Airplane Factory SLING 4, Pilot Operating Handbook

Page: 124 / 157

Airplane Factory SLING 4
Pilot Operating Handbook
Page | 7-21
DC-POH-001-X-C-3 Revision : 1.3
MGL EFIS instruments, including the Voyager, Odyssey, Discovery, Explorer
and Challenger, are multifunction “glass cockpit” instruments and typically
incorporate a range of different instruments and functions. Although only
the minimum specified instrumentation is required (see paragraphs 2.13
and 7.14 of this Pilot Operating Handbook), the full instrumentation
provided by the EFIS will typically include:

ASI (IAS as well as TAS and ground speed).

ALT (and typically also height above ground).

VSI.

Compass.

Attitude indicator.

Turn coordinator.

G meter (load factor meter).

Clock, stopwatch and flight time record.

Comprehensive mapping and navigation software and data,
including GLS (GPS Landing System) capability.

GPS.

Autopilot (if servos are fitted).

Full engine monitoring and management capacity including :

RPM indicator.

CHT and EGT indicators.

Oil temperature and oil pressure indicators.

Fuel level, fuel flow and fuel pressure indicator.

Hobbs and flight time recorder.

Voltmeter.
The EFIS installed in the aircraft is (can be) powered from two separate
power sources:

From the main bus, through a circuit breaker and a main selection
switch (labeled EFIS) mounted on the instrument panel. Refer to
paragraph 7.19.2.