Rockwell Collins ADS-B Out ICA Supplement

CESSNA AIRCRAFT COMPANY AIRCRAFT DIVISION WICHITA, KANSAS 67277 Rockwell Collins ADS-B Out ICA Supplement MODEL NO: 560XL SUPPLEMENT NO: ICA-560XL-...
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CESSNA AIRCRAFT COMPANY AIRCRAFT DIVISION WICHITA, KANSAS 67277

Rockwell Collins ADS-B Out ICA Supplement

MODEL NO: 560XL

SUPPLEMENT NO: ICA-560XL-34-00009 SUPPLEMENT DATE: 10/19/2015

© Cessna Aircraft Company Form 2261 Rev 1

CESSNA AIRCRAFT COMPANY AIRCRAFT DIVISION WICHITA, KANSAS 67277 REVISIONS ICA-560XL-34-00009

Rev: -

ICA Summary

Pages 1-6

Manuals Affected

Description

Title

Maintenance Manual

34-00-00 pages 1-4

Navigation - General



Adds the IFR 6000 Flightline Test set.

Maintenance Manual •

Collins TDR-94D Dual Transponder System - Description And Operation

34-53-07 pages 201-205

Collins TDR-94D Dual Transponder System Maintenance Practices

Adds a step to test the ADS-B functions of the transponders

Maintenance Manual •

34-53-07 pages 1-1

Provides a brief description of the ADS-B transponder

Maintenance Manual •

Date: Oct 19/2015

34-53-07 pages 501-504

Collins TDR-94D Dual Transponder System Adjustment/Test

Adds steps to test the ADS-B functions of the transponders

Appendix A: Illustrated Parts Catalog

Not Used

Appendix B: Wiring Diagram Manual

34-53-07 pages 1-4

Appendix C: Maintenance Manual

24-52-01 page 1 Electrical Load Analysis Addition

1.

TDR-94D Dual Transponder System

Export Compliance A.

This publication contains technical data and is subject to U.S. export regulations. This information has been exported from the United States in accordance with export administration regulations. Diversion contrary to U.S. law is prohibited. ECCN: 9E991

2.

Revision Bars A.

3.

Revision bars in this ICA supplement identify new ICAs and/or changes to the current ICAs in the released maintenance manual. • New ICAs that are not in the current maintenance manual will have a revision bar from top to bottom along the left margin. • ICAs that are in the current maintenance manual and have information added, deleted or revised will have a revision bar(s) in the left margin adjacent to the added, deleted or revised information. • New or changed illustrations will have a change bar for the entire length of the page.

Page Numbering A.

The page number system for ICA included in this supplement have three-element numbers that are separated by dashes. The three-element number is found at the bottom right corner of the page, left of the page number. The date is found below the page number.

ICA-560XL-34-00009

© Cessna Aircraft Company

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CESSNA AIRCRAFT COMPANY AIRCRAFT DIVISION WICHITA, KANSAS 67277

B.

When the chapter/system element number is followed with zeros in the section/subsystem and subject/unit element number (28-00-00), the information is applicable to the entire system.

C.

When the section/subsystem element number is followed with zeros in the subject/unit element number (28-21-00), the information is applicable to the subsystems in the system.

D.

The subject/unit element number is used to identify information applicable to units in the subsystems. The subject/unit element number continues in sequence from the number -01- with the number of subsystem units in which maintenance information is necessary.

E.

All system/subsystem/unit (chapter/section/subject) maintenance data is separated into speciied types of information: Description and Operation, Troubleshooting, Maintenance Practices, etc. Blocks of page numbers that are in sequence are used to identify the type of information: (1) Description and Operation or Troubleshooting information may not be included if the procedure is easy. When subtopics are short, they may be put together into the Maintenance Practices section. Maintenance Practices can have a mix of subtopics that includes information to service, remove, install, adjust, test, clean, paint or do approved repairs. (2) Longer procedures that are not as easy to do may be included in a speciied section. Page 1 through 99 - Description and Operation Page 101 through 199 - Troubleshooting Page 201 through 299 - Maintenance Practices Page 301 through 399 - Servicing Page 401 through 499 - Removal/Installation Page 501 through 599 - Adjustment/Test Page 601 through 699 - Inspection/Check Page 701 through 799 - Cleaning/Painting Page 801 through 899 - Approved Repairs

F.

A typical page number:

G.

Illustrations use the same igure numbers as the page block in which they appear. For example, Figure 202 would be the second igure in a Maintenance Practices section.

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CESSNA AIRCRAFT COMPANY AIRCRAFT DIVISION WICHITA, KANSAS 67277 4.

5.

Supplement Revisions A.

Revisions to this supplement may be accomplished if changes to this supplement are required after release of the original issue and prior to incorporation into the manuals listed in the REVISIONS table.

