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December 1982 - American Bonanza Society

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It sounds as if your instrument air<br />

pump is wearing. It is important to use<br />

th e new pleated-type instrument<br />

induction air filter and to replace the<br />

inline filter on a regular basis. It helps<br />

to install an air blast tube to cool the<br />

pump . The pump vanes are made of<br />

carbon and run dry and hot, so they do<br />

sluff off. The black you see is on the<br />

pressure relief valve and is norm al.<br />

H-35 CABIN NOISE LEVEL<br />

Dear Norm :<br />

l awn a 1957 H-35 <strong>Bonanza</strong>. The<br />

engine noise level in the cabin is very<br />

high, especially when compared to the<br />

S and later model <strong>Bonanza</strong>s which I fly<br />

regularly . New mufflers and Beryl<br />

D'Shannon exhaust pipe extenders<br />

have not improved the situation<br />

appreciably. Even the exhaust manifold<br />

gaskets were replaced to no avail.<br />

Could you please advise as to wh at<br />

type of soundproofing materials could<br />

be used, along with installation<br />

instructions and where in the air frame<br />

soundproofing would be most effecti ve<br />

Ron Saglimbene<br />

ABS # 13335<br />

Dear Mr. Saglimbene:<br />

The primary source of cabin noise<br />

comes through the windshield and side<br />

cabin windows. Replacing the<br />

windshield and windows with thicker<br />

glass is th e easiest way to lower noise<br />

level.<br />

3M Products makes a sound<br />

deadener called, ·'Scotch Foam Y-370··.<br />

This is a self-adhesive foam in sheet<br />

form . GT Sales and Manufacturing at<br />

220 2 South West Street, Wichita,<br />

Kansas 67203, 3 16 / 943-2171 , stocks<br />

this material along with other sound<br />

deadeners. The firewall and cabin side<br />

panels forward of the firewall require<br />

the most deadener. The belly skins<br />

below the floorboard s take a black<br />

spray-on sound deadener; however,<br />

factory installed material in this area<br />

should be adequate.<br />

Be sure the exhaust stacks clear the<br />

fuselage structure in the cowl flap well.<br />

And , remember, in cruise the engine<br />

cants to the left about 3 / 8 inch .<br />

Skin canning in flight can make a<br />

terrible noise, so be sure that<br />

somethIng other than normal engine<br />

and propeller sound is not contributing<br />

to cabin sound.<br />

SECOND INSTRUMENT PUMP<br />

ADDITION TO DEBONAIR<br />

Dear Norm:<br />

I have a few questions concerning<br />

our 1960 Debonair (CD-1 20):<br />

1) Is it possible to install a second<br />

vacuum pump on the spare accessory<br />

pad on the 10-470 I want to have this<br />

pump drive a second and separate<br />

horizon rather than tie it into th e<br />

existing horizon. An y ideas<br />

2) Both main fuel gauges show full<br />

when the tanks are full , but after using<br />

either tank for a short period (20 - 30<br />

min) the indicator goes down to 1/ 2 to<br />

1/ 4. Cycling the gauge selector switch<br />

from left to right sometimes helps, but<br />

not usually .<br />

3) I would like to replace the existing<br />

mixture control to a vernier type and<br />

need to know where to get one. Al so ,<br />

how long is the cable - as I see them<br />

adverti sed with varying cable lengths<br />

4) Where can I get a copy of the<br />

book, " Those Incomparable<br />

<strong>Bonanza</strong>s" <br />

S. P. Simpson<br />

ABS # 15346<br />

Dear Mr. Simpson :<br />

I can see no reason why a second<br />

pump could not be added. At the<br />

moment, I do not know of such an<br />

installation; so you would have to work<br />

out th e plumbing details (which should<br />

not be a big deal) and either obtain an<br />

STC approval or obtain a one-time FAA<br />

approval.<br />

You can purchase a throttle vernier<br />

control from any Beechcraft dealer. I<br />

think Part # 35-944046-1, which fits a<br />

Model M-35 <strong>Bonanza</strong>, will work. I do<br />

not have access to cable lengths.<br />

