Publications and Training Solutions Course Syllabus:
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1 COURSE TITLE: Pro Line 4 Learjet 60 Flight Line Maintenance PREREQUISITES: Students should have a basic knowledge of aircraft avionics systems and a working command of the English language. Students should be familiar with MS Windows based Operating Systems. PURPOSE: This course provides line maintenance personnel with training to operate and perform flight line maintenance for the Pro Line 4 system. OBJECTIVES: Upon completing this course, the student should be able to: 1. Provide an overall understanding of Pro Line 4 Avionics principles and operation. 2. Identify system components and the functional/operational characteristics of each Line Replaceable Unit (LRU). 3. Identify typical aircraft system interface/system architecture. 4. Perform fault isolation to a faulty LRU using built-in test diagnostics. COURSE LENGTH: 2 Hours 30 Minutes REFERENCES: 1. Learjet 60 Avionics System Manual Learjet 60 Avionics System Diagnostic Guide Collins Pro Line 4 Avionics System for the Learjet 60 Operator s Guide MCS-65/AHS-85/86 Compass Swing Procedure Test Program Rockwell Collins. All rights reserved. Page 1
2 COURSE OUTLINE 0. Introduction 1. Data Buses C. ARINC Data Buses i. Specifications ii. ARINC 429 iii. ARINC Instrument Display System (IDS) i. Primary Flight Display (PFD) ii. Multifunction Display (MFD) iii. Sensor Display Unit (SDU) iv. Sensor Display Driver (SDD) D. Summary Test 3. Integrated Avionics Processing System (IAPS) i. Integrated Card Cage (ICC) ii. IAPS Power Supply iii. Input/Output Concentrator (IOC) 2017 Rockwell Collins. All rights reserved. Page 2
3 D. Maintenance & Troubleshooting i. Power Supply ii. Environmental Control Card E. Summary/Test 4. Air Data System (ADS) i. Air Data Computer (ADC) ii. Air Data Reference Panel (ARP) iii. Signal Interface Adapter (SIA-850) 5. Attitude Heading System (AHS) i. Attitude Heading Computer (AHC) ii. Flux Detector Unit (FDU) iii. Internal Compensation Unit (ICU) 6. Compass Swing C. Compass Alignment Setup i. Pre-Alignment ii. During Alignment 2017 Rockwell Collins. All rights reserved. Page 3
4 1. Entered Results 2. Computer Results iii. Post-Alignment iv. Test Alignment 7. Flight Control System (FCS) i. Flight Control Computer (FCC) ii. Servo Motor (SVO) iii. Flight Control Panel (FCP) iv. Flight Control Switches D. FCC Diagnostics E. Summary/Test 8. Radio Sensor System (RSS) i. Radio Tuning Unit (RTU) ii. VHF Communication Transceiver iii. Navigation Receiver iv. Distance Measuring Equipment (DME) v. Automatic Direction Finder (ADF) vi. Radio Altimeter (ALT) vii. Radio Altimeter Converter (RAC) 2017 Rockwell Collins. All rights reserved. Page 4
5 viii. GPS Navigation Receiver ix. TCAS II Transmitter/Receiver D. Troubleshooting E. Summary/Test 9. Weather Radar System (WXR) i. Receiver/Transmitter Antenna (RTA) 10. Aircraft Data Acquisition System (ADAS) i. Data Acquisition Unit (DAU) 11. Troubleshooting 2017 Rockwell Collins. All rights reserved. Page 5
6 EQUIPMENT TYPE: EQUIPMENT NOMENCLATURE PART NUMBER Primary Flight Display EFD / 022 / 024 / 026 Multifunction Display MFD / 022 / 024 / 026 Sensor Display Unit SDU-640B Sensory Display Driver SDD-640A Integrated Card Cage ICC-851A Input/Output Concentrator IOC-851A / 202 / 203 / 205 / 206 / 220 / 221 / 222 / 223 / 233 IAPS Power Supply PWR-851A / 003 Air Data Computer ADC-850D / 133 Air Data Reference Panel ARP Signal Interface Adapter SIA Attitude Heading Computer AHC-85E Flux Detector Unit FDU Internal Compensation Unit ICU Flight Control Computer FCC-850A / 107 / 207 / 307 / 407 Servo Motor SVO-85B / 102 Radio Tuning Unit RTU-870C Radio Tuning Unit RTU-870F Rockwell Collins. All rights reserved. Page 6
7 EQUIPMENT NOMENCLATURE PART NUMBER VHF Comm Transceiver VHF-422A VHF Comm Transceiver VHF-422C Navigation Receiver VIR Distance Measuring Equipment Transceiver Automatic Direction Finder Receiver DME ADF Radio Altimeter ALT-55B / 011 Radio Altimeter Converter RAC Global Positioning System GPS Transponder TDR / 003 / 004 Transponder TDR-94D / 004 Transponder TDR TCAS II Transmitter/Receiver Receiver/Transmitter Antenna Receiver/Transmitter Antenna TTR / 120 / 420 RTA RTA Data Acquisition Unit DAU Rockwell Collins. All rights reserved. Page 7
Publications and Training Solutions Course Syllabus:
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Specifications and Summary. Cessna Citation CJ Cessna Citation CJ3 Serial Number 525B-0133, N233MM
Specifications and Summary Cessna Citation CJ3 2007 Cessna Citation CJ3 Serial Number 525B-0133, N233MM Guardian Jet, LLC 1445 Boston Post Road Guilford, Connecticut 06437 203-453-0800 203-453-4527 Fax
2007 Gulfstream G200 Serial Number: 174 Registration: N851SC
Specifications are subject to verification by Purchaser. All times and cycles are current through October 30, 2014. Airframe: Total Time: 1,081.4 Total Cycles: 576 Certification: FAR Part 91 (FAR Part
Aircraft Profile. Manufacturer` Piaggio Aerospace / Italy exclusive by NeBeSci, Inc.
