
Text extracted from the exhibit documents filed with the FCC. Open a document above to read the original.
86(5∂6+$1'%22. Documentation P/N: 02E62356 Rev C Initial issue: Jun 30/02 Title Page Jul 30/03 86(5∂6+$1'%22. ,1&/8',1*,167$//$7,210$18$/ $1'/2*%22. (0(5*(1&</2&$72575$160,77(5 02'(/$'7$)$3 ,17+(&263$66$56$76<67(0 Issued by (/7$ ) 14 Place Marcel Dassault 31702 BLAGNAC France www.elta.fr SERIAL NUMBER LABEL 86(5∂6+$1'%22. Page 1 Apr 30/03 LIST OF UPDATES INSERTION INSERTION UPDATE No. ISSUE DATE BY UPDATE No. ISSUE DATE BY A B C INITIAL Jun 30/02 Apr 30/03 Jul 30/03 C.CRESP E.LABRIFFE E.LABRIFFE 86(5∂6+$1'%22. Page 2 BLANK PAGE INTENTIONALLY LEFT BLANK 86(5∂6+$1'%22. Page 3 Apr 30/03 LIST OF EFFECTIVE PAGES CHAPTER/ SECTION PAGE DATE CHAPTER/ SECTION PAGE DATE TITLE PAGE LISTE OF UPDATES LIST OF EFFECTIVE PAGE TABLE OF ILLUSTRATIONS LEADING PARTICULARS TABLE OF CONTENTS 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 Jul 30/03 Apr 30/03 BLANK Apr 30/03 BLANK Jun 30/02 BLANK Jun 30/02 BLANK Jun 30/02 BLANK Jun 30/02 Jun 30/02 Jun 30/02 Apr 30/03 Apr 30/03 Apr 30/03 Apr 30/03 Jun 30/02 Apr 30/03 Apr 30/03 Apr 30/03 Apr 30/03 Jul 30/03 Jun 30/02 Apr 30/03 Jun 30/02 Apr 30/03 Apr 30/03 Apr 30/03 Apr 30/03 Jun 30/02 Jun 30/02 Appendix A Appendix B 1 2 3 4 5 6 1 2 3 4 5 6 7 8 9 10 11 12 13 14 Apr 30/03 Apr 30/03 Apr 30/03 Apr 30/03 Apr 30/03 Apr 30/03 Jun 30/02 Jun 30/02 Jun 30/02 Jun 30/02 Jun 30/02 Jun 30/02 Jun 30/02 Jun 30/02 Jun 30/02 Jun 30/02 Jun 30/02 Jun 30/02 Jun 30/02 Jun 30/02 86(5∂6+$1'%22. Page 4 BLANK PAGE INTENTIONALLY LEFT BLANK 86(5∂6+$1'%22. Page 5 Jun 30/02 TABLE OF ILLUSTRATIONS Page Figure 1 : COSPAS/SARSAT - System Principle 12 Figure 2 : ELT ADT 406 AF / AP Presentation 14 Figure 3 : ELT ADT 406 AF / AP – Dimensions (Basic Configuration) 15 Figure 4 : Tolerances on the Axis for Installation of the ELT ADT 406 AF / AP 22 Figure 5 : Installation of the ELT ADT 406 AF / AP - Drilling Pattern Dimensions 24 Figure 6 : ELT ADT 406 AF / AP Installation - Wiring Diagram 25 Figure 7 : ELT ADT 406 AF / AP - Detailed Description 32 86(5∂6+$1'%22. Page 6 BLANK PAGE INTENTIONALLY LEFT BLANK 86(5∂6+$1'%22. Page 7 Jun 30/02 LEADING PARTICULARS &$87,21 7+,675$160,77(5,6$87+25,=(')2586(21/<'85,1*6,78$7,2162)*5$9( $1',00,1(17'$1*(5 &$87,21,7,6,03(5$7,9(7+$7($&+%($&212:1(55(*,67(567+(,5%($&21&217$&7 (/7$25$33529('$*(17722%7$,17+(,1)250$7,215(/$7,9(727+,6 5(*,675$7,21 &$87,21 7+(%($&210867,03(5$7,9(/<%(352*5$00(':,7+7+(5(/(9$17 ,'(17,),&$7,21$87+25,=('%<7+(/2&$/$,5:257+,1(66 &$87,2121&(7+(%($&21+$6%((1352*5$00(',7,6*(1(5$/<$66,*1('72$1 $,5&5$)7 1$0($1','(17,),&$7,21 ,)7+,6%($&21,686('21$127+(5 $,5&5$)7,7:28/'+$9(72%(5(352*5$00(' 1(:1$0($1','(17,),&$7,21 &$87,21 %()25(,167$//,1*2586,1*7+,6(48,30(177+(9$/,',7<2)7+(,1)250$7,21 217+(%($&21/$%(/0867,03(5$7,9(/<%(&+(&.(' 86(5∂6+$1'%22. Page 8 BLANK PAGE INTENTIONALLY LEFT BLANK 86(5∂6+$1'%22. Page 9 Jun 30/02 TABLE OF CONTENTS PAGE 1. INTRODUCTION TO THE COSPAS-SARSAT SYSTEM 11 A. The COSPAS-SARSAT system 11 B. System organization 11 C. The distress frequencies 13 D. ELTA and the COSPAS-SARSAT system 13 2. GENERAL DETAILS OF THE ELT ADT 406 AF / AP 14 A. Purpose of the ELT ADT 406 AF / AP 14 B. Characteristics 16 3. DESCRIPTION OF THE ELT ADT 406 AF / AP AND OF THE AIRCRAFT COMPONENTS 18 A. General description 18 B. Detailed description 18 4. INSTALLATION OF THE ELT ADT 406 AF / AP 22 A. General 22 B. Installation of the beacon on the aircraft 22 C. External antenna installation 24 D. Remote control unit installation 24 E. Installation and configuration of the beacon 26 5. UTILIZATION OF THE ELT ADT 406 AF / AP 27 A. Automatic activation 27 B. Manual activation 27 C. Beacon shutdown 28 D. Beacon self-test 28 6. MAINTENANCE OF THE ELT ADT 406 AF / AP 30 A. Beacon self-test 30 B. Maintenance periodicity table 30 C. Battery replacement 30 D. Battery discarding 31 E. Test to do at the time of a beacon return in workshop 31 86(5∂6+$1'%22. Page 10 BLANK PAGE INTENTIONALLY LEFT BLANK 86(5∂6+$1'%22. Page 11 Jun 30/02 1. INTRODUCTION TO THE COSPAS-SARSAT SYSTEM A. The COSPAS-SARSAT* system The purpose of the COSPAS-SARSAT satellite system is to detect and locate all distress signals transmitted by aeronautical, maritime or land-based beacons, for the search and rescue organizations. This program is the result of an international collaboration between the United States, Canada and France on the one hand (SARSAT project), and Russia on the other hand (COSPAS project). These two projects are fully compatible. Since the first results were obtained several countries have joined the program. Several other countries have shown an interest and will soon be joining the COSPAS-SARSAT system partners. ELTA in relation with CNES (French National Space Agency) has developed the complete range of products required for COSPAS-SARSAT system operation. Following an in-depth study phase, ELTA has arrived at highly conclusive technical results, and experimental and operational use of the "ground" equipment have proven this equipment’s reliability and ease-of-use. B. System organization (Ref. Fig. 1) In the COSPAS-SARSAT system, space equipment is placed on board several satellites in low near-polar orbit to capture transmissions from emergency transmitters and to retransmit these signals to specialized ground stations called / ocal 8 ser 7 erminals (LUT). These ground stations determine the position of the emergency transmitters and then retransmit the position data to the designated 0 ission & ontrol & enters (MCC). The MCCs in turn retransmit these data to the appropriate 5 escue & oordination & enters (RCC) so that they can start the search and rescue operations. * COSPAS-SARSAT : COSPAS = Kosmicheskaya Sistyema Poiska Avariynych Sudov SARSAT = Search and Rescue Satellite-Aided Tracking 86(5∂6+$1'%…
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86(5∂6+$1'%22. Documentation P/N: 03E61013 Rev B Initial issue: Feb 15/03 Title Page Apr 17/03 86(5∂6+$1'%22. ,1&/8',1*,167$//$7,210$18$/ $1'/2*%22. (0(5*(1&</2&$72575$160,77(5 02'(/$'7$3 ,17+(&263$66$56$76<67(0 Issued by (/7$ ) 14 Place Marcel Dassault 31702 BLAGNAC France www.elta.fr SERIAL NUMBER LABEL 86(5∂6+$1'%22. Page 1 Apr 17/03 LIST OF UPDATES INSERTION INSERTION UPDATE No. ISSUE DATE BY UPDATE No. ISSUE DATE BY A B INITIAL Feb 15/03 Apr 17/03 E.LABRIFFE E.LABRIFFE 86(5∂6+$1'%22. Page 2 BLANK PAGE INTENTIONALLY LEFT BLANK 86(5∂6+$1'%22. Page 3 Apr 17/03 LIST OF EFFECTIVE PAGES CHAPTER/ SECTION PAGE DATE CHAPTER/ SECTION PAGE DATE TITLE PAGE LISTE OF UPDATES LIST OF EFFECTIVE PAGE TABLE OF ILLUSTRATIONS LEADING PARTICULARS TABLE OF CONTENTS 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 Apr 17/03 Apr 17/03 BLANK Apr 17/03 BLANK Feb 15/03 BLANK Feb 15/03 BLANK Feb 15/03 BLANK Feb 15/03 Feb 15/03 Feb 15/03 Apr 17/03 Apr 17/03 Apr 17/03 Apr 17/03 Apr 17/03 Feb 15/03 Apr 17/03 Feb 15/03 Feb 15/03 Feb 15/03 Feb 15/03 Feb 15/03 Apr 17/03 Feb 15/03 Apr 17/03 Apr 17/03 Apr 17/03 Apr 17/03 Feb 15/03 Feb 15/03 Apr 17/03 Appendix A Appendix B 1 2 3 4 5 1 2 3 4 5 6 7 8 9 10 11 12 13 14 Feb 15/03 Feb 15/03 Feb 15/03 Feb 15/03 Feb 15/03 Feb 15/03 Feb 15/03 Feb 15/03 Feb 15/03 Feb 15/03 Feb 15/03 Feb 15/03 Feb 15/03 Feb 15/03 Feb 15/03 Feb 15/03 Feb 15/03 Feb 15/03 Feb 15/03 86(5∂6+$1'%22. Page 4 BLANK PAGE INTENTIONALLY LEFT BLANK 86(5∂6+$1'%22. Page 5 Feb 15/03 TABLE OF ILLUSTRATIONS Page Figure 1 : COSPAS/SARSAT - System Principle 12 Figure 2 : ELT ADT 406 AP Presentation 14 Figure 3 : ELT ADT 406 AP – Dimensions (Basic Configuration) 15 Figure 4 : Tolerances on the Axis for Installation of the ELT ADT 406 AP 22 Figure 5 : Installation of the ELT ADT 406 AP - Drilling Pattern Dimensions 24 Figure 6 : ELT ADT 406 AP Installation - Wiring Diagram 26 Figure 7 : ELT ADT 406 AP - Detailed Description 34 86(5∂6+$1'%22. Page 6 BLANK PAGE INTENTIONALLY LEFT BLANK 86(5∂6+$1'%22. Page 7 Feb 15/03 LEADING PARTICULARS &$87,21 7+,675$160,77(5,6$87+25,=(')2586(21/<'85,1*6,78$7,2162)*5$9( $1',00,1(17'$1*(5 &$87,21,7,6,03(5$7,9(7+$7($&+%($&212:1(55(*,67(567+(,5%($&21&217$&7 (/7$25$33529('$*(17722%7$,17+(,1)250$7,215(/$7,9(727+,6 5(*,675$7,21 &$87,21 7+(%($&210867,03(5$7,9(/<%(352*5$00(':,7+7+(5(/(9$17 ,'(17,),&$7,21$87+25,=('%<7+(/2&$/$,5:257+,1(66 &$87,2121&(7+(%($&21+$6%((1352*5$00(',7,6*(1(5$/<$66,*1('72$1 $,5&5$)7 1$0($1','(17,),&$7,21 ,)7+,6%($&21,686('21$127+(5 $,5&5$)7,7:28/'+$9(72%(5(352*5$00(' 1(:1$0($1','(17,),&$7,21 &$87,21 %()25(,167$//,1*2586,1*7+,6(48,30(177+(9$/,',7<2)7+(,1)250$7,21 217+(%($&21/$%(/0867,03(5$7,9(/<%(&+(&.(' 86(5∂6+$1'%22. Page 8 BLANK PAGE INTENTIONALLY LEFT BLANK 86(5∂6+$1'%22. Page 9 Feb 15/03 TABLE OF CONTENTS PAGE 1. INTRODUCTION TO THE COSPAS-SARSAT SYSTEM 11 A. The COSPAS-SARSAT system 11 B. System organization 11 C. The distress frequencies 13 D. ELTA and the COSPAS-SARSAT system 13 2. GENERAL DETAILS OF THE ELT ADT 406 AP 14 A. Purpose of the ELT ADT 406 AP 14 B. Characteristics 16 3. DESCRIPTION OF THE ELT ADT 406 AP AND OF THE AIRCRAFT COMPONENTS 18 A. General description 18 B. Detailed description 18 4. INSTALLATION OF THE ELT ADT 406 AP 22 A. General 22 B. Installation of the beacon on the aircraft 22 C. External antenna installation 25 D. Remote control unit installation 25 E. Installation and configuration of the beacon 27 5. UTILIZATION OF THE ELT ADT 406 AP 28 A. Automatic activation 28 B. Manual activation 28 C. Beacon shutdown 30 D. Beacon self-test 30 6. MAINTENANCE OF THE ELT ADT 406 AP 32 A. Beacon self-test 32 B. Maintenance periodicity table 32 C. Battery replacement 32 D. Battery discarding 33 E. Test to do at the time of a beacon return in workshop 33 86(5∂6+$1'%22. Page 10 BLANK PAGE INTENTIONALLY LEFT BLANK 86(5∂6+$1'%22. Page 11 Feb 15/03 1. INTRODUCTION TO THE COSPAS-SARSAT SYSTEM A. The COSPAS-SARSAT* system The purpose of the COSPAS-SARSAT satellite system is to detect and locate all distress signals transmitted by aeronautical, maritime or land-based beacons, for the search and rescue organizations. This program is the result of an international collaboration between the United States, Canada and France on the one hand (SARSAT project), and Russia on the other hand (COSPAS project). These two projects are fully compatible. Since the first results were obtained several countries have joined the program. Several other countries have shown an interest and will soon be joining the COSPAS-SARSAT system partners. ELTA in relation with CNES (French National Space Agency) has developed the complete range of products required for COSPAS-SARSAT system operation. Following an in-depth study phase, ELTA has arrived at highly conclusive technical results, and experimental and operational use of the "ground" equipment have proven this equipment’s reliability and ease-of-use. B. System organization (Ref. Fig. 1) In the COSPAS-SARSAT system, space equipment is placed on board several satellites in low near-polar orbit to capture transmissions from emergency transmitters and to retransmit these signals to specialized ground stations called / ocal 8 ser 7 erminals (LUT). These ground stations determine the position of the emergency transmitters and then retransmit the position data to the designated 0 ission & ontrol & enters (MCC). The MCCs in turn retransmit these data to the appropriate 5 escue & oordination & enters (RCC) so that they can start the search and rescue operations. * COSPAS-SARSAT : COSPAS = Kosmicheskaya Sistyema Poiska Avariynych Sudov SARSAT = Search and Rescue Satellite-Aided Tracking 86(5∂6+$1'%22. Page 12 Feb 15/03 Legend : ELT : ( mergency / ocator 7 ransmitter …
