Download
Share
Print this page
  1. Manuals
  2. Brands
  3. Honeywell Manuals
  4. Conference System
  5. THALES MCS-4200
  6. Installation and maintenance manual

Honeywell THALES MCS-4200 Installation And Maintenance Manual

Multi-channel satcom system
Hide thumbs

Advertisement

Quick Links

Download this manual
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
1. Overview
A. General
(1) This section supplies electrical installation procedures, power distribution, and
interconnect diagrams for each component of the MCS system.
2. Equipment and Materials
A. General
(1) None.
3. Electrical Installation Procedure
A. Connector Layout and Contact Arrangement
(1) Each front panel connector of the SDU, HSU, and HPA complies with ARINC
characteristic 615, and is used to interface the LRU with an ARINC 615 portable data
loader for software uploads. Pin callouts are specified in Table 5-1. See the
MECHANICAL INSTALLATION section for specifics regarding connector part
numbers for the ARINC 615 connector for each LRU and the corresponding mating
connector.
(2) Table 5-2 lists the pin arrangements for the RJ--45 jack for the Ethernet Port 1. When
a user terminal is connected to this jack, the rear connectors are disconnected so
only the Ethernet Port 1 communications are available from this interface.
(3) The rear connectors of the SDU, HPA, RFUIA, and HSU comply with ARINC
characteristic 600 as specified in Table 5-3. The ARINC 600 connector layouts and
contact arrangement for the various connector plugs for each LRU of the MCS
system are shown in Figure 5-1 thru Figure 5-11.
(4) Table 5-4 and Table 5-5 list the contact arrangements for the top and middle inserts
for the SDU ARINC 600 connector. Table 5-6 lists the ICAO Block Strapping.
 Honeywell International Inc. Do not copy without express permission of Honeywell.
MCS--4200/7200 Multi--Channel SATCOM System
SECTION 5
ELECTRICAL INSTALLATION
23- -20- -35
Page 5--1
15 Jul 2006

