Attachment 20130326124822.pdf

20130326124822.pdf

DECISION submitted by IB/FCC

Grant STA

2013-03-26

This document pretains to SES-STA-20120913-00820 for Special Temporal Authority on a Satellite Earth Station filing.

IBFS_SESSTA2012091300820_991517

                                        1B2012002135
E100089     SES—STA—20120913—00820
                             on
Panasonic Avionics Corporati


                                                                                                                                             Approved by OMB
                                                                                                                                                   3060—0678
                                    APPLICATION FOR EARTH STATION SPECIAL TEMPORARY AUTHORITY



 APPLICANT INFORMATIONEnter a description of this application to identify it on the main menu:
 Panasonic application for interim operation ofAura LE terminal and to correct number of MELCO terminals
  1. Applicant


              Name:           Panasonic Avionics Corporation   Phone Number:                                         949—462—1683
              DBA Name:                                        Fax Number:

              Street:         26200 Enterprise Way             E—Mail:                                               mark.defazio@panasonic.aero


              City:           Lake Forest                      State:                                                    CA
              Country:            USA                          Zipcode:                                              92630        =
              Attention:      Mark DeFazio




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     Applicant:     Panasonic Avionics Corporation
     Call Sign:     E100089
     File No.:      SES—STA—20120913—00820

     Panasonic Avionics Corporation (Panasonic) is granted special temporary authority from
     March 22, 2012 to May 21, 2013 to operate twenty technically identical aircraft earth
     stations aboard U.S.—registered aircraft using Panasonic model AURA LE 0.89 meter
     antennas. The aircraft earth stations will transmit to the following geostationary—orbit
     space stations in the 14.0—14.5 GHz (Earth—to—space) bands: Galaxy 17 (Call Sign $2715)
     at 91° W.L; EutelSat 172A (formerly GE—23) (Call Sign $2610) at 172° E.L.; Estrela do
     Sul 2 (Call Sign $2821) at 63° W.L; and Telstar 11N (Call Sign $2357) at 37.5° W.L.
     The aircraft earth stations will receive transmissions in the 11.45—11.7 GHz, 10.95—11.2
     GHz, and 12.2—12.75 GHz (space—to—Earth) frequency bands from EutelSat 172A; in the
     11.45—12.2 GHz (space—to—Earth) frequency band from Estrela do Sul 2; in the 11.7—12.2
     GHz (space—to—Earth) frequency band from Galaxy 17; and in the 11.45—12.2 GHz and
     11.7—12.2 GHz (space—to—Earth) frequency bands from Telstar 11N. Operations under
     this STA must be in accordance with the terms and conditions contained in Panasonic‘s
     application, as supplemented, and the Federal Communications Commission‘s rules, and
     are subject to the following conditions:

     1. Communications with Panasonic‘s aircraft earth stations in the space—to—Earth
     direction are limited to the following frequency bands and coverage areas identified by
     Panasonic in its supplemental letter dated November 30, 2012

Space Station                       Downlink                TITU Region(s)
                                    Frequencies
                                    (space—to—Earth)
EutelSat 172A (Call Sign $2610)     11.45—11.7 GHz          Region 2 (incl. AK and HI) and Region
                                                            3
                                    10.95—11.2 GHz          Region 3
                                    12.2—12.75 GHz          Region 3
Estrela do Sul 2 (Call Sign         11.45—12.2 GHz          Regions 1 and 2 (outside US airspace)
$2821)
Galaxy 17 (Call Sign $2715)         11.7—12.2 GHz           Region 2 (Continental U.S.)
Telstar 11N (Call Sign $2357)       11.45—12.2 GHz          Regions 1 and 2 (outside US airspace)
                                    11.7—12.2 GHz           Region 2 (Continental U.S.)

     2. Operation under this grant of special temporary authority must be on an unprotected
     and non—harmful interference basis, i.e., while operating under this temporary authority
     Panasonic must not cause harmful interference to, and must not claim protection from
     interference caused to it by, any other lawfully operating radiocommunication system.
     Panasonic must cease operations immediately upon notification of such interference and
     must immediately inform the Commission, in writing, of such an event.




