AlliedSignal KAP 140 Manuel d'installation

INSTALLATION MANUALKAP 140FLIGHT CONTROL SYSTEMMANUAL NUMBER 006--00991--0006REVISION 6 OCT, 2002

BENDIX/KINGKAP 140Page 1--4Revision 6, Oct 2002CS:00991I06.IDU1.2.1 MODES OF OPERATIONMODE FUNCTION PROVIDEDVertical Speed(VS) Pitch default mode to h

BENDIX/KINGKAP 140Page 1--5Revision 6, Oct 2002CS:00991I06.IDU1.3 TECHNICAL CHARACTERISTICS1.3.1 System Technical Characteristics (In smooth air)Maxim

BENDIX/KINGKAP 140Page 1--6Revision 6, Oct 2002CS:00991I06.IDU1.3.2 System Components Technical CharacteristicsKC 140TSO Compliance: See Appendix APhy

BENDIX/KINGKAP 140Page 1--7Revision 6, Oct 2002CS:00991I06.IDUGlideslope Valid: >180mV for ValidNAV Valid: >180mV for ValidMiddle Marker Sense:

BENDIX/KINGKAP 140Page 1--8Revision 6, Oct 2002CS:00991I06.IDUKS 270/1/2 CTSO Compliance: See Appendix APhysical Dimensions(Nominal):Length: 4.605 in

BENDIX/KINGKAP 140Page 1--9Revision 6, Oct 2002CS:00991I06.IDU1.4 UNIT INSTALLATION1.4.1 Unit Flavors1.4.1.1 KC 140The KC 140 is available in the foll

BENDIX/KINGKAP 140Page 1--10Revision 6, Oct 2002CS:00991I06.IDU1.4.1.3 KM 275The KM 275 is available in the following versions:Part NumberSlip Clutch

BENDIX/KINGKAP 140Page 1--11Revision 6, Oct 2002CS:00991I06.IDU1.4.2.2 KS 270C/271C/272CThe Installation Kit (PN 050--00398--0000) for the KS270C, KS

BENDIX/KINGKAP 140Page 1--12Revision 6, Oct 2002CS:00991I06.IDU1.4.2.4 KCM 100 Configuration Module Installation KitThe KCM 100 Installation Kit (PN 0

BENDIX/KINGKAP 140Page 1--13Revision 6, Oct 2002CS:00991I06.IDU1.4.3 Certification DiskettesInstallation of the KAP 140 Automatic Flight Control Syste

W ARNINGPrior the export of this document, review for export license re-quirement is needed.COPYRIGHT NOTICE. 1998, 2002 Honeywell International Inc.R

BENDIX/KINGKAP 140Page 1--14Revision 6, Oct 2002CS:00991I06.IDU1.5 ACCESSORIES REQUIRED BUT NOT SUPPLIEDSome of the following accessories are required

BENDIX/KINGKAP 140Page 2--1Revision 6, Oct 2002CS:00991I06.IDUSECTION IIINSTALLATION2.1 GENERAL INFORMATIONThis section contains general suggestions a

BENDIX/KINGKAP 140Page 2--2Revision 6, Oct 2002CS:00991I06.IDU2.3.2 KC 140 InstallationThe KC 140 installation will conform to standards designated by

BENDIX/KINGKAP 140Page 2--3Revision 6, Oct 2002CS:00991I06.IDU2.3.3.1.2 RTI Menu OperationThe main menu provides selection of entering diagnostic mode

BENDIX/KINGKAP 140Page 2--4Revision 6, Oct 2002CS:00991I06.IDU2.3.3.1.3 Configuration Procedure1. To configure/install the flight computer, the follow

BENDIX/KINGKAP 140Page 2--5Revision 6, Oct 2002CS:00991I06.IDUA “1” for “Remote Baro” will cause the system to use the baro set input from the altimet

BENDIX/KINGKAP 140Page 2--6Revision 6, Oct 2002CS:00991I06.IDUNOTEFor the roll and pitch axis null adjustments, adjust the pot until 0+.020 volts DC i

BENDIX/KINGKAP 140Page 2--7Revision 6, Oct 2002CS:00991I06.IDUIn a two--axis installation, create a valid Glideslope signal and null the deviation dis

BENDIX/KINGKAP 140Page 2--8Revision 6, Oct 2002CS:00991I06.IDUpress the UP switch without pressing ARM and check for no trim response. Do the same wit

