MDC , 402, 403, -404, -405 Display Control Panel DCP , 104, 106, -204, 206 Electronic Flight Display (PFD, MFD)
|
|
|
- Shana Armstrong
- 5 years ago
- Views:
Transcription
1 COURSE TITLE: Pro Line 4 Bombardier Challenger CL-604 Level I Operations & Flightline Maintenance EQUIPMENT TYPE: EQUIPMENT NOMENCLATURE PART NUMBER IAPS Card Cage ICC IAPS Power Supply PWR I/O Concentrator IOC , 702, 703, -704, -705 Configuration Strapping Unit CSU Configuration Strapping Unit CSU Option Control Module OCM , -212, -214, IAPS Environmental Controller IEC Lightning/HIRF Protection (Left) Lightning/HIRF Protection (Right) Maintenance Diagnostic Computer LHP , 702 LHP , 702 MDC , 402, 403, -404, -405 Display Control Panel DCP , 104, 106, -204, 206 Electronic Flight Display (PFD, MFD) EFD , 304, -306, 308, -310, -312 EICAS Data Concentrator Unit DCU , 002, 003, -013 EICAS Control Panel ECP , -102 EICAS Routing Unit ERU Electronic Flight Display (ED) EFD , 304, -306, - 308, 310, -312 Lamp Driver Unit LDU Air Data Computer ADC 850E , 142, -421 July 2,
2 Air Data Reference Panel ARP , 006, 104, -106 Control Display Unit CDU , 004, 006, -008 Flight Management Computer (in IAPS) Data Base Unit (DSDD Disk Drive) Flight Control Computer (in IAPS) FMC , 004, 010, -029 DBU 4100 * , 004, 006, -008 FCC , 110, 210, -310 Flight Control Panel FCP Primary Servo (aileron) SVO 85A , 101 Primary Servo (elevator) SVO 85B , 101 Linear Actuator (rudder) SVL Servo Switching Module SSM Radio Tune Unit RTU , 122, 124 VHF Comm Transceiver VHF 422B , 121 VHF Comm Transceiver VHF-422C VHF Navigation Receiver VIR DME Transceiver DME Radio Altimeter ALT 55B Radio Altitude Converter RAC Mode S Transponder TDR 94D , 004 TCAS II Receiver Transmitter TTR TCAS II Receiver Transmitter TTR TCAS II Antenna TRE HF Receiver/Transmitter HF 9031A HF Antenna Coupler HF Audio Control Panel ACP , -030 Remote Electronics Unit REU GPS Navigation Receiver GPS , 002 July 2,
3 Receiver/Transmitter/Antenna (14 inch) RTA Weather Radar Control Panel WXP HGS Combiner Combiner HGS Control Panel HCP HGS Computer HC HGS Drive Electronics Unit DEU HGS Over Head Unit OHU Satellite Data Unit SDU-906-4, , Radio Frequency Unit RFU High Power Amplifier HPA-901A SATCOM Receiver/Transmitter SRT , , Intermediate Gain Antenna IGA Lightning Detection System WX 1000E , 020 July 2,
4 PREREQUISITES: Students should have basic knowledge of aircraft avionics systems and a working command of the English language (interpreters are available for special cases). PURPOSE: This course provides line maintenance personnel with training to operate and perform flightline maintenance for the Proline 4 system. OBJECTIVES: Upon completing this course, the student will be able to: 1. Provide an overall understanding of Proline 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: 5 Days TRAINING DEVICES: CL604 Test Rig TRAINING MATERIALS: 1. PowerPoint Presentation with LCD projector 2. Information sheets 3. Student Training Guide REFERENCES: 1. Bombardier Challenger 604 Avionics System Manual Pilot s Guide For The Challenger 604 Collins Pro Line 4 Avionics System Bombardier Challenger 604 Avionics Diagnostic Guide July 2,
5 PRO LINE 4 BOMBARDIER CHALLENGER CL-604 COURSE OUTLINE I. Welcome A. Training Overview (Customer Ambassador) 1. Welcome 2. Student Registration 3. Student Policies and Procedures II. Introduction to Materials and Handouts A. System manual introduction and use B. Test and troubleshooting guide introduction C. Equipment Description D. Equipment Specifications 1. Business & Regional Systems Equipment Leading Particulars III. Data Bus A. Why we use Data Buses B. Arinc Data Buses 1. Arinc Arinc 453 C. CSDB Data Buses IV. Integrated Avionics Processing System (IAPS) A. Over view B. System architecture C. Integrated Card Cage (ICC) D. Lightning/HIRF protection (LHP) July 2,
