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ARTEX PRODUCTS / ACR ELECTRONICS, INC

DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL

B406-4 (453-5004)

Page 35 of 70

25-62-03

7)

Activate the ELT by placing the cockpit r

emote switch in the “ON” position. The panel light will illuminate

and stay on steady.
NOTE:

The LED on the ELT will begin flashing continuously when the ELT is activated.

8)

Listen for 3 audible sweeps on the receiver, which takes about 1 second.

9)

Verify the buzzer sounds immediately upon activation.

10)

Return the remote switch to the “OFF” position while monitoring the ELT LED activity when the ELT
enters the “OFF” condition.

If the ELT is working properly, the LED will stay on for approximately 1

second and then turn off.
NOTE:

This test also completes the requirement to check ELT controls by verifying operation of the
remote switch.

11)

Refer to Table 6 on page 37 if the ELT LED displays a series of flashes.

SUBTASK 25-62-03-750-013

R.

Antenna Test

–

Item 7

CAUTION: DO NOT ALLOW THE DURATION OF THIS TEST TO EXCEED 5 SECONDS.

1)

Tune a low quality AM receiver (i.e., radio) to 121.5 MHz.
NOTE:

The aircraft transceiver is not recommended for this test, because it is too sensitive to verify
the integrity of the antenna system and it may pick up a weak signal even if the antenna is

disconnected from the ELT. An AM radio provides a better level of confidence for this test.

2)

Place the radio approximately six inches from the antenna.

3)

Activate the ELT by placing the cockpit remote switch in the “ON” position.

NOTE:

Perform this test within the first five minutes after the hour UTC.

4)

Listen for 3 audible sweeps on the radio, which takes about 1 second. An audible signal verifies energy
is being transmitted by the antenna.

5)

Reset the ELT by placing the cockpit remote switch in the “ARM” position.

SUBTASK 25-62-03-750-014

S.

Inspection and Test Documentation

–

Item 8

1)

Make an appropriate entry in the aircraft maintenance records (i.e., logbook), including the date the ELT
inspection and testing was satisfactorily completed.

2)

In addition to the requirements of Step (1), for aircraft operating under Canadian authority and
following satisfactory completion of performance testing, the date on which the test was performed shall
be marked on the ELT external casing in a legible and permanent manner.

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Содержание B406-4

Страница 1: ...S INC 5757 Ravenswood Rd Ft Lauderdale FL 33312 Cage Code 18560 25 62 03 B406 4 Emergency Locator Transmitter Description Operation Installation and Maintenance Manual This manual includes data for the equipment that follows Component Part No Model No Emergency Locator Transmitter 453 5004 B406 4 ...

Страница 2: ... contained herein ACR Electronics is not liable in the event of incidentals special consequential or any other damages in connection with or arising from furnishing performance or use of this manual Reproduction of this publication or any portion thereof by any means is prohibited For further information contact Sales ACR Electronics 5757 Ravenswood Rd Fort Lauderdale FL 33312 Telephone 954 981 33...

Страница 3: ...22 2000 B DCN 1641 Apr 11 2001 B DCN 1747 Jul 19 2001 B DCN 1965 Apr 04 2002 B DCN 2115 Dec 10 2002 B DCN 2356 Feb 11 2004 C DCN 2968 Mar 20 2007 C DCN 3174 Feb 26 2008 C DCN 3282 Aug 25 2008 D DCA W9414 Apr 06 2010 E ECO 14756 Jul 28 2011 F ECO 15177 Aug 27 2012 G ECO 15330 Mar 1 2013 H ECO 15410 Jun 20 2013 J ECO 15510 Oct 14 2013 K ECO 15830 Dec 01 2014 L ECO 16361 May 11 2016 M ECO 16887 Mar 3...

Страница 4: ...UCTS ACR ELECTRONICS INC DESCRIPTION OPERATION INSTALLATION AND MAINTENANCE MANUAL B406 4 453 5004 Page 4 of 70 25 62 03 SERVICE BULLETIN LIST SERVICE BULLETIN NO ISSUE DATE SUBJECT MANUAL REV NO MANUAL REV DATE ...