                                                                                                ) of[


3. Communications in the 11.45—11.7 GHz band (space—to—Earth) must be in accordance
with the space station authorization for EutelSat 172A. See SAT—LOA—20031218—00358
(granted July 13, 2004).

4. Panasonic must maintain records of the following data for each earth station operating
pursuant to this temporary authorization: location (latitude, longitude, altitude); aircraft
attitude (pitch, yaw, roll); transmit frequency and occupied bandwidth; data rate; EIRP;
and target satellite. This data must be recorded at intervals of no more than two minutes
while an aircraft earth station is transmitting and every 30 seconds when aircraft roll
angle is greater than 10 degrees. Panasonic must also record antenna pointing error at 30—
second intervals when the error exceeds 0.25 degrees. Panasonic shall make this data
available upon request to an FSS system operator or the Commission within 24 hours
after receiving the request.

5. When operating in international airspace within line—of—sight of the territory of a
foreign administration where Fixed Service networks have a primary allocation in the
14.0—14.5 GHz band, an AURA LE earth station must not produce ground—level pfd in
such territory in excess of the following values unless the foreign administration has
imposed other conditions for protecting its FS stations: —132 + 0.5 x THETA dB(W/(m*"2
MHz)) for THETA <= 40° —112 dB(W/(m*~2 MHz)) for 40° < THETA <= 90°. Where:
THETA is the angle of arrival of the radio—frequency wave in degrees above the
horizontal, and the aforementioned limits relate to the pfd and angles of arrival that
would be obtained under free space propagation conditions.

6. Operation pursuant to this authorization must be in compliance with of Panasonic‘s
coordination agreements with the National Aeronautics and Space Administration and
National Science Foundation pertaining to the operation of aircraft earth stations in the
Ku—band. (See e.g.,"Coordination Agreement for the Joint Usage of the Band 14.0 — 14.5
GHz Between the National Science Foundation and Panasonic Avionics Corporation,"
Version 1.1, signed on December 18, 2009).

7. Operation pursuant to this authorization outside the United States in the 14.0—14.5 GHz
band must be in compliance with the provisions of Annex 1, Part C of Recommendation
ITU—R M.1643, with respect to any radio astronomy station performing observations in
the 14.47—14.5 GHz band.

8. Operation pursuant to this authorization must be in compliance with the terms of
coordination agreements between the operators of the Galaxy 17, EutelSat 172A, Estrela
do Sul 2, and Telstar 1 1N space stations and operators of other Ku—band geostationary
space stations within six angular degrees of those space stations. In the event that another
GSO FSS space station commences operation in the 14.0—14.5 GHz band at a location
within six degrees of any of these space stations, aircraft earth stations operating pursuant
to this temporary authority shall cease transmitting to that space station unless and until
such operation has been coordinated with the new space station‘s operator or Panasonic
demonstrates that such operation will not cause harmful interference to the new co—
frequency space station.




                                                                                                2 f4/


9. Communications between Panasonic‘s aircraft earth stations and the Estrela do Sul 2
space station must be in compliance with all existing and future space station
coordination agreements reached between Brazil and other administrations.

10. Panasonic‘s aircraft earth stations must employ a tracking algorithm that is resistant
to capturing and tracking adjacent satellite signals, and each station must be capable of
inhibiting its own transmission in the event it detects unintended satellite tracking.

11. Panasonic‘s aircraft earth stations must be monitored and controlled by a ground—
based network control and monitoring center. Such stations must be able to receive
"enable transmission" and "disable transmission" commands from the network control
center and must cease transmission immediately after receiving a "parameter change"
command until receiving an "enable transmission" command from the network control
center. The network control center must monitor operation of each aircraft earth station
to determine if it is malfunctioning, and each aircraft earth station must self—monitor and
automatically cease transmission on detecting an operational fault that could cause
harmful interference to a fixed satellite service network.

