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AVIATOR pOinls - American Bonanza Society

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ELECTRICAL PROBLEMS<br />

Again this month, I am covering some common electrical problems<br />

that ABS members have asked me about over the years.<br />

Troubleshooting alternator-out light(s)<br />

One of the more common calls for advice goes something<br />

like this :"My alternator-out light is on, but the alternator seems to<br />

be working just fine:<br />

The early <strong>Bonanza</strong>s had generators and therefore did not<br />

use an alternator-out light. so this discussion does not apply. The<br />

P model and the S model had alternator options, but the warning<br />

light was an over-voltage indicator; so this discussion does<br />

not apply to them either.<br />

Starting with the 1968 model year for most <strong>Bonanza</strong> models,<br />

the alternator had an aux post added and an "alternatorout"<br />

light was added to the pilot panel. It was attached to a<br />

relay that turned off the light whenever the voltage at the aux<br />

post of the alternator exceeded a threshold voltage (about half<br />

the normal alternator voltage).<br />

The alternator-out relays proved to be problematic; so in May<br />

1969 Beechcraft issued Service Instruction No. 0180-364 that<br />

replaces the relay and a resistor with a transistor-based alternatorout<br />

sensor (PIN 36-380000-1). Note: This was not a mandatory<br />

change, so your aircraft may still have the original relay,<br />

The wire from the altematoI aux post was protected with an<br />

AGC3 fuse, usually mounted on an alternator fuse block on the<br />

engine side of the firewall, pilot side. If the fuse is burned out or<br />

any corrosion exists on either the fuse holder or the fuse itself,<br />

this can cause the alternator-out light to give a false indication.<br />

The fuse is supposed to protect the wire coming from the<br />

alternator-aux terminal to the alternator-out sensor. Since most<br />

of the wire is unprotected from the alternator to the fuse block,<br />

in August 1981 Beechcraft issued Service Instruction No. 1157<br />

that replaced the fuse with an inline fuse mounted near the alternator<br />

aux tenninal. It also changed the fuse to an AGCS.<br />

This exposed the fuse to the incoming airstream into the<br />

engine, so moisture could easily get into the inline fuse and<br />

accelerate corrosion, causing the false alternator-out indication<br />

to occur more frequently.<br />

To help solve the problem, Beechcraft issued Service<br />

Bulletin No. 2016 that replaced the inLine fuse with a small<br />

printed circuit board (PCB) that was mounted directly on the<br />

alternator aux post. The only component mounted on the PCB is<br />

a fusible resistor that perfonned the same function as the fuse.<br />

The PCB attaches to a wire via a screw and washer, which was<br />

in tum butt-spliced to the existing wire to the sensor. (See photo)<br />

There are some advantages to using the PCB mounted to<br />

the alternator aux post. For instance, it protects the entire wire<br />

to the sensor and the fusible resistor is fully encapsulated and<br />

therefore well-protected from corrosion. Unfortunately, there<br />

are problems as well.<br />

The PCB is located in a high-vibration area of the engine<br />

and is subject to cracking. or the solder lands separate from the<br />

PCB. Of course, if this happens, the sensor may get a false<br />

alternator-out indication.<br />

Beechcraft then changed the design to eliminate the PCB<br />

and simply mounted a fusible resistor with leads instead. This<br />

seems to give good reliability, but the vendor that supplies<br />

Beechcraft with the part stopped making them; so Beechcraft<br />

returned to the PCB design.<br />

Know how your airplane is wired<br />

With all the possible updates, one of the first things you<br />

need to do is to figure out how your airplane is currently wired.<br />

If you have the PCB, inspect it for any cracks or to see if the<br />

solder lands have lifted off the surface of the PCB, In all cases,<br />

check for signs of corrosion in any of the connections and<br />

clean as required.<br />

Then check the voltage of the input to the alternator-out<br />

sensor with the engine running and the alternator on. You should<br />

see half of the alternator regular output voltage at the aux tenni-<br />

Alternator with fusible resistor (yellow arrow) on a printed circuit board.<br />

RAPID LIST PIICE$<br />

Replacement 14-volt alternator-out sensor<br />

(PIN 36-380000-1) - $196.<br />

The 28-volt version (PIN 36-380000-3) - $122.<br />

The Baron uses replacement alternator-out<br />

(PIN 36-380000-11) - $119.<br />

A replacement PCB kit (PIN 55-3025-1 S) - $108.<br />

Use your ABS credit card for a discount on RAPID's list prices.

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