B.

All revisions to this supplement will have changes identiied in detail in the revision block(s) above.

C.

All pages in this ICA supplement will have the same date and are valid as of the date shown.

ICA Incorporation into Applicable Manuals NOTE:

Most ICA supplements will be incorporated in the next available revision to the manuals listed above and should be used in conjunction with those manuals until the next available revision is released.

A.

The ICA Supplement List located in the Introduction section of each manual listed in the REVISIONS table will indicate the incorporation status as of the release date of the published revision.

B.

The manual revision level of the supplement incorporation will be listed in the "Manual Incorporation Status" column in the ICA Supplement List, when those ICAs associated with that manual have been incorporated. After ICAs are incorporated, the manual that they are incorporated in must now be used for those ICAs instead of the supplement. • Based on revision cycle times for the affected manuals, MM ICAs, WDM ICAs, etc. in this supplement may be incorporated in the manuals at different times. • There will not be a revision to this supplement to indicate incorporation in the manuals. Users are required to check the ICA Supplement List for each manual affected to determine incorporation status.

C.

This supplement will be completely superseded by the manuals listed in the REVISIONS table when it has been incorporated in all of the manuals.

ICA-560XL-34-00009

© Cessna Aircraft Company

Page 3 of 6 Oct 19/2015 Form 2261 Rev 1

CESSNA AIRCRAFT COMPANY AIRCRAFT DIVISION WICHITA, KANSAS 67277 INTRODUCTION 1.

Purpose A.

The purpose of this Supplement is to provide the maintenance technician with the information necessary to ensure the correct functionality and performance of the Rockwell Collins ADS-B Out on the Cessna Model 560XL until this information gets incorporated into the next revision to the manuals listed in the "REVISIONS" section of this supplement.

B.

This ICA supplement is designed to satisfy the requirements of 14 CFR 25.1529 "Instructions for Continued Airworthiness" associated with this installation. This document is a supplement to the Model 560XL Maintenance Manual and will be incorporated in the next revision to the manual.

C.

When this information is incorporated in the next revision to the manuals listed in the "REVISIONS" section, those manuals shall take precedence over this supplemental document. Refer to the "ICA Supplement List" in the "Introduction" section of the respective manual for the status of all applicable ICA Supplements.

D.

Revisions to this supplement may occur if there is a change to any of the ICAs in this supplement prior to incorporation into all of the affected manuals. NOTE:

2.

This document must be placed with the aircraft operator's Technical Library CD-ROM or Model 560XL Maintenance Manual and incorporated into the operator's scheduled maintenance program.

Effectivity A.

These Instructions for Continued Airworthiness (ICA) are effective for the following aircraft model and serialization.

Model

Beginning Effectivity

Ending Effectivity

560XL

-006001

and On

3.

Complete ICA Documents A.

4.

The following document(s), in conjunction with this supplement, constitute the Instructions for Continued Airworthiness for the Rockwell Collins ADS-B Out on the Cessna Model 560XL. All items must be available to the operator at initial delivery. (1) Model 560XL Maintenance Manual (2) Model 560XL Wire Diagram Manual

System Components A.

Refer to Appendix A: Illustrated Parts Catalog

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© Cessna Aircraft Company

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CESSNA AIRCRAFT COMPANY AIRCRAFT DIVISION WICHITA, KANSAS 67277 LIST OF INSTRUCTIONS FOR CONTINUED AIRWORTHINESS 1.

Model 560XL Maintenance Manual A.

2.

Chapter 34 - Navigation (1) Refer to 34-00-00 Navigation - General (2) Refer to 34-53-07 Collins TDR-94D Dual Transponder System - Description And Operation (3) Refer to 34-57-07 Collins TDR-94D Dual Transponder System - Maintenance Practices (4) Refer to 34-53-07 Collins TDR-94D Dual Transponder System - Adjustment/Test

Model 560XL Wiring Diagram Manual A.

Chapter 34 - Navigation (1) Refer to Appendix B, 34-53-07 (Sheet 1-4) TDR-94D Dual Transponder System wiring diagram.

ICA-560XL-34-00009

© Cessna Aircraft Company

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CESSNA AIRCRAFT COMPANY AIRCRAFT DIVISION WICHITA, KANSAS 67277 INSPECTION PROGRAM AND AIRWORTHINESS LIMITATIONS 1.

Continuous Inspection Program A.

2.

This ICA Supplement does not affect the current inspection program.

Airworthiness Limitations A.

Cessna Aircraft Company Model 560XL Maintenance Manual, Chapter 4, Airworthiness Limitations, contains the system and airframe limitations for the Model 560XL. NOTE:

(1)

The Airworthiness Limitations section is FAA-approved and speciies maintenance required under Section 43.16 and 91.403 of Title 14 Code of Federal Regulations, unless an alternative program has been FAA approved.