Страница 5: ... 14 13 Introduction 10 Oct 14 13 45 Oct 14 13 11 Oct 14 13 46 Oct 14 13 12 Oct 14 13 47 Oct 14 13 13 Oct 14 13 48 Oct 14 13 14 Oct 14 13 49 Oct 14 13 15 Oct 14 13 50 Oct 14 13 16 Oct 14 13 51 Oct 14 13 Description and Operation 17 Oct 14 13 52 Oct 14 13 18 Oct 14 13 53 Oct 14 13 19 Oct 14 13 54 Oct 14 13 20 Oct 14 13 55 Oct 14 13 21 Oct 14 13 56 Oct 14 13 22 Oct 14 13 57 Oct 14 13 23 Oct 14 13 58 ...

Страница 6: ...0D Compliance 11 4 Frequency Allocations 13 A Application 13 B Discussion 13 5 List of Acronyms Abbreviations and Definitions 14 6 References 16 A Regulatory Documents 16 B Other Documents 16 DESCRIPTION AND OPERATION 17 1 Description 17 A Functional Overview 17 B Components 18 2 Operation 21 A Operational Overview 21 B Normal Operation 22 C Manual Activation 22 D ELT Reset 22 E Functional Check 2...

Страница 7: ...z Power Output Measurement Item 5e 32 N Current Draw Test Item 5f 32 O Digital Message Verification Item 5g 33 P ELT Reset Check Item 5h 34 Q Installed Transmitter Test Item 6 34 R Antenna Test Item 7 35 S Inspection and Test Documentation Item 8 35 3 Troubleshooting 36 A Self Test Error Troubleshooting Guidelines 36 B ELT Troubleshooting Guidelines 38 REMOVAL 39 1 ELT 39 A ELT Removal 39 2 Batter...

Страница 8: ... 7 ELT Installation 58 A Installation and Test 58 B Harness ELT Receptacle Sealing 59 C Installation Documentation 59 8 Battery Pack Installation 60 A Battery Reinstallation 60 B New Battery Installation 61 APPENDIX A ELT REGISTRATION 62 1 Background Information 62 A Hex ID Code 62 B Reason for Registration 62 C Registration Information Resources 62 2 Registration 63 A Responsibility 63 B Required...

Страница 9: ...oval 40 Figure 13 B406 4 ELT Outline and Dimensions 44 Figure 14 Typical Mounting Tray Installation 45 Figure 15 Rod Antenna 110 320 and Blade Antenna 110 328 01 Outlines and Dimensions 47 Figure 16 Blade Antennas 110 333 and 110 337 Outlines and Dimensions 48 Figure 17 Blade Antenna 110 337 11 Outline and Dimensions 49 Figure 18 Remote Switch Panel Assembly Outline and Dimensions 50 Figure 19 Buz...

Страница 10: ... SUBTASK 25 62 03 990 002 B Application 1 This manual constitutes supporting data documentation for the B406 4 ELT including a Description and Operation b Test and Fault Isolation includes inspection criteria c Removal d Installation e Registration f Illustrated Parts List 2 In the United States the B406 4 ELT must be installed and maintained in accordance with the requirements herein and 14 CFR F...

Страница 11: ...t have separate approval for installation in an aircraft The article may be installed only if performed under 14 CFR Part 43 or the applicable airworthiness requirements 2 Transport Canada Type Certificate Data Sheet AP 47 Issue 2 3 Industry Canada Certification Number 1215873110AF 4 JTSO 2C126 5 COSPAS SARSAT Certificate No 112 or 170 SUBTASK 25 62 03 990 002 B Battery CAUTION LITHIUM BATTERY SAF...

Страница 12: ... Operational Shock and Crash Safety Vibration X 9 0 Explosion R 10 0 Waterproofness X 11 0 Fluids Susceptibility X 12 0 Sand and Dust X 13 0 Fungus X 14 0 Salt Spray X 15 0 Magnetic Effect Z 16 0 Power Input A 17 0 Voltage Spike Z 18 0 Audio Frequency Susceptibility Z 19 0 Induced Signal Susceptibility 204 20 0 Radio Frequency Susceptibility B 21 0 Emission of RF Energy X 22 0 Lightning X 23 0 Lig...

