Ameri-King AK-451 Series Installation And Operation Manual Download | Manualshive

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3.3.5

TRANSMITTER FUNTIONAL TEST FOR ELT-(S) ONLY

The ELT-(S) should be tested every month.

3.3.5.1 Main Switch ON / OFF / SELF TEST Operation

:

The ELT-(S) has an "OFF" position. This allows the beacon to be handled or shipped
without 'nuisance' activation. Care should be taken when transporting or shipping the
ELT-(S) not to move the switch or to allow packing material to become lodged such
as to toggle the switch.
Main Switch, alternate / alternate / momentary positions:



"

ON

:" Alternate position. ELT-(S) transmits immediately. Green ON light on the

main unit flashes, 1 second ON, 4 seconds OFF. The ELT swept Tone must be
heard on the 121.5 MHz VHF Radio.



"

OFF

:" Alternate position. The ELT-(S) is turned off.



"

SELF TEST

:" Momentary position. ELT-(S) self-test is confirmed after the

switch is held for 25 seconds. If the self-test is passed, the Green ON light must
be extinguished. ELT swept Tone must be silent on the 121.5 MHz VHF Radio.

The ELT-(S) system is fully self-tested.

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Summary of Contents for AK-451 Series

Page 1: ...ATION AND OPERATION MANUAL FOR MODEL AK 451 Series 406 MHz ELT Emergency Locator Transmitter with GPS NAV position AMERI KING CORPORATION 17881 Sampson Lane Huntington Beach CA 92648 Tel 714 842 8555 Fax 714 842 4235 Email ameriking9 aol com www ameri king com ...

Page 2: ... 4 2 1 2 4 3 and 1 2 4 4 revised NC 2 Para 2 4 5 deleted T N K V 9 10 07 Add Volume 2 for AK 451 PLB for clarity NC 3 Para 1 2 1 c and 3 1 c revised T N K V 9 11 07 Para 3 3 5 added Volume 2 Para 4 1 4 3 2 revised NC 4 Para 1 2 1 b and 2 2 3 revised T N K V 9 26 07 NC 4 1 Para 1 2 2 2 2 2 4 6 FAA form 337 2 5 1 revised TSO C142 information RTCA DO 160E form for TSO C 227 deleted QP KV 6 16 08 ...

Page 3: ...ved updated QP KV 11 26 08 NC 4 1d Brazil Anatel Approval updated T N KV 11 27 08 NC 4 1e Japan Approval Certificates added T N KV 11 30 08 NC 4 1f FAA and EASA Antenna approvals added T N KV 01 27 12 NC 4 1g Clarify statement for battery pack service T N KV 01 09 12 NC 4 1h Delete Optional Multi Axes G Sw Provision 12 16 13 19 KV KV 7 5 14 ...

Page 4: ...ntenna P N AK 451 017 4 S AK 451 AF AP Rod4 Por AK 451 4 ELT Set for Business Jet Aircraft Rod4 Antenna P N AK 451 017 2A and Portable Antenna P N AK 451 017 4 S AK 451 AF AP Bla Por AK 451 5 ELT Set for Transport Aircraft Blade Antenna P N AK 451 017 3A and Portable Antenna P N AK 451 017 4 S AK 451 AP AK 451 10 ELT Set Auto Portable with portable soft case ONLY no other accessories included Port...

Page 5: ...017 4 S AK 451 AF AP w GPS Blade Por AK 451 9 ELT Set with GPS NAV Position for Transport Aircraft Blade Antenna P N AK 451 017 3A and Portable Antenna P N AK 451 017 4 S AK 451 AF AP w GPS Heli Whip Por AK 451 17 ELT Set for Helicopter with GPS NAV Position Whip Antenna P N AK 451 017 1B and Portable Antenna P N AK 451 017 4 S AK 451 AF AP w GPS Heli Rod3 Por AK 451 18 ELT Set for Helicopter with...

Page 6: ... 243 MHz Portable Whip Antenna AK 451 017 4 S 406 121 5 243 MHz AK 451 AF AK 451 AF AP AK 451 AP AK 451 S S S S S S S M M M M Mandatory The respective model must be accompanied by this antenna S Selective The respective model must be accompanied by at least 1 of these antennas Not applicable 4500010 1 Battery Package Lithium LiMnO2 90 Hrs Lasting TS 451 Computer Test Set and ELT Coding Equipment f...

Page 7: ...age 19 1 3 Technical Characteristics 19 1 4 Accessories supplied 24 1 4 1 Installation kit 24 1 5 License requirement 24 SECTION II INSTALLATION AND TEST 2 1 Unpacking and inspecting equipment 25 2 2 Mechanical installation 25 2 2 1 ELT main unit location and installation 26 2 2 1 1 ELT Location Determination 26 2 2 1 2 Mounting tray and Clamp Holder installation 29 2 2 2 Antenna location and inst...

Page 8: ...itter ID Programming and Self Test 76 3 3 3 System Integration Test 77 3 3 4 Green ON Lights Buzzer Sound and Antenna check 80 3 3 5 Transmitter Functional Test for ELT S only 81 3 4 Periodic Maintenance Instructions for Continued Airworthiness 86 3 4 1 Secure Inspection 86 3 4 2 Corrosion Inspection for Coaxial Cable 86 3 4 3 Corrosion Inspection for Remote Wiring Modular Cable 86 3 4 4 Expiratio...

Page 9: ... Log Book Entry 99 3 5 7 Shipping 99 SECTION IV REGISTRATION AND RESPONSIBLE USE 4 1 Registration 100 4 1 1 Registration importance 100 4 1 2 Where to register 100 4 1 3 Registration in the United States 100 4 1 4 Registration in Canada 101 4 1 5 Registration outside of the United States and Canada 101 4 1 6 Change of ownership or contact information 101 4 1 7 Lost ELT s 102 4 1 8 Stolen ELT s 102...

Page 10: ... FAA Action Notice A 8150 3 Emergency Locator Transmitter recommended Supplemental Inspection Procedure FAR Part 91 Operations 119 APPENDIX D Excerpt from FAA AC 91 44A Paragraph 8 a which defines when Battery Replacement may be done under FAR 43 3 h as Preventive Maintenance 123 APPENDIX E FAA Advisory Circular AC 13 2B Section 37 C 124 APPENDIX F Registering a 406 MHz Beacon for U S A 125 ...

Page 11: ...pproval Brazil Certificado Anatel dated 03 31 2009 159 Approval EASA Minor Change Approval 10027068 dated 9 3 2009 160 Approval EASA Minor Change Approval 10027068 Rev 1 dated 1 10 2011 162 Approval EASA Minor Change Approval 10026866 dated 8 18 2009 165 Approval EASA Minor Change Approval 10026863 dated 8 18 2009 167 Approval EASA Minor Change Approval 10026863 Rev 1 dated 11 15 2010 169 Approval...

