Part #:

Model: AIS-450

Shadin - ARINC 429Hdg, Pitch, Roll to 3 ARINC 407
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AIS-450
 
DESCRIPTION
  • The AIS-450 is a digital to synchro based converter that receives angular data (Heading, Pitch, and Roll) on two ARINC 429 inputs and converts it to three ARINC 407 synchro outputs (3-wire)
  • Two ARINC 429 high speed (H/S) inputs and accept only angular ARINC 429 labels for Heading, Pitch, and Roll (ARINC Labels 314, 320, 324, and 325)
  • The ARINC 429 outputs are high speed (H/S) and pass through only the valid angular
  • ARINC 429 labels received on the inputs. The AIS-450 has three ARINC 407 outputs that are configured as 3-wire synchro.
  • The first output is mapped to the True or Magnetic Heading ARINC 429 label (314 or 320) depending on the state of the Heading Select Discrete Input
  • A High/Open state maps the output to Magnetic
  • Heading and a Low/Ground state maps the output to True Heading
  • The second output is mapped to the Pitch ARINC 429 label (324)
  • The third output is mapped to the Roll ARINC label (325)
  • The Synchro Validity Discrete Outputs indicate whether each of the ARINC 407 outputs is valid
  • The ARINC 429 Input 1 takespriority over the ARINC 429 Input 2
  • Valid Pitch and Roll labels must be received on the same ARINC Input to enable the Pitch and Roll Validity Discrete Outputs
  • Digital I/O
  • 3 Channel ARINC 407 3 wire synchro out
  • Discrete I/O
  • ARINC 429 label 314 or 320 to synchro heading output
  • ARINC 429 labels 314 or 320, 324, and 325 to synchro heading, pitch and roll output
  • ARINC 429 to ADF, DME synchro
  • ARINC 429 or serial to selected course waypoint bearing
  • Serial to synchr

 

 

 

SPECIFICATIONS

 DIMESIONS: 8.5”L x 4.0”W x 2.5”H WEIGHT: (P/N 834510-00) 1.7 lbs, (P/N 834511-00) 1.42 lbs
power supply voltage: +18VDC to 33VDC operating temperature:  -40°C to +70°C
supply current: 520 mA Max (745 mA Max including external loads) storage temperature: -55 C to +85 C
inputs: (P/N 834511-00) ARINC 429 High Speed, 100 Kbps ± 1%, 26 VAC Reference CH1 and CH3 24.7 VAC to 27.3 VAC1, Discrete Input (ARINC 763-3) Active: Low / Ground Signal V < 3.5 VDC with I < 20 mA sink or R < 10 Ω Inactive: High / Open Signal 18.5 VDC < V < 36.0 VDC or R > 100 K Ω

outputs:

(P/N 834511-00) ARINC 429 High Speed, 100 Kbps ± 1%, Synchro-X, Y, and Z (ARINC 407) 0 to 11.8 VAC Typical, 12.4 VAC Max 0.209 VA into 500 Ω each channel, Synchro Angle Accuracy Input Angle ± 0.5°,  Synchro-Valid-CH1 +28VDC(Valid) / Open(Invalid) Discrete, 75mA Max Short Circuit Protected, 1. Input Voltage in excess of 27.3 VAC may result in Synchro output voltage greater than 12.5 VAC 

environment: RTCA/DO-160F Categories: F1-BAB[R(B, B1)]XXXXXXZ[AXX]AR[CC][WW]M[XXXXX]XXAX in-flight loss of cooling: Equipment can run indefinitely with no cooling
certification: (P/N 834511-00) TSO-C5f, TSO-C6e “Incomplete System”, (P/N 834510-00) TSO-C4c, TSO-C5f, TSO-C6e “Incomplete System” mounting locations: 8.00”L x 2.00”W
Mounting: Screw size #8 operating altitude: Up to 55,000ft
protection: Active current limiting to 2.0 Amps outputs: (P/N 834510-00) ARINC 429 High Speed, 100 Kbps 1%, Synchro-X, Y, and Z (ARINC 407) 0 to 11.8 VAC Typical, 12.4 VAC Max (Heading, Pitch and Roll) 0.209 VA into 500 Ω each channel, Synchro Angle Accuracy Input Angle ± 0.5° Synchro-Valid-CH1, CH2, and CH3 +28VDC(Valid) / Open(Invalid) Discrete, 75mA Max Short Circuit Protected, Or Alternate 2-wire Synchro (ARINC 561) 200mV/Deg (Pitch and Roll), 1. Input Voltage in excess of 27.3 VAC may result in Synchro output voltage greater than 12.5 VAC
inputs: (P/N 834510-00) ARINC 429 High Speed, 100 Kbps 1%, 26 VAC Reference CH1 and CH3 24.7 VAC to 27.3 VAC1, Discrete Input (ARINC 763-3) Active: Low / Ground Signal V < 3.5 VDC with I < 20 mA sink or R < 10 Ω Inactive: High / Open Signal 18.5 VDC < V < 36.0 VDC or R > 100 K Ω MTBF (Mean Time Between Failures): 24,000 hours [Airborne Inhabited Cargo (AIC), 30°C], The reliability predictions were performed using the general methodology of MIL-HDBK-217F. The component failure rate calculation models presented in MIL-HDBK-217F were used as a guide to determine each component’s initially assigned predicted failure rate
Part Number: Description:                  
834510-00 AIS-450  ARINC 429Hdg, Roll to 3 ARINC 407
834511-00 AIS-450  ARINC 429Hdg, Roll to 3 ARINC 407

 

 

834510-00
- Synchro Converter
Price Condition Status
REQUEST NEW OUTRIGHT REQUEST
834511-00
- Heading Synchro Output
Price Condition Status
REQUEST NEW OUTRIGHT REQUEST