6 E. Power supply module (PWR) F. IAPS environmental controller (IEC) G. Input output concentrator (IOC) H. Maintenance Diagnostic Computer (MDC) I. Configuration strapping unit (CSU) J. Detailed functional theory 1. IAPS power distribution 2. Temperature monitoring 3. Overheat reporting 4. Power supply inhibit 5. CSU detailed theory K. Maintenance and troubleshooting 1. PWR fault indications 2. IEC fault indications 3. Status messages 4. Diagnostics V. Maintenance Diagnostics B. Maintenance Diagnostic Computer (MDC) July 2,
7 VI. Electronic Flight Instrument System (EFIS) B. Electronic Flight Display (EFD) 1. Primary Flight Display (PFD) 2. Multifunction Display (MFD) a. MFD formats 3. EFD Detailed Theory of operation a. Reversionary mode select b. Cooling requirements C. Display Control Panel (DCP) 1. DCP switchology description 2. Detailed theory of operation VII. Engine Indicating and Crew Alerting System (EICAS) B. Electronic Flight Display (EFD)/EICAS Display (ED) 1. Primary ED 2. Secondary ED C. Secondary ED 1. Display formats D. EICAS Control Panel (ECP) 2. ECP switchology description 3. Detailed theory of operation E. Data Concentrator Unit (DCU) 2. Integration theory 3. Theory of operation F. EICAS Routing Unit (ERU) G. Lamp Driver Unit July 2,
8 H. Maintenance and troubleshooting 1. Status messages 2. Diagnostics VIII. Air Data System (ADS) B. Air Data Computer C. Air Reference Panel (ARP) 2. ARP switchology description 3. Theory of operation D. Maintenance and troubleshooting 1. Status message 2. Diagnostics IX. Flight Control System (FCS) B. Flight Control Computers (FCC) C. Servo Switching Modules (SSM) a. AFCS selection D. Flight Control Panel (FCP) 2. FCP switchology description 3. Theory of operation E. Primary Servo (SVO) F. Servo Linear Actuator (SVL) July 2,
9 G. Yaw Damper Engage Panel (YDEP) 2. Operation 3. Theory of operation H. Autopilot and yaw damp detailed theory of operation of fail passive system 2. Description of null seeking servo loops 3. Description of yaw damp system I. Autopilot diagnostics 1. Entering and using autopilot diagnostics a. Input mode b. Output mode c. Report Mode 2. Servo Spin test 3. Linear actuator test X. Flight Management System (FMS) B. Flight Management Computer (FMC) C. Control Display Unit (CDU) D. Data Base Unit (DBU) E. Flight Management Data Base operations day database load procedure 2. Fault history download procedure XI. Radio Sensor System (RSS) B. Radio Tuning Unit (RTU) July 2,
10 2. Operation 3. Theory of operation C. VHF Comm receiver/transmitter (VHF) D. VOR/ILS/MB Receiver (VIR) E. Distance Measuring Equipment (DME) F. Automatic Direction Finder receiver (ADF) G. High Frequency receiver/transmitter (HF) H. HF Antenna Coupler I. Radio Altimeter (ALT) and Radio Altimeter Converter (RAC) J. Mode S transponder (TDR-94D) with Traffic Alert and Collision Avoidance System (TCAS) 3. Video presentation (TCAS 2 operations with change 7.0) K. General Maintenance Procedures for Comm /Nav /Pulse Equipment 1. Flight line diagnostic procedures 2. Antenna maintenance considerations XII. Weather Radar (WXR) B. Microwave Radiation Hazards 1. AC 20-68B July 2,
11 C. Weather radar theory 1. Mediums that reflect 2. Turbulence detection and ground clutter suppresion D. Receiver Transmitter Assembly (RTA-8xx) E. Maintenance 1. Radome maintenance (AC 43-13) 2. Flight line diagnostic procedures XIII. Head Up Guidance System (HGS) B. Combiner Element C. HGS Computer (HC) D. HGS Drive Electronics Unit (DEU) E. HGS Over Head Unit (OHU) F. HGS Control Panel (HCP) G. HGS Diagnostics 1. HCP Test menu 2. Fault Code interpretation July 2,
