Eclipse EA500 Maintenance Manual Download

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GPS400W

COMBINATION

ANTENNAS

GPS400W

(ROTATED FOR CLARITY)

GPS — Combination Antenna Location

Figure 1 (Sheet 1 of 1)

EA500 Aircraft Maintenance Manual — 06-117751

Temporary Revision No. 34-21

EFFECTIVITY: 0001-0262 POST SB 500-99-005; AND

0266-0267; ALL POST MB 500-31-018

34-50-10

CONFIG B

Page 3

Sep 30/20

Summary of Contents for EA500

Page 1: ...ed MB 500 34 028 to effectivity for Pitot AOA Probe auxiliary heaters Installation Config C 34 40 50 PgBlk 1 A Description and Operation Config A Corrected effectivity 34 40 50 PgBlk 1 B Description a...

Page 2: ...Transponder Address Module Programming Procedure AMC no longer supports this task Revised Job Close Up Config A Added UC 584 antenna couplers to equipment table Renamed existing procedures to with IF...

Page 3: ...Job Set Up 34 50 23 PgBlk 401 Inst Installation Revised Job Close up test reference 34 50 26 PgBlk 401 Rem Removal Added ADS B Fail Indicator Removal procedure 34 50 26 PgBlk 401 Inst Installation Add...

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: ...t and Static Verification Test SUBTASK AMM 34 10 00 071 701 005 and Angle of Attack Test SUBTASK AMM 34 10 00 071 701 004 and AMM 24 00 00 071 801 Electrical Power Adjustment Test SUBTASK AMM 24 00 00...

Page 6: ...Static Tester Barfield DPS450 or Barfield Pitot Static Tester Barfield DPS500 or Equivalent Tester Air Data Accessories Kit NavAids P N ADA500MD 945 or Air Data Accessories Kit Nav Aids PN ADA500945...

Page 7: ...ng ECBs WARNING BECAUSE THIS TEST IS PERFORMED WITH WOFFW THE HEATERS WILL BE COMMANDED ON BY THE SYSTEM IF THE PITOT STATIC HEAT ECBS ARE NOT COLLARED OFF HARM TO PERSONNEL OR DAMAGE TO AIR DATA TEST...

Page 8: ...AMAGE MAY OCCUR TO TEST EQUIPMENT HOSES SHOULD BE SNUG CAUTION THE LEAK TEST CAN BE ACCOMPLISHED WITH ELECTRICAL POWER OFF MAKE SURE THAT IF THE WOW BOX IS CONNECTED THE SWITCHES ARE SET TO WONW DURIN...

Page 9: ...5160 long hose 12 to the Barfield Pitot Static Tester DPS450 Ps connection 1 Connect the other end of the Static Test Hose Assembly to the quick connect cross 11 f Connect the short hose 9 to the top...

Page 10: ...ALT ROC CAS and Rt CAS 5 Press Setup and press F1 to select Display Press F3 to select Quad Make sure that Alt is in ft CAS is in kts and Rt CAS is in kts min If not press F2 to select Units and then...

Page 11: ...emote Cord P N ADTS405 1728 28M0 to the Barfield Pitot Static Tester DPS500 Hand Terminal Connection NOTE The Pt Hose p n ADTS405 1729 62m0 may be used in place of the hose p n E500 7270 The AN6 AN4 a...

Page 12: ...finger tighten the screws to seat the seals over the Static ports NOTE The right static upper port can be tested from the left Static lower port by connecting the short hose to the lower port connecti...

Page 13: ...ATE to select the ROC control aim enter 4000 and press the Enter button 6 Press ALT Ps to select the ALT control aim enter 30000 and press the Enter button The system starts to control to the new set...

Page 14: ...EELS THE HEATERS ARE COMMANDED ON BY THE AIRCRAFT COMPUTER SYSTEM IF THE PITOT STATIC HEAT ECBS ARE NOT COLLARED OFF HARM TO PERSONNEL OR AIR DATA TEST EQUIPMENT CAN OCCUR NOTE Refer to step 1 if usin...

Page 15: ...DE 9 Press ROC RATE Ps to select the ROC control aim enter 4000 and press Enter 10 Press ALT Ps to select the ALT control aim enter 30000 and press Enter The system starts to control to the new set po...

Page 16: ...e 3 from the Pt connection 2 on the Barfield Pitot Static Tester DPS450 to the end fitting on the Pitot Static probe adaptor PS35210 4 4 6 c Connect the hose from the Ps 1 connection on the fitting on...

Page 17: ...ing Hoses SUBTASK AMM 34 10 00 071 701 003 ALL A If leakage is excessive during the left and right Pitot and Static System Leak Test for unpressurized aircraft do the following test with the Barfield...

Page 18: ...the ROC and CAS achieves the new air data parameter set points values before moving to the next step 10 Press LEAK MEASURE CONTROL to change to LEAK MEASURE MODE 11 Press F1 to select Rate Timer and...

Page 19: ...IGHTEN HOSES DAMAGE MAY OCCUR TO TEST EQUIPMENT HOSES SHOULD BE SNUG NOTE The Pitot AOA probes with a drain hole near the base of mast must have the drain hole covered Failure to do so will result in...

Page 20: ...align with the holes of the Pitot AOA Probe and adjust until the seals are snug DO NOT over tighten 7 Power on the Barfield Pitot Static Tester DPS450 if needed Wait for the Barfield Pitot Static Test...

Page 21: ...bel TOP facing up on the Pitot AOA probe If needed lubricate with Pitot adaptor Lubricating fluid Part Number LF5050 Adjust Pitot AOA Probe Adaptor nozzles to align with the holes of the Pitot AOA pro...

Page 22: ...ecks and the system changes to the Leak Measure mode shown lower left display corner 7 Press LEAK MEASURE CONTROL to select the CONTROL MODE 8 Press ALT Ps enter 6000 and press Enter 9 Press SETUP Uni...

Page 23: ...Adaptor Nav Aids APA94520 4 4 4 7 with the label TOP facing up on the Pitot AOA probe If needed lubricate with Pitot adaptor lubricating fluid Part Number LF5050 Adjust the Pitot AOA Probe Adaptor noz...

Page 24: ...itot AOA Probe Make sure that the internal seal of the adapter covers the pitot probe drain hole If using the P22201 3 adapter make sure that the pitot probe drain hole is covered with tape If needed...

Page 25: ...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 16 Record the left PFD altitude and airspeed...

Page 26: ...ir Data Accessories Kit NavAids P N ADA500MD 945 un 4 Connect the Barfield Pitot Static Tester DPS500 to the aircraft using the Air Data Accessories Kit Nav Aids PN ADA500945 as follows a Install the...

Page 27: ...of mast must have the drain hole covered Failure to do so will result in a failure of this test a Connect the Pitot Test Hose Assembly 3 to the Pt connection 2 on the Barfield Pitot Static Tester DPS...

Page 28: ...e these new air data parameter set point values to continue 14 Record the left PFD altitude and airspeed Expected results are 30 000 40 feet 200 2 7 knots and 0 557 0 006 Mach 15 Set the Barfield Pito...

Page 29: ...Pitot Static Tester DPS500 is used go to paragraph B A Standby Pitot Static Probe Verification Test with a Barfield Pitot Static Tester DPS450 1 Connect the WOW Box or AMC to the aircraft and make su...

Page 30: ...values to continue 14 Record the Standby Pitot Static probe altitude and airspeed from the MFD Expected Results 10 000 33 feet and 100 3 knots 15 Set the static pressure to 5 999 feet and set the airs...

Page 31: ...andby Pitot Static probe altitude and airspeed from the MFD Expected Results 30 000 75 feet 240 2 7 knots 0 665 0 011 Mach 11 Set the static pressure to 19 899 feet and increase airspeed to 247 5 Knot...

Page 32: ...andby Pitot Static Probe Verification Test with a Barfield Pitot Static Tester DPS450 1 Connect the WOW Box to the aircraft and make sure that the ECBs are collared Refer to SUBTASK AMM 34 10 00 071 9...

Page 33: ...e 14 Record the Standby Pitot Static probe altitude and airspeed from the SDU Expected Results 10 000 33 feet and 100 3 knots 15 Set the static pressure to 5 999 feet and set the airspeed to 64 9 Knot...

Page 34: ...iod after the altitude and airspeed achieve these new air data parameter set point values to continue 10 Record the Standby Pitot Static probe altitude and airspeed from the SDU Expected Results 30 00...

