Eclipse EA500 Maintenance Manual

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TO: HOLDERS OF THE AIRCRAFT MAINTENANCE MANUAL (06-117751)

Pages that have been added or revised are summarized below. Remove and insert the affected

pages as listed, and enter the above revision number with issue date into the Record of Revisions

sheet.

This Temporary Revision incorporates and supersedes previously released temporary

revisions for the chapters listed below.

Do not remove this page. Keep it in place as a record of previous changes.

CH/SE/SU

Page Block No.

34-10-00

Adjustment / Test - Added Standby Pitot/Static Verification with Standby

PgBlk 501

Display Unit (SDU).

34-10-10

PgBlk 401-Rem

Added MB 500-34-028 to effectivity for Pitot/AOA Probe auxiliary heaters -

(C)

Removal - Config C.

34-10-10

PgBlk 401-Inst

Added MB 500-34-028 to effectivity for Pitot/AOA Probe auxiliary heaters -

(C)

Installation - Config C.

34-40-50

PgBlk 1 (A)

Description and Operation – Config A. Corrected effectivity.

34-40-50

Description and Operation – Config B. Added configuration B – POST SB

PgBlk 1 (B)

500-31-024.

34-40-50

PgBlk 501 (A)

Adjustment/Test – Config A. Corrected effectivity.

34-40-50

Adjustment/Test – Config B. Added configuration for Stormscope lightning

PgBlk 501 (B)

strike test post SB 500-31-024.

34-50-10

Description and Operation - Revised Effectivity (ALL POST MB

PgBlk 1 (B)

500-31-018). Revised Description.

34-50-10

Description and Operation - Revised Effectivity (ALL POST MB

PgBlk 201 (A)

500-31-018). Updated for ADS-B Out – Config A.

34-50-10

PgBlk 201 (B)

Added GPS 3 (GDL 88) Maintenance Practices – Config B.

34-50-10

PgBlk 501 (C)

Adjustment/Test for GPS Units – Config C.

34-50-11

PgBlk 401-Rem

(C)

Added GPS 3 (GDL 88) Unit Removal procedure.

EA500 Aircraft Maintenance Manual — 06-117751

CHAPTER - 34 HIGHLIGHTS

(Summary of Changes)

