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Seite 1 - AMERI - KING CORPORATION

1 Document No. IM-451 Rev NC-4.1h dated July 5, 2014 INSTALLATION AND OPERATION MANUAL FOR MODEL AK-451

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10 APPENDIX A Retrofit Instructions from AK-450 to AK-451 ...106 APPENDIX A.1 Quick Operation

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100 3.5.4 AUDIO MODULATION, PERFORMANCE TESTING: Perform the transmitter tests by activating the ELT and listening on 121.5 MHz. The audio swept t

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101 SECTION IV REGISTRATION AND RESPONSBLE USE 4.1 REGISTRATION 4.1.1 Registration Importance It is mandatory that the owner of this 406 MHz ELT

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102 ELT registration is also available online at: www.beaconregistration.noaa.gov The information provided on the Registration Form is used only for

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103 4.1.7 Lost ELT’s Inform NOAA immediately at 1-888-212-SAVE (7283), or your national authority, that your ELT has been lost. They will

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104 4.2.2 Preventing False Alarms  Ensure that your ELT is registered with NOAA or your national authority. This does nothing to reduce false alar

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105 SECTION V WARRANTY 5.1 LIMITED WARRANTY All equipments manufactured by Ameri-King Corp. are guaranteed against defective materials and workm

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106 No warranty will be activated for Ameri-King Corp. products unless the installation is approved by an FAA Certified Installer and the warranty

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107 APPENDIX A RETROFIT INSTRUCTIONS FROM AK-450 TO AK-451 Old Model No.: AK-450-(AF)(AP), ELT 121,5/243 MHz. New Model No.: AK-451-(AF)(AP)

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11 APPENDIX G International 406 MHz Beacon Registration Database (IBRD) Countries Allowing Individual Registration ...

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115 APPENDIX A.1 QUICK OPERATION CHECK ELT ON LEDs (Main Unit + Remote Unit) Buzzer sound Swept tone on 121.5 MHz VHF Radio 1. ELT s

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116 APPENDIX B PERIODIC MAINTENANCE CHECK LIST WITH COMPLIANCE CROSS REFERENCES REQUIREMENTS TEST PROCEDURE Paragraphs TEST RESULT PASS FAIL FAR 91

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117 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 c

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118 (B) Operational Testing The periodicity of operational checks is at the operator's discretion, but the check shall only be conducted durin

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119 (D) Battery Replacement And Recharging (Checks are to be performed every year) 2.5.1 ELT Main Battery Replacement Check 2.5.2 ELT Remot

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12 List of Figures Figure A: Front view of ELT ... 23 Figure B: 3-D view of E

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120 APPENDIX C EMERGENCY LOCATOR TRANSMITTER RECOMMENDED SUPPLEMENTAL INSPECTION PROCEDURE (FAR PART 91 OPERATIONS) FAR Part 91.207 Paragraph (d); P

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121 INSPECTION A TSO-C91 ELT can be activated by using a quick rap with the palm. A TSO-C91a ELT can be activated by using a rapid forward (throwin

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122 (2) Wiring and conduits--for improper routing, insecure mounting, and obvious defects. (3) Bonding and shielding--for improper installation and p

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123 6. Activate the ELT using the “ON” of “Test” Switch. A low quality AM Broadcast Radio Receiver should be sued to determine

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124 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 MAINENAN

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125 APPENDIX E FAA ADVISORY CIRCULAR AC43.13-2B, SECTION 303 a. The antenna’s structural load, plus any required allowances, may not exceed the desi

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126 APPENDIX F REGISTERING A 406 MHz BEACON IN THE U.S.A. Important Notice - Please Read Before Completing Registration Registration is an import

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129 APPENDIX G International 406 MHz Beacon Registration Database (IBRD) Countries Allowing Individual Registration Website: www.cospas-sarsat.com

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13 Figure 14.1d: Wiring Diagram for retrofitting AK-451 with 2-wire interconnecting ELT Main Unit and Remote Switch Unit, D&M, Narco, Joliet, e

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130 Process for Registering a Beacon in the Cospas-Sarsat International 406 MHz Beacon Registration Database (IBRD) Your country may have elected t

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131 Sorted By Country Name Sorted By Country Code Country Code Country Name Country Code Country Name 401 Afghanistan 201 Albania 201 Albania 202 And

