ALT-1 Operating Manual
Page 12
12 Disclaimer
Operation of this instrument is the sole responsibility of the purchaser of the unit. The user must make themselves familiar
with the operation of this instrument and the effect of any possible failure or malfunction.
This instrument is not certified by the FAA. Fitting of this instrument to certified aircraft is subject to the rules and
conditions pertaining to such in your country. Please check with your local aviation authorities if in doubt. This instrument
is intended for ultralight, microlight, homebuilt and experimental aircraft. Operation of this instrument is the sole
responsibility of the pilot in command (PIC) of the aircraft. This person must be proficient and carry a valid and relevant
pilot’s license. This person has to make themselves familiar with the operation of this instrument and the effect of any
possible failure or malfunction. Under no circumstances does the manufacturer condone usage of this instrument for IFR
flights.
Other instruments in the
Stratomaster Infinity
series
ALT-1
Precision encoding altimeter and vertical speed indicator
ALT-2
Precision encoding altimeter and vertical speed indicator with a serial RS232
transponder output
ASI-1
Airspeed indicator (ASI) with automatic flight log
ASX-1
Encoding aviation altimeter with serial output and airspeed indicator (ASI)
AV-1
Artificial horizon and magnetic compass indicator
BAT-1
Battery voltage and current monitor
E-3
Universal engine monitor
FF-1
Fuel Computer (single or dual fuel tanks)
GF-1
+-10G tilt compensated dual range G-force meter
MAP-1
Manifold pressure and RPM Indicator
RV-1
Universal engine RPM and rotor RPM Indicator
RV-2
Universal turbine RPM / RPM factor display
RTC-2
Aviation real time clock (RTC) and outside air temperature (OAT) display
TC-1
4-Channel thermocouple indicator
TP-1
Universal temperature and pressure gauge
The manufacturer reserves the right to alter any specification without notice.