Revision No. TR34-21 Sep 30/20

Description of Change

Temporary Revision No. 34-21

34-HIGHLIGHTS

Sep 30/20

Page 1

Table of Contents

Summary of Contents for Eclipse EA500

Page 1 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 CHAPTER - 34 HIGHLIGHTS (Summary of Changes) Revision No. TR34-21 Sep 30/20 TO: HOLDERS OF THE AIRCRAFT MAINTENANCE MANUAL (06-117751) Pages that have been added or revised are summarized below. Remove and insert the affected pages as listed, and enter the above revision number with issue date into the Record of Revisions sheet.
Page 2 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 CH/SE/SU Page Block No. Description of Change 34-50-11 PgBlk 401-Rem Added Removal procedure for iFMS 2.7 GPS. 34-50-11 PgBlk 401-Inst GPS Installation - Revised Effectivity (ALL POST MB 500-31-018) and Job Close-Up.
Page 3 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 CH/SE/SU Page Block No. Description of Change 34-50-21 PgBlk 501 Adjustment/Test - Added ADS-B Out check. Added antenna coupler to test. 34-50-21 PgBlk 401-Inst Installation - Revised Job Set-Up. 34-50-23 PgBlk 401-Inst Installation - Revised Job Close-up test reference.
Page 4 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 THIS PAGE INTENTIONALLY LEFT BLANK 34-HIGHLIGHTS Page 4 Sep 30/20 © 2020 Eclipse Aerospace, Inc.
Page 5 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 FLIGHT ENVIRONMENT DATA - ADJUSTMENT/TEST AMM-34-10-00-071-801 1. General A. This task gives procedures to do an adjustment/test of the flight environment data components. NOTE: This test procedure complies with the requirements of 14 CFR Part 43 Appendix (1) Unless indicated differently, the adjustment/test procedures are the same for both left and right sides.
Page 6 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 Component to be Tested Test Standby Pitot/Static probe Standby Pitot/Static Probe System Leak Test SUBTASK AMM-34-10-00-071-701-002, Standby Pitot/Static Probe Verification Test (Effectivity Noted) SUBTASK AMM-34-10-00-071-701-006 SUBTASK AMM-34-10-00-071-701-007 AMM-30-30-00-071-801 – Pitot and Static Anti-Ice System - Adjustment/Test.
Page 7 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 3. Job Set-Up SUBTASK AMM-34-10-00-071-921-001 * * * ALL A. Make aircraft safe for maintenance. Refer to AMM-20-00-01-051-801 – Make Safe For Maintenance. B. Apply external power to the aircraft. Refer to AMM-24-40-00-051-801 –...
Page 8 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (6) Set both the left and right PFD Baro to 29.92 by pressing the BARO SET knob on the Autopilot Control Panel (ACP). Make sure the baro setting matches on the left and right PFD.
Page 9 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 Adjust the Pitot/AOA Probe Adaptor nozzles to align with the holes of the Pitot/AOA probe. NOTE: No other lubricating fluid is permitted. Malfunction of the equipment in flight is possible.
Page 10 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 P22201-3 adapter, make sure that the pitot probe drain hole is covered with tape. If needed, lubricate with Pitot adaptor lubricating fluid (Part Number LF5050). NOTE: No other lubricating fluid is permitted. Malfunction of the equipment in flight is possible.
Page 11 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 • After the Waiting and Timing intervals are complete, the Barfield Pitot/Static Tester DPS450 displays Timed Rates Available. (16) Check that the maximum ROC is 100 ft/min or less and the maximum Rt CAS is 2 kts/min.
Page 12 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 needed, lubricate with Pitot adaptor lubricating fluid (Part Number LF5050). Adjust the Pitot/AOA Probe Adaptor nozzles to align with the holes of the Pitot/AOA probe. NOTE: No other lubricating fluid is allowed, possible malfunction of the...
Page 13 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 P22201-3 adapter, make sure that the pitot probe drain hole is covered with tape. If needed, lubricate with Pitot adaptor lubricating fluid (Part Number LF5050). NOTE: No other lubricating fluid is permitted. Malfunction of the equipment in flight is possible.
Page 14 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (13) If no further maintenance is required, remove all of the Nav Aids test equipment from the aircraft. Stow all the Air Data Accessories Kit ; (Nav Aids PN ADA500945) equipment and the Barfield Pitot/Static Tester DPS500.
Page 15 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (a) Remove the P22201MD-4 adapter (or the P22201-3 adapter) from the Pt Hose. Connect the hose from the Pt adapter on the Barfield to PS35210MD-4-4 adapter (or PS35210- 4-4 adapter) connector marked PITOT (this is the connector at the end of the adapter).
Page 16 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (16) If no further maintenance is required, remove all of the Nav Aids test equipment from the aircraft. Stow the Air Data Accessories Kit ; (Nav Aids PN ADA500945) equipment and Barfield Pitot/Static Tester DPS450.
Page 17 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (3) Press LEAK MEASURE/ CONTROL for CONTROL MODE. (4) Press ROC RATE Ps to select the ROC control aim, enter 4000 and press Enter. (5) Press ALT Ps to select the ALT control aim, enter 30000 and press Enter.
Page 18 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (4) Skip this step if the Barfield Pitot/Static Tester DPS450 is in Quad mode. Quad mode will display four values: Ps, RtPc, Qc, RtQc. Press SETUP, press F1 to select Display.
Page 19 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 7. Angle of Attack Test SUBTASK AMM-34-10-00-071-701-004 * * * ALL NOTE: If a Barfield Pitot/Static Tester DPS450 is used for this test complete paragraph A. If a Barfield Pitot/Static Tester DPS500 is used, go to paragraph B.
Page 20 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (a) Remove the PS35210 Pressure Test Adaptor from the Pitot/Static probe. (b) Remove the E500-7270 hose from the PITOT (end) connector of the PS35210 adapter and connect to a NAV Aids quick connect cross (leave other end of hose connected to the Barfield Pt connector).
Page 21 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 B. Angle of Attack Test with the Barfield Pitot/Static Tester DPS500: Procedure is given for the left side and is the same for the right side. (1) Connect the WOW Box or AMC to the aircraft and make sure that the ECB's are collared.
Page 22 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (c) Connect another LH and/or RH MFP pitot hose approximately 2 ft long to the upper nozzle of the APA94250 adapter. Connect the other end to a second NAV Aids quick connect cross.
Page 23 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 8. Pitot and Static Verification Test SUBTASK AMM-34-10-00-071-701-005 * * * ALL NOTE: If a Barfield Pitot/Static Tester DPS450 is used for this test complete paragraph A. If a Barfield Pitot/Static Tester DPS500 is used, go to paragraph B.
Page 24 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 end of the long hose (12) to the quick-connect cross (11) . Connect the static short hose to the top fitting of the Static Port Adaptor (Nav Aids, SS53515-4-4) (10)
Page 25 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (11) Set the Barfield Pitot/Static Tester DPS450 static pressure to 40,613 feet and set the airspeed to 159.2 knots as follows: (a) Press ALT Ps to select the ALT control aim, enter 40613 and press ENTER.
Page 26 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (a) If the Barfield Pitot/Static Tester DPS450 is not in CONTROL MODE, press LEAK MEASURE/CONTROL. (b) After the Barfield Pitot/Static Tester DPS450 displays shows SAFE AT GROUND prompt, power off the Barfield Pitot/Static Tester DPS450.
Page 27 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (d) Connect the Static Test Hose Assembly ; (Nav Aids PN E500-5160) (long hose) (12) to the Barfield Pitot/Static Tester DPS500 Ps connection. Connect other end of long hose (12)
Page 28 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (9) Set both the left and right PFD Baro to 29.92 by using the BARO SET knob on the ACP. • Make sure the baro setting matches on the left and right PFD.
Page 29 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (a) Press ALT Ps to select the ALT control aim, enter 6008 and press Enter. Press SPEED Qc, enter 66.1 and press Enter. Wait for at least a 15 second stabilization period after the altitude and airspeed achieve these new air data parameter set point values to continue.
Page 30 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (9) Set the static pressure to 29,874 feet and set the airspeed to 247.1 Knots. (a) Press ALT Ps to select the ALT control aim, enter 29874 and press ENTER.
Page 31 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (2) Set the WOW Box switches to WOnW. (3) Power up the aircraft by setting the SYS BATT and START BATT switches to ON and the BUS TIE switch to AUTO.
Page 32 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 stabilization period after the altitude and airspeed achieve these new air data parameter set point values to continue. (16) Record the Standby Pitot/Static probe altitude and airspeed from the MFD.
Page 33 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (9) Set the static pressure to 29,874 feet and set the airspeed to 247.1 Knots. (a) Press ALT Ps to select the ALT control aim, enter 29874 and press ENTER.
Page 34 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (2) Set the WOW Box switches to WOnW. (3) Power up the aircraft by setting the SYS BATT and START BATT switches to ON and the BUS TIE switch to AUTO.
Page 35 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (a) Press ALT Ps to select the ALT control aim, enter 5999 and press ENTER. Press SPEED Qc and enter 64.9 then press ENTER. Wait for at least a 15 second stabilization period after the altitude and airspeed achieve these new air data parameter set point values to continue.
Page 36 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 • ECB - L STATIC HEAT (R FWD Bus) • ECB - R STATIC HEAT (R FWD Bus) • ECB - R STATIC HEAT (L FWD Bus) • ECB - STBY PITOT HEAT (BATT Bus) or ECB - STBY PITOT HEAT (L FWD) •...
Page 37 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 Left Pitot/Static Hose Configuration (Three Port Adapter) Figure 501 (Sheet 1 of 1) 34-10-00 EFFECTIVITY: NOTED Page 533 Sep 30/20 © 2020 Eclipse Aerospace, Inc.
Page 38 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 Left Angle of Attack Hose Configuration Figure 502 (Sheet 1 of 1) 34-10-00 EFFECTIVITY: NOTED Page 534 Sep 30/20 © 2020 Eclipse Aerospace, Inc.
Page 39 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 Standby Pitot/Static Test Adaptor Connections Figure 503 (Sheet 1 of 1) 34-10-00 EFFECTIVITY: NOTED Page 535 Sep 30/20 © 2020 Eclipse Aerospace, Inc.
Page 40 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 Left Right AOA Data AOA Data Left ADC Right ADC Right Pitot/AOA Probe Left Pitot/AOA Probe PSIA PSIA Trans Trans Left Dual Static Port Right Dual Static Port Primary Static...
Page 41 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 PITOT/AOA PROBES - REMOVAL AMM-34-10-10-001-C-801 1. General A. This task gives the procedures to remove the Pitot/Angle of Attack (AOA) probes. B. There are two Pitot/AOA probes on the fuselage, forward of the cockpit. Access procedures for the right Pitot/AOA probe are given in Job Setup.
Page 42 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 3. Procedure SUBTASK AMM-34-10-10-001-C-011-001 (Refer to Fig. 401.) A. Disconnect electrical connector (17) from aircraft wiring harness. B. Remove jam nut (15) from electrical connector (17) and remove electrical connector from...
Page 43 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 5 (x5) Pitot/AOA Probes - Removal/Installation Figure 401 (Sheet 1 of 4) 34-10-10 EFFECTIVITY: ALL, POST MB 500-34-027 AND MB 500-34-028 CONFIG C Page 403-Rem Sep 30/20 © 2020 Eclipse Aerospace, Inc.
Page 44 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 13, 14 PITOT/AOA PROBE AIRCRAFT STRUCTURE Pitot/AOA Probes - Removal/Installation Figure 401 (Sheet 2 of 4) 34-10-10 EFFECTIVITY: ALL, POST MB 500-34-027 AND MB 500-34-028 CONFIG C Page 404-Rem Sep 30/20...
Page 45 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 13, 14 PITOT/AOA PROBE AIRCRAFT STRUCTURE Pitot/AOA Probes - Removal/Installation Figure 401 (Sheet 3 of 4) 34-10-10 EFFECTIVITY: ALL, POST MB 500-34-027 AND MB 500-34-028 CONFIG C Page 405-Rem Sep 30/20...