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132 626 Gabon Republic 417 Sri Lanka 629 Gambia 422 Iran 627 Ghana 425 Iraq 330 Grenada 428 Israel 332 Guatemala 434 Turkmenistan 632 Guinea 436 Kaza

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133 Authority 351, 352, 353, 354, 355, 356, 357, 371, 372 Panama 627 Ghana 555 Pitcairn Island 629 Gambia 466 Qatar 630 Guinea-Bissau 661 Rwanda 631

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134 APPENDIX H ELT CODING PROGRAMMING, ID READER AND MAINTENANCE TEST, P/N TS-451 Important Note: These tests should be performed only with

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135 Note 2: If there is no programming command input in this time window, the ELT will enter the Self-Test mode, and you cannot program the ELT. In

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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

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137 Example: To program 30 Hex ID to the ELT: (Long Messages), at the command prompt type: 06 -30 97142CC1637FDFF9996CF583E0FAA8 A scree

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

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139 ELT Location Protocols User Location Protocols

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14 SECTION I GENERAL INFORMATION 1.1 SCOPE This manual contains information necessary for the installation, test and operation of the model AK-4

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140 ELT Location Protocols Standard Location Protocols National Location Protocols http://www.cospas-sarsat.org/BeaconsTutorial/tutori

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141 3. ELT Maintenance Self-Test: To perform ELT Maintenance Self-Test: Use command “ 05 ” Figure 6: Maintenance Self-Test Maintenance Test incl

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142 4. Functional Test, GPS Position Coordinates Simulation: (Ref.: E6557-CS Annex-E, Page 7) (Table F-D-2) In this example, the “Ameri-King GPS L

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143 Figure 8  Inserting Ameri-King GPS Location Coordinate (See Figure 9) 1. Single-Click on “Ameri-King GPS Location” (The file contains the

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144  To verify the coordinate in the 30 Hex digits message: o Double-click on “406MHz Decode” Icon to open up the 406MHz Decode Program (See Figu

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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 val

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146 APPENDIX I RTCA DO-160D ENVIRONMENTAL QUALIFICATION FORM NOMENCLATURE: ELT EMERGENCY LOCATOR TRANSMITTER TYPE/MODEL/PART NO: AK-451-( ) SERIES.

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147 Fungus 13.0 X Salt Pray 14.0 S Magnetic Effect 15.0 Z Power Input 16.0 X Voltage Spike 17.0 X Audio Frequency Susceptibility 18.0 X Induced Signa

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148 APPENDIX I.1 RTCA DO-160E ENVIRONMENTAL QUALIFICATION FORM TYPE/MODEL/PART NO: Lithium Battery Pack P/N 4500010-( ) TSO NUMBER: C142 MANUFACTUR

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149 performed Voltage Spike 17.0 Equipment identified as Category X, no test performed Audio Frequency Susceptibility 18.0 Equipment identified as Ca

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15 b. Automatic Portable-ELT (AF) (AP) with dual antennas: The ELT (AF) (AP) is designed to be rigidly attached to the aircraft before the crash, b

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150 APPENDIX J Approval, FAA TSO C-126 / C-91a Equipment Approval dated 07/24/2008 Approval, Incomplete Technical Standard Order for ELT Antenna T

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16 d. Survival-ELT (S, Category A): The ELT (S) shall survive the shock, impact and crush tests, after a crash. This type of ELT does not have auto

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17 The Main Unit features include:  ON / OFF / ARM Main Switch  Green ON Light  RESET Push Button Switch The Remote Unit features include: 

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18 The AK-451 ELT described in this manual was designed, tested and certified as a complete system including the following components:  ELT T

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19 1.2.4.2 Standard Location Protocols (Long Message):  Coding ELT with 24-bit address  Coding ELT with Type approval number and a serial numb

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2 REVISION TABLE REVISION DESCRIPTION CHANGED BY APPROVED BY DATE NC First Release T.N. K. V. 4/4/07 NC-1 Add PLB Programming T.N. K.V. 9/5/07 Para.

