Part #: 011-01057-00

Model: GPS-400W

Garmin - WAAS GPS System
Part Number :


GPS-400W
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 with color moving map
  • Jeppesen database (front-loading data card) contains all airports, VORs, NDBs, intersections, FSS, Approach, SIDs/STARs, and SUA information
  • 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

 

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 info), 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; timers; airspace alarms at 10 minutes, 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)
GPS PERFORMANCE
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:  Position: 15 meters (49 feet) RMS*, 1-5 meters with differential corrections 
  Velocity: 0.1 knot RMS steady state
Dynamics:  Velocity: 999 knots
  Acceleration: 6g's
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 (Gillham/Greycode and serial), Fuel Sensor, Fuel/Air Data 
Map Datums:  124 and 1 user-defined 
PHYSICAL SPECIFICATIONS
Unit Size Width = 6.25"; Height = 2.65"; Depth = 11.00" behind panel, with connectors
Unit Weight 6.6 pounds installed
Display:  Color LCD 
Power:  27.5 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 GPS Description:
011-01057-00 Black
011-01057-10 Gray
011-01057-40 Black, Upgrade of the non-WAAS unit
011-01057-50 Gray, Upgrade of the non-WAAS unit

 

011-01057-40
- Color IFR WAAS GPS (Black, Upg unit)
Price Condition Delivery
$5,250.00 SV OUTRIGHT VIEW STOCK
$1,250.00 SV EXCHANGE VIEW STOCK

SEA Repair Capabilities: Yes

011-01057-00
- Color IFR WAAS GPS (Black, Orig prod)

NSN: 5820-01-645-5152

Price Condition Delivery
$5,250.00 SV OUTRIGHT RFQ
$1,250.00 SV EXCHANGE RFQ

SEA Repair Capabilities: Yes

011-01057-10
- Color IFR WAAS GPS (Gray, Orig prod)
Price Condition Delivery
CALL OR RFQ SV OUTRIGHT RFQ

SEA Repair Capabilities: Yes

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

Citation S550 equipped with: Transponders MST-67A 066-01143-2101. Chance to update to ES?

Garmin GPS400. Chance to update software to WAAS? Or maybe to replace with a GPS400W and link it with transponders? - FMS UNS-1L SCN 803.1. Citation Mustang C510 equipped with G1000 Integrated Flight Deck. It is a 2008 plane.

What can I do to get ADS-B at an affordable price?

A: Since the aircraft are operated in Spain, what region or ADS-B spec do you need to meet? (i.e. USA, DO-260B?)

Without knowing exactly what ADS-B requirement or mandate you might be trying to comply with, I can only provide information relative to what we know here in the USA in reference to ADS-B for Part 25 aircraft.

For the Citation 550, the MST-67A will be superseded by the MST-100B if/when Honeywell can produce and certify the MST-100B. I have attached the only details that we currently have on the MST-100B. Honeywell has not even released pricing on this unit yet, however, ideally it would be an ideal solution ultimately since it is said to be plug and play with the MST-67A. With a WAAS GPS interfaced it would meet all ADS-B mandates. Also, keep in mind, that your CAS-67 can be upgraded fairly easily to Change 7.1 via Honeywell sales bulletin upgrading the TPU-67A processor to the TPU-67B. There is a company that offers some STCs for Part 25 aircraft if your region requires an STC for the 7.1 upgrade - http://www.prostaraviation.com/

If the MST-100B does not pan out for some reason and/or Honeywell keeps delaying its release, then there is a company named Jettech that has released Garmin GTX 3000ES ADS-B capable transponder to its existing STC covering Garmin GTN install on Citation and Citation Jet aircraft equipped with TCAS II. In addition, the company amended its Garmin GTN autopilot coupled LPV FAA STC for the Citation 500 series to include all Primus 1000 equipped Bravo, Ultra, Encore and Excel aircraft. They do not have much information on their website about the ADS-B STC but I recently learned about it at the AEA convention last week - http://jettechllc.net/index.html

Regardless of what direction you might go in, you should most likely get your GPS-400 upgraded to the GPS-400W while Garmin is still offering the upgrade. It is relatively inexpensive at around $3000 USD. Most FANS type systems will require WAAS GPS input or accuracy ultimately. Plus, Garmin's WAAS interface tis very compatible with most ADS-B solutions. Regarding the Citation Mustang C510 equipped with G1000, Garmin is still working on this solution. We assume it will include the GTX-3000 transponder(s) as this aircraft will require a 1090 MHz, (not 978 MHz UAT) system. I would continue to monitor Garmin's website for announcements relating to the G1000.

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.

See this PDF document for a detailed listing of currently available IFR GPS systems and a brief comparison.

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.