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Picture of product GNS-530AW

Part #: 011-01067-40

Model: GNS-530AW

OEM:

Garmin

Desc:

WAAS GPS/NAV/COM (28v/16w)
Part Number :


 
GNS-530AW

 

FEATURES

  • Complies with WAAS TSO C146a
  • Terrain database for terrain awareness is standard
  • WAAS GPS receiver allows for primary naviagation and vertical guidance for LPV, L/VNAV, and LNAV+V approaches
  • IFR GPS, 16 watt com, VOR, LOC and glideslope with color moving map in one unit
  • TSO'd VHF Comm offers choice of 25 kHz or 8.33 kHz spacing
  • Jeppesen database (front-loading data card) contains all airports, VORs, NDBs, intersections, FSS, Approach, SIDs/STARs, and SUA information
  • 5" color display
  • Offers enhanced situational awareness with relation to cities, highways, railroads, rivers, lakes and coastlines
  • Use of color separates land data, terminal areas, route, and approach information for easy pilot scanning
  • Able to interface with WX-500 stormscope for storm information
  • Interfaces to Ryan 9900B / 9900BX TCAD and Goodrich Skywatch to display traffic information
  • Scheduled to include Terrain Awareness information

 

 
SPECIFICATIONS

Jeppesen Database

Coverage: Americas, International, or Worldwide

Airports: Identifier, city/state, country, facility name, lat/lon, elevation, fuel service, control, approach information

VORs: Identifier, city/state, country, facility name, lat/lon, frequency, co-located DME/TACAN, magnetic variation, weather broadcast indication

NDBs: Identifier, city/state, country, facility name, lat/lon, frequency, weather broadcast indication

Intersections: Identifier, country, lat/lon, nearest VOR

Frequencies: Approach, arrival, control area, departure, Class B, Class C, TMA, TRSA (with sector, altitude, and text usage), ASOS, ATIS, AWOS, center clearance delivery, tower, ground, unicom, pre-taxi, localizer, and ILS

Runways: Designation, length, width, surface, lighting, pilot-controlled lighting frequency

FSS: Identifier, reference VOR, frequency, usage

ARTCC: Identifier, frequency, usage

MSA: Minimum safe altitude along and in proximity to active flight plan

Approaches: Non-precision and precision approaches throughout the database coverage

SIDs/STARs: Contains all pilot/nav SIDs/STARs

Airspaces: Class B & C with sectors, International CTA & TMA with sectors, all SUAs, including MOAs, prohibited and restricted areas with controlling agency and airport

Safety Features

Emergency Search: 9 nearest airports, VORs, NDBs, intersections, or user waypoints; 2 nearest FSS and ARTCC frequencies

Alarms: Arrival and CDI, timers, SUAs less than 10 min, 2NM and inside SUA

User Customization

Waypoints: 1,000 User Defined

Flight Plans: 20 reversible routes of up to 31 waypoints each

Certification:

GPS: TSO C129a, Class A1 (en route, terminal, and approach)

VOR: TSO C40c

LOC: TSO C36e

GS: TSO C34e

VHF COM: TSO C37d, Class 4 and 6 (transmit) and TSO C38d, Class C and E (receiver)

GPS Performance:

Position: 15 meters (49 feet) RMS*, 1-5 meters with differential corrections

Velocity: 0.1 knot RMS steady state

Velocity: 999 knots

Acceleration: 6g's

Receiver: twelve parallel channel receiver simultaneously tracks and uses up to 12 satellites

Acquisition Time: 12 seconds (warm), 45 seconds (cold)

Update Rate: Once per second, continuous

Accuracy:

Dynamics:

Nav Features: Pilot-defined Course Selection and Waypoint Hold, Closest Point of Approach, Departure and Arrival Frequencies, Approach Navigation using published approach procedures stored on NavData card, Terminal Navigation using SIDs/STARs from NavData card

Planning Features: True Airspeed, Density Altitude, Winds Aloft, RAIM Availability, Sunrise/Sunset Times, Trip and Fuel Planning, Vertical Navigation (VNAV)

Interfaces: ARINC 429, Aviation RS-232, CDI/HSI, RMI (digital: clock/data); Superflag Out, Altitude (serial: Icarus, Shadin-Rosetta, encoded Gillham/Greycode), Fuel Sensor, Fuel/Air Data

Map Datums: 124 and 1 user-defined

VOR Performance

Frequency Range: 108.00 MHz to 117.95 MHz

VOR/LOC Composite: 0.50Vrms/0.35Vrms

CDI Output: plus or minus 150mV Full Scale

Centering Accuracy: plus or minus 2.0 degrees

Flag Sensitivity: -103.5 dBm

DME Channeling: 2x5 available, Slip Code, BCD, King Serial

Audio Sensitivity: -103.5 dBm for 6 dB S/N with 1 kHz 30% mod.