Page 12: ...gure 7 1 Rod Antenna AK 451 017 2A 1 42 Figure 8 Blade Antenna AK 451 017 3A 46 Figure 9 Integral Portable Whip Antenna AK 451 017 4 S Ant ground plane is not required 47 Figure 10 ELT Remote Switch Installation 49 Figure 10 1 Mounting bracket for ELT Remote Unit Continued 49 Figure 11 Remote Audio Buzzer Monitor P N 451018 50 Figure 11 1 Buzzer may be fastened directly onto the Remote Switch Unit...

Page 13: ...iagram for AK 451 with GPS Position and 3 inch T adapter with 2 wire interconnecting ELT Main Unit and Remote Switch Unit 67 Figure 15 Battery Replacement for ELT Main Unit 69 Figure 16 Battery Pack Replacement for ELT Main Unit Actual View 70 Figure 16 1 Battery Cell Replacement for ELT Main Unit Actual View 70 Figure 17 Battery Replacement for ELT Remote Unit 71 Figure 18 ELT Front Panels Main U...

Page 14: ... Air Force AFSR Ground Operation Search and Rescue Team with 100 fully confidence due to transmitting on both 243 0 MHz Military and 121 5 MHz Civilian bands for immediate ground search dispatch narrowing the searching time The AK 451 ELT Emergency Locator Transmitter is micro controller based equipment It is extremely reliable equipment designed to meet TSO C126 and TSO C91A requirements batterie...

Page 15: ...ed If for any reason a fixed mounting is not required the ELT AF AP can be used as a Portable Device due to it s manual operated hand use Portability Check Local and or national regulations for this issue c Automatic Portable ELT AP with integral antenna The ELT AP is designed to be rigidly attached to the aircraft before the crash but readily removable from the aircraft after a crash It functions...

Page 16: ...ing light indicator on the ELT is provided to alert the user that the ELT has been activated and is transmitting The ELT can be tethered to a survivor or a life raft It is designed to aid the Cospas Sarsat satellite and SAR teams in locating the crash site or survivor s The model AK 451 S consists of an ELT main unit with integral antenna and a portable soft case The ELT S has no automatic activat...

Page 17: ...FAA ACO for clarification In Canada Installation of an ELT in an aeronautical product is carried out under a Supplemental Type Certificate STC This is a separate regulatory requirement and should therefore refer to Ameri King Document No ICA 451 for the Operations and Instructions for Continued Airworthiness ICA The conditions and tests required for TSO approval of this article are minimum perform...

Page 18: ...er Verification method Note The AK 451 is certified to meet the requirements of FAA TSO C126 TSO C91a and EASA ETSO 2C126 per EUROCAE ED 62 For use outside the US or EASA member states contact your local civil aviation authority for ELT requirements 1 2 4 Programming Ameri King will program in any protocol at no charge The AK 451 supports all available worldwide ELT protocols in long message and s...

Page 19: ...er Standard Location Protocol Long Message or Serial User Protocol Short Message for US aircraft Note 2 The AK 451 is pre programmed at the factory using ELT with 24 Bit aircraft address Standard Location Long Message or Serial User Short Message for Canadian aircraft Your 24 Bit aircraft address may be obtained from http www tc gc ca aviation activepages ccarcs aspscripts en quicksearch asp Note ...

Page 20: ...ely CASE AND COLOR No Sharp Edges High Impact Flame Retorted Fire Resistant Waterproof High Temperature ABS Plastic Safety International Orange Color GENERAL SPECIFICATIONS STANDARD CONDITIONS TRANSMITTER Operating Frequencies 406 028 MHz 0 001 MHz 121 500 MHz 0 005 243 000 MHz 0 005 Note AK 451 2D 6D 20D 21D 23D will turn off 243 MHz Short term stability 2 x 10 9 100ms Medium slope 1 to 1x10 9 mi...

Page 21: ...tal Plane CRASHWORTHINESS 100g 23 ms 6 directions ACTIVATION MONITOR Manual ON and RESET functions are located on both ELT Main Unit and Remote Unit The two Green ON lights flashing located on the ELT Main Unit and Remote Switch Unit and a buzzer are to indicate when the ELT is transmitting Both ELT Main Unit and Remote Unit are self powered by their internal batteries Automatic activation is rema...

Page 22: ...XXSXXXXAC 204 183 BXXXX 204 TEMP AND ALTITUDE Category F1 Low Temperature 20 C Operating 55 C Storage High Temperature 55 C Operating 85 C Storage OPERATING LIFE 5W 406 208 MHz for 24 hrs 20 C 50mW 121 5 MHz 50mW 243 0 MHz Minimum Requirement throughout a 50 hour period at 20 C TEMP VARIATION Category B 10 C minimum per minute HUMIDITY Category A 95 RH 50 hours operating SHOCK 500G 4 1msec IMPACT ...

Page 23: ...23 Figure A Front view of ELT Figure B 3 D view of ELT ...

Page 24: ...13 450013 1 Mounting Tray 451014 450014 Clamp Holder 4510171 Coaxial cable assembly 451018 Audible Buzzer Monitor 4510181 T Adapter connector AK 451 017 1B 2A 2A 1 3A 4 S Antenna Assembly 4510131 Optional Floating Collar SC 451 Soft Case SC 451 T Tether 1 5 FCC LICENSE REQUIREMENT In the U S A Not required per FCC Note Radio station license of the aircraft is required by telecommunication regulati...

Page 25: ... unique as is the installation of any TSO C126 and TSO C91a ELT it requires experience in sheet metal work and avionics Only licensed technicians should install the ELT Many problems associated with the older ELTs were due to poor installation Therefore duplicating a previous ELT installation with the AMERI KING ELT may not be acceptable Installations must be made by qualified personnel in accorda...

Page 26: ...e as far as unit location and surface rigidity are concerned Just because the old ELT was located in a particular position doesn t mean the new ELT should be located there as well The tail section of an airplane is least likely to be damaged during a crash and therefore it provides a good mounting environment for the ELT unit Refer to Figure 1 for Direction Determination for Fixed Wing Aircraft an...

Page 27: ...nd a location per the following RTCA suggests the aft section of the fuselage Statistically this is the least likely section of the aircraft to receive damage in a crash It is also near the antenna connection minimizing cable length between the transmitter and antenna Maintain access for maintenance If possible avoid locating the ELT where it will be subjected to chemical fluids such as deicing co...