Страница 13: ...25 MHz In order to comply with COSPAS SARSAT frequency allocation requirements changes to the 406 MHz frequency may occur since the original release of this product 2 While the original B406 4 ELTs covered by this manual transmit on 406 025 MHz current B406 4 ELTs may not The product identification label on each ELT specifies the transmitting frequencies of the individual ELT The 406 MHz component...

Страница 14: ... for the International COSPAS SARSAT Program DER Designated Engineering Representative An individual qualified and designated by the FAA to approve or recommend approval of technical data to the FAA Drip Loop Extra wire length used to form a U shaped bend in a wire or cable Water or other fluids will flow down to the bottom of the loop and drip off Electrical connections are made at the top of the...

Страница 15: ... RTV A rubbery silicon based adhesive typically used to prevent vibration problems and water intrusion SAR Search and Rescue Screen Room The term Screen Room within the context of this document refers to a room designed to suppress RF signals such that the broadcast of an ELT placed in the screen room cannot reach the SAR satellite system Service Loop A length of wire or cable at the connection po...

Страница 16: ...raft Alterations f FAR Part 43 Maintenance Preventive Maintenance Rebuilding and Alteration g FAR Part 91 General Operating and Flight Rules 4 Canada a CAR Part V Airworthiness b CAR Part VI General Operating and Flight Rules 5 COSPAS SARSAT a C S G 005 Cospas Sarsat Guidelines on 406 MHz Beacon Coding Registration and Type Approval b C S S 007 Handbook of Beacon Regulations 6 RTCA The following d...

Страница 17: ...tically The 121 5 243 0 transmitter will continue to operate until the batteries are exhausted which is at least 50 hours 4 The 406 MHz transmitter produces a much more accurate position typically 3 kilometers as compared with 15 to 20 kilometers for 121 5 243 0 MHz transmitters When coupled to the aircraft navigation system via the ELT NAV Interface B the accuracy improves to approximately 100 me...

Страница 18: ... extremely harsh environments and have been subjected to the rigorous environmental testing required by COSPAS SARSAT for certification Figure 1 B406 4 ELT and Mounting Frame Assembly 2 The cockpit mounted Control Panel G737 remote switch panel assembly is a backlit panel comprised of an ELT status indicator light and a control switch which allows an operator to manually activate the ELT for testi...

Страница 19: ...Figure 3 Buzzer 4 The battery pack for the B406 4 ELT consists of four D size lithium manganese dioxide cells connected in series In an effort to increase the safety of the battery pack a number of features were designed into the battery pack To prevent the cells from being charged diodes are connected across each cell and fuses are connected to the output See Figure 4 Battery Pack Assembly Figure...

Страница 20: ...ND MAINTENANCE MANUAL B406 4 453 5004 Page 20 of 70 25 62 03 5 Five dual input antennas are approved for use with the B406 4 ELT Selection of the proper antenna is dependent upon end use aircraft configuration speed and other factors See Figure 5 Antennas Figure 5 Antennas ...

Страница 21: ...gram 3 ELT operation is designed to prevent human error and misuse in regards to automatic activation The ELT cannot be activated by dropping rough handling or during shipping 4 When the ELT is activated the presence of the emergency sweep tone and the illuminated cockpit remote switch panel light indicates an active ELT The cockpit ELT remote panel light must immediately illuminate upon ELT activ...

Страница 22: ...espectively the ELT will automatically activate on impact SUBTASK 25 62 03 870 004 D ELT Reset 1 If the ELT is activated accidently it will need to be reset 2 Reset the ELT from the cockpit by moving the remote switch to the ON position waiting approximately one second and then moving it back to the ARM position If the switch is already in the ON position move it to the ARM position 3 Reset the EL...