There are no new (or additional) airworthiness limitations associated with this equipment and/or installation.

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CESSNA AIRCRAFT COMPANY

MODEL 560XL

MAINTENANCE MANUAL NAVIGATION - GENERAL 1.

2.

Scope A.

This chapter describes units and components which provide airplane navigational information. This includes pitot static, light director, VOR and other navigational systems and indicators.

B.

Each Model 560XL airplane is delivered with complete Avionics Wiring Diagrams speciically prepared for that serial number airplane. These diagrams, which are to be carried aboard the airplane, must be used in conjunction with this manual when performing maintenance on the airplane.

C.

Technical publications available from the manufacturer of the various components and systems which are not covered in this manual must be utilized as required for maintenance of those components and systems.

Tools and Equipment

Table 1. Equivalent substitutes may be used for the following listed items. NAME

NUMBER

MANUFACTURER

USE

AHRS Leveling Tool Harness

9812101-1

Cessna Aircraft Co. Citation Marketing Div. Department 579 P.O. Box 7706 Wichita, KS 67277

To make the AHRS mounting tray level.

AHRS Tray Leveling Tool Assembly or AHRS Alignment Fixture Assembly

8656553-1 or CJMDL34-005

Cessna Aircraft Co.

To make the AHRS mounting tray level.

Aircraft Leveling Harness

6688018-2

Cessna Aircraft Co.

To make the airplane level.

Aircraft Leveling Tool Assembly

6500900-1

Cessna Aircraft Co.

To make the airplane level.

Air Data Test Set

Model 6300

Laversab Inc.

To test pitot/static system.

Air Data Test Set

Model 6520

Laversab Inc. 10435 Greenbough Suite 300 Stafford, TX 77477

To test pitot/static system.

CA-320A/B Base System (kit)

091-0320-20

Capital Avionics, Inc. 3701 Hartsield Rd. Tallahassee, FL 32303

To calibrate the standby magnetic compass - The kit contains the transmitter, receiver, stand, case, and charger.

CA-320C Wing Mount

071-0105-00

Capital Avionics, Inc.

To calibrate the standby magnetic compass

CA-320 Wind Screen

071-0114-00

Capital Avionics, Inc.

To calibrate the standby magnetic compass

Digital Voltmeter

Model 8100A

John Fluke Mfg. Co. Box 742 Seattle, WA 98133

Electrical circuit maintenance tests.

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Form 2261 Rev 1

CESSNA AIRCRAFT COMPANY

MODEL 560XL

MAINTENANCE MANUAL Table 1. Equivalent substitutes may be used for the following listed items. (continued) NAME

NUMBER

MANUFACTURER

USE

Gyro Tilt Table

CJMD334-101

Cessna Aircraft Co. Citation Marketing Div. Department 579 P.O. Box 7706 Wichita, KS 67277

To mount AHRS units for tilt tests.

Litef Level 1 Maintenance Set

309444-0000 or 309946-0600

LITEF GmbH P/O Box 774 Freiburg Germany 79007

To conigure the LCR-93 AHRS system.

Litef Level 1 Maintenance Set

309946-0000 or 309946-0600

LITEF GmbH P/O Box 774 Freiburg Germany 79007

To conigure the LCR-100 AHRS system.

AHRS Extender Cables

CJMDL34-002

Cessna Aircraft Co.

To mount AHRS units for tilt tests.

Zee Bracket Kit

CJMDL34-001

Cessna Aircraft Co.

To mount AHRS units for tilt tests.

AHRS Test Box

6588025-1

Cessna Aircraft Co.

To test the AHRS system.

AHRS Tilt Table Trays

1243260

LITEF GmbH P/O Box 774 Freiburg Germany 79007

To mount AHRS units for tilt tests.

Navigation Test Set

T30D

Tel-Instrument Corp. 728 Garden Street Carlstadt, NJ 07072

To provide test localizer and glideslope signals for functional test.

Transponder and DME Test Set

ATC-600

Aerolex, Wichita Division 10200 W. York Wichita, KS 67215

To give signals for the DME, transponder functional test.

Transponder Ramp Test Set

ATC-601

Aerolex, Wichita Division

To give test signals for the transponder functional test.

TCAS Test Set

TCAS 201

Aerolex, Wichita Division

To do a test on the Trafic Collision and Avoidance system.

Fuselage Vane Protractor

1939-6

Safe Flight Instrument Corp. 20 New King Street White Plains, NY 10604

Protractor used to calibrate AOA vane.

Display Extraction Tool

CJMD234-10

Cessna Aircraft Company

Removal of Display Units, DU870

Main Gear Simulator Test Box

6688002-1

Cessna Aircraft Company

Simulate airplane air and ground modes of operation for the main gear.