Page 28: ... patterns See Figure 2 1 1 include ACK Technologies E 01 Artex 100 110 G406 C406 and B406 series ELT 200 series Narco ELT 910 ELT 10 Pointer model ELT 3000 XX Figure 1 Direction Determination for Fixed Wing Aircraft ...

Page 29: ...e requirement drill mount must install the ELT MountingTray as shown in Figures2 1 2and 3 Mark the4 holes in trapezoidal locations needed for the tray using the tray as a guide Be sure the tray aligns within 10 degrees of the longitudinal axis of the aircraft and in direction of flight The mounting Tray may be mounted on the Horizontal plane or Side wall or Overhead as long as the FORWARD Arrow di...

Page 30: ...30 Figure 2 2a Holder for ELT AP with integral antenna and ELT S P N 450 014 1 Figure 2 1a Mounting Tray for ELT AP with integral antenna and ELT S P N 450 013 2 ...

Page 31: ...31 Figure 2 1 Mounting Tray for ELT AF AP P N 450 013 Figure 2 2 Holder for ELT AF AP P N 450 014 ...

Page 32: ...32 Figure 3 Mounting Tray with Clamp Holder for ELT AF AP ...

Page 33: ...itter as practical The Coaxial Cable connecting the Antenna to the ELT should avoid crossing aircraft production breaks i e riveted fuselage sections The Antenna must be within 20 degrees of vertical when the aircraft is in a normal flight altitude If the Antenna is mounted to a non metallic airframe a supplementary ground plane must be installed The installed Antenna must be able to withstand a s...

Page 34: ...m A star washer should be used between the antenna connector housing and ground plane Take precautions to guard against corrosion loosening etc Ground Plane On fabric covered aircraft or aircraft with other types of nonmetallic skin the manufacturer s recommendations should be followed in order to provide the necessary ground plane An acceptable method of accomplishing this is by providing a numbe...

Page 35: ... provide increased surface contact area between the ground plane and the Antenna 4 Assemble of the Antenna as shown in Figure 3 Make sure the rubber washer which forms a moisture seal between the Antenna base and the aircraft structure is in place before installing the Antenna Also make sure the serrated locking washing is in place 2 2 2 2 1 Whip Antenna Installation AK 451 017 1B The AK 451 017 1...

Page 36: ... loading during flight Refer to FAA Advisory Circular 43 13 2B for complete information 3 Remove the 1 2 28 hex nut and external tooth lock washer from the base of the antenna Insert antenna connector through mounting hole make sure the O ring remains in the base of the antenna connector flange groove and that the connector has sufficient clearance through the aircraft skin To mount the antenna pl...

Page 37: ...37 Figure 6 Whip Antenna Model AK 451 017 1B ...

Page 38: ...38 Figure 2 1 1 Optional Adapter Tray for ELT AF AP P N 450 013 1 for ACK Tech Artex Narco Pointer ELT Retrofit ...

Page 39: ...39 Figure 2 1 2 ELT with mounting tray holder and adapter tray ...

Page 40: ...to ensure a ground contact of less than 0 003Ω If bare metal surfaces are needed for surface preparation they should be treated with Alodine 1200 or similar application to eliminate aluminum oxidation NOTE The AK 451 017 2A Rod Antenna bonds through the base plate not through the mounting screws 2 Use the AK 451 017 2A outline drawing on Fig 7 to determine hole pattern and drill size Type of aircr...

Page 41: ...mall smooth fillet with RTV sealant around the periphery of the antenna base to seal out moisture 6 For maximum signal strength the length of the antenna coax cable to the ELT should be as short as possible use of the standard 6 foot coax cable is recommended when possible Figure 7 Rod Antenna AK 451 017 2A ...

Page 42: ...42 Figure 7 1 Rod Antenna AK 451 017 2A 1 ...

Page 43: ...r torque the mounting screws in an attempt to reduce gaps between the antenna base plate and aircraft mounting surface If gaps over 0 020 appear between the base plate and mounting surface use of a mounting saddle is recommended Refer to Fig 8 for a drawing of the antenna Installation Preparation Prepare the surface for blade antenna installations in such a manner to ensure a ground contact of les...

Page 44: ...should be installed to ensure adequate structural strength for associated air loading during flight Refer to FAA Advisory Circular 43 13 2B for complete information 7 Remove the 1 2 28 hex nut and external tooth lock washer from the base of the antenna Insert antenna connector through mounting hole make sure the O ring remains in the base of the antenna connector flange groove and that the connect...

Page 45: ...45 Figure 8 Blade Antenna AK 451 017 3A ...

Page 46: ...ne The antenna ground plane installation is not required Type of aircraft The AK 451 017 4 S Integral Antenna is designed for installation for any aircraft including fix wing and helicopters Installation Installation is not required The AK 451 AP with Integral Antenna and AK 451 S are the best ELT configurations for composite aircraft because the Antenna ground plane is not required ...

Page 47: ...47 Figure 9 Integral Portable whip Antenna AK 451 017 4 S with 2 attached string bands supplied Antenna ground plane is not required ...

Page 48: ...48 ...

Page 49: ...wn in Figure 10 Install the Remote Unit assembly by fitting it into the cutout using four 4 40 screws and Nylock nuts If the unit is to be mounted in a location that does not have a flush mounting surface i e beneath the panel glare shield an angle bracket should be fabricated See Figure 10 1 TSO C126 RTCA DO 204 paragraphs 1 3 and 2 2 6 1 state A remote control to operate and monitor the transmit...

Page 50: ...50 Figure 10 ELT Remote Switch Installation Figure 10 1 Mounting bracket for ELT Remote Unit Continued ...

Page 51: ...51 Figure 11 Remote Audio Buzzer Monitor P N 451018 ...

Page 52: ...4 Wiring interconnecting harness The wiring cable is 25 feet long if the cable is too long looping the wire in order to have shorter wiring is acceptable Please contact Ameri King if you need shorter or longer wiring cables Use only Ameri King supplied interconnects wiring cables ...

Page 53: ... the same side You must see wiring color codes Yellow Green Red Black Orange alternatively on both plugs The wiring configuration is not a telephone application Telephone application is a cross wire configuration i e Pin 1 to 6 Pin 2 to 5 and Pin 3 to 4 To convert from cross wire to straight wire configuration just simply reverse either plug upside down Figure 12 1 Interconnecting Wiring Cable bet...

Page 54: ...54 Figure 12 2 Interconnecting Wiring Cable between ELT Remote Unit and Main Unit Part No 4500041 4 ...

Page 55: ...Remote Switch Unite via T Adapter connector The rear of the buzzer can be sealed with RTV however the front must be left open Note If the Buzzer for AK 451 is located inside the ELT Main Unit it is powered by the ELT Main batteries The ELT Main Batteries will continue to supply power to the Buzzer for 78 hours at 20 deg C at end of 5 years battery life Connect Harness With the harness installed Se...

