360 degree product image of VIR-30A
360
360 image holder for VIR-30A
360 degree product image thumbnail of VIR-30A
360
Thumbnail product image of VIR-30A

Part #:

Model: VIR-30A

OEM:

Collins Aerospace

Desc:

Nav Receiver
Part Number :


VIR-30A
FEATURES
  • Radio Navigation System providing VOR, localizer, glideslope, and marker beacon outputs and VOR/ADF display for general aviation aircraft
  • Has 200 VOR/LOC channels and 40 glideslope channels
  • Compatible with standard 2-out-of-5 control units
  • Provides navigation outputs to interface with pictorial navigation systems, analog area navigation systems, and conventional flight control systems
  • Supplies automatic/manual VOR information
  • Supplies localizer and glideslope deviation outputs
  • Supplies high and low level flag signals, to/from information, marker beacon lamp signals, and VOR, localizer, and marker beacon audio outputs
  • Provides sine/cosine VOR outputs to drive RMI-30
  • Can be used with either 313N-4 series analog controls or CTL-30 and CTL-32 (w/ CAD adapter) digital controls
  • Can be used with 3-wire synchro type RMI with use of 699Z-1 RMI adapter
  • Models available with rotor modification for operation in helicopters (see table below)
  • Models available with different combinations of included or excluded glideslope receiver or marker beacon receiver (see table below)
  • Model available with modification to meet ICAO Annex 10 for reduction of FM interference by high-power FM broadcast radio stations (see table below)
  • Can be directly replaced by the VIR-32 (rack & connector remain the same), however you must also install a CTL-32 Control and CAD-31 Adapter when replacing the VIR-30A.
SPECIFICATIONS
FAA TSO: C40a (VOR), C36c Class D (LOC), C34c Class D (GS), C35d Class A (MB) Environmental: DO-138, Category AD/A/JNG/AAAEXXXXX
Dimensions: 3.49"H x 3.73"W x 13.84"L Weight: 5.6 lbs.
Altitude: 45000 ft. max. Temperature: -54 to +55C (operation)
Frequency Range: 108.00-117.95 MHz with 50-kHz spacing Frequency Control: ARINC 2 out of 5
Selectivity: 6 dB: 34-kHz minimum bandwidth; 60 dB: 82-kHz maximum bandwidth VOR Channels: 160
LOC Channels: 40 Flag Sensitivity: Flag out of view at 3.0 uV
VOR Deviation Accuracy: +-1.0 deg. Deviation Loads: 5-load capability, 1000 ohms each without external strapping
Maximum Deviation Voltage: VOR (1V), LOC (500mV) To/From Loads: 2-load capability, 200 ohms each
Max To/From Voltage: 130 mV High-level Flag: 18 V dc minimum at 250 mA
Low-Level Flags: 1.2V dc, current limited to mA; four loads, 1000 ohms each without external strapping RMI Output: 4-wire sine/cosine; compatible with Collins RMI-30 or 699Z-1 RMI Adapter, capable of driving 3 RMI pointers
RMI Output Accuracy: +-1.5 degrees bench, +-2.7 degrees environmental Audio Output: 100 mW +-1 dB, 600 ohms
Glideslope Frequency Range: 329.15-335.000 MHz Glideslope Channels: 40 with 150-kHz spacing
Glideslope Frequency Control: ARINC 2 out of 5 Glideslope Selectivity: 6 dB: 41-kHz minimum bandwidth; 60 dB: 188-kHz maximum bandwidth
Glideslope Sensitivity: Flag out of view at 5 uV Glideslope Deviation Loads: 5-load capability, 1000 ohms each without external strapping
Glideslope Max Deviation Voltage: +-900 mV in ILS mode Glideslope Flag: Biased out of view in VOR mode with approx +1.0 V
Glideslope High-level Flag: +18 V dc minimum at 250 mA Glideslope Low-level Flags: 1.2 V dc, current limited at 10 mA; four loads, 1000 ohms with each without external strapping
Marker Beacon Frequency: 75 MHz Marker Beacon Sensitivity: (High) 200 uV +-6 dB; (Low) 1500 uV +-6 dB
Marker Beacon Audio Output: 100 mW into 600 ohms at 2000-uV input level (high sensitivity) Marker Beacon Load Capacity: Dual 3-lamp load
Part NumberNavigation Receiver Description:
622-0876-001 VOR/LOC/Glideslope/Marker Beacon Receivers
622-0876-002 VOR/LOC/Glideslope Receivers
622-0876-003 VOR/LOC/Marker Beacon Receivers
622-0876-004 VOR/LOC Receiver ONLY
622-0876-011 VOR/LOC/Glideslope/MB Receivers with rotor mod. for helicopter use
622-0876-012 VOR/LOC/Glideslope Receivers with rotor mod. for helicopter use
622-0876-013 VOR/LOC/MB Receivers with rotor mod. for helicopter use
622-0876-014 VOR/LOC Receiver ONLY with rotor mod. for helicopter use
622-0876-201 VOR/LOC/Glideslope/Marker Beacon Receivers with FM immunity mod.
622-0876-202 VOR/LOC/Glideslope Receivers with FM immunity mod.
622-0876-203 VOR/LOC/Marker Beacon Receivers with FM immunity mod.
622-0876-204 VOR/LOC Receiver ONLY with FM immunity mod.
622-0876-211 VOR/LOC/Glideslope/MB Receivers with rotor mod. for helicopter use and FM immunity mod.
622-0876-212 VOR/LOC/Glideslope Receivers with rotor mod. for helicopter use and FM immunity mod.
622-0876-213 VOR/LOC/MB Receivers with rotor mod. for helicopter use and FM immunity mod.
622-0876-214 VOR/LOC Receiver ONLY with rotor mod. for helicopter use and FM immunity mod.


