360 degree product image of IN-182A
360
360 image holder for IN-182A
360 degree product image thumbnail of IN-182A
360
Thumbnail product image of IN-182A

Part #:

Model: IN-182A

OEM:

BendixKing

Desc:

Color Radar Indicator
Part Number :


IN-182A
FEATURES
  • Five color radar indicator used with RDS-82 and RDR-2000 radar systems
  • Solid-state
  • Display Range/Range Marks of 10/2.5, 20/5, 40/10, 80/20, 160/40 and 240/60
  • EFIS compatible
  • ARINC 453 bus, ARINC 708 data word weather data inputs
  • ARINC 429 control data outputs
  • Self test capability
  • 5,14, or 28 Volt panel lighting
  • Models available with or without vertical profile capability (see table below)
  • Models available with black or gray bezel (see table below)
  • Models available with graphics compatibility for display of navigation information (see table below)

 

SPECIFICATIONS

Modes: STBY,WX,WXA,MAP,VP and TEST Range Scales: 10,20,40,80,160 and 240 NM
Altitude: 25000 ft. unpressurized Temperature: -55 to 70C
Dimensions: 6.4"W x 4.11"H x 8.9"L Weight: 8.9 lbs.
TSO: C63b Class 7 Env. Categories: DO-160A; A1B1/A/PKS/XXXXXXABABA
Part Number: Description:
066-3084-00 black bezel, non-vertical profile
066-3084-01 gray bezel, non-vertical profile
066-3084-02 black bezel, non-vertical profile, graphics compatible
066-3084-03 gray bezel, non-vertical profile, graphics compatible
066-3084-10 unique version, only works w/RS-181A, P/N 071-1315-10
066-3084-30 black bezel, vertical profile
066-3084-31 gray bezel, vertical profile
066-3084-32 black bezel, vertical profile, graphics compatible
066-3084-33 gray bezel, vertical profile, graphics compatible



PLEASE NOTE: THE ABOVE LISTED PART NUMBERS REFLECT THE DIFFERENT UNITS ORIGINALLY AVAILABLE BY THE MANUFACTURER AND DO NOT NECESSARILY INDICATE OR REFLECT THE CURRENT AVAILBILITY OF THESE DIFFERENT UNITS BY SOUTHEAST AEROSPACE OR THE AFTERMARKET

 

 

066-3084-32
- Radar Indicator
Price Condition Status
$3,295.00 SV OUTRIGHT 1 IN STOCK
$1,995.00 SV EXCHANGE 1 IN STOCK
066-3084-01
- Radar Indicator
Price Condition Status
REQUEST OH OUTRIGHT REQUEST LEAD TIME
066-3084-30
- Radar Indicator
Price Condition Status
REQUEST SV OUTRIGHT REQUEST LEAD TIME
066-3084-31
- Radar Indicator
Price Condition Status
REQUEST SV OUTRIGHT REQUEST LEAD TIME
066-3084-33
- Radar Indicator
Price Condition Status
$2,975.00 SV OUTRIGHT REQUEST LEAD TIME
$1,750.00 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.

The IN-182A radar indicator has been replaced with the KMD-850 Multi-Function Display (MFD) in their Hazard Awareness product line. The KMD-850 consists of the KMD-540 display with KAC-501 radar interface module internally installed. The KMD-850 is compatible with most RS-181A, RS-811A, and ART-2000 radar sensors. Along with weather radar display, the KMD-850 provides other features such as:

Moving map (w/ GPS input)
Traffic display (with KAC-504 installed and compatible traffic system)
Terrain display (with KAC-502 installed and compatible TAWS system)
Datalink weather (with KAC-503 installed and KDR-610 interface)

"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.

Although, both the IN-182A P/N 066-3084-32 and IN-182A P/N 066-3084-00 or 3614078-8201 all use the same connector, it is not recommended to interchange these indicators. The IN-182A P/N 066-3084-32 and -33 have a selection for VP mode. This mode provides a vertical scan of weather. The sensor compatible (RS-181A) with the IN-182A must have VP capability as well. If a VP (-32/33) IN-182A is used with a non-VP (-00) RS-181A, then theoretically you will have a button on the radar indicator that does not perform as expected. This could be confusing to the pilot. In addition, using a VP indicator with non-VP sensor is not a true RDS-82 system of any type thus possibly creating certification issues.

IN FLT 1.....Indicates CPU ALU internal test failure on the logic module.
IN FLT 2.....Indicates failure in the program PROM on the logic module.
IN FLT 3.....Indicates failure in the microprocessor internal RAM on the logic module.
IN FLT 4.....Indicates failure in the shared RAM on the interface module.
IN FLT 5.....Indicates a failure in the analog-to-digital converter circuit, on the logic module, used to convert front panel control values to digital values.
IN FLT 6.....Indicates that one of the two interrupts to the microprocessor (60 Hz weather or 453 label) has failed or does not exist.