12. Panasonic must take all necessary measures to ensure that the operation authorized
herein does not create potential exposure of humans to radiofrequency radiation in excess
of the FCC exposure limits defined in 47 CFR 1.1307(b) and 1.1310. Measures must be
taken to ensure compliance with limits for both occupational/controlled exposure and for
general population/uncontrolled exposure, as defined in these rule sections.
Requirements for restrictions can be determined by predictions based on calculations,
modeling or by field measurements. The FCC‘s OET Bulletin 65 (available on—line at
ww.fee.gov/oet/rfsafety) provides information on predicting exposure levels and on
methods for ensuring compliance, including the use of warning and alerting signs and
protective equipment for workers.

13. Panasonic must maintain a point of contact available 24 hours per day, seven days
per week, with the authority and ability to terminate operations authorized herein, for
discussing interference concerns with other licensees and U.S. Government agencies, and
must submit a letter to be included in its license file with the name and telephone number
of the point of contact prior to commencing operation.

14. Stations authorized herein must not be used for air traffic control communications.

15. In connection with the provision of service in any particular country, Panasonic is
obliged to comply with the applicable laws, regulations, rules, and licensing procedures
of that country.

16. Grant of this authorization is without prejudice to any determination that the
Commission may make regarding pending applications. E.g. IBFS File No. SES—MFS—
20120913—00818.


17. Any action taken or expense incurred as a result of operations pursuant to this special
temporary authority is solely at Panasonic‘s risk.
18. Panasonic is afforded thirty days from the date of action to decline this temporary
authorization as conditioned. Failure to respond within this period will constitute formal
acceptance of the authorization as conditioned.
19. This action is issued pursuant to Section 0.261 of the Commission‘s rules on
delegated authority, 47 C.F.R. § 0.261, and is effective immediately. Petitions for
reconsideration under Section 1.106 or applications for review under Section 1.115 of the
Commission‘s rules, 47 C.F.R. §§ 1.106, 1.115, may be filed within 30 days of the date of
the public notice indicating that this action was taken.




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2. Contact


             Name:          Carlos M. Nalda                       Phone Number:                      202—626—6659
             Company:       Squire Sanders (US) LLP               Fax Number:
             Street:        1200 19th Street NW                   E—Mail:                            Carlos.Nalda@squiresanders.com

                            Suite 300
             City:          Washingon                             State:                              DC
             Country:      USA                                  Zipcode:                             20036      —
             Attention:    Carlos Nalda                         Relationship:                         Legal Counsel


(If your application is related to an application filed with the Commission, enter either the file number or the IB Submission ID of the related
application. Please enter only one.)
 3. Reference File Number or Submission ID

 4a. Is a fee submitted with this application?
@ IfYes, complete and attach FCC Form 159.         If No, indicate reason for fee exemption (see 47 C.F.R.Section 1.1114).
C Governmental Entity        (a) Noncommercial educational licensee
3 Other(please explain):

4b. Fee Classification    CGB — Mobile Satellite Earth Stations

5. Type Request

y Use Prior to Grant                              qy Change Station Location                        C Other



6. Requested Use Prior Date
       10/01/2012


7. City                                                                     8. Latitude
                                                                           (dd mm ss.s h)     0   0   0.0

9. State                                                                   10. Longitude
                                                                           (dd mm ss.s h)     0   0   0.0

11. Please supply any need attachments.
Attachment 1: Narrative Statement                 Attachment 2: Specs and Tech Appen                  Attachment 3: Coordination


12. Description.   (If the complete description does not appear in this box, please go to the end of the form to view it in its entirety.)
    Panasonic application for interim operation of Aura LE terminal and to correct number of
    MELCO terminals




13. By checking Yes, the undersigned certifies that neither applicant nor any other party to the application is           @ Yes          C No
subject to a denial of Federal benefits that includes FCC benefits pursuant to Section 5301 of the Anti—Drug Act
of 1988, 21 U.S.C. Section 862, because of a conviction for possession or distribution of a controlled substance.
See 47 CFR 1.2002(b) for the meaning of &quot;party to the application&quot; for these purposes.