Cessna Aircraft Company

Simulate radio altimeter altitudes.

Cessna Radio Altitude Simulator

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Form 2261 Rev 1

CESSNA AIRCRAFT COMPANY

MODEL 560XL

MAINTENANCE MANUAL Table 1. Equivalent substitutes may be used for the following listed items. (continued) NAME

NUMBER

MANUFACTURER

USE

Static Port Connectors

33410SM125-4

NAVAIDS 2955 Diab Street Montreal, Quebec Canada H4S1M1

Connect test set to static ports.

Pitot Connectors

P86892-4

NAVAIDS Lt. 2955 Diab Street Montreal, Quebec Canada H4S1M1

Connect test set to pitot tubes.

Pitot Tube Adapter

18821-4

NAVAIDS

Connect the air data test set to the pitot tubes.

Altitude Encoder Test Set

2656-G

Barield Instrument Corp. 1478 Central Ave. Atlanta, GA 30344

Display encoder output for altimeter testing

Calibration Test Set

JT-147A

BF Goodrich Avionics Systems Inc. 5353 52nd St. S.E. Grand Rapids, MI 49512

Calibrate the MAG-3000 magnetometer.

Digital Inclinometer

PRO360 or equivalent

Kellstrom

Roll/Pitch Check

Flightline Test Set

IFR 6000 with software 2.08.00 or later

Aerolex, Wichita Division

To do the TCAS functional checks, transponder functional check, automatic dependent surveillance broadcast (ADS-B) functional check, and the distance measuring equipment (DME) system functional check.

WX-PA Portable Analyzer

78-8060-5710-1

L3 Communications Avionics Systems 5353 52nd Street, S.E. Grand Rapids, MI 49512-9704

To test the Stormscope system

WX-PA Antenna

78-8060-5744-0

L3 Communications

To test the Stormscope system

WX-PA Antenna Cable

78-8060-5783-0

L3 Communications

To test the Stormscope system

WX-PA Battery Charger

78-8060-5797-8

L3 Communications

To test the Stormscope system

3.

Deinition A.

This chapter is divided into sections to aid maintenance personnel in locating information. The sections are titled as follows: Flight Environment Data Systems, Attitude and Direction Systems, Landing and Taxiing Aids, Independent Position Determining Systems, Dependent Position Determining Systems, and Flight Management Computing. (1) The Flight Environment Data section describes that portion of the system which senses environmental conditions and uses the data to inluence navigation. (a) Pitot and static system includes the standby altimeter/airspeed indicator system, and micro air data computers. Altitude alerting and reporting system uses pitot and static information. (b) Angle-of-attack system utilizes a probe to sense an environmental condition for airplane attitude.

ICA-560XL-34-00009

© Cessna Aircraft Company

34-00-00

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Form 2261 Rev 1

CESSNA AIRCRAFT COMPANY

MODEL 560XL

MAINTENANCE MANUAL (c) (d)

(2)

(3) (4) (5)

(6)

Ram air temperature uses sensor to get the outside air temperature. Radio Altimeter system transmits radio signals and receives relected radio signals to get the airplane’s distance above ground, up to 2500 feet (762 m). Attitude and Direction section discusses that portion of the system which uses magnetic gyroscopic and inertia forces. This includes standby gyro, standby horizontal situation indicator (HSI), standby magnetic compass, attitude heading reference system (AHRS), and electronic light instruments (EFIS). Landing and Taxiing Aids covers the systems which provide guidance during approach, landing and taxiing. These systems include the glideslope, localizer and marker beacon. Independent Position Determining section describes systems which provide information to determine position and is mainly independent of ground installations or orbital satellites. This includes the weather radar, collision avoidance, and proximity warning systems. Dependent Position Determining section covers the systems which provide information to determine position and is mainly dependent on ground installations or orbital satellites. This includes low frequency, VHF and UHF systems, distance measuring equipment (DME), transponders, automatic direction inding (ADF), and global positioning system (GPS). Flight Management Computing section describes systems which combine navigational data to compute or manage airplane’s geographical position or theoretical light path. Included in this section is the light management system.

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Form 2261 Rev 1

CESSNA AIRCRAFT COMPANY

MODEL 560XL

MAINTENANCE MANUAL COLLINS TDR-94D DUAL TRANSPONDER SYSTEM - DESCRIPTION AND OPERATION 1.

2.

General A.

The Collins TDR-94D Dual Transponder System is an integrated part of the Collins Pro Line 21 Avionics Suite. This section gives the description and operation of the Collins TDR-94D Dual Transponder System components.

B.

The Collins TDR-94D Dual Transponder System components include two TDR-94D Transponders, two Transponder Antennas, and two Diversity Transponder Antennas.