Страница 23: ...to TSO C126 FAA Reference 98 130S 108 February 6 1998 CRITERIA PARAMETER CHARACTERISTIC Temperature Storage 55 C to 85 C Operating 20 C to 70 C Mechanical Vibration 10 g Sinusoidal 6 1 GRMS Random Shock 500 g for 4 ms Crashworthiness 100 g for 23 ms Humidity 95 for 240 hours Penetration 55 lbs from 6 in 25 kg from 15 cm Crush 1 000 lbs 454 kg Altitude 55 000 ft 16 764 m Automatic Activation G Swit...

Страница 24: ...hase L G1D 121 5 and 243 0 MHz Amplitude Modulation A3X Transmitter Duty Cycle 406 MHz 440 ms 1 or 520 ms 1 every 50 seconds 5 121 5 and 243 0 MHz Continuous Peak Effective Radiated Power PERP 406 MHz 5 W 37 2 dB PERP or EIRP for 24 hrs 20 to 55 C 121 5 and 243 0 MHz Min 50 mW 17 dBm PERP for 50 hrs 20 to 55 C or 100 mW EIRP 20 dBm for 48 hrs 20 to 55 C Occupied Bandwidth 406 MHz 20 KHz max 121 5 ...

Страница 25: ...43 0 406 MHz VSWR 121 5 and 243 0 MHz 2 0 1 Max 406 MHz 1 5 1 Max 121 5 243 0 MHz 2 0 1 or better 406 MHz 1 5 1 or better 121 5 243 0 MHz 2 0 1 Max 406 MHz 1 5 1 Max Polarization Vertical Monopole Radiation Pattern 121 5 243 MHz Omnidirectional 406 MHz Hemispherical Impedance ohms 50 Nominal Weight 0 45 lbs 0 20 kg 1 20 lbs 0 54 kg 0 76 lbs 0 34 kg 1 30 lbs 0 59 kg 1 60 lbs 0 73 kg Coax Cable RG 1...

Страница 26: ...tion and poor condition and d Antenna including trailing antenna for poor condition insecure mounting and improper operation SUBTASK 25 62 03 990 002 B Canada 1 CAR Part VI Standard 625 Appendix C requires the ELT to be inspected at intervals not exceeding 12 months 2 All maintenance and testing shall be performed in accordance with the requirements of CAR Part V Standard 571 Appendix G which requ...

Страница 27: ...quirements only in Canada in addition to meeting the other inspection and test requirements listed in Table 5 ITEM NO DESCRIPTION BY 1 Coax Cable and Wiring Connections Inspection 2 ELT Mounting Tray and Hardware Inspection 3 ELT Battery Pack Inspection 4a G Switch Functional Check 4b G Switch Functional Check Helicopter Models Only 5a 121 5 MHz Frequency Measurement 5b Audio Modulation Check 5c 1...

Страница 28: ...ins or antenna connections of ELT 4 Replace remote switch if any of the following conditions are true a Cracks on the casing b Illegible lettering on the face c Damaged wiring and connections of remote switch SUBTASK 25 62 03 220 003 E Battery Pack Inspection Item 3 CAUTION THE BATTERY PACK CONTAINS ELECTROSTATIC DISCHARGE SENSITIVE ESD COMPONENTS AND AS SUCH IT MUST BE HANDLED WITH CARE IF POSSIB...

Страница 29: ...the ELT switch is in the OFF position 6 Monitor 121 5 MHz on an AM receiver 7 Activate the ELT by using a rapid forward i e throwing motion in the direction of the arrow on the ELT label followed by a rapid reversing action 8 Verify activation by listening for the aural sweep tone on the receiver 9 Reset the ELT by toggling the control switch to the ON position and then back to the OFF position SU...

Страница 30: ... If the ELT is left activated beyond the first 30 seconds additional time is added in 30 second increments NOTE Careful planning of the performance tests is necessary to avoid activating the ELT more than necessary Plan the performance testing in a manner that allows tests to be run concurrently and test equipment settings to be quickly switched from one test to another By doing so the three minut...

