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Part #: 066-3114-00

Model: IN-812A

NSN:

5841-01-326-6141

OEM:

BendixKing

Desc:

Radar Indicator

Part Number :


IN-812A

 

FEATURES

  • Color radar indicator used with RDS-81
  • Display range/range marks of 10/2.5,20/5,40/10,80/20,160/40,240/60
  • Special inputs provided for direct external control of CRT color guns allowing an external graphics unit such as GC-360A or GC-381A to control display
  • Provides four color display of weather and a three color display of ground targets
  • Capable of handling 5,14, or 28 V panel lighting
  • Available with black or gray bezel (see table below)

 

SPECIFICATIONS

Altitude: 25000 ft. unpressurized Temperature: -20 to 55C
Dimensions: 6.4"W x 4.11"H x 12.75"L Weight: 8.9 lbs.
TSO: C63b Class 7 Env. Categories: DO-160A; A1B1/A/PKS/XXXXXXABABA
Input Power: 28VDC @ 2.0 amps continuous (operating); 14VDC @ 1mA, 28VDC @ 264mA or 5VAC @ 1mA (lighting) Self Test Capability: TST position on indicator selects test pattern
Part Number: Description:
066-3114-00 Black panel color, 5/14/28 volt lighting, Radar Indicator
066-3114-01 Gray panel color, 5/14/28 volt lighting, Radar Indicator

 

Serial # 12408
Condition SV
Mods 1-7
Tag Date 11/27/24
Shop Southeast Aerospace Inc.
Warranty 6 Months
066-3114-00
- Radar Indicator

NSN: 5841-01-326-6141

Price Condition Status
$2,950.00 SV OUTRIGHT 1 IN STOCK
$2,250.00 SV EXCHANGE 1 IN STOCK
066-3114-01
- Color Radar Indicator
Price Condition Status
REQUEST SV OUTRIGHT REQUEST LEAD TIME
REQUEST SV EXCHANGE REQUEST LEAD TIME

Click on a question below to see the answer. If you have a question about this model that is not answered below, please contact questions@seaerospace.com


In relation to NE (New) parts, many OEMs change their prices and availability without any notice to dealers or the industry. Therefore, through the REQUEST or RFQ indication, we ask that customers contact us for the most accurate price and availability.

In relation to SV & OH parts, the used parts aftermarket in the aviation industry is not an infinite supply. It is a dynamic, constantly changing market that is significantly affected by and susceptible to highs and lows in supply and demand. Therefore, although we attempt to, at times, we are unable to predict the exact moment when an item may be available. Once again, through the REQUEST or RFQ indication on our website, we ask that customers contact us for the most current and accurate price and availability.

Many avionics systems require a configuration or setup process. This process is required to interface certain avionics systems to other systems in the aircraft that will be inputting or outputting information to and from these systems. Some examples of systems that require a configuration or setup process include:

Autopilot
EFIS
GPS
EGPWS
EHSI
RADAR
TAWS
TCAS


In addition, most newer technology or solid state systems require configuration via computer interface of some type. A qualified avionics technician should always refer to the appropriate manufacturer's installation manual for complete information and instructions.
"IN FLT6" is an abbreviation for indicator fault code 6. The conditions which cause this code to be displayed have to do with the indicator transmitting ARINC 429 control data to the radar sensor but not receiving ARINC 453 data back from the sensor. A common cause for this error code being displayed is a failed radar sensor or faulty wiring. Although possible, rarely is the problem found to be the radar indicator.

Negotiating the exchange price of a unit only limits the allowable repair cap for the core unit. Southeast Aerospace's exchange transactions are based on the return of economically repairable core unit. Once the core is received and evaluated, the core repair cost incurred by SEA cannot exceed 75% of the original exchange price. That is, it cannot cost SEA more than 75% of the original OH/SV exchange price collected from the customer. Therefore, when and if an SEA exchange price is discounted, there is a risk that additional charges may be assessed once the core is returned and evaluated.