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Garmin

Garmin GNS 530W

Name: Garmin GNS 530W
Brand: Garmin
SKU: 011-01064-00-RPO
Price: 90748.79 CZK
Availability: InStock

Garmin GNS 530W is a GPS/NAV/COM navigator with a 5-inch display, SBAS GPS to TSO-C146a for LPV approaches, 8.33/25 kHz VHF COM and VOR/LOC/GS; the GNS 530AW is the 28 V version with a 16 W COM. Offered serviceable/overhauled or as a repair.

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P/N011-01064-00

011-01064-00 011-01064-40 011-01064-45 011-01066-00

Condition

Repair (RPO)P/N 011-01064-00-RPO Serviceable / OverhauledP/N 011-01064-00-SV

Your selection: P/N: 011-01064-00 · Condition: Repair (RPO)

Ships in 1 week Ordered from supplier before dispatch

90.748,79 CZK incl. VAT

74.999,00 Kč excl. VAT

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Garmin GNS 530W is a panel-mounted GPS/NAV/COM navigator with a 5-inch color display (320 × 234 pixels) in a 6.25 × 4.58 in bezel. It combines a 15-channel SBAS GPS to TSO-C146a for IFR en route, terminal and approach operations including LPV, a VHF COM with 25 kHz and 8.33 kHz channel spacing, and VOR, localizer and glideslope receivers. Navigation and terrain databases load from two front data cards.

The GNS 530W transmits at least 10 W; the GNS 530AW is the 28 V model with a 16 W COM transmitter. ARINC 429 and RS-232 interfaces connect autopilots, CDI/HSI indicators, EFIS, air data and AHRS. The main connector accepts 10–33.2 V DC. Garmin lists 011-01064-00 (GNS 530W, black bezel), 011-01064-40 (GNS 530W, WAAS upgrade of a non-WAAS unit), 011-01064-45 (GNS 530W, 28 V DC upgrade unit) and 011-01066-00 (GNS 530AW, black bezel).

Serviceable/overhauled units are offered as GNS 530W 011-01064-00 and 011-01064-45; repair covers 011-01064-00, 011-01064-40 and GNS 530AW 011-01066-00. EASA accepts the GPS, COM and NAV functions of GNS units under CS-STAN without an autopilot connection. An installation beyond these limits needs an approved modification, such as an EASA STC, and a Certificate of Release to Service; the US AML STC SA01933LA is not EASA approval. Fit depends on the P/N and aircraft type; a repair quote needs the P/N and S/N.

Technical specifications

Part number	011-01064-00 / 011-01064-40 / 011-01064-45 / 011-01066-00	Supply voltage	10–33.2 V DC
Manufacturer	Garmin	Mounting	6.25″ avionics stack
Display	5" (320 × 234)	Dimensions	159 × 116 × 279 mm
Approach capability	LPV	Weight	3.18 kg
GPS receiver	Yes	Operating temperature	−20 … +55 °C
VOR / ILS	Yes	TSO / ETSO	TSO-C146a / C37d / C38d / C40c / C36e / C34e / C113; ETSO-C146 / 2C37e / 2C38e / 2C40c / 2C36f / 2C34f / C113
Channel spacing	8.33 / 25 kHz	Interfaces	ARINC 429 / RS-232
COM output	10 W (530W) / 16 W (530AW)	STC	SA01933LA (FAA AML)
Frequency range	118.000–136.990 MHz

Advanced Exchange ships a serviceable unit before the core is returned. Future Exchange begins after receipt and evaluation of the core and does not require a deposit. Repair retains the original serial number and starts with inspection and quotation.

Advanced Exchange

What happens: You receive a serviceable unit first. Your core goes back afterward.
Pay now: Full SV price plus core deposit.
Core: Return within 15 calendar days. Repairable (not BER) — deposit refunded. Missing or BER — deposit stays.
Time: Typically 2–3 weeks. Warranty 3 months. Released on EASA Form 1 or FAA 8130-3.

Future Exchange

What happens: You send the core first. After we confirm it is repairable, we ship the serviceable replacement.
Pay now: Net exchange price only. No deposit.
Core: Must be repairable (not BER). Same or superseded P/N, data plate on.
Time: Typically 3–4 weeks. Warranty 3 months. Released on EASA Form 1 or FAA 8130-3.