Description A.

3.

Collins TDR-94D Dual Transponder System (1) The Collins TDR-94D Dual Transponder System is a solid-state, airborne, air trafic control (ATC) transponder system installed in a dual coniguration. The TDR-94D Transponder is a diversity version that can transmit and receive on two antennas. The Collins TDR-94D Dual Transponder System is fully compatible with the TCAS II system installation where antenna diversity is necessary. It operates in Mode A by responding to normal beacon radar interrogations. In Mode C (altitude encoding), the TDR-94D Transponder supplies altitude data with the normal reply. In Mode S, each airplane is assigned a unique identiication code that gives an automatic and unique interrogation and display of a speciic aircraft. The unique identiication code is related to the airplane's identiication (tail) number and is necessary with TCAS operation. Eight different formats of interrogation in Mode S lets the ground controller monitor only the aircraft that are necessary. The Collins TDR-94D Dual Transponder System also has an Enhanced Surveillance function that sends more airplane parameters to ATC to help give separation of aircraft. The Collins TDR-94D Dual Transponder System has two antennas for each TDR-94D Transponder. There is a Transponder Antenna installed on the nose and a Diversity Transponder Antenna installed on top of the fuselage. The CDU-3000 Control Display Units give the pilots the primary interface to control the Collins TDR-94D Dual Transponder System.

Operation A.

The Collins TDR-94D Dual Transponder System is an integral part of the Air Trafic Control Radar Beacon System (ATCRBS). It gives the identiication of transponder-equipped aircraft on the ATC ground controller's plan position indication (PPI). An altitude encoder gives ATC the aircraft's pressure altitude. The Collins TDR-94D Dual Transponder System can operate in Mode S and it gives a unique aircraft identiication code, and air-to-air and air-to-ground interrogation replies. The TDR-94D Transponder can also send and receive data link messages that are necessary for ATC automation. The data link lets the TDR-94D Transponder do more ATC and airplane separation assurance (ASA) functions. In Mode A or Mode C operation, the TDR-94D Transponder replies automatically to radar pulses from the ground station. Those replies are decoded for identiication and altitude data. In Mode S operation, the TDR-94D Transponder replies automatically to radar pulses from the ground station or from other aircraft.

B.

Some airplanes may have TDR-94D Automatic Dependant Surveillance Broadcast (ADS-B) Out capable transponders. ADS-B Out transponders transmit enhanced surveillance data with some additional light information. Some of the data transmitted is Satellite-Based Augmentation System (SBAS) position, speed, and altitude. A service integrity level is also transmitted that indicates the accuracy of the SBAS data. The data is transmitted on a 1090 MHz extended squitter that constantly broadcasts the ADS-B Out data. Some of the ADS-B Out data is transmitted when the airplane is on the ground.

ICA-560XL-34-00009

© Cessna Aircraft Company

34-53-07

Page 1 Oct 19/2015

Form 2261 Rev 1

CESSNA AIRCRAFT COMPANY

MODEL 560XL

MAINTENANCE MANUAL COLLINS TDR-94D DUAL TRANSPONDER SYSTEM - MAINTENANCE PRACTICES 1.

2.

General A.

The Collins TDR-94D Dual Transponder System is an integrated part of the Collins Pro Line 21 Avionics Suite. This section gives the instructions for removal and installation of the Collins TDR-94D Dual Transponder System components.

B.

The Collins TDR-94D Dual Transponder System components include two TDR-94D Transponders, two Transponder Antennas, and two Diversity Transponder Antennas.

Tools and Equipment A.

3.

For a list of tools and equipment, refer to Navigation - General.

TDR-94D Transponder Removal/Installation NOTE:

A.

The TDR-94D Transponder 1 (XPDR 1) is installed in the left side nose avionics compartment. The TDR-94D Transponder 2 (XPDR 2) is installed in the right side nose avionics compartment. The removal and installation procedures for XPDR 1 and XPDR 2 are typical.

Remove the TDR-94D Transponder. Refer to Figure 201. (1) Make sure that the ELECTRICAL BATT ON/OFF switch/light on the left tilt panel is in the OFF position. (2) Disengage the XPDR 1 or XPDR 2 circuit breaker on the right circuit breaker panel. (3) Get access to the TDR-94D Transponder 1 (XPDR 1) or Transponder 2 (XPDR 2). (a) Open the left side nose avionics compartment door to get access to the XPDR 1. (b) Open the right side nose avionics compartment door to get access to the XPDR 2. (4) Loosen the knurled nuts to release the TDR-94D Transponder from the mounting tray. (5) Lift the handle at the front of the TDR-94D Transponder and carefully pull it out to disengage it from the electrical connectors and coaxial cable connectors in the rear of the mounting tray. NOTE:

(6) B.

