To get the most out of your
instruments some straight forward installation guidelines should be followed.
Please take the time to read these guidelines in full BEFORE commencing installation.
AT
ALL TIMES EXTREME CARE SHOULD BE USED TO PREVENT ANY INTERFERENCE WITH FULL
CONTROL MOVEMENT OF THE SAILPLANE. WE
STRONGLY SUGGEST THAT YOU HAVE A
QUALIFIED PERSON INSTALL OR CHECK YOUR INSTALLATION BEFORE FLIGHT.
Mechanical:
Install the instruments in
standard 57mm or 80mm panel holes with the fixing bolts supplied.
Do not use longer bolts.
To mount the
B500GCD(Glareshield controller/display) see the mounting suggestions.
Cruise/climb switch - to be
installed in a convenient location. Suggested places are on the control column
beside the radio press-to-talk switch. (many sailplane factories offer this option
in new sailplanes); on flap handle in flapped sailplanes. Switch bushing
requires 1/4"(6.35mm) hole
Mount the speaker(s) supplied
in a convenient location. e.g. on instrument panel, facing aft toward the pilot,
under the seatpan (this works extremely well) or just behind the rear canopy
bow on either or both (B500) sides.
Any other 8 ohm speaker(s) may
be used.
Optional Outside Air
Temperature(OAT) probe should be installed
in the air vent.
Electrical:
Follow the wiring diagram
attached to the top of the instruments.
Power and mode (cruise/climb)
switch wiring attaches to the external connection board (XCB) by way of screw
terminal connectors. DO NOT OVERTIGHTEN
THE SCREWS on the XCB as the connector may suffer damage.
The OAT probe plugs into its
socket and the speaker(s) plug into 3.5mm sockets on the XCB.
After the power , mode switch,
speaker(+optional OAT) have been attached to the XCB the cable tie (supplied)
may be used as a strain relief for these wires. Use any 2 of the 4 M3 holes in
the XCB for this.
The XCB may be removed by
removing the 2 x M3 machine screw in the top corners, tilting back to disengage
the DB15 connector then lifting to remove from the bottom M3 screw which is
fixed. Do not remove this screw it has been glued in place with anaerobic
adhesive. The lower XCB fixture has a slot to facilitate removal.
This allows the XCB with
wiring to remain in the aircraft in the event that the instrument requires
servicing.
Extreme care should be taken
to ensure correct polarity power is connected
to the instruments. While reverse polarity protection has been fitted,
we do not guarantee that under all circumstances this will necessarily protect
from damage.
Instruments which receive
aircraft power directly are fused on the XCB.
Power requirements are 10 to
15 volts DC from the aircraft power. Do not exceed 15 volts. 14 volt batteries
are not recommended as a fully charged battery will supply greater than 15
volts.
Pneumatic:
All tubing must be in good
condition and should be a very tight
press fit over the fitting to avoid air leaks. Even a small air leak
will compromise any variometer's performance. For extra insurance against air
leaks we supply small, thick walled
elastic `donuts' which you may install over tubing several inches past the end.
After the tubing is properly attached to the fitting on the instrument, slide
the `donut' back toward the end of the tube so that it supplies extra squeeze
around the tubing/fitting area. Do not use
electronic type nylon cable ties or twisted wire as this will guarantee a leak.
Connections are marked on the
label on the top of the instrument..
Connect the tubes leading from
the sailplane PITOT and STATIC and T.E. source to the pneumatic connections on
the rear of the B50 labelled `PITOT' and `STATIC' and `TE PROBE'. Providing a
good pitot and static source is very important. A Prandtl probe works well and
has minimal position error.
Position error will result in
incorrect speed commands and netto computation (B500).
The B500 has provision for
position error correction (contact factory or dealer with copy of glider flight
manual position error curve.)
{
Leak
check the system following installation. (See leak checking article)
Good practice hints
Mechanical
Plan your instrument panel
layout for optimum scan.
{
Require
assistance with layout? Contact Borgelt Instruments
Electrical
Separate power circuits for
the radio and vario systems are highly recommended. The reason for this is that
varios draw 100-200mA and a typical radio on TRANSMIT draws 2 AMPS.
If the radios and varios share
the same power buss any resistance in the circuit is multiplied by the 2 AMP
current draw of the radio on transmit instead of the 200mA of the vario circuit
resulting in a much larger voltage drop. This can result in your vario failing
to work properly during radio transmissions particularly if the battery is low.