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

 

622-0876-002
- Nav Receiver

NSN: 5895-01-162-9391

Price Condition Status
$300.00 SV OUTRIGHT 2 IN STOCK
622-0876-001
- Nav Receiver

NSN: 5895-01-014-1704

Price Condition Status
REQUEST SV OUTRIGHT REQUEST LEAD TIME
622-0876-004
- Nav Receiver

NSN: 5826-01-359-9930

Price Condition Status
$285.00 OH OUTRIGHT REQUEST LEAD TIME
622-0876-011
- Nav Receiver

NSN: 5826-01-309-9786

Price Condition Status
$375.00 OH OUTRIGHT REQUEST LEAD TIME
622-0876-201
- Navigation Receiver
Price Condition Status
$495.00 OH OUTRIGHT REQUEST LEAD TIME
622-0876-202
- Nav Receiver
Price Condition Status
REQUEST OH OUTRIGHT REQUEST LEAD TIME
REQUEST OH EXCHANGE REQUEST LEAD TIME
622-0876-211
- Nav Receiver
Price Condition Status
$750.00 OH 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.

The -011 versions incorporate a rotor modulation modification on the VOR instrumentation circuit card This modification includes an RC filter at the outputs of the sine/cosine DC signals that smooths these outputs to minimize the effects of interference by rotor action of a helicopter.
No, although the -01X versions incorporate a rotor modulation filter on the VOR instrumentation card for helicopter applications, the pin designation for the 27.5 DC Bus is different for the two versions. On the -01X versions, the 27.5 DC is assigned to Pin P1-41. On the -00X versions, the 27.5 DC is assigned to Pin P1-18.

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.

Collins Proline I began production in the early to mid 1970s and was very common in many business aircraft in the 1970s and early 1980s. The original instruction manuals for most of the units is dated in 1974. Although production of the Proline continued through the 1980s, it can be assumed that a Proline I unit is 20-30 years old on average.
Most of the Collins Proline I components were originally manufactured in the early 1970s. Collins has continued to produce some of the Proline I components by special order over the past 30 years however large scale production stopped many years ago. Most of the Collins Proline I product lines incorporates 1960s and 70s analog technology. Collins has superseded the Proline I product line several times with the Proline II, Proline IV, and Proline 21 lines. As a result, some service parts needed to maintain and repair original Collins Proline I components are no longer available. Therefore, you may experience limited to no warranty available and unreliability for many of the Proline I units.

Southeast Aerospace offers many affordable, upgradeable options that are available for aircraft with Collins Proline I. As avionics integration specialists and premiere Collins dealer, Southeast Aerospace is experienced and knowledgeable on all Collins Proline generations.

If you are interested in upgrading any of your original Collins Proline I systems, please contact us for the most reasonable, optimal choice available.