Page 56: ... 4510042 to the ELT Remote Switch Unit via T Adapter Connector as well See Fig 14 1 14 1 1 14 1 2 and 14 2 Note All wiring harness assemblies P N 4510041 4510042 were Qualification tested including Flame Test per TSO C126 RTCA DO 204 requirements Avoid running this cable near sources of strong EMI RFI radiation Secure the Cable along its run with Tie wraps or other suitable methods The interconnec...

Page 57: ...ghts and buzzer will show 1 flash or 2 flashes or 3 flashes or 4 flashes etc Refer to Operation Manual paragraph 2 4 4 for details Next in order to check G Switch Throw the ELT forward and backward 2 3 times the ELT must activate ELT swept Tone must be heard on the VHF Radio 121 5 MHz The 2 LED lights flashing 4 sec OFF 1 sec ON synchronized with the Buzzer sound 4 sec OFF 1 sec ON Next Press eith...

Page 58: ...be heard on the Com Receiver Push the RESET button on the Remote Unit Verify that the Audio ELT Sweep Tone is ceased Verify the two Green ON lights are extinguished and the buzzer sound is silent Note Always perform the tests within the first 5 minutes of the hour Notify any nearby control tower of your intensions in accordance with AC 43 13 2B Section 12 22 Note 3 If outside of the US always foll...

Page 59: ...by a rapid reversing action Verify that the ELT has been activated by use of the Wattmeter the Airplane s VHF Radio Communications Receiver when tuned to 121 5 MHz or other means see Note 1 The ELT must then be reset by pressing either the RESET push button located on the ELT main unit or the ELT Remote Unit Note 1 This is not a measured check It only indicates that the G Switch is working ...

Page 60: ...level 33 dBm 406 028 MHz 7 flashes F1 F2 VHF RF power level 17 dBm 121 5 243 MHz 9 flashes PLL locked in F3 or F1 or F2 at fault Continuous flash no F3 F2 F1 RF output power ELT shuts down completely Note The self test mode that transmits a 406 MHz test code pulse monitors certain system functions before returning to the ARM mode The 406 MHz test pulse is ignored by any satellite that receives the...

Page 61: ...tion Verify the following setting See Figure 13 From the Hyper Terminal window or equivalent RS 232 window Click File Properties Settings tab Click OK to go back to Hyper Terminal window Figure 13 Verify parameter setting Waiting for 50s verify the 36 Hex digits ignore first 6 digits The last 30 Hex digits will be used for Cospas Sarsat Decode program in order to see the Latitude Longitude Positio...

Page 62: ...e reset by pressing either the RESET push button located on the ELT Main unit or the ELT Remote Unit Note This is not a measured check but it does provide confidence that the Antenna is radiating with sufficient power to aid search and rescue The Aircraft s VHF Receiver tuned to 121 5 MHz may also be used This Receiver however is more sensitive and could pick up a weak signal even if the radiating...

Page 63: ...63 Figure 14 1a Wiring Diagram for AK 451 with 4 wire interconnecting ELT Main Unit and Remote Switch Unit ...

Page 64: ...64 Figure 14 1b Wiring Diagram for AK 451 with 2 wire interconnecting ELT Main Unit and Remote Switch Unit ...

Page 65: ...65 Figure 14 1c Wiring Diagram for retrofitting AK 451 with 4 wire interconnecting ELT Main Unit and Remote Switch Unit Artex Pointer Kannad ACK Tech ...

Page 66: ...66 Figure 14 1d Wiring Diagram for retrofitting AK 451 with 2 wire interconnecting ELT Main Unit and Remote Switch Unit D M Narco Joliet ...

Page 67: ...67 Figure 14 2a Wiring Diagram for AK 451 with GPS Position and 3 inch T adapter with 4 wire interconnecting ELT Main Unit and Remote Switch Unit ...

Page 68: ...68 Figure 14 2b Wiring Diagram for AK 451 with GPS Position and 3 inch T adapter with 2 wire interconnecting ELT Main Unit and Remote Switch Unit ...

Page 69: ...Box Silkscreen The owner or operator may perform Battery replacement provided that the accessibility removal and reinstallation of the ELT can be considered simple as prescribed in Advisory Circular 91 44A Paragraph 8 a See Appendix B All batteries are strongly advised to be serviced by Ameri King or its authorized service centers End users may return the entire ELT for replacing the batteries and...

Page 70: ...ate labels from the battery case and install the new label you prepared in step 3 above in a readily visible location on the ELT 5 After battery replacement a transmitter function test must be performed as described in section 3 3 of this manual FIXED OPERATION IN AIRCRAFT FOR NORMAL OPERATION MAIN CONTROL SWITCH MUST BE IN ARM POSITION F O R W A R D To Activate Lift flip the switch to the ON posi...

Page 71: ...71 Figure 16 Battery Pack Replacement for ELT Main Unit Actual View Figure 16 1 Battery Pack Replacement for ELT Main Unit Actual View ...

Page 72: ...Figure 17 Carefully remove the top half of the Remote unit exposing the battery compartment Figure 17 If replacing an old battery carefully inspect the battery contacts for dirt or corrosion IF the contacts need cleaning use only non abrasive electrical contact cleaner and a stiff brush Badly corroded contacts should be replaced Insert the battery with the polarity as shown in Figure 17 The polari...

Page 73: ...FAA approved prior to its use for that purpose and includes FAR e g airworthiness directives ACs e g AC 43 13 2B under certain circumstances TSOs parts manufacturing approval PMA FAA approved manufacturer s instructions kits and service handbooks type certificate data sheets and aircraft specifications Other forms of approved data would be those approved by a designated engineering representative ...

Page 74: ... ELT automatically activates during a crash and transmits the standard swept tone The Green ON lights flashing located on both the ELT Main Unit and the Cockpit Remote Switch unit and the buzzer sound periodically indicates when the ELT is activated The ON switch on the Remote Switch Unit allows you to turn on the ELT for testing The RESET Switch on the Remote Switch Unit enables to reset the ELT ...

Page 75: ...mits the standard swept tone on 243 121 5 MHz lasting until battery power is gone This 243 121 5 MHz signal is mainly used to pinpoint the beacon during search and rescue operations For the first 24 hours of operations a 406 MHz signal is transmitted at 50 second intervals This transmission lasts 520 ms and contains identification data programmed into the beacon and is received by COSPAS SARSAT sa...