Страница 31: ...SUBTASK 25 62 03 750 004 above 2 Monitor 121 5 MHz on an AM receiver 3 Listen for the aural sweep tone on the receiver The audio should sound like an ELT SUBTASK 25 62 03 750 006 K 121 5 243 0 MHz Power Output Measurement Item 5c 1 Connect the measuring device referring to SUBTASK 25 62 03 750 003 on page 29 2 Activate the ELT if necessary by placing the control switch in the ON position 3 Wait th...

Страница 32: ...Read the displayed amplitude of the 406 MHz burst that follows the three minute wait period The amplitude must be within the minimum specified for 406 MHz in Table 3 on page 24 at the output terminal 5 Deactivate the ELT by placing the control switch in the OFF position SUBTASK 25 62 03 750 009 N Current Draw Test Item 5f CAUTION EXERCISE EXTREME CAUTION TO AVOID CAUSING A SHORT CIRCUIT CONDITION ...

Страница 33: ... with SUBTASK 25 62 03 450 001 on page 60 SUBTASK 25 62 03 750 010 O Digital Message Verification Item 5g 1 Set the 453 1000 ELT Test Set ETS beacon reader to receive and decode the ELT digital message Refer to the ETS operating manual 570 1000 for ETS operating instructions and additional details NOTE A beacon reader equivalent to the ETS may be used provided it is capable of receiving and decodi...

Страница 34: ... 37 SUBTASK 25 62 03 750 011 P ELT Reset Check Item 5h 1 Place the ELT control switch in the ON position 2 Return the switch to the OFF position 3 If the ELT is working properly the LED will stay on for approximately 1 second and then turn off If a series of flashes are displayed refer to Table 6 on page 37 NOTE A 5 flash error indication will occur if the ELT is programmed with a location protoco...

Страница 35: ...er i e radio to 121 5 MHz NOTE The aircraft transceiver is not recommended for this test because it is too sensitive to verify the integrity of the antenna system and it may pick up a weak signal even if the antenna is disconnected from the ELT An AM radio provides a better level of confidence for this test 2 Place the radio approximately six inches from the antenna 3 Activate the ELT by placing t...

Страница 36: ... Remote switch harness connector loose or disconnected at ELT Check connector and tighten as necessary ELT connector pins bent or broken Check condition of connector pins and repair or replace as necessary Connector pins 5 and 8 jumper open internal to remote switch harness connector at ELT end Repair open jumper 3 Flash Indicates a 406 MHz transmission problem Open or short condition on antenna o...

Страница 37: ...repaired in field Return to factory for servicing 5 Flash Indicates there is no navigation position data present Aircraft navigation system off Turn on navigation system Faulty system interface wiring or connections Check wiring and connections for continuity and security No 453 6501 ELT NAV Interface B installed Install 453 6501 ELT NAV Interface B Reprogram to short message 7 Flash Indicates a b...

Страница 38: ...rt circuit Check for frayed insulation Verify integrity of all crimp and solder connections ELT will not turn off Battery too low to support 406 burst and causes circuit to reset Remove battery pack to disable ELT and replace battery pack Turn off ELT using local switch If ELT turns off Defective remote panel harness reset circuit wiring Check wiring continuity and repair as necessary Defective re...

Страница 39: ...thumbscrews 3 Slide the mounting frame cap back away from the ELT 4 Lift the protective top cover up away from the ELT and set it aside 5 Disconnect the two antenna coax cables from the ELT 6 Disconnect the harness receptacle from the ELT if necessary NOTE The receptacle may disconnect when the mounting frame cap is pulled back 7 Lift the ELT up from the connector end NOTE Careful use of a flat bl...

Страница 40: ...HE BATTERY PACK IS CONNECTED TO THE ELT VIA SHORT INTERCONNECT HARNESSES WHICH LIMIT THE DISTANCE THE TWO COMPONENTS CAN BE SEPARATED UNTIL THE HARNESSES ARE DISCONNECTED 1 See Figure 12 Battery Pack Removal Figure 12 Battery Pack Removal 2 Turn the ELT upside down such that the battery pack is bottom side up 3 Remove the four retaining screws 4 Lay the ELT on its side while keeping the ELT and ba...

