Technical Specifications; Warranty - MGL Avionics Stratomaster Smart Single Manual

G/M: U.S. Gallons and statute miles
L/Nm: Liters and nautical miles
G/Nm: U.S. Gallons and nautical miles
L/Km: Liters and kilometers
G/Km: U.S. Gallons and kilometers

Technical specifications:

Display temperature range (operational): -20 to +80 degrees C
Supply voltage: +8 to +18V. +24/28V with optional pre regulator.
Supply current: 35mA/70mA (backlight off/on)
Fuel level input: Maximum voltage: 5V, 5mA maximum current.
Fuel level senders supported: Any resistive type with common ground and capacitate probes with
active voltage outputs up to 5V level (push pull or pullup).
Fuel flow senders: Supply 5V, 20mA maximum current. TTL level input with noise filter and
schmidt trigger hysteresis. Required input voltage swing: less than 1.5V to more than 3.5V.
Maximum input voltage range -5V to +18V.
Weight: 90 grams.

Warranty:

MGL avionics warrants their products for a period of one year from date of purchase against faulty
workmanship. Warranty is limited to the replacement of faulty components and includes the cost
of labor. Shipping costs are for the account of the purchaser.
Note for operation on supplies with inductive loads:
Any operation of electronic instrumentation on power supplies that are subject to high voltages
caused by operation of inductive loads (starter motors, solenoids, relays) are required to be fitted
with suitable protection.
All Smart Singles are guaranteed to withstand temporary over voltage up to 40V without additional
protection. We recommend that measures are taken to prevent voltage transients in excess of
this limit.
MGL Avionics recommends the fitment of a fuse in line with a 33V transorb (available from MGL
Avionics at low cost) to protect electronic instruments, radios and intercom systems. Only one
such arrangement is required for a cluster of instruments.
Please note that product warranty excludes damages caused by unprotected, unsuitable or
incorrectly wired electrical supplies.
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 pilots license. This person has to
make him/herself 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.