Page 46 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 Pitot/AOA Probes - Removal/Installation Figure 401 (Sheet 4 of 4) 34-10-10 EFFECTIVITY: ALL, POST MB 500-34-027 AND MB 500-34-028 CONFIG C Page 406-Rem Sep 30/20 © 2020 Eclipse Aerospace, Inc.
Page 47 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 Co-pilot's Armrest USB Port - AMC Hookup Figure 402 (Sheet 1 of 1) 34-10-10 EFFECTIVITY: ALL, POST MB 500-34-027 AND MB 500-34-028 CONFIG C Page 407-Rem Sep 30/20 © 2020 Eclipse Aerospace, Inc.
Page 48 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 VCS Door Cals Page Figure 403 (Sheet 1 of 1) 34-10-10 EFFECTIVITY: ALL, POST MB 500-34-027 AND MB 500-34-028 CONFIG C Page 408-Rem Sep 30/20 © 2020 Eclipse Aerospace, Inc.
Page 49 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 PITOT/AOA PROBE - INSTALLATION AMM-34-10-14-041-C-801 1. General A. This task gives the procedures to install the Pitot/Angle of Attack (AOA) probes. 2. Job Set-Up SUBTASK AMM-34-10-10-041-C-921-001 (Refer to Fig. 401, Sheet A.
Page 50 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 3. Procedure SUBTASK AMM-34-10-10-041-C-411-001 (Refer to Fig. 401.) CAUTION: REMOVE THE NOTED SCREW FROM THE PITOT/AOA PROBE ONLY. DO NOT LOOSEN OR DISTURB OTHER MOUNTING HARDWARE. NOTE: The fastener securing the grounding jumper to the probe shall be installed using torque required to bring the bearing faces into positive contact and have Loctite 242 to applied to the screw threads.
Page 51 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 N. Use PRC-Desoto aerodynamic smoothing sealant (PR-2050) to close gaps and seal around Pitot/AOA probes. AMM-20-08-00-051-801 – Sealants and Adhesives - Maintenance Practices. 4. Job Close-Up SUBTASK AMM-34-10-10-041-C-921-002 CAUTION: MAKE SURE ANY PACKING/MATERIALS SUPPLIED WITH THE UNIT ARE REMOVED AND NOT LEFT IN PLACE BETWEEN THE PROBE BODY AND THE AIRCRAFT AFTER INSTALLATION.
Page 52 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 Pitot/AOA Probes - Removal/Installation Figure 401 (Sheet 1 of 5) 34-10-10 EFFECTIVITY: ALL, POST MB 500-34-027 AND MB 500-34-028 CONFIG C Page 404-Inst Sep 30/20 © 2020 Eclipse Aerospace, Inc.
Page 53 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 5 (x5) Pitot/AOA Probes - Removal/Installation Figure 401 (Sheet 2 of 5) 34-10-10 EFFECTIVITY: ALL, POST MB 500-34-027 AND MB 500-34-028 CONFIG C Page 405-Inst Sep 30/20 © 2020 Eclipse Aerospace, Inc.
Page 54 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 13, 14 PITOT/AOA PROBE AIRCRAFT STRUCTURE Pitot/AOA Probes - Removal/Installation Figure 401 (Sheet 3 of 5) 34-10-10 EFFECTIVITY: ALL, POST MB 500-34-027 AND MB 500-34-028 CONFIG C Page 406-Inst Sep 30/20...
Page 55 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 13, 14 PITOT/AOA PROBE AIRCRAFT STRUCTURE Pitot/AOA Probes - Removal/Installation Figure 401 (Sheet 4 of 5) 34-10-10 EFFECTIVITY: ALL, POST MB 500-34-027 AND MB 500-34-028 CONFIG C Page 407-Inst Sep 30/20...
Page 56 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 Pitot/AOA Probes - Removal/Installation Figure 401 (Sheet 5 of 5) 34-10-10 EFFECTIVITY: ALL, POST MB 500-34-027 AND MB 500-34-028 CONFIG C Page 408-Inst Sep 30/20 © 2020 Eclipse Aerospace, Inc.
Page 57 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 Co-pilot's Armrest USB Port - AMC Hookup Figure 402 (Sheet 1 of 1) 34-10-10 EFFECTIVITY: ALL, POST MB 500-34-027 AND MB 500-34-028 CONFIG C Page 409-Inst Sep 30/20 © 2020 Eclipse Aerospace, Inc.
Page 58 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 VCS Door Cals Page Figure 403 (Sheet 1 of 1) 34-10-10 EFFECTIVITY: ALL, POST MB 500-34-027 AND MB 500-34-028 CONFIG C Page 410-Inst Sep 30/20 © 2020 Eclipse Aerospace, Inc.
Page 59 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 STORMSCOPE - DESCRIPTION AND OPERATION AMM-34-40-50-081-A-801 1. Introduction A. The Lightning Detection System (LDS) on the aircraft is referred to by it’s trademark name Stormscope®. Stormscope is a passive thunderstorm detection sensor. The sensor maps electrical discharge activity 360 degrees around the aircraft to a distance of 200 nautical miles for display on the GPS 400W display.
Page 60 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 Stormscope - GPS 400W Display Figure 1 (Sheet 1 of 1) 34-40-50 EFFECTIVITY: 0001 - 0008, 0010 - 0050, 0052, 0054 - 0267 PRE SB 500-31-024 CONFIG A Page 2 Sep 30/20 ©...
Page 61 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 STORMSCOPE - DESCRIPTION AND OPERATION AMM-34-40-50-081-B-801 1. Introduction A. The Lightning Detection System (LDS) on the aircraft is referred to by it’s trademark name Stormscope®. Stormscope is a passive thunderstorm detection sensor. The sensor maps electrical discharge activity 360 degrees around the aircraft to a distance of 200 nautical miles for display on the PFD.
Page 62 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 PFD Stormscope Overlay (Cell Mode / Strike Mode) Figure 1 (Sheet 1 of 1) 34-40-50 EFFECTIVITY: 0001 - 0008, 0010 - 0050, 0052, 0054 - 0267 POST SB 500-31-024 CONFIG B...
Page 63 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 STORMSCOPE - ADJUSTMENT/TEST AMM-34-40-50-071-A-801 1. General A. This task gives the procedures to perform the Adjustment/Test for the Lightning Detection System (LDS). The LDS on the aircraft is referred to by it’s trademark name Stormscope®.
Page 64 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 4. Procedure – Upper Over Fin Fairing – NOT INSTALLED – SUBTASK AMM-34-40-50-071-A-701-001 A. Test Set-Up NOTE: The operator should be familiar with the WX-PA Portable Analyzer Kit. (1) Make sure that all aircraft power is off.
Page 65 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 • ECB - LIGHTNING DETECT SYS (R AFT Bus) (7) On the MFD ECB AVIONICS synoptic page, PULL the following ECB: • ECB - LIGHTNING DETECT SYS (R AFT Bus) (8) Turn on the left Garmin 400W and allow it to initialize: (a) On the left Garmin 400W, turn the small upper left knob clockwise until it “clicks”,...
Page 66 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 B. Initial System Test Refer to Fig. 504 (1) On the left Garmin 400W, select the 360° display mode (if not already in 360° mode) and verify proper 360° display format on the left Garmin 400W unit.
Page 67 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (9) Verify aircraft is positioned so that it can be freely turned 45° (± 5°) clockwise (to the right). (a) Make sure area around aircraft is clear. (b) Make sure that WX-PA tester can be moved with the aircraft.
Page 68 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 C. Cardinal Bearings Test (1) On the LH Garmin 400W, press the MENU button. Highlight CLEAR STORM DATA? (if not already highlighted), then press the ENT button. (2) Verify that the Strike Rate is displayed on the Garmin 400W as shown in Fig.
Page 69 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 D. Heading Input Check (1) On the WX-PA, select “Continuous Out” on the MODE MENU, then press the MENU/ ENTR button once (so that WX-PA indicates “PAUSED” and not “RUNNING”).
Page 70 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 5. Procedure – Upper Over Fin Fairing – INSTALLED – SUBTASK AMM-34-40-50-071-A-701-002 A. Test Set-Up NOTE: With the WX-PA antenna placed on top of the fin fairing cap (over the Stormscope antenna), the Stormscope unit will plot data on the GPS 400W display at a farther range than the range selected on the WX-PA.
Page 71 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (5) If the aircraft is in the W-off-W condition, the following ECB’s must be collared: CAUTION: IF THE PITOT/STATIC HEAT ECB’S ARE NOT COLLARED OFF, HARM TO PERSONNEL OR AIR DATA TEST EQUIPMENT CAN OCCUR.
Page 72 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 • ECB - LIGHTNING DETECT SYS (R AFT Bus) (11) Make sure that no self-test failure messages appear. (12) Stormscope is now powered up and initialized. (a) Make sure that no self-test failure messages appear.
Page 73 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (6) Key the VHF 1 Comm mic (transmit on VHF 1 Comm) repeatedly. (a) Make sure no strike data appears on the GPS 400W Lightning display as a result of keying the VHF 1 transmitter.
Page 74 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 C. Cardinal Bearings Test (1) On the LH Garmin 400W, press the MENU button. Highlight CLEAR STORM DATA? (if not already highlighted), then press the ENT button. (2) Verify that the Strike Rate is displayed on the Garmin 400W as shown in Fig.
Page 75 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 D. Heading Input Check (1) On the WX-PA, select “Continuous Out” on the MODE MENU, then press the MENU/ ENTR button once (so that WX-PA indicates “PAUSED” and not “RUNNING”).
Page 76 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 6. Job Close-Up SUBTASK AMM-34-40-50-071-A-921-002 A. If no other work is to be performed, turn off the aircraft power by setting the SYS BATT and START BATT Switches to the OFF (down) position and BUS TIE to OPEN (down) position.
Page 77 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 WX-PA Antenna Alignment Figure 501 (Sheet 1 of 1) 34-40-50 EFFECTIVITY: 0001 - 0008, 0010 - 0050, 0052, 0054 - 0267 PRE SB 500-31-024 CONFIG A Page 515 Sep 30/20...
Page 78 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 Positioning the WX-PA Antenna on the Over Fin Fairing Figure 502 (Sheet 1 of 1) 34-40-50 EFFECTIVITY: 0001 - 0008, 0010 - 0050, 0052, 0054 - 0267 PRE SB 500-31-024...
Page 79 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 WX-PA Antenna Attachment Figure 503 (Sheet 1 of 1) 34-40-50 EFFECTIVITY: 0001 - 0008, 0010 - 0050, 0052, 0054 - 0267 PRE SB 500-31-024 CONFIG A Page 517 Sep 30/20...
Page 80 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 Stormscope — GPS 400W Display Figure 504 (Sheet 1 of 1) 34-40-50 EFFECTIVITY: 0001 - 0008, 0010 - 0050, 0052, 0054 - 0267 PRE SB 500-31-024 CONFIG A Page 518 Sep 30/20 ©...
Page 81 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 STORMSCOPE - ADJUSTMENT/TEST AMM-34-40-50-071-B-801 1. General A. This task gives the procedures to perform the Adjustment/Test for the Lightning Detection System (LDS). The LDS on the aircraft is referred to by it’s trademark name Stormscope®.
Page 82 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 4. Procedure – Upper Over Fin Fairing – NOT INSTALLED – SUBTASK AMM-34-40-50-071-B-701-001 A. Test Set-Up (1) Attach the WX-PA test set’s antenna to the LDS NY-163 antenna. (a) Position the WX-PA antenna on the LDS antenna as shown in Fig.
Page 83 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (11) Key the pilot’s Comm mic switch (transmit on VHF 1 Comm) repeatedly. (a) Verify no strike data appears on the PFDs as a result of keying the VHF 1 transmitter.
Page 84 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (21) Verify that the Strike Rate is displayed on the PFDs. (a) When Strike Rate reaches approximately 580 ± 40 strikes per minute, verify that the strikes appear within the required bearing limits for each of the settings on...
Page 85 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (22) On the WX-PA, press 2 , then press MENU/ENTR to return to Main Menu. (23) On the WX-PA, select “Continuous Out” on the MODE MENU, then press the MENU/ ENTR button once (so that WX-PA indicates “PAUSED”...
Page 86 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 5. Procedure – Upper Over Fin Fairing – INSTALLED – SUBTASK AMM-34-40-50-071-B-701-002 A. Test Set-Up IMPORTANT! If for any reason the WX-PA tester produces "double image" lightning strikes on the PFD display, where the programmed strike pattern appears and additional strikes appear on a reciprocal bearing (180°...
Page 87 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (10) Depress the right LSK #4 to set the Stormscope mode to STRIKE. (a) Verify that the Strike Rate is displayed on the PFDs (‘x’ shaped symbols may also be displayed on the HSI, if lightning is present).
Page 88 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (22) Verify that the Strike Rate is displayed on the PFDs. (a) When Strike Rate reaches approximately 580 ± 40 strikes per minute, verify that the strikes appear within the required bearing limits for each of the settings on...