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20 PHYSICAL CHARACTERISTICS:  SIZE AND WEIGHT: Main Unit: (4.27”Wx2.95”Hx5.64”L) 1lbs 14oz Remote Unit: (1.58”W x 0.65”H x 2.00”L) 1.0 oz

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21 Equivalent Isotropic 100mW (-10dBW) @121.5/243.0 MHz (min) Radiated Power (EIRP): 6dBW ± 4dB @406.028 MHz (max) Emission Designator: 16K

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22 Arnav Systems Inc.: • R50, R50i, STAR 5000, FMS 5000, MFD (Multi-Functional Display). II Morrow: • FLYBUDDY, 2001 NMS Trimble Nav Inc.: • NAV

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221 Email Response from EASA to Ameri-King regarding Acceptability of FAA Form 8130-3 Export Form in EU Europe Union From: Ameri-King Corporation

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222 From: Runge Friedhelm <[email protected]> To: Keith Van <[email protected]> Date: Wed, Oct 7, 2009 4:44 am RE:

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223 Japan Civil Aviation Board Approval

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224 -----Original Message----- From: 新山 紘加 [mailto:[email protected]] Sent: Wednesday, April 07, 2010 10:52 AM To: 'Yasuhiro Kato' Cc:

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226 This page is left blank on purpose.

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23 Figure A: Front view of ELT Figure B: 3-D view of ELT

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230 APPENDIX K MATERIAL SAFETY DATA SHEET FOR BATTERY

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24 1.4 ACCESSORIES SUPPLIED 1.4.1 INSTALLATION KIT: PART NO. DESCRIPTION 4500010-1 Lithium Battery Pack LiMnO2 or 4500010-2 Lithiu

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25 SECTION II INSTALLATION AND TEST 2.1 UNPACKING AND INSPECTING EQUIPMENT Handle with extreme care when unpacking the equipment. Visual inspecti

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26 Note: Installation in a pressurized aircraft constitutes a major modification. Consult the Department of Transportation Regional Officer

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27 Following are the FAA guidelines for mounting a TSO-C91a ELT, per RTCA DO-183 paragraph 3.1.8: 1. “The ELT shall be mounted to primary airc

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28 Compatible patterns (See Figure 2.1.1) include:  ACK Technologies E-01  Artex 100/110, G406, C406 and B406 series, ELT-200 series  Narco EL

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29 Helicopter Installations: The AK-451-(14)(15)(17)(18) may be mounted so that the arrow aligns with the longitudinal axis of the aircraf

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3 NC-4.1a Revise: Para 2.5.1 & 3.5 to meet Canadian compliances QP KV 10/22/08 NC-4.1b EASA Review updated QP KV 10/31/08 NC-4.1c EASA, T.C. app

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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

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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

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32 Figure 3: Mounting Tray with Clamp Holder for ELT- (AF)(AP)

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33 2.2.2 ANTENNA LOCATION AND INSTALLATION In order to meet the requirements of TSO-C91a and FAR 91.207, an External Antenna must be u

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34 Each of the above listed antennas requires a ground plane. On aircraft constructed with non-conductive materials, such as composite or fibergla

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35 2.2.2.2 ANTENNA INSTALLATION: Please refer to FAA AC 43.13 for guideline. After determining the Antenna mounting location per paragraph 2.2.2

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36 Installation Preparation: 1. Prepare the surface for antenna installations in such a manner to ensure a ground contact of less

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37 Figure 6: Whip Antenna (Model AK 451.017-1B)

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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

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39 Figure 2.1.2: ELT with mounting tray, holder, and adapter tray

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4 AK-451 ELT Sets *** with no GPS / NAV Position: Ameri-King P/N Description Antennas Included AK-451-(AF)(AP)/ Whi/Por (AK-451-2/2D) triple/dual Fre

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40 2.2.2.2.2 Rod Antenna Installation: (AK 451.017-2A) The AK 451.017-2A Rod Antenna delivers optimum performance only when installed correctly. To

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41 4. Apply a layer of anti-corrosion bonding grease between aircraft skin and bottom of antenna. 5. Apply a small, smooth fillet with RTV seala

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42 Figure 7.1: Rod Antenna AK 451.017-2A-1

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43 2.2.2.2.3 Blade Antenna Installation: (AK 451.017-3A) Installations must be made by qualified personnel, and in accordance with Federal Regulati

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44 Installation: 1. Mounting the Blade antenna using #10-32 SS machine screws and associated hardware and torque to 20 in-lbs. 2. For BNC connect

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45 Figure 8: Blade Antenna (AK 451.017-3A)

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46 2.2.2.2.4 Integral Antenna Installation: (AK 451.017-4(S)) The integral Antenna AK 451.017-4(S) is fastened to the ELT-(AP) with Int

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47 Figure 9: Integral Portable whip Antenna (AK 451.017-4(S)) (with 2 attached string bands supplied) (Antenna ground plane is not required.)

