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FAU27

Revision : 05 First Issue : JAN 14/2003

25-63-50

© Orolia S.A.S.
REF.: DOC02373G

  Page 1

AUG 12/2013

CS144 INTERFACE MODULE

PART NUMBER

S1825501-01 / S1825501-02

ABBREVIATED COMPONENT MAINTENANCE MANUAL

Description and Operation

TASK 25-63-50-870-801A01

1.

Description and Operation

A.

General

(1)

Purpose

(a)

The purpose of the CS144 Interface module is to combine the aircraft identification with the
aircraft position to generate the appropriate long message.

(b)

The CS144 Interface module is designed to be connected between the ELT and the dongle
(that is part of the wiring to the RCP).

(c)

The  CS144  Interface  module  is  compatible  with  all  3-Frequencies  KANNAD  406  ELTs
except KANNAD 406 AS.
NOTE:  2-Frequencies  KANNAD  ELTs, KANNAD  406  AF-COMPACT, P/N  S1840501-01,
KANNAD  406  AF-COMPACT  (ER),  P/N  S1840501-04  and  INTEGRA  ELTs  families  P/N
S185X501-XX are not compatible with CS144 Interface module.

(d)

Two versions are available:

1

CS144-RS connected to a NAV equipment by RS232, RS422 or RS485 link,

2

CS144-A connected to the NAV equipment of the aircraft via an ARINC 429 link.

(c)

The CS144 Interface module is designed to be mounted on a mounting bracket 1 strap,
P/N S1820511-01.

Summary of Contents for aviation CS144

Page 1: ...e is designed to be connected between the ELT and the dongle that is part of the wiring to the RCP c The CS144 Interface module is compatible with all 3 Frequencies KANNAD 406 ELTs except KANNAD 406 AS NOTE 2 Frequencies KANNAD ELTs KANNAD 406 AF COMPACT P N S1840501 01 KANNAD 406 AF COMPACT ER P N S1840501 04 and INTEGRA ELTs families P N S185X501 XX are not compatible with CS144 Interface module...

Page 2: ...ion Refer to Figure 1 Item Description 1 Housing 2 Red LED 3 J1 Female DIN 12 receptacle 4 ON OFF switch 2 locked positions 5 J2 Male DIN 12 receptacle 6 J3 Male 19 receptacle 7 Name Plate with the following information P N amendment serial number S N qualification manufacturer name code and details 8 Mounting bracket 1 strap not supplied 1 2 3 4 5 6 7 8 ...

Page 3: ... AF COMPACT ER and INTEGRA ELTs families P N S185X501 XX All remote control panels supplied by Orolia S A S RC1xx RC200 RC300 RC400 RC500 RC600 RC800 RC810 Programming dongles Programming dongles A320 and A320 340 Programming dongle ASSY Tested with the following GPS HONEYWELL KLN90 KLN94 GARMIN GNS430 GNS530 TRIMBLE TNL2101 I O Approach Plus CS144 RS NMEA 0183 or ARNAV labels A B CS144 RS ARINC 4...

Page 4: ...y with a high nominal voltage with regards to the clamping voltage of the CR12 protection the CR12 protection LCDA05 must be replaced by a protection with a higher clamping voltage LCDA12 This replacement See TASK 25 63 50 000 801A01 para E and TASK 25 63 50 400 801A01 para C should be performed if this failure occurs or during maintenance The manpower estimated time is 20 minutes Necessary parts ...

Page 5: ...e resistor is less than 10 ohms between a R18 and pin 1 of CR12 85 b R18 and pin 2 of CR12 85 c R22 and pin 3 of CR12 85 d R22 and pin 4 of CR12 85 e the ground of PCB and pin 5 6 7 and 8 of CR12 Figure 1001 25 63 50 991 03 Check of CR12 connections 2 Test of LRU housing closed Refer to Figure 1002 With an ohmmeter check that the resistor is less than 10 ohms between a J1 K RCP ON and J2 K RCP ON ...

Page 6: ...nectors Schematics and Wiring Diagrams TASK 25 63 50 995 801A01 1 Schematics and Wiring Diagrams A General The following abbreviations are used in the tables hereunder I Input O Output N C not connected 1 J1 pin assignment J1 J2 J3 B A M C P N L D R V U K H F G E S T J A K B J L C H M D G F E A K B J L C H M D G F E Note Front view of connectors ...

Page 7: ...ame Destination I O Viewed from back face of mating connector J1 A RCP TEST RESET RCP I J1 B DONGLE Rx DONGLE I J1 C DONGLE Cs DONGLE O J1 D DONGLE SK DONGLE O J1 E DONGLE Tx DONGLE O J1 F DONGLE ALE2P DONGLE O J1 G RCP COMMON RCP O J1 H RCP BUZZER RCP O J1 J RCP LED RCP O J1 K RCP ON RCP I J1 L DONGLE GND DONGLE O J1 M N C A K B J L C H M D G F E ...