Advertisement

loading

Related Manuals for Honeywell THALES MCS-4200

Summary of Contents for Honeywell THALES MCS-4200

  • Page 1: Section 5 Electrical Installation

    (4) Table 5-4 and Table 5-5 list the contact arrangements for the top and middle inserts for the SDU ARINC 600 connector. Table 5-6 lists the ICAO Block Strapping. Page 5--1 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 2 RJ--45 from User (+) TX -- RJ--45 from User (--) RX + RJ--45 to User (+) RX -- RJ--45 to User (--) Page 5--2 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 3 • Type 08 Top Insert • Type 05 Middle Insert • Type 04 Bottom Insert • Index Pin Code 03 Page 5--3 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 4 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System Figure 5-1. SDU ARINC 600 Connector Layout Page 5--4 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 5 (RS232 (RS232 (RS232 POS_MON NEG_MON COMMON) RX- -SDU) TX- -SDU) RX- -SDU) TX- -SDU) (CM- -250) 2A (CM- -250) 2B Page 5--5 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 6 BIT NO. 17 BIT NO. 18 BIT NO. 19 NO. 20 BIT NO. 21 BIT NO. 22 BIT NO. 23 COMMON (LSB) Page 5--6 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 7 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System Figure 5-2. Contact Arrangements for Bottom Insert, SDU ARINC 600 Connector Page 5--7 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 8 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System Figure 5-3. HPA ARINC 600 Connector Layout Page 5--8 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 9 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System Figure 5-4. Contact Arrangements for the Top Insert 60 Watt HPA ARINC 600 Connector Page 5--9/5--10 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 10 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System Figure 5-5. Contact Arrangements for Middle Insert, HPA (60 Watt) ARINC 600 Page 5--11/5--12 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 11 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System Figure 5-6. Contact Arrangements for Bottom Insert, HPA (60 Watt) ARINC 600 Connector Page 5--13 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 12 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System Figure 5-7. HS- -720 ARINC 600 Connector Layout Page 5--14 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 13 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System Figure 5-8. Contact Arrangements for Top Insert, HSU ARINC 600 Connector Page 5--15/5--16 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 14 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System Figure 5-9. Contact Arrangements for the Middle Insert, HSU ARINC 600 Connector Page 5--17/5--18 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 15 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System Figure 5-10. Contact Arrangements for the Bottom Insert, HSU ARINC 600 Connector Page 5--19 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 16 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System Figure 5-11. RFUIA ARINC 600 Connector Layout Page 5--20 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 17 100k ohms or greater. (4) Table 5-6 lists ICAO Block Strapping. Page 5--21 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 18 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System Blank Page Page 5--22 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 19 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System Figure 5-12 (Sheet 1). Satellite Data Unit & HSU Interface Diagram Page 5--23/5--24 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 20 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System Figure 5-12 (Sheet 2). Satellite Data Unit & HSU Interface Diagram Page 5--25/5--26 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 21 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System Figure 5-12 (Sheet 3). Satellite Data Unit & HSU Interface Diagram Page 5--27/5--28 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 22 Binary 1 = Open; Binary 0 = Ground. Pins assigned a zero (0) are wired to SDU connector pin MP--K15 (common). Page 5--29 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 23 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System Blank Page Page 5--30 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 24 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System Figure 5-13. CMC Top- -mounted High Gain Antenna (HGA) Interface Diagram Page 5--31/5--32 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 25 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System Figure 5-14. WH- -10 Handset Interface Diagram Page 5--33 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 26 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System Figure 5-15. HF-SAT Transfer Panel Interface Diagram Page 5--34 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 27 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System Figure 5-16. Signal Conditioning Unit Interface Diagram Page 5--35 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 28 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System Blank Page Page 5--36 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 29 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System Figure 5-17. Maintenance Panel Assembly Interface Diagram Page 5--37/5--38 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 30 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System Figure 5-18. HS- -720 Interface Diagram Page 5--39/5--40 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 31 To add Note 3 to incorporate SBB operation data to Figure 5-19. Replace Figure 5-19 with the new illustration as follows: Figure 5-19. HS-720 Forward ID & Configuration Pins Page 40 of 53 23-20-35 28 Sep 2009 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 32 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System Figure 5-19. HS- -720 Forward ID & Configuration Pins Page 5--41/5--42 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 33 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System Figure 5-20. Tecom Top- -Mount High Gain Antenna Interface Diagram Page 5--43/5--44 