of load was on the system during this measurement? I'm not
certain, but believe wih minimal load, the field voltage on my 14V
system was around 6-7V.

This was with the engine off and no load to speak of. Maybe I will
try monitoring it as I add load, and see what it does.

The documents at www.zeftronics.com suggested that the VR field output
of "0.5-2.0v less than the VR input" was acceptable (22.6 - 21.6 =
1.0v)


The 2.2V drop between the master bus and VR is not good and can lead
to several problems in the electrical system. I would fix this before
doing anything else.

#1. The bus voltage will be high. The VR will crank up the field
voltage until its input 'sees' 24V. Given a constant drop of 2.2V
between bus and VR, the bus will be at 26.2.


Per your logic I think I would be seeing 30.2 instead of nominal 28.0
when the engine is running? I will check that.

#2. If the resistance causing the 2.2V drop is caused by a bad CB,
switch, or loose/corroded connection before the OVR, the resistance
will vary depending on temperature and turbulence knocking the system
around. This will cause OVR cutouts as the OVR will occasionally see
the full bus voltage which is 24V + the voltage drop from a second ago
(26.2V or higher).

#3. Resistance between the master bus and the VR input sets up an RC
circuit which (when extreme) can cause charging system oscillation.


I have noticed the ammeter bouncing slightly at about 4 per second
(when in the VR "control region") ever since we have owned the plane.
Maybe that was not acceptable?

I like your idea of trying to eliminate the drop between the bus and
the VR input by direct connecting it to the bus. (Make sure to have
your avionics master OFF when doing this kind of troubleshooting!).


Thanks, I thought of it myself but have since read of it elsewhere

Another approach would be to measure the voltage after each of the
field CB, field switch, OVR, and VR input. This will probably tell
you where the drop is, and you can do this without the plane running.


Yeah but aren't those buggers hard to get to? At least I have never
attempted it.

BE EXTRA CAREFUL when probing around under the panel, it is easy to
short things with voltmeter probes.


Ok, thanks for all the info!

Cheers,
John Clonts
Temple, Texas
N7NZ