Repair

Serial: Yours stays. No swap unit — that is Exchange.
Shop: We inspect, quote, then repair. Accept the repair quote and the evaluation fee already paid is deducted. Decline or BER — unit returns as-is; evaluation fee stays.
Time: Typically 2–6 weeks after you approve the quote, parts depending. Warranty 3 months. Released on EASA Form 1 or FAA 8130-3.

Return the core in equivalent packaging, with removal data and a non-incident statement where you have them. Late, incomplete, or rejected-core terms are on the quote.

500W Series Pilot's Guide & Reference Pilot's guide · Rev. K · EN · 8.0 MB Open PDF

Manufacturer documents, provided for reference. Before installation or operation, make sure you have the current revision.

What transponder and other components are needed to upgrade to a Garmin GNS 530W and make the aircraft ADS-B In/Out compliant?

The existing nav/com can be upgraded to a used GNS 530W or to the newer GTN 750.

If you already have a Garmin transponder, for example a GTX 330, the following applies:

Get the ES upgrade and interface it to the GNS 530W or GTN 750.
Allow for a few other minor installation considerations.
Have the shop complete the appropriate paperwork based on Garmin's AML STC.

Which indicators are compatible with the Garmin GNS 430 and GNS 530 series?

According to the Installation Manual, the following indicators are compatible with the main switchable VOR/ILS/GPS indicator output (connector P4001) of the Garmin GNS 430 and GNS 530 GPS/Nav/Comms:

Garmin GI-102 (no longer available), GI-102A, GI-106 (no longer available), GI-106A; S-Tec ST-180 HSI; King KI-202, KI-206, KI-208A, KI-209A, KI-525A, KPI-552, KPI-552B, KPI-553, KPI-553A, KPI-553B
Collins 331A-3G HSI, 331A-9G HSI, 331A-6P HSI; Bendix IN-831A; Century NSD-360, NSD-360A, NSD-1000 HSI; Sperry/Honeywell RD-550A, 650 HSI

The following indicators are compatible as well, but are not mentioned in the installation manual: King KNI-520, Collins/S-Tec IND-350, IND-350A, IND-351, IND-351A, 331H-3G. A non-converter type indicator is required for the VOR/ILS/GPS indicator interface to the GNS 430/530.

Note: King KI-203, KI-204, KI-208 and KI-209 may be connected to the secondary VOR/ILS output of the GNS 430/530 (connector P4006). This output provides only VOR/ILS information on the indicator, not GPS deviation information.

What items are needed to install the GNS 430/430W/530/530W into my aircraft?

To use all functions of the GNS 430/430W/530/530W, the following items are required:

GPS antenna (usually included when the system is purchased)
External CDI* for VOR/ILS navigation and glideslope information; also required for IFR certification
Nav antenna* for VHF Nav functions
COMM antenna* for COMM functions

*These items are not included with the standard GNS system. Existing aircraft units may be interfaced, but the GNS installation manual should be consulted for complete compatibility information. As with all avionics installations, other general materials are required but not supplied with the standard system. These can include, but are not limited to, wire, mounting screws, circuit breakers, tie wraps, ring terminals, coaxial cable, hand crimping tools, and crimp positioner/insertion/extraction tools.

Which traffic systems interface with and display on the Garmin GNS 430/530 series?

The GNS 430/530 series units can accept information from any traffic advisory system with ARINC 429 transmit formats.

Can original Garmin GNS 400/500 series units be upgraded to HTAWS?

Garmin HTAWS (Helicopter Terrain Awareness) is only available for Garmin WAAS GPS receivers.

The added GPS integrity, quality and performance of WAAS GPS is needed for the helicopter terrain functions.

An original GNS 430, GNC 420, GPS 400, GNS 530 or GPS 500 navigator must therefore be upgraded to WAAS ("W" status) before HTAWS can be incorporated.

Can the Garmin GNS 430/530 and GNS 430W/530W be upgraded to the A version?

No. Garmin does not offer an upgrade to add the 16 watt comm (the "A" version) to the GNS 430/530 and GNS 430W/530W units.

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