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 34 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System Figure 5-21. Thales Mechanically Steered High Gain Antenna Interface Diagram Page 5--45/5--46 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 35 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System Figure 5-22. EMS AMT- -50 Mechanically Steered High Gain Antenna Interface Diagram Page 5--47/5--48 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 36 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System Figure 5-23. Dassault Conformal High Gain Antenna Interface Diagram Page 5--49/5--50 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 37 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System Figure 5-24. Ball Conformal High Gain Antenna Interface Diagram Page 5--51/5--52 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 38 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System Figure 5-25. Low Gain Antenna Interface Diagram Page 5--53/5--54 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 39 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System Figure 5-26. Toyocom Top- -mounted High Gain Antenna Interface Diagram Page 5--55/5--56 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 41 TP11J HPA ANTENNA SUBSYSTEM CONFIGURATION AND GNSS FREQUENCY CHECK ALGORITHM TP11K HPA ANTENNA SUBSYSTEM CONFIGURATION AND GNSS FREQUENCY CHECK ALGORITHM Page 41 of 53 23-20-35 28 Sep 2009 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 42 HPR/HPA/BSU/LGA CONFIGURATION TP11H HPR/HPA/BSU/LGA CONFIGURATION TP11J HPR/HPA/BSU/LGA CONFIGURATION TP11K HPR/HPA/BSU/LGA CONFIGURATION TP12A CFDS TYPE TP12B CFDS TYPE TP12C CFDS TYPE Page 5--57 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 43 B. Availability of ARINC 429 ICAO ADDRESS (AES ID) from 429 Ports (1) The interpretation of this configuration pin is given in Table 5-8. Page 5--58 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 44 This requirement is intended to effectively pair the label 214/275 and 216/276 transmissions. Page 5--59 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 45 Table 5-10. ARINC 429 Speed to/from CMU No. 1 and CMU No. 2 TP10 Pin D Interpretation LOW SPEED ARINC 429 DATA BUS HIGH SPEED ARINC 429 DATA BUS Page 5--60 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 46 HSU input bus when this strap is in the zero state. The SDU assumes, for functional purposes, the presence of the HSU from the state of this strap. Page 5--61 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 47 An invalid state of the parity pin is logged/reported/indicated; the states of the other configuration pins are used as read despite the parity error. Page 5--62 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 48 ARINC 429 source. The SDU can assume (for functional purposes) the presence of the IRS connections from the state of these pins. Page 5--63 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 49 Note 2 NOTES: Not defined at this time. Other configurations are possible and can be added at a later date. Page 5--64 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 50 Frequency Check Not Required” are identical except for TP11J. Refer to ARINC 741 Part 2 Section 3.5.4.1.1 regarding the frequency check for GNSS interference prevention. Page 42 of 53 23-20-35 28 Sep 2009 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 52 MP4C/MP4D CFDS interface input bus if the configuration pins indicate the CMC/CFDS is supposed to be installed. Page 5--65 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 53 SDI fields. In a single MCS system installation, the status of this configuration pin is ignored. Page 5--66 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 54 MCDU/WSC NO. 1 NOT INSTALLED Table 5-26. MCDU/WSC No. 2 TP12 Pin K Interpretation MCDU/WSC NO. 2 INSTALLED MCDU/WSC NO. 2 NOT INSTALLED Page 5--67 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 55 4 calls be initiated from the cockpit and lets ground-to-air calls be routed to the cockpit based upon ORT item xiii. Page 5--68 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 56 The light remains on (steady) for the duration of the call after the acknowledgement of the annunciation for either the steady or flashing light option. Page 5--69 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 57 Table 5-33. Cockpit Hookswitch Signaling Method TP13 Pin K Interpretation SWITCHED PTT AND/OR SCDU LINE SWITCH(ES) LATCHED AUDIO CONTROL PANEL SATCOM MICROPHONE SWITCH Page 5--70 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 58 (c) This method also allows usage of the mic--on discrete input and switch to initiate calls to preselected numbers. Page 5--71 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 59 ONLY (3) Selecting the EPIC cockpit call discrete signaling mode (MP11F=0) is only required when the SDU is connected to the Honeywell AV--900 audio control panel (ACP). This ACP is typically installed on EPIC equipped aircraft. (4) When MP11F is wired to the zero state, the SDU output pins identified in Table 5-36 function as combinational logic to indicate one of the four states shown in Table 5-37.
  • Page 60 (2) This pin is set to the zero or one state to yield an even number of strapped pins (MP11E to MP11K). Page 5--73 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 61 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System Blank Page Page 5--74 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 62 • Reporting failure status in the air and on the ground • Ground test capability for isolating faulty LRUs, performance verification, and system level testing. Figure 6-1. System BITE Communication Page 6--1 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 63 (a) The following are defined as the MCS LRUs (i.e., those manufactured by Honeywell/Thales): • SDU • HPA • HSU. Page 6--2 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 64 • All memory devices (RAM, ROM, etc). (2) All discrete drivers between the SDU and the avionics LRUs have over current protection and open-circuit detection. Page 6--3 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 65 For primary power interrupts greater than 200 milliseconds duration that causes