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03B65215 Page 1/2 FEDERAL COMMUNICATION COMMISSION 445 12TH STREET, SW WASHINGTON, DC 20554 USA Blagnac, on September 5, 2003 V/Réf. : N/Réf : 03B65215 P.J. : ELTA Grantee Code: LYJ ELTA contact : C. CRESP, [email protected] SUBJECT : Attestations Statement (Request for Equipment notification) Dear Sir, Please find here included the obtained approvals related to our new Emergency Locator Transmitter (ELT) model ADT 406. This model can be divided in two versions: • ADT 406 AF/AP, designed for Automatic Fixed application or Automatic Portable application when floatation is not required, • ADT 406 AP designed for Automatic Portable application when floatation is required. These two versions use the same transmitter board. A common FCC-ID: LYJADT406 is required. These ELT are approved by: • COSPAS-SARSAT, with the Type Approval Number N° 0131 dated July 15, 2002 • FAA, with the TSO C91a & TSO C126 letter dated February 24, 2003 • FAA, with the TSO C91a & TSO C126 letter dated June 12, 2003 • JAA, with the JTSO2 C91a & JTSO2 C126 letter N° F.O. 089 dated October 3, 2002 • JAA, with the JTSO2 C91a & JTSO2 C126 letter N° F.O. 112 dated April 29, 2003 Copies of these approvals are presented here under. Note: For information we present also the FCC ID:LYJA06T already obtained on our previous range of ELT (model A06T) 03B65215 page 2 / 2 COSPAS-SARSAT Type Approval Certificate N° 0131 FAA TSO C91a & TSO C126 LETTER dated February 24, 2003 FAA TSO C91a & TSO C126 LETTER dated June 12, 2003 JAA JTSO2 C91a & JTSO2 C126 LETTER F.O. 089 dated October 3, 2002 JAA JTSO2 C91a & JTSO2 C126 LETTER F.O. 112 dated April 29, 2003 Note: For information FCCID:LYJA06T already obtained on our previous A06T ELT (CEIS TM was the previous name of ELTA) C . CRESP Product Support Manager tac131_ADT406AF-AP.pdf TSO_ADT_406_AF_AP.pdf TSO_ADT_406_AP.pdf FO089-JTSO-ADT406-AF-AP.pdf JTSO_ADT_406_AP.pdf FCC-ID_A06T.pdf
DRAFT Mr. Andy Leimer Federal Communications Commission Equipment Authorization Branch 7435 Oakland Mills Road Columbia, Maryland 21046 Dear Mr. Leimer: The Federal Aviation Administration (FAA) Office of Spectrum Policy and Management, has reviewed the Type Acceptance Certification request from ELTA for their Emergency Locator Transmitter Model ADT 406, ID number LYJADT406. With the addition of the enclosed information from ELTA, the technical data for this equipment is consistent with the spectrum requirements and we have no objections to certification of this device. Should you have any questions or concerns, please contact Mr. Donald Nellis, Spectrum Planning and International Division, at (202) 267-9779. Sincerely, Donald K. Willis, Manager, Spectrum Planning and International Division Enclosure File: 1200-5-1 S/ASRSHARE/DNELLIS/ljg/2/2/04/LYJADT406_ELT.doc Enclosure From: ABADIE Jean-Paul [mailto:[email protected]] Sent: Monday, February 02, 2004 9:30 AM To: '[email protected]'; Andrew Leimer Cc: CRESP Claude Subject: TR: Demande FCC/FAA - ma visite à la FAA de mardi pour terminer ce dossier qui "traine depuis Début Décembre", pas par notre faute. Dear Sir, Please find here-attached spectrum at 121,5 MHz and 243 MHz, for our ADT406 beacon. For 121,5 MHz, the spectrum show power distribution : - from Fo+6KHz (resp. Fo-6KHz) to Fo+12 KHz (resp. Fo-12 KHz) : Power level < 30 dBc at +/-6KHz offset from Fo. - above Fo+12 KHz (resp. under Fo-12KHz) : Power level < 38 dBc at +/-12KHz offset from Fo. We consider that assigned frequency band is 121,5 MHz +/- 6KHz, so assigned frequency band is 12KHz. Please note that Max power of the AM signal at 121,5 MHz (when modulation is high) is 23 dBm. For 243 MHz, the spectrum show power distribution : - from Fo+12KHz (resp. Fo-12KHz) to Fo+24 KHz (resp. Fo-24 KHz) : Power level < 39 dBc at +/-12KHz offset from Fo. - above Fo+24 KHz (resp. under Fo-24KHz) : Power level < 42 dBc at +/-24KHz offset from Fo. We consider that assigned frequency band is 243MHz +/- 12KHz, so assigned frequency band is 24KHz. Please note that Max power of the AM signal at 243 MHz (when modulation is high) is 23 dBm. Best regards, Jean-Paul Abadie > -----Message d'origine----- > De: LABRIFFE Emmanuel > Date: lundi 2 février 2004 13:05 > À: CRESP Claude; ABADIE Jean-Paul; CAZAL Antoine > Objet: RE: Demande FCC/FAA - ma visite à la FAA de mardi pour > terminer ce dossier qui "traine depuis Début Décembre", pas par notre > faute. > > Bonjour Claude, > > Voici de la part de Jean-Paul les spectres demandés. > Deux pour le 121.5 et deux pour le 243 Mhz. > > Je n'ai pas de détails sur les conditions de mesure... > > <<spectres 121 & 243.tif>> > @+, > Emmanuel LABRIFFE > > ------- ELTA ------- tel. : 05 34 36 10 00 L.D. : 05 34 36 10 42 [email protected] 14, place Marcel Dassault BP 48 31702 BLAGNAC > > > -----Message d'origine----- > De : CRESP Claude > Envoyé : dimanche 1 février 2004 16:22 > À : ABADIE Jean-Paul; CAZAL Antoine > Cc : LABRIFFE Emmanuel > Objet : Demande FCC/FAA - ma visite à la FAA de mardi pour terminer > ce dossier qui "traine depuis Début Décembre", pas par notre faute. > > Salut Jean Paul, > Ne m'oubliez pas lundi matin (mesures des spectres 121.5 et 243 MHz > des ADT 406, C'est la dernière ligne droite et surtout la dernière > chance, sinon Japan Airlines va demander à BOEING de monter une balise > concurente (Honeywell très certainement)sur leur nouveaux avions (le > prochain est en Avril). Ce serait très domage après tous ces efforts. > Précisez moi aussi les conditions de mesures sur l'analyseur de spectre > au > cas où j'ai des questions de niveau 0 (Il y a si longtemps que je n'ai pas > manipé que j'ai quelques troups de mémoire). > Merci d'avance pour votre aide. Je pars pour Little Rock (Dassault Falcon Jet) dans une heure Best Regards Sincères Salutations ---------------------------------------------------------------------- Claude CRESP ELTA, 14 Place Marcel Dassault, BP 48 Product Support Manager 31702 Blagnac Cedex France Phone +33 534 361 080 Mobile + 33 632 646 690 Fax +33 534 361 152 email [email protected] >
DRAFT Mr. Andy Leimer Federal Communications Commission Equipment Authorization Branch 7435 Oakland Mills Road Columbia, Maryland 21046 Dear Mr. Leimer: The Federal Aviation Administration (FAA) Office of Spectrum Policy and Management, has reviewed the Type Acceptance Certification request from ELTA for their Emergency Locator Transmitter Model ADT 406, ID number LYJADT406. With the addition of the enclosed information from ELTA, the technical data for this equipment is consistent with the spectrum requirements and we have no objections to certification of this device. Should you have any questions or concerns, please contact Mr. Donald Nellis, Spectrum Planning and International Division, at (202) 267-9779. Sincerely, Donald K. Willis, Manager, Spectrum Planning and International Division Enclosure File: 1200-5-1 S/ASRSHARE/DNELLIS/ljg/2/2/04/LYJADT406_ELT.doc Enclosure From: ABADIE Jean-Paul [mailto:[email protected]] Sent: Monday, February 02, 2004 9:30 AM To: '[email protected]'; Andrew Leimer Cc: CRESP Claude Subject: TR: Demande FCC/FAA - ma visite à la FAA de mardi pour terminer ce dossier qui "traine