Page 35: ...00 071 921 002 11 Outside Air Temperature Test SUBTASK AMM 34 10 00 071 701 008 ALL A Do an Outside Air Temperature Test as follows 1 Power up the aircraft by setting the SYS BATT and START BATT switc...

Page 36: ...C from aircraft Refer to AMM 20 00 04 051 801 Weight On Wheels WOW Box Connect Disconnect B Remove the external power from the aircraft Refer to AMM 24 40 00 051 801 External Power Maintenance Practic...

Page 37: ...9 10 11 7 Left Pitot Static Hose Configuration Three Port Adapter Figure 501 Sheet 1 of 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY NOTED 34 10 00 Page 533 Se...

Page 38: ...12 6 8 9 10 11 7 Left Angle of Attack Hose Configuration Figure 502 Sheet 1 of 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY NOTED 34 10 00 Page 534 Sep 30 20...

Page 39: ...3 9 8 7 6 Standby Pitot Static Test Adaptor Connections Figure 503 Sheet 1 of 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY NOTED 34 10 00 Page 535 Sep 30 20 2...

Page 40: ...han A FADEC Left Chan B Left Aircraft Computer Right Aircraft Secondary Static Autopilot Servos Right Dual Static Port PSIA Trans PSIA Trans Left APC Right APC T1B T1A T2A T2B Byteflight Byteflight P...

Page 41: ...ss Panel C To gain access to remove the right Pitot AOA use the Air Conditioning controls to open the VCS doors as follows 1 Connect AMC to right armrest USB port Refer to Fig 402 2 On the MFD ENVIR p...

Page 42: ...m hole 12 in the aircraft structure H For the RH Pitot AOA probe Fig 401 Sheet 3 remove the self locking nut 8 flat washer 10 grounding jumper 7 and the hex head screw 11 from hole 12 in the aircraft...

Page 43: ...A Probes Removal Installation Figure 401 Sheet 1 of 4 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY ALL POST MB 500 34 027 AND MB 500 34 028 34 10 10 CONFIG C Pag...

Page 44: ...13 7 11 10 8 B B Pitot AOA Probes Removal Installation Figure 401 Sheet 2 of 4 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY ALL POST MB 500 34 027 AND MB 500 34...

Page 45: ...7 11 10 8 12 B B Pitot AOA Probes Removal Installation Figure 401 Sheet 3 of 4 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY ALL POST MB 500 34 027 AND MB 500 34...

Page 46: ...bes Removal Installation Figure 401 Sheet 4 of 4 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY ALL POST MB 500 34 027 AND MB 500 34 028 34 10 10 CONFIG C Page 406...

Page 47: ...USB Port AMC Hookup Figure 402 Sheet 1 of 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY ALL POST MB 500 34 027 AND MB 500 34 028 34 10 10 CONFIG C Page 407 Rem...

Page 48: ...Figure 403 Sheet 1 of 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY ALL POST MB 500 34 027 AND MB 500 34 028 34 10 10 CONFIG C Page 408 Rem Sep 30 20 2020 Ecli...

Page 49: ...ith a packing block 1 in order to protect the device during shipping handling and installation 1 It is strongly recommended that new Pitot AOA probe s should be mounted to the aircraft with the packin...

Page 50: ...e grounding jumper with flat washer 10 lock washer 9 and self locking nut 8 F For the RH Pitot AOA probe Fig 401 Sheet 4 install the grounding jumper 7 to the aircraft structure by placing hex head sc...

Page 51: ...Do adjustment test of the Pitot AOA probe s following installation Refer to AMM 34 10 00 071 801 Flight Environment Data Adjustment Test CAUTION DURING THIS TEST THE HEATERS WILL BE COMMANDED ON BY TH...

Page 52: ...s Removal Installation Figure 401 Sheet 1 of 5 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY ALL POST MB 500 34 027 AND MB 500 34 028 34 10 10 CONFIG C Page 404 I...

Page 53: ...Probes Removal Installation Figure 401 Sheet 2 of 5 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY ALL POST MB 500 34 027 AND MB 500 34 028 34 10 10 CONFIG C Page...

Page 54: ...3 7 11 10 8 B B Pitot AOA Probes Removal Installation Figure 401 Sheet 3 of 5 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY ALL POST MB 500 34 027 AND MB 500 34 0...

Page 55: ...11 10 8 12 B B Pitot AOA Probes Removal Installation Figure 401 Sheet 4 of 5 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY ALL POST MB 500 34 027 AND MB 500 34 0...

Page 56: ...bes Removal Installation Figure 401 Sheet 5 of 5 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY ALL POST MB 500 34 027 AND MB 500 34 028 34 10 10 CONFIG C Page 408...

Page 57: ...USB Port AMC Hookup Figure 402 Sheet 1 of 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY ALL POST MB 500 34 027 AND MB 500 34 028 34 10 10 CONFIG C Page 409 Ins...

Page 58: ...Figure 403 Sheet 1 of 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY ALL POST MB 500 34 027 AND MB 500 34 028 34 10 10 CONFIG C Page 410 Inst Sep 30 20 2020 Ecl...

Page 59: ...ive sensor that receives electronic signals through a stormscope antenna The processor receives electrical discharge information from the antenna processes it to determine range and azimuth and proces...

Page 60: ...lay Figure 1 Sheet 1 of 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY 0001 0008 0010 0050 0052 0054 0267 PRE SB 500 31 024 34 40 50 CONFIG A Page 2 Sep 30 20 20...

Page 61: ...c signals through a stormscope antenna The processor receives electrical discharge information from the antenna processes it to determine range and azimuth and processes the heading input 3 Operation...

Page 62: ...Strike Mode Figure 1 Sheet 1 of 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY 0001 0008 0010 0050 0052 0054 0267 POST SB 500 31 024 34 40 50 CONFIG B Page 2 Sep...

Page 63: ...Table 501 Special Tools and Equipment AMC Automated Procedure Name and Part Number External Battery Pack PowerVamp Model APS1500 WX PA Portable Analyzer L3 Com P N 78 8060 5791 1 3 Job Set Up SUBTASK...

Page 64: ...BATT Switches to the ON up position and BUS TIE to AUTO up position a Clear any MASTER CAUTIONS and MASTER WARNINGS as needed b On the MFD press the PROCEED Line Select Key LSK 5 If the aircraft is i...

Page 65: ...Garmin 400W unit LTNG page NOTE Left Garmin 400W LTNG page will display LIGHTNING FAILED 10 On the MFD ECB AVIONICS synoptic page reset the following ECB ECB LIGHTNING DETECT SYS R AFT Bus 11 Make sur...

Page 66: ...decrease range 4 Make sure Strike RATE counter is displayed in STRIKE mode NOTE Strike RATE counter should be displaying 0 unless there is real thunderstorm activity within detection range nearby man...

Page 67: ...then press the MENU ENTR button once so that WX PA indicates PAUSED and not RUNNING 12 On the WX PA press the FLAPS A button to select top mount antenna configuration 13 On the WX PA select a cardina...

Page 68: ...0 Set WX PA bearing 090 Verify the displayed bearing 090 10 Set WX PA bearing 180 Verify the displayed bearing 180 10 Set WX PA bearing 270 Verify the displayed bearing 270 10 TEST 2 Set WX PA range 3...

Page 69: ...lighted then push the ENT button NOTE Strike RATE will recede then ramp up toward 600 200 strikes per minute again 6 Observe the GPS 400W Lightning display to ensure proper positioning of the test str...

Page 70: ...SUBTASK AMM 34 40 50 071 A 701 001 NOTE Operator should be familiar with the WX PA Portable Analyzer Kit 1 Make sure that all aircraft power is off 2 Attach the WX PA test set s antenna on top of the...

Page 71: ...turn the small upper left knob clockwise until it clicks to turn the left Garmin 400W on After a short time period the left Garmin 400W will display a features and status page and will prompt a flash...

Page 72: ...the ENT button 2 On left Garmin 400W select STRIKE mode if not already in STRIKE mode Verify STRIKE MODE is displayed on the left Garmin 400W Lightning display format a If not already in STRIKE mode o...

Page 73: ...ure adequate cable is deployed from the external power cart to allow the aircraft to turn 45 to the right 10 Power up the WX PA Portable Analyzer unit After the WX PA completes self test the MODE MENU...

Page 74: ...0 Set WX PA bearing 090 Verify the displayed bearing 090 10 Set WX PA bearing 180 Verify the displayed bearing 180 10 Set WX PA bearing 270 Verify the displayed bearing 270 10 TEST 2 Set WX PA range 3...