normal operation to cease, the LRU performs a cold start following restoration of primary power. Page 6--4 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 66 (PLO) that derive the dependent clocks can lock onto the OCXO frequency reference. Page 6--5 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 67 • SSM field of the HPA command word sent to the HPA from the SDU • BIT request in HSU command word sent to the HSU from the SDU. Page 6--6 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 68 HPA, and 07 for the LGA HPA). External failures are defined as those failures not having the same level 1 code as the LRU recording the failure. Page 6--7 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 69 LEDs, and through communication to the SDU. (b) HPA Front Panel Indicators and Controls The HPA indicators and controls are given in Table 6-2. Page 6--8 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 70 SSM FW state or the discrete failure bits in the maintenance word, no functional test failures need to be latched until the next functional testing sequence. Page 6--9 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 71 HSU detects only functional test failures (i.e., no CM failures are currently active), the red LED lights for 30 ± 5 seconds and is then turned off. Page 6--10 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 72 CMT. (b) SDU Front Panel Indicators and Controls The SDU indicators and controls are given in Table 6-4. Page 6--11 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 73 LEDs (as appropriate) are turned off if they were exclusively indicating functional test failures with no current CM failures. Page 6--12 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 74 SDU failed OTHER SDU Other SDU (of a dual system) failed HSU failed HPA--HI GAIN High Gain Antenna HPA failed Page 6--13 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 75 Inactive BITE Bus Input to SDU from other LRU: HSU/SDU HSU bus (CFS/CPDF)/SDU Cabin file server/cabin packet data function bus (ACARS MU/CMU)1/SDU No. 1 AFIS/ACARS unit bus Page 6--14 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 76 Control bus to HSU from SDU SDU/WSC1 Bus to WSC1 from SDU SDU/WSC2 Bus to WSC2 from SDU SDU/WSC3 Bus to WSC3 from SDU Page 6--15 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 77 Starboard BSU identification strapped incorrectly HPA--HI GAIN COAX HGA HPA input coax cable HPA--LO GAIN COAX LGA HPA input coax cable Page 6--16 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 78 Because of this approach, it is possible (in this specific case) for an operator to receive two consecutive front panel display messages that are the same. Page 6--17 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 79 ARINC 429 source, as determined by the state of configuration pin TP10A, and a valid ICAO has not been received, the octal and hexadecimal values are replaced with dashes. Page 6--18 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 80 SDU Temperature Following the display of the ORT Identification, the SDU temperature is displayed as shown below: SDU TEMP (--)XXXC Page 6--19 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 81 32 ASCII Characters a--z, A--Z, 0--9 Phone Number 18 ASCII Numerics 0--9 Total On-Time Clock (Hours) 6 ASCII Numerics 0--200,000 Page 6--20 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 82 The LS key/line pair relations are given in Table 6-8. Page 6--21 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 83 The scratchpad is not used for fixed format display purposes. The mechanism used for data entry is described below. Page 6--22 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 84 For compatibility with the Boeing 777 AIMS/CDU, the SDU clears the entire scratchpad when the CLR command is received with the repeat bit set. Page 6--23 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 85 1/1. (f) Special Symbols When displayed, special symbols are defined as given in Table 6-9. Page 6--24 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 86 See Figure 6-3 for example pages. Page 6--25 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 87 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System Blank Page Page 6--26 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 88 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System Figure 6-2. SATCOM SCDU Page Hierarchy Page 6--27/6--28 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 89 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System Figure 6-3 (Sheet 1, Boeing/Corporate). SATCOM SCDU Main Menu Page Page 6--29 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 90 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System Figure 6-3 (Sheet 2, Airbus). SATCOM SCDU Main Menu Page Page 6--30 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 91 • The SDU issues scratchpad message 1 (i.e., NOT ALLOWED) if any LS key is pushed adjacent to a blank or display-only field. Page 6--31 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 92 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System Figure 6-4 (Sheet 1, Boeing/Corporate). SATCOM SUBMENU Page Page 6--32 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 93 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System Figure 6-4 (Sheet 2, Airbus). SATCOM STATUS Page Page 6--33 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 94 5 minutes of the completion of an SCDU-initiated PAST, the page hierarchy is reset to its original structure as shown in Figure 6-2. Page 6--34 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 95 2. Pushing LS key 2l configures the SATCOM system to perform an audio loopback test of flight deck channel 1. Page 6--35 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 96 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System Figure 6-6 (Sheet 1). TEST Page Page 6--36 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 97 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System Figure 6-6 (Sheet 2). TEST Page Page 6--37 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 98 The commands on lines 8 and 9 are displayed only if the configuration straps indicate this channel is wired for headset