depuis Début Décembre", pas par notre faute. Dear Sir, Please find here-attached spectrum at 121,5 MHz and 243 MHz, for our ADT406 beacon. For 121,5 MHz, the spectrum show power distribution : - from Fo+6KHz (resp. Fo-6KHz) to Fo+12 KHz (resp. Fo-12 KHz) : Power level < 30 dBc at +/-6KHz offset from Fo. - above Fo+12 KHz (resp. under Fo-12KHz) : Power level < 38 dBc at +/-12KHz offset from Fo. We consider that assigned frequency band is 121,5 MHz +/- 6KHz, so assigned frequency band is 12KHz. Please note that Max power of the AM signal at 121,5 MHz (when modulation is high) is 23 dBm. For 243 MHz, the spectrum show power distribution : - from Fo+12KHz (resp. Fo-12KHz) to Fo+24 KHz (resp. Fo-24 KHz) : Power level < 39 dBc at +/-12KHz offset from Fo. - above Fo+24 KHz (resp. under Fo-24KHz) : Power level < 42 dBc at +/-24KHz offset from Fo. We consider that assigned frequency band is 243MHz +/- 12KHz, so assigned frequency band is 24KHz. Please note that Max power of the AM signal at 243 MHz (when modulation is high) is 23 dBm. Best regards, Jean-Paul Abadie > -----Message d'origine----- > De: LABRIFFE Emmanuel > Date: lundi 2 février 2004 13:05 > À: CRESP Claude; ABADIE Jean-Paul; CAZAL Antoine > Objet: RE: Demande FCC/FAA - ma visite à la FAA de mardi pour > terminer ce dossier qui "traine depuis Début Décembre", pas par notre > faute. > > Bonjour Claude, > > Voici de la part de Jean-Paul les spectres demandés. > Deux pour le 121.5 et deux pour le 243 Mhz. > > Je n'ai pas de détails sur les conditions de mesure... > > <<spectres 121 & 243.tif>> > @+, > Emmanuel LABRIFFE > > ------- ELTA ------- tel. : 05 34 36 10 00 L.D. : 05 34 36 10 42 [email protected] 14, place Marcel Dassault BP 48 31702 BLAGNAC > > > -----Message d'origine----- > De : CRESP Claude > Envoyé : dimanche 1 février 2004 16:22 > À : ABADIE Jean-Paul; CAZAL Antoine > Cc : LABRIFFE Emmanuel > Objet : Demande FCC/FAA - ma visite à la FAA de mardi pour terminer > ce dossier qui "traine depuis Début Décembre", pas par notre faute. > > Salut Jean Paul, > Ne m'oubliez pas lundi matin (mesures des spectres 121.5 et 243 MHz > des ADT 406, C'est la dernière ligne droite et surtout la dernière > chance, sinon Japan Airlines va demander à BOEING de monter une balise > concurente (Honeywell très certainement)sur leur nouveaux avions (le > prochain est en Avril). Ce serait très domage après tous ces efforts. > Précisez moi aussi les conditions de mesures sur l'analyseur de spectre > au > cas où j'ai des questions de niveau 0 (Il y a si longtemps que je n'ai pas > manipé que j'ai quelques troups de mémoire). > Merci d'avance pour votre aide. Je pars pour Little Rock (Dassault Falcon Jet) dans une heure Best Regards Sincères Salutations ---------------------------------------------------------------------- Claude CRESP ELTA, 14 Place Marcel Dassault, BP 48 Product Support Manager 31702 Blagnac Cedex France Phone +33 534 361 080 Mobile + 33 632 646 690 Fax +33 534 361 152 email [email protected] >
03B65217 Page 1/1 FEDERAL COMMUNICATION COMMISSION 445 12TH STREET, SW WASHINGTON, DC 20554 USA Blagnac, on September 5, 2003 V/Réf. : N/Réf : 03B65217 P.J. : ELTA Grantee Code: LYJ ELTA contact : C. CRESP, [email protected] SUBJECT : Cover Letter – ELT models ADT 406 Request for Equipment notification: FCCID:LYJADT406 Dear Sir, By this letter ELTA is requiring a new Equipment Authorization Notification for our new Emergency Locator Transmitter (ELT) model ADT 406. This model can be divided in two versions: • ADT 406 AF/AP, designed for Automatic Fixed application or Automatic Portable application when floatation is not required, • ADT 406 AP designed for Automatic Portable application when floatation is required. These two versions use the same transmitter board . These equipment (New ELT) were designed to upgrade and in a medium term to replace our previous range of ELT already approved by FCC per the FCCID: LYJA06T. These new ELT keeps the same functionality’s and transmits both on 121.5-243 and 406 MHz. Note: on 406 MHz we are using the latest channel authorized by Cospas-Sarsat (406.028 MHz) . Transmission characteristics are the same but use updated components. C. CRESP Product Support Manager