Page 75: ...ighlighted then push the ENT button NOTE Strike RATE will recede then ramp up toward 600 200 strikes per minute again 6 Observe the GPS 400W Lightning display to ensure proper positioning of the test...

Page 76: ...051 801 Aircraft Access Panels for location and installation instructions D Install if removed 311 AL Maintenance Bay Panel Refer to AMM 06 50 00 051 801 Aircraft Access Panels for location and instal...

Page 77: ...1 WX PA Antenna Alignment Figure 501 Sheet 1 of 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY 0001 0008 0010 0050 0052 0054 0267 PRE SB 500 31 024 34 40 50 CONF...

Page 78: ...er Fin Fairing Figure 502 Sheet 1 of 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY 0001 0008 0010 0050 0052 0054 0267 PRE SB 500 31 024 34 40 50 CONFIG A Page 5...

Page 79: ...Figure 503 Sheet 1 of 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY 0001 0008 0010 0050 0052 0054 0267 PRE SB 500 31 024 34 40 50 CONFIG A Page 517 Sep 30 20 20...

Page 80: ...y Figure 504 Sheet 1 of 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY 0001 0008 0010 0050 0052 0054 0267 PRE SB 500 31 024 34 40 50 CONFIG A Page 518 Sep 30 20...

Page 81: ...able 501 Special Tools and Equipment Name and Part Number External Battery Pack PowerVamp Model APS1500 WX PA Portable Analyzer L3 Com P N 78 8060 5791 1 3 Job Set Up SUBTASK AMM 34 40 50 071 B 921 00...

Page 82: ...SK 4 Verify that no CAS messages are displayed indicating Lightning equipment failures 5 On the MFD ECB AVIONICS synoptic page PULL the ECB ECB LIGHTNING DETECT SYS R AFT Bus 6 Verify that a LIGHTNING...

Page 83: ...e WX PA Portable Analyzer unit After the WX PA completes self test the MODE MENU will be displayed 16 On the WX PA select Continuous Out on the MODE MENU then press the MENU ENTR button once so that W...

Page 84: ...t WX PA bearing 270 Verify the displayed bearing 270 10 TEST 2 Set WX PA range 30 NM Set PFD range 80 NM Result PASS FAIL Set WX PA bearing 000 Verify the displayed bearing 000 10 Set WX PA bearing 09...

Page 85: ...nute 29 Test strikes appearing on the PFDs are at approximately 180 10 relative and 75 NM 30 With aircraft magnetic heading active turn the aircraft 45 5 clockwise or to the right 31 Older test strike...

Page 86: ...und See also Fig 503 3 Route the WX PA antenna cable away from the aircraft a Connect the antenna cable to the WX PA test box b DO NOT POWER UP THE TEST SET 4 On the IPL set the SYS BATT and START BAT...

Page 87: ...tester can be moved with the aircraft c Make sure adequate cable is deployed from the external power cart to allow the aircraft to turn 45 to the right 16 Power up the WX PA Portable Analyzer unit Aft...

Page 88: ...t WX PA bearing 270 Verify the displayed bearing 270 10 TEST 2 Set WX PA range 30 NM Set PFD range 80 NM Result PASS FAIL Set WX PA bearing 000 Verify the displayed bearing 000 10 Set WX PA bearing 09...

Page 89: ...strikes per minute 30 Test strikes appearing on the PFDs are at approximately 180 10 relative and 75 NM 31 With aircraft magnetic heading active turn the aircraft 45 5 clockwise or to the right 32 Ol...

Page 90: ...EPTICLE C Install if removed 331 DT Upper Overfin Fairing Refer to AMM 06 50 00 051 801 Aircraft Access Panels for location and installation instructions D Remove all tools equipment and unwanted mate...

Page 91: ...1 WX PA Antenna Alignment Figure 501 Sheet 1 of 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY 0001 0008 0010 0050 0052 0054 0267 POST SB 500 31 024 34 40 50 CON...

Page 92: ...r Fin Fairing Figure 502 Sheet 1 of 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY 0001 0008 0010 0050 0052 0054 0267 POST SB 500 31 024 34 40 50 CONFIG B Page 5...

Page 93: ...Figure 503 Sheet 1 of 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY 0001 0008 0010 0050 0052 0054 0267 POST SB 500 31 024 34 40 50 CONFIG B Page 513 Sep 30 20 2...

Page 94: ...rike Mode Figure 504 Sheet 1 of 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY 0001 0008 0010 0050 0052 0054 0267 POST SB 500 31 024 34 40 50 CONFIG B Page 514 S...

Page 95: ...8 pixel color LCD display and a re moveable data card containing a Jeppesen data base It presents an active flight plan and moving map on its display and provides guidance and status display on its LC...

Page 96: ...051 A 801 GPS Maintenance Practices for general operating information and instructions for configuring the unit to the aircraft A Two GPS antennas Combination Antennas and two GPS WAAS units make up t...

Page 97: ...A GPS Combination Antenna Location Figure 1 Sheet 1 of 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY 0001 0262 POST SB 500 99 005 AND 0266 0267 ALL POST MB 500...

Page 98: ...nce Manual 06 117751 Temporary Revision No 34 21 THIS PAGE INTENTIONALLY LEFT BLANK EFFECTIVITY 0001 0262 POST SB 500 99 005 AND 0266 0267 ALL POST MB 500 31 018 34 50 10 CONFIG B Page 4 Sep 30 20 202...

Page 99: ...ke Safe For Maintenance B Connect the ground power cart to electrical utility connector Connect the ground power cart to the aircraft EXTERNAL POWER RECEPTACLE and turn on power on the cart Ensure the...

Page 100: ...mall right knob may be used to select a page within the page group Other page groups are available via dedicated keys DRCT MSG FPL and PROC The NAV page group may be accessed directly by pressing and...

Page 101: ...AVIONICS synoptic page ensure ECB GPS 1 L FWD Bus and ECB GPS 2 R FWD Bus are AUTO ON Make sure the circuit breakers in the pilot s and co pilot s armrest Com Jack Panels MECHANICAL CIRCUIT BREAKER CI...

Page 102: ...e MAIN ARINC 429 CONFIG page Different configuration screens may be selected using the small right knob while in configuration mode 2 While on the MAIN ARINC 429 CONFIG screen press the small right kn...

Page 103: ...LED EQUIPMENT 2 On the GPS 400W rotate small right knob to select MAIN RS232 CONFIG page 3 Press the small right knob to turn on the cursor 4 Using the large right knob to select fields as necessary t...

Page 104: ...small right knob to select MAIN SYSTEM CONFIG page 2 Press the small right knob to turn on the cursor 3 With the cursor at the CONFIGURE field rotate the small right knob to select Fuel Press ENT 4 W...

Page 105: ...configured correctly in previous steps or there is a communication problem between the PFD and the GPS 400W This should be resolved before proceeding with the remaining procedures G Configure Backlig...

Page 106: ...the small right knob to return to the first AUX page after CROSSFILL configuration is set Press the small right knob again to dismiss the cursor on AUX page 1 8 Rotate the small right knob to select t...

Page 107: ...ections and enter values and ENT to confirm selections set up the DISPLAY configuration as shown in Fig 217 27 Press the small right knob to return to the SETUP 2 page after DISPLAY configuration is s...

Page 108: ...d BUS TIE to OPEN down position D If no other requirements for External Power Power down the GPU Disconnect the GPU from the aircraft EXTERNAL POWER RECEPTICLE on the aircraft Disconnect the GPU from...

Page 109: ...01 Sheet 1 of 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY 0001 0262 POST SB 500 99 005 AND 0266 0267 ALL POST MB 500 31 018 34 50 10 CONFIG A Page 211 Sep 30...

Page 110: ...ngs Figure 202 Sheet 1 of 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY 0001 0262 POST SB 500 99 005 AND 0266 0267 ALL POST MB 500 31 018 34 50 10 CONFIG A Page...

Page 111: ...s Figure 203 Sheet 1 of 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY 0001 0262 POST SB 500 99 005 AND 0266 0267 ALL POST MB 500 31 018 34 50 10 CONFIG A Page 2...

Page 112: ...ings Figure 204 Sheet 1 of 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY 0001 0262 POST SB 500 99 005 AND 0266 0267 ALL POST MB 500 31 018 34 50 10 CONFIG A Pag...

Page 113: ...ttings Figure 205 Sheet 1 of 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY 0001 0262 POST SB 500 99 005 AND 0266 0267 ALL POST MB 500 31 018 34 50 10 CONFIG A P...