14. Name of Person Signing                                                 15. Title of Person Signing
  Mark DeFazio                                                                Manager, GCS Regulatory and Business Operations
           WILLFUL FALSE STATEMENTS MADE ON THIS FORM ARE PUNISHABLE BY FINE AND / OR IMPRISONMENT
                  (U.S. Code, Title 18, Section 1001), AND/OR REVOCATION OF ANY STATION AUTHORIZATION
                   (U.S. Code, Title 47, Section 312(a)(1)), AND/OR FORFEITURE (U.S. Code, Title 47, Section 503).


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THE FOREGOING NOTICE IS REQUIRED BY THE PAPERWORK REDUCTION ACT OF 1995, PUBLIC LaAW 104—13, OCTOBER
1, 1995, 44 U.S.C. SECTION 3507.


     ATTACHMENT 3




COORDINATION INFORMATION


     L                                                                                                   December 16, 2009
    19 |NTELSAT
                        Federal Communications Commission
                        International Bureau
*                       445 12th Street, S.W.
                        Washington, D.C. 20554


                        To Whom It May Concern:

                        This letter certifies that Intelsat is aware that Panasonic Avionics Corporation
                        ("PAC") is seeking FCC authorization to access Gelaxy 17 at 91° WL, as an
                        authorized point of communication, for its eXConnect Ku—band acronautical
                        mobile—satelliteservice (""AMSS") system using transmit/receive antcnnas that are
                        not strictly compliant with the FCC‘s antenna gain requirements.‘ Howsve.r, as
                        described below; the terminals comply with the FCC‘s two—degree spacing rules by
                        maintaining offaxis BIRP spectral density levels below those set forth in
                        analogous Ku—band earth stanons onboard vessels ("ESY") and vehicle—mounted
                        earthstations ("VMES") rules:*

                        Intelsat understends that PAC plansto operate two AMSS antenna types: (i) the
                        MELCO aritennas previously operated with the Connexion by Boeing system; and
                        {ii) the Aura LE antenna designed specifically for the eKConnect system and
                       manufactured by EMS Technologiss            The MELCO antenna is a
                       mechanically—steered Cassegrain antenna with an elliptical profile that was
                       previously examined by the FCC and authorized for AMSS operations in
                       experimental Call Siga WC2XVE (File No. O0O2—EX—PL—2004) and commercial
                       blanket licensé Call Sign E000723 (File No. SES—MOD—20030512—00639). The
                       Aura LE antepns is a mechamcally steered, flat—plate AEBS with two
                       transmit/receive apertures that is similarly desgigned to meet the technical
                       requirements imposed on U.S. and international AMSS opcratzons The basic

         ! See 47 CFR §25.209.
         *See 47 CFR §25.222.
         ‘ The Aura LB antenna‘s two transmit/receive apertures are coherently combined to form a single
         bearn. Af very lowelevation angles, only the front aperture is used due to blockage. This allows
         the antenna to maintain high performance over a largerange ofelevation angles between 5 degrecs
         and 90 degrees while maintaining a low profile for aerodynamicintegration with an aircraft.

                            Intelsat Corporation                                                                         Page 1 of
                                                                                                                                 4
                            3400 International Ore NW, Washington DC 20008—3006.U5A wruwintaisat.com T41 207—944—6800 F +1 202—944—7898


                characteristics of the MELCO and Aura LE antenzna are also summmarized in Table
                1.

                               Table 1. Aura LE and MELCO Antenra Characteristics
    ____ Characteristic                      EMS Aura LE                               MELCO Reflector
    Frequency                       Tx: 14.0 Hazto 14.5 GHz.                    Tx: 14.0 GHz to 14.4 GHz
                                    Rx: 10.7 GHz to 12.75 GHz,                  Rx: 11.2 GHz to 12.8 GHz
   TELSAT.                          (11.7—12.2 GHz in theU.S.)____|             (11.7—12.2 GHz in the U.S)
    Aperture Size                   2 Apertures of35" X §" each 25.6" X7.7"
    EIRP                            42.5 dBW @.5 deg Elevation  47.2 dBW
                                    48.0dBW @ 90 deg Elevation            .
    G/T                             11 dB/K @ 5 deg Elevation   £.0 dB/KX @ 11.2 to 11.7GHz
                                    14 dB/K @90 deg Elevation   9.3 dB/K @11.9 to 12.8GHz
    Tracking Rate                   40 deg/sec in Azimuth                      40 deg/sec in Azimuth
                                    25 deg/sec in Elevation                    25 deg/sec in Elevation
  | Az Pointing Aceuricy           06.2 deg 1—sigma                             0.25 deg 1—sigma