Page 76: ...for 4 sec then extinguish This is to make sure LED and Buzzer are properly powered Note Press RESET anytime to turn off unwanted transmission The ELT will then automatically enter Self test mode Self test takes 25 sec If ELT Self test is passed No light illuminate no buzzer sound If ELT malfunctions the LED Lights and buzzer will show 1 flash 2 flashes 3 flashes or 4 flashes etc Refer to Operation...

Page 77: ...LT not to move the switch or to allow packing material to become lodged such as to toggle the switch Main switch alternate positions ON ELT transmits immediately Both Green ON lights on the main unit and remote switch unit flash and the buzzer sound at rate of 1 second ON 4 seconds OFF The ELT swept Tone must be heard on the 121 5 MHz VHF Radio OFF The ELT is turned off ARM ELT self test is confir...

Page 78: ...z test code pulse monitors certain system functions before returning to the ARM mode The 406 MHz test pulse is ignored by any satellite that receives the signal but the ELT uses this output to check output power and correct frequency Self test is 520 ms long message burst on the 406 MHz signal Synchronization pattern is 011 010 000 Self test is then 121 243 MHz VHF Continuous Wave during 1s During...

Page 79: ...79 Figure 18 ELT Front Panels Main Unit and Remote Unit ...

Page 80: ...itch is working Note In normal configuration the main switch on the ELT Main Unit must be selected to the ARM position Whenever both the Green ON lights located on the Main Unit and the Remote Switch Unit flash and the Buzzer sound periodically they indicate the ELT is transmitting If the ELT be accidentally activated by turbulence hard landing etc or if this occur under any conditions other than ...

Page 81: ...und periodically The ELT swept Tone must be heard on the 121 5 MHz VHF Radio This is to indicate that the ELT has been manually activated In ARM mode Green ON light flashes continuously 1 second ON 4 second OFF and the Buzzer sound periodically ELT swept Tone is heard on the 121 5 MHz VHF Radio This is to indicate that the ELT has been auto activated by the G switch 3 3 4 2 Antenna Check A low qua...

Page 82: ...odged such as to toggle the switch Main Switch alternate alternate momentary positions ON Alternate position ELT S transmits immediately Green ON light on the main unit flashes 1 second ON 4 seconds OFF The ELT swept Tone must be heard on the 121 5 MHz VHF Radio OFF Alternate position The ELT S is turned off SELF TEST Momentary position ELT S self test is confirmed after the switch is held for 25 ...

Page 83: ...red in Memory at fault 3 flashes Battery voltage is low Useful Life Battery Voltage setting 4 flashes Vcc supplies for F3 F2 or F1 at fault 5 flashes F3 RF power level 33 dBm 406 028 MHz 7 flashes F1 F2 VHF RF power level 17 dBm 121 5 243 MHz 9 flashes PLL locked in F3 or F1 or F2 at fault Continuous flash no F3 F2 F1 RF output power ELT shuts down completely Note The self test mode that transmits...

Page 84: ...84 ELT S Top Label Figure 19 Automatic Portable ELT AP with integral antenna Survival ELT S ...

Page 85: ... ELT back and forth rapidly in direction of FORWARD arrow ELT must activate and swept tone heard on 121 5 Radio This satellite ELT only floats w floating collar WARNING FOR AVIATION EMERGENCY USE ONLY UNLICENSED OPERATION UNLAWFUL LITHIUM BATTERY PACK NON RECHARGEABLE FAA TSO C142 approved For use on Model AK 451 P N 4500010 1 Lithium LiMnO2 2 Lithium LiSO2 RTCA DO 160E Environmental Categories F1...

Page 86: ...h to ARM position Verify Green ON LED is on for 4 sec then off Wait for an additional 21 sec If Pass Green ON LED stays off No swept tone on 121 5 Radio If Fail Green ON LED flashes See Operation Manual for details Check G switch Next If pass Self Test shake ELT back and forth rapidly in direction of FORWARD arrow ELT must activate and swept tone heard on 121 5 Radio This satellite ELT only floats...

Page 87: ...connecting the ELT Main Unit to the Remote Unit of signs of wear or abrasion on its outer jacket Remove the Modular Connecting Cable and inspect and jack and plug assembly for corrosion 3 4 4 Battery Expiration Date Check Check the expiration date of the ELT Main Unit and the Remote Unit Batteries Replace if necessary 3 4 5 Battery Leakage Check Remove the Battery Case and inspect the Battery Comp...

Page 88: ...ote 3 Because the ELT radiates on the emergency frequency the Federal Communications Commission allows these tests to be conducted only within the first 5 minutes after any hour IMPORTANT NOTE IN NORMAL CONFIGURATION THE MAIN SWITCH LOCATED ON THE ELT MAIN UNIT MUST BE SELECTED AT ARM POSITION AT ALL TIMES 3 4 8 Verification of Digital Message Note This test is not mandatory per FAR 91 207 d howev...

Page 89: ...ort to the PC USB port 3 4 8 1 ELT ID Reading Step1 Double Click AK451 Icon to run the program The programming window appears as below Note If you don t see the window above you may try the other USB port Step 2 Set the ELT main switch to ARM position Step 3 Verify the LED ON light illuminates for 4 seconds Step 4 At the _ prompt type Password command then press Enter to go to main menu Must type ...

Page 90: ...of Registration Note This verification is not mandatory per FAR 91 207 d however Ameri King strongly recommends that it be performed as part of periodic maintenance at least every year Check ELT for signs of registration In the US NOAA supplies a beacon registration label that is applied to the ELT when it is registered The following address should be used to register and obtain information on how...

Page 91: ...s This feature will allow the ELT to be transferred between aircraft This makes maintenance of the ELT a simple matter of replacing the ELT Note There is no electronic connection between TCAS or Mode S systems and the ELT only the ID number is common The AK 451 receives position data longitude and latitude from the aircraft s on board GPS system The ELT may be programmed with the aircraft s 24 bit...

Page 92: ...be required if the contact information does not change however contact your local civil aviation or beacon registration authority when in doubt Both serialized long message and 24 Bit address long message re programmed ELT that is moved to another aircraft shall need to be re registered Online or by Mail The user must specify 24 bit long message programming when ordering the ELT Changing the progr...

Page 93: ...s transmitted at turn off is required to verify the ELT and ELT GPS Interface function Note It is extremely important that the ELT GPS Interface installation not be in conflict with the GPS FMC manufacturer s installation instructions in order to avoid an installation that may degrade the GPS FMC performance As a result the Post Installation checkout in the GPS FMC Installation Manual may be follo...

Page 94: ...uter Test Set TS 451 Turn the switch of the ELT to ON position Verify the following setting See Figure 20 From the Hyper Terminal window or the equivalent RS 232 window Click File Properties Settings tab Click OK to go back to Hyper Terminal window Figure 20 Verify parameter setting Waiting for 50s verify the 36 Hex digits ignore first 6 digits The last 30 Hex digits will be used for Cospas Sarsat...