Page 114: ...ettings Figure 206 Sheet 1 of 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY 0001 0262 POST SB 500 99 005 AND 0266 0267 ALL POST MB 500 31 018 34 50 10 CONFIG A...

Page 115: ...Figure 207 Sheet 1 of 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY 0001 0262 POST SB 500 99 005 AND 0266 0267 ALL POST MB 500 31 018 34 50 10 CONFIG A Page 217...

Page 116: ...Figure 208 Sheet 1 of 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY 0001 0262 POST SB 500 99 005 AND 0266 0267 ALL POST MB 500 31 018 34 50 10 CONFIG A Page 218...

Page 117: ...gs Figure 209 Sheet 1 of 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY 0001 0262 POST SB 500 99 005 AND 0266 0267 ALL POST MB 500 31 018 34 50 10 CONFIG A Page...

Page 118: ...s Figure 210 Sheet 1 of 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY 0001 0262 POST SB 500 99 005 AND 0266 0267 ALL POST MB 500 31 018 34 50 10 CONFIG A Page 2...

Page 119: ...tings Figure 211 Sheet 1 of 2 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY 0001 0262 POST SB 500 99 005 AND 0266 0267 ALL POST MB 500 31 018 34 50 10 CONFIG A Pa...

Page 120: ...tings Figure 211 Sheet 2 of 2 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY 0001 0262 POST SB 500 99 005 AND 0266 0267 ALL POST MB 500 31 018 34 50 10 CONFIG A Pa...

Page 121: ...Figure 212 Sheet 1 of 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY 0001 0262 POST SB 500 99 005 AND 0266 0267 ALL POST MB 500 31 018 34 50 10 CONFIG A Page 22...

Page 122: ...igure 213 Sheet 1 of 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY 0001 0262 POST SB 500 99 005 AND 0266 0267 ALL POST MB 500 31 018 34 50 10 CONFIG A Page 224...

Page 123: ...Figure 214 Sheet 1 of 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY 0001 0262 POST SB 500 99 005 AND 0266 0267 ALL POST MB 500 31 018 34 50 10 CONFIG A Page 225...

Page 124: ...tings Figure 215 Sheet 1 of 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY 0001 0262 POST SB 500 99 005 AND 0266 0267 ALL POST MB 500 31 018 34 50 10 CONFIG A Pa...

Page 125: ...gure 216 Sheet 1 of 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY 0001 0262 POST SB 500 99 005 AND 0266 0267 ALL POST MB 500 31 018 34 50 10 CONFIG A Page 227 S...

Page 126: ...ure 217 Sheet 1 of 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY 0001 0262 POST SB 500 99 005 AND 0266 0267 ALL POST MB 500 31 018 34 50 10 CONFIG A Page 228 Se...

Page 127: ...tings Figure 218 Sheet 1 of 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY 0001 0262 POST SB 500 99 005 AND 0266 0267 ALL POST MB 500 31 018 34 50 10 CONFIG A Pa...

Page 128: ...Figure 219 Sheet 1 of 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY 0001 0262 POST SB 500 99 005 AND 0266 0267 ALL POST MB 500 31 018 34 50 10 CONFIG A Page 23...

Page 129: ...tings Figure 220 Sheet 1 of 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY 0001 0262 POST SB 500 99 005 AND 0266 0267 ALL POST MB 500 31 018 34 50 10 CONFIG A Pa...

Page 130: ...W STANDBY ALTITUDE AIRSPEED OPTION GPS 400W Standby Altitude Airspeed Indication Option Figure 221 Sheet 1 of 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY 0001...

Page 131: ...source for downloading Garmin software and tools for a particular product 3 Job Set Up SUBTASK AMM 34 50 10 051 B 921 001 A Make aircraft safe for maintenance Refer to AMM 20 00 01 051 801 Make Safe...

Page 132: ...ive actions as required or contact Eclipse Service Engineering 11 On the GDL 8x Install Tool select Configuration Aircraft Refer to Fig 202 Sheet 1 Populate the following aircraft specifics Aircraft I...

Page 133: ...Up SUBTASK AMM 34 50 10 051 B 921 002 A Remove all tools equipment and unwanted material from work area EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY ALL POST MB...

Page 134: ...ool Unit Information Figure 201 Sheet 1 of 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY ALL POST MB 500 34 030 34 50 10 CONFIG B Page 204 Sep 30 20 2020 Eclips...

Page 135: ...Aircraft Configuration Figure 202 Sheet 1 of 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY ALL POST MB 500 34 030 34 50 10 CONFIG B Page 205 Sep 30 20 2020 Ecl...

Page 136: ...l Antenna Configuration Figure 203 Sheet 1 of 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY ALL POST MB 500 34 030 34 50 10 CONFIG B Page 206 Sep 30 20 2020 Ecl...

Page 137: ...S 232 RS 422 Configuration Figure 204 Sheet 1 of 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY ALL POST MB 500 34 030 34 50 10 CONFIG B Page 207 Sep 30 20 2020...

Page 138: ...Ethernet Configuration Figure 205 Sheet 1 of 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY ALL POST MB 500 34 030 34 50 10 CONFIG B Page 208 Sep 30 20 2020 Ecl...

Page 139: ...h GPS receivers are displaying satellite status signal strength information E On the other side of the MFD select the system synoptic page ECB tab 4 GPS 1 Test SUBTASK AMM 34 50 10 071 C 801 002 A Do...

Page 140: ...MFD ECB page pull ECB INTEGRATED SENSOR 2 L AFT Bus After 5 seconds make sure that GPS 2 is displaying satellite status information G On the MFD ECB page reset ECB INTEGRATED SENSOR 2 L AFT Bus 6 Job...

Page 141: ...THE GPS 3 GDL 88 MOUNT AND WIRING ARE ATTACHED TO THE UNDERSIDE OF THE FLOOR PANEL A Remove screws but do not remove 131 CZ B Floor Panel Aft Short Left Cabin 3 Refer to AMM 25 11 30 001 801 Cockpit F...

Page 142: ...PS 3 Removal Installation Figure 401 Sheet 1 of 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY ALL POST MB 500 34 030 34 50 11 CONFIG C Page 402 Rem Sep 30 20 20...

Page 143: ...ove the 231 JZ Cabin Headliner Assembly Refer to AMM 06 50 00 051 801 Aircraft Access Panels 3 Procedure SUBTASK AMM 34 50 11 001 D 011 001 Refer to Fig 401 A Remove the four bolts 1 that attach the G...

Page 144: ...x2 5 x4 6 x4 A GPS Removal Installation Figure 401 Sheet 1 of 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY ALL POST MB 500 31 007 OR MB 500 31 008 34 50 11 CON...

Page 145: ...s on the back plate in the slots of the left side of the GPS bracket assembly 6 viewing it from the cockpit and attaching it by replacing the two screws 4 2 Remove protective caps on electrical connec...

Page 146: ...D Bus ECB GPS 2 L FWD Bus C Complete GPS 400W configuration if not previously accomplished refer to AMM 34 50 10 051 801 GPS Maintenance Practices D Do an adjustment test of the GPS Refer to AMM 34 50...

Page 147: ...2 3 4 GPS Removal Installation Figure 401 Sheet 1 of 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY 0001 0262 POST SB 500 99 005 AND 0266 0267 ALL POST MB 500 3...

Page 148: ...Manual 06 117751 Temporary Revision No 34 21 THIS PAGE INTENTIONALLY LEFT BLANK EFFECTIVITY 0001 0262 POST SB 500 99 005 AND 0266 0267 ALL POST MB 500 31 018 34 50 11 CONFIG B Page 404 Inst Sep 30 20...

Page 149: ...Procedure SUBTASK AMM 34 50 11 041 C 411 001 Refer to Fig 401 A Slide the GPS 3 unit 1 straight into the rack until it stops B Lift the lock down arm 2 over the right angled hook on the unit and hand...

Page 150: ...S 3 Removal Installation Figure 401 Sheet 1 of 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY ALL POST MB 500 34 030 34 50 11 CONFIG C Page 402 Inst Sep 30 20 20...

Page 151: ...GPS WAAS sensor 4 mounting flange is toward the inboard side on the aircraft and away from the mounting bracket 5 B Attach the GPS WAAS sensor 4 to the mounting bracket 5 1 For the left side GPS WAAS...

Page 152: ...l the 231 JZ Cabin Headliner Assembly Refer to AMM 06 50 00 051 801 Aircraft Access Panels C If all other maintenance is complete return the aircraft to service Refer to AMM 20 00 02 051 801 Return To...

