Part #: MI-585200-1

Model: RT-4001

NSN:

5826-01-361-2022

OEM:

Honeywell

Desc:

Radar Transceiver

Part Number :


 
RT-4001
FEATURES
  • Radar receiver/transmitter used in Primus 400 and Primus 400SL Radar Systems
  • Housed in short 1/2-ATR case
  • 10kw peak nominal power output

 

SPECIFICATIONS

Dimensions: 5.01"W x 7.615"H x 15.5"D Weight: 16.2
TSO: Category D2AJXXXXXXCBBBB Operating Frequency: X-Band, 9345 +-30 MHz
Part Number: Description:
MI-585200 Can be used with either 12" or 18" antenna array (must request 18" interface when ordering), Radar Transceiver
MI-585200-01 Can be used with 18" antenna array ONLY, Radar Transceiver

 

MI-585200
- Radar Transceiver

NSN: 5826-01-361-2022

Price Condition Status
REQUEST OH OUTRIGHT REQUEST LEAD TIME
MI-585200-1
- Radar R/T
Price Condition Status
REQUEST SV OUTRIGHT 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.

Weather radar transceivers use a magnetron which is basically a cathode emission device. The magnetron is subject to deteriorization due to aging. Therefore, it is recommended to perform some type of periodic maintenance to detect and correct the effects of aging. This reduces the chance of an in-service failure.

An annual, routine test of the following parameters should made:

- Power output
- Transmitter frequency
- AFC voltage
- Sensitivity (MDS)

Ideally, the test should take place between December and March prior to the peak thunderstorm season.
Radar stabilization uses an aircraft's vertical gyro (if equipped) to maintain the selected radar antenna beam relative to the horizon. Therefore, while in a turn, the radar will maintain the selected tilt angle instead of changing in relation to turn.
As of January 2010, the only Multi Function Displays that are compatible with the Primus 300 or Primus 400 radar systems are the Honeywell MFRD and the Universal MFD-640. For pricing and additional information on these MFDs, please submit an RFQ to SEA today.

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.