use. Page 6--38 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 99 Pushing LS key 6L when the asterisk prompt is displayed causes the cockpit voice go-ahead chime to be activated for a single stroke. Page 6--39 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 100 TEST OK is displayed. If there are current failures to report at the conclusion of the PAST (including the POST/PAST results delay period), refer to paragraph 4 for line requirements. Page 6--40 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 101 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System Figure 6-7 (Sheet 1). SATCOM SELF- -TEST Page Page 6--41 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 102 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System Figure 6-7 (Sheet 2). SATCOM SELF- -TEST Page Page 6--42 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 103 Table 6-10. In the figure, digits 0 thru 9 correlate to hexadecimal digits 0 thru 9 in the table. Page 6--43 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 104 (1) This line displays the MIC--1 status of the SDU cockpit voice microphone On discrete input No. 1 as ACTIVE or INACTIVE. Page 6--44 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 105 (1) This line displays the PLACE/END CALL 2 status of the SDU cockpit voice place/end call 2 discrete input as ACTIVE or INACT. Page 6--45 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 106 (1) This line displays C(0) FMC2 CONNECTED or C(1) FMC2 NOT CONNECTED left-justified as determined by the state of system configuration pin TP10C. Page 6--46 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 107 (1) This line displays F(0) HS 429 ICAO ADRS or F(1) LS 429 ICAO ADRS left-justified as determined by the state of system configuration pin TP10F. Page 6--47 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 108 (1) This line displays K(0) LAMP ON CALL INIT or K(1) LAMP ON CALL CONNCT left-justified as determined by the state of system configuration pin TP10K. Figure 6-8 (Sheet 4). Configuration Data Page 6--48 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 109 (1) This line displays D(0) SEC IRS INSTALLED or D(1) SEC IRS NOT INSTLLD left-justified as determined by the state of system configuration pin TP11D. Page 6--49 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 110 Table 6-11) in lines 4 thru 9 (as needed), where an x indicates the message(s) to be displayed based on the state of system configuration pins TP11E, TP11F, TP11G, TP11H, TP11J, and TP11K. Page 6--50 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 111 Textual Messages To Display Based On System Configuration Pin Settings LO GAIN ANT+DLNA HPA--LO GAIN HI GAIN ANT+BSU--T/L HI GAIN ANT+BSU--R HPA--HI GAIN HI POWER RELAY HPA--IGA ERROR/UNDEFINED Page 6--51 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 112 (1) This line displays E(0) OTHER SDU INSTALLED or E(1) OTHER SDU NOT INSTD left-justified as determined by the state of system configuration pin TP12E. Page 6--52 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 113 TP12C Textual Message Textual Messages To Display Based On System Configuration Pin Settings MCDONNELL--DOUGLAS AIRBUS BOEING NOT INSTALLED ERROR/UNDEFINED CAIMS Page 6--53 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 114 (1) This line displays K(0) SCDU2 INSTALLED or K(1) SCDU2 NOT INSTALLED left-justified as determined by the state of system configuration pin TP12K. Page 6--54 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 115 (1) This line displays B(0) LS 429 TO SCDUS or B(1) HS 429 TO SCDUS left-justified as determined by the state of system configuration pin TP13B. Page 6--55 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 116 (1) This line displays E(0) SCDU3 INSTALLED or E(1) SCDU3 NOT INSTALLED left-justified as determined by the state of system configuration pin TP13E. Page 6--56 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 117 9 according to Table 6-15, where an x indicates the message to be displayed based on the state of system configuration pins TP13H and TP13J. Page 6--57 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 118 K(1) HOOK SWITCH IS left-justified and line 12 displays SWITCHED PTT/SCDU beginning in column 6, as determined by the state of system configuration pin TP13K. Page 6--58 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 119 AMS 2 NOT WIRED (Line 8) CABIN 2 WIRED (Line 9) AMS 2 NOT WIRED (Line 8) CABIN 2 NOT WIRED (Line 9) Page 6--59 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 120 (m) CONFIGURATION DATA Page 12 (Figure 6-8, Sheet 12): General Page 12 of the CONFIGURATION DATA page is shown below. Page 6--60 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 121 (1) This line displays the DUAL SYS SELECT status of SDU Dual System Select Discrete Output as ACTIVE or INACT as appropriate. Page 6--61 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 122 Label 143. The ranged allowed for display of the backoff is 0 to 31 dB in increments of 1 dB. Page 6--62 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 123 Line 6 (1) This line displays POWER(WATTS) beginning in column 1. Page 6--63 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 124 0.000 to 80.000 Watts. If the power level is unavailable, dashes are displayed. Page 6--64 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 125 (1) This line displays RETURN> right-justified. Pushing LS key 6L causes the page display to revert to the SAT--N (SATCOM MAINTENANCE) page. Page 6--65 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 126 • READY -- Displayed when a data loader status is READY. • BUSY -- Displayed when a data loader status is BUSY. Page 6--66 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 127 Asterisks are only displayed adjacent to the left LS keys when the data loader status is READY. Figure 6-9 (Sheet 1). DATA LOADER MENU Page 6--67 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 128 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System Figure 6-9 (Sheet 2). DATA LOADER MENU Figure 6-9 (Sheet 3). DATA LOADER MENU Page 6--68 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 129 ORT version upload is attempted and the setting for ORT