Audio Output: 100 mW (minimum) into 500 ohm load; External amplifier required

GS Performance

Frequency Range: 329.15 MHz to 335.00 MHz

CDI Output: plus or minus 150mV Full Scale

Centering Accuracy: 0 ddm plus or minus .0091 ddm

LOC Performance

Frequency Range: 108.10 MHz to 111.95 MHz

CDI Output: plus or minus 150mV Full Scale

Accuracy

Flag Sensitivity: -103.5 dBm

Audio Sensitivity: -103.5 dBm for 6 dB S/N with 1 kHz 30% mod.

Audio Output: 100 mW (minimum) into 500 ohm load; External speaker amplifier required

VHF COM Performance

Frequency Display: Upper-left corner of active matrix LCD, 2-lines with active frequency above standby

Channels: 760 (25 kHz spacing); configuration for 3040 channels (8.33 kHz spacing) also provided

Frequency Range: 118.000 MHz to 136.975 MHz

Transmit Power: 16 watts (minimum)

Modulation: 70% (minimum)

Receive Sensitivity: 2.0 microvolts (hard) for 6 dB S/N with 1 kHz 30% mod.

Squelch Sensitivity: 2.0 microvolts (hard) typical

Audio Output: 100 mW (minimum) into a 500 ohm load; External speaker amplifier required

Certifications:

GPS: TSO C129a A1

VOR: TSO C40c

LOC: TSO C36e

GS: TSO C34e

VHF COM: TSO C37d, Class 4 and 6 (transmit) and TSO C38d, Class C and E (receive)

Physical Specifications

Unit Size: Width = 6.25"; Height = 4.30"; Depth = 11.00" behind panel, with connectors

Unit Weight: 7.0 pounds installed

Display: Color LCD

Power: 14/28 VDC

Data Storage: Separate internal battery protects stored data for up to five years

Environmental

Temperature: -20°C to +55°C (operating range); -20°C to +70°C (short-term operation)

Humidity: 95% non-condensing

Altitude Range: -1,500 ft to 50,000 ft

Part Number: Description:
010-00418-01 Black, Original catalog PN
010-00418-11 Gray, Original catalog PN
010-00419-01 TAWS, Black, Original catalog PN
010-00419-11 TAWS, Gray, Original catalog PN
   
011-01066-00 Black, 28 Volt
011-01066-10 Gray, 28 Volt
011-01066-40 Black, 28 Volt, Upgrade from non-WAAS unit
011-01066-50 Gray, 28 Volt, Upgrade from non-WAAS unit
011-01067-00 Black, 28 Volt, w/ TAWS
011-01067-10 Gray, 28 Volt, w/ TAWS
011-01067-40 Black, 28 Volt, w/ TAWS, Upgrade from non-WAAS unit
011-01067-50

Gray 28 Volt, w/ TAWS, Upgrade from non-WAAS unit

 

Serial # 85600143
Condition SVC
Mods None
Tag Date 05/31/24
Shop Southeast Aerospace Inc.
Warranty 6 Months
011-01067-00
- WAAS GPS/Nav/Comm w/TAWS
Price Condition Status
$5,750.00 SV EXCHANGE 1 IN STOCK
$11,750.00 SV OUTRIGHT 1 IN STOCK
011-01067-40
- WAAS GPS/Nav/Comm w/TAWS
Price Condition Status
$12,250.00 SV OUTRIGHT 1 IN STOCK
$5,750.00 SV EXCHANGE 1 IN STOCK
011-01067-10
- WAAS GPS//Nav/Comm w/TAWS
Price Condition Status
REQUEST 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.

