Ex. 1039, p. 86o
`BOEING
`
`w.g.amo_.xm
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`
`ARINC CHARACTERISTIC 741 PART 1 - Page 78
`
`REVISED: March 31, 1994
`
`(1-5 |
`
`-
`NT I-9
`ATTAC
`TYPE A - DIPLEXERJLNA FORM FAC OR FOR PROTECTION OF PS ONLY
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`Ex. 1039, p. 87~
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`_ ARINC CHARTERISTRIC ‘741 PART 1 - Page 79
`
`TYPE B - DIPLEXER/LNA FORM FACTOR FOR PROTECTION OF GPS GLONASS AND TFTS
`
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`

`
`ARINC CHARACTERJSTIC 741 PART 1 - Page 80
`
`REVISED: June 28, 1991
`
`ATTACHIWENT 1-10
`I-IPA FORM FACTOR
`
`I
`
`SIZE 4 or B MCU
`
`#2 Shell Connector
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`BOEING
`BOEING
`Ex. 1039, p. 88
`EX. 1039, p. 88
`
`
`
`
`

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`ATTACHMENT. 1-10A I
`HPA TOP PLUG CONNECTOR LAYOUT
`
`REVISED: December 30, 1994
`ARINC CHARACTERISTIC 741 PART 1 - Page 81
`
` RF COAX
`
`0
`
`FROM RFU MCP1
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`Ex. 1039, p. 89
`EX. 1039__, p. 89
`
`

`
`ARINC CI-IARACTERISTIC 741 PART 1 - Page 82
`
`REVISED: June 28, 1991
`
`
`
`BOEING
`BOHNG
`Ex. 1039, p. 90
`Ex.1039,p.90
`
`ATTACHMENT 1-10B
`HPA MIDDLE PLUG CONNECT R LAYOUT
`
`N
`
`RF COAX
`
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`
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`‘
`
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`
`3
`
`ATTACHMENT 1-10C
`HPA BOTTOM PLUG CONNECTOR LAYOUT
`
`REVISED: June 23,1991
`ARINC CHARACTERISTIC 741 - Part 1 Page 83
`
`Reserved
`+ 28 VDC
`Ground
`
`8
`
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`
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`
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`BOHNG
`Ex. 1039, p. 91
`Ex.1039,p.91
`
`

`
`ARINC CHARACTERISTIC 741 PART 1 - Page 84
`
`REVISED: June 28, 1991
`
`ATTACHMENT I-11A
`HIGH-GAIN ANTENNA FORM FACTOR
`"CONFORMAL-PHASE!) ARRAY ANTENNA 19.55 X 22.36 EICI-IES"
`
` RCRAFTMJUNTING RFC I.500MAX
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`BOEING
`Ex. 1039, p. 92
`EX. 1039, p. 92
`
`
`
` 0OFFUSLACE
`
`

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`’
`
`3
`
`I-IIGI-I-GAIN ANTENNA FORM FACTOR
`"CONFORMAL-PHASED ARRAY ANTENNQ 16 X 32 INCHES"
`
`ATTACHMENT 1-113
`
`REVISED: June 23, 1991
`ARINC CHARACTERISTIC 741 PART 1 - Page ss
`
`'
`
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`BOEIN
`Ex. 1039, p. 93
`EX. 1039, p. 93
`
`

`
`ARINC CI-IARACTERISTIC 741 PART 1 - Page 86
`
`REVISED: June 28, 1991
`
`1-11C
`ATTACHME
`TOP MOUNTED LOW-PROFILE
`SIDE VIE
`
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`
`
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`BOEING
`Ex. 1039, p. 94
`EX. 1039, p. 94
`
`
`
`

`
`1!
`
`ATTACHIVIENT 1-111)
`TOP OUNTED LOW -PROFILE ARRAY -12 dB'Ic
`
`REVISED: June 28, 1991
`ARJNC CHARACTERISTIC 741 PART 1 - Page 87
`
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`BOEING
`Ex. 1039, p. 95
`EX. 1039,-p. 95
`
`
`
`

`
`ARINC CHARACTERISTIC 741 PART 1 - Page 88
`
`REVISED: June 28, 1991
`
`ATTACHMENT 1-11E
`
`CLOSEUP VIEW OF TE COAXIAL INTERFACE
`TOP MOUNTED LOVV-PROFILE AQBAY -l2dBic
`
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`BOEING
`Ex. 1039, p. 96
`EX. 1039, p. 96
`
`

`
`1 I
`
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`
`ATTACHIVIENT 1- IF
`BLADE §§f]Efl1§A HIGH-GA!§] FOOTPRINT
`
`REVISED: June 28, 1991
`ARINC CHARACTERISTIC 741 PART 1 - Page 89
`
`-" - 6 7(O2B)L.E.
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`Ex. 1039, p. 97
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`Ex. 1039, p. 98
`EX. 1039, p. 98
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`REVISED: June 23, 1991
`ARINC CHARACTERISTIC 741 PART 1 - Page 91
`
`ATTACHMENT 1-11G--2
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`Ex. 1039, p. 99
`Ex.1039,p.99
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`
`ARINC CHARACTERISTIC 741 PART 1 - Page 92
`
`REVISED: June 28; 1991
`
`ATTAC
`
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`
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`Ex. 1039, p. 100
`EX. 1039, p. 100
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`
`ARINC CHARACTERISTIC 741 PART 1 - Page 94
`
`REVISED: June 28, 1991
`
`ATTACHIVIENT 1-11G-5
`DOUBLER OUTLINE
`
`PRESSUR
`
`ELE CTRI'C,AL_ up
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`
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`
`BOEING
`BOEING
`Ex. 1039, p. 102
`EX. 1039, p. 102
`
`

`
`REVISED: June 28,1991
`ARINC CHARACTERISTIC 741 PART 1 - Page 95
`
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`Ex. 1039, p. 103
`EX.1039,p.103
`
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`
`ARINC CHARACTERISTIC 741 PART 1 - Page 96
`
`REVISED: June 28, 1991
`
`ATTACHMENT 1-111-I-2
`TAIL FIN INSTALLATION - 747SP
`
`
`
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`BOEING
`Ex. 1039, p. 104
`EX. 1039, p. 104
`
`