                BoththeMELCO and AuraLB antennas are designed to maintainpointing towards _
                the intended satellite through the full range of mancsuvers carried out by
                commercial aircraft, The antennas are pointed basedon aireraft position and
               attitude information obtained from the ARINC 429 data bus, which is standard on
               commercial atroraft. This information is augmented with higher rated data from an
               inertial sensor package that is integrated with the antenna and compensates for INS
              ‘errors that result from latency and bending ofthe airframe between the aircraft INS
              unit and the antenna. The pointing accuracy of the MELCO reflector is 0.25 deg
               l—sigma and the pointing accuracy of the EMS Axira LE antenua will be less than
               0.2 deg l—sigma. Pointing error will be continuously monitored and if it ever
              excs,eds 0.5 degrees, then transmissions will be automatically inhibited within 100
              ms.

              The FCC‘s off axis EIRP spectral density limits for anilogous ESV and VMES
              operations aredefined by Sections 25.222(a)(1} and 25.226(a)(1)(1). The effective
              off—axis EIRP spectral density generated by a conforming terminal will be:

                        15~25log10 (® + 0.2}                    dBWAkHz for                      1.5°<05<7°
                        —6                                      dBW/AkHz for                     7°<0<9.2°
                        18—25l0g10(B® + 0.2)                     dBWAMAkHz           for       9.2%°<@4$48°
                        —24                                     dBW/AkHz             for       48°<@<85°
                        —14                                     dBW/AkHz             for       §5°<@<180°

              where ® is the angle in degrees from the line connecting the focal point ofthe
              antenna to the orbital location of the target satellite.



* See 47 CBR. § 25.222(a)(7) (Ku—band ESVs) and § 25.226(b)(1)(iv)(B)(Ku—band VMESs)}.

                     Intesat Corporation                                                                         }3   e 2 of 4
                     3400Intergtiona) Orive NW, Washington DC 20008—3006 USA wewe.intefsat.enin T+1 202:944—5800 F+] 2025447258


                        The eXConnect system will limit off—axis EIRP spectral density tono more than
                        this level through varfous means, including: (i) limiting transmit power spectral
                        density by controlling the trapsrait power of the temminal and by selecting
             appropriaté carrier bandwidths; (i#) controlling the off—axis gain of the antenna
             along the GSO by inhibiting transmissions when the skew angle exceeds a
    i        specified threshold and(#it) controlling pointing error and inhibiting transmissions
    @ INTELSATY» the pointingoffset exceeds a threshold of 0.5 deg. The specific transmit
                   ~    power, bandwidth and skew angle thresholds will be selected based on the desired
                        terminal transmissionrates, coverage area, and satellite performance.

                        Based on the foregoing factors, the MELCO antenna will operate at a maximum
                       input power density at the antenna waveguide flange of —21.6 dBW /4 kHz,
                       eniploying BPSK modulation; and the AnraLE antenna will opgrate at a maximum
                       input power density at the antenna waveguide flange of —15.1 dBW /kHz,
                       employing RPSK modulation. Even in the rare cireummstance when transmitting at
                       pointing offsets equivalent to their design tolerances, these antenna terminals are
                       compliant with the off—axis EIRP density.level requirements specified in Sections
                       §25.222 and §25.226, or the combined effect of §25.209 and §25.212(c) of the
                       Commission‘s Rules, at all off—axis angles up to and including 6 degrees off—axis
                       angle. PAC‘s conservative sapproach of including antemna pointing offsets in
                       selectingthe maximumpower levels defined above ensures that the. operation of
                       , these antennas; with the associated off—axis EIRP density envelope, will not cause
                         unacceptableinterference into adjacent satellites.
                       The undersigned firther certifies that the maximurs downlink satellite EIRP
                       density of13.0 dBW/4KHz, operstional level of the Ku—band AMSS network
                       operated by PAC, is routinely used at 2—degree spacing without causing
                       unacceptable interference to adjacent satellite operators.

