PlaneTools.com
Digital Tachometer

The Digital
tachometer is recommended to replace outdated mechanical tachometers
and cables.
Approved by
the FAA for installation on most single engine aircraft as the primary
instrument.
Accurate in
all conditions, easy to install, provides diagnostic and performance
information for the engine and ignition system and eliminates operational
and maintenance problems related to mechanical tachometers and cables.
Kit includes
all parts, STC, Operating and Installation manual. Patented software technologies bring to the aviation instrument panel
an Electronic Digital Engine
Tachometer. The tachometer is light-weight, accurate
under all operating conditions, easy to install and maintain, and easy
to view.
Additionally, it provides diagnostic and performance information
about the aircraft engine and ignition system not normally available
with current mechanical or electrical/electronic tachometers.
The digital tachometer eliminates problems resulting from inaccurate
tachometers: engine operation outside of allowable RPM ranges, reduced
engine life, reduced fuel economy, reduced power or propeller
overspeeding -- all of which and result in hazardous flying conditions.
Special ordering instructions:
When you order on-line send us a separate email to advise the hours
to set in the hour meter, aircraft "N" number and shipping instructions
(UPS overnight, 2-day, 3-day or ground; actual shipping will be charged
to your credit card).
STC approved for primary installation, not just secondary on the
following airplanes:
Aerospatiale TB9, TB10, TB20, TB21
Air Tractor, Inc. AT-250, -300, -301, -401, -401A,
-401B, -501
Ayres Corp., Rockwell, Aero Commander 600-S2C, S-28,
S-2C, 600-S2D, S-2R-R1340, S2R-R3S, 600-S2D, S-2R, 2R-R3S
Beech Aircraft Corp. E33, E33A, E33C, F33, F33A,
F33C, G33, 35, A35, B35, C35, D35, E35, F35, G35, H35, J35, K35, M35,
N35, P35, S35, V35, V35A, V35B, V35ATC, V35BTC, 35-33, 35-A33, 35-B33,
35-C33, 35-C33A, H35, J35, K35, M35, N35, P35, S35, V35, V35A, V35B,
36, A36, A36TC, B36TC
Cessna Aircraft Corp. 172 through 172Q, FP172,
P172D, R172K, R172K with 210 Horsepower, 172RG, 175 through 175C, 177,
177A, 177B, 177RG, 180 through 180K, 182 through 182S, A182K, A182L,
A182S, T182R, R182, TR182, 185 through 185E, A185E, A185F, 206, P206
through P206E, TP206A through TP206E, TU206A through TU206G, U206
through U206G, 207, 207A, T207, T207A, 210 through 210N, T210F through
T210R, P210N, P210R, 210-5, 210-5A,
Gulfstream AA-5, -5A, -5B, AG-5B
Lake C-1, C-2, LA-4, LA-4A, LA-4P, LA-4-200
Mooney M20 through M20M, M20T
Piper PA-23, PA-23-160, PA-23-235, PA-23-250,
PA-E23-250, PA-24, PA-24-250, PA-24-260, PA-24-400, PA-28-140, -150,
-151, -161, -180, -181, 235, -236, -201T, -R-180, -R-200, -R-201,
-R201T, -RT-201, -RT-201T, -S-160, PA30, PA39, PA-40, PA32-260, -300,
-301, -301T, R-300, RT-300, -300T, PA46-310P, PA46-350P
Schweizer, Grumman, AG-Cat G-164 through G-164C
Weatherly 620
Technical Description of the Tachometer Operation
The operation of the Electronic Digital Tachometer is straight
forward. After power is supplied to the Tachometer, the engine is
started, and the self-tests are performed, the default display of engine
RPM appears on the display. The default display is insured via the use
of internal timers that will restore the display to the current RPM even
in the event that one of the panel buttons becomes stuck or defective.
Internally, two independent tachometers watch the pulses received
from each magneto. Each tachometer is accurate to less than 1 RPM and
can be individually enabled/disabled via buttons on the face of the
Tachometer.
Engine operation ranges are indicated on the large green, yellow and
red LEDs, see Figure 3, items D, E, and F.
Three small LED magneto system alert indicator lights
are located within the "Status" area on the upper left corner of the
Tachometer face, see Figure 3, items A, B, and C. The left and right red
alert indicator lights, when illuminated, indicate,
because of a loss of ignition signal to the tachometer, a possible
malfunction of the respective left or right magneto ignition system.
While performing a magneto check during engine run-up, the red
alert indicator lights will illuminate, thus identifying the
grounding of the respective right of left magneto systems.
Between the left and right red magneto ignition system alert
indicators is a yellow "RPM Synchronization" indicator.
This small yellow indicator is illuminated when there is a difference of
more than 80 RPM between the right and left tachometers. This indicator
also may flicker during extreme RPM excursions of the engine.