Page 95: ...ttery replacement or recharge instructions battery capacity test procedures if applicable transmission or functional test procedures procedures necessary to accomplish the performance tests specified in Chapter 571 Appendix B and for 406 MHz ELTs instructions to verify the aircraft 24 bit address protocol as applicable Appendix B a Corrosion Inspection b Operational Testing c Performance Testing d...

Page 96: ...rds Part V Airworthiness Manual 571 Appendix B 3 5 2 Power Output Test Performance Testing NOTE Using of ELT Test set TS 451 or equivalent test equipment is acceptable 3 5 2 1 121 5 243 0 MHz Power Output Connect the equipment as shown below Note Use as fresh battery pack 12 5 0 5 VDC nominal or a 2 amp 12 5 VDC power supply as power source The test equipment specified in the following steps is on...

Page 97: ...between the ELT s 406 028 MHz output and the input to the spectrum analyzer to protect the analyzer s input circuitry Connect the equipment as shown below Set the Spectrum Analyzer as follows Center freq 406 028 MHz Span 1 MHz Resolution bandwidth 1 MHz Vertical display 10dB Div Sweep Auto Peak Avg Peak Reference level 30 dBm Time Div 20ms Max hold On Attenuator as required on Input Turn the ELT o...

Page 98: ...Hz Notch Filter The ELT frequency should be within 50 ppm 12 150 KHz of 243 000 000 Hz after 3 minutes of operation 3 5 3 3 Measure the 406 028 MHz frequency Ensure that adequate attenuation rated for 406 028 MHz 37 dBm and 5 Watts is installed between the ELT s 406 028 MHz output and the input to the frequency counter to prevent damaging the frequency counter s input circuitry Set up the equipmen...

Page 99: ...sts This is normal Press the RESET Switch to Reset the unit OFF Mode Current Measurement Remove the battery pack as described in Section 2 5 1 Disconnect the 2 pin harness Install the test harness P N TS 451 HN 1 and inline ammeter as shown in Fig 4 2 Ensure the ELT is OFF Measure the current with the ammeter The measured current should be 0 microamps uA ARM Mode Current Measurement Measure the cu...

Page 100: ...thin the first five minutes of the hour 3 5 6 PERFORMANCE TEST MARKING AND LOG BOOK ENTRY Following satisfactory completion of all of the above Performance Testing the date on which the test was performed shall be marked on the external casing in a legible and permanent manner Enter the test date and Technician Initials as ELT Pass or Fail into the aircraft Log Book 3 5 7 SHIPPING In order to prev...

Page 101: ... as the 15 digit hex ID shown on the ELT name plate It is important to fill in the sticker This ELT belongs to A C Tail _________ 4 1 2 Where to register The owner of a 406 MHz ELT should register it with the National Authority of which the ELT was programmed typically the country where purchased regardless of where you use your ELT Each ELT is programmed with a UIN for the country where the unit ...

Page 102: ...3W0 Phone 1 877 406 SOS1 7671 Fax 1 877 406 FAX8 3298 Email cbr sarnet dnd ca Online www canadianbeaconregistry forces gc ca 4 1 5 Registration Outside of the United States and Canada In countries other than the United States 406 MHz ELTs are registered with that country s National Authority at the time of Purchase The Sales agent should assist in filling out the forms and sending to that country ...

Page 103: ...ster a ELT reported as stolen NOAA or your national authority will notify the appropriate Police Department Visit the COSPAS SARSAT website for more detailed information www cospas sarsat org 4 2 RESPONSIBILITY 4 2 1 Responsible Use The Ameri King AK 451 should only be used in situations of grave and imminent danger What exactly does this mean Technically speaking you should only activate your ELT...

Page 104: ... demolishing it Please update your ELT Registration if you sell or dispose of your registered 406 MHz ELT Finally realize that the COSPAS SARSAT satellites are very good at what they do detecting emergency ELTs An activation of a 406 MHz for just a few seconds will usually be detected After a few minutes it will usually be detected and located This is good if you re in distress but if you re not y...

Page 105: ...iscovery of a condition believed to be caused by a defect in manufacturing Ameri King Corp without prior authorization Any equipment returned to Ameri King Corp without prior authorization Any equipment returned to Ameri King Corp should be accompanied by a failure report in writing giving full particulars in support of the claim This limited warranty does not cover or apply to any of the followin...

Page 106: ...ed at the facility of Ameri King Corp The entire repair service shall be performed and completed within 3 days upon repairing estimate is approved by equipment user or installation dealer Shipping charge shall be paid both ways by the Customers IMPORTANT NOTE In order to prevent accidental activation of the ELT during transit the ELT ON OFF ARM Main Switch must be set in the OFF position Note The ...

Page 107: ...d cut out holes are exactly the same Note 2 Wiring Harness between ELT and Remote Switch Unit is exactly the same i e Do not change the wiring harness It is OK to use the existing AK 450 wiring Note 3 Adding a new Buzzer to be mounted anywhere in the cockpit i e Tie wrap into the aircraft Wiring Harness or Fasten onto or behind the instrument Panel or fasten on the Remote Switch Unit 2 Register wi...

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Page 115: ...Unit None Now the ELT switch on the Main Unit should be left at ARM position and the ELT is ready to go Note 1 The ELT switch is make before break Return to OFF for at least 1 sec before changing positions Note 2 Press RESET anytime to turn off unwanted transmission WARNING Do not allow ELT On test duration and G Switch test duration to exceed 5 10 seconds A false alarm may be generated Any time t...

Page 116: ...y year Approved Batteries Main ELT Unit Ameri King P N 4500010 Remote Switch Unit Duracell DL1 3NB Source of Supply Ameri King FAR 91 207 d 91 409 and 43 Appendix D Transport Canada Civil Aviation Part V Airworthiness Standards Chapter 551 104 d 1 VI Battery replacement or recharge instructions Checks are to be performed every year 2 5 1 ELT Main Battery Replacement instructions 2 5 2 ELT Remote U...

Page 117: ...es are recommended by Ameri King to be performed every 1 2 months 3 3 1 Main Switch ON OFF ARM Operation 3 3 2 Transmitter ID Programming and Self Test 3 3 3 System Integration Test 3 3 4 Green ON Lights and Buzzer Sound Functions 3 3 5 Transmitter Functional Test For ELT S only 3 3 5 1 Main Switch ON OFF SELF TEST Operation 3 3 5 2 Transmitter Self Test FAR 91 207 d 91 409 and 43 Appendix D Proce...