Of course it is a good idea to
minimise resistance in the power wiring for optimal radio performance. Sources
of unwanted resistance are poor switch contacts, poor fuses, poor fuseholders,
poor battery connectors, wire gauge too small and bad soldering.
We recommend 18 gauge or
larger aircraft wire, electronics
industry type switches (not automotive as these sometimes have unplated brass
contacts which oxidise) and CANNON type latching connectors for the
battery. (4 pin - pin 1 positive, pin 4
ground. 3 pin - pin 1 positive, pin 3 ground.)
You may find that one power
buss with suitable wire and good quality connectors and switches will work
acceptably.
Extremely effective radio
interference protection is built into the instruments and no difficulties
should be experienced. However, it is good practice not to run antenna coax and
power leads in close proximity for any great length. The instruments will
perform properly down to a delivered voltage at the instrument of 10 volts.
On the B500 there is a voltage
display on one page of the GCD.
Pneumatic
The most common mistake in
variometer installations is to connect two vario systems to one Total Energy
line with a T-piece at the instrument panel. The only time that this is permissible
is when both instruments are of the pressure transducer type. (for example a
B400 and B500) That is no flasks hence no flow. Flow sensor type instruments
cause significant flows in the line to the T.E. probe and these flows can cause
these instruments to interact with each other or with a pressure transducer
type variometer causing weird behaviour or a general slowing of the response of
both instruments connected to the T.E. probe.
The T-piece in the T.E. line
should be as close as possible to the T.E. probe although in practice it has
been found that if the T.E. line is split under the pilot's seat, further aft
behind the seat or near the trailing
edge of the wing no problems will result. Maximising the flow resistance
between two vario systems and minimising the flow resistance between each
system and the outside air is the aim here. DO NOT place restrictors or gust
filters in the T.E. line and then split the line to two vario systems. If
installing these, place a separate restrictor or gust filter in each line to
the separate vario systems. Try also to ensure that there is no excessive flow
resistance in the T.E. probe mount or in the probe itself.
If a paper element filter is
installed in the TE line the filter body MUST BE EXTREMELY RIGID otherwise the
static pressure changes during a pullup will cause spurious variometer
readings. This applies also to any gust
filter bottles which may be installed
ANYWHERE in the T.E. system.
There should be no leaks in
any of the plumbing and long lengths of tubing should be of the less flexible
plastic or rigid nylon pressure hose. This prevents problems with the sudden
static pressure changes in the fuselage during zoom or pushover causing weird
transients in the T.E. vario readings due to these presssure changes being
transmitted through soft tubing in the T.E. line. Tubing should be securely
tied down.
General:
All aircraft instruments
contain glues, paints and plastics. Their life may be extended by not
subjecting them to extreme heat. It is good practice to use a canopy cover if
the sailplane sits in the sun before and after flying and also to insulate
under the black antireflection cover. `Space blanket material' works well. Make
sure the material does not short any electrical connections.
Other
Important Considerations
CAUTION: No matter what the
instrument indications may indicate is the optimum speed to fly:
{
AT
ALL TIMES THE FLIGHT ENVELOPE OF THE SAILPLANE MUST BE ADHERED TO.
{ DO
NOT EXCEED PLACARDED AIRSPEEDS FOR THE PREVAILING CONDITIONS.
Cleaning:
LCDs(Liquid crystal Displays -
B500 GCD, B2000) - if required use only a soft cloth and gently wipe the
display, taking care not to scratch the surface. Caution: the LCD is easily
damaged. Solvents MUST NOT BE USED on LCD or labels.
Meter glass: use a soft cloth
dampened with water or a small amount of proprietory glass cleaning solution.
Conversion to Metric Units(B400/B500):
If ordered with metric units
this will have been done in the factory.
The variometer scale on the
B400 or B500 may be converted to metric indication or knots by adding or
removing the 6 m/s label. The instrument calibration can be changed by
contacting your dealer or the factory.
WARRANTY
If, under normal operating
use, any part of the Borgelt Instruments
hardware proves to be defective in material and/or workmanship within
the warranty period of twenty-four months from date of purchase such defective
parts and/or workmanship will be repaired by Borgelt Instruments or their
approved agent. All freight charges are to be borne by the owner. This warranty
is not transferrable.
This warranty does not cover
damage caused by misuse, neglect, accident, reversal of polarity or repair or
attempts to repair by unauthorized personnel.
Any returns must be authorised
by Borgelt Instruments prior to shipping.
Please see “Return of
Instruments guidelines”