Страница 41: ...horization 1 Upon receipt of such notice ACR Electronics will issue a Return Material Authorization RMA number which then authorizes return of the material or equipment to the following address Repair and Overhaul ACR Electronics 5757 Ravenswood Road Fort Lauderdale FL 33312 USA Phone 954 981 3333 Fax 954 983 5087 a Failure to obtain a RMA number and provide the details listed in SUBTASK 25 62 03 ...

Страница 42: ...n registration information NOAA will provide registrants with proof of registration and change of registration postcards B TSO C126 Paragraph D 1 TSO approval of the ELT does not constitute installation approval All ELT installations are subject to field approval for a given airframe by either an approved FAA DER or FAA FSDO For installations outside the US contact your local civil aviation regula...

Страница 43: ...mounting location 2 DO 182 6 2 2 b recommends that a To maximize the probability of the ELT transmitting a detectable signal after a crash all ELT system components which must survive a crash intact e g transmitter and external antenna should be attached to the airframe in such a manner that the attachment system can support a 100 g load ELT weight x 100 ELT antenna weight x 100 etc applied throug...

Страница 44: ... AIRCRAFT SKIN INDUCES CRASH HIDING VIBRATIONS AND PROVIDES A VERY POOR MOUNTING SURFACE CAUTION AVOID LOCATING THE ELT WHERE IT WILL BE SUBJECTED TO UNPROTECTED EXPOSURE TO HARSH CHEMICAL FLUIDS SUCH AS DEICING COMPOUNDS THESE TYPES OF CHEMICAL FLUIDS CAN PROMOTE CRACKING AND FRACTURING OF THE ELT MOUNTING FRAME AND HOUSING COMPONENTS BY DEGRADING THE STRUCTURAL INTEGRITY OF THESE COMPONENTS THES...

Страница 45: ...ng structure as appropriate for the specific installation 3 Align the mounting tray 452 5050 on the mounting structure such that the arrow on the tray is within 10 of the longitudinal axis of the aircraft and pointing in the direction of flight 4 Mark the four holes needed for mounting the tray using the tray as a pattern The hole pattern is also illustrated in Figure 13 B406 4 ELT Outline and Dim...

Страница 46: ...llations SUBTASK 25 62 03 450 002 C Installation NOTE Refer to the airframe manufacturer s written instructions and AC 43 13 2 Chapter 3 for antenna installation practices and requirements 1 Install a doubler plate if necessary to meet rigidity requirements A 20 lb 9 1 kg force applied to the antenna in all directions should not cause an appreciable distortion in the aircraft skin 2 Install a grou...

Страница 47: ...PRODUCTS ACR ELECTRONICS INC DESCRIPTION OPERATION INSTALLATION AND MAINTENANCE MANUAL B406 4 453 5004 Page 47 of 70 25 62 03 Figure 15 Rod Antenna 110 320 and Blade Antenna 110 328 01 Outlines and Dimensions ...

Страница 48: ...ARTEX PRODUCTS ACR ELECTRONICS INC DESCRIPTION OPERATION INSTALLATION AND MAINTENANCE MANUAL B406 4 453 5004 Page 48 of 70 25 62 03 Figure 16 Blade Antennas 110 333 and 110 337 Outlines and Dimensions ...

Страница 49: ...ARTEX PRODUCTS ACR ELECTRONICS INC DESCRIPTION OPERATION INSTALLATION AND MAINTENANCE MANUAL B406 4 453 5004 Page 49 of 70 25 62 03 Figure 17 Blade Antenna 110 337 11 Outline and Dimensions ...

Страница 50: ...e and Dimensions Figure 18 Remote Switch Panel Assembly Outline and Dimensions SUBTASK 25 62 03 450 002 B Installation 1 Provide an opening in the instrument panel or other mounting location which meets the dimensional requirements shown in Figure 18 Remote Switch Panel Assembly Outline and Dimensions 2 Mount Dzus rails on the sides of the opening if necessary See Figure 18 Remote Switch Panel Ass...