12 XIV. Satellite Communication System (SATCOM) B. Video Presentation (What is SATCOM?) C. SAT 906 System 1. Component description D. Sat 5000 System 1. Component description E. Sat 6000 System 1. Component description XV. Dataloading A. Data loading Procedures 1. PCD 2. DBU XVI. Critique/Review July 2,
Publications and Training Solutions Course Syllabus:
COURSE TITLE: PROLINE 4 CRJ 700/900 Level I Operators & Flightline Maintenance PREREQUISITES: 1. Students should have basic knowledge of aircraft avionics systems and a working command of the English language
Publications and Training Solutions Course Syllabus:
COURSE TITLE: Pro Line 21 Advanced Bombardier Challenger 300/350 Combo, Level I Operations & Flightline Maintenance PREREQUISITES: Students should have basic knowledge of aircraft avionics systems and
Publications and Training Solutions Course Syllabus:
COURSE TITLE: Pro Line 21 King Air C90GTi Level I Operations & Flightline Maintenance EQUIPMENT TYPE: EQUIPMENT NOMENCLATURE PART NUMBER IAPS Card Cage ICC 3000 822-1129-001 IAPS Environmental Controller
Publications and Training Solutions Course Syllabus:
COURSE TITLE: Pro Line 21 Lear 60XR Level I Operations & Flightline Maintenance EQUIPMENT TYPES: EQUIPMENT NOMENCLATURE PART NUMBER Integrated Card Cage ICC-3000 822-1129-001 IAPS Environmental Control
Level I Operator & Flightline Maintenance
COURSE TITLE: PRO LINE II (Generic) Level I Operator & Flightline Maintenance EQUIPMENT TYPES: LRU DSP-8X DCP-8X MFD-85X MPU-85 DPU-8X EFD-8X PRE-8XX VSI-8X ALI-8X ASI/MSI-8X ADC 81, -82, -8X AHC-85/85E
Publications and Training Solutions Course Syllabus:
COURSE TITLE: Pro Line II (Generic) Level I Operations & Flight Line Maintenance PREREQUISITES: Students should have basic knowledge of aircraft avionics systems and a working command of the English language
Publications and Training Solutions Course Syllabus:
COURSE TITLE: Bombardier Challenger 604 Pro Line Fusion PREREQUISITES: 1. Students should have basic knowledge of aircraft avionics systems and experience operating the Challenger 604. PURPOSE: This course
2009 Bombardier Challenger 300 S/N: Reg: T7-GOB
2009 Bombardier Challenger 300 S/N: 20255 Reg: T7-GOB 2009 Challenger 300 Serial Number: 20255 Reg: T7-GOB Airframe / Engines / APU Airframe: 4,877.46 Hours Since New / 2,972 Landings Since New (as
Publications and Training Solutions Course Syllabus:
COURSE TITLE: SATCOM (SAT-906, 2000, 2100) Operations & Flightline Maintenance PREREQUISITES: Students should have completed a two-year technical electronics school or have equivalent knowledge of aircraft
RADIO SYSTEM DESCRIPTION The radio system consists of the following equipment:
COMMUNICATION SYSTEM RADIO SYSTEM DESCRIPTION The radio system consists of the following equipment: Radio tuning function located in MFD s Dual CDU s (for tuning - shared with FMS) Two VHF communication
2007 BOMBARDIER CHALLENGER 605
2007 BOMBARDIER CHALLENGER 605 OVERVIEW AVIONICS Date of Manufacture: 10th January 2007 Entry Into Service: 22nd November 2007 EASA JAR OPS 1 Compliant One owner since new AIRFRAME Total Time: 2840 Hours
2007 bombardier challenger 605. serial number 5709 registration 9H-AFQ
2007 bombardier challenger 605 overview AVIONICS Date of Manufacture: 10th January 2007 Entry Into Service: 22nd November 2007 EASA JAR OPS 1 Compliant One owner since new AIRFRAME Total Time: 3022 Hours
BEECHCRAFT SUPER KING AIR B200 Model: 1998 Crew: 2 pilots Passengers: 7
BEECHCRAFT SUPER KING AIR B200 Model: 1998 Crew: 2 pilots Passengers: 7 AIRFRAME: 2996:09 Hours TSN Landings: 2314 ENGINES: Pratt & Whitney PW545A Left Engine: 2996:09 Hours TSN 2314 Cycles SN Right Engine:
Specifications are subject to verification by purchaser. Aircraft is subject to prior sale, and/or removal from market without notice.