Page 118: ...3 4 9 Verification of Registration 3 4 10 Verification of ELT GPS interface if equipped C Performance Testing These Tests are required for Canadian compliance only Tests are to be performed every year 3 5 1 Regular Periodic Maintenance Test 3 5 2 Power Output Test 20 3 dBm at 121 5 243 MHz 35 34 to 38 18 dBm 5W 1 58W at 406 028 MHz 3 5 3 Frequency Test 121 5 MHz 6 075 KHz 243 MHz 12 150 KHz 406 02...

Page 119: ...5 7 Shipping Transport Canada Civil Aviation Part V Airworthiness Standards Chapter 551 104 d 1 VI Verify the aircraft 24 bit address This Test is required for Canadian compliance only Tests are to be performed every year 3 4 8 Verification of Digital Message 3 4 10 4 24 Bit Address Maintenance Test Test Equipment Test Set TS 451 or equivalent Test Equipment Spectrum Analyzer or equivalent Test Eq...

Page 120: ...stallation According to the ELT mfg instructions and According to FAA supplemental inspection procedures in Notice A8310 1 According to AC91 44A INSPECTION Remove all interconnections to the ELT unit and ELT antenna Visually inspect and confirm proper seating of all connector pins Special attention should be given to coaxial center conductor pins which are prone to retracting into the connector ho...

Page 121: ...the antenna of the AM broadcast radio receiver tuning dial on any setting is held about 6 inches from the activated ELT antenna the ELT aural tone will be heard INSPECTION Verify that all switches are properly labeled and positioned TEMPORARY REMOVAL An aircraft may be operated during any period for which the transmitter has been temporarily removed for inspection repair modification or replacemen...

Page 122: ...t the maintenance preventive maintenance rebuilding or alteration has not appreciably changed the flight characteristics or substantially affected the flight operation of the aircraft FAA Action Notice A 8150 3 1 Remove all interconnections to the ELT Main Unit and ELT antenna Visually inspect and confirm proper seating of all connector pins Special attention should be given to coaxial center cond...

Page 123: ...at the G Switch is working Note 2 This is not a measured check but it does provide confidence that the Antenna is radiating with sufficient power to aid search and rescue The Aircraft s VHF Receiver tuned to 121 5 MHz may also be sued This Receiver however is more sensitive and could pick up a weak signal even if the radiating ELT s Antenna is disconnected Thus it does not check the integrity of t...

Page 124: ...craft by a simple operation should be considered Preventive Maintenance Fixed type ELT installations are often permanently mounted in a remote area of the Aircraft near flight control cables vital Aircraft components and critical attachments to the Aircraft structures Installations of this nature require an external Antenna and often a remote ON OFF transmitter control switch that is usually locat...

Page 125: ...g saddle is recommended c Since antenna systems typically require a ground plane this may be a conductive surface that the antenna mounts to any separation of an antenna from its ground plane may impact performance Contact the manufacturer for recommendations if a gasket or mounting saddle is needed see figure below d Mounting screws must never be over torqued in an attempt to distort aircraft str...

Page 126: ...weeks please 6 call NOAA toll free at 1 888 212 SAVE 7283 or 301 817 4515 Failure to register re register as required every two years or to notify NOAA of any changes to the status of your 406 MHz beacon could result in penalties and or fines being issued under Federal Law The owner or user of the beacon is required to notify NOAA of any changes to the registration information at any time By submi...

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Page 129: ...eacon its owner and the vehicle vessel on which the beacon is mounted is vital for the effective use of Search and Rescue resources The proper registration of a beacon could make the difference between success and failure of a search and rescue mission Click here for examples of how the registration information may be used to enable the proper SAR response Process for Registering a Beacon If the A...

Page 130: ...n paper format or via other communication facilities will not be accepted The Cospas Sarsat Secretariat mail cospas sarsat int is available to answer questions from National Administrations concerning beacon coding and registration matters Administration User Accounts The IBRD is freely available to users with no access to national registration facilities and to Administrations who wish to avail t...

Page 131: ...08 Brunei 314 Barbados 633 Burkina Faso 319 Cayman Islands 506 Burma 323 Cuba 609 Burundi 325 Dominica 364 Turks And Caicos Islands 327 Dominican Republic 514 515 Cambodia 330 Grenada 617 Cape Verde 332 Guatemala 319 Cayman Islands 336 Haiti 612 Central African Republic 339 Jamaica 670 Chad 341 St Kitts 616 Comoros 343 St Lucia 615 Congo 348 Montserrat 323 Cuba 350 Nicaragua 270 Czech Republic 351...

Page 132: ...Korea North 470 United Arab Emirates 447 Kuwait 473 475 Yemen 451 Kyrgyz Republic 506 Burma 531 Lao 508 Brunei 450 Lebanon 510 Micronesia 644 Lesotho 511 Palau 642 Libya 514 515 Cambodia 453 Macao 529 Kiribati 274 Macedonia 531 Lao 255 Madeira 544 Nauru 655 Malawi 555 Pitcairn Island 649 Mali 557 Solomon Islands 654 Mauritania 574 Vietnam 645 Mauritius 608 Ascension 510 Micronesia 609 Burundi 214 ...

Page 133: ...auritania 665 St Helena 655 Malawi 341 St Kitts 656 Niger 343 St Lucia 661 Rwanda 662 Sudan 662 Sudan 669 Swaziland 663 Senegal 468 Syria 665 St Helena 674 677 Tanzania 666 Somali 671 Togo 667 Sierra Leo 362 Trinidad 668 Sao Tome 434 Turkmenistan 669 Swaziland 470 United Arab Emirates 670 Chad 675 Uganda 671 Togo 437 Uzbekistan 674 677 Tanzania 208 Vatican 675 Uganda 775 Venezuela 676 Zaire 574 Vi...

Page 134: ...gramming 2 1 Double Click AK451 Icon to run the program The programming window appears as below Figure 1 Note If you don t see the window above you may try the other USB port 2 2 Set the ELT main switch to ARM position 2 3 Verify the LED ON light illuminates for 4 seconds 2 4 At the _ prompt type cn Password command then press Enter to go to main menu Must type this command within next 20 seconds ...

Page 135: ...owing information via Email or fax or call Ameri King in order to obtain 22 Hex Digit ID Country Protocol required See Table 1 for List of all available Protocols 24 Bit aircraft address if applicable Ameri King shall then provide 22 Hex Digit ID Short Message or 30 Hex Digit ID Long Message accordingly The 06 command syntax 06 s 1 22 30 123456789ABCDEF 0 F To program 22 Hex Digits ID to the ELT S...