The electrical connectors (PN863 PN865 XPDR 1, PN864 PN866 XPDR 2) and coaxial cable connectors (PN1131 PN1833 XPDR 1, PN1002 PN1008 XPDR 2) are attached to the rear of the mounting tray.

Remove the TDR-94D Transponder from the airplane.

Install the TDR-94D Transponder. Refer to Figure 201. (1) Put the TDR-94D Transponder into position on the mounting tray.

CAUTION: Make sure that the electrical connectors and coaxial cable connectors are aligned correctly, to prevent damaged or bent pin contacts. (2) (3) (4) (5) (6) (7) (8)

Carefully push the TDR-94D Transponder to the rear of the mounting tray until it is tight. Make sure that the electrical connectors (PN863 PN865 XPDR 1, PN864 PN866 XPDR 2) and coaxial cable connectors (PN1131 PN1833 XPDR 1, PN1002 PN1008 XPDR 2) are engaged. Tighten the knurled nuts to attach the TDR-94D Transponder to the mounting tray. Close the left or right side nose avionics compartment door. Engage the XPDR 1 or XPDR 2 circuit breaker on the right circuit breaker panel. Do a self-test of the TDR-94D Transponder System. Refer to Collins TDR-94D Dual Transponder System - Adjustment/Test, TDR-94D Dual Transponder System Self-Test. Do the ADS-B Out check. Refer to Collins TDR-94D Dual Transponder System - Adjustment/ Test Automatic Dependant Surveillance Broadcast (ADS-B) Out Functional Check.

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Form 2261 Rev 1

CESSNA AIRCRAFT COMPANY

MODEL 560XL

MAINTENANCE MANUAL

Collins TDR-94D Dual Transponder System Installation Figure 201 (Sheet 1)

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Form 2261 Rev 1

CESSNA AIRCRAFT COMPANY

MODEL 560XL

MAINTENANCE MANUAL

Collins TDR-94D Dual Transponder System Installation Figure 201 (Sheet 2)

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Form 2261 Rev 1

CESSNA AIRCRAFT COMPANY

MODEL 560XL

MAINTENANCE MANUAL 4.

Transponder Antenna Removal/Installation NOTE:

5.

The Transponder 1 Antenna is installed on the left side of the nose near the bottom at FS 54.68 and LBL 9.27. The Transponder 2 Antenna is installed on the right side of the nose near the bottom at FS 94.57 and RBL 10.00. The removal and installation procedures for the Transponder 1 and Transponder 2 antennas are typical.

A.

Remove the Transponder Antenna. Refer to Figure 201. (1) Make sure that the ELECTRICAL BATT ON/OFF switch/light on the left tilt panel is in the OFF position. (2) Disengage the XPDR 1 or XPDR 2 circuit breaker on the right circuit breaker panel. (3) Get access to the Transponder antenna coaxial cable connector. (a) Open the left side nose avionics compartment door for the Transponder 1 antenna. (b) Open the right side nose avionics compartment door for the Transponder 2 antenna. (4) Disconnect the coaxial cable connector (PN1093 Transponder 1, PN1004 Transponder 2) from the Transponder antenna. (a) Put a cap or cover on the coaxial connector. (5) Remove the screws that attach the Transponder antenna to the fuselage skin. (6) Carefully pull the Transponder antenna away from the fuselage skin. (7) Remove the Transponder antenna from the airplane. (8) Carefully remove the sealant from the Transponder antenna and the fuselage skin. Refer to Chapter 20, Fuel, Weather, Pressure and High-Temperature Sealing - Maintenance Practices .

B.

Install the Transponder Antenna. Refer to Figure 201. (1) Make sure that the mounting surfaces of the Transponder antenna and the fuselage skin are free from old sealant. Refer to Chapter 20, Fuel, Weather, Pressure and High-Temperature Sealing - Maintenance Practices. (2) Make sure that the antenna and airplane are prepared for electrical bonding. Refer to Chapter 20, Electrical Bonding - Maintenance Practices. (3) Remove cap or cover on the coaxial connector. (4) Connect the coaxial cable connector (PN1093 Transponder 1, PN1004 Transponder 2) to the antenna. (5) Apply a 1/4 inch bead of Type XV, Class B conductive sealant around the base of the antenna. Refer to Chapter 20, Fuel, Weather, Pressure and High Temperature Sealing - Maintenance Practices. (6) Put the transponder antenna in the correct position on the fuselage skin. (7) Install the screws that attach the transponder antenna to the fuselage skin. (8) Apply a 1/4 inch bead of Type XV, Class B conductive sealant to make a 1/4 inch illet seal around the perimeter of the antenna and connector cutout. Refer to Chapter 20, Fuel, Weather, Pressure and High-Temperature Sealing - Maintenance Practices. (9) Make sure there is a good electrical bond (Type I) between the antenna base and the airplane skin. Refer to Chapter 20, Electrical Bonding - Maintenance Practices. (10) Close the left or right side nose avionics compartment door. (11) Engage the XPDR 1 or XPDR 2 circuit breaker on the right circuit breaker panel. (12) Do a self-test of the TDR-94D Transponder System. Refer to Collins TDR-94D Dual Transponder System - Adjustment/Test, TDR-94D Dual Transponder System Self-Test.