Page 89 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (23) On the WX-PA, press 2 , then press MENU/ENTR to return to Main Menu. (24) On the WX-PA, select “Continuous Out” on the MODE MENU, then press the MENU/ ENTR button once (so that WX-PA indicates “PAUSED”...
Page 90 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 6. Job Close-Up SUBTASK AMM-34-40-50-071-B-921-002 A. If no other work is to be performed, turn off the aircraft power by setting the SYS BATT and START BATT Switches to the OFF (down) position, and the BUS TIE to OPEN (down) position.
Page 91 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 WX-PA Antenna Alignment Figure 501 (Sheet 1 of 1) 34-40-50 EFFECTIVITY: 0001 - 0008, 0010 - 0050, 0052, 0054 - 0267 POST SB 500-31-024 CONFIG B Page 511 Sep 30/20...
Page 92 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 Positioning the WX-PA Antenna on the Over Fin Fairing Figure 502 (Sheet 1 of 1) 34-40-50 EFFECTIVITY: 0001 - 0008, 0010 - 0050, 0052, 0054 - 0267 POST SB 500-31-024...
Page 93 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 WX-PA Antenna Attachment Figure 503 (Sheet 1 of 1) 34-40-50 EFFECTIVITY: 0001 - 0008, 0010 - 0050, 0052, 0054 - 0267 POST SB 500-31-024 CONFIG B Page 513 Sep 30/20...
Page 94 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 PFD Stormscope Overlay (Cell Mode / Strike Mode) Figure 504 (Sheet 1 of 1) 34-40-50 EFFECTIVITY: 0001 - 0008, 0010 - 0050, 0052, 0054 - 0267 POST SB 500-31-024 CONFIG B...
Page 95 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 GPS - DESCRIPTION AND OPERATION AMM-34-50-10-081-B-801 1. Introduction A. Global Positioning System/Wide Area Augmentation System (GPS/WAAS) is a U.S. satellite-based navigational, positioning and time transfer system operated by the Department of Defense (DOD). The GPS system provides highly accurate position and velocity information and precise time on a continuous global basis to an unlimited number of properly-equipped users.
Page 96 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 2. Description SUBTASK AMM-34-50-10-081-B-871-001 A. Garmin GPS 400W (1) The left-side GPS 400W is referred to as “GPS 1” and the right side GPS 400W installed will be called “GPS 2”.
Page 97 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 COMBINATION ANTENNAS GPS400W GPS400W (ROTATED FOR CLARITY) GPS — Combination Antenna Location Figure 1 (Sheet 1 of 1) 34-50-10 EFFECTIVITY: 0001-0262 POST SB 500-99-005; AND 0266-0267; ALL POST MB 500-31-018...
Page 98 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 THIS PAGE INTENTIONALLY LEFT BLANK 34-50-10 EFFECTIVITY: 0001-0262 POST SB 500-99-005; AND 0266-0267; ALL POST MB 500-31-018 CONFIG B Page 4 Sep 30/20 © 2020 Eclipse Aerospace, Inc.
Page 99 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 GPS - MAINTENANCE PRACTICES AMM-34-50-10-051-A-801 1. General A. The purpose of this task is to provide instructions for configuring the GPS 400W for use on the Eclipse Model 500 aircraft.
Page 100 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 F. Make sure the following circuit breakers in the pilot's and co-pilot's armrest (Com-Jack Panels) are engaged: • MECHANICAL CIRCUIT BREAKER - CIRCUIT BREAKER BOX LEFT, XPDR1/ GPS1 (or) MECHANICAL CIRCUIT BREAKER - CIRCUIT BREAKER BOX LEFT, XPDR1/GPS1/ATT3 •...
Page 101 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 5. Procedure SUBTASK AMM-34-50-10-051-A-701-002 NOTE: This configuration procedure is for one GPS 400W unit. However, both installed GPS 400W units must be configured. Differences in the configuration of the left and right GPS 400W units are indicated in the procedure.
Page 102 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 • “CONTINUING IN x SECONDS” (10) After approximately one minute, the GPS 400W will start Self Test. Several screens of information will be displayed. When a flashing OK? is displayed, press ENT.
Page 103 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (not selectable), select OFF and return to this field to select EFIS / Airdata after other fields on the page have been configured. NOTE: Note 1 in Fig. 202. For left GPS 400W, on aircraft configured for (Standby Indication and Electrical Provisions Package option), enter: “Off”;...
Page 104 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (c) Use the following settings for CHNL 4 INPUT and OUTPUT: “WX-500” for left GPS 400W on Stormscope-equipped aircraft (INPUT and OUTPUT). “Off” for left GPS 400W on aircraft not equipped with Stormscope (INPUT and OUTPUT).
Page 105 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 CAUTION: HANDLE THE DATA CARDS CAREFULLY. DO NOT TOUCH THE CONNECTOR EDGE OF THE DATA CARD. DO NOT INSTALL OR REMOVE A DATA CARD WHILE THE GPS 400W IS ON.
Page 106 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (2) Verify communication with Stormscope by confirming STORMSCOPE CONFIG page appears as shown in Fig. 210. If page appears different from Fig. 210, re-check settings in section C., and Stormscope installation and communication.
Page 107 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (17) Press the small right knob to return to the SETUP 1 page after UNITS / MAG VAR configuration is set. (18) Rotate the large right knob to select Position / Map Datum and press ENT.
Page 108 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (36) Press the small right knob to return to the SETUP 2 page after DATA FIELD CONFIGURATION configuration is set. Press the small right knob again to dismiss the cursor on SETUP 2.
Page 109 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 GPS 400W Panel – Layout Figure 201 (Sheet 1 of 1) 34-50-10 EFFECTIVITY: 0001-0262, POST SB 500-99-005; AND 0266-0267; ALL POST MB 500-31-018 CONFIG A Page 211 Sep 30/20 © 2020 Eclipse Aerospace, Inc.
Page 110 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 GPS 400W Panel – MAIN ARINC 429 CONFIG Settings Figure 202 (Sheet 1 of 1) 34-50-10 EFFECTIVITY: 0001-0262, POST SB 500-99-005; AND 0266-0267; ALL POST MB 500-31-018 CONFIG A Page 212 Sep 30/20 ©...
Page 111 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 GPS 400W Panel – MAIN RS232 CONFIG Settings Figure 203 (Sheet 1 of 1) 34-50-10 EFFECTIVITY: 0001-0262, POST SB 500-99-005; AND 0266-0267; ALL POST MB 500-31-018 CONFIG A Page 213 Sep 30/20 ©...
Page 112 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 GPS 400W Panel – MAIN SYSTEM CONFIG – Fuel Settings Figure 204 (Sheet 1 of 1) 34-50-10 EFFECTIVITY: 0001-0262, POST SB 500-99-005; AND 0266-0267; ALL POST MB 500-31-018 CONFIG A...
Page 113 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 GPS 400W Panel – MAIN SYSTEM CONFIG – Terrain Settings Figure 205 (Sheet 1 of 1) 34-50-10 EFFECTIVITY: 0001-0262, POST SB 500-99-005; AND 0266-0267; ALL POST MB 500-31-018 CONFIG A...
Page 114 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 GPS 400W Panel – MAIN SYSTEM CONFIG – Discretes Settings Figure 206 (Sheet 1 of 1) 34-50-10 EFFECTIVITY: 0001-0262, POST SB 500-99-005; AND 0266-0267; ALL POST MB 500-31-018 CONFIG A...
Page 115 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 GPS 400W Panel – MAIN INPUTS 1 Display Figure 207 (Sheet 1 of 1) 34-50-10 EFFECTIVITY: 0001-0262, POST SB 500-99-005; AND 0266-0267; ALL POST MB 500-31-018 CONFIG A Page 217 Sep 30/20 ©...
Page 116 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 GPS 400W Panel – MAIN LIGHTING Settings Figure 208 (Sheet 1 of 1) 34-50-10 EFFECTIVITY: 0001-0262, POST SB 500-99-005; AND 0266-0267; ALL POST MB 500-31-018 CONFIG A Page 218 Sep 30/20...
Page 117 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 GPS 400W Panel – GPS VERTICAL OFFSET Settings Figure 209 (Sheet 1 of 1) 34-50-10 EFFECTIVITY: 0001-0262, POST SB 500-99-005; AND 0266-0267; ALL POST MB 500-31-018 CONFIG A Page 219 Sep 30/20 ©...
Page 118 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 GPS 400W Panel – STORMSCOPE CONFIG Settings Figure 210 (Sheet 1 of 1) 34-50-10 EFFECTIVITY: 0001-0262, POST SB 500-99-005; AND 0266-0267; ALL POST MB 500-31-018 CONFIG A Page 220 Sep 30/20...
Page 119 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 GPS 400W Panel – AUX Page Group & CROSSFILL Settings Figure 211 (Sheet 1 of 2) 34-50-10 EFFECTIVITY: 0001-0262, POST SB 500-99-005; AND 0266-0267; ALL POST MB 500-31-018 CONFIG A...
Page 120 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 GPS 400W Panel – AUX Page Group & CROSSFILL Settings Figure 211 (Sheet 2 of 2) 34-50-10 EFFECTIVITY: 0001-0262, POST SB 500-99-005; AND 0266-0267; ALL POST MB 500-31-018 CONFIG A...
Page 121 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 GPS 400W Panel – AIRSPACE ALARMS Settings Figure 212 (Sheet 1 of 1) 34-50-10 EFFECTIVITY: 0001-0262, POST SB 500-99-005; AND 0266-0267; ALL POST MB 500-31-018 CONFIG A Page 223 Sep 30/20...
Page 122 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 GPS 400W Panel – CDI / ALARMS Settings Figure 213 (Sheet 1 of 1) 34-50-10 EFFECTIVITY: 0001-0262, POST SB 500-99-005; AND 0266-0267; ALL POST MB 500-31-018 CONFIG A Page 224 Sep 30/20 ©...
Page 123 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 GPS 400W Panel – UNITS / MAG VAR Settings Figure 214 (Sheet 1 of 1) 34-50-10 EFFECTIVITY: 0001-0262, POST SB 500-99-005; AND 0266-0267; ALL POST MB 500-31-018 CONFIG A Page 225 Sep 30/20 ©...
Page 124 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 GPS 400W Panel – POSITION FORMAT / MAP DATUM Settings Figure 215 (Sheet 1 of 1) 34-50-10 EFFECTIVITY: 0001-0262, POST SB 500-99-005; AND 0266-0267; ALL POST MB 500-31-018 CONFIG A...
Page 125 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 GPS 400W Panel – DATE / TIME Settings Figure 216 (Sheet 1 of 1) 34-50-10 EFFECTIVITY: 0001-0262, POST SB 500-99-005; AND 0266-0267; ALL POST MB 500-31-018 CONFIG A Page 227 Sep 30/20 ©...
Page 126 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 GPS 400W Panel – DISPLAY Settings Figure 217 (Sheet 1 of 1) 34-50-10 EFFECTIVITY: 0001-0262, POST SB 500-99-005; AND 0266-0267; ALL POST MB 500-31-018 CONFIG A Page 228 Sep 30/20...
Page 127 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 GPS 400W Panel – NEAREST AIRPORT CRITERIA Settings Figure 218 (Sheet 1 of 1) 34-50-10 EFFECTIVITY: 0001-0262, POST SB 500-99-005; AND 0266-0267; ALL POST MB 500-31-018 CONFIG A Page 229 Sep 30/20 ©...
Page 128 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 GPS 400W Panel – SBAS SELECTION Settings Figure 219 (Sheet 1 of 1) 34-50-10 EFFECTIVITY: 0001-0262, POST SB 500-99-005; AND 0266-0267; ALL POST MB 500-31-018 CONFIG A Page 230 Sep 30/20...
Page 129 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 GPS 400W Panel – DATA FIELD CONFIGURATION Settings Figure 220 (Sheet 1 of 1) 34-50-10 EFFECTIVITY: 0001-0262, POST SB 500-99-005; AND 0266-0267; ALL POST MB 500-31-018 CONFIG A Page 231 Sep 30/20 ©...
Page 130 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 RS-232 L. ACS RS-422 STANDARD CONFIGURATION LEFT RS-232 GPS 400W L. ACS RS-422 RS-232 SHADIN CONVERTER GPS 400W (STANDBY ALTITUDE/AIRSPEED OPTION) GPS 400W – Standby Altitude/Airspeed Indication Option Figure 221 (Sheet 1 of 1) 34-50-10 EFFECTIVITY: 0001-0262, POST SB 500-99-005;...
Page 131 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 GPS 3- MAINTENANCE PRACTICES AMM-34-50-10-051-B-801 1. General A. The purpose of this task is to provide instructions for configuring GPS 3 (GDL 88) for use on the Eclipse Model 500 aircraft.
Page 132 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (5) Connect the USB connector of the GDL 88 software download cable, 87-125272-1001, to the PC. (6) Turn the power supply on. (7) Run the GDL 8X Install Tool. NOTE: USB drivers automatically install and it might take a few minutes before Install Tool can connect to GDL 88.
Page 133 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (20) Turn off power supply. (21) Disconnect GDL 88 from backplate. 5. Job Close-Up SUBTASK AMM-34-50-10-051-B-921-002 A. Remove all tools, equipment, and unwanted material from work area. 34-50-10 EFFECTIVITY: ALL POST MB 500-34-030...
Page 134 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 GDL 8x Install Tool: Unit Information Figure 201 (Sheet 1 of 1) 34-50-10 EFFECTIVITY: ALL POST MB 500-34-030 CONFIG B Page 204 Sep 30/20 © 2020 Eclipse Aerospace, Inc.
Page 135 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 GDL 8x Install Tool: Aircraft Configuration Figure 202 (Sheet 1 of 1) 34-50-10 EFFECTIVITY: ALL POST MB 500-34-030 CONFIG B Page 205 Sep 30/20 © 2020 Eclipse Aerospace, Inc.