1 ddobbins@mentegroup.com www.mentegroup.com 214.351.9595 2 ddobbins@mentegroup.com www.mentegroup.com 214.351.9595 3 ddobbins@mentegroup.com www.mentegroup.com 214.351.9595 4 ddobbins@mentegroup.com www.mentegroup.com
EMBRAER LEGACY 500 PRE-OWNED. Year Belted toilet. Atlas Air Service AG Hanna-Kunath-Str Bremen / Germany
PRE-OWNED EMBRAER LEGACY 500 Year 2015 Engine Type Total Hours Seating Honeywell AS907-3-1E ~ 1200 hrs. TSN 2 + 9 + Belted toilet AVIONICS Four 15.1-inch active matrix liquid crystal smart displays Dual
ST02893CH FAA Supplemental Type Certificate
ST02893CH FAA Supplemental Type Certificate Installation of a SATCOM System on Boeing 767 Series Aircraft (FAA STC ST02893CH) OVERVIEW FAA STC ST02893CH. Argentina Civil Aviation Administration STC 1205.18.
EE Chapter 14 Communication and Navigation Systems
EE 2145230 Chapter 14 Communication and Navigation Systems Two way radio communication with air traffic controllers and tower operators is necessary. Aviation electronics or avionics: Avionic systems cover
Sikorsky S-76C++ N722JE S/N
Sikorsky S-76C++ N722JE S/N 760750 Sikorsky S-76C++ N722JE S/N 760750 OFFERED AT: Make Offer Entry into Service: March 17 th, 2010 Executive Cabin Interior Iridium Phone System Cabin Soundproofing XM Satellite
Publications and Training Solutions Course Syllabus:
COURSE TITLE: Tailwind 500/550 Installation and Maintenance PREREQUISITES: 1. Familiarity with computers, DOS commands, and Windows Operating Systems 2. Basic understanding of electronics 3. Proficiency
Module 13 Aircraft Aerodynamics, Structures and Systems
13.1 Theory of Flight (a) Aeroplane Aerodynamics and Flight Controls Operation and effect of: roll control: ailerons and spoilers, pitch control: elevators, stabilators, variable incidence stabilisers
2016 Bombardier Global 6000
2016 Bombardier Global 6000 cbaviation.com/2015-bombardier-global-6000/ 10/21/2015 1/8 2/8 3/8 4/8 Asking Price: $49,900,000.00 USD Ser#: Reg#: CB Aviation is proud to bring this brand new 2016 Global
Engineering. Aim. Unit abstract. QCF level: 6 Credit value: 15
Unit T22: Avionic Systems Engineering Unit code: R/504/0134 QCF level: 6 Credit value: 15 Aim The aim of this unit is to provide learners with a detailed knowledge and understanding of a wide range of
GULFSTREAM G200 SN 005 RANGE (NM) 3400 PASSENGERS 8 MACH 0.85 CONTACT: MATT STRINGFELLOW I
MACH 0.85 PASSENGERS 8 RANGE (NM) 3400 AIRCRAFT LISTING DETAILS: Total Hours: 6712 AVIONICS: Collins Proline IV with 5-upgraded EFIS Tubes (10/17/2013) Collins ICC-4005 Integrated Avionics Processor Subsystem
Exhibit 1 - Product Description
Exhibit 1 - Product Description SRT-2000 The SAT-2000 Satellite Communications System, an all solid-state aircraft earth station (AES) that operates as part of the SATCOM system, is designed to be compatible
Fokker 50 - Automatic Flight Control System
GENERAL The Automatic Flight Control System (AFCS) controls the aircraft around the pitch, roll, and yaw axes. The system consists of: Two Flight Directors (FD). Autopilot (AP). Flight Augmentation System