BENDIX/KINGKAP 140Page 2--9Revision 6, Oct 2002CS:00991I06.IDU

BENDIX/KINGKAP 140CS:00991I06.IDURH--1REVISION HISTORYREV DATE CHANGES4 August, 1998 Add unit versions5 March, 2002 Add unit versions --2603, --5403,

BENDIX/KINGKAP 140Page 2--10Revision 6, Oct 2002CS:00991I06.IDUFACE VIEWINPUT=> OUTPUT=<TABLE 2--1 KC 140 CONNECTOR J1401 PIN FUNCTIONSPinI/O De

BENDIX/KINGKAP 140Page 2--11Revision 6, Oct 2002CS:00991I06.IDUPin DescriptionI/O26 > CWS27 > CRS/HDG DATUM REF28 < TXD RS23229 > RXD RS23

BENDIX/KINGKAP 140Page 2--12Revision 6, Oct 2002CS:00991I06.IDUFACE VIEWINPUT=> OUTPUT=<TABLE 2--2 KC 140 CONNECTOR J1402 PIN FUNCTIONSPinsI/O D

BENDIX/KINGKAP 140Page 2--13Revision 6, Oct 2002CS:00991I06.IDUPins DescriptionI/O23 > TRIM SENSE24 < PITCH SERVO CMD REF25 > TRIM ARM26 >

BENDIX/KINGKAP 140Page 2--14Revision 6, Oct 2002CS:00991I06.IDUP270C1ATACH +*B VALID TPC POWER GNDD COMMAND REFE AP DISCONNECTF CLUTCH LOWH +28VJ TRIM

BENDIX/KINGKAP 140Page 2--15Revision 6, Oct 2002CS:00991I06.IDUP271C1ATACH TESTB VALID TPC POWER GNDD COMMAND REFE AP DISCONNECTF CLUTCH LOWH +28VJ SP

BENDIX/KINGKAP 140Page 2 -- 16Revision 6, O c t 2002CS: 00991I 06. I DUTOP VERSION #CLUTCH LO W CO NNECTI O N ( PI N LETTER)065 -- 00180 -- 0400 B065

BENDIX/KINGKAP 140Page 2--17Revision 6, Oct 2002CS:00991I06.IDUFACE VIEWINPUT=> OUTPUT=<PinI/O Description1 > +5VDCIN2 <> GROUND3 >

BENDIX/KINGKAP 140Page 2--18Revision 6, Oct 2002CS:00991I06.IDUBLANK PAGE MARKER (NEW)

BENDIX/KINGKAP 140Page 2--19Revision 6, Oct 2002CS:00991I06.IDUFIGURE 2--1 KC 140 OUTLINE AND INSTALLATION DRAWING(Dwg No 155--06027--0001, Rev 4)(She

BENDIX/KINGKAP 140RH--2

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BENDIX/KINGKAP 140Page 2--21Revision 6, Oct 2002CS:00991I06.IDUFIGURE 2--2 KS 270C, KS271C & KS 272C WITH KM 275 INSTALLATION DRAWING(Dwg No 155--

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BENDIX/KINGKAP 140Page 2--23Revision 6, Oct 2002CS:00991I06.IDUFIGURE 2--3 KS 270C, KS 271C, KS 272C WITH KM 277 INSTALLATION DRAWING(Dwg No 155--0524

BENDIX/KINGKAP 140Page 2--24Revision 6, Oct 2002CS:00991I06.IDUBLANK PAGE MARKER (NEW)

BENDIX/KINGKAP 140Page 2--25Revision 6, Oct 2002CS:00991I06.IDUFIGURE 2--4 KCM 100 INSTALLATION DRAWING(Dwg No 155--06008--0000, Rev 1)(Sheet 1 of 1)

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BENDIX/KINGKAP 140Page 2--27Revision 6, Oct 2002CS:00991I06.IDUFIGURE 2--5 KC 140 INTERCONNECT(Dwg No 155--01679--0000, Rev AC, Sheet 1 of 5)

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BENDIX/KINGKAP 140Page 2--29Revision 6, Oct 2002CS:00991I06.IDUFIGURE 2--5 KC 140 INTERCONNECT(Sheet 2 of 5)

BENDIX/KINGKAP 140iRevision 6, Oct 2002CS:00991I06.IDUSECTION IGENERAL INFORMATIONParagraph Page1.1 KAP 140 FLIGHT CONTROL SYSTEMS 1 -- 1...