Page 136 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 GDL 8x Install Tool: Antenna Configuration Figure 203 (Sheet 1 of 1) 34-50-10 EFFECTIVITY: ALL POST MB 500-34-030 CONFIG B Page 206 Sep 30/20 © 2020 Eclipse Aerospace, Inc.
Page 137 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 GDL 8x Install Tool: RS-232/RS-422 Configuration Figure 204 (Sheet 1 of 1) 34-50-10 EFFECTIVITY: ALL POST MB 500-34-030 CONFIG B Page 207 Sep 30/20 © 2020 Eclipse Aerospace, Inc.
Page 138 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 GDL 8x Install Tool: Ethernet Configuration Figure 205 (Sheet 1 of 1) 34-50-10 EFFECTIVITY: ALL POST MB 500-34-030 CONFIG B Page 208 Sep 30/20 © 2020 Eclipse Aerospace, Inc.
Page 139 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 GPS - ADJUSTMENT/TEST AMM-34-50-10-071-C-801 1. General A. This task gives procedures to do the adjustment/test of the Global Positioning System (GPS 1 & GPS 2) components. 2. Job Set-Up SUBTASK AMM-34-50-10-071-C-921-001 A.
Page 140 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 G. On the MFD ECB page, reset ECB - INTEGRATED SENSOR 1 (BATT Bus). 5. GPS 2 Test SUBTASK AMM-34-50-10-071-C-801-003 A. Do Job Set-Up. Refer to SUBTASK AMM-34-50-10-071-C-921-001. B. Do MFD Set-Up. Refer to SUBTASK AMM-34-50-10-071-C-701-001.
Page 141 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 GPS 3- REMOVAL AMM-34-50-11-001-C-801 1. General A. This task gives procedures to remove the Global Positioning System (GPS 3) unit. B. There is one GPS 3 (GDL 88) installed on the aircraft under 131 CZ-B - Floor Panel, Aft Short, Left Cabin.
Page 142 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 GPS 3- Removal/Installation Figure 401 (Sheet 1 of 1) 34-50-11 EFFECTIVITY: ALL POST MB 500-34-030 CONFIG C Page 402-Rem Sep 30/20 © 2020 Eclipse Aerospace, Inc.
Page 143 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 GPS - REMOVAL AMM-34-50-11-001-D-801 1. General A. This task gives the procedure to remove the Global Positioning System/Wide Area Augmentation System (GPS/WAAS) sensors. B. There are two GPS/WAAS sensors installed in the aircraft. Removal steps are the same for the light and right sides, unless specified.
Page 144 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 1 (x4) 6 (x4) 4(x2) 5 (x4) (ROTATED FOR CLARITY) GPS - Removal/Installation Figure 401 (Sheet 1 of 1) 34-50-11 EFFECTIVITY: ALL POST MB 500-31-007 OR MB 500-31-008 CONFIG D...
Page 145 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 GPS - INSTALLATION AMM-34-50-11-041-B-801 1. General A. This task gives procedures to install the Global Positioning System/Wide Area Augmentation System (GPS/WAAS) Garmin GPS 400W Navigator. B. There are two GPS 400W units installed on the aircraft. Installation procedures are the same for both sides and given for the left side GPS 400W unit.
Page 146 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 access hole at the bottom of the unit face. Rotate the hex tool clockwise while pressing on the left side of the bezel until the unit is firmly seated in the rack.
Page 147 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 NOTE: STRUCTURE AND EQUIPMENT REMOVED FOR CLARITY GPS - Removal/Installation Figure 401 (Sheet 1 of 1) 34-50-11 EFFECTIVITY: 0001-0262 POST SB 500-99-005; AND 0266-0267; ALL POST MB 500-31-018 CONFIG B...
Page 148 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 THIS PAGE INTENTIONALLY LEFT BLANK 34-50-11 EFFECTIVITY: 0001-0262 POST SB 500-99-005; AND 0266-0267; ALL POST MB 500-31-018 CONFIG B Page 404-Inst Sep 30/20 © 2020 Eclipse Aerospace, Inc.
Page 149 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 GPS 3 - INSTALLATION AMM-34-50-11-041-C-801 1. General A. This task gives procedures to install the Global Positioning System (GPS 3) unit. B. There is one GPS 3 installed on the aircraft under 131 CZ-B - Floor Panel, Aft Short, Left Cabin.
Page 150 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 GPS 3 - Removal/Installation Figure 401 (Sheet 1 of 1) 34-50-11 EFFECTIVITY: ALL POST MB 500-34-030 CONFIG C Page 402-Inst Sep 30/20 © 2020 Eclipse Aerospace, Inc.
Page 151 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 GPS - INSTALLATION AMM-34-50-11-041-801-D 1. General A. This task gives the procedure to install the Global Positioning System/Wide Area Augmentation System (GPS/WAAS) sensors. B. There are two GPS/WAAS sensors installed in the aircraft. Installation steps are the same for the light and right sides, unless specified.
Page 152 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 H. Do an adjustment/test of the GPS system. Refer to AMM-34-50-10-071-801 – GPS - Adjustment/Test. 4. Job Close-Up SUBTASK AMM-34-50-11-041-D-921-002 A. Remove all tools, equipment, and unwanted material from the work area.
Page 153 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 1 (x4) 6 (x4) 4(x2) 5 (x4) (ROTATED FOR CLARITY) GPS - Removal/Installation Figure 401 (Sheet 1 of 1) 34-50-11 EFFECTIVITY: ALL POST MB 500-31-007 OR MB 500-31-008 CONFIG D...
Page 154 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 THIS PAGE INTENTIONALLY LEFT BLANK 34-50-11 EFFECTIVITY: ALL POST MB 500-31-007 OR MB 500-31-008 CONFIG D Page 404-Inst Sep 30/20 © 2020 Eclipse Aerospace, Inc.
Page 155 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 GPS 3 MOUNT - REMOVAL AMM-34-50-13-001-801 1. General A. This task gives procedures to remove the Global Positioning System (GPS 3) mount. B. There is one GPS 3 mount installed under the baggage floor panel.
Page 156 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 1 (X4) GPS 3 Mount - Removal/Installation Figure 401 (Sheet 1 of 2) 34-50-13 EFFECTIVITY: ALL POST MB 500-34-030 Page 402-Rem Sep 30/20 © 2020 Eclipse Aerospace, Inc.
Page 157 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 7 (X2) GPS 3 Mount - Removal/Installation Figure 401 (Sheet 2 of 2) 34-50-13 EFFECTIVITY: ALL POST MB 500-34-030 Page 403-Rem Sep 30/20 © 2020 Eclipse Aerospace, Inc.
Page 158 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 THIS PAGE INTENTIONALLY LEFT BLANK 34-50-13 EFFECTIVITY: ALL POST MB 500-34-030 Page 404-Rem Sep 30/20 © 2020 Eclipse Aerospace, Inc.
Page 159 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 GPS 3 MOUNT - INSTALLATION AMM-34-50-13-041-801 1. General A. This task gives the procedures to install the Global Positioning System (GPS 3) mount. B. There is one GPS 3 mount installed under the baggage floor panel.
Page 160 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 1 (X4) GPS 3 Mount - Removal/Installation Figure 401 (Sheet 1 of 2) 34-50-13 EFFECTIVITY: ALL POST MB 500-34-030 Page 402-Inst Sep 30/20 © 2020 Eclipse Aerospace, Inc.
Page 161 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 7 (X2) GPS 3 Mount - Removal/Installation Figure 401 (Sheet 2 of 2) 34-50-13 EFFECTIVITY: ALL POST MB 500-34-030 Page 403-Inst Sep 30/20 © 2020 Eclipse Aerospace, Inc.
Page 162 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 THIS PAGE INTENTIONALLY LEFT BLANK 34-50-13 EFFECTIVITY: ALL POST MB 500-34-030 Page 404-Inst Sep 30/20 © 2020 Eclipse Aerospace, Inc.
Page 163 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 GPS 2 ANTENNA SPLITTER - REMOVAL AMM-34-50-14-001-801 1. General A. This task gives procedures to remove the GPS 2 Antenna Splitter. B. There is one GPS 2 Antenna Splitter installed on the aircraft under 231 NZ - Floor Panel, Baggage Compartment.
Page 164 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 2 (X2) 3 (X3) (SOME STRUCTURE REMOVED FOR CLARITY) GPS 2 Antenna Splitter - Removal/Installation Figure 401 (Sheet 1 of 1) 34-50-14 EFFECTIVITY: ALL POST MB 500-34-030 Page 402-Rem Sep 30/20...
Page 165 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 GPS 2 ANTENNA SPLITTER - INSTALLATION AMM-34-50-14-041-801 1. General A. This task gives procedures to install the GPS 2 Antenna Splitter. B. There is one GPS 2 Antenna Splitter installed on the aircraft under 231 NZ - Floor Panel, Baggage Compartment.
Page 166 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 2 (X2) 3 (X3) (SOME STRUCTURE REMOVED FOR CLARITY) GPS 2 Antenna Splitter - Removal/Installation Figure 401 (Sheet 1 of 1) 34-50-14 EFFECTIVITY: ALL POST MB 500-34-030 Page 402-Inst Sep 30/20...
Page 167 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 TRANSPONDER - DESCRIPTION AND OPERATION AMM-34-50-20-081-C-801 1. Introduction A. Standard Transponder System with or without Extended Squitter: (1) The standard transponder system provides aircraft identification (Mode S), and altitude (Mode C) information to Air Traffic Control.
Page 168 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 3. Operation SUBTASK AMM-34-50-20-081-C-871-002 A. Standard Transponder System: The two transponder units located behind the left and right PFDs provide identification information (Modes A and S) and altitude reporting information (Mode C).
Page 169 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 TRANSPONDER - DESCRIPTION AND OPERATION AMM-34-50-20-081-D-801 1. Introduction A. Standard Transponder System: (1) The standard transponder system provides aircraft identification (Mode S), altitude (Mode C), and Automatic Dependent Surveillance Broadcast (ADS-B) OUT information to Air Traffic Control.
Page 170 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 C. ADS-B Function The Extended Squitter enabled transponders provide the capabilities of ADS-B technology, which improves situational awareness and flight safety. The ADS-B OUT function is an option and may be activated through the MFD software key pertinent to a specific aircraft registration number.
Page 171 B. If installed on aircraft, remove affected transponder from aircraft. Refer to AMM-34-50-21-001-801 – Transponder - Removal C. Obtain the transponder configuration files from Eclipse Service Engineering. One of the configuration files sets transponder configuration to factory defaults; another file enables the ADS-B OUT function and configures the associated parameters to the required values.
Page 172 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (1) On the PC with Windows XP OS only, open Windows Hyper Terminal app (All Programs>Accessories>Communications>Hyper Terminal) and enter xpdr_configuration as name for the connection. Refer to Fig. 202, Sheet (2) Enter the following connection properties: Refer to Fig.
Page 173 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 5. Job Close-Up SUBTASK AMM-34-50-20-051-921-002 A. Disconnect Harness Assy, GTX-33 Test (87-124598-1001) from Power Supply and Transponder. 34-50-20 EFFECTIVITY: ALL POST MB 500-31-018 OR MB 500-34-030 Page 203 Sep 30/20...
Page 174 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 Test Setup Figure 201 (Sheet 1 of 1) 34-50-20 EFFECTIVITY: ALL POST MB 500-31-018 OR MB 500-34-030 Page 204 Sep 30/20 © 2020 Eclipse Aerospace, Inc.
Page 175 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 Hyper Terminal – New Connection Figure 202 (Sheet 1 of 4) 34-50-20 EFFECTIVITY: ALL POST MB 500-31-018 OR MB 500-34-030 Page 205 Sep 30/20 © 2020 Eclipse Aerospace, Inc.
Page 176 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 Hyper Terminal – Connection Properties Figure 202 (Sheet 2 of 4) 34-50-20 EFFECTIVITY: ALL POST MB 500-31-018 OR MB 500-34-030 Page 206 Sep 30/20 © 2020 Eclipse Aerospace, Inc.
Page 177 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 Hyper Terminal – Comm Demo Figure 202 (Sheet 3 of 4) 34-50-20 EFFECTIVITY: ALL POST MB 500-31-018 OR MB 500-34-030 Page 207 Sep 30/20 © 2020 Eclipse Aerospace, Inc.
Page 178 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 Hyper Terminal – Send File Figure 202 (Sheet 4 of 4) 34-50-20 EFFECTIVITY: ALL POST MB 500-31-018 OR MB 500-34-030 Page 208 Sep 30/20 © 2020 Eclipse Aerospace, Inc.
Page 179 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 TRANSPONDER - ADJUSTMENT/TEST AMM-34-50-20-071-A-801 1. General A. This task gives procedures to do the adjustment/test of the transponder components. • An adjustment/test is only required for the transponder that is being installed. The...
Page 180 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 3. Job Set-Up with UC-584 Antenna Couplers SUBTASK AMM-34-50-20-071-921-001-A Refer to Fig. 501. A. Make aircraft safe for maintenance. Refer to AMM-20-00-01-051-801 – Make Safe For Maintenance. B. If on jacks, refer to AMM-07-10-00-051-801 –...