2010 EMBRAER LINEAGE 1000
HIGHLIGHTS AIRFRAME Engines on GE Onpoint No Damage History ADS-B Upgraded Fresh 96 Month Inspection Will Deliver With; Crew Training EASA / Isle of Man Certification Post Delivery; FANS-1/A & CPDLC Upgrade
Communication and Navigation Systems for Aviation
Higher National Unit Specification General information for centres Unit title: Communication and Navigation Systems for Aviation Unit code: F0M3 35 Unit purpose: This Unit is designed to allow candidates
NAVIGATION INSTRUMENTS - BASICS
NAVIGATION INSTRUMENTS - BASICS 1. Introduction Several radio-navigation instruments equip the different airplanes available in our flight simulators software. The type of instrument that can be found
CHAPTER AIRPLANE GENERAL
Table of Contents Vol. 1 18--00--1 CHAPTER 18 --- AIRPLANE GENERAL TABLE OF CONTENT Page TABLE OF CONTENT 18-00 Table of Contents 18--00--1 INTRODUCTION 18-10 Introduction 18--10--1 FLIGHT MANAGEMENT YTEM
CHAPTER NAVIGATION SYSTEMS
18--00--1 NAVIGATION SYSTEMS Table of Contents REV 3, May 03/05 CHAPTER 18 --- NAVIGATION SYSTEMS Page TABLE OF CONTENTS 18-00 Table of Contents 18--00--1 INTRODUCTION 18-10 Introduction 18--10--1 FLIGHT
Head-Up Guidance System. HGS Pilot Guide for the Bombardier CRJ 700
Head-Up Guidance System HGS Pilot Guide for the Bombardier CRJ 700 Registration Notice HGS is a registered trademark of Rockwell Collins Flight Dynamics Proprietary Notice The information contained in
THEORY AND HANDS-ON TRAINING IN AVIONICS
Training catalog 2019 THEORY AND HANDS-ON TRAINING IN AVIONICS Develop your skills on our avionics products and systems 2 TRAINING CONTENTS Training Center.................. 3 Presentation of courses.............4
Description MFG P/N S/N STC Captains Instruments Audio Panel Autech 6608213-3 (2050-1) 175 ADI 84A Indicator Collins 622-3594-003 4 HSI Indicator Collins 622-4151-003 19 Emergency Gyro Jet 501-1105-04
AIRCRAFT AVIONIC SYSTEMS
AIRCRAFT AVIONIC SYSTEMS B-777 cockpit Package C:\Documents and ettings\administrato Course Outline Radio wave propagation Aircraft Navigation Systems - Very High Omni-range (VOR) system - Instrument Landing
CALL GULFSTREAM III PARTS FOR SALE
CALL 386-341-0423 GULFSTREAM III PARTS FOR SALE Part Number Serial Number Bleed Air Control 8606 38201 ANTENNA 10706 9757 ANTENNA 10706 9758 Ignition Exciter 43663 2149 Indidcator Dual Temperature 253682
Cockpit Voice Recorder Intelligibility Analysis Flight Test Procedures
Registration: Serial #: Model: Date: Important Note To Flight Crew The procedures detailed in this report are intended to demonstrate that the CVR records the required information. Failure to follow each
General. VHF Communications System. HF Communications System
Comm.10 Communications-Description and Operation General The MD-11communications system consists of the following: VHF communications system. HF communications system. Communication Radio Panels (CRP).