Diversity Transponder Antenna Removal/Installation NOTE:

A.

The Diversity Transponder 1 Antenna is installed near the top of the fuselage on the left side aft of the cabin door at FS 234.25 and LBL 11.20. The Diversity Transponder 2 Antenna is installed near the top of the fuselage on the right side aft of the cabin door at FS 234.25 and RBL 11.20. The removal and installation procedures for the Diversity Transponder 1 and Diversity Transponder 2 antennas are typical.

Remove the Diversity Transponder Antenna. Refer to Figure 201. (1) Make sure that the ELECTRICAL BATT ON/OFF switch/light on the left tilt panel is in the OFF position. (2) Disengage the XPDR 1 or XPDR 2 circuit breaker on the right circuit breaker panel.

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MODEL 560XL

MAINTENANCE MANUAL (3) (4) (5) (6) (7)

B.

Remove the screws that attach the Diversity Transponder antenna to the fuselage skin. Carefully pull the Diversity Transponder antenna away from the fuselage skin. Disconnect the coaxial cable connector (PC1003 Transponder 1, PF1004 Transponder 2) from the Diversity Transponder antenna. Remove the Diversity Transponder antenna from the airplane. Carefully remove the sealant from the Diversity Transponder antenna and the fuselage skin. Refer to Chapter 20, Fuel, Weather, Pressure and High-Temperature Sealing - Maintenance Practices .

Install the Diversity Transponder Antenna. Refer to Figure 201. (1) Make sure that the mounting surfaces of the Diversity Transponder antenna and the fuselage skin are free from old sealant. Refer to Chapter 20, Fuel, Weather, Pressure and High-Temperature Sealing - Maintenance Practices. (2) Connect the coaxial cable connector (PC1003 Transponder 1, PF1004 Transponder 2) to the Diversity Transponder antenna. (3) Put the Diversity Transponder antenna in the correct position on the fuselage skin. (4) Install the screws that attach the Diversity Transponder antenna to the fuselage skin. (5) Use Type I, Class B sealant to make a illet seal around the perimeter of the Diversity Transponder antenna. Refer to Chapter 20, Fuel, Weather, Pressure and High-Temperature Sealing - Maintenance Practices. (6) Do an electrical bonding test. Refer to Chapter 20, Electrical Bonding - Maintenance Practices. (a) Make sure that the resistance is not more than 0.0025 ohms. (7) Use Type V, Class A sealant to make a seal that is lush with the counterbored holes of the Diversity Transponder antenna. Refer to Chapter 20, Fuel, Weather, Pressure and High-Temperature Sealing - Maintenance Practices. (8) Engage the XPDR 1 or XPDR 2 circuit breaker on the right circuit breaker panel. (9) Do a self-test of the TDR-94D Transponder System. Refer to Collins TDR-94D Dual Transponder System - Adjustment/Test, TDR-94D Dual Transponder System Self-Test.

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Form 2261 Rev 1

CESSNA AIRCRAFT COMPANY

MODEL 560XL

MAINTENANCE MANUAL COLLINS TDR-94D DUAL TRANSPONDER SYSTEM - ADJUSTMENT/TEST 1.

2.

General A.

The Collins TDR-94D Dual Transponder System is an integrated part of the Collins Pro Line 21 Avionics Suite. This section gives the adjustment/test procedures of the Collins TDR-94D Dual Transponder System components.

B.

The Collins TDR-94D Dual Transponder System components include two TDR-94D Transponders, two Transponder Antennas, and two Diversity Transponder Antennas.

Tools and Equipment A.

3.

For a list of tools and equipment, refer to Navigation - General.

TDR-94D Dual Transponder System Self-Test A.

Do a self-test of the Collins TDR-94D Dual Transponder System. (1) Connect 28.5 VDC, +0.5 or -0.5 VDC external electrical power to the airplane. (2) Push the ELECTRICAL BATT switch/light on the left tilt panel in the ON position. (3) Make sure that the ELECTRICAL NORM/EMER switch/light on the left tilt panel is in the NORM position. (4) Push the ELECTRICAL AVIONICS switch/light on the left tilt panel in the ON position. (5) Push the TUN button on the pilot's Control Display Unit (CDU 1) to go to the Tune Page. (6) Push the ATC line select key (LSK) on CDU 1 to go to the ATC CONTROL Page. (7) Push the SELECT LSK on CDU 1 to select ATC 1. (8) Tune the ATC 1 to a transponder code of 0600 with the scratch pad and Code LSK.

