Ameri-king AK-451-ELT Manual do Utilizador

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

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

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

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

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

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

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

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

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

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)

108

109

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

110

111

112

113

114

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

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

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

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

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

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

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

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

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

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

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

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

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

127

128

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

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

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

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

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

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

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

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

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

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

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

139 ELT Location Protocols User Location Protocols

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

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

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

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

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

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

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

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

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

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

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

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

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

151

152

153

154

155

156

157

158

159

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

160

161

162

163

164

165

166

167

168

169

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

170

171

172

173

174

175

176

177

178

179

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

180

181

182

183

184

185

186

187

188

189

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

190

191

192

193

194

195

196

197

198

199

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.

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

200

201

202

203

204

205

206

207

208

209

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

210

211

212

213

214

215

216

217

218

219

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

220

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

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

223 Japan Civil Aviation Board Approval

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

225

226 This page is left blank on purpose.

227

228

229

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

230 APPENDIX K MATERIAL SAFETY DATA SHEET FOR BATTERY

231

232

233

234

235

236

237

238

239

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

240

241

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

48

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

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

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

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

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

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

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

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

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

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

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

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

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-

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

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

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

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

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

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

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…

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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