AIRPLANE FLIGHT MANUAL AQUILA AT01. Date of Issue A.01 Initial Issue (minor change MB-AT ) all March
0.1 LIST OF REVISIONS AND AMENDMENTS Revision Reason for Amendment/Revision Affected Pages Date of Issue A.01 Initial Issue (minor change MB-AT01-00297) all 2009 19. March 0.2 LIST OF EFFECTIVE PAGES Page
A-VIATOR (AP68TP-600) STANDARD EQUIPMENT LIST
A-VIATOR (AP68TP-600) STANDARD EQUIPMENT LIST V13.04.16 IMPORTANT NOTE: this document is a general description of the aircraft equipment only. It is not a technical document and is to be used only for
MINIMUM EQUIPMENT LIST OPERATIONAL PROCEDURES ATA 34 NAVIGATION F100 ATA 34/ NAVIGATION CAA-01 ATA 34
1 of 12 ATA 34/ NAVIGATION 2 of 12 11-1 Static ports Dispatch with ports at one side inoperative Take-off: With the static ports capped at one side, compensation for slip and crosswind conditions (take-off
Official Journal of the European Union L 298/75
16.11.2011 Official Journal of the European Union L 298/75 A3 A4 B1.3 B1.4 Electronic library system; Printing; Structure monitoring (damage tolerance monitoring). 12.19 Information Systems (ATA46) 1 2
Independent Position Determining
GENERAL Independent Position Determining 34-40: INDEPENDENT POSITION DETERMINING 1. General This section covers that portion of the system which provides information to determine position from sources
SUPPLEMENT REVISION CESSNA MODEL 182T
SUPPLEMENT REVISION CESSNA MODEL 182T NAV III AVIONICS OPTION - Serials 18281228 and 18281318 thru 18281868 and 18281870 thru 18281875 PILOTS OPERATING HANDBOOK AND AIRPLANE FLIGHT MANUAL REVISION 1 1
P/N 135A FAA Approved: 7/26/2005 Section 9 Initial Release Page 1 of 10
FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT FOR GARMIN GNS 430 - VHF COMM/NAV/GPS Serial No: Registration No: When installing the Garmin GNS 430 - VHF COMM/NAV/GPS in the Liberty Aerospace XL2, this
Training contents. General Courses. Equipment Courses. System Courses. Information. Training Center 3 Presentation of courses 4
Training 2018 Training contents Training Center 3 Presentation of courses 4 General Courses Basic Principles in Avionics 5 Radio Communication 6 Radio Communication Concepts 7 Airborne Radio Communication
Rockwell Collins Vhf 4000 Manual READ ONLINE
Rockwell Collins Vhf 4000 Manual READ ONLINE If looking for a book Rockwell collins vhf 4000 manual in pdf format, then you've come to the faithful website. We present the utter release of this ebook in
Master Parts Inventory
ID Nomenclature Part Alternate P/N Manufacturer 44 Automatic Annunicator 103500 Sunstrand MTA 554 47 Tape Reproducer 108002 0004JL 980 9000 004 Sundtrand 201AACB 97 Tape Reproducer 108002 0004JL 980 9000
If yes, details, including whether internal or external, the size & if tethered. Internal, tehered
3 Safety equipment Epiry (mm/yy) number Yes No 3.1 Recognition lights Strobe lights 3.2 Fire etinguisher, with pressure gauge 25.11.2014 2 3.3 First aid kit 06.03.2015 2 3.4 Life jackets, one per occupant
GIA 64 Installation/User Guide
GIA 64 Installation/User Guide OEMs should obtain the most recent copy of the Installation Guide or Manual documents prior to equipment, configuration, installation and/or use. DRAFT Contents 1. Overview...