Page 181 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (1) Place Antenna Coupler over the antenna , guiding antenna in to the slot on the bottom of the coupler. (2) Lock Antenna Coupler into place by pushing lever on the side of the coupler into a down and locked position.
Page 182 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 4. Procedure with UC-584 Antenna Couplers SUBTASK AMM-34-50-20-071-A-701-001 A. Do adjustment/test of the Transponder System as follows: (1) Perform job setup, refer to SUBTASK AMM-34-50-20-071-A-921-001-B. (2) Push ECB BY SYSTEM soft key. Scroll to FLT CTRLS using outer knob. Push inner knob to select.
Page 183 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (c) Press XPDR SQWK. (d) Using the keyboard numbers, set the code to 1200. (e) Press Enter. • CODE status box on the left PFD shows 1200. C. Transponder-1 MODE A,C,S Test using Transponder Test Set, IFR6000 (1) Power Up: Press the POWER Key to power the Test Set.
Page 184 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (16) Press IDNT key on the Pilot’s keyboard. • IDENT is displayed on Transponder Test Set, IFR6000. NOTE: IDENT disappears from the IFR test set in approximately 20 seconds. (17) Press IDNT key on the Copilot’s keyboard (If Installed).
Page 185 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (10) Press STOP TEST button. (11) Repeat until all FAILED tests have been completed. (12) Press Return button on IFR 6000 to return to XPDR-AUTO TEST screen appears. • A PASS message should appear.
Page 186 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (3) On Transponder Test Set, IFR6000, select XPDR button. On CONFIG line, scroll using up/down buttons to GENERIC MODE S. Press Return button. (4) On Transponder Test Set, IFR6000, select Run Test. Expected results are as follows: •...
Page 187 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 5. Job Set-Up with IFR-6000 Test Antenna SUBTASK AMM-34-50-20-071-A-921-001-B A. Make aircraft safe for maintenance. Refer to AMM-20-00-01-051-801 – Make Safe For Maintenance. B. If on jacks, refer to AMM-07-10-00-051-801 – Jacking - Maintenance Practices AMM-08-20-00-051-801 –...
Page 188 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 6. Procedure with IFR-6000 Test Set Antenna SUBTASK AMM-34-50-20-071-A-701-001-A A. Do adjustment/test of the Transponder System as follows: (1) Perform job setup, refer to SUBTASK AMM-34-50-20-071-A-921-001-B. (2) Push ECB BY SYSTEM soft key. Scroll to FLT CTRLS using outer knob. Push inner knob to select.
Page 189 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (c) Press XPDR SQWK. (d) Using the keyboard numbers, set the code to 1200. (e) Press Enter. • CODE status box on the left PFD shows 1200. C. Transponder-1 MODE A,C,S Test using Transponder Test Set, IFR6000 (2) Power up the Transponder Test Set, IFR6000 and press SET UP button on the test set.
Page 190 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 • A PASS message should be displayed. NOTE: If POWER/FREQ test fails, after pressing RUN TEST, adjust antenna until PASS message appears. Stop adjusting antenna as soon as PASS message appears and press STOP TEST button.
Page 191 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (2) Power up the Transponder Test Set, IFR6000 (if required), and press SET UP button one time on the test set, and press XPDR to display AUTO TEST until XPDR-AUTO TEST.
Page 192 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 • A PASS message should appear. NOTE: If POWER/FREQ test fails, after pressing RUN TEST, adjust Antenna until PASS message appears. Stop adjusting antenna as soon as PASS message appears and press STOP TEST button. This test performs a LIVE update of the dBm values needed to achieve a PASS message for test.
Page 193 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (3) On Transponder Test Set, IFR6000, select XPDR button. On CONFIG line, scroll using up/down buttons to GENERIC MODE S. Press Return button. (4) On Transponder Test Set, IFR6000, select Run Test. Expected results are as follows: •...
Page 194 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 F. Disconnect external power. Refer to AMM-24-40-00-051-801 – External Power - Maintenance Practices. G. If all other maintenance is complete, return aircraft to service. Refer to AMM-20-00-02-051-801 – Return To Service (After Maintenance).
Page 195 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 TRANSPONDER 1 TRANSPONDER 2 Transponder - Adjustment/Test Figure 501 (Sheet 1 of 1) 34-50-20 EFFECTIVITY: 0001-0104, 0113-0115, 0120, 0123-0124 PRE SB 500-99-002 AND SB 500-99-005 CONFIG A Page 517 Sep 30/20...
Page 196 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 HANDLE ANTENNA PATTERN BEAMWIDTH TNG CONNECTION ± 20° VERTICAL ± 25° HORIZONTAL CABLE TO TEST SET FLAT ANTENNA BUILDING BUILDING FOR OPTIMUM PERFORMANCE IFR-6000 TEST BUILDINGS, VEHICLES, AND OTHER SET AND AIRCRAFT SHOULD BE LOCATED AT ANTENNA.
Page 197 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 TRANSPONDER - ADJUSTMENT/TEST AMM-34-50-20-071-B-801 1. General A. This task gives procedures to do the adjustment/test of the: • Dual Standard (Non-Diversity) Transponder System and components (or) Optional Dual Diversity Transponder System and components.
Page 198 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 2. Equipment and Materials Table 502. Special Tools and Equipment Name and Part Number Transponder Test Set (Aeroflex, IFR6000) or equivalent UC-584 Universal Transponder Antenna Coupler | Dual Antenna Kit (Viavi 112349)[1] Weight-on-Wheels (WOW) Box (EAI, 87-117390-1001) or AMC 2.4.01 (or higher).
Page 199 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 3. Job Set-Up with UC-584 Antenna Coupler SUBTASK AMM-34-50-20-071-B-921-001-A Refer to Fig. 501. A. Make aircraft safe for maintenance. Refer to AMM-20-00-01-051-801 – Make Safe For Maintenance. B. If on jacks, refer to AMM-07-10-00-051-801 –...
Page 200 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (1) Place Antenna Coupler over the antenna , guiding antenna in to the slot on the bottom of the coupler. (2) Lock Antenna Coupler into place by pushing lever on the side of the coupler into a down and locked position.
Page 201 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 4. Transponder–1 Adjustment/Test (Standard System) with UC-584 Antenna Coupler SUBTASK AMM-34-50-20-071-B-701-001-A A. Begin adjustment/test as follows: (1) Perform Job Set-Up with UC-584 Antenna Coupler, refer to SUBTASK AMM-34-50-20-071-B-921-001-A. (2) Use the small rotary knob on the left PFD to select XPDR page.
Page 202 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 • RF PORT: DIR W/COUPLER • CPL CABLE LOSS: Set to loss found on cable. • COUPLER LOSS: Set to loss found on coupler. • UUT ADDRESS: AUTO • MANUAL AA: Ignore •...
Page 203 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (12) On MFD, press SYS along bottom of MFD. Use the small lower knob on the MFD to scroll to the SETUP page. On the SETUP page, press the SETTINGS softkey to bring up the SETTINGS page.
Page 204 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 5. Transponder–2 Adjustment/Test (Standard System) with UC-584 Antenna Coupler SUBTASK AMM-34-50-20-071-B-701-002-A A. Begin adjustment/test as follows: (1) Perform Job Set-Up with UC-584 Antenna Coupler, refer to SUBTASK AMM-34-50-20-071-B-921-001-A. (2) Re-align the Transponder Test Set, IFR6000 antenna to point at the aircraft’s lower Transponder–2 antenna (bottom of the center cabin/fuselage).
Page 205 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (6) With GENERIC MODE S highlighted, push RETURN soft key to confirm selection. This will also cause a return to the XPDR-AUTO TEST page. (7) Set the WOW Box Switches to W-off-W (airborne).
Page 206 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (19) Set XPDR 2 to STANDBY MODE. 6. Diversity Transponder–1 Adjustment/Tests with UC-584 Antenna Coupler SUBTASK AMM-34-50-20-071-B-701-003-A A. Begin adjustment/test as follows: (1) Install Antenna Clamp and Shield Assembly (part of Transponder Test Set IFR 6000) on lower transponder antenna (bottom of the center cabin/fuselage), in accordance with instructions in IFR 6000 Ramp Test Set Operation Manual.
Page 207 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (3) Make sure that the selected transponder is in Standby Mode. (4) Push CODE soft key on left PFD and enter the transponder code used for this test or 1200.
Page 208 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 • “FLT ID” = same as tail number • DF17 DETECTED” = YES (IF ADS-B OUT IS INSTALLED) / NO (IF ADS-B OUT IS NOT INSTALLED) • “AA” = ICAO code assigned to this aircraft/tail number (8 digit number in parenthesis) •...
Page 209 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (6) Push CONFIG soft key to display the XPDR-CONFIG SCREEN page. (7) On the XPDR-CONFIG SCREEN, scroll to GENERIC MODE S using the UP/Down DATA keys. (8) With GENERIC MODE S highlighted, push RETURN soft key to confirm selection.
Page 210 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 7. Diversity Transponder–2 Adjustment/Tests with UC-584 Antenna Coupler SUBTASK AMM-34-50-20-071-B-701-004-A A. Begin adjustment/test as follows: (1) Install Antenna Clamp and Shield Assembly (part of Transponder Test Set IFR 6000) on lower transponder antenna (bottom of the center cabin/fuselage), in accordance with instructions in IFR 6000 Ramp Test Set Operation Manual.
Page 211 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (4) Push CODE soft key on left PFD and enter the transponder code used for this test or 1200. C. Diversity Transponder-2 MODE A,C,S Test using Transponder Test Set, IFR6000 (Upper Antenna) (1) Power up the Transponder Test Set (IFR 6000).
Page 212 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 • “DF17 DETECTED” = YES (IF ADS-B OUT IS INSTALLED) / NO (IF ADS-B OUT IS NOT INSTALLED) • “FLT ID” = same as tail number • “AA” = ICAO code assigned to this aircraft/tail number (8 digit number in parenthesis) •...
Page 213 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (6) Install Antenna Clamp and Shield Assembly (part of Transponder Test Set IFR 6000) on upper transponder antenna (top of the center cabin/fuselage), in accordance with instructions in IFR 6000 Ramp Test Set Operation Manual.
Page 214 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 8. Job Set-Up with IFR-6000 Antenna SUBTASK AMM-34-50-20-071-B-921-001-B A. Make aircraft safe for maintenance. Refer to AMM-20-00-01-051-801 – Make Safe For Maintenance. B. If on jacks, refer to AMM-07-10-00-051-801 – Jacking - Maintenance Practices AMM-08-20-00-051-801 –...
Page 215 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 9. Transponder–1 Adjustment/Test (Standard System) with IFR-6000 Antenna SUBTASK AMM-34-50-20-071-B-701-001-B A. Begin adjustment/test as follows: (1) Perform job setup, refer to SUBTASK AMM-34-50-20-071-B-921-001-B. (2) Re-align the Transponder Test Set, IFR6000 antenna to point at the aircraft’s Transponder–1 antenna (top of the center cabin/fuselage).
Page 216 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (2) On the Transponder Test Set (IFR 6000)’s SETUP-XPDR page, use NEXT PARAM or PREV PARAM soft keys to select each parameter, and the “arrow” DATA keys to set the values listed below.
Page 217 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (9) Top ERP should be between 48 to 60 dBm and MTL should be between -68 to -80 dBm to PASS. NOTE: If values are obtained and any of the individual tests FAIL during AUTO TEST, press TEST LIST button on IFR 6000 and using UP/DOWN buttons scroll to the specific Failed test(s).
Page 218 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (14) On the MFD, scroll to the SETUP tab, press the SENSOR Soft Key. (15) Set the ADC PFD source selection from AUTO to ADC 2. (16) On the IFR 6000, press the XPDR button once. Once XPDR – ALT ENCODER is displayed, press the SOURCE SELECT Soft Key until SOURCE - XPDR is displayed.
Page 219 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 10. Transponder–2 Adjustment/Test (Standard System) with IFR-6000 Antenna SUBTASK AMM-34-50-20-071-B-701-002-B A. Begin adjustment/test as follows: (1) Perform job setup, refer to SUBTASK AMM-34-50-20-071-B-921-001-B. (2) Re-align the Transponder Test Set, IFR6000 antenna to point at the aircraft’s lower Transponder–2 antenna (bottom of the center cabin/fuselage).