item liv does not allow it. Page 6--69 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 130 No asterisk is displayed beside the 5L key when the data loader status is either NOT CONNECTED, CONNECTED, BUSY, or ERROR. Page 6--70 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 131 The purpose of this page is to display Class 1 and 2, Level 1 diagnosed, failures reported during the last leg. See Figure 6-10 for example pages. Page 6--71 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 132 10, and 11 are blank. Line 5 displays NO FAULT DETECTED beginning in column 4 if there are no failures to report. Page 6--72 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 133 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System Figure 6-10. LAST LEG REPORT Page Page 6--73 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 134 When there are no failures to report for a given flight leg, nothing is reported for that flight leg (i.e., the flight leg is skipped). Page 6--74 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 135 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System Figure 6-11 (Sheet 1). PREVIOUS LEG REPORT Page Page 6--75 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 136 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System Figure 6-11 (Sheet 2). PREVIOUS LEG REPORT Page Page 6--76 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 137 ORT identification data. See Figure 6-12 for example pages. (b) If a Honeywell/Thales HPA is installed, the associated part/serial number is displayed; otherwise the HPA display entry is removed. The number of LRU IDENTIFICATION pages depends on the number of LRUs to list.
  • Page 138 LRU serial number. Dashes are displayed if no valid data is available. (h) For the Honeywell/Thales MCS system, the two-digit LRU hardware and LRU serial number must be manually entered through the CMT interface for valid data to be available for display.
  • Page 139 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System Figure 6-12 (Sheet 1). LRU IDENTIFICATION Page Page 6--79 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 140 Appendix C) is modified. If the state of the ORT secured partition modified flag is unmodified, the MODIFIED flag is not displayed. Page 6--80 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 141 20. The failure code is displayed as two hexadecimal digits beginning in column 22. Page 6--81 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 142 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System Figure 6-13. TROUBLESHOOTING DATA Page Page 6--82 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 143 The purpose of this page is to display Class 3, Level 1 diagnosed, failures reported during the last leg. See Figure 6-14 for example pages. Page 6--83 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 144 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System Figure 6-14. LAST LEG CLASS 3 FAULTS Page Page 6--84 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 145 11 are blank. If there are no failures to report, lines 6, 7, 9, 10, and 11 are blank. Line 5 displays NO FAULT DETECTED beginning in column 4 if there are no failures to report. Page 6--85 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 146 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System Figure 6-15. GROUND REPORT Page Page 6--86 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 147 SRU failure code is displayed as one hexadecimal digit beginning in column 20. The failure code is displayed as two hexadecimal digits beginning in column 22. Page 6--87 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 148 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System Figure 6-16. GROUND REPORT TROUBLE SHOOTING DATA Page Page 6--88 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 149 12, as appropriate. The DC state is displayed as DC0, DC0’, DC1, DC1’, or DC2 right-justified from column 23. Page 6--89 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 150 CMC at a rate of 1 to 2 Hz, with the SSM bits set to normal operation during reporting of the test results. Page 6--90 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 151 For software package C3.5, the ORT is not partitioned so only a single ORT IDENTIFICATION is supplied for the ORT display lines. Page 6--91 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 152 The LRU serial number is displayed as ssssssss, where ssssssss represents the LRU serial number. Dashes are displayed if no valid data is available. Page 6--92 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 153 (a) As specified, the SDU transmits failure messages and LRU/ORT identification information while operating in the normal mode. The following paragraphs defined the contents of these reports. Page 6--93 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 154 LRUs and their interfaces. The member systems support CAIMS during normal operation and during on--ground maintenance. Page 6--94 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 155 Boeing (refer to Table 6-18). However, no ATA reference numbers are displayed. Page 6--95 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 156 MCDU2 346100 MCDU3 346100 (ACARS MU/CMU)1 232700 23219 (ACARS MU/CMU)2 232700 23219 IRS--PRI 342100 34222 IRS--SEC 342100 34224 RESERVED RESERVED Page 6--96 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 157 Boeing Level I Failure Messages and ATA Reference Numbers Failure SCDU Accessed Maintenance Pages ATA Number Code Message ID 232500 Page 43 of 53 23-20-35 28 Sep 2009 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 159 [HGA] HPA--LO GAIN/SDU 232500 23225 BSU--(TOP/PORT)/SDU 232500 23213 BSU--STBD/SDU 232500 23214 MCDU3/SDU 346100 RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED Page 6--97 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 160 TX PATH VSWR--LO GAIN 232500 23216 [IGA] HPA--HI GAIN/OVER TEMPERATURE 232500 23247 HPA--HI GAIN/OVER TEMPERATURE [HGA] BAD DATA FROM GROUND EARTH STATION None Page 6--98 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 161 SDU OWNER REQS -- USER None [IGA] IN GAIN SUBSYSTEM 232500 HI GAIN SUBSYSTEM [HGA] RESERVED BAD HSU DISABLE DISCRETE 232500 