`
`1 ’
`
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`
`AT] ACI-IMENT 1-11H-3
`TAIL FIN INSTALLATION - 747-200 AND 300
`
`REVISED: June 28,1991
`ARINC CHARACTERISTIC 741 PART 1 - Page 97
`
` ]
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`Ex. 1039, p. 105
`Ex.1039,p.105
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`

`
`ARINC CHARACTERISTIC 741 PART 1 - Page 98
`
`ATTAC
`
`NT 1-11H-4
`VIEW
`
`REVISED: June 28, 1991
`
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`Ex. 1039, p. 106
`EX. 1039, p. 106
`
`

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`REVISED: June 1,1992
`ARINC CHARACTERISTIC 741 PART 1 — Page 99
`
`ATTACI-IMENT I-11I-1
`HIGH GAIN ANTEEEA FORM FACTOR
`PHASED ARRAY ANTENNA (19.55 X 23.00)
`FAIRING FORM FAQTOR (30.25 X 35.00;
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`Ex. 1039, p. 107
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`
`ARINC CHARACTERISTIC 741 PART 1 - Page 100
`
`REVISED: June 1, 1992
`
`i
`
`ATTACHMENT 1-111-2
`CONNECTOR INTERFACE
`ANTENNA SEAL DETAIL
`
`H-' CONNECT!!! TNC
`SEALEIJ
`
`
`
`PRESSURE
`
`- C0|TRll.'/PDVEI CONNECTOR
`SEALED
`
`LOCAL JIIIILEII
`
`FUSELAGE
`
`3.00
`
`R AIRCRAFT
`
`C-4
`
`BOEING
`BOEING
`Ex. 1039, p. 108
`EX. 1039, p. 108
`
`

`
`1
`
`’
`
`=
`
`ATTACI-IMENT 1-12A
`BEAM STEERING UNIT gggm
`"A-ENNA CONFIGURATIOfl A"
`
`.
`
`‘I
`
`REVISED: June 28, 1991
`ARJNC CHARACTERISTIC 741 PART 1 - Page 101
`
`__1
`
`,
`
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`
`:1
`
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`
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`BOEING
`Ex. 1039, p. 109
`EX. 1039, p. 109
`
`BOEING
`
`H
`
`Ii
`
`H
`
`5
`
`E
`
`L
`
`“
`M
`
`

`
`ARINC CHARACTERISTIC 741 mar 1 - Page 102
`
`REVISED: June 23,1991
`
`AT] ACLEEEII 1-12B
`BEAM STEERING UNIT ]§§l_J[
`"QQIEEQA COEEIGURATION B"
`
`
`
`ANTENNA
`
` DIPLEXER/
`
`
`LNA
`
`'
`
`
`
`D/LNA DIRECTLY CONNECTED
`TO ANTENNA
`
`CONNECTOR , WIRI NG AND
`INTERWORKS CONNECTORS
`AS SPECIFIED BY
`MANUFACTURER
`
`(11.7"X9.84"X3 .25")
`
`
`
`CONNECTOR PER SECTION
`2.3.3.10.1
`
`SDU
`
`ARINC 741 STANDARD
`INTERWIRING
`
`(3-3 | Note: The BSU may be implemented remote from the antenna in a ZMCU Configuration.
`
`BOEING
`BOEING
`Ex. 1039, p. 110
`EX. 1039, p.—1 10
`
`

`
`REVISED: June 1,1992
`ARINC CHARACTERISTIC 741 PART 1 — Page 103
`
`ATTACHDIENT 1-12C
`BEAM STEERING UNIT (Egg)
`
`"CONFIGURATION C"
`
`SIDE MDUNT ANTENNA CDNFIGURATIDN
`
`SIDE MDUNT ANTENNA
`
`
`
`
`DIPLEXER/
`
`LNA
`
`‘
`
`DIPLEXER/LNA DIRECTLY
`CUNNECTED TD ANTENNA
`
`C-4
`
`ARINC 741 STANDARD
`INTERWIRING
`
`SDU
`
`BOEING
`BOEING
`Ex. 1039, p. 111
`EX. 1039, p. 111
`
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`
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`

`
`ARINC CI-IARACTERISTIC 741 PART 1 — Page 104
`
`REVISED: March 31, 1994
`
`ATTACHMENT 1-13
`LOW G IN ANTENNA
`
`C—5
`
`Imago:t
`
`=a-3fln:.‘I
`
`In83.8....
`
`3Sn...
`
`\/fininn.2
`
`
`
`2.8...:..:w2.o
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`
`
`
`
`
`
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`
`
`
`
`
`5....3.12:m_.__§.B.:9=:<$30..
`
`
`
`
`
`BOEING
`THE NEXT PAGE INTENTIONALLY LEFT BLBNKING
`Ex. 1039, p. 112
`EX. 1039, p. 112
`
`
`