Page 8: ... 02 J2 PIN Signal name Destination I O Viewed from back face of mating connector J2 A RCP TEST RESET ELT O J2 B DONGLE Rx ELT O J2 C DONGLE Cs ELT I J2 D DONGLE SK ELT I J2 E DONGLE Tx ELT I J2 F DONGLE ALE2P ELT I J2 G RCP COMMON ELT I J2 H RCP BUZZER ELT I J2 J RCP LED ELT I J2 K RCP ON ELT O J2 L DONGLE GND ELT I J2 M N C A K B J L C H M D G F E ...

Page 9: ...ounded 4 Parity check Without parity strap between J3 P and J3 R With odd parity no strap J3 PIN Signal name Destination I O Viewed from back face of mating connector J3 A RS Tx1 Nav equipment O J3 B RS Tx2 Nav equipment O J3 C RS GND Nav equipment O J3 D PWR GND A C PS I J3 E PROTOCOL GND 1 J3 F J3 F PROTOCOL 1 J3 E J3 G I1 2 Not used I J3 H I2 Not used I J3 J I3 3 Not used I J3 K ARINC Rx1 Posit...

Page 10: ...UIVALENT OR SIMILAR MEMORY CAN RESULT IN MALFUNCTION FALSE MEMORY READING BY ELT ONLY USE MEMORIES SUPPLIED BY OROLIA S A S B Opening the electronic compartment 1 Unscrew the 8 TORX screws 50 of upper lid 40 2 Remove the upper lid 40 3 Discard O ring 90 C Desiccant capsule removal 1 Remove desiccant capsule 100 2 Remove foam wedge 110 D Memory disassembly NOTE To ease its replacement the memory is...

Page 11: ... 06 CR12 removal Cleaning TASK 25 63 50 100 801A01 1 Cleaning A General 1 Clean the housing with absorbent cotton wool C01 soaked in alcohol C02 2 Clean the connectors with a soft brush C03 or a lint free rag C04 If necessary blow them out with low pressure dry compressed air Check TASK 25 63 50 200 801A01 1 Check A General 1 Make sure there is no oxidation on the pins of connectors Dessicant Foam...

Page 12: ... socket Refer to Figure 3001 2 On the I402 board 70 insert the memory 80 onto its socket 3 Fill the memory replacement label 120 with the date of memory replacement and stick it on the identification label 60 as shown Figure 10001 25 63 50 991 09 CS144 Interface module Illustrated Parts C CR12 assembly NOTE Necessary parts to perform this task are included in CR12 replacement kit See TASK 25 63 50...

Page 13: ... 05 Internal View E Closing the electronic compartment Refer to Figure 7002 CAUTION TIGHTENING TORQUE FOR EIGHT TORX SCREWS 50 0 9 0 0 1 NEWTON X METER BEFORE TIGHTENING A SCREW TURN IT COUNTER CLOCKWISE TO FIND THE START OF THE HOUSING THREAD AUDIBLE CLICK 1 Install a new O Ring 90 on the upper lid 40 2 Install the upper lid 40 in the correct assembly direction and install the eight TORX screws 5...

Page 14: ...rnative consumable from other suppliers if the consumable has equivalent properties Table 9002 25 63 50 992 05 List of Consumables NOTE The meanings of the numbers in the USE column are as follows 2 TESTING AND FAULT ISOLATION 3 DISASSEMBLY 4 CLEANING 5 CHECK 6 REPAIR 7 ASSEMBLY DESIGNATION CHARACTERISTICS USE 2 3 4 5 6 7 Dynamometric screwdriver FACOM A 312 or equivalent X TORX bit size 10 Commer...

Page 15: ...oduction 1 The IPL contains a list of components used in the equipment Figure items proceed by Item not illustrated NP Not procurable Items 80 and 120 are only procurable as part of EEPROM replacement kit S1825515 01 see Description and Operation para D Memory replacement Item 85 is only procurable as part of CR12 replacement kit S1825515 02 see Description and Operation para E Upgrade ...

Page 16: ... Sequence Short flash every second Short message available Long flash every second Acquiring position from NAV equipment Series of short flashes Error Permanent ON Idle during 60 sec The internal memory must be replaced every 16000 flight hours or 10 years whichever first Date of last memory replacement Database version when applicable 1610D FAU27 JTSO 2C91a JTSO 2C126 P N AMDT S N KANNAD Z I des ...

Page 17: ...UNIT ELT NAV INTERFACE NP CS144 A 1B 1 20A S1825503 01 CABLE CS144 TO ELT 1 30A 0133910 CAP PROTECTIVE 1 40A 0131948 LID 1 50A 1452K30X14 SCREW SST A2 TORX SELF THR VF9213 0137375 8 60A 0123248 LABEL IDENTIFICATION CS144 RS EES01610 1 60B 0123249 LABEL IDENTIFICATION CS144 A EES01611 1 70A S1825603 01 PC BOARD I402 NP RS 10A 1 70B S1825603 02 PC BOARD I402 NP ARINC 10B 1 80A 0125267 MEMORY CIRCUIT...

Page 18: ...lia S A S Abbreviated Component Maintenance Manual S1825501 01 S1825501 02 Page 18 AUG 12 2013 TASK 25 63 50 500 801A01 1 Storage and Transportation 1 Storage temperature 55 C to 85 C PAGE INTENTIONALLY LEFT BLANK ...

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