CAUTION: Do not set the transponder to any of the codes that follow: 0000 7500 7600 7700

(9)

- Military Intercept Code - Hijack Code - VHF Com Receiver Failure Code - Emergency Code

Push the TEST LSK on CDU 1 to start the self-test for ATC 1. NOTE:

During the self-test, the word TEST will change to a larger size and be cyan in color. After the test is done, the word TEST will change back to the usual size and be white in color.

(a)

Make sure that the word TEST changes to a larger size and is cyan in color during the self-test. (b) Make sure that the word TEST changes back to the usual size and is white in color after the self-test is done. (c) Make sure that XPDR FAIL is not shown on CDU 1. (10) Push the SELECT LSK on CDU 1 to select ATC 2. (11) Tune the ATC 2 to a transponder code of 0600 with the scratch pad and Code LSK.

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MAINTENANCE MANUAL

CAUTION: Do not set the transponder to any of the codes that follow: 0000 7500 7600 7700

- Military Intercept Code - Hijack Code - VHF Com Receiver Failure Code - Emergency Code

(12) Push the TEST LSK on CDU 1 to start the self-test for ATC 2. NOTE:

During the self-test, the word TEST will change to a larger size and be cyan in color. After the test is done, the word TEST will change back to the usual size and be white in color.

(a)

Make sure that the word TEST changes to a larger size and is cyan in color during the self-test. (b) Make sure that the word TEST changes back to the usual size and is white in color after the self-test is done. (c) Make sure that XPDR FAIL is not shown on CDU 1. (13) Push the ELECTRICAL AVIONICS switch/light on the left tilt panel in the OFF position. (14) Push the ELECTRICAL BATT switch/light on the left tilt panel in the OFF position. (15) Remove the external electrical power from the airplane. 4.

(Airplanes -6204 and On and Airplanes -6001 thru -6203 incorporating SB560XL-34-76) Automatic Dependant Surveillance Broadcast (ADS-B) Out Functional Check A.

Functional Check Preparation. NOTE: (1)

This check requires the use of the IFR-6000 Flightline Test Set, or equivalent. An air data test set is not required to complete this functional check.

Make sure the airplane is located outside with a clear view of the southern sky. NOTE:

(2) (3) (4) (5) (6) (7) B.

Connect the landing gear simulator test boxes and move the switch to ON GROUND. Connect the external electrical power unit to the airplane. (a) Adjust the electrical power to 29.0 VDC, +0.5 or -0.5 VDC. Set the BATTERY switch on the ELECTRICAL POWER switch panel in the cockpit to the ON position. Set the AVIONICS switch on the ELECTRICAL POWER switch panel in the cockpit to the ON position. Set both transponders to transmit 1200. Set transponder 1 to ON.

ADV CIRC 20-165 AIR Check (1) Set the landing gear simulator test boxes and move the switch to IN AIR. (2) Run the AC 20-165 AIR test on the IFR-6000 Flightline Test Set. NOTE: (3) (4) (5) (6) (7)

C.

The airplane must be able to receive a strong and constant GPS signal for the ADS-B to properly test.

The lower transponder antennas should be used to perform this test.

Make sure that NACP = 8 or more Make sure that NACV = 2 or less Make sure that PASS is displayed on the ADV CIRC 20-165 AIR page. Do this check again for transponder 2. Set transponder 1 to ON.

ADV CIRC 20-165 SURFACE Check (1) Set the landing gear simulator test boxes and move the switch to ON GROUND.

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MODEL 560XL

MAINTENANCE MANUAL (2)

Run the AC 20-165 SURFACE test on the IFR-6000 Flightline Test Set. NOTE:

(3) (4) (5) (6)

The upper transponder antennas should be used to perform this test.

Make sure that NIC = 8 or less. Make sure that PASS is displayed on the ADV CIRC 20-165 SURFACE page. Do this check again for transponder 2. Set transponder 1 to ON.

D.

ADS-B Out Surface Data Check (1) Make sure that the information that follows is displayed on the IFR-6000 Flightline Test Set MON BDS 0,8 page. • EMIT CAT = SMALL (2) Make sure that the information that follows is displayed on the IFR-6000 Flightline Test Set MON BDS 6,5 SUR page. • SUBTYPE = 1 - SUR • VERSION = 2 - DO-260B • SDA = 2 • SAF = 0 • ANT OFF = RT 0m, 4m • POA = 0 • SIL SUP = 0 • SIL = 3 • LN/WD = 2 -