Specifications - L3 Communications GH-3100 Pilot's Manual

Electronic standby instrument system
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Specifications

Specifications
GH-3100 ESIS and DCM-3100 Detachable Configuration Module
TSO No.: C2d, C4c, C6d, C8d, C10b, C34e, C36e, C40c, C46a, C66c, C113,
C115b
MAG-3000 Magnetometer
TSO No.: C6d
Power
Requirements
Weight
Connector (J1)
Connector (J2)
Static Air Port:
Pitot Air Port
Service Life
Schedules
Maintenance
Storage
Operation
Requirements
Mach Range
Altitude Range
Indicated
Airspeed Range

GH-3100 Electronic Standby Indicator
Starting: (warm up) 50.0 watts at +28.0 Vdc, continues
for first five minutes of operation.
Running: (with heaters, fan, and thermal electrical
cooler off) will not exceed 23.5 watts at 28 Vdc input.
Lighting Power: 0.708 watts at 5.0 Vac or Vdc or
0.9 watts at 28.0 Vac or Vdc (dependent on model
variant).
4.00 Lbs. (1.81 Kg) maximum.
Avionics Systems P/N 563-1113-01 mates with
MS3116F18-32S (solder contacts) or MS3126F18-32S
(front crimp contacts) or MS3476L18-32S (rear crimp
contacts) with M85049/52S18W strain relief.
Avionics Systems P/N 563-1013-21 for interface port
to DCM-3100 and diagnostic port.
IAW MS33649-05
IAW MS33649-04
Repairable by an authorized commercial instrument
repair station. Service Life is unlimited.
No scheduled maintenance interval applicable. Unit
is subject to bi-annual requirements of FAA CFR par
FAR 91.411.
Indicator performs satisfactorily after periods of up to
24 months.
DCM-3100 installed at J2 is required to operate.
0.30 to 1.00
–1,000 to +55,000 feet
0 to 450 knots
GH-3100
Pilot's Guide

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