Page 153: ...2 5 x4 6 x4 A GPS Removal Installation Figure 401 Sheet 1 of 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY ALL POST MB 500 31 007 OR MB 500 31 008 34 50 11 CONF...

Page 154: ...Maintenance Manual 06 117751 Temporary Revision No 34 21 THIS PAGE INTENTIONALLY LEFT BLANK EFFECTIVITY ALL POST MB 500 31 007 OR MB 500 31 008 34 50 11 CONFIG D Page 404 Inst Sep 30 20 2020 Eclipse...

Page 155: ...BIN UNTIL MOUNT HAS BEEN DETACHED THE GDL 88 MOUNT AND WIRING ARE ATTACHED TO THE UNDERSIDE OF THE FLOOR PANEL A Lift the forward edge and pivot 131 CZ B Floor Panel Aft Short Left Cabin 2 while suppo...

Page 156: ...4 GPS 3 Mount Removal Installation Figure 401 Sheet 1 of 2 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY ALL POST MB 500 34 030 34 50 13 Page 402 Rem Sep 30 20 20...

Page 157: ...0 11 GPS 3 Mount Removal Installation Figure 401 Sheet 2 of 2 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY ALL POST MB 500 34 030 34 50 13 Page 403 Rem Sep 30 20...

Page 158: ...EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 THIS PAGE INTENTIONALLY LEFT BLANK EFFECTIVITY ALL POST MB 500 34 030 34 50 13 Page 404 Rem Sep 30 20 2020 Eclipse Aerospace Inc...

Page 159: ...35 1 69 Nm D Connect fan electrical molex connector 10 to harness molex connector 11 E Connect the GPS antenna coax cable connector to the GPS coax receptacle 6 marked GPS F Connect 50 ohm 5 watt ter...

Page 160: ...GPS 3 Mount Removal Installation Figure 401 Sheet 1 of 2 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY ALL POST MB 500 34 030 34 50 13 Page 402 Inst Sep 30 20 20...

Page 161: ...11 GPS 3 Mount Removal Installation Figure 401 Sheet 2 of 2 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY ALL POST MB 500 34 030 34 50 13 Page 403 Inst Sep 30 20...

Page 162: ...A500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 THIS PAGE INTENTIONALLY LEFT BLANK EFFECTIVITY ALL POST MB 500 34 030 34 50 13 Page 404 Inst Sep 30 20 2020 Eclipse Aerospace Inc...

Page 163: ...e 231 NZ Floor Panel Baggage Compartment Refer to AMM 06 50 00 051 801 Aircraft Access Panels for location and removal instructions 3 Procedure SUBTASK AMM 34 50 14 001 C 011 001 Refer to Fig 401 A Di...

Page 164: ...FOR CLARITY GPS 2 Antenna Splitter Removal Installation Figure 401 Sheet 1 of 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY ALL POST MB 500 34 030 34 50 14 Pag...

Page 165: ...n 3 4 4 5 Nm D Connect the three coaxial connectors 3 on the splitter 1 E Electrically bond the GPS 2 Antenna Splitter to the structure Refer to AMM 20 03 00 051 801 Electrical Bonding Maintenance Pra...

Page 166: ...FOR CLARITY GPS 2 Antenna Splitter Removal Installation Figure 401 Sheet 1 of 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY ALL POST MB 500 34 030 34 50 14 Pag...

Page 167: ...enna switching relays 2 Description SUBTASK AMM 34 50 20 081 C 871 001 A Standard Transponder System 1 There are two transponders one transponder number 1 is installed in the instrument panel behind t...

Page 168: ...replies include framing pulses and encoded altitude There are two transponder antennas The number 1 upper transponder antenna is mounted on the top of the fuselage and is connect to transponder number...

Page 169: ...s 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 Multi Function Display MFD software key pertinent to a...

Page 170: ...ransponder antennas The number 1 upper transponder antenna is mounted on the top of the fuselage and is connect to transponder number 1 behind the left PFD The number 2 lower transponder antenna is mo...

Page 171: ...e Refer to AMM 20 00 01 051 801 Make Safe For Maintenance B If installed on aircraft remove affected transponder from aircraft Refer to AMM 34 50 21 001 801 Transponder Removal C Obtain the transponde...

Page 172: ...is in the OFF position 2 Turn the power supply on and power up the transponder 3 Ensure the connection with transponder can be established by pressing the call button on the Hyper Terminal interface 4...

Page 173: ...ect Harness Assy GTX 33 Test 87 124598 1001 from Power Supply and Transponder EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY ALL POST MB 500 31 018 OR MB 500 34 03...

Page 174: ...tup Figure 201 Sheet 1 of 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY ALL POST MB 500 31 018 OR MB 500 34 030 34 50 20 Page 204 Sep 30 20 2020 Eclipse Aerospa...

Page 175: ...ew Connection Figure 202 Sheet 1 of 4 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY ALL POST MB 500 31 018 OR MB 500 34 030 34 50 20 Page 205 Sep 30 20 2020 Eclip...

Page 176: ...ction Properties Figure 202 Sheet 2 of 4 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY ALL POST MB 500 31 018 OR MB 500 34 030 34 50 20 Page 206 Sep 30 20 2020 Ec...

Page 177: ...Comm Demo Figure 202 Sheet 3 of 4 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY ALL POST MB 500 31 018 OR MB 500 34 030 34 50 20 Page 207 Sep 30 20 2020 Eclipse...

Page 178: ...Send File Figure 202 Sheet 4 of 4 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY ALL POST MB 500 31 018 OR MB 500 34 030 34 50 20 Page 208 Sep 30 20 2020 Eclipse...

Page 179: ...Set Aeroflex IFR6000 UC 584 Universal Transponder Antenna Coupler Dual Antenna Kit Viavi 112349 1 Weight on Wheels WOW Box EAI 87 117390 1001 or Avio Maintenance Computer AMC EAI 20 120576 1001 or 20...

Page 180: ...e for Test Set to function correctly Coupler will lock into place when the black rubber gasket is not completely depressed against the aircraft but the Test Set will not measure functions accurately C...

Page 181: ...ector CAUTION THE RF COAXIAL CABLE CAN BE A TRIPPING HAZARD MAKE SURE TO SECURE THE CABLE PERSONAL INJURY AND DAMAGE TO THE ANTENNAS AND TEST EQUIPMENT COULD OCCUR 4 Temporarily secure the coaxial cab...

Page 182: ...ht button on the left PFD to select XPDR1 3 CODE status box on the left PFD and right PFD shows 1200 a To change CODE scroll to XPDR using softkey Use outer knob to highlight and inner knob to change...

Page 183: ...STOP TEST button 7 Repeat until all FAILED tests have been completed 8 Press Return button on IFR 6000 to return to XPDR AUTO TEST screen appears A PASS message should be displayed 9 On left PFD scro...

Page 184: ...UPXPDR Screen Use NEXT PARAM and PREV PARAM Soft Keys to select each parameter 4 Select RF PORT Select DIR W COUPLER a Select CPL CABLE LOSS Set to loss found on cable b Select COUPLER LOSS Set to los...

Page 185: ...NT is displayed on Transponder Test Set IFR6000 NOTE IDENT will disappear from the IFR test set in approximately 20 seconds 20 Press IDNT key on the Copilot s keyboard If Installed IDENT is displayed...

Page 186: ...ber NOTE If the tail number is not displayed refer to SUBTASK AMM 34 50 20 071 A 701 002 5 Scroll to XPDR on Left PFD Press the MODE softkey button to change the mode to STBY 6 On Transponder Test Set...

Page 187: ...other aircraft Refer to Fig 501 CAUTION FAILURE TO COMPLY WITH THIS STEP AND CONTINUING WITH THIS PROCEDURE COULD IMPACT LOCAL AIRPORT TOWER OPERATIONS F If applicable contact local airport tower to...

Page 188: ...ight button on the left PFD to select XPDR1 3 CODE status box on the left PFD and right PFD shows 1200 a To change CODE scroll to XPDR using softkey Use outer knob to highlight and inner knob to chang...

Page 189: ...value from cable running between antenna and Test set denoted by Value followed by dB Enter the data on Transponder Test Set IFR6000 e Press NEXT PARAM and enter the dBi value directly beneath the GHz...

Page 190: ...sts 17 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 18 Press IDNT key on the Copilo...

Page 191: ...h the GHz values 1 03 and 1 09 from antenna data plate Enter the data on Transponder Test Set IFR6000 4 On left PFD use lower right softkey to scroll to XPDR press ACTIVE softkey upper right button on...