Aircraft Profile Manufacturer` Piaggio Aerospace / Italy exclusive by NeBeSci, Inc. Series / Model P.180 Avanti II SN 3007 Year 2016 82 TTSN / 64 cyl as of June 2018 Location Italy one owner since new
1988 Gulfstream GIV N200LC S/N1067. Specifications and Summary
1988 Gulfstream GIV N200LC S/N1067 Specifications and Summary 1 1988 Gulfstream G-IV N200LC S/N 1067 OFFERED AT: $ 2,495,000 AIRCRAFT HIGHLIGHTS: OPERATED PART 135 AVAILABLE: Immediately STATUS: As of
2007 Hawker 850XP / N403CT
258818 / N403CT 8,630.8 Hours since New Collins ProLine 21 Avionics Engines Enrolled on MSP ATG-5000 WiFi Text and Talk ADSB-Out Landing Gear OH cw. December 2017 For more information, please contact:
NZQA unit standard version 2 Page 1 of 7. Apply knowledge of aircraft radio systems to the certification of aeronautical maintenance
Page 1 of 7 Title Apply knowledge of aircraft radio systems to the certification of aeronautical maintenance Level 6 Credits 30 Purpose This knowledge-based unit standard is one of a series intended for
2003 Beechcraft Premier I SN RB-74
SARASOTA I TAMPA I LOS ANGELES 2003 Beechcraft Premier I SN RB-74 MAX CRUISE S P E E D 426 Kts PASSENGERS 6 RANGE(NM) 1,072 AIRCRAFT LISTING DETAILS: Hours Since New: 2,012 Landings SinceNew: 1,790 HIGHLIGHTS:
2001 Challenger 604 N670CM S/N5488
2001 Challenger 604 N670CM S/N5488 Specifications and Summary 1445 BOSTON POST ROAD GUILFORD CONNECTICUT 06437 203-453-0800 WWW.GUARDIANJET.COM 1 2001, Challenger 604 N670CM S/N5488 OFFERED AT: $7,995,000
2002 Challenger 604 Bombardier
2002 Challenger 604 Bombardier Available for Lease Until October 15, 2012 September 27, 2010 Page 2 of 10 Aft Double Club, With High-Lo Conference Table Specifications and/or descriptions are provided
2014 Embraer Legacy 500 S/N
HIGHLIGHTS 750 HOUR AIRFRAME & ENGINE INSPECTION JULY 2018 AT EMBRAER, FT. LAUDERDALE, FL AIRFRAME TOTAL TIME SINCE NEW 677.5 Hours (as of May 2, 2018) TOTAL LANDINGS SINCE NEW 544 Landings ENTRY INTO
GULFSTREAM G280 N7HB S/N 2021
GULFSTREAM G280 N7HB S/N 2021 Specifications and Summary 1 2013 GULFSTREAM G280 N7HB S/N 2021 OFFERED AT: $15,950,000 Aircraft Highlights: Engines and APU enrolled on MSP Gold Airframe enrolled on Gulfstream
1990 CHALLENGER 601-3A N9771C S/N 5063
1990 CHALLENGER 601-3A N9771C S/N 5063 Specification and Summary 1 1990 CHALLENGER 601-3A N9771C S/N 5063 OFFERED AT: $1,700,000 AIRCRAFT HIGHLIGHTS: APU on MSP Gold Avionics on HAPP & CASP Flight Phone
2008 HAWKER 900XP Serial Number HA-0015 Registration C-GVMP
2008 HAWKER 900XP Serial Number HA-0015 Registration C-GVMP 2008 HAWKER 900XP Serial Number HA-0015 Registration C-GVMP TOTAL TIME: 2,816.4 LANDINGS: 1,501 ENGINES: Honeywell TFE731-50R-1H Honeywell MSP
ASTRA 1125 S/N 028. Left Engine: s/n P96107 Right Engine: s/n P96112 Engine Time Hours: 6785 Engine Time Hours: 6986
ASTRA 1125 S/N 028 AIRCRAFT INFORMATION: S/N: 028 Registration: N800ZZ Yr MFT: 1989 Airframe Total Time: 7105 Cycles: 5540 ENGINE AND APU: Engine Model: TFE 731 3C Engine Program: on MSP Left Engine: s/n