                       Furthermore, in order to prevent unacceptable interference futo adjacent satellites,
                       Horizons and PAC acknowledgethat the antennas will be instalied in compliance
                       with the technical, operational and performance requirements ofPart 25 ofthe FCC.
                       Rules and any requirements set forth in the licenses granted by the FCC for the
                       above AMSS antenna system.

                       Horizons and PAC confitm that the use of the above antennas will not cause
                       unacceptable interference into adjacent satellites in accordance with the FCC‘s—
                       two—degree spacing policy and accept that theseantennaswill not require more
                       protection from adjacent satellites compared to an earth station employing an
                       anterna conforraing to the FCC antennaperformance standards defined in Section
                       25.209 of the FCC rules. If the use of this sntenna should cause unacceptable
                       intferference into other system$, PAC has agreed that it will terminate transmission
                       immediately upon notice from the affected parties.


|
                            Intesat Corporation                                                                        Page.3 of 4
                            3400inmarnational Drive NW, Washington DC 20008—3006 USA wwwintelsaucom T+1 202—944—5800 Fai   202—944—7898


                  Sincerely,



                  es &lmquzgggg                                                     . 16 decoubo. 00
{.@
g@ INTELSAT:Seni’or Director, Spectrum Engineering
                  Intelsat




                 Acceptance by Panasonic Avionics Corporation:

                  PAC testifies that theinformationprovided to Intelsat and reflected in this affidavit
                  is true and accurate to the best of PAC‘s knowledge.



                     %/%M;Z/fi/                                                             //ZzC Ax:F
                  Paul Sarraffe                                                      Date
                  Panasonic Avionics Corporation
                  eXConnect Systems Engineering


                 Acbeptame by SES Americom:

                 SES Americom agrees to the use of the PAC MELCO and Auta LE antennas with
                 the above:—power density into the antenna flange and the uplink EIRPdensity level
                 as stated in this letter, with respect to SES satellites and the associated satellite
                 networksthat are within +/— 6 degrees orbital spacing from Galaxy 17 at 91° WL.



                 KrishJomxa.lagadda |                           Date
                 Manager, Spectrum Development
                 SES Amsticom




                      Intelsat Corsoration
                      1400 imerrational Orive NW, Washington CC 20008—3005 USA wwewintelsatcom T+1 202—344—6800 Ffl2 -944-7838


                      August 2, 2010
         1


    3 ;g(‘ INTE LSAT-Federal Communications Commission
     '                International Bureau
3                     445 12th Street, S.W.
                      Washington, D.C. 20554

                      To Whom It May Concern:

                      This letter supplements the letter dated December 16, 2009 from Intelsat regarding
                      Panasonic Avionics Corporation‘s ("PAC") proposed Ku—band aeronautical
                      mobile—satellite service ("AMSS") operations with the Galaxy 17 satellite at 91°
                      W.L. Intelsat confirms that so long as PAC maintains FCC authority to
                      communicate with Galaxy 17, Intelsat will include the technical parameters
                      described in the aforementioned letter in all future satellite network coordinations
                      for the satellite.

                      Sincerely,



                     Abupop
                     Nes
                      JosE      Albuquerque                               Date
                                                                                 _2 August 2040t¥
                      for Intelsat



                     Acceptance by Panasonic Avionics Corporation:

                     PAC hereby certifies that it will comply with the all coordination agreements
                     reached by Intelsat for the G—17 satellite.



                         LPoalshwalte                                                     Ainst~>2 200
                      Paul Sarraffe                 ¥                                Date                        *
                      Panasonic Avionics Corporation
                     eXConnect Systems Engineering




                             Intelsat Corporation                                                                            Page | of |
                             3400 international Drive NW, Washington OC 20008—3006 USA wwwiintelsat.com T +1 202—944—6800 F +1 2%2-944-7898



Document Created: 2019-05-04 13:45:32
Document Modified: 2019-05-04 13:45:32

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