Page 220 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 • DIVERSITY TEST: OFF • PWR LIM: FAR 43 • CHECK CAP: YES (3) Push XPDR button to go to the XPDR-AUTO TEST page. (4) Push CONFIG soft key to display the XPDR-CONFIG SCREEN page.
Page 221 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 • “VS” = IN-AIR (11) On MFD, press SYS along bottom of MFD. Use the small lower knob on the MFD to scroll to the SETUP page. On the SETUP page, press the SETTINGS softkey to bring up the SETTINGS page.
Page 222 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 11. Diversity Transponder–1 Adjustment/Tests with IFR-6000 Antenna SUBTASK AMM-34-50-20-071-B-701-003-B A. Begin adjustment/test as follows: (1) Install Antenna Clamp and Shield Assembly (part of Transponder Test Set IFR 6000) on lower transponder antenna (bottom of the center cabin/fuselage), in accordance with instructions in IFR 6000 Ramp Test Set Operation Manual.
Page 223 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (4) Push CODE soft key on left PFD and enter the transponder code used for this test or 1200. (5) Make sure the selected transponder is in Standby Mode. C. Diversity Transponder-1 MODE A,C,S Test using Transponder Test Set, IFR6000 (Upper Antenna) (1) Power up the Transponder Test Set (IFR 6000).
Page 224 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (9) Top ERP should be between 48 to 60 dBm and MTL should be between -68 to -80 dBm to PASS. NOTE: If values are obtained and any of the individual tests FAIL during AUTO TEST, press TEST LIST button on IFR 6000 and using UP/DOWN buttons scroll to the specific Failed test(s).
Page 225 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (12) On the MFD, scroll to the SETUP tab, press the SENSOR Soft Key. Set the ADC PFD source selection from AUTO to ADC 2. (13) On the IFR 6000, press the XPDR button once.
Page 226 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (10) Bottom ERP should be between 48 to 60 dBm and MTL should be between -68 to -80 dBm to PASS. NOTE: If values are obtained and any of the individual tests FAIL during AUTO TEST, press TEST LIST button on IFR 6000 and using UP/DOWN buttons scroll to the specific Failed test(s).
Page 227 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 12. Diversity Transponder–2 Adjustment/Tests with IFR-6000 Antenna SUBTASK AMM-34-50-20-071-B-701-004-B A. Begin adjustment/test as follows: (1) Install Antenna Clamp and Shield Assembly (part of Transponder Test Set IFR 6000) on lower transponder antenna (bottom of the center cabin/fuselage), in accordance with instructions in IFR 6000 Ramp Test Set Operation Manual.
Page 228 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (4) Push CODE soft key on left PFD and enter the transponder code used for this test or 1200. C. Diversity Transponder-2 MODE A,C,S Test using Transponder Test Set, IFR6000 (Upper Antenna) (1) Power up the Transponder Test Set (IFR 6000).
Page 229 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (9) Top ERP should be between 48 to 60 dBm and MTL should be between -68 to -80 dBm to PASS. NOTE: If values are obtained and any of the individual tests FAIL during AUTO TEST, press TEST LIST button on IFR 6000 and using UP/DOWN buttons scroll to the specific Failed test(s).
Page 230 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (12) On the MFD, scroll to the SETUP tab, press the SENSOR Soft Key. Set the ADC PFD source selection from AUTO to ADC 2. (13) On the IFR 6000, press the XPDR button once.
Page 231 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 • CHECK CAP: YES (5) Push XPDR button to go to the XPDR-AUTO TEST page. (6) Push CONFIG soft key to display the XPDR-CONFIG SCREEN page. (7) On the XPDR-CONFIG SCREEN, scroll to GENERIC MODE S using the UP/Down DATA keys.
Page 232 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 • ECB - NOSE LDG GEAR (L AFT Bus) • ECB - L MAIN LDG GEAR (L AFT Bus) • ECB - R MAIN LDG GEAR (L AFT Bus) D. Scroll to ENGINE using outer knob. Press inner knob to select. Scroll to the listed ECB using outer knob and highlight.
Page 233 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 TRANSPONDER 1 TRANSPONDER 2 Transponder - Adjustment/Test Figure 501 (Sheet 1 of 1) 34-50-20 EFFECTIVITY: 0001-0104, 0113-0115, 0120, 0123-0124 POST SB 500-99-002; AND 0105-0112, CONFIG B 0116-0119, 0121-0122, 0125-0262 PRE SB...
Page 234 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 HANDLE ANTENNA PATTERN BEAMWIDTH TNG CONNECTION ± 20° VERTICAL ± 25° HORIZONTAL CABLE TO TEST SET FLAT ANTENNA BUILDING BUILDING FOR OPTIMUM PERFORMANCE IFR-6000 TEST BUILDINGS, VEHICLES, AND OTHER SET AND AIRCRAFT SHOULD BE LOCATED AT ANTENNA.
Page 235 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 TRANSPONDER - ADJUSTMENT/TEST AMM-34-50-20-071-C-801 1. General A. This task gives procedures to do the adjustment/test of the: • Dual Standard (Non-Diversity) Transponder System and components or Dual Diversity Transponder System and components.
Page 236 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 System Test Procedures ADS-B Out System Tests ADS-B Out Test Set-Up SUBTASK AMM-34-50-20-071- C-701-005 ADS-B Out Functional Test: SUBTASK AMM-34-50-20-071- C-701-006 ADS-B Out Parameter Test: SUBTASK AMM-34-50-20-071- C-701-007 ADS-B Out Fail Indicator Functional Test:...
Page 237 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 3. Job Set-Up with UC-584 Antenna Coupler SUBTASK AMM-34-50-20-071-C-921-001-A * * * 0001-0104, 0113-0115, 0120, 0123-0124 POST SB 500-99-002; 0105-0112, 0116-0119, 0121-0122, 0125-0265 POST SB 500-99-005; AND 0266-0267; ALL POST MB 500-31-016, MB 500-31-018.
Page 238 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 F. Connect Antenna Coupler UC-584 to Aircraft lower Transponder Antenna as follows: (as applicable) NOTE: For Transponder–2 Adjustment/Test (1) Place Antenna Coupler over the antenna , guiding antenna in to the slot on the bottom of the coupler.
Page 239 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 4. Transponder–1 Adjustment/Test (Standard System) with UC-584 Antenna Coupler SUBTASK AMM-34-50-20-071-C-701-001-A * * * 0001-0104, 0113-0115, 0120, 0123-0124 POST SB 500-99-002; 0105-0112, 0116-0119, 0121-0122, 0125-0265 POST SB 500-99-005; AND 0266-0267; ALL POST MB 500-31-016, MB 500-31-018.
Page 240 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (1) Power up the Transponder Test Set (IFR 6000). After tester performs Self Test, push SETUP button on the test set to bring up the SETUP-XPDR page. If necessary, continue pressing SETUP button until tester cycles to SETUP-XPDR page.
Page 241 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 • “AA” = ICAO code assigned to this aircraft/tail number (8 digit number in parenthesis) • “FS” = IN-AIR • “VS” = IN-AIR (12) On MFD, press SYS along bottom of MFD. Use the small lower knob on the MFD to scroll to the SETUP page.
Page 242 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 5. Transponder–2 Adjustment/Test (Standard System) with UC-584 Antenna Coupler SUBTASK AMM-34-50-20-071-C-701-002-A * * * 0001-0104, 0113-0115, 0120, 0123-0124 POST SB 500-99-002; 0105-0112, 0116-0119, 0121-0122, 0125-0265 POST SB 500-99-005; AND 0266-0267; ALL POST MB 500-31-016, MB 500-31-018.
Page 243 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (6) With GENERIC MODE S highlighted, push RETURN soft key to confirm selection. This will also cause a return to the XPDR-AUTO TEST page. (7) Set the WOW Box Switches to W-off-W (airborne).
Page 244 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (19) Set XPDR 2 to STANDBY MODE. 6. Diversity Transponder–1 Adjustment/Tests with UC-584 Antenna Coupler SUBTASK AMM-34-50-20-071-C-701-003-A * * * 0001-0104, 0113-0115, 0120, 0123-0124 POST SB 500-99-002; 0105-0112, 0116-0119, 0121-0122, 0125-0265 POST SB 500-99-005; AND 0266-0267; ALL POST MB 500-31-016, MB 500-31-018.
Page 245 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (1) Use the small rotary knob on the left PFD to select XPDR page. NOTE: The XPDR select page times out and switches back to the COM page after 30 seconds. Select XPDR page from time to time during this test.
Page 246 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 • “C ALT” = left PFD altitude indication +/- 100 ft. • “S CODE” = ICAO code assigned to this aircraft/tail number • “TAIL” = tail number assigned to this aircraft •...
Page 247 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (3) Install Antenna Clamp and Shield Assembly (part of Transponder Test Set IFR 6000) on upper transponder antenna (top of the center cabin/fuselage), in accordance with instructions in IFR 6000 Ramp Test Set Operation Manual.
Page 248 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 7. Diversity Transponder–2 Adjustment/Tests with UC-584 Antenna Coupler SUBTASK AMM-34-50-20-071-C-701-004-A * * * 0001-0104, 0113-0115, 0120, 0123-0124 POST SB 500-99-002; 0105-0112, 0116-0119, 0121-0122, 0125-0265 POST SB 500-99-005; AND 0266-0267; ALL POST MB 500-31-016, MB 500-31-018.
Page 249 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (2) Push ACTIVE soft key (upper right button) on the left PFD to select D-XPDR2. (3) Make sure that D-XPDR2 is in Standby Mode. (4) Push CODE soft key on left PFD and enter the transponder code used for this test or 1200.
Page 250 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 • “DF17 DETECTED” = YES (IF ADS-B OUT IS INSTALLED) / NO (IF ADS-B OUT IS NOT INSTALLED) • “FLT ID” = same as tail number • “AA” = ICAO code assigned to this aircraft/tail number (8 digit number in parenthesis) •...
Page 251 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (6) Install Antenna Clamp and Shield Assembly (part of Transponder Test Set IFR 6000) on upper transponder antenna (top of the center cabin/fuselage), in accordance with instructions in IFR 6000 Ramp Test Set Operation Manual.
Page 252 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 8. Job Set-Up with IFR-6000 Test Set Antenna SUBTASK AMM-34-50-20-071-C-921-001 * * * 0001-0104, 0113-0115, 0120, 0123-0124 POST SB 500-99-002; 0105-0112, 0116-0119, 0121-0122, 0125-0265 POST SB 500-99-005; AND 0266-0267; ALL POST MB 500-31-016, MB 500-31-018.
Page 253 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 9. Transponder-1 Adjustment/Test (Standard System) with IFR-6000 Test Set Antenna SUBTASK AMM-34-50-20-071-C-701-001-B * * * 0001-0104, 0113-0115, 0120, 0123-0124 POST SB 500-99-002; 0105-0112, 0116-0119, 0121-0122, 0125-0265 POST SB 500-99-005; AND 0266-0267 A.
Page 254 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (1) Power up the Transponder Test Set (IFR 6000). After tester performs Self Test, push SETUP button on the test set to bring up the SETUP-XPDR page. If necessary, continue pressing SETUP button until tester cycles to SETUP-XPDR page.
Page 255 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (9) Top ERP should be between 48 to 60 dBm and MTL should be between -68 to -80 dBm to PASS. NOTE: If values are obtained and any of the individual tests FAIL during AUTO TEST, press TEST LIST button on IFR 6000 and using UP/DOWN buttons scroll to the specific Failed test(s).
Page 256 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (b) The “ICAO 24-BIT (OCT)” number matches the “AA” ICAO 24-bit code displayed on the IFR 6000 (above). NOTE: If the aircraft’s registration number and/or ICAO 24-bit (octal) number are not present on the MFD’s SETTINGS page, the Aircraft Configuration...
Page 257 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 10. Transponder-2 Adjustment/Test (Standard System) with IFR-6000 Test Set Antenna SUBTASK AMM-34-50-20-071-C-701-002-B * * * 0001-0104, 0113-0115, 0120, 0123-0124 POST SB 500-99-002; 0105-0112, 0116-0119, 0121-0122, 0125-0265 POST SB 500-99-005; AND 0266-0267 A.
Page 258 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 • MANUAL AA: Ignore • DIVERSITY TEST: OFF • PWR LIM: FAR 43 • CHECK CAP: YES (3) Push XPDR button to go to the XPDR-AUTO TEST page. (4) Push CONFIG soft key to display the XPDR-CONFIG SCREEN page.
Page 259 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 • “FS” = IN-AIR • “VS” = IN-AIR (11) On MFD, press SYS along bottom of MFD. Use the small lower knob on the MFD to scroll to the SETUP page. On the SETUP page, press the SETTINGS softkey to bring up the SETTINGS page.
Page 260 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 11. Diversity Transponder-1 Adjustment/Tests with IFR-6000 Test Set Antenna SUBTASK AMM-34-50-20-071-C-701-003-B * * * 0001-0104, 0113-0115, 0120, 0123-0124 POST SB 500-99-002; 0105-0112, 0116-0119, 0121-0122, 0125-0265 POST SB 500-99-005; AND 0266-0267 A.