The 400/500W units with WAAS capability offer many new features and enhancements over the classic models. Some enhancements include WAAS enable GPS antenna, receiver, and software. The 400W/500W series units comply with WAAS TSO C146a and include hardware upgrades with a faster micro-processor. A terrain database for terrain awareness is included a standard feature. Most importantly, the WAAS GPS receiver allows pilots to use the GNS-400W/500W units for primary navigation and vertical guidance for LPV, L/VNAV, and LNAV+V approaches.

For a complete summary of the feature changes and enhancements, click Here.
In short, WAAS approach-capable GPS units provide lateral and vertical guidance to many airports that have never had a precision approach. As of Feb. 2007, there are 640 GPS-based LPV approaches with minimums as low as 200 feet and 1/2 mile visibility. There are also over 1000 LNAV/VNAV approaches that provide vertical guidance with WAAS capable GPS units. There are also 1000s of other approaches with advisory vertical guidance. More and more approaches are being added each month.
Yes, but please note the following considerations.

For the S-Tec System 20 or 40, these systems are roll axis only. However, if equipped with a GPSS converter, these systems will follow the lateral steering commands from the GPS for a WAAS approach. Vertical guidance is pilot controlled.

For the S-Tec System 30 or 50, these systems are roll axis and altitude hold only. However, with a GPSS converter, these systems will follow the lateral steering commands from the GPS for a WAAS approach. Vertical guidance is pilot controlled.

For the Systems 55, 55X, 60-2, 60PSS, or 65, these systems will track the lateral deviation from the GPS navigator in the Approach (APR) mode and the vertical deviation in the Glideslope (GS) mode. If you are using a 55X or other autopilot systems equipped with a GPSS converter, they will not couple to a WAAS approach in GPSS mode. To follow both the vertical and horizontal deviations of a WAAS approach, the autopilot must be in Approach (APR) mode and Glideslope (GS) mode. The 60PSS system is pitch axis only and will follow the vertical deviation in Glideslope (GS) mode.
Under certain conditions, the Garmin 400W/500W series units will not provide serial heading information to the L3 WX-500 Stormscope. Even if the WX-500 unit is wired for synchro heading, there may be issues with the WX-500, GDL-69 datalink, and crossfill between two Garmin units. Also, some issues have been encountered with the COM flip/flop key not switching between the active and standby frequencies. As of 8/20/07, Garmin plans to resolve these issue with the next software release. The software upgrade should be able to be completed at your local Garmin authorized facility.
At this time, the Garmin 400W/500W series WAAS units are approved for interface to the following EFIS systems:

Honeywell EFIS 40/50 with the SG 465 symbol generator with the following limitation: No vertical guidance is provided for GPS approaches.

Sandel SN3308 with the following limitation: GPS lateral and vertical guidance is provided using the analog interface.

Sandel SN3500 with the following limitation: Vertical guidance is provided for GPS approaches.

This is specified in the latest Garmin 400W series installation manual P/N 190-00356-02 Rev. C, dated April 2007.

For handheld GPS receivers, database updates can be ordered and downloaded directly through Garmin's Internet site.

For panel mount GPS receivers, all database cards and computer downloads (if applicable) must be ordered through Jeppesen. Contact Jeppesen at www.jeppesen.com for more information.

The Garmin GNS400/500 series units require setup and configuration before proper function and use. The system does not utilize a configuration module to allow easy removal and replacement of units while retaining the programmed configuration information. Therefore, if you are exchanging units in an aircraft, then you must have record of the configuration parameters to reprogram into the replacement unit.
There is some confusion in the avionics industry relating to the various terms used for terrain awareness, terrain advisory, and terrain alerting systems. Not all terrain systems are certified to Class A or B TAWS standards specified in FAA TSO C147b. If a terrain system is certified and approved to FAA TAWS standards, then the manufacturer will specifically use the term "TAWS" and/or "Class A/B TAWS". In most if not all cases, the term "terrain advisory" should not be understood to indicate "TAWS" or imply the product meets TSO C147b.
Newly Overhauled parts obtained from Garmin are designated with an N in their part number. This usually follows the 010- in the part number. As with most Garmin 010 part numbers, the N part numbers are for ordering purposes only and do not actually appear on the dataplate of the unit.
No, Garmin does not offer an upgrade to incorporate the 16 watt comm. (i.e. "A" version) into the GNS-430/530 and GNS-430W/530W units.