Write to Larry Ball , 8529 Chapel<br />

Glen Drive, Indianapolis, Indiana 46234,<br />

to request one of his books.<br />

VACUUM PUMP FAILURES<br />

Dear Norm:<br />

During the past several months,<br />

there have been many articles in<br />

various trade publications regarding<br />

vacuum pump failure during IFR fli ght.<br />

I'm now a " nervous believer".<br />

I would like to install a vacuum<br />

failure warning light or horn on an<br />

F-35, but our local Beech facility does<br />

not know how to proceed. To your<br />

knowledge, can this be accomplished<br />

D. W. Wennberg<br />

AB S # 11 64 3<br />

Dear Mr. Wennberg:<br />

This is in reply to your letter in which<br />

you talked about vacuum pumps.<br />

I think that most of the talk you have<br />

been hearing about instrument air pump<br />

failures are related to the dry<br />

instrument air pressu re pumps.<br />

Your instrument air pump is a wet<br />

vacuum pump which is intern ally<br />

lubricated and will norm ally run trouble<br />

free between engine overhauls. Like<br />

anything mechanical there is always the<br />

possibility of failure but from past<br />

service experience, it is remote.<br />

A light or horn could be hooked into<br />

the system, by installing a pressure<br />

switch, but pressure switches give<br />

trouble, too and I really believe they<br />

would not accomplish what you want,<br />

because when pumps fail , the drive<br />

shaft shears and the pump stops<br />

without warning.<br />

I feel that your fears are unfounded.<br />

Just be sure that the vacuum pump is<br />

overh auled at engine overhaul.<br />

Thank you for writing.<br />

FUEL VENT SYSTEM IN A<br />

TRAVEL AIR<br />

Dear Norm:<br />

I have read several incidents recently<br />

on problems with the <strong>Bonanza</strong> fu el<br />

venting tubes. Since my Travel Air is<br />

very similar to a <strong>Bonanza</strong> in many<br />

aspects, I am concerned that the fuel<br />

venting tu bes are not positioned in the<br />

proper angle nor extend from the base<br />

of the wing the proper length to give<br />

proper venting per article, " Damage to<br />

Venting System", page 1243, October<br />

Newsletter).<br />

Nowhere in either my maintenance or<br />

parts manual are there any indications<br />

on the length or angle that these vent<br />

tu bes should take. If there is any<br />

inform ation you can provide me, I would<br />

appreciate it very much.<br />

Clifton M. Buell<br />

ABS # 14983<br />

Dear Mr. Buell:<br />

Fuel vents in your Travel Air should<br />

protrude below the wing or fuselage<br />

one-and-three-quarter inches and<br />

should be bent forward ten degrees .<br />

The end of the tube should be<br />

champhered at 45 degrees. Vent tubes<br />

have a small ice-free vent hole drilled<br />

through the back side of the vent tube.<br />

When bending th e vent, always bend<br />

the tube below this vent hole.<br />

It is a good idea to occasionally<br />

apply low pressure air to the vent tubes<br />

to be sure they are free of internal<br />

obstructions. Always remove the fuel<br />

caps before applying compressed air to<br />

the vent tubes.<br />

OIL COOLER ON MODEL 35<br />

BONANZA<br />

Dear Norm:<br />

I have a question regarding repair (or<br />

rebuilding) of the E-series oil radiator<br />

used on SI N 0-11 17 and later. Since<br />

Beech can no longer supply this part, I<br />

am wondering if you could put us in<br />

touch with the original manufacturer. I<br />

would like to obtain a new radiator only<br />

(not inc luding tank) for welding into our<br />

existing tank.<br />

We have a leak at present involving<br />

only one of the radiator tubes. It is a<br />

simple-enough matter to plug oft one or<br />

two tubes: however, if one tube is<br />

corroded through, several others may<br />

not be far from failing.<br />

Our problem is not urgent. This is a<br />

spare tank which we purchased several<br />

years ago as part of a run out E-225.<br />

The leak was not discovered until 1<br />

american bonanza society<br />

page 1269

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