NAVIGATION AND PITOT-STATIC SYSTEMS
NAVIGATION AND PITOT-STATIC SYSTEMS. GENERAL This chapter describes the navigation systems, units, and components which provide airplane navigational information. Included are pitot-static, gyros, compass,
Flight Management, Navigation Chapter 11
Flight Management, Navigation Chapter 11 Controls and Indicators Section 10 11.10 Flight Management, Navigation-Controls and Indicators Flight Management System Control Display Unit (CDU) [Option Liquid
LISTA DE CAPACIDADE JET AVIONICS EQUIPAMENTOS AERONÁUTICOS LTDA
1 ITEM FABRICANTE DESCRICAO MODELO PART NUMBER LIMITAÇÃO 1 ACK ALTITUDE ENCODER A-30 A-30 REPARO 2 ACK ELT E-01-( ) E-01-( ) R/I; T/I 3 AERO MECHAN ALTITUDE ALERTER AM-275 AM-275 REPARO 4 AERONETICS DUAL
G1000TM. audio panel pilot s guide
G1000TM audio panel pilot s guide Record of Revisions Revision Date of Revision Revision Page Range Description A 12/01/04 6A-1 6A-17 Initial release. Garmin G1000 Audio Panel Pilot s Guide 190-00378-02
10 Secondary Surveillance Radar
10 Secondary Surveillance Radar As we have just noted, the primary radar element of the ATC Surveillance Radar System provides detection of suitable targets with good accuracy in bearing and range measurement
INSTRUCTOR REVIEW GUIDE LESSON N4SYS-17_IGR 1.5 HOURS AVIONICS SYSTEMS REVIEW
Lecture Discussion 1 INSTRUCTOR REVIEW GUIDE LESSON N4SYS-17_IGR 1.5 HOURS AVIONICS SYSTEMS REVIEW Class Preparation Instructional Aids Aircrew Operating Handbook Volume 2.1 Aircraft Systems for the C-146A
Publications and Training Solutions Course Syllabus:
COURSE TITLE: CabinConnect TM System (for Norwegian Air Shuttle). PREREQUISITES: 1. Students should have an avionics background, a working knowledge of aircraft avionic systems and troubleshooting techniques,
Sigma-Tek 1U Radio Control Panel Operator s Manual
Sigma-Tek 1U619-001 Radio Control Panel Operator s Manual 86M069 TABLE OF CONTENTS 1.0 GENERAL...1 1.1 DESCRIPTION...1 1.2 THEORY OF OPERATION...2 2.0 VHF COMMUNICATION MODULES...7 2.1 OPERATING PROCEDURE...8
2A Page 1 May 30/02 COMMUNICATIONS. 2A-23-10: General PRODUCTION AIRCRAFT SYSTEMS OPERATING MANUAL
COMMUNICATIONS 2A-23-10: General The communications system for the Gulfstream IV, shown in Figure 1, provides the flight crew with a means of communicating with ground stations and other aircraft using
Dash8 - Q400 - Autoflight
12.3.1 Introduction The Automatic Flight Control System (AFCS), provides fail-safe operation of flight director guidance, autopilot, yaw damper and automatic pitch trim functions. 12.3.2 General The Automatic
Technology Considerations for Advanced Formation Flight Systems
Technology Considerations for Advanced Formation Flight Systems Prof. R. John Hansman MIT International Center for Air Transportation How Can Technologies Impact System Concept Need (Technology Pull) Technologies
Bendix King Allied Signal Installation Manuals
Bendix King Allied Signal Installation Manuals If you are searched for the ebook Bendix king allied signal installation manuals in pdf format, in that case you come on to correct site. We presented full
KGX 150/130 ADS -B Certified Transceivers & Receivers
BendixKing By Honeywell 9201 -B San Mateo Blvd. NE Albuquerque, NM 87113 U.S.A. CAGE: 6PC31 Telephone: 1-505 -903-6148 Telephone: 1-855 -250-7027 (Toll Free in U.S.A.) Web site: http://www.bendixking.com
G1000TM. audio panel pilot s guide
G1000TM audio panel pilot s guide Record of Revisions Revision Date of Revision Revision Page Range Description A 08/20/04 6A-1 6A-18 Initial release. Garmin G1000 Audio Panel Pilot s Guide 190-00378-01
Series III Avