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Rockwell Collins Pro Line Fusion for King Air Aircraft Maintenance Manual
$44.95 Original price was: $44.95.$26.95Current price is: $26.95.
1,410-page factory Aircraft Maintenance Manual for the Rockwell Collins Pro Line Fusion avionics system on the King Air C90GTi, B200GT, B200CGT, B300 and B300C. 1st Edition, Dec 02/14. Instant PDF download.
SKU: HDL-RC-PLF-KINGAIR-AMM-2014
Category: Aircraft Manuals
Tags: B200GT B300 maintenance manual, King Air avionics manual, Pro Line Fusion King Air manual, Rockwell Collins AMM
Vendor: Wiring Manuals
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Description
Rockwell Collins Pro Line Fusion for King Air Aircraft Maintenance Manual
This is the complete Rockwell Collins Pro Line Fusion for King Air Aircraft Maintenance Manual, a 1,410-page factory-issued technical publication (Manual Part No. 523-0821905-001129, 1st Edition, Dec 02/14) covering the Pro Line Fusion avionics suite as installed on the Beechcraft King Air C90GTi, B200GT, B200CGT, B300, and B300C. This edition is marked for training purposes, making it an ideal deep-reference document for avionics technicians, maintenance students, and King Air operators who want to understand the Pro Line Fusion system architecture in detail.
- Manual type: Aircraft Maintenance Manual (AMM)
- Brand/System: Rockwell Collins Pro Line Fusion avionics
- Aircraft models: King Air C90GTi, B200GT, B200CGT, B300, B300C
- Language: English
- Page count: 1,410 pages
- File format: PDF (digital download)
- Document number: 523-0821905-001129
- Edition: 1st Edition, December 02, 2014
IMAGES PREVIEW
Chapters Covered
- Introduction — manual arrangement, AMTOSS task numbering, systems/equipment covered, associated publications, abbreviations
- 22 – Auto Flight: Flight Guidance System (FGS), Flight Guidance Computer, Flight Guidance Panel, Aileron/Elevator/Rudder Servos, Elevator Trim Servo — theory, controls and displays, component data, removal/installation, adjustment/test
- 23 – Communication: HF Communication System, VHF Communication System, VHF Data System, Communications Management Unit (CMU), External Compensation Unit (ECU)
- 31 – Indicating/Recording Systems: Integrated Avionics Processor System (IAPS), Data Concentration System (DCS), Electronic Flight Instrument System (EFIS), Adaptive Flight Displays (AFD), Cursor Control Panel, Multifunction Keypad Panel
- 34 – Navigation: Air Data System (ADS), Attitude Heading Reference System (AHRS), Synthetic Vision System (SVS), Weather Radar System, Radio Altimeter System, TCAS II, GNSS/GPS, VHF Navigation, DME, ATC Transponder, Flight Management System (FMS)
- 44 – Cabin Systems: Video Surveillance System
- 45 – Central Maintenance System: Onboard Maintenance System (OMS)
- 46 – Systems Integration and Display: Integrated Flight Information System, XM Weather, Information Management System (IMS)
- 77 – Engine Indicating: Engine Indication and Crew Alert System (EICAS)
Across these chapters the manual walks a technician through every Pro Line Fusion line-replaceable unit fitted to these King Air variants — general description and theory of operation, cockpit controls and displays, physical and electrical component data, certification categories, component location diagrams, and the removal/installation and adjustment/test procedures needed to service each unit.
Complete PDF Bookmark Tree
Complete Bookmarks
The complete bookmarks in the “Rockwell Collins Pro Line Fusion for King Air Aircraft Maintenance Manual” are as follows:
+Pro Line Fusion® for King Airp. 1
TITLE PAGEp. 3
RECORD OF REVISIONSp. 5
RECORD OF TEMPORARY REVISIONSp. 7
SERVICE BULLETIN LISTp. 9
LIST OF EFFECTIVE PAGESp. 11
TABLE OF CONTENTSp. 27
LIST OF FIGURESp. 53
LIST OF TABLESp. 65
+Introductionp. 73
+INTRODUCTIONp. 75
Generalp. 75
Verification Statementp. 75
Warnings, Cautions, and Notesp. 75
Safety Precautionsp. 76
Revision Servicep. 76
Manual Arrangement and Formatp. 76
Application of Task Numbering Systemp. 78
System/Equipment Covered by the Manualp. 80
List of Associated Publicationsp. 88
List of Abbreviationsp. 102
List of Manufacturersp. 113
How to Use the AMMp. 113
+Part 1 – System Descriptionp. 115
+22 AUTO FLIGHTp. 117
+Flight Guidance System (FGS)p. 119
Introductionp. 119
General Descriptionp. 119
FGS Modes of Operationp. 123
+Flight Guidance Computer – Theory of Operationp. 127
Flight Guidance Computer No. 1p. 127
Flight Guidance Computer No. 2p. 139
+Flight Guidance Computer – Controls and Displaysp. 147
Cockpit Controlsp. 147
Component Datap. 158
Component Locationp. 159
+Flight Guidance Panelp. 161
Theory of Operationp. 161
+Flight Guidance Panel – Controls and Displaysp. 175
Cockpit Controlsp. 175
Unit Controlsp. 175
Control Wheel and Power Level Handle Controlsp. 181
Component Datap. 183
Component Locationp. 184
+Aileron Servop. 187
Theory of Operationp. 187
Aileron Servo – Component Datap. 191
Component Locationp. 191
+Elevator Servop. 193
Theory of Operationp. 193
Component Datap. 197
Component Locationp. 197
+Rudder Servop. 201
Theory of Operationp. 201
Component Datap. 205
Component Locationp. 206
+Elevator Trim Servop. 209
Theory of Operationp. 209
Component Datap. 213
Component Locationp. 214
+23 COMMUNICATIONp. 217
+HF Communication Systemp. 219
Introductionp. 219
General Descriptionp. 219
+HF Receiver/Transmitterp. 221
Theory of Operationp. 221
+HF Receiver/Transmitter – Controls and Displaysp. 225
Cockpit Controlsp. 225
Component Datap. 226
Component Locationp. 226
+HF Antenna Couplerp. 229
Theory of Operationp. 229
Component Datap. 231
Component Locationp. 231
+VHF Communication Systemp. 233
Introductionp. 233
General Descriptionp. 233
+VHF Communication System – Theory of Operationp. 235
VHF COMM Transceiver No. 1p. 235
VHF COMM Transceiver No. 2p. 238
+VHF Comm Transceiver – Controls and Displaysp. 241
Cockpit Controlsp. 241
Component Datap. 245
Component Locationp. 245
+VHF Data Systemp. 247
Introductionp. 247
General Descriptionp. 247
+VHF Comm Transceiver (Datalink) – Theory of Operationp. 249
VHF COMM Transceiver No. 3 (OPTION)p. 249
Component Datap. 251
Component Locationp. 251
+Communications Management Unit (CMU)p. 253
Theory of Operationp. 253
+Communications Management Unit (CMU) – Controls and Displaysp. 257
Cockpit Controlsp. 257
Cockpit Controls – Datalink APPLICATION MENUp. 257
Cockpit Controls – CPDLC MENU – LOGON/STATUSp. 258
Cockpit Controls – Sending/Receiving Messagesp. 262
Cockpit Controls – CPDLC MENU – ATC LOGp. 263
Cockpit Controls – CPDLC MENU – ATN LINK STATUSp. 264
Component Datap. 265
Component Locationp. 266
+External Compensation Unit (ECU)p. 269
Theory of Operationp. 269
Component Datap. 271
Component Locationp. 271
+31 INDICATING/RECORDING SYSTEMSp. 273
+Integrated Avionics Processor System (IAPS)p. 275
Introductionp. 275
General Descriptionp. 275
+Integrated Card Cage (ICC) – Theory of Operationp. 279
Integrated Card Cage (No. 1 Side)p. 279
Integrated Card Cage (No. 2 Side)p. 282
Component Datap. 285
Component Locationp. 285
+IAPS Environmental Controller (IEC)p. 287
Theory of Operationp. 287
+IAPS Environmental Controller (IEC) – Controls and Displaysp. 289
Cockpit Controlsp. 289
Unit Controlsp. 289
Component Datap. 290
Component Locationp. 291
+Input/Output Concentrator (IOC) – Theory of Operationp. 293
Input/Output Concentrator No. 1p. 293
Input/Output Concentrator No. 2p. 296
+Input/Output Concentrator (IOC) – Controls and Displaysp. 299
Cockpit Controlsp. 299
Unit Controlsp. 299
Component Datap. 300
Component Locationp. 301
+Power Supply Module – Theory of Operationp. 303
Power Supply Module No. 1p. 303
Power Supply Module No. 2p. 306
+Power Supply Module – Power Supply Module – Controls and Displaysp. 309
Cockpit Controlsp. 309
Unit Controlsp. 309
Component Datap. 310
Component Locationp. 311
+Configuration Strapping Unit (CSU) – Theory of Operationp. 313
Configuration Strapping Unit No. 1p. 313
Configuration Strapping Unit No. 2p. 315
+Configuration Strapping Unit (CSU) – Controls and Displaysp. 317
Cockpit Controlsp. 317
Unit Controlsp. 317
Component Datap. 317
Component Locationp. 317
+Option Control Module (OCM) – Theory of Operationp. 321
Option Control Module No. 1p. 321
Option Control Module No. 2p. 323
Component Datap. 325
Component Locationp. 325
+Data Concentration System (DCS)p. 327
Introductionp. 327
General Descriptionp. 327
+Data Concentration System (DCS) – Theory of Operationp. 329
Data Concentrator Unit No. 1p. 329
Data Concentrator Unit No. 2p. 337
Engine Data Concentrator No. 1p. 344
Engine Data Concentrator No. 2p. 348
Component Datap. 352
Component Locationp. 352
+Remote Data Concentrator (RDC) – Theory of Operationp. 355
Remote Data Concentrator No. 1p. 355
Remote Data Concentrator No. 2p. 360
Component Datap. 364
Component Locationp. 364
+Electronic Flight Instrument System (EFIS)p. 367
Introductionp. 367
General Descriptionp. 367
Adaptive Flight Displayp. 368
Cursor Control Panelp. 368
Multifunction Keypad Panelp. 368
Aircraft Personality Modulep. 368
Barometric Single Knob Panelp. 368
Adaptive Flight Display Runtimep. 368
Flight Display System Applicationp. 369
Protocol Manager Applicationp. 370
Radio Tuning System Applicationp. 370
Airframe Parameter Configuration Tablep. 371
Integrated Modular Avionics Tablep. 371
Emulated Control Display Applicationp. 372
EFIS Intefacep. 372
+Adaptive Flight Display (AFD) – Theory of Operationp. 375
Adaptive Flight Display No. 1p. 375
Adaptive Flight Display No. 2p. 386
Adaptive Flight Display No. 3p. 400
+Adaptive Flight Display (AFD) – Controls and Displaysp. 411
Cockpit Controls – Functional Descriptionp. 411
Cockpit Controls – Operational Descriptionp. 426
Component Datap. 440
Component Locationp. 443
+Cursor Control Panel (CCP) – Theory of Operationp. 445
Cursor Control Panel No. 1p. 445
Cursor Control Panel No. 2p. 449
+Cursor Control Panel (CCP) – Controls and Displaysp. 451
Unit Controlsp. 451
Component Datap. 453
Component Locationp. 454
+Multifunction Keypad Panel (MKP)p. 457
Theory of Operationp. 457
+Multifunction Keypad Panel (MKP) – Controls and Displaysp. 461
Unit Controlsp. 461
Component Datap. 464
Component Locationp. 465
+Aircraft Personality Module (APM)p. 467
Theory of Operationp. 467
Component Datap. 469
Component Locationp. 469
+Baro Single Knob Panel – Theory of Operationp. 471
Baro Single Knob No. 1p. 471
Baro Single Knob No. 2p. 473
+Baro Single Knob Panel – Controls and Displaysp. 475
Unit Controlsp. 475
Component Datap. 476
Component Locationp. 477
+Emulated Control Display Unit (ECDU)p. 479
Theory of Operationp. 479
+Emulated Control Display Unit (ECDU) – Controls and Displaysp. 481
Cockpit Controlsp. 481
+34 NAVIGATIONp. 485
+Air Data System (ADS)p. 487
Introductionp. 487
General Descriptionp. 487
+Air Data Computer (ADC) – Theory of Operationp. 491
Air Data Computer No. 1p. 491
Air Data Computer No. 2p. 500
+Air Data Computer (ADC) – Controls and Displaysp. 507
Cockpit Controlsp. 507
Unit Controlsp. 509
Component Datap. 510
Component Locationp. 511
+Attitude Heading Reference System (AHRS)p. 513
Introductionp. 513
General Descriptionp. 513
+Attitude Heading Computer (AHC) – Theory of Operationp. 515
Attitude Heading Reference Computer No. 1p. 515
Attitude Heading Reference Computer No. 2p. 519
+Attitude Heading Computer (AHC) – Controls and Displaysp. 523
Cockpit Controlsp. 523
Unit Controlsp. 525
Component Datap. 526
Component Locationp. 526
+Flux Detector Unit (FDU) – Theory of Operationp. 529
Flux Detector Unit No. 1p. 529
Flux Detector Unit No. 2p. 530
Component Datap. 531
Component Locationp. 533
+External Compensation Unit (ECU) – Theory of Operationp. 535
External Compensation Unit No. 1p. 535
External Compensation Unit No. 2p. 537
Component Datap. 539
Component Locationp. 539
+Synthetic Vision System (SVS)p. 541
Introductionp. 541
General Descriptionp. 541
+Synthetic Vision System (SVS) – Controls and Displaysp. 543
Cockpit Controlsp. 543
Component Datap. 545
+Weather Radar Systemp. 547
Introductionp. 547
General Descriptionp. 547
Weather Radar Modes of Operationp. 550
+Tilt Single Knob Panel – Theory of Operationp. 551
Tilt Single Knob No. 1p. 551
Tilt Single Knob No. 2p. 553
+Tilt Single Knob Panel – Controls and Displaysp. 555
Unit Controlsp. 555
+Weather Radar Receiver/Transmitter Antenna (RTA)p. 559
Theory of Operationp. 559
Component Datap. 562
Component Locationp. 563
+Radio Altimeter Systemp. 565
Introductionp. 565
General Descriptionp. 565
+Radio Altimeter Transceiverp. 567
Theory of Operationp. 567
Component Datap. 571
Component Locationp. 571
+Traffic Alert and Collision Avoidance System IIp. 573
Introductionp. 573
General Descriptionp. 573
+TCAS Transmitter/Receiverp. 577
Theory of Operationp. 577
+TCAS Transmitter/Receiver – Controls and Displaysp. 581
Cockpit Controlsp. 581
Cockpit Controls – Traffic Modesp. 581
Cockpit Controls – Altitude Limitp. 583
Cockpit Controls – Traffic Overlayp. 584
Cockpit Controls – Traffic Symbolsp. 584
Unit Controlsp. 585
Component Datap. 587
Component Locationp. 588
+TCAS Directional Antennap. 591
Component Datap. 591
Component Locationp. 591
+Global Navigation Satellite System (GNSS)p. 593
Introductionp. 593
General Descriptionp. 593
+Global Positioning System (GPS) Receiver – Theory of Operationp. 595
Global Positioning System Receiver No. 1p. 595
Global Positioning System Receiver No. 2p. 598
+Global Positioning System (GPS) Receiver – Controls and Displaysp. 601
Cockpit Controlsp. 601
Unit Controlsp. 601
Component Datap. 603
Component Locationp. 604
+VHF Navigation Systemp. 607
Introductionp. 607
General Descriptionp. 607
+VHF Navigation Receiver – Theory of Operationp. 611
VHF Navigation Receiver No. 1p. 611
VHF Navigation Receiver No. 2 (NAV-4500)p. 616
VHF Navigation Receiver No. 2 (NAV-4000 – Option)p. 619
+VHF Navigation Receiver – Controls and Displaysp. 623
Cockpit Controlsp. 623
Component Datap. 624
Component Locationp. 625
+Automatic Direction Finder (ADF) Antenna – Theory of Operationp. 627
Automatic Direction Finder (ADF) Antenna No. 1p. 627
Automatic Direction Finder (ADF) Antenna No. 2p. 629
Component Datap. 631
Component Locationp. 632
+Distance Measuring Equipment (DME)p. 635
Introductionp. 635
General Descriptionp. 635
+Distance Measuring Equipment (DME) Transceiver – Theory of Operationp. 637
DME Transceiver No. 1p. 637
DME Transceiver No. 2 (Option)p. 639
+Distance Measuring Equipment (DME) Transceiver – Controls and Displaysp. 641
Cockpit Controlsp. 641
Component Datap. 641
Component Locationp. 642
+Air Traffic Control (ATC) Transponder Systemp. 645
Introductionp. 645
General Descriptionp. 645
+Diversity Transponder – Theory of Operationp. 649
Diversity Transponder No. 1p. 649
Diversity Transponder No. 2p. 654
+Diversity Transponder – Controls and Displaysp. 657
Cockpit Controlsp. 657
Selecting the Active Transponderp. 657
Setting the Squawk Codep. 658
Setting the Flight IDp. 658
IDENT Buttonp. 658
Component Datap. 659
Component Locationp. 659
+Flight Management System (FMS)p. 661
Introductionp. 661
General Descriptionp. 661
Theory of Operationp. 664
FMS Position Determinationp. 664
FMS Navigation and Steeringp. 664
FMS NAV-to-NAV Transferp. 665
FMS-GPS Wrap Testp. 665
FMS Auto-Tunep. 666
FMS Datalinkp. 666
FMS Pilot Waypoint and Routes Load/Storep. 666
+Flight Management System (FMS) – Controls and Displaysp. 667
Cockpit Controlsp. 667
Component Datap. 669
+44 CABIN SYSTEMSp. 671
+Video Surveillance Systemp. 673
Introductionp. 673
General Descriptionp. 673
+Video Surveillance System – Controls and Displaysp. 675
Cockpit Controlsp. 675
+45 CENTRAL MAINTENANCE SYSTEMp. 677
+Onboard Maintenance System (OMS)p. 679
Introductionp. 679
General Descriptionp. 679
Onboard Maintenance Systemp. 679
Onboard Maintenance System Applicationp. 679
Onboard Maintenance System Tablep. 680
Onboard Data Loader Applicationp. 680
OMS Interfacep. 680
Theory of Operationp. 682
Onboard Diagnosticsp. 682
Configurationp. 683
Reportingp. 683
Database Managementp. 683
Data Loadp. 684
Controls and Displaysp. 685
Component Datap. 685
+46 SYSTEMS INTEGRATION AND DISPLAYp. 689
+Integrated Flight Information Systemp. 691
Introductionp. 691
General Descriptionp. 691
+Integrated Flight Information System – Controls and Displaysp. 693
Cockpit Controls – File Sever Applicationp. 693
Cockpit Controls – Data Link Weather Keyp. 693
Cockpit Controls – Electronic Charts Keyp. 695
Cockpit Controls – Enhanced Maps Overlay Keyp. 699
Cockpit Controls – Outboard IFIS Keyp. 699
Component Datap. 700
+XM Weatherp. 701
Introductionp. 701
General Descriptionp. 701
+XM Weather Receiverp. 705
Theory of Operationp. 705
+XM Weather Receiver – Controls and Displaysp. 707
Cockpit Controlsp. 707
Component Datap. 708
Component Locationp. 709
+Information Management System (IMS)p. 711
Introductionp. 711
General Descriptionp. 711
Theory of Operationp. 714
+Information Management System (IMS) – Controls and Displaysp. 717
Cockpit Controlsp. 717
Unit Controlsp. 717
Component Datap. 719
Component Locationp. 720
+77 ENGINE INDICATINGp. 723
+Engine Indication and Crew Alert System (EICAS)p. 725
Introductionp. 725
General Descriptionp. 725
+Engine Indication and Crew Alert System (EICAS) – Controls and Displaysp. 729
Cockpit Controlsp. 729
Component Datap. 730
+Part 2 – Proceduresp. 733
+22 AUTO FLIGHTp. 735
+Flight Guidance System (FGS) – Component Locationp. 737
Component Locationp. 737
+Flight Guidance Computer (FGC) – Removal/Installationp. 743
Generalp. 743
Removalp. 743
Installationp. 746
+Flight Guidance Computer (FGC) – Adjustment/Testp. 749
Generalp. 749
Operational Testp. 749
+Flight Guidance Panel – Removal/Installationp. 763
Generalp. 763
Removalp. 763
Installationp. 766
+Flight Guidance Panel – Adjustment/Testp. 769
Generalp. 769
Operational Testp. 769
+Aileron Servo – Removal/Installationp. 775
Generalp. 775
Removalp. 775
Installationp. 777
+Aileron Servo – Adjustment/Testp. 779
Generalp. 779
Operational Testp. 779
+Aileron Servo Mount – Removal/Installationp. 783
Generalp. 783
Removalp. 783
Installationp. 786
+Elevator Servo – Removal/Installationp. 789
Generalp. 789
Removalp. 789
Installationp. 791
+Elevator Servo – Adjustment/Testp. 793
Generalp. 793
Operational Testp. 793
+Elevator Servo Mount – Removal/Installationp. 797
Generalp. 797
Removalp. 797
Installationp. 800
+Rudder Servo – Removal/Installationp. 803
Generalp. 803
Removalp. 803
Installationp. 805
+Rudder Servo – Adjustment/Testp. 807
Generalp. 807
Operational Testp. 807
+Rudder Servo Mount – Removal/Installationp. 811
Generalp. 811
Removalp. 811
Installationp. 814
+Trim Servo – Removal/Installationp. 817
Generalp. 817
Removalp. 817
Installationp. 819
+Trim Servo – Adjustment/Testp. 821
Generalp. 821
Operational Testp. 821
+Trim Servo Mount – Removal/Installationp. 823
Generalp. 823
Removalp. 823
Installationp. 826
+23 COMMUNICATIONp. 829
+HF Communication System – Component Locationp. 831
Component Locationp. 831
+HF Communication System – Adjustment/Testp. 833
Generalp. 833
Operational Testp. 833
+HF Receiver/Transmitter – Removal/Installationp. 839
Generalp. 839
Removalp. 839
Installationp. 842
+HF Antenna Coupler – Removal/Installationp. 845
Generalp. 845
Removalp. 845
Installationp. 848
+HF Feedline Adapter – Removal/Installationp. 851
Generalp. 851
Removalp. 851
Installationp. 854
+VHF Communication System – Component Locationp. 857
Component Locationp. 857
+VHF Communication System – Adjustment/Testp. 859
Generalp. 859
Operational Testp. 859
+VHF Comm Transceiver – Removal/Installationp. 871
Generalp. 871
Removalp. 871
Installationp. 874
+VHF Comm Transceiver – Adjustment/Testp. 877
Generalp. 877
Operational Testp. 877
+VHF Data System – Component Locationp. 881
Component Locationp. 881
+VHF Data Transceiver – Removal/Installationp. 883
Generalp. 883
Removalp. 883
Installationp. 886
+VHF Data Transceiver – Adjustment/Testp. 889
Generalp. 889
Operational Testp. 889
+Communications Management Unit (CMU) – Removal/Installationp. 891
Generalp. 891
Removalp. 891
Installationp. 894
+Communications Management Unit (CMU) – Adjustment/Testp. 897
Generalp. 897
Operational Testp. 897
+External Compensation Unit (ECU) – Removal/Installationp. 899
Generalp. 899
Removalp. 899
Installationp. 902
+External Compensation Unit (ECU) – Adjustment/Testp. 905
Generalp. 905
Operational Testp. 905
+31 INDICATING/RECORDING SYSTEMp. 907
+Integrated Avionics Processor System (IAPS) – Component Locationp. 909
Component Locationp. 909
+Integrated Card Cage (ICC) – Removal/Installationp. 911
Generalp. 911
Removalp. 911
Installationp. 914
+IAPS Environmental Controller (IEC) – Removal/Installationp. 917
Generalp. 917
Removalp. 917
Installationp. 920
+IAPS Environmental Controller (IEC) – Adjustment/Testp. 923
Generalp. 923
Operational Testp. 923
+Input/Output Concentrator (IOC) – Removal/Installationp. 925
Generalp. 925
Removalp. 925
Installationp. 928
+Input/Output Concentrator (IOC) – Adjustment/Testp. 931
Generalp. 931
Operational Testp. 931
+Power Supply Module – Removal/Installationp. 933
Generalp. 933
Removalp. 933
Installationp. 936
+Power Supply Module – Adjustment/Testp. 939
Generalp. 939
Operational Testp. 939
+Configuration Strapping Unit (CSU) – Maintenance Practicesp. 941
Generalp. 941
Configuration Settingp. 941
+Configuration Strapping Unit (CSU) – Removal/Installationp. 951
Generalp. 951
Removalp. 951
Installationp. 954
+Configuration Strapping Unit (CSU) – Adjustment/Testp. 957
Generalp. 957
Operational Testp. 957
+Option Control Module (OCM) – Removal/Installationp. 959
Generalp. 959
Removalp. 959
Installationp. 962
+Data Concentration System (DCS) – Component Locationp. 965
Component Locationp. 965
+Data Concentration System (DCS) – Adjustment/Testp. 967
Generalp. 967
Operational Testp. 967
+Data Concentrator Unit (DCU) – Removal/Installationp. 969
Generalp. 969
Removalp. 969
Installationp. 972
+Remote Data Concentrator Unit (RDC) – Removal/Installationp. 975
Generalp. 975
Removalp. 975
Installationp. 978
+Electronic Flight Instrument System (EFIS) – Component Locationp. 981
Component Locationp. 981
+Electronic Flight Instrument System (EFIS) – Adjustment/Testp. 985
Generalp. 985
Operational Testp. 985
+Adaptive Flight Display (AFD) – Maintenance Practicesp. 993
Generalp. 993
Creating USB Mediap. 993
Field Load Procedurep. 997
Periodic Database Field Load Procedurep. 1010
+Adaptive Flight Display (AFD) – Removal/Installationp. 1023
Generalp. 1023
Removalp. 1023
Installationp. 1026
+Adaptive Flight Display (AFD) – Adjustment/Testp. 1029
Generalp. 1029
Operational Testp. 1029
+Adaptive Flight Display (AFD) – Cleaning/Paintingp. 1035
Generalp. 1035
Cleaningp. 1035
+Cursor Control Panel (CCP) – Removal/Installationp. 1037
Generalp. 1037
Removalp. 1037
Installationp. 1039
+Cursor Control Panel (CCP) – Adjustment/Testp. 1041
Generalp. 1041
Operational Testp. 1041
+Multifunction Keypad Panel (MKP) – Removal/Installationp. 1043
Generalp. 1043
Removalp. 1043
Installationp. 1045
+Multifunction Keypad Panel (MKP) – Adjustment/Testp. 1047
Generalp. 1047
Operational Testp. 1047
+Aircraft Personality Module (APM) – Maintenance Practicesp. 1049
Generalp. 1049
Load the Aircraft Personality Module (APM)p. 1049
+Aircraft Personality Module (APM) – Removal/Installationp. 1059
Generalp. 1059
Removalp. 1059
Installationp. 1062
+Baro Single Knob Panel – Removal/Installationp. 1065
Generalp. 1065
Removalp. 1065
Installationp. 1067
+Emulated Control Display Unit (ECDU) – Adjustment/Testp. 1069
Generalp. 1069
Operational Testp. 1069
+34 NAVIGATIONp. 1073
+Air Data System (ADS) – Component Locationp. 1075
Component Locationp. 1075
+Air Data Computer (ADC) – Removal/Installationp. 1077
Generalp. 1077
Removalp. 1077
Installationp. 1080
+Air Data Computer (ADC) – Adjustment/Testp. 1083
Generalp. 1083
Functional Testp. 1083
+Attitude Heading Reference System (AHRS) – Component Locationp. 1097
Component Locationp. 1097
+Attitude Heading Computer (AHC) – Removal/Installationp. 1099
Generalp. 1099
Removalp. 1099
Installationp. 1102
+Attitude Heading Computer (AHC) – Adjustment/Testp. 1105
Generalp. 1105
Functional Testp. 1105
+Flux Detector Unit (FDU) – Removal/Installationp. 1115
Generalp. 1115
Removalp. 1115
Installationp. 1118
+External Compensation Unit (ECU) – Removal/Installationp. 1121
Generalp. 1121
Removalp. 1121
Installationp. 1124
+External Compensation Unit (ECU) – Adjustment/Testp. 1127
Generalp. 1127
Operational Testp. 1127
+Attitude Heading Reference System (AHRS) – Adjustment/Testp. 1129
Generalp. 1129
Compass Swingp. 1129
+Synthetic Vision Systemp. 1137
Generalp. 1137
Operational Testp. 1137
+Weather Radar System – Component Locationp. 1143
Component Locationp. 1143
+Weather Radar System – Adjustment/Testp. 1145
Generalp. 1145
Operational Testp. 1145
+Tilt Single Knob Panel – Removal/Installationp. 1153
Generalp. 1153
Removalp. 1153
Installationp. 1155
+Weather Radar Receiver/Transmitter Antenna (RTA) – Removal/Installationp. 1159
Generalp. 1159
Removalp. 1159
Installationp. 1162
+Weather Radar Receiver/Transmitter Antenna (RTA) – Adjustment/Testp. 1167
Generalp. 1167
Adjustment Testp. 1167
+Weather Radar Receiver/Transmitter Antenna (RTA) – Visual Inspectionp. 1173
Generalp. 1173
Visual Inspectionp. 1173
+Radio Altimeter System – Component Locationp. 1177
Component Locationp. 1177
+Radio Altimeter System – Adjustment/Testp. 1179
Generalp. 1179
Operational Testp. 1179
+Radio Altimeter Transceiver – Removal/Installationp. 1181
Generalp. 1181
Removalp. 1181
Installationp. 1183
+Traffic Alert and Collision Avoidance System (TCAS) II – Component Locationp. 1185
Component Locationp. 1185
+Traffic Alert and Collision Avoidance System (TCAS) II – Adjustment/Testp. 1187
Generalp. 1187
Operational Testp. 1187
+TCAS Transmitter/Receiver – Removal/Installationp. 1193
Generalp. 1193
Removalp. 1193
Installationp. 1195
+TCAS Directional Antenna – Removal/Installationp. 1197
Generalp. 1197
Removalp. 1197
Installationp. 1198
+Global Navigation Satellite System (GNSS) – Component Locationp. 1203
Component Locationp. 1203
+Global Navigation Satellite System (GNSS) – Adjustment/Testp. 1205
Generalp. 1205
Operational Testp. 1205
+Global Positioning System (GPS) Receiver – Removal/Installationp. 1211
Generalp. 1211
Removalp. 1211
Installationp. 1214
+VHF Navigation System – Component Locationp. 1217
Component Locationp. 1217
+VHF Navigation System – Adjustment/Testp. 1219
Generalp. 1219
Operational Testp. 1219
+VHF Navigation Unit – Removal/Installationp. 1227
Generalp. 1227
Removalp. 1227
Installationp. 1230
+VHF Navigation Unit – Adjustment/Testp. 1233
Generalp. 1233
Operational Testp. 1233
+Automatic Direction Finder (ADF) Antenna – Removal/Installationp. 1239
Generalp. 1239
Removalp. 1239
Installationp. 1242
+Distance Measuring Equipment (DME) – Component Locationp. 1245
Component Locationp. 1245
+Distance Measuring Equipment (DME) – Adjustment/Testp. 1247
Generalp. 1247
Functional Testp. 1247
+Distance Measuring Equipment (DME) Transceiver – Removal/Installationp. 1255
Generalp. 1255
Removalp. 1255
Installationp. 1258
+Air Traffic Control (ATC) Transponder System – Component Locationp. 1261
Component Locationp. 1261
+Diversity Transponder – Removal/Installationp. 1263
Generalp. 1263
Removalp. 1263
Installationp. 1266
+Diversity Transponder – Adjustment/Testp. 1269
Generalp. 1269
Operational Testp. 1269
+Flight Management System (FMS) – Maintenance Practicesp. 1289
Generalp. 1289
Load the FMS Search and Rescue Encrypted Application Key (EAK)p. 1289
Load the FMS System Applicationp. 1290
+Flight Management System (FMS) – Adjustment/Testp. 1293
Generalp. 1293
Operational Testp. 1293
+44 CABIN SYSTEMSp. 1299
+Video Surveillance System – Maintenance Practicesp. 1301
Generalp. 1301
Load the Video Surveillance Encrypted Application Key (EAK)p. 1301
+45 CENTRAL MAINTENANCE SYSTEMp. 1303
+Onboard Maintenance System (OMS) – Maintenance Practicesp. 1305
Generalp. 1305
Access the Onboard Maintenance System (OMS) Pagesp. 1305
Access the Onboard Maintenance System (OMS) Maintenance Reports Functionp. 1307
Access the Onboard Maintenance System (OMS) Utility Functionsp. 1309
Load the Onboard Maintenance System Application (OMSA)p. 1311
Load the Onboard Maintenance System Table (OMST)p. 1311
Load the Onboard Data Loader Application (ODLA)p. 1312
+46 SYSTEMS INTEGRATION AND DISPLAYp. 1315
+Integrated Flight Information System – Maintenance Practicesp. 1317
Generalp. 1317
Enable the Data Link Weather Encrypted Application Key (EAK)p. 1317
Activate the Electronic Charts Encrypted Application Key (EAK)p. 1318
Enable the Enhanced Maps Overlay Encrypted Application Key (EAK)p. 1320
Enable the Outboard IFIS Encrypted Application Key (EAK)p. 1322
Enable the Chart Extension Encrypted Application Key (EAK)p. 1323
Activate the Electronic Charts Subscriptionp. 1325
+Integrated Flight Information System – Adjustment/Testp. 1327
Generalp. 1327
Operational Testp. 1327
+XM Weather – Component Locationp. 1333
Component Locationp. 1333
+XM Weather – Maintenance Practicesp. 1335
Generalp. 1335
Enable the XM Weather Encrypted Application Key (EAK)p. 1335
Activate the XM Weather Subscriptionp. 1337
Refresh the XM Weather Subscriptionp. 1338
+XM Weather – Adjustment/Testp. 1341
Generalp. 1341
Operational Testp. 1341
+XM Weather Receiver – Removal/Installationp. 1345
Generalp. 1345
Removalp. 1345
Installationp. 1348
+Information Management System (IMS) – Component Locationp. 1351
Component Locationp. 1351
+Information Management System (IMS) – Maintenance Practicesp. 1353
Generalp. 1353
Aircraft and IMS Configuration Check – AscendTMp. 1353
Subscribe to the Aircraft Information Manager (AIM) Service – AscendTMp. 1358
Configure Wireless LAN and Cellular – AscendTMp. 1362
Download Aircraft Information Manager (AIM) Media Sets – Ascendp. 1368
IMS Interlock Testp. 1374
Manage Wireless LAN Connection – AscendTMp. 1379
+Information Management System (IMS) – Adjustment/Testp. 1381
Generalp. 1381
Operational Testp. 1381
+Information Management System (IMS) Unit – Maintenance Practicesp. 1387
Generalp. 1387
Loading of the Information Management System Operating System (IMSOS) Softwarep. 1387
Loading of the Information Management System Application (IMSA) Softwarep. 1394
Manage the Information Management System (IMS) Unit – AscendTMp. 1401
+Information Management System (IMS) Unit – REMOVAL/INSTALLATIONp. 1403
Generalp. 1403
Removalp. 1403
Installationp. 1406
BACK COVERp. 1410
What This Rockwell Collins Pro Line Fusion for King Air Manual Gives You
With this Pro Line Fusion for King Air Aircraft Maintenance Manual on hand, a technician can identify every avionics LRU by Rockwell Collins part number, understand how the Flight Guidance System, EFIS, FMS, and related subsystems operate together, and follow the manufacturer’s own removal, installation, adjustment, and test steps for each unit — the kind of correct, system-specific procedure and specification data that generic references can’t provide. Because the manual is organized around the actual ATA/AMTOSS chapter structure used across the C90GTi, B200GT, B200CGT, B300, and B300C, it lets you cross-reference a single fault or component across the whole Pro Line Fusion product line. This Rockwell Collins Pro Line Fusion for King Air Aircraft Maintenance Manual downloads instantly as a PDF — no shipping, no waiting — and can be viewed, searched, or printed from a laptop, tablet, or phone in the hangar or workshop.
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