Page 192: ...IDENT Tests 18 Press IDNT key on the pilot s keyboard IDENT is displayed on Transponder Test Set IFR6000 NOTE IDENT will disappear from the IFR test set in approximately 20 seconds 19 Press IDNT key o...

Page 193: ...back of PFD 2 Use address module programmer kits AMP6400 1 parallel interface or AMP6400 2 USB interface along with a PC to program the Address Module NOTE The CD ROM which is part of the address mod...

Page 194: ...s complete return aircraft to service Refer to AMM 20 00 02 051 801 Return To Service After Maintenance EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY 0001 0104 01...

Page 195: ...nsponder Adjustment Test Figure 501 Sheet 1 of 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY 0001 0104 0113 0115 0120 0123 0124 PRE SB 500 99 002 AND SB 500 99...

Page 196: ...OCCUPYING 20 BEAMWIDTH IFR 6000 TEST SET AND ANTENNA BUILDING BUILDING HANDLE TNG CONNECTION CABLE TO TEST SET FLAT ANTENNA ANTENNA PATTERN BEAMWIDTH 20 VERTICAL 25 HORIZONTAL Transponder Adjustment T...

Page 197: ...s Dual Standard Transponder System Test Std Transponder 1 Adjustment Test SUBTASK AMM 34 50 20 071 B 701 001 A or SUBTASK AMM 34 50 20 071 B 701 001 B and Std Transponder 2 Adjustment Test SUBTASK AMM...

Page 198: ...117390 1001 or AMC 2 4 01 or higher Ground Power Unit GPU AllStar 450 or AllStar G S E or Hobart GPU 400 or Hobart GPU 600 or Bycan PS 28100 1 For test with UC 584 antenna coupler EA500 Aircraft Main...

Page 199: ...tion correctly Coupler will lock into place when the black rubber gasket is not completely depressed against the aircraft but the Test Set will not measure functions accurately CAUTION DO NOT CONNECT...

Page 200: ...AXIAL CABLE CAN BE A TRIPPING HAZARD MAKE SURE TO SECURE THE CABLE PERSONAL INJURY AND DAMAGE TO THE ANTENNAS AND TEST EQUIPMENT COULD OCCUR 4 Temporarily secure the coaxial cable to the aircraft with...

Page 201: ...eded 6 Set both left and right PFD baro set to 29 92 in Hg on Autopilot Control Panel ACP by pushing BARO SET knob B Transponder 1 Setup 1 Use the small rotary knob on the left PFD to select XPDR page...

Page 202: ...e through separate tests after which a PASS message should be displayed 9 Top ERP should be between 48 to 60 dBm and MTL should be between 68 to 80 dBm to PASS 10 Push RUN TEST soft key on Transponder...

Page 203: ...ms Maintenance Practices Steps 15 through this step must then be repeated 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 t...

Page 204: ...signed enter 1200 C Transponder 2 MODE A C S Test using Transponder Test Set IFR6000 1 Power up the Transponder Test Set IFR 6000 After tester performs Self Test push SETUP button on the test set to b...

Page 205: ...page At the bottom of the SETTINGS page check a The REGISTRATION NO number alphanumeric matches the TAIL number alphanumeric displayed on the IFR 6000 above 12 The ICAO 24 BIT OCT number matches the...

Page 206: ...listed ECB using outer knob and highlight Push COLLAR soft key Push CONFIRM COLLAR soft key ECB NOSE LDG GEAR L AFT Bus ECB L MAIN LDG GEAR L AFT Bus ECB R MAIN LDG GEAR L AFT Bus 4 Scroll to ENGINE u...

Page 207: ...the XPDR AUTO TEST page 4 Push CONFIG soft key to display the XPDR CONFIG SCREEN page 5 On the XPDR CONFIG SCREEN scroll to GENERIC MODE S using the UP Down DATA keys 6 With GENERIC MODE S highlighte...

Page 208: ...CODER is displayed press the SOURCE SELECT Soft Key until SOURCE XPDR is displayed Press the RUN TEST Soft Key 15 Make sure that an altitude reported on IFR 6000 matches L PFD altitude indication 100...

Page 209: ...sequence through separate tests after which a PASS message should be displayed 11 ERP should be between 48 to 60 dBm and MTL should be between 68 to 80 dBm to PASS 12 Remove Antenna Clamp and Shield...

Page 210: ...ght Push COLLAR soft key Push CONFIRM COLLAR soft key ECB NOSE LDG GEAR L AFT Bus ECB L MAIN LDG GEAR L AFT Bus ECB R MAIN LDG GEAR L AFT Bus 4 Scroll to ENGINE using outer knob Push inner knob to sel...

Page 211: ...sh CONFIG soft key to display the XPDR CONFIG SCREEN page 5 On the XPDR CONFIG SCREEN scroll to GENERIC MODE S using the UP Down DATA keys 6 With GENERIC MODE S highlighted push RETURN soft key to con...

Page 212: ...ey until SOURCE XPDR is displayed Press the RUN TEST Soft Key 15 Make sure that an altitude reported on IFR 6000 matches L PFD altitude indication 100 ft 16 On the MFD set the ADC source back to AUTO...

Page 213: ...o display the XPDR CONFIG SCREEN page 11 On the XPDR CONFIG SCREEN scroll to GENERIC MODE S using the UP Down DATA keys 12 With GENERIC MODE S highlighted push RETURN soft key to confirm selection Thi...

Page 214: ...N FAILURE TO COMPLY WITH THIS STEP AND CONTINUING WITH THIS PROCEDURE COULD IMPACT LOCAL AIRPORT TOWER OPERATIONS F If applicable contact local airport tower to inform them a transponder test is being...

Page 215: ...FIRM COLLAR soft key ECB L ENG FIRE EXTNGR L FWD Bus ECB R ENG FIRE EXTNGR R FWD Bus 6 Clear any MASTER CAUTIONS and MASTER WARNINGS as needed 7 Set both left and right PFD baro set to 29 92 in Hg on...

Page 216: ...4 Push CONFIG soft key to display the XPDR CONFIG SCREEN page 5 On the XPDR CONFIG SCREEN scroll to GENERIC MODE S using the UP Down DATA keys 6 With GENERIC MODE S highlighted push RETURN soft key to...

Page 217: ...owing appears on the Transponder Test Set IFR 6000 A CODE transponder code entered C ALT left PFD altitude indication 100 ft S CODE ICAO code assigned to this aircraft tail number TAIL tail number ass...

Page 218: ...ft Key 17 Make sure that an altitude reported on IFR 6000 matches L PFD altitude indication 100 ft 18 On the MFD set the ADC source back to AUTO 19 Set the WOW Box Switches to W on W on ground 20 Set...

Page 219: ...was assigned enter 1200 C Transponder 2 MODE A C S Test using Transponder Test Set IFR6000 1 Power up the Transponder Test Set IFR 6000 After tester performs Self Test push SETUP button on the test se...

Page 220: ...until IFR 6000 and aircraft Transponder Sync up Press STOP TEST button Repeat until all individual FAILED tests have achieved a PASS It is not necessary to re run AUTO TEST AUTO TEST is a convenience...

Page 221: ...0 051 801 Aircraft Computer Systems Maintenance Practices 13 On the MFD scroll to the SETUP tab press the SENSOR Soft Key Set the ADC PFD source selection from AUTO to ADC 2 14 On the IFR 6000 press t...

Page 222: ...key Push CONFIRM COLLAR soft key ECB NOSE LDG GEAR L AFT Bus ECB L MAIN LDG GEAR L AFT Bus ECB R MAIN LDG GEAR L AFT Bus 4 Scroll to ENGINE using outer knob Push inner knob to select Scroll to the lis...

Page 223: ...S As marked on blue cable should be 0 1 dB ANT GAIN dBi 1 03 GHz As marked on test set antenna ANT GAIN dBi 1 09 GHz As marked on test set antenna UUT ADDRESS AUTO MANUAL AA Ignore DIVERSITY TEST ON P...

Page 224: ...Test Set IFR 6000 A CODE transponder code entered 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 FLT ID sa...

Page 225: ...der antenna top of the center cabin fuselage in accordance with instructions in IFR 6000 Ramp Test Set Operation Manual 3 Pre position the Transponder Test Set IFR 6000 antenna to point at the aircraf...

Page 226: ...tests have achieved a PASS It is not necessary to re run AUTO TEST AUTO TEST is a convenience feature only NOTE If POWER FREQ test Fails After pressing RUN TEST adjust IFR 6000 test set positioning wh...