03B65228 Page 1/1 FEDERAL COMMUNICATION COMMISSION 445 12TH STREET, SW WASHINGTON, DC 20554 USA Blagnac, on September 5, 2003 V/Réf. : N/Réf : 03B65228 P.J. : ELTA Grantee Code: LYJ ELTA contact : C. CRESP, [email protected] SUBJECT : EXHIBIT DESCRIPTION (Request for Equipment notification). Dear Sir, Please find here under the exhibit list related to our new Emergency Locator Transmitter (ELT) model ADT 406 that can be divided in two versions: • ADT 406 AF/AP, designed for Automatic Fixed application or Automatic Portable application when floatation is not required, • ADT 406 AP designed for Automatic Portable application when floatation is required. Exhibit 1 “Attestation Statements”, ELTA letter 03B65215 (Word document) Exhibit 2 “Block Diagrams”, ELTA letter 03B65216 (Word document) Exhibit 3 “Cover letter”, ELTA letter 03B65217 (Word document) Exhibit 4 “External photo”, ELTA letter 03B65218 (Word document) Exhibit 5 “ID Label/location Info”, ELTA letter 03B65219 (Word document) Exhibit 6 “Internal Photos”, ELTA letter 03B65220 (Word document) Exhibit 7 “Operational Description”, ELTA letter 03B65221 (Word document) Exhibit 8 “Parts List/Tune Info.”, ELTA letter 03B65222 (Word document) Exhibit 9 “RF Exposure Info.”, ELTA letter 03B65223 (Word document) Exhibit 10 “Schematics”, ELTA letter 03B65224 (Word document) Exhibit 11 “Test Reports”, ELTA letter 03B65225 (Word document) Exhibit 12 “Test setup Info.”, ELTA letter 03B65226 (Word document) Exhibit 13 “ADT 406 AF/AP User’s Manual”, ELTA doc 02E65336 (pdf document) Exhibit 14 “ADT 406AP User’s Manual”, ELTA doc 03E61013 (pdf document) Exhibit 15 “Confidentiality”, ELTA letter 03B65227 (Word document) Exhibit 16 “Exhibit list”, this ELTA letter 03B65228 (Word document) C. CRESP Product Support Manager
03B65227 Page 1/1 FEDERAL COMMUNICATION COMMISSION 445 12TH STREET, SW WASHINGTON, DC 20554 USA Blagnac, on September 5, 2003 V/Réf. : N/Réf : 03B65227 P.J. : ELTA Grantee Code: LYJ ELTA contact : C. CRESP, [email protected] SUBJECT : Confidentiality for our ELT models ADT 406 (Request for Equipment notification) Dear Sir, By this letter ELTA is requesting confidentiality on the following items presented to FCC for Equipment Authorization: • Block diagram per ELTA letter N° 03B65216, • Internal photos per ELTA letter N° 03B65220, • Schematics per ELYTA letter N° 03B65224, Related to our new Emergency Locator Transmitter (ELT) model ADT 406 that can be divided in two versions: • ADT 406 AF/AP, designed for Automatic Fixed application or Automatic Portable application when floatation is not required, • ADT 406 AP designed for Automatic Portable application when floatation is required. Internal photo need to be kept confidential as these ELT are new equipments and we wants to protect our marketing advance in this domain. C. CRESP Product Support Manager