`
`AEJNC3CIUURACTTEUETTCIi41lHlRJ'1—Phge105
`
`'
`
`BOHNG
`BOEING
`Ex. 1039, p. 113
`EX.1039,p.113
`
`

`
`ARINC CHARACTERISTIC 741 PART I - Page 106
`
`REVISED: December 30, 1994
`
`ATTACHMENT 2
`TS USED IN THE
`ARINC 429 LABELS AND WORD F0
`AVIATION SATELLITE COMMUNIC TIONS SYSTEM
`
`
`
`-
`I
`BIT
`POSITION
`
`FUNCTION
`
`
`
`
`
`1
`1
`1
`1
`1
`3 3 2 2 2 2 2 2 272 2 2 1,1 1
`1 O 9 8 7 6 5 4 3 2 1 0 9 8 7 6 5 4 3 2
`
`HPA
`BACKOFF
`
`PAD
`
`
`PEAK]
`?Eg
`
`
`1
`0 9
`
`LABEL
`8 7 6 5 4 3 2 1
`
`
`1 O
`1_1 O O O 1
`
`
`RSVD
`
`LABEL 143 (Octal)
`
`SDU Equipment Identifier Code: 041 (HEX)
`
`SIGN/STATUS MATRIX
`
`(Z)
`
`BITS
`31
`
`30
`
` NORMAL OPERATION
`
`FAILURE HARNING
`NO COMPUTED DATA
`FUNCTIONAL TEST
`
`
`
`BITS
`29 - 25
`
`OOOO0
`
`
`
`
`NOMINAL HPA BACKOFF
`
`I
`
`CODING
`
`
`
`
`
`HEIGHT-ON-WHEELS-(NONI.--
`
`BIT
`17
`
`AIRBORNE OR NO
`HON CAPABILITY
`AIRCRAFT ON GROUND
`
`NO BACKOFF
`1 dB BACKOFF
`2 dB BACKOFF
`
` 3 dB BACKOFF
`4 dB BACKOFF
`
`
`
`
`NOTE:
`
`‘Default Value of Bit 17=0.
`
`BACKOFF
`BACKOFF
`BACKOFF
`BACKOFF
`EACKOFF
`BACKOFF
`BACKOFF
`BACKOFF
`BACKOFF
`25 dB BACKOFF
`26 dB BACKOFF
`27 dB BACKOFF
`28 dB BACKOFF
`29 dB BACKOFF
`30 dB BACKOFF
`BACKOFF
`
`D_D.D.D.D.fl.£I.D.fl..
`wwwmmmuuuuua
`
`
`
`
`
`SDI cone
`
`Qi)
`
`
`
`
`
`Ao
`
`ALL CALL
`LGA HPA
`HGA HPA
`UNUSED
`
`
`
`
`
`n
`01
`10
`11
`
`
`
`'
`
`
`
`
`$-51
`
`IHPA CONTROL (BIT 16)
`CARRIERIS) arr
`CARRIER(S) on
`
`(Z)
`
`
`
`
`
`¢—5 1
`
`Figure 1 I-IPA COMMAND WORD - SDU to I-IPA
`
`BOEING
`BOEING
`Ex. 1039, p. 114
`EX. 1039, p. 114
`
`

`
`‘
`
`'
`
`I
`
`I
`
`I
`
`I
`
`1
`
`'
`
`¢.5 ‘
`
`¢_4
`
`¢ 5
`
`¢_4
`
`[C-5
`
`‘:5
`
`¢-4
`
`HPA BACKOFF RANGE @
`*5-"2A
`16 dB BACKDFF
`17 dB BACKOFF
`18 dB BACKUFF
`19 dB BACKUFF
`
`BITS
`10 - 9
`
`00
`01
`10
`1 1
`
`CODING
`
`RESERVED
`LGA HPA
`HGA HPA
`
`HPA TYPE
`
`
`
`
`
`
`1?
`CLASS B
`LINEAR
`
`
`
`
`
`I-IPA CONTROL
`
`(E)
`
`o
`1
`
`%
`
`.
`
`,
`
`CARRlER(S> or:
`CARRIERCSD on
`
`Figure 2 HPA STATUS WORD - I-IPA to SDU
`
`I (I-6
`BOEING
`BOEING
`Ex. 1039, p. 115
`EX. 1039, p. 115
`
`.
`
`‘-
`
`' ’
`
`ATTACHMENT 2 cont’d
`ARINC 42.9 LABELS AND WORD FORMATS USED IN TI-IE
`AVIATION SATELLITE COMMUNICATIONS SYSTEM
`
`REVISED: December 30,1994
`ARINC CHARACTERISTIC 741 PART 1 - Page 107
`
`332222222222111
`10987654321098?
`
`1111
`5432
`
`LABEL
`1
`0937654321
`
`
`
`MAX. AVAIL.
`
`ACT. P. OUT
`
`RMS POUER
`
`HPA
`
`R
`
`BACKOFF
`
`Label 143 (Octal)
`
`HPA Equipment denifier Code: 241 EX)
`
`TYPEI
`CLASS C
`
`TYPE 11
`LINEAR
`
`29-25
`
`29-24
`
`ACTUAL PONER OUT
`
`16.5 dB LESS THAN 40H
`17.0 dB LESS THAN 40H
`
`27.0 dB LESS THAN 40H
`
`AT/BELON MEASURABLE RANGE
`
`
`
`FAILURE NARNING
`
`N0 COMPUTED DATA
`FUNCTIONAL TEST
`NORMAL OPERATION
`
`—
`
`
`
`N11
`0
`
`0
`1
`1
`
`
`
`SIGN/STATUS MATRIX
`
`®
`
`3 dB GREATER THAN 400
`0.5 dB GREATER THAN 40H
`
`40 NATTS
`0.5 dB LESS THAN 40H
`
`1 dB LESS THAN 40H
`1
`
`000110
`000010
`
`000001
`000000
`
`3 dB GREATER THAN 40N
`1.0 dB GREATER THAN 40H
`
`0.5 dB GREATER THAN AON
`40 HATTS
`
`111111
`111110
`
`0.5 dB LESS THAN 40“
`1.0 dB LESS THAN 400
`
`100010
`100001
`
`100000
`
`15.0 as LESS THAN 401.:
`15.5 dB LESS THAN 401.:
`
`16.0 as LESS THAN now
`
`ACT. POWER OUT STATUS (APDS)
`18
`ACTUAL POWER
`HELD POWER
`
`3 as Léss THAN 401.:
`UNUSED 30 dB BACKOFF
`31 dB BACKOFF
`
`J
`:
`
`1
`
`i
`
`A
`
`.1
`
`_1
`
`—
`
`-
`J ._.2
`
`