Page 136: ...136 Figure 3 To program 30 Hex ID to the ELT Long Messages At the command prompt type 06 30 XXXXXXXXXXXXXXXXXXXXXX Where X X 30 HEX Digits ID See Figure 4 Figure 4 ...

Page 137: ...e To program 30 Hex ID to the ELT Long Messages at the command prompt type 06 30 97142CC1637FDFF9996CF583E0FAA8 A screen as shown in figure 5 below should appear indicating that the program is a success Figure 5 ...

Page 138: ...138 Table 1 List of all available Protocols ELT Non Location Protocols ...

Page 139: ...139 ELT Location Protocols User Location Protocols ...

Page 140: ...140 ELT Location Protocols Standard Location Protocols National Location Protocols http www cospas sarsat org BeaconsTutorial tutorial_map htm ...

Page 141: ...tput level F3 RF power level 33 dBm 406 028 MHz 5 flashes Internal 3V3 Vcc supplies for F3 F2 or F1 at fault 4 flashes Internal 5V VHF Vcc supplies for F3 F2 or F1 at fault 4 flashes Internal 7V3 406 Vcc supplies for F3 F2 or F1 at fault 4 flashes Internal LDO status Internal Data stored in Memory at fault 1 flash Battery level Battery voltage is low Useful Life Battery Voltage setting 3 flashes E...

Page 142: ...ion Note You can use Notepad Editor Program to modify the coordinate of this location Ameri King GPS Location Text file Figure 7 Below are the steps of inserting location coordinate IMPORTANT NOTE ONCE THE HEX DIGITS APPEAR ON THE SCREEN TURN THE UNIT OFF IMMEDIATELY FAILURE TO DO SO WILL RESULT IN THE SIGNAL TO NOTIFY THE EMERGENCY RESCUE AUTHORITIES 1 Single Click Transfer 2 Single Click Send Te...

Page 143: ... of the ELT to ON position 3 Single Click on Open button to insert the coordinate of Ameri King GPS Location to the ELT 4 DO NOT turn the ELT off Wait for 50 seconds and you will receive 30 Hex digits Ignore the first 6 digits coming from the ELT that contains the coordinate of the Ameri King GPS Location See Figure 10 Use the 406MHz Decode Program to verify the coordinate input Figure 9 ...

Page 144: ...ure 11 o Enter last 30Hex digits last 30 digits of 36 into the 406 MHz Decode Program The 30 Hex digits are the numbers you just have seen from the ELT which appears after 50 seconds on the programming window In this example you have to select the 30 Hexadecimal round button and press Process button to decode these 30 Hex numbers Figure 10 ...

Page 145: ...145 Figure 11 NOTE 1 BCH 1 Encoded and BCH 1 Calculated MUST have the same value 2 BCH 2 Encoded and BCH 2 Calculated MUST have the same value ...

Page 146: ...83 BC XXXX C 204 CONDITIONS SECTION TEST CONDUCTED CATEGORIES Temperature and Altitude 4 0 F1 Low Temperature 4 5 1 F1 Low Temperature 4 5 1 F1 High Temperature 4 5 2 4 5 3 F1 In Flight Loss of Cooling 4 5 X Altitude 4 6 1 F1 Decompression 4 6 2 Per DO 204 183 Overpressure 4 6 3 Per DO 204 183 Temperature Variation 5 0 B Humidity 6 0 A Operational Shock and Crash Safety 7 0 Per DO 204 183 Vibratio...

Page 147: ... Frequency Susceptibility 18 0 X Induced Signal Susceptibility 19 0 A Radio Frequency Susceptibility 20 0 Per DO 204 183 Radio Frequency Emission 21 0 B Lightning Induced Transient Susceptibility 22 0 X Lightning Direct Effects 23 0 X Icing 24 0 X Electrostatic Discharge 25 0 X Flame Test Per DO 204 183 ...

Page 148: ...to Category F1 Overpressure 4 6 3 Equipment identified as Category X no test performed Temperature Variation 5 0 Equipment tested to Category B Humidity 6 0 Equipment tested Per RTCA DO 227 Operational Shock and Crash Safety 7 0 Equipment tested Per RTCA DO 227 Vibration 8 0 Equipment tested Per RTCA DO 227 Explosion 9 0 Equipment identified as Category X no test performed Waterproofness 10 0 Equi...

Page 149: ...ied as Category X no test performed Radio Frequency Emission 21 0 Equipment identified as Category X no test performed Lightning Induced Transient Susceptibility 22 0 Equipment identified as Category X no test performed Lightning Direct Effects 23 0 Equipment identified as Category X no test performed Icing 24 0 Equipment identified as Category X no test performed Electrostatic Discharge 25 0 Equi...

Page 150: ... Minor Change Approval 10027068 Rev 1 dated 1 10 2011 Approval EASA Minor Change Approval 10026866 dated 8 18 2009 Approval EASA Minor Change Approval 10026863 dated 8 18 2009 Approval EASA Minor Change Approval 10026863 Rev 1 dated 11 15 2010 Approval EASA Minor Change Approval P EASA A C 12674 dated 7 24 2009 Approval Austria for Historic Aircraft like PA 18 19 Series Bücker T131 JOB 15 CSS13 da...

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Page 221: ...te 8130 3 export form for each of the 27 countries is not necessary Member states 27 countries Austria Belgium Bulgaria Cyprus Czech Republic Denmark Estonia Finland France Germany Greece Hungary Ireland Italy Latvia Lithuania Luxembourg Malta Netherlands Poland Portugal Romania Slovakia Slovenia Spain Sweden UK note Canary Islands Spain Azores and Madeira Portugal French Guiana Guadeloupe Martini...

Page 222: ...be accepted in all the named countries based on the grandfathered existing bilateral agreement with the main players in EU and the US Due to the fact that the new bilateral is not in place we cannot guarantee that especially as some countries seem not to be accepted by the US side to be eligible to export into the US Unless you state FOR DOMESTIC SHIPMENTS ONLY on the Form 8130 3 the Form issued a...

Page 223: ...223 Japan Civil Aviation Board Approval ...

Page 224: ...iro Kato Cc Takashi Eno 田中友 Subject みなし型式検定につきまして航空部品株式会社加藤様いつもお世話になっております総務省電波環境課の新山です下記についてみなし型式検定の型式に追加されましたのでお知らせしますよろしくお願いいたします AK 451 AF AK 451 AF AP AK 451 AP AK 451 S 製造者 Ameri King Corp 総務省総合通信基盤局電波部電波環境課基準認証係新山紘加 NIIYAMA Hiroka Tel 03 5253 5908 PHS 26788 mailto h niiyama soumu go jp ...

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Page 230: ...230 APPENDIX K MATERIAL SAFETY DATA SHEET FOR BATTERY ...

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