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49 2.2.3 ELT REMOTE UNIT LOCATION AND INSTALLATION The ELT Remote Unit assembly must be mounted in the cockpit where the pilot can easily reach th

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5 AK-451 ELT Sets *** with GPS / NAV Position: Ameri-King P/N Description Antennas Included AK-451-(AF)(AP) w/ GPS/Whi/Por (AK-451-23/6) Triple Freq

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50 Figure 10: ELT Remote Switch Installation Figure 10.1: Mounting bracket for ELT Remote Unit (Continued)

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51 Figure 11: Remote Audio Buzzer Monitor P/N 451018

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52 Figure 11.1: Buzzer may be fastened directly onto the Remote Switch Unit 2.2.4 Wiring interconnecting harness The wiring cable is 25 feet lo

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53 Note: The interconnecting wiring is a straight wiring configuration, i.e. Pin 1 to 1, Pin 2 to 2, Pin 3 to 3, and Pin 4 to 4, Pin 5 to 5. To veri

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54 Figure 12.2: Interconnecting Wiring Cable between ELT Remote Unit and Main Unit, Part No. 4500041-4

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55 2.2.5 Audible Monitor Location and Installation: A warning buzzer is required for TSO-C126 approval. The buzzer (P/N 451018) is powered by the E

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56 2.2.6 WIRING CABLE INSTALLATION After installing the ELT Main Unit, Antenna and Remote Unit in the aircraft, install the Coaxial Cable between th

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57 2.4.0 QUICK OPERATION CHECK Note: Refer to Appendix A.1 for Quick Operation Check in sequence order. 2.4.0.1. ELT Main Switch @ ON position: E

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58 Detail Operation Check: 2.4.1 Monitor 121.5 MHz using the Aircraft Communication Receiver or a Portable Hand Held Receiver. Important:

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59 Activate the ELT using applied force. The direction forward force activation is indicated on the ELT. The AK-451-(AF) (AP) ELT can be a

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6 DOCUMENT NO.: IM-451 REV. NC- 4.1g APPLICABILITY Model/Part No.: Fixed Whip Antenna AK 451.017-1B 406/121.5 MHz Or Fixed Rod Antenna AK 451.017-

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60 Detail Test Procedure for ELT ID Programming and Self Test: Turn the main switch from the "OFF" position to the "ARM" posit

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61 2.4.6 GPS Position Test (If GPS is connected) (for using TS-451 Computer Test Set or equivalent): Note: Per FCC Regulation, this test shou

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62 2.4.7 Antenna Check: A low quality AM Broadcast Radio Receiver or Equivalent Test Equipment should be used to determine if energy is bein

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63 Figure 14.1a: Wiring Diagram for AK-451 with 4-wire interconnecting ELT Main Unit and Remote Switch Unit

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64 Figure 14.1b: Wiring Diagram for AK-451 with 2-wire interconnecting ELT Main Unit and Remote Switch Unit

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65 Figure 14.1c: Wiring Diagram for retrofitting AK-451 with 4-wire+ interconnecting ELT Main Unit and Remote Switch Unit, Artex, Pointer, K

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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…

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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

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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

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69 2.5 BATTERY INSTALLATION AND REPLACEMENT 2.5.1 ELT MAIN UNIT BATTERY INSTALLATION AND REPLACEMENT The Ameri-King Corp. Model AK-451 ELT is des

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7 TABLE OF CONTENTS Revision Page ...2 Table of Conte

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70 The following is a step-by-step instruction for replacing ELT Battery Pack P/N 4500010-( ) Series: 1. Using the 3/32” Hex Driver supplied