Page 6--99 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 162 232838 DLNA--L(20RV1) [Conformal] 232837 DLNA--R(20RV2) [Conformal] 232837 DLNA--LO GAIN(14RV) 232836 BSU(8RV1) [Top Mount] 232846 BSU--L(15RV1) [Conformal] 232844 BSU--R(15RV2) [Conformal] 232844 Page 6--100 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 163 Airbus Level I (SDU No. 1) Failure Messages and ATA No. Failure SDU/SDU No. 1 – CFDS Normal and Interactive Modes ATA Number Code 232832 Page 44 of 53 23-20-35 28 Sep 2009 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 165 ADIRU2(1FP2) 341234 RESERVED RESERVED RESERVED FMGC1(1CA1) [A320] 228334 FMGEC1(1CA1) [A330/A340] 228334 FMGC2(1CA2) [A320] 228334 FMGEC2(1CA2) [A330/A340] 228334 ARINC 429 ICAO Page 6--101 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 166 MCDU(3CA1)/SDU1(5RV1) [HGA A320] 228212 MCDU2(2CA2)/SDU1(105RV1) [IGA A330/A340] 228212 MCDU2(2CA2)/SDU1(5RV1) [HGA A330/A340] 228212 MCDU2(3CA2)/SDU1(105RV1) IGA A320 228212 MCDU2(3CA2)/SDU1(5RV1) HGA A320 228212 Page 6--102 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 167 [IGA A330/A340] 228212 MCDU3(2CA3)/SDU1(5RV1) [HGA A330/A340] 228212 MCDU3(3CA3)/SDU1(105RV1) [IGA A320] 228212 MCDU3(CA3)/SDU1(5RV1) [HGA A320] 228212 RESERVED RESERVED RESERVED RESERVED RESERVED Page 6--103 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 168 [Conformal] 232834 BSU--L (15RV1) XTALK BUS/BSU--R(15RV2) [Conformal] 232844 SDU1 (5RV1) /HSDU1 (63RV1) 232834 Not applicable for package 6.0 and beyond Page 6--104 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 169 WRG:CONFIG PIN PROG/SDU1(5RV1) [HGA] 232800 OWNER REQS DB HPA--LO GAIN(9RV)/VSWR 232835 HPA(110RV1)/OVER TEMPERATURE [IGA] 232831 HPA--HI GAIN(7RV1)/OVER TEMPERATURE [HGA] 232831 Page 6--105 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 170 232834 SDU1 (105RV1)/TXCOAX [IGA+LGA] 232834 SDU1(5RV1)/TXCOAX [HGA+LGA] 232834 RESERVED SDU1(105RV1)/RXCOAX [IGA] 232834 SDU1(5RV1)/RXCOAX [HGA] 232834 SDU2(5RV1)/RXCOAX 232834 SDU1(105RV1)/RXCOAX [IGA+LGA] 232834 Page 6--106 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 171 HSDU1(63RV1)/RXCOAX 232839 N/A to Airbus MCDU1(2CA1)+MCDU2(2CA2)+MCDU3(2CA3) [RMP only] 228212 INACTIVE WRG:CONFIG PIN PROG/HSDU1(63RV1) 232800 WRG:CONFIG PIN PROG/HSDU1(63RV1) 232800 SDU ORT Page 6--107 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 172 HI GAIN ANTENNA--L(17RV) [Conformal] 232812 HI GAIN ANTENNA--R(18RV) [Conformal] 232812 LO GAIN ANTENNA(13RV) 232811 MCDU1(2CA1) [A330/A340] 228212 MCDU1(3CA1) [A320] 228212 Page 6--108 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 173 Airbus Level I (SDU No. 2) Failure Messages and ATA No. Failure SDU/SDU No. 2 – CFDS Normal and Interactive Modes ATA Number Code 232832 Page 45 of 53 23-20-35 28 Sep 2009 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 175 233000 IFE 429 BUS/SDU2(105RV2) [A330/A340 IGA] IFE 429 BUS/SDU2(105RV2) [A320 IGA] 233000 IFE 429 BUS/SDU2(5RV2) [A320 HGA] HSDU2(63RV2)/SDU2(5RV2) 232839 RESERVED Page 6--109 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 176 232434 ACARS MU2 (1RB2)/SDU2(105RV2) [IGA A330/A340 ACARS] 232434 ACARS MU2/SDU2(5RV2) [HGA A320 ACARS] 232434 ACARS MU2(1RB2)/SDU2(5RV2) [HGA A330/A340 ACARS] 232434 Page 6--110 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 177 228212 MCDU3(3CA3)/SDU2(5RV2) [HGA A320] 228212 RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED SDU1(105RV1)CROSSTALK [IGA] 232834 BUS/SDU2(105RV2) [HGA] 232834 SDU1(5RV1)CROSSTALK BUS/SDU2(5RV2) Page 6--111 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 178 232834 Not applicable for package 6.0 and beyond SDU2(105RV2)/MCDU1(2CA1) [IGA] 228212 SDU2(5RV2)/MCDU1(2CA1) [HGA] 228212 SDU2(105RV2)/MCDU2(2CA2) [IGA] 228212 SDU2(RV2)/MCDU2(2CA2) [HGA] 228212 Page 6--112 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 179 232831 SDU2(105RV2)/BAD DATA FROM GROUND [IGA] 232834 STATION SDU2(5RV2)/BAD DATA FROM GROUND [HGA] 232834 EARTH STATION HPA--LO GAIN(9RV)/OVER TEMPERATURE 232835 Page 6--113 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 180 SDU2(5RV2)/RXCOAX [HGA] 232834 SDU2(105RV2)/RXCOAX LGA+(HGA or IGA) 232834 SDU2(5RV2)/RXCOAX LGA+(HGA or IGA) 232834 LO GAIN ANTENNA(13RV) LOG ON FAILURE 232811 Page 6--114 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 181 WRG:CONFIG PIN PROG/HSDU2(63RV2) 232800 WRG:CONFIG PIN PROG/HSDU2(63RV2) 232800 SDU ORT WRG:FWD ID1 ADDRESS PIN 232800 PROG/HSDU2(63RV2) POWER SUPPLY INTERRUPT 240000 Page 6--115 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 182 MCDU2 232636 MCDU3 232637 (ACARS MU/CMU) 23243C (ACARS MU/CMU)2 (IRS/ADIRU)--PRI 23263E (IRS/ADIRU)--SEC 23263F RESERVED RESERVED RESERVED (FMC/VIA)1 232642 (FMC/VIA)2 232643 Page 6--116 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 183 McDonnell Douglas Level I Failure Messages and ATA Reference Numbers Failure CFDS Normal and Interactive Modes ATA Number Code 232664 Page 46 of 53 23-20-35 28 Sep 2009 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 185 232623 BSU--(TOP/L)/SDU 232626 BSU--R/SDU 232627 MCDU3/SDU 232637 RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED OTHER SDU/THIS SDU 232600 (FMC/VIA)1/SDU 232642 Page 6--117 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 186 HPA--IN GAIN/OVER TEMPERATURE [IGA] 232600 HPA--HI GAIN/OVER TEMPERATURE [HGA] 23262C BAD DATA FROM GROUND EARTH STATION None HPA--LO GAIN/OVER TEMPERATURE 232634 Page 6--118 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 187 SDU OWNER REQS -- USER None IN GAIN SUBSYSTEM [IGA] 232600 HI GAIN SUBSYSTEM [HGA] 232600 RESERVED BAD HSU DISABLE DISCRETE 232664 Page 6--119 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 188 WRG:CONFIG PIN PROG/HSU 232664 WRG:CONFIG PIN PROG/HSU SDU OWNER REQS 232664 WRG:FWD ID PIN PROG/HSU 232664 POWER SUPPLY INTERRUPT None Page 6--120 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 189 SDU. The panel also contains lamps to indicate the status of the MCS system. These lamps are defined in Table 6-22. Page 6--121 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 190 The lamp indicates an HGA failure due to the reduction from normal high speed capability. Page 6--122 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.