`
`REPLACEMENT PAGE
`ARINC CHARACTERISTIC ‘[41 PART 1 - Page 108
`
`REVISED: December 8, 1995
`
`ATTACHMENT 2 cont’d
`TS USED IN THE
`ARINC 429 LABEL fly
`RD F0
`ATIO
`TEM
`A
`T
`ATELLITE 0
`
`
`
`
`2222222222111111111
`98765 4321098 7654321
`
`LABEL
`87654321
`
`°°°1°*”
`
`
`
`
`
`G4
`
`LABEL 350 (Octal)
`
`I-IPA Equipment Identifier Code: 241 (Hex)
`
`
`
`SIGN/STATUS MATRIX
`
`(aj)
`
`-
`
`-
`FAILURE unanma
`no COMPUTED DATA
`FUNCTIONAL TEsT
`NORMAL OPERATION
`
`IIJTERNAL POHER SUPPLY
`OUTPUT VSHR
`HPA TEMPERATURE
`RF POHER INPUT
`CONTROL sus INPUT
`INTERNAL RAM
`INTERNAL ROM
`
`DISCRETES
`
`(B) @
`
`VALUES
`
` I I smcune H. (E)
`
`
`
`
`EITS
`V
`10-9
`
`
`
`
`
`_
`¢ 5
`
`on
`01
`10
`11
`
`LEA HPA
`REA HPA
`UNUSED
`
`¢-=5]
`
`Figure 3 I-IPA MAINTENANCE WORD - HLPA. to SDU
`
`BOEING
`BOEING
`Ex. 1039, p. 116
`EX. 1039, p. 116
`
`
`
`
`
`
`FAILURE
`FAILURE
`OVER
`Lou
`mAcT1vE
`FAILURE
`
`
`
`
`
`
`
`ox
`OK
`ox
`ox c>-32 dBm)
`ox
`ox
`OK
`
`
`
`
`
`
`FAI LURE
` RESERVED
`
`

`
`'
`
`1
`
`'
`
`.
`
`I
`
`¢-4
`
`<=~4
`
`T 4'
`~
`
`\
`
`ATTACHMENT 2 §cont’d[
`ARINC 429 LABELS AND WORD FORMATS USED IN THE
`AVIATION SATELLITE COMMUNICATIONS SYSTEM
`
`REVISED: December 30, 1994
`ARINC CI-IARACTERISTIC 741 PART 1 - Page 109
`
`2
`9
`
`2
`8
`
`2
`7
`
`2
`6
`
`2
`5
`
`2
`4
`
`2
`3
`
`2
`2
`
`2
`1
`
`2
`O
`
`1
`9
`
`1
`8
`
`1
`7
`
`1
`6
`
`1
`5
`
`1
`4
`
`1
`3
`
`1
`2
`
`1
`1
`
`1
`O
`
`9
`
`8
`
`7 6
`
`LABEL
`5
`
`4
`
`3
`
`2
`
`1
`
`
`I
`smwsmus MATRIX
`
`LABEL 144 (Octal)
`
`SDU Equipment Identifier Code: 041 (Hex)
`
`FAILURE WARNING
`N0 COMPUTED DATA
`FUNCTIONAL TEST
`NORMAL OPERATION
`
`oxscaenzs
`
`fie)
`
`ANTENNA SYSTEM SELECT
`HPR PRESENT
`
`LGA
`NO
`
`HGA
`YES
`
`sm com:
`
`@
`
`BITS
`10 - 9
`
`00-
`U1
`10
`11
`
`ALL CALL
`PORT/TOP
`STARBOARD
`RESERVED
`
`!!
`
`J
`
`-1
`
`NI
`‘
`
`Figure 4 ACU/BSU CONTROL WORD - SDU to ACUIBSU
`
`-
`
`] ¢-6
`BOEING
`BOEING
`Ex. 1039, p. 117
`EX. 1039, p. 117
`
`

`
`ARINC CHARACTERISTIC 741 PART 1 - Page 110
`
`REVISED: December 30, 1994
`
`ATTACHMENT 2 cont’d
`TS USED IN THE
`ARINC 429 LABELS
`WORD F0
`
`
`TI NAVIAT N ATE LITE OMMUNI Y TEM
`
`3
`1
`
`3
`0
`
`2
`9
`
`2
`8
`
`2
`7
`
`
`
`1
`7
`
`1
`6
`
`1
`5
`
`1
`A
`
`1
`3
`
`1
`2
`
`1
`1
`
`1
`0
`
`9
`
`8
`
`7
`
`6
`
`5
`
`4
`
`3
`
`2
`
`1
`
`LABEL 144 (Octal)
`
`ACU/BSU Equipment Identifier Code: 341 (Hex)
`
`
`
`szen/smrus MATRIX ®
`
` I
`
`FAILURE WARNING
`NO COMPUTED DATA
`
`FUNCTIONAL TEST
`
`
`NORMAL OPERATION
`
`
`
`
`C-2
`
`(2-6 I
`
`DISCRETES
`
`VALUES
`
`
`
`
`
`
`
`STARBOARD
`PORT/TOP
`BSU SELECTED
`18
`
`
`RESERVED
`
`RESERVED
`
`RESERVED
`RESERVED
`
`RESERVED
`
`HGA LNA STATUS
`DISABLED
`ENABLED
`
`RESERVED
`TRACKING MODE
`OPEN
`CLOSED
`
`
`
`
`
`OPERATIONAL STATUS
`
`CODING
`
`DMNIDIRECTIONAL MODE
`ACQUISITION MODE ACTIVE
`ACQUISITION COMPLETE
`CLOSED LOOP TRACKING MODE ACTIVE
`
`ACU
`
`BITS
`15 - 11
`
`BITS
`10 - 9
`
`CODING
`
`00
`O1
`10
`11
`
`RESERVED
`PORT/TOP BSU
`STARBOARD BSU
`
`C-6 [
`
`Figure 5 ACUIBSU STATUS WORD - ACUIBSU to SDU
`
`BOEING
`BOEING
`Ex. 1039, p. 118
`EX. 1039, p. 118
`
`