There are three panel buttons, see Figure 3, items I, J, and K. Each
button has two modes of operation:
- Press-and-hold,
- Press-and-release.
Press-and-hold button operations instruct the Tachometer to perform a
specific operation when a button is pressed and held for more than 2/3
of a second.
Press-and-hold button operations are placarded on the face of the
Tachometer above each button.
Similarly, press-and-release button operation instructs the
Tachometer to perform a specific operation when a button is pressed and
released in less than 2/3 of a second. Press-and-release button
operations are placarded on the face of the Tachometer below each
button.
PRESS AND HOLD OPERATIONS:
The left button, K, upon depression, will cause the Tachometer to
display the non-fractional portion (0000.) of the current accumulated
engine hours. When the button is released, the fractional part of the
engine hour (.00) is displayed for a short period of time. The clock is
started whenever the engine RPM exceeds 800 RPM and is recorded in real
hours.
The right button, I, upon depression, will cause the Tachometer to
display the current contents of the RPM trap. This trap records the
highest engine RPM achieved before the button was pressed.
The middle button, J, upon depression, clears the RPM trap. During
depression of the switch, the RPM trap is zeroed. When the button is
released, the trap will record the current engine RPM.
PRESS AND RELEASE OPERATIONS:
During normal operation, the Tachometer presents the average of the
left and right internal tachometers on the display. However, a mechanism
exists to mask either tachometer from the display, leaving the remaining
tachometer to display its RPM.
A masked tachometer is indicated by the regular flashing of the right
or left signal loss status indicator LEDs. This feature is handy when
attempting to determine magneto/ignition problems.
Quickly pressing and releasing the left button, K, causes the
Tachometer to mask or un-mask the left internal tachometer.
Quickly pressing and releasing the right button, I, causes the
Tachometer to mask or un-mask the right internal tachometer.
An internal interlock prevents masking both internal tachometers at
the same time, therefore preventing total loss of RPM indication.
If the tachometer is masked, pressing the button will un-mask it and
allow its RPM to show on the display, and conversely, if the tachometer
is un-masked, pressing the button will mask it from display.
Quickly pressing and releasing the center button, J, causes the
Tachometer to alternately dim or brighten the LED indicators.
The LED indicators, see Figure 3, items A through F, are bright
enough to overcome daylight washout conditions. However, during night
operations the large green, yellow, and small red and yellow LEDs are
dim-able. The large red LED still operates at full intensity to maximize
the possibility of gaining pilot attention during excursion into
restricted RPM ranges.
The Tachometer differs from the existing mechanical tachometer in the
following areas:
The Tachometer is fully electronic and uses timing information from
the primary leads ("P-Leads") of both the left-hand and right-hand
magneto ignition systems, operating the Tachometer's internal left and
right tachometers, to determine engine RPM instead of a rotating cable
driving a magnetic slip-clutch analog type display;
The Tachometer uses super-bright LED indicators to indicate normal
range engine operation (Green LED), cautionary range operations (Yellow
LED), and do-not-exceed or restricted range RPM (Red LED) as substitutes
for the ranges normally painted on the tachometer dial.
The primary display consists of four 1/2" high characters on a
back-lit Liquid Crystal Display (LCD), easily and clearly visible in
daylight and night flying.
Diagnostic features available include: alert
indication of loss of magneto signal, indication that both magnetos are
reporting different RPM, and the ability to mask RPM from either
magneto.
Magneto test, via the ignition switch, is indicated by the
illumination of the grounded magneto system's alert light
and the display of the amount of RPM that the engine has slowed. This is
indicated as a negative number on the display (number is preceded by a
leading hyphen or minus sign);
LED indicators are dim-able (except the restricted or red-light
indicator) to reduce pilot annoyance during night flying;
A specific engine hour is pre-set at the factory to accommodate
tachometer changes on non-zero-time engines. Engine time may be changed
only by Horizon Instruments, Inc., Repair Facility.
A) Right Magneto System Alert Indicator
B) RPM Sync Loss Indicator
C) Left Magneto System Alert Indicator
D) Normal Operating Green RPM Range Indicator
E) Cautionary Yellow RPM Range Indicator
F) Restricted Red RPM Range Indicator
G) Limitations Placard
H) 4 Digit LCD Display
I) Right switch for Overspeed Trap display and right tachometer
enable/disable
J) Middle switch for Overspeed Trap Clear and LED indicator dimming
K) Left switch for engine hours display and left tachometer
enable/disable.
CLICK HERE FOR SECURE ORDERING ON-LINE.
Please note that although the link is for the 210
horsepower XP you may order a digital tach for any of the above
airplanes at this link.
Isham Inc.
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