Страница 51: ...e buzzer is loud enough to be heard outside the aircraft when the engine s is not running When the engine s is running the LED on the cockpit remote switch panel will warn the pilot the ELT is active SUBTASK 25 62 03 450 002 B Installation 1 Fabricate a bracket suitable for supporting the buzzer See Figure 19 Buzzer Outline and Dimensions NOTE Refer to the aircraft manufacturer s written instructi...

Страница 52: ...h quality conductor meeting MIL W 16878 M22759 M27500 or a commercial equivalent acceptable for use in aircraft applications d Provide a Drip Loop in the remote switch harness connection to the ELT to divert moisture from the connector See TASK 25 62 03 990 805 on page 14 for a definition e Provide a Service Loop in the remote switch harness connection to the remote switch panel such that the asse...

Страница 53: ...ARTEX PRODUCTS ACR ELECTRONICS INC DESCRIPTION OPERATION INSTALLATION AND MAINTENANCE MANUAL B406 4 453 5004 Page 53 of 70 25 62 03 Figure 20 Remote Switch Panel Harness Wiring Diagram ...

Страница 54: ...in 12 to the Master Lighting Test circuit i Pin 13 to the 5VAC Lighting circuit j Pin 14 to aircraft ground k Prepare the wires as described in Steps 2 a and 2 b 4 Terminate the remote switch panel end of all wires in an MS24266R16B24S7 connector in accordance with the aircraft manufacturer s written instructions or AC43 13 1 as applicable See Figure 20 Remote Switch Panel Harness Wiring Diagram o...

Страница 55: ...as applicable SUBTASK 25 62 03 450 003 D ELT 12 Pin Receptacle Wiring Fabrication and Installation 1 Fabricate a ground wire long enough to reach from the harness ELT receptacle to aircraft ground NOTE This wire will be crimped in the same pin as the wire running from Pin 11 of the ELT receptacle to the cockpit remote switch panel ONLY if a ground wire is connected between the ELT and the remote s...

Страница 56: ... Pin 8 of the receptacle NOTE Terminal pins may be removed from the receptacle using Molex extraction tool 11030002 or equivalent b Insert the harness ELT wire ends into the receptacle See Figure 20 Remote Switch Panel Harness Wiring Diagram on page 53 c Ring out the wiring between the remote switch panel and the ELT verifying proper continuity d Insert the buzzer wire YELLOW in Pin 2 of the recep...

Страница 57: ...r s written instructions or as described in AC 43 13 1 Chapter 11 15 as applicable See Figure 20 Remote Switch Panel Harness Wiring Diagram on page 53 SUBTASK 25 62 03 450 007 H Buzzer Connections 1 Connect the RED wire to the 28 VDC aircraft battery power source 2 Connect the BLUE wire to remote switch panel plug Pin 8 3 Connect the YELLOW wire to ELT receptacle Pin 2 4 Connect the BLACK wire to ...

Страница 58: ...e protective top cover assembly 452 3052 on the ELT by fitting the cover locking slots over the locking ears on the ELT 6 Push the cover toward the connector end of the ELT and seat it down in place on the ELT 7 Route the antenna coax cables through the appropriate mounting frame cap access holes 8 Connect the antenna coax cables to the ELT 9 Connect the 12 pin harness receptacle to the ELT 10 Sli...

Страница 59: ...on of the ELT Use the following procedure NOTE Perform the sealing process once all tests have been satisfactorily completed and all harness connections have been verified to be correct a Remove the mounting frame cap from the ELT b Unplug the receptacle from the ELT or pull the receptacle free of the mounting frame cap as applicable c Seal the back of the receptacle with GE RTV 162 or equivalent ...

Страница 60: ... and testing 2 See Figure 23 Battery Pack Installation Figure 23 Battery Pack Installation 3 Apply a thin coating of non petroleum based silicone grease such as GE G 635 to the rubber seal to facilitate installation and allow the ELT and battery pack to slide together without binding on the rubber seal 4 Lay the battery pack and ELT on their sides such that the two components are aligned but separ...

