Rockwell COLLINS VIR-32 NAVIGATION RECEIVER P/N: 622-6137-001 S/N: 2466


Click here to purchase or contact the seller of this item on eBay

Current Price: 499.00 USD


COLLINS VIR-32 NAVIGATION RECEIVER
P/N: 622-6137-001 S/N: 86001130
TSO-C40b C36d C34d C35d

-Removed To Upgrade Cessna 425 Conquest
- Shown in 1st 4 Photos

VIR-32
FEATURES


    Proline II Navigation Receiver including fully digital VOR/LOC, glideslope, and marker beacon receivers
    Provides serial-digital I/O interface and features digital signal processing for improved performance
    Accepts conventional 2-out-of-5 tuning and provides conventional sine/cosine outputs
    The VIR-32 can be installed as a direct replacement for the VIR-30A (rack & connector remain the same), however you must also install a CTL-32 Control and CAD-31 Adapter.
    Models and modification available for units to meet ICAO Annex 10 which reduces interference by high-power FM broadcast radio stations (see table below)
SPECIFICATIONS
TSO:     (VOR) C40b; (LOC) C36d; (GS) C34d; (MB) C35d     EUROCAE:     (VOR) ED-22A; (LOC) ED-46; (GS) ED-47; (MB) 1/WG7/70
RTCA:     (VOR) DO-153A; (LOC) DO-131A; (GS) DO-132A; (MB) DO-143     Environmental:     DO-160A, categories /A2E1/B/JY/ EXXXXXZ/BZ/AZA; EUROCAE ED-14A
Temperature:     -55 to 70C (operation)     Dimensions:     3.762"W x 3.360"H x 13.969"L
Weight:     4.5 lb.     Altitude:     70000 ft.
Channels:     160 VOR, 40 LOC, and 40 GS     Frequency control:     CSDB serial data or ARINC 2-out-of-5
VOR/LOC Frequency Range:     VOR- 108.00 to 117.95 MHz. LOC- 108.10 to 111.95 MHz     VOR/LOC Channel Spacing:     50 kHz
VOR/LOC Sensitivity:     (aural) 3uV for 10dB; (flag) 2.8uV for flag out-of-view     VOR/LOC Selectivity:     6dB +-15 kHz min; 60dB +-41 kHz max
VOR/LOC Spurious Responses:     At least 70dB below desired response     VOR/LOC Audio Output:     100mW nom into 600 ohm load with 30% modulation, at least 1000Hz
VOR/LOC Analog Output:     OBI sine/cosine; capable of driving three RMI pointers     VOR/LOC OBS Resolver:     Provides HSI course resolver signals. Outputs ac signals on OBS E and F. HSI return ac signals on OBS A and B. OBS G,C, and D connected to internal common
VOR/LOC Deviation:     Output capable of driving one to five loads, 1000 ohm each, without external strapping. Deviation sensitivity in VOR, 150 mV for 10 deg; in LOC, 90 mV for 0.093 DDM. VOR deviation accuracy +-0.75 deg; LOC deviation centering accuracy +-4.0 mV dc. Polarity: VOR, positive deviation for airplane left of course; LOC, positive deviation for 90 Hz > 150 Hz     VOR TO/FROM:     Output capable of driving one to three loads, 200 ohm each. Drive level TO: +80 to +165 mV. Drive level FROM: -80 to -165 mV
VOR/LOC Flag:     (low level) output capable of driving one to five loads, 1000 ohm each. Output 1.0 to 1.9 V dc, current limit 10 mA     VOR/LOC Superflag:     Nominal output +26Vdc, min output 12.0 Vdc at 250 mA with input power at +16 Vdc
VOR/LOC RNAV:     Output is a buffered VOR/LOC detector output adjusted nominally for 0.5 Vrms with standard VOR signal input     GS Frequency Range:     329.15 to 335.00 MHz
GS Channel Spacing:     150 kHz     GS Sensitivity:     5 uV for flag out-of-view
GS Selectivity:     6 dB at +-25.5 kHz min; 60 dB at +-160 kHz max     GS Spurious Response:     -60 dB
GS Deviation Output:     Capable of driving one to five 100ohm loads. 78 mV for 0.091 DDM, max output is +-0.35Vdc. Polarity: positive down for 90 Hz > 150 Hz     GS Flag:     (low level) +1.0 to +1.9 Vdc for flag out-of-view, current limited to 10mA; capable of driving one to five 1000 ohm loads
GS Superflag:     (high level) Nominal output is +26 Vdc, current limited to 250 mA for a valid input signal     MB Frequency:     75.00 MHz
MB Sensitivity:     High sens: 200 uV +-6dB; Low sens: 1500 uV +-6dB     MB Selectivity:     6dB at +-16 kHz min; 60dB at +-170 kHz max
MB Lamp Output:     Capable of driving dual 3-lamp load, 6.3V lamps at 200 mA or less per blub on each bulb     MB Hi/Lo Strap:     Used when parallel control is selected
Part Number    Navigation Receiver Description:
622-6137-001     Standard version, see features above
622-6137-201     Meets ICAO Annex 10

 



CESSNA CONQUEST 425 Avionics Partial List (*Connectors Available):

-GARMIN GPS 500 WATT TAWS PN: 011-01063-40 SN: 86001130

-COLLINS AVIONICS VHF-22A COMM TRANSCEIVER 622-6158-001 S/N: 20067

 *Includes Mount PN: 390R-19 S/N: 622-1195

-COLLINS AVIONICS VIR-32 NAVIGATION RECEIVER PN: 6226137-001 SN:2466

-AERO-MACH LABS VERTICAL GYRO OVH VAC GAGE PN:300-3CFC S/N: 3032

-COLLINS AVIONICS CTL-92 ATC CONTROL DO-160A PN:622-6523-005 SN:582

-COLLINS AVIONICS CTL-22 ACT CONTROL DO-160A PN:622-6520-005 SN:248


 
Question  Would this fit my.....
 Answer:    They're From a Cessna Conquest 425.  DO YOUR RESEARCH, PLEASE.


  
 
-182/210/310/320/340/404/414/425/441 Avionics & More In Our eBay Store
https://www.ebay.com/str/unlimitedoriginals
 

Know your aircraft – As an example, Some Nav Receivers can’t directly interface to an HSI without a converter. Seek Professional advice before you buy any time you are in question. When it comes to aircraft, you are far more important than money you hope to save.

Rockwell COLLINS VIR-32  NAVIGATION RECEIVER P/N: 622-6137-001 S/N: 2466 Rockwell COLLINS VIR-32  NAVIGATION RECEIVER P/N: 622-6137-001 S/N: 2466 Rockwell COLLINS VIR-32  NAVIGATION RECEIVER P/N: 622-6137-001 S/N: 2466
Rockwell COLLINS VIR-32  NAVIGATION RECEIVER P/N: 622-6137-001 S/N: 2466 Rockwell COLLINS VIR-32  NAVIGATION RECEIVER P/N: 622-6137-001 S/N: 2466 Rockwell COLLINS VIR-32  NAVIGATION RECEIVER P/N: 622-6137-001 S/N: 2466


Click here to purchase or contact the seller of this item on eBay