Page 227: ...t key Push CONFIRM COLLAR soft key ECB NOSE LDG GEAR L AFT Bus ECB L MAIN LDG GEAR L AFT Bus ECB R MAIN LDG GEAR L AFT Bus 4 Scroll to ENGINE using outer knob Push inner knob to select Scroll to the l...

Page 228: ...ould be 0 1 dB ANT GAIN dBi 1 03 GHz As marked on test set antenna ANT GAIN dBi 1 09 GHz As marked on test set antenna UUT ADDRESS AUTO MANUAL AA Ignore DIVERSITY TEST ON PWR LIM FAR 43 CHECK CAP YES...

Page 229: ...Test Set IFR 6000 A CODE transponder code entered 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 DF17 DETE...

Page 230: ...the center cabin fuselage in accordance with instructions in IFR 6000 Ramp Test Set Operation Manual 3 Pre position the Transponder Test Set IFR 6000 antenna to point at the aircraft s lower Transpon...

Page 231: ...at until all individual FAILED tests have achieved a PASS It is not necessary to re run AUTO TEST AUTO TEST is a convenience feature only NOTE If POWER FREQ test Fails After pressing RUN TEST adjust I...

Page 232: ...cks lower aircraft and remove jacks Refer to AMM 07 10 00 051 801 Jacking Maintenance Practices H If applicable call the local control tower and tell them the transponder test is complete I Remove all...

Page 233: ...st Figure 501 Sheet 1 of 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY 0001 0104 0113 0115 0120 0123 0124 POST SB 500 99 002 AND 0105 0112 0116 0119 0121 0122 0...

Page 234: ...IFR 6000 TEST SET AND ANTENNA BUILDING BUILDING HANDLE TNG CONNECTION CABLE TO TEST SET FLAT ANTENNA ANTENNA PATTERN BEAMWIDTH 20 VERTICAL 25 HORIZONTAL Transponder Adjustment Test Figure 502 Sheet 1...

Page 235: ...1 only 1 Refer to Table 501 for testing procedures Table 501 Test Matrix System Test Procedures Dual Standard Transponder System Test Std Transponder 1 Adjustment Test SUBTASK AMM 34 50 20 071 C 701 0...

Page 236: ...ial 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 E...

Page 237: ...he bottom of the coupler 2 Lock Antenna Coupler 2 into place by pushing lever on the side of the coupler into a down and locked position NOTE Coupler must be tightly pressed and locked in place for Te...

Page 238: ...T WILL OCCUR 3 Connect long RF coaxial cable 1 between the Antenna Coupler and Test Set RF I O Connector CAUTION THE RF COAXIAL CABLE CAN BE A TRIPPING HAZARD MAKE SURE TO SECURE THE CABLE PERSONAL IN...

Page 239: ...L MAIN LDG GEAR L AFT Bus ECB R MAIN LDG GEAR L AFT Bus 5 Scroll to ENGINE using outer knob Push inner knob to select Scroll to the listed ECB using outer knob and highlight Push COLLAR soft key Push...

Page 240: ...URN soft key to confirm selection This will also cause a return to the XPDR AUTO TEST page 7 Set the WOW test box or AMC to W off W airborne NOTE Transponders will transition to ALT mode automatically...

Page 241: ...page the Aircraft Configuration File must be updated refer to AMM 31 40 00 051 801 Aircraft Computer Systems Maintenance Practices Steps 10 through this step must then be repeated 13 On the MFD scroll...

Page 242: ...by the control tower for this test If no code was assigned enter 1200 C Transponder 2 MODE A C S Test using Transponder Test Set IFR6000 1 Power up the Transponder Test Set IFR 6000 After tester perfo...

Page 243: ...press the SETTINGS softkey to bring up the SETTINGS page At the bottom of the SETTINGS page verify a The REGISTRATION NO number alphanumeric matches the TAIL number alphanumeric displayed on the IFR...

Page 244: ...the transponders Antenna is restricted d Secure Antenna Shield by tightening thumbscrews 2 Perform Job Set Up with UC 584 Antenna Coupler refer to SUBTASK AMM 34 50 20 071 C 921 001 A 3 Push ECB BY SY...

Page 245: ...ys to set the values listed below 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 DIVERSITY TEST ON CHECK CA...

Page 246: ...ion File must be updated refer to AMM 31 40 00 051 801 Aircraft Computer Systems Maintenance Practices Steps 10 through this step must then be repeated 12 On the MFD scroll to the SETUP tab press the...

Page 247: ...g the UP Down DATA keys 8 With GENERIC MODE S highlighted push RETURN soft key to confirm selection This will also cause a return to the XPDR AUTO TEST page 9 Set the WOW Box Switches to W off W airbo...

Page 248: ...584 Antenna Coupler refer to SUBTASK AMM 34 50 20 071 C 921 001 A 3 Push ECB BY SYSTEM soft key Scroll to FLCS using outer knob Push inner knob to select Scroll to the listed ECB using outer knob and...

Page 249: ...ITY TEST ON CHECK CAP YES PWR LIM FAR 43 RAD47 OFF 3 Push XPDR button to go to the XPDR AUTO TEST page 4 Push CONFIG soft key to display the XPDR CONFIG SCREEN page 5 On the XPDR CONFIG SCREEN scroll...

Page 250: ...LT ENCODER is displayed press the SOURCE SELECT Soft Key until SOURCE XPDR is displayed Press the RUN TEST Soft Key 15 Make sure that an altitude reported on IFR 6000 matches L PFD altitude indication...

Page 251: ...e XPDR AUTO TEST page 10 Push CONFIG soft key to display the XPDR CONFIG SCREEN page 11 On the XPDR CONFIG SCREEN scroll to GENERIC MODE S using the UP Down DATA keys 12 With GENERIC MODE S highlighte...

Page 252: ...t a metal wall or another aircraft If necessary position the aircraft outside away from metal buildings or other aircraft Refer to Fig 501 CAUTION FAILURE TO COMPLY WITH THIS STEP AND CONTINUING WITH...

Page 253: ...OSE LDG GEAR L AFT Bus ECB L MAIN LDG GEAR L AFT Bus ECB R MAIN LDG GEAR L AFT Bus 6 Scroll to ENGINE using outer knob Push inner knob to select Scroll to the listed ECB using outer knob and highlight...

Page 254: ...s marked on test set antenna UUT ADDRESS AUTO 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...

Page 255: ...tion the test set anywhere within a 30 foot arc between the aircraft s right wingtip and the nose Press the STOP TEST button as soon as PASS message is displayed 10 Push RUN TEST soft key on Transpond...

Page 256: ...b press the SENSOR Soft Key Set the ADC PFD source selection from AUTO to ADC 2 14 On the IFR 6000 press the XPDR button once Once XPDR ALT ENCODER is displayed press the SOURCE SELECT Soft Key until...

Page 257: ...soft key on right PFD and enter the transponder code provided by the control tower for this test If no code was assigned enter 1200 C Transponder 2 MODE A C S Test using Transponder Test Set IFR6000 1...

Page 258: ...ssage is received this may take several test set position adjustments until IFR 6000 and aircraft Transponder Sync up Press STOP TEST button Repeat until all individual FAILED tests have achieved a PA...

Page 259: ...t Configuration File must be updated refer to AMM 31 40 00 051 801 Aircraft Computer Systems Maintenance Practices 13 On the MFD scroll to the SETUP tab press the SENSOR Soft Key Set the ADC PFD sourc...

Page 260: ...Y SYSTEM soft key Scroll to FLCS using outer knob Push inner knob to select Scroll to the listed ECB using outer knob and highlight Push COLLAR soft key Push CONFIRM COLLAR soft key ECB NOSE LDG GEAR...

Page 261: ...M 1 ft DIR CABLE LOSS Ignore ANT CABLE 1 ft ANT CABLE LOSS As marked on blue cable should be 0 1 dB ANT GAIN dBi 1 03 GHz As marked on test set antenna ANT GAIN dBi 1 09 GHz As marked on test set ante...

Page 262: ...10 Make sure the following appears on the Transponder Test Set IFR 6000 A CODE transponder code entered C ALT left PFD altitude indication 100 ft S CODE ICAO code assigned to this aircraft tail numbe...

Page 263: ...art 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 3 Pre position the Transpo...

Page 264: ...STOP TEST button Repeat until all individual FAILED tests have achieved a PASS It is not necessary to re run AUTO TEST AUTO TEST is a convenience feature only NOTE If POWER FREQ test Fails After press...