03B65227 Page 1/1 FEDERAL COMMUNICATION COMMISSION 445 12TH STREET, SW WASHINGTON, DC 20554 USA Blagnac, on September 5, 2003 V/Réf. : N/Réf : 03B65227 P.J. : ELTA Grantee Code: LYJ ELTA contact : C. CRESP, [email protected] SUBJECT : Confidentiality for our ELT models ADT 406 (Request for Equipment notification) Dear Sir, By this letter ELTA is requesting confidentiality on the following items presented to FCC for Equipment Authorization: • Block diagram per ELTA letter N° 03B65216, • Internal photos per ELTA letter N° 03B65220, • Schematics per ELYTA letter N° 03B65224, Related to our new Emergency Locator Transmitter (ELT) model ADT 406 that can be divided in two versions: • ADT 406 AF/AP, designed for Automatic Fixed application or Automatic Portable application when floatation is not required, • ADT 406 AP designed for Automatic Portable application when floatation is required. Internal photo need to be kept confidential as these ELT are new equipments and we wants to protect our marketing advance in this domain. C. CRESP Product Support Manager
03B65228 Page 1/1 FEDERAL COMMUNICATION COMMISSION 445 12TH STREET, SW WASHINGTON, DC 20554 USA Blagnac, on September 5, 2003 V/Réf. : N/Réf : 03B65228 P.J. : ELTA Grantee Code: LYJ ELTA contact : C. CRESP, [email protected] SUBJECT : EXHIBIT DESCRIPTION (Request for Equipment notification). Dear Sir, Please find here under the exhibit list related to our new Emergency Locator Transmitter (ELT) model ADT 406 that can be divided in two versions: • ADT 406 AF/AP, designed for Automatic Fixed application or Automatic Portable application when floatation is not required, • ADT 406 AP designed for Automatic Portable application when floatation is required. Exhibit 1 “Attestation Statements”, ELTA letter 03B65215 (Word document) Exhibit 2 “Block Diagrams”, ELTA letter 03B65216 (Word document) Exhibit 3 “Cover letter”, ELTA letter 03B65217 (Word document) Exhibit 4 “External photo”, ELTA letter 03B65218 (Word document) Exhibit 5 “ID Label/location Info”, ELTA letter 03B65219 (Word document) Exhibit 6 “Internal Photos”, ELTA letter 03B65220 (Word document) Exhibit 7 “Operational Description”, ELTA letter 03B65221 (Word document) Exhibit 8 “Parts List/Tune Info.”, ELTA letter 03B65222 (Word document) Exhibit 9 “RF Exposure Info.”, ELTA letter 03B65223 (Word document) Exhibit 10 “Schematics”, ELTA letter 03B65224 (Word document) Exhibit 11 “Test Reports”, ELTA letter 03B65225 (Word document) Exhibit 12 “Test setup Info.”, ELTA letter 03B65226 (Word document) Exhibit 13 “ADT 406 AF/AP User’s Manual”, ELTA doc 02E65336 (pdf document) Exhibit 14 “ADT 406AP User’s Manual”, ELTA doc 03E61013 (pdf document) Exhibit 15 “Confidentiality”, ELTA letter 03B65227 (Word document) Exhibit 16 “Exhibit list”, this ELTA letter 03B65228 (Word document) C. CRESP Product Support Manager
03B65312 Page 1/1 FEDERAL COMMUNICATION COMMISSION 445 12TH STREET, SW WASHINGTON, DC 20554 USA Blagnac, on September 9, 2003 V/Réf. : N/Réf : 03B65312 P.J. : ELTA Grantee Code: LYJ ELTA contact : C. CRESP, [email protected] SUBJECT : Confirmation for test modification on our ELT models ADT 406 (Request for Equipment notification) Dear Sir, By this letter we, ELTA , confirm that all the modifications found during the qualification process (tests) will be implemented into all production units. This rule is part of our Quality plan and specially apply for all the Aeronautic equipment such as the ELT (Emergency Locator transmitter). Our basic development is as follow: • Design, • Internal tests and verification • Qualification test • Design file evolution following qualification tests • Pre production run • First article Inspection • Update of design and production file. Any evolution are approved by the…
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| # | Rule Parts | Frequency Range | Power Output | Emission | Tolerance |
|---|---|---|---|---|---|
| 3 | 87 | 242.988 MHz - 243.012 MHz | 200.00 mW | 3K20A3X | 12000 Hz |

ELT model ADT 406S (Emergency Locator Transmitter)
Equipment Class
TNB - Licensed Non-Broadcast Station TransmitterGET - 406 MHz ELT
Equipment Class
GET - 406 MHz ELTSRT - Radar Transponder
Equipment Class
SRT - Radar Transponder