`
`REVISED: December 30, 1994
`ARJNC CHARACTERISTIC 741 PART 1 - Page 111
`
`ATTACHMENT 2 §cont’d}
`ARINC 429 LABELS AND WORD FORMATS USED IN THE
`AVIATION SATELLITE COMMUNICATIONS SYSTEM
`
`
`
`
`
`-
`
`I
`
`3.
`2
`
`2
`9
`
`2
`8
`
`2
`7
`
`2
`6
`
`2
`5
`
`2
`4
`
`
`2
`2
`2
`3
`2
`1
`
`2
`D
`
`1
`9
`
`1
`8
`
`1
`7
`
`1
`6
`
`1 K1
`5
`4
`
`1’ 1
`3
`2
`
`-1
`1
`
`8
`
`7 6
`
`LABEL
`5
`4
`
`3
`
`2
`
`1
`
`
`
`LABEL 350 (Octal)
`
`ACU/BSU Equipment Identifier Code: 341 (Hex)
`
`(1-4
`
`(1-4
`
`
`
`
`
`
`
`SIGN/STATUS MATRIX
`
`FAILURE WARNING
`ND COMPUTED DATA
`FUNCTIONAL TEST
`NORMAL OPERATION
`
`VALUES
`
`1O
`
`K
`
`FAILED
`INACTIVE
`INACTIVE
`FAILED
`FAILED
`FAILED
`FAILED
`FAILED
`
`FAILED
`
`OVER
`
`DISCRETES
`
`@ ,
`
`RESERVED FOR HGA @
`CROSSTALK INPUT
`CONTROL BUS INPUT
`INTERNAL RAM
`INTERNAL ROM
`INTERNAL POHER SUPPLY
`HIGH POHER RELAY (HPR) STATUS @
`ANY INTERNAL BSU PARAMETER
`RESERVED
`LNA/DIPLEXER
`@
`RESERVED
`ACU/BSU TEMPERATURE
`RESERVED
`
`-1
`_|
`12
`13
`14
`15
`16
`17
`18
`19
`20
`21
`22
`23
`24
`
`
`RESERVED
`
`BITS
`1D - 9
`
`
`
`
`
`DD
`RESERVED
`D1
`PORT/TOP BSU
`
`
`STARBOARD BSU
`10
`ACU
`11
`
`
`Figure 6 ACU/BSU MAINTENANCE WORD - ACUIBSU to SDU
`
`|¢-6
`BOEING
`BOEING
`Ex. 1039, p. 119
`EX. 1039, p. 119
`
`

`
`ARINC CHARACTERISTIC 741 PART 1 -‘Page 112
`
`REVISED: December 30, 1994
`
`AT 1 ACI-INTENT 2 jcont’dL
`ARJNC 422 LABELS AND WORD FORMATS USED IN THE
`AVIATION SATELLITE CO1\dM'UNICATIONS SYSTEM
`
`3
`1
`
`3
`D
`
`2
`9
`
`2
`8
`
`2
`7
`
`@
`2
`2
`6
`5
`
`2
`4
`
`2
`3
`
`2
`2
`
`2
`1
`
`2
`O
`
`1
`9
`
`1
`8
`
`1
`1
`7 6
`
`1
`5
`
`1
`4
`
`1
`3
`
`1
`2
`
`1
`1
`
`1
`0
`
`9
`
`8
`
`7
`
`(M53)
`
`AZIMUTH
`
`(L53)
`
`(MSB)
`
`ELEVATION
`
`(LSB)
`
`D.
`
`1
`
`
`
`LABEL
`5
`4
`
`1
`
`0
`
`6
`
`D
`
`3
`
`1
`
`2
`
`1
`
`1
`
`0
`
`®®®
`
`C-4
`
`LABEL 152 (Octal)
`
`SDU Equipment Identifier Code: 041 (Hex)
`
`SIGN/STATUS MATRIX
`
`NORMAL OPERATION
`
`FAILURE WARNING
`NO COMPUTED DATA
`FUNCTIONAL TEST
`
`c-6 |
`
`Figure 7 OPEN LOOP STEERING WORD - SDU to ACU/BSU
`
`BOEING
`BOEING
`Ex. 1039, p. 120
`EX. 1039, p. 120
`
`

`
`'
`
`'
`
`1
`
`I
`
`'
`
`1
`
`'
`
`I
`
`1
`
`'
`
`I ’
`
`I
`
`REVISED: December 30, 1994
`ARINC CHARACTERISTIC 741 PART 1 - Page 113
`
`ATTACHMENT 2. [cont’d[
`ARINC 429 LABELS AND WORD FORMATS USED IN THE
`AVIATION SATELLITE COMIMUNICATIONS SYSTEM
`
`1
`
`2
`9
`
`2
`8
`
`2
`2
`7 6
`
`2
`5
`
`2
`4
`
`2
`3
`
`2
`2
`
`2
`1
`
`2
`
`1
`9
`
`1
`8
`
`1
`7
`
`1
`6
`
`1
`5
`
`1
`4
`
`1
`3
`
`1
`2
`
`1
`1
`
`1
`0
`
`1
`
`0J
`
`9
`
`8 7 6
`
`5
`
`4
`
`3
`
`2
`
`f§1@E—’-BO
`
`_.1
`
`1
`3
`1
`
`|
`1
`1
`‘
`‘
`
`:1
`
`7
`
`—
`
`1
`_: \_,v
`
`LABEL 153 (Octal)
`
`SDU Equipment Identifier Code: 041 ‘(I-Iex)
`
`FAILURE WARNING
`N0 COMPUTED DATA
`FUNCTIONAL TEST
`NORMAL OPERATION
`
`-
`
`-
`
`¢-4
`
`————
`25
`RESERVED
`26
`CARRIER LOCK SIGNAL
`27
`BIT SYNC SIGNAL
`28
`FRAME SYNC SIGNAL
`29
`RX CARRIER FREQ. STATUS-
`
`UNLOCK
`UNLOCK
`UNSYNC
`FREO. SEARCH
`
`LOCK
`LOCK
`SYNC
`FREQ. FOUND
`
`
`
`BITS
`16 - 9
`
`.
`
`CODING
`
`-
`
`I
`
`00000000
`11111111
`
`
`LOHEST C+N
`HIGHEST c+N
`
`
`
`While the OPEN LOOP STEERING WORD’s SSM contains "No Computed Data" or is absent for 1 second or more,
`the ACU/BSU should operate In Closed_ Loop Mode.
`If the next recelved CLOSED LOOP STEERING WORD’s
`discrete "RX Carrier Fr uenc Status" 15 c1_ea.red _to "SEARCH", the ACU/BSU will set the Operational Status field
`in the ACU/BSU STATU W RD t_o "O_mmdirectu1al" and o&e)r(ate its_I-IGA in Omnidirectional mode.
`It should then
`Exgeeed to follow the s uence outlmed 111 Note 33.
`_If the ‘_
`Ca1;ne_r Frequency Status" dlscrete In the CLOSED
`OP STEERING W0
`1s set to "FOUND" and Bxt Sync 1s aIso 1nd1cateri,_the ACU/BSU W111 set the Oper_at1onal
`Status F1e1d 1n the ACU/BSU Status Wprd to "Closed Loop Trackmg Mode Actwe" and enter that mode, bypassmg the
`sateihte acqu1s1t1on sequence outlmed 1n the commentary accompanymg the ACU/BSU Status Word.
`
`Figure 8 CLOSED LOOP STEERING WORD - SDU to ACU/BSU
`(SIGNAL QUALITY - SDU MULTICONTROL OUTPUT) OPTIONAL WORD FOR TEST PURPOSES
`
`¢_6
`
`BOEING
`BOEING
`Ex. 1039, p. 121
`Ex. 1039, p. 121
`
`