Page 261 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (3) Make sure that the selected transponder is in Standby Mode. (4) Push CODE soft key on left PFD and enter the transponder code used for this test or 1200.
Page 262 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (9) Top ERP should be between 48 to 60 dBm and MTL should be between -68 to -80 dBm to PASS. NOTE: If values are obtained and any of the individual tests FAIL during AUTO TEST, press TEST LIST button on IFR 6000 and using UP/DOWN buttons scroll to the specific Failed test(s).
Page 263 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (12) On the MFD, scroll to the SETUP tab, press the SENSOR Soft Key. Set the ADC PFD source selection from AUTO to ADC 2. (13) On the IFR 6000, press the XPDR button once.
Page 264 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (10) ERP should be between 48 to 60 dBm and MTL should be between -68 to -80 dBm to PASS. NOTE: If values are obtained and any of the individual tests FAIL during AUTO TEST, press TEST LIST button on IFR 6000 and using UP/DOWN buttons scroll to the specific Failed test(s).
Page 265 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 12. Diversity Transponder-2 Adjustment/Tests with IFR-6000 Test Set Antenna SUBTASK AMM-34-50-20-071-C-701-004-B * * * 0001-0104, 0113-0115, 0120, 0123-0124 POST SB 500-99-002; 0105-0112, 0116-0119, 0121-0122, 0125-0265 POST SB 500-99-005; AND 0266-0267 A.
Page 266 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (3) Make sure that D-XPDR2 is in Standby Mode. (4) Push CODE soft key on left PFD and enter the transponder code used for this test or 1200. C. Diversity Transponder-2 MODE A,C,S Test using Transponder Test Set, IFR6000 (Upper Antenna) (1) Power up the Transponder Test Set (IFR 6000).
Page 267 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (9) Top ERP should be between 48 to 60 dBm and MTL should be between -68 to -80 dBm to PASS. NOTE: If values are obtained and any of the individual tests FAIL during AUTO TEST, press TEST LIST button on IFR 6000 and using UP/DOWN buttons scroll to the specific Failed test(s).
Page 268 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (12) On the MFD, scroll to the SETUP tab, press the SENSOR Soft Key. Set the ADC PFD source selection from AUTO to ADC 2. (13) On the IFR 6000, press the XPDR button once.
Page 269 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 • CHECK CAP: YES (5) Push XPDR button to go to the XPDR-AUTO TEST page. (6) Push CONFIG soft key to display the XPDR-CONFIG SCREEN page. (7) On the XPDR-CONFIG SCREEN, scroll to GENERIC MODE S using the UP/Down DATA keys.
Page 270 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 13. ADS-B Out System Test SUBTASK AMM-34-50-20-071-C-701-005 * * * ALL POST MB 500-31-016, MB 500-31-018 AND MB 500-34-030 A. ADS-B Out Test Set-Up (1) Power up the Transponder Test Set (IFR 6000).
Page 271 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (7) Power up the aircraft. NOTE: After initial system installation, the initial acquisition of GPS position can take up to 20 minutes. Subsequent acquisitions should take no more than 150 seconds.
Page 272 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 SURVEILLANCE STATUS = NO INFO SUBTASK AMM-34-50-20-071-C-701-007 * * * ALL POST MB 500-31-016, MB 500-31-018 AND MB 500-34-030 A. ADS-B Parameter Test (1) Do ADS-B Out Test Set-Up. Refer to...
Page 273 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 EMIT CAT = LIGHT (k) Select BDS 6,1 A/C STATUS ST1 and check the following data: AA = matches aircraft ICAO code displayed on the MFD Settings Page MODE A (4096) CODE = Entered Squawk Code from the PFD...
Page 274 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 C. Scroll to FLCS using outer knob. Press inner knob to select. Scroll to the listed ECB using outer knob and highlight. Push “RESET” Soft key. Press “CONFIRM RESET” soft key.
Page 275 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 TRANSPONDER 1 TRANSPONDER 2 Transponder - Adjustment/Test Figure 501 (Sheet 1 of 1) 34-50-20 EFFECTIVITY: NOTED CONFIG C Page 541 Sep 30/20 © 2020 Eclipse Aerospace, Inc.
Page 276 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 HANDLE ANTENNA PATTERN BEAMWIDTH TNG CONNECTION ± 20° VERTICAL ± 25° HORIZONTAL CABLE TO TEST SET FLAT ANTENNA BUILDING BUILDING FOR OPTIMUM PERFORMANCE IFR-6000 TEST BUILDINGS, VEHICLES, AND OTHER SET AND AIRCRAFT SHOULD BE LOCATED AT ANTENNA.
Page 277 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 ADS-B Fail Annunciation Figure 503 (Sheet 1 of 1) * * * ALL POST MB 500-34-030 34-50-20 EFFECTIVITY: NOTED CONFIG C Page 543 Sep 30/20 © 2020 Eclipse Aerospace, Inc.
Page 278 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 THIS PAGE INTENTIONALLY LEFT BLANK 34-50-20 EFFECTIVITY: NOTED CONFIG C Page 544 Sep 30/20 © 2020 Eclipse Aerospace, Inc.
Page 279 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 ADS-B OUT WITH GPS 3 - DESCRIPTION AND OPERATION AMM-34-50-21-081-801 1. Introduction A. The Automatic Dependent Surveillance – Broadcast Out (ADS-B Out) provides air traffic controllers with real-time position information.
Page 280 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 THIS PAGE INTENTIONALLY LEFT BLANK 34-50-21 EFFECTIVITY: ALL POST MB 500-34-030 Page 2 Sep 30/20 © 2020 Eclipse Aerospace, Inc.
Page 281 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 ADS-B - ADJUSTMENT/TEST AMM-34-50-21-071-801 1. General A. This task gives procedures to do the adjustment/test of the ADS-B. NOTE: ADS-B test is only required, if the ADS-B function is enabled.
Page 282 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (1) Place Antenna Coupler over the antenna , guiding antenna in to the slot on the bottom of the coupler. (2) Lock Antenna Coupler into place by pushing lever on the side of the coupler into a down and locked position.
Page 283 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (5) Push Antenna Coupler firmly against the aircraft skin until the black rubber gasket on the rim of the coupler is completely depressed tightly against the aircraft. G. Connect Weight On Wheels (WOW) box or Aircraft Maintenance Computer (AMC) and set switches on Box to W-On-W (on-ground).
Page 284 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 5. ADS-B System Test SUBTASK AMM-34-50-21-071-701-002 A. In order to verify ADS-B OUT function is active, perform the following test using IFR 6000 or an equivalent test set. NOTE: If IFR 6000 (or an equivalent transponder test set) does not include the ADS-B test capability, at a minimum, verification that the DF17 extended squitter format is being detected is sufficient.
Page 285 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 ADSB MON: DF17 NOTE: LAT and LON must be set to the values corresponding to the location of the test as shown on the MFD GPS Status Page. In this example, for the test set entry, the position data corresponds to the MFD displayed position data of N35⁰02.23’...
Page 286 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 6. Job Close-Up SUBTASK AMM-34-50-21-071-921-003 A. Reset the collared ECB’s. Refer to AMM-20-00-03-051-801 – Prepare Anti-Ice Systems For Maintenance. B. Scroll to FLCS using outer knob. Press inner knob to select. Scroll to the listed ECB using outer knob and highlight.
Page 287 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 TRANSPONDER 1 TRANSPONDER 2 Transponder - Adjustment/Test Figure 501 (Sheet 1 of 1) 34-50-21 EFFECTIVITY: ALL POST MB 500-31-016 Page 507 Sep 30/20 © 2020 Eclipse Aerospace, Inc.
Page 288 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 HANDLE ANTENNA PATTERN BEAMWIDTH TNG CONNECTION ± 20° VERTICAL ± 25° HORIZONTAL CABLE TO TEST SET FLAT ANTENNA BUILDING BUILDING FOR OPTIMUM PERFORMANCE IFR-6000 TEST BUILDINGS, VEHICLES, AND OTHER SET AND AIRCRAFT SHOULD BE LOCATED AT ANTENNA.
Page 289 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 TRANSPONDER - INSTALLATION AMM-34-50-21-041-801 1. General A. This task gives the procedures to install the transponder. B. There are two transponders, one is behind the left PFD and the other is behind the right PFD.
Page 290 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 4. Job Close-Up SUBTASK AMM-34-50-21-041-921-002 A. Remove all tools, equipment, and unwanted material from the work area. B. Install the following: Refer to AMM-31-10-16-041-801 – Primary Flight Display - Installation.
Page 291 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 NOTE: STRUCTURE AND EQUIPMENT REMOVED FOR CLARITY Transponder - Removal/Installation (Avio NG +1.5 display shown) Figure 401 (Sheet 1 of 1) 34-50-21 EFFECTIVITY: ALL Page 403-Inst Sep 30/20 © 2020 Eclipse Aerospace, Inc.
Page 292 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 THIS PAGE INTENTIONALLY LEFT BLANK 34-50-21 EFFECTIVITY: ALL Page 404-Inst Sep 30/20 © 2020 Eclipse Aerospace, Inc.
Page 293 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 TRANSPONDER ANTENNA RELAY - INSTALLATION AMM-34-50-23-041-801 1. General A. This task gives the procedures to install the transponder antenna relay(s). (1) Single Diversity Transponder Configuration: (a) There is one transponder lower antenna relay installed with the optional Single Diversity Transponder configuration behind the instrument panel.
Page 294 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 H. Connect the coax cable connectors 23K02P03 to the transponder lower antenna relay coax receptacle marked NO (Normally Open) If transponder upper antenna relay installed, connect the coax cable connectors...
Page 295 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 2 (x2) 3 (x2) NOTE: STRUCTURE AND EQUIPMENT REMOVED FOR CLARITY Transponder Antenna Relay - Removal/Installation (Avio NG +1.5 Display shown) Figure 401 (Sheet 1 of 1) 34-50-23 EFFECTIVITY: 0001-0104, 0113-0115, 0120, 0123-0124 POST SB 500-99-002;...
Page 296 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 THIS PAGE INTENTIONALLY LEFT BLANK 34-50-23 EFFECTIVITY: 0001-0104, 0113-0115, 0120, 0123-0124 POST SB 500-99-002; 0105-0112, 0116-0119, 0121-0122, 0125-0265 POST Page 404-Inst SB 500-99-005; AND 0266-0267 Sep 30/20 © 2020 Eclipse Aerospace, Inc.
Page 297 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 ADS-B FAIL INDICATOR - REMOVAL AMM-34-50-26-001-801 1. General A. This task gives procedures to remove the ADS-B Fail Indicator. B. There is one ADS-B Fail Indicator installed on the lower left instrument panel.
Page 298 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 (7) Remove switch body from the bracket 34-50-26 EFFECTIVITY: ALL POST MB 500-34-030 Page 402-Rem Sep 30/20 © 2020 Eclipse Aerospace, Inc.
Page 299 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 2 (x2) ADS-B Fail Indicator - Removal/Installation Figure 401 (Sheet 1 of 2) 34-50-26 EFFECTIVITY: ALL POST MB 500-34-030 Page 403-Rem Sep 30/20 © 2020 Eclipse Aerospace, Inc.
Page 300 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 ADS-B Fail Indicator - Removal/Installation Figure 401 (Sheet 2 of 2) 34-50-26 EFFECTIVITY: ALL POST MB 500-34-030 Page 404-Rem Sep 30/20 © 2020 Eclipse Aerospace, Inc.
Page 301 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 ADS-B FAIL INDICATOR - INSTALLATION AMM-34-50-26-041-801 1. General A. This task gives procedures to install the ADS-B Fail Indicator. B. There is one ADS-B Fail Indicator installed on the lower left instrument panel.
Page 302 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 4. Job Close-Up SUBTASK AMM-34-50-26-041-921-002 A. Remove all tools, equipment, and unwanted material from the work area. B. Do ADS-B FAIL Indicator Functional Test. Refer to SUBTASK AMM-34-50-20-071- C-701-008. C. If all other maintenance is complete, return the aircraft to service. Refer to AMM-20-00-02-051-801 –...
Page 303 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 2 (x2) ADS-B Fail Indicator - Removal/Installation Figure 401 (Sheet 1 of 2) 34-50-26 EFFECTIVITY: ALL POST MB 500-34-030 Page 403-Inst Sep 30/20 © 2020 Eclipse Aerospace, Inc.
Page 304 EA500 Aircraft Maintenance Manual — 06-117751 Temporary Revision No. 34-21 ADS-B Fail Indicator - Removal/Installation Figure 401 (Sheet 2 of 2) 34-50-26 EFFECTIVITY: ALL POST MB 500-34-030 Page 404-Inst Sep 30/20 © 2020 Eclipse Aerospace, Inc.

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