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BENDIX/KINGKAP 140Page 2--31Revision 6, Oct 2002CS:00991I06.IDUFIGURE 2--5 KC 140 INTERCONNECT(Sheet 3 of 5)

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BENDIX/KINGKAP 140Page 2--33Revision 6, Oct 2002CS:00991I06.IDUFIGURE 2--5 KC 140 INTERCONNECT(Sheet 4 of 5)

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BENDIX/KINGKAP 140Page 2--35Revision 6, Oct 2002CS:00991I06.IDUFIGURE 2--5 KC 140 INTERCONNECT(Sheet 5 of 5)

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BENDIX/KINGKAP 140Page 2--37Revision 6, Oct 2002CS:00991I06.IDUFIGURE 2--6 KC140 COMPUTER CABLE ASSEMBLY(Dwg No 155--02794--0000/0002, Rev 1)(Sheet 1

BENDIX/KINGKAP 140Page 2--38Revision 6, Oct 2002CS:00991I06.IDUBLANK PAGE MARKER (NEW)

BENDIX/KINGKAP 140Page 2--39Revision 6, Oct 2002CS:00991I06.IDUFIGURE 2--7 CLUTCH ADJUSTMENT(Dwg No 159--08155--5006, Rev 1)(Sheet 1 of 5)

BENDIX/KINGKAP 140iiRevision 6, Oct 2002CS:00991I06.IDULIST OF ILLUSTRATIONSFigure Page2 -- 1 KC 140 OUTLINE AND INSTALLATION DWG 2 -- 19...

BENDIX/KINGKAP 140Page 2--40Revision 6, Oct 2002CS:00991I06.IDUBLANK PAGE MARKER (NEW)

BENDIX/KINGKAP 140Page 2--41Revision 6, Oct 2002CS:00991I06.IDUFIGURE 2--7 CLUTCH ADJUSTMENT(Dwg No 159--08155--5006, Rev 1)(Sheet 2 of 5)

BENDIX/KINGKAP 140Page 2--42Revision 6, Oct 2002CS:00991I06.IDUBLANK PAGE MARKER (NEW)

BENDIX/KINGKAP 140Page 2--43Revision 6, Oct 2002CS:00991I06.IDUFIGURE 2--7 CLUTCH ADJUSTMENT(Dwg No 159--08155--5006, Rev IR)(Sheet 3 of 5)

BENDIX/KINGKAP 140Page 2--44Revision 6, Oct 2002CS:00991I06.IDUBLANK PAGE MARKER (NEW)

BENDIX/KINGKAP 140Page 2--45Revision 6, Oct 2002CS:00991I06.IDUFIGURE 2--7 CLUTCH ADJUSTMENT(Dwg No 159--08155--5006, Rev 1)(Sheet 4 of 5)

BENDIX/KINGKAP 140Page 2--46Revision 6, Oct 2002CS:00991I06.IDUBLANK PAGE MARKER (NEW)

BENDIX/KINGKAP 140Page 2--47Revision 6, Oct 2002CS:00991I06.IDUFIGURE 2--7 CLUTCH ADJUSTMENT(Dwg No 159--08155--5006, Rev IR)(Sheet 5 of 5)

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BENDIX/KINGKAP 140Page 3--1Revision 6, Oct 2002CS:00991I06.IDUSECTION 3.0OPERATION3.1 GENERALRefer to the STC installation manual of the particular ai

BENDIX/KINGKAP 140Page 1--1Revision 6, Oct 2002CS:00991I06.IDUSECTION IGENERAL INFORMATION1.1 KAP 140 FLIGHT CONTROL SYSTEMSThe KAP 140 Flight Control

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BENDIX/KINGKAP 140Page A--1Revision 6, Oct 2002CS:00991I06.IDUTSO APPENDIXRTCA DO--160CENVIRONMENTAL QUALIFICATIONFORMS

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BENDIX/KINGKAP 140Page 1--2Revision 6, Oct 2002CS:00991I06.IDU1.2 EQUIPMENT DESCRIPTIONThe system modes for the KAP 140 Flight Control System is as fo

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BENDIX/KINGKAP 140Page 1--3Revision 6, Oct 2002CS:00991I06.IDUThe KAP 140 Flight Control System for a two axis configuration consists of the following

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