`
`ARINC CI-IARACTERISTIC 741 PART 1 - Page 114
`
`REVISED: December 30, 1994
`
`ATTACHMENT 2. jcont’d|
`ARINC 429 LABELS AND WORD F0
`TS USED IN THE
`AVIATION SATELLITE COMJVIUNICATIONS SYSTEM
`
`The following describes the implementation of the optional GSDB service; if this optional service is
`rovided by the SDU, it shall
`be in accordance with these r uirements. Followingsuccessful receipt, CRC verification and identi cation ofDirect Link Service
`(DLS) GSDB S37 Lone Sign Units (LSUs) from t e P-channel, the SDU shall extract the D2 9-octet GSDB Protocol Data Unit
`(GSDBPDU, octets 2 throu h 10 of S37), discarding the received Message Type and CRC fields. The SDU shall then construct
`a Link Interface Data Unit ( DU) consisting of a Link Service Data Unit (LSDU) plus Link Interface Control Information (LICI).
`The LSDU shall contain the D2 GSDBPDU. The LICI shall include the current log-on GES ID, Satellite ID, Spot Beam ID, and
`a "fla s" field. The ID fields shall be derived from the current Log-On Confirm table (specified in Part 2 Section 4.5.2.4); the
`gpot
`cam ID field shall contain the code "zero" if thedglobal beam is currently being used« rather than a spot beam. The flags
`eld shall specify the current P-channel rate (the P fiel ).
`
`A simple Variant of the ARINC 429 Williamsburg methodology (reference ARINC 429 Attachment 11) shall be used to enable
`a sequence of six Label 374 ARINC 429 words to transmit the GSDB LIDU via the GSDB ort. The Williamsbur Word Type
`field (bits 29-31) is not necessary, and shall be replaced by a Word Sequence Number ( SN) field, which shal
`indicate t e
`relative position of each word within -the sequence of six words (numbered from 0 to 5) to facilitate LDU frame synchronization
`at the receiver. The first five words shall be full data words (each containing five nibbles of data), and the sixth word shall be
`a partial data word (containing one nibble of data). No other aspects of the Williamsbnrg protocol (handshake words, timers, etc.)
`shall be utilized on the GSDB interface.
`
`The six ARINC 429 words shall be transmitted at the physical layer as specified in ARINC 429, including the minimum word
`gap of four bit times between successive words in the six-word sequence.
`
`The SDU shall map the LIDU to the ARINC 429 words as shown. All spare bits shall be set to zero.
`
`Note: Except for the SAL, least significant bits of octets and nibbles are right-justified.
`
`1st Word
`
`2
`
`2
`222
`22
`2
`876543
`
`2
`1
`
`2
`0
`
`
`1
`1
`1
`111
`1111'
`9a7e54321o9a7s54321
`
`
`
`
`
`
`
`
`Bitsl-4 xxxxxxxx [Spare]
`an in
`ass ID
`Flags
`
`
`[P] 00111111
`sin. 37:.
`
`2
`2
`
`2 I
`6
`5
`7
`
`2
`h
`
`
`2.
`2221111
`2
`0
`s7
`5
`1
`9
`6
`3
`
`
`1
`4
`
`1
`2
`
`1
`1
`
`1
`D
`
`9
`
`8
`
`T
`
`6
`
`5
`
`4
`
`3
`
`2
`
`1
`
`1
`3
`
`
`
`S37 Octet No. 2
`
`00xxxxxxOUxx0O111111
`Spot Beam ID
`SAT ID
`SAL 374
`
`
`1
`8
`
`1
`7
`
`1
`6
`
`1
`5
`
`1
`4
`
`1
`3
`
`1
`2
`
`1
`1
`
`1
`0
`
`9
`
`8
`
`7
`
`6
`
`5
`
`4
`
`3
`
`2
`
`1
`
`25
`
`
`
`
`
`2
`8
`
`
`
`
`
`C-6 1
`
`
`
`
`
`
`
`
`
`
`
`2
`2. 2
`4
`3
`2
`
`2
`1
`
`2
`0
`
`1
`9
`
`
`
`Bits 1-4
`337 Octet 5
`
`
`S37 Octet Ho. 4
`
`S3? Octet No. 3
`
`U
`
`0
`
`1
`
`1
`1
`SAL 374
`
`1
`
`1
`
`1
`
`4th Word
`
`2
`6
`
`2
`5
`
`2
`4
`
`2
`3
`
`2
`7
`
`
`
`
`S37 Octet No: 7
`
`
`
`2
`1
`
`2
`2
`
`
`
`2
`0
`
`1
`9
`
`1
`8
`
`1
`1
`7 6
`
`1
`5
`
`1
`4
`
`1
`3
`
`1
`2
`
`1
`1
`
`1
`U
`
`9
`
`S37 Octet No. 6
`
`Bits 5-8
`S37 Octet 5
`
`I
`
`8
`
`0
`
`T
`
`U
`
`K
`6
`
`5
`
`4
`
`1
`
`1
`1
`SAL 374
`
`3
`
`1
`
`2
`
`1
`
`1
`
`1
`
`Figure 9 GSDB WORD SEQUENCE - SDU to SNU
`
`BOEING
`BOEING
`Ex. 1039, p. 122
`EX. 1039,
`122
`
`(3-6 I
`
`(3-6 I
`¢—5 I
`
`es 1
`
`

