4300 Attitude Indicator

4300 Attitude Indicator

Mid-Continent Electric Attitude Indicator 4300-411. Mid-Continent 4300 Series Lifesaver Electric Attitude Indicator with Standby battery system provides up to one hour of emergency attitude reference in the event of aircraft power failure, a safe alternative to unreliable vacuum systems. This Mid-Continent Electric Attitude Indicator 4300-411 is an exceptional Value – 7,500 hours MTBF, which is more than double the life of most electric gyros. Perfect for use as a primary or standby artificial horizon in fixed-wing aircraft and helicopters. The 10–32 volt DC operation is for use in both 14 and 28 volt aircraft. Anti-reflective glass enhances visibility and reduces fatigue. Approved to FAA TSO-C4c and RTCA/DO-160D certified and qualified to DO-160 for helicopter vibration.
  • Custom versions available to match existing instrument/EFIS displays
  • Optional self-contained battery backup (Provides up to one hour of emergency attitude reference in the event of aircraft power failure)
    • Built-in annunciation
    • Internal emergency lighting
  • Single connector installation for primary and optional standby battery models
  • Exceptional value - 7,500 hrs. MTBF, more than double the life of most electric gyros
  • Perfect for use as a primary or standby artificial horizon in fixed-wing aircraft and helicopters
  • 10-32 volt DC replacement for use in either 14 or 28 volt aircraft
  • Anti-reflective glass enhances visibility and reduces fatigue
  • Field replaceable lighting
  • Approved to FAA TS)-C4c
  • One-year limited liability
  • Lifesaver® self-contained battery backup features:
    • One hour of emergency power*
    • Built-in annunciation
    • Internal emergency lighting
  • Versions available to match existing instrument/EFIS displays
  • A safe alternative to unreliable vacuum systems
  • Ideal primary or standby artificial horizon in fixed-wing and helicopter applications
  • Single 4-pin connector installation
  • 7,500 hours MTBF — more than double the life of most electric gyros
  • 10–32 volt DC operation for use in both 14 and 28 volt aircraft
  • Field-replaceable lighting
  • Anti-reflective glass enhances visibility and reduces pilot fatigue
  • FAA TSO-C4c certified and RTCA DO-160D qualified
  • DO-160 qualified for helicopter vibration
  • Designed and built in Wichita, Kansas, USA
  • One-year limited warranty
* Fully charged and properly maintained battery. See installation manual.
Specifications:
MTBF: 7,500 Hours
High-stability tungsten rotor operates at lower rotational speed, extending bearing life
Certification: FAA TSO-C4c
Power Input:

28 VDC version: 560 mA start, 250 mA max. running
Optional 10-32 VDC version:

  • 1290 mA start, 540 mA max. running at 14 VDC input
  • 560 mA start, 250 mA max. running at 28 VDC input
Battery: Rechargeable, custom lead-acid cell array
Life = 3 years in average arcraft environment
Runtime = 60 minutes minimum, when fully charged
Annunciators: Push to engage annunciator:
  • STBY PWR - standby power mode
  • TEST - battery test
Lighting: 5, 14, or 28 VDC; fuield replaceable tray wired through main connector
Glass: Special HEA anti-reflective coating
Weight: 2.7 lbs. or 3.7 lbs. with battery option
Length: 6.6 inches maximum, 8.6 inches with battery option
Mounting: Rear mount standard 3-1/8" round panel cutout
Temperature Range: -30°C to +50°C, -22°F to +122°F

Options: (please specify)

Power Output: 28 VDC fixed or 10 to 32 VDC
Lighting: 5, 14 or 28 VDC
Lighting Color: White, Blue/White or Red
Panel Tilt: 0° to 20°
Dial: Fixed or rotating roll dial configurations, traditional or delta wing airplane
Knob Cover: Restricts reference airplane adjustment
Emergency Battery: One hour run time; automatic charging system. Remote mountable
Inclinometer: Front-mounted, ball-type slip indicator
Mounting: Front mount available with ARINC style adapter plate

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