  • Page 191: Section 7 Maintenance Practices

    1/2 hour) — Pro--Seal 870B--1/2 NOTES: NOTES: Equivalent alternatives are permitted for materials in this list. The HMN codes in the list of materials identify the Honeywell Material Number (HMN) given to each material. Page 7--1 23- -20- -35 15 Jul 2006...
  • Page 192 A. General (1) The following paragraphs describe general information when removing or installing antennas. NOTE: For all antennas not supplied by Honeywell, removal and installation should be done according to installation instructions from the manufacturer. B. Antenna Weather Protection (1) Some antennas require gaskets and others have O--rings. When reinstalling antennas, new gaskets or O--rings should be used.
  • Page 193 (c) Make sure the index pin coding on the rear connector is correct for the mating connector. Page 7--3 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 194 (1) When the SDU is replaced, the ORT needs to be uploaded before normal operation can begin. Refer to SYSTEM OPERATION, for the ORT uploading procedure. Page 7--4 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 195 FAR 91.413 to be completed every 24 calender months. Recommended periodic scheduled preventative maintenance tests (Tests to determine system condition and/or latent failures): None required. Page 7--5 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 196 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System Blank Page Page 7--6 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 197 • Each set of cable assemblies is assigned a serial number, which is printed on the part number label. Serialization makes sure each cable assembly is traceable and repeatable. Page A--1 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 198 Connector part numbers are: (2) ECS supplies ARINC 600 Size 1 coaxial connectors with the requisite termination kit and assembly instructions (Figure A--2). Page A--2 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 199 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System Figure A- -1. ARINC Connectors Figure A- -2. ARINC Assembly Page A--3 23- -20- -35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 200 G. SATCOM Hardware Component Kits (1) This paragraph contains information on how to select SATCOM hardware component kits offered by ECS for the Honeywell MCS--4200/7200 avionic units in Table A--3 thru Table A--8. ECS supplies several options for each kit to accommodate the variety of mounting requirements specific to each aircraft installation.

This manual is also suitable for:

Thales mcs-7200