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71 Figure 16: Battery Pack Replacement for ELT Main Unit (Actual View) Figure 16.1: Battery Pack Replacement for ELT Main Unit (Actual View)

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72 2.5.2 ELT REMOTE UNIT BATTERY INSTALLATION AND REPLACEMENT INSTRUCTIONS The ELT Remote Unit is designed to be powered by a Durace

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73 2.6 FAA Form 337 For most installations an FAA Form 337 will be required for FAA registration. Additional information regarding the completion o

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74 SECTION III OPERATION 3.1 GENERAL This section describes the operation of the ELT, Emergency Locator Transmitter, mo tdel AK-451. The followi

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75 3.2 OPERATION The AK-451 ELT, Emergency Locator Transmitter, is a state of the art Micro controller technology, long lasting, sol

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76 WARNING Do not allow test duration to exceed 5-10 seconds. A false alarm may be generated. Any time the ELT is activated, it is transmitting a 12

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77 Detailed Operation Check: 3.3.1 Main Switch ON/OFF/ARM Operation: In normal operation, the Main Switch, located on the ELT main unit, must be i

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78 Note: The ELT may be ID coding programming during the aforementioned 20 seconds window period. If no programming happened the ELT will t

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

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8 2.2.3 ELT remote unit location and installation ... 48 2.2.4 Wiring interconnecting harness ...

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80 3.3.3.1 Monitor 121.5 MHz using the Aircraft Com Receiver or Portable Hand Held Receiver. Turn the Squelch all the way up or ON. 3.3.3.2 Ensur

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81 In the event of an accident, ensure that the External Aircraft Antenna has no damage. Important: If the ELT is accessible after the acciden

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82 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 Operati

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83 3.3.5.2 Transmitter Self-Test: Turn and hold the main switch, from the "OFF" position to the "SELF TEST" position. The Gree

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84 ELT-(S) Top Label Figure 19: Automatic Portable-ELT (AP) with integral antenna Survival-ELT (S)

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85 Front label Front label for AK-451-(AF)(AP) with dual antennas and (S) Back label F O R W A R D To Activate: Li

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86 Front label for AK-451-(AP) with integral antenna Side label for AK-451-(AP) with integr

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87 3.4 PERIODIC MAINTENANCE (INSTRUCTIONS FOR CONTINUED AIRWORTHINESS): REFERENCES: FAR Part 91.207, Part 43 Appendix D (i). FAR Part 91.207 Para

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88 Note 1: This is not a measured check. It only indicates that the G-Switch is working. 3.4.7.2 Antenna Check: A low quality AM Broadcast R

Seite 230 - APPENDIX K

89 Note: For the following example, the programming protocol is assumed to be Standard Location Protocol, ELT with C/S type approval

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9 3.4.10.4 24-Bit Address Installation Test (mandatory for Installations reprogramming by Ameri-King’s authorized dealer) ...

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90 Step 5: To read ELT ID: Use command “ 03 “ Step 6: View message, ensure that all applicable information is correct (country code, a

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91 The Ameri-King website also contains information on registering beacons in other countries http://www.Ameri-King.com NOTICE: FOR ELTS

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92 communication with the ELT. Without the position data being transmitted, it is necessary for the polar orbiting satellites to pa

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93 II MORROW: • FLYBUDDY, 2001 NMS TRIMBLE NAV INC.: • NAV 1000, NAV 2000, TNL 2100, and TNL3100. The following Trimble systems all require a RS-4

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94 3.4.10.5 GPS Position Test, if equipped (for using TS-451 Computer Test Set or equivalent) : Note: Per FCC Regulation, this test should be cond

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95 Note: When used with ELT's that are programmed for Standard Location 24 bit protocol, the ELT to be program itself to the

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96 PERIODIC MAINTENANCE (at least every year) Note: * These tests should be performed only within an RF Screen Room or Facility providing shielding

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97  Adjust the reference amplitude to place the peak of the carrier slightly above the top graticule fine.  Enable the "fine" amplitude

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98 3.5.3 Frequency Test / Current Draw Test, Performance Testing: NOTE: Using of ELT Test set TS-451 or equivalent test equipment is acceptable Th

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99 3.5.3.4 Current draw tests: CAUTION: The following tests involve measurement of the lithium battery pack. Exercise extreme caution t

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