Страница 61: ...3 flash errors which are generated because the ELT is not installed and connected to an antenna etc 7 A 5 flash error will be indicated if the ELT is programed with a location protocol and is generated because the ELT is not connected to the navigation system and receiving position data c If a 7 flash error code is indicated there is a problem with the battery or battery connection wiring Refer to...

Страница 62: ...pped with a navigation interface device SUBTASK 25 62 03 990 002 B Reason for Registration 1 ELT registration aids the Rescue Coordination Center RCC in determining if an actual emergency exists by accessing a database containing the registration information which facilitates inquiries as to the whereabouts of the aircraft existence of a flight plan etc a Owner s name b Address c Telephone number ...

Страница 63: ...information i e address telephone number etc filed as part of the registration process should be kept up to date SUBTASK 25 62 03 990 003 C Where to Register 1 In the United States the National Oceanic and Atmospheric Administration NOAA is the registration agency 2 Specific registration web sites and information may be found at a The Artex products web site at www acrartex com which has links to ...

Страница 64: ...m number assigned to the part c Refer to the associated parts list and find the item number in the Fig Item column 2 If the part number is known a Refer to the parts list and find the part in the Part column b Note the figure number and item number assigned to the part c Refer to the illustration in the applicable IPL figure to find attaching hardware and related assembly parts 3 In cases where mu...

Страница 65: ...to identify added parts alternate parts and service bulletin modified parts SUBTASK 25 62 03 990 002 B Part Column 1 This column contains the manufacturer s part number for each part SUBTASK 25 62 03 990 003 C Nomenclature Column 1 This column contains descriptive nomenclature for each part service bulletin numbers affecting the part and obsolete part numbers 2 The indenture system used in the Nom...

Страница 66: ...to and interchangeable with other parts within the same item number variant group or other item numbers if designated Superceded By SUPSD BY The part is replaced by and is not interchangeable with the item number designated in the notation Supersedes SUPSDS The part replaces and is not interchangeable with the item number designated in the notation Replaced By REPLD BY The part is replaced by and ...

Страница 67: ...K 25 62 03 990 804 4 Detailed Parts List Figure 25 B406 4 ELT Main Assembly and Installation FIG ITEM PART 1234 NOMENCLATURE UPA 24 01 452 3052 Protective Top Cover Assembly 1 02 452 5052 Mounting Frame Cap Assembly 1 03 452 5050 Mounting Tray Assembly 1 ATTACHING PARTS 201 0810 Screw PHP 8 32 x 5 8 SS 4 246 0008 Washer Flat 1 2 SS 8 4 ...

Страница 68: ...AL B406 4 453 5004 Page 68 of 70 25 62 03 247 0800 Washer Lock Internal Tooth SS 8 4 241 0832 Nut 8 32 x 1 4 Hex SS 4 04 453 5004 B406 4 Main Assembly 1 591 0999 Label Hex Code 1 591 0429 Label Country Code 1 05 452 0133 406 Lithium Battery Pack 1 ATTACHING PARTS 217 0606 Screw with O Ring 4 ...

Страница 69: ...4 453 5004 Page 69 of 70 25 62 03 Figure 26 Electrical Components FIG ITEM PART 1234 NOMENCLATURE UPA 25 01 453 0161 Control Panel G737 1 591 0428 Label ELT Cautionary Use Advisory Optional 1 02 151 5012 Receptacle 12 Pin 1 151 6627 Terminal Crimp Male 0 062 Dia 12 03 130 4005 Horn Mod ELT Buzzer 1 ...

Страница 70: ...FIG ITE M PART 1234 NOMENCLATURE UPA 26 01 110 337 Antenna 406 Blade 319 Dual Input 1 02 110 328 01 Antenna 406 Blade Dual Input 1 03 110 333 Antenna Tri Band Blade White Dual Input 1 04 110 320 Antenna Tri Band Rod Dual Input 1 05 110 337 11 Antenna 406 Blade w prot edge 1 611 6013 04 Cable Coax BNC to BNC 6 ft 1 611 6052 Cable Coax TNC to TPS 6 ft 1 ...

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