Page 265: ...Y SYSTEM soft key Scroll to FLCS using outer knob Push inner knob to select Scroll to the listed ECB using outer knob and highlight Push COLLAR soft key Push CONFIRM COLLAR soft key ECB NOSE LDG GEAR...

Page 266: ...IR CABLE LOSS Ignore ANT CABLE 1 ft ANT CABLE LOSS As marked on blue cable should be 0 1 dB ANT GAIN dBi 1 03 GHz As marked on test set antenna ANT GAIN dBi 1 09 GHz As marked on test set antenna UUT...

Page 267: ...d 10 Make sure the following appears on the Transponder Test Set IFR 6000 A CODE transponder code entered C ALT left PFD altitude indication 100 ft S CODE ICAO code assigned to this aircraft tail numb...

Page 268: ...r 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 3 Pre position the Transponder Test Set IFR...

Page 269: ...t s right wingtip and the nose as required and Press RUN TEST button until PASS Message is received this may take several test set position adjustments until IFR 6000 and aircraft Transponder Sync up...

Page 270: ...ple POS DECODE GLOBAL LAT 35 02 13 80 N LON 106 37 1 80 W BARO PRES ALT 5450 ft 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 o...

Page 271: ...BTASK AMM 34 50 20 071 C 701 006 ALL POST MB 500 31 016 MB 500 31 018 AND MB 500 34 030 A ADS B Out Functional Test 1 Do ADS B Out Test Set Up Refer to SUBTASK AMM 34 50 20 071 C 701 005 2 In order to...

Page 272: ...TSS SUBTYPE 1 and check the following data AA matches aircraft ICAO code displayed on the MFD Settings Page SIL 3 TCAS OP NO SELECTED ALTITUDE comparable Selected Altitude using ACP controls BARO PRE...

Page 273: ...to 20 minutes Subsequent acquisitions should take no more than 150 seconds This test must be done prior to GPS position acquisition and extinguishing of the ADS B FAIL indicator 1 Power up the aircraf...

Page 274: ...he BUS TIE to OPEN F Disconnect WOW Box from aircraft Refer to AMM 20 00 04 051 801 Weight On Wheels WOW Box Connect Disconnect G If on jacks lower aircraft and remove jacks Refer to AMM 07 10 00 051...

Page 275: ...ANSPONDER 1 A B B 1 2 3 2 1 4 Transponder Adjustment Test Figure 501 Sheet 1 of 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY NOTED 34 50 20 CONFIG C Page 541 S...

Page 276: ...TEST SET AND ANTENNA BUILDING BUILDING HANDLE TNG CONNECTION CABLE TO TEST SET FLAT ANTENNA ANTENNA PATTERN BEAMWIDTH 20 VERTICAL 25 HORIZONTAL Transponder Adjustment Test Figure 502 Sheet 1 of 1 000...

Page 277: ...nnunciation Figure 503 Sheet 1 of 1 ALL POST MB 500 34 030 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY NOTED 34 50 20 CONFIG C Page 543 Sep 30 20 2020 Eclipse A...

Page 278: ...EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 THIS PAGE INTENTIONALLY LEFT BLANK EFFECTIVITY NOTED 34 50 20 CONFIG C Page 544 Sep 30 20 2020 Eclipse Aerospace Inc...

Page 279: ...under the aft baggage compartment floor 4 ADS B system failure annunciation based on the GPS 3 position source failure is located in the cockpit on the lower left instrument panel 3 Operation A The A...

Page 280: ...EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 THIS PAGE INTENTIONALLY LEFT BLANK EFFECTIVITY ALL POST MB 500 34 030 34 50 21 Page 2 Sep 30 20 2020 Eclipse Aerospace Inc...

Page 281: ...S E or Hobart GPU 400 or Hobart GPU 600 or Bycan PS 28100 1 For test with UC 584 antenna coupler 3 Job Set Up with UC 584 Antenna Couplers SUBTASK AMM 34 50 21 071 921 001 A A Make aircraft safe for...

Page 282: ...sed tightly against the aircraft 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 2 over t...

Page 283: ...are minimized The area on the left side of the aircraft should not be up against a metal wall or another aircraft If necessary position the aircraft outside away from metal buildings or other aircraft...

Page 284: ...t set with the ADS B test capability is available as an additional or alternate method of verifying proper operation and performance of the installed ADS B OUT function the FAA Public ADS B Performanc...

Page 285: ...ure aircraft power is off b Set WOW Box switches to W on W on ground c On IFR 6000 press XPDR mode Key until ADSB GICB UAT MAIN menu is displayed Press the ADS B MON Soft Key to display the ADS B MON...

Page 286: ...aircraft by setting the SYS BATT and START BATT switches to OFF and the BUS TIE to OPEN E Disconnect WOW Box from aircraft Refer to AMM 20 00 04 051 801 Weight On Wheels WOW Box Connect Disconnect F I...

Page 287: ...ONDER 1 A B B 1 2 3 2 1 4 Transponder Adjustment Test Figure 501 Sheet 1 of 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY ALL POST MB 500 31 016 34 50 21 Page 5...

Page 288: ...GS SHOULD BE AT OBLIQUE ANGLES OCCUPYING 20 BEAMWIDTH IFR 6000 TEST SET AND ANTENNA BUILDING BUILDING HANDLE TNG CONNECTION CABLE TO TEST SET FLAT ANTENNA ANTENNA PATTERN BEAMWIDTH 20 VERTICAL 25 HORI...

Page 289: ...01 A Make sure that the aircraft is in same configuration as it was when the removal task was completed Refer to AMM 34 50 21 001 801 Transponder Removal B As required make sure that transponder is co...

Page 290: ...ight Primary Flight Display PFD C Remove the warning placard D Do an adjustment test of the transponder system Refer to AMM 34 50 20 071 C 801 Transponder Adjustment Test E If all other maintenance is...

Page 291: ...ARITY NOTE WING INSP R ENG L ENG WING Transponder Removal Installation Avio NG 1 5 display shown Figure 401 Sheet 1 of 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTI...

Page 292: ...EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 THIS PAGE INTENTIONALLY LEFT BLANK EFFECTIVITY ALL 34 50 21 Page 404 Inst Sep 30 20 2020 Eclipse Aerospace Inc...

Page 293: ...their respective diversity transponder s A Remove the protective caps from the electrical connectors B Put the transponder lower and or if installed upper antenna relay 1 on the structure and align t...

Page 294: ...5 milliohms or less 4 Job Close Up SUBTASK AMM 34 50 23 041 921 002 A Remove all tools equipment and unwanted material from the work area B If removed install the air conditioning ducts Refer to AMM 2...

Page 295: ...ation Avio NG 1 5 Display shown Figure 401 Sheet 1 of 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY 0001 0104 0113 0115 0120 0123 0124 POST SB 500 99 002 0105 0...

Page 296: ...Revision No 34 21 THIS PAGE INTENTIONALLY LEFT BLANK EFFECTIVITY 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 34 50 2...

Page 297: ...ectrical connector 3 from switch body 6 with extraction tool 18 234 3 Identify the two extraction slots positioned on either side of the cap 7 Extract the switch cap 7 by using the Cap Extractor Tool...

Page 298: ...emove switch body 6 from the bracket 1 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY ALL POST MB 500 34 030 34 50 26 Page 402 Rem Sep 30 20 2020 Eclipse Aerospace...

Page 299: ...Fail Indicator Removal Installation Figure 401 Sheet 1 of 2 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY ALL POST MB 500 34 030 34 50 26 Page 403 Rem Sep 30 20 2...

Page 300: ...S B Fail Indicator Removal Installation Figure 401 Sheet 2 of 2 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY ALL POST MB 500 34 030 34 50 26 Page 404 Rem Sep 30...

Page 301: ...the locking sleeve 4 onto the switch body 6 and sliding it forward against the mounting bracket 1 3 From the front of the switch body 6 locate the two slot head integral mounting screws 8 in the base...

Page 302: ...l 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 Return To Service After Maintenance EA500 Aircraf...

Page 303: ...Fail Indicator Removal Installation Figure 401 Sheet 1 of 2 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY ALL POST MB 500 34 030 34 50 26 Page 403 Inst Sep 30 20...

Page 304: ...B Fail Indicator Removal Installation Figure 401 Sheet 2 of 2 EA500 Aircraft Maintenance Manual 06 117751 Temporary Revision No 34 21 EFFECTIVITY ALL POST MB 500 34 030 34 50 26 Page 404 Inst Sep 30...

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