`
`‘
`
`1 1'
`E
`
`'\
`'
`
`REVISED: December 30, 1994
`ARINC CHARACTERISTIC 74] PART 1 - Page 115
`
`ATTACHIVIENT 2. §cont’dz
`ARINC 429 LABELS AND WORD FORMATS USED IN THE
`AVIATION SATELLITE COMMUNICATIONS SYSTEM
`
`2222
`8765
`
`Bits 1-4
`s37#10
`
`
`
`
`
`6th word
`
`
`
`K
`0
`0
`1
`1
`SAL 374
`
`
`87654321
`
`1 ¢-6
`
`¢-5
`
`I C-6
`
`spare
`
`Spare
`
`S3? # 10
`
`
`
`SAL 374
`
`P Field:
`
`_l_3__1'__1;
`
`fi Q 2
`
`Rate, bgs
`
`O
`0
`0
`0
`1
`1
`1
`1
`
`0
`0
`1
`1
`0
`D
`1
`1
`
`0
`1
`0
`1
`0
`1
`0
`1
`
`Reserved
`600
`1200
`2400
`4800
`10500
`Reserved
`Reserved
`
`Figure 9 GSDB WORD SEQUENCE - SDU to SNU (cont’d)
`
`|¢-e
`BOEING
`BOEING
`Ex. 1039, p. 123
`EX. 1039, p. 123
`
`H.
`21111111111
`
`0987654321098?65ln321
`
`ODOUODDOUOUODUOU B1'ts5-8 00111111
`
`
`
`
`—'I.
`
`_
`
`_
`
`5
`
`1
`_| x’!
`
`

`
`REPLACEMENT PAGE
`
`ARINC CHARACTERISTIC 741 PART 1 - Page 116
`
`REVISED: December 8, 1995
`
`ATTACHIVIENT 2 [cont’g[
`ARINC 429 LABELS AND WORD FORMATS USED IN THE
`AVIATION SATELLITE COMMUNICATIONS SYSTEM
`
`NOTES
`
`field data bits are transmitted Least Significant Bit (LSB) first, and the Most
`Unless otherwise noted,
`Significant Bit is transmitted last.
`
`HPA CONTROL bit 16 is used to turn the HPA on or off for HGA/LGA selection. The carriers off level
`should be as specified in Section 2.2.5.6.
`
`PEAK/AVERAGE CODE 0000 has no explicit operation within the HPA. PEAK!AVERAGE is calculated
`from (2 Vi)’/2 V,” where V, is the relative voltage of the i"‘ carrier.
`It is rounded to the nearest integer for
`reporting. If all carriers have the same power level, this is the same as the number of carriers.
`
`RATE: 5-10 words per" second.
`
`Not used.
`
`‘The I-IPA will initiate its Functional Test following receipt of one or more valid Command words having the
`SSM set to Functional Test. The I-IPA Functional Test will execute until its completion, at which time the
`HPA will automatically return to Normal Operation (even if Functional Test is still being received in the SSM).
`Following such completion of the Functional Test, the HPA will not reinitiate the Functional Test until after
`it receives one or more subsequent Normal Operation commands followed by one or more Functional Test
`commands via the SSM.
`‘The I-IPA will ignore any Command words with the SSM set to No Computed Data
`or Failure Warning.
`
`The HPA shall indicate No Computed Data if no I-IPA Command Word -is received from the SDU for one or
`more seconds. The I-IPA shall indicate Functional Test following initiation, and during execution, of its
`Functional Test, whether commanded by the SDU or by any other means such as power-on or a front panel
`test switch. Upon the completion of Functional Test, the HPA shall indicate Normal Operation if no failures
`were detected, or Failure Warning if one or more failures were detected. Failure Warning shall also be
`indicated at any time outside of Functional Test when a monitored (or otherwise tested) parameter is in its
`failure state. A Failure Warning indication should persist until all conditions and parameters are subsequently
`re-tested by appropriate test and are found to be ’OK’.
`
`Reserved.
`
`Bit 16 shall indicate that the HPA has received the corresponding command from the SDU. Any discrepancy
`between the commanded and actual carrier state may be ascertained by the SDU by examination of the Actual
`Power Out Field.
`'
`
`The actual power output reported by the HPA shall be the highest level measured since the previous report was
`transmitted. Bit 18 shall be set to 0' if, at any time during the reporting interval, the HPA RF input power is
`2 —32 dBm while the BSU is not muting the HPA.
`In this case, the Actual Power Out field will thus reflect
`the (highest) measured value for the reporting interval. Conversely, bit 18 shall be set to 1 if, during the
`entirety of the reporting interval, either or both of the following conditions are true at any given time:
`(A) the
`HPA RF input power is < -32 dBm or (B) the BSU is muting the HPA. In this case, the last reported output
`power shall be held and continue to be reported in the Actual Power Out field. Power cannot be more than
`3 dB above 40 Watts.
`
`‘The HPA shall only report actual output power
`Use of the 16.5 to 27.5 dB less than 40W range is optional.
`down to the level where measurement accuracy is consistent with the required baclc—off setting accuracy as
`specified in Section 2.2.5 (i.e. , 1 0.5 dB down to 16.0 dB below 40W and 1 1 dB for the optional extended
`range). If its Actual Power Out is at or below its limit of measurement accuracy, the HPA should output code
`00100/001000 for “AtlBelow Measurable Range" in this field. In lieu of information to the contrary via the
`Actual Power Out field, the SDU should assume that an HPA not indicating usage of the optional extended
`backoff range has a usable Actual Power Out reporting range down to 16.0 dB less than 40 watts.
`
`The SDI bits should be set to reflect the I-IPA’s application as defined in Note 19 of Attachment 1-4.
`
`The -maximum available RMS power is determined by the Linear I-IPA from the Peal:/Average Input Power
`as well as other data. If the SDU wishes to add a carrier, it should send the PealdAverage ratio for the new
`rather than the current set of carriers.
`
`@ @
`
`@@
`
`('39
`
`¢-4
`
`¢-5 I
`
`¢-4
`
`‘FT‘Chun
`
`¢-4
`
`6.3-7 I
`... |
`¢—7 I
`.4 |
`
`(1-5
`
`@®
`
`(1-4
`
`BOEING
`BOEING
`Ex. 1039, p. 124
`EX. 1039, p. 124
`
`

`
`’
`
`}
`
`ARINC 429 LABELS AND WORD FORNIATS USED IN THE
`AVIATION SATELLITE COMIVIUNICATIONS SYSTEM
`
`ATTACHMENT 2 cont’d
`
`REVISED: December 30, 1994
`ARINC CHARACTERISTIC 741 PART I - Page 117
`
`g
`
`©8653@
`
`(6566
`
`®®@®@©®
`
`A "1" state in bits 12 and/or 13 and/or 14 andfor 15 will not cause the Sign/Status Matrix to indicate a Failure
`Warning.
`
`<>~5
`
`Only applicable to HGAs having self-test capability; all others will always be cleared to "OK".
`
`Reserved.
`
`RATE: 5- 10 words per second (not synchronized to I-IPA commands).
`
`'
`
`¢_4
`
`The SSM should be used as follows:
`
`FUNCTIONAL TEST =
`NORMAL OPERATION =
`FAILURE WARNING =
`
`N0 COMPUTED DATA =
`
`Test in Progress (ignore DISCRETE field, invalid).
`No failures detected in ACU/BSU.
`Fai1ure(s) detected in the ACU/BSU and indicated in DISCRETE field; does
`not include failures in the LNA}Diplexer, HPR, HGA or Control bus input.
`No BSU Control Word or no BSU _Open Loop Steering Word has been
`received from the SDU for one or more seconds.
`
`The ACU/BSU shall indicate Functional Test following initiation, and during execution, of its Functional Test,
`whether commanded by the SDU or by any other means such as power-on or a front panel test switch. Upon
`the completion of Functional Test, the ACUIBSU shall indicate Normal Operation if no failures were detected,
`or Failure Warning if one or more failures were detected. Failure Warning shall also be indicated at any time
`outside of Functional Test when a monitored (or otherwise tested) parameter is in its failure state.
`
`The SDI bits should be set to reflect the ACU/BSU’s application as defined in Note 19 of Attachment 1-4.
`
`The state "Functional Test" in the SSM will command the destination ACU/BSU to conduct a self—test and
`respond with the appropriate data. These data are included in the ACU/BSU MAINTENANCE WORD, which
`is output continuously at the rate specified.
`
`While commanding the Functional Test mode, the SDU will continuously send the CONTROL WORD with
`the SSM set to "Functional Test." The ACU/BSU will continue to perform the self-test until the test is
`completed. The ACUIBSU will then automatically return to normal operation. Functional test will not be re-
`initiated until after receipt of SSM fields containing normal operation followed by functional test.
`
`The states "Failure Warning" and "No Computed Data" are not used and should be ignored.
`
`When the Antenna System Select discrete is cleared to the I./GA state, each ACU/BSU will turn-off the
`associated LNA. The SDU should turn off the associated HPA(s) via the Multi-Control ARINC 429 output
`bus (HPA COMMAND word, bit 16).
`
`ARINC 429 labels 270 through 274 (octal) are reserved on all ACU/BSU ARINC 429 buses for testing and
`cross-talk.
`
`$45
`
`I (I-5
`I ¢-6
`
`I ¢—5
`
`(1-4
`
`Elevation data, bits 9-18, has a range of approximately —t-89.8 to -90 degrees. Bit 18 is used as the sign bit.
`A positive angle is considered upward toward the zenith. Resolution of angle is approximately 0.17 degrees.
`
`Azimuth data, bits 19—29, has a range of approximately +179.8 to -180 degrees. Bit 29 is used as the sign
`bit. A positive angle is considered right of the nose reference. Resolution of the angle is approximately 0.17
`degrees.
`
`Data is encoded in BNR, 2's complement as defined in ARINC 429; with the exception of Note 24 above.
`
`The ACU/BSU should operate in the Closed Loop mode when the SDU Open Loop Steering Word is either
`not received for one second after receipt of the last Open Loop Steering Word or when the SSM of that word
`indicates "No Computed Data."
`
`'
`
`'
`
`'
`
`L;
`
`I
`
`l
`
`BOEING
`BOEING
`Ex. 1039, p. 125
`EX. 1039, p. 125
`
`

`
`ARINC CHARACTERISTIC 741 PART 1 - Page 118
`
`REVISED: December 30, 1994
`
`ATTACHMENT 2 §cont’d[
`ARINC 429 LABELS AND WORD FORMATS USED IN THE
`AVIATION SATELLITE COIVIMUNICATIONS SYSTEM
`
`Least Significant Bit is transmitted first in each data field.
`
`The C+N Data field is defined as the carrier plus noise (C+ N) level as determined by the demodulator and
`is an eight bit BNR field which represents the RSS value of the demodulator, the square root of the sum of
`I’ and Q’ integrated over approximately a 40 ms time period. Note: The SDU will inhibit beam steering
`during this 40 ms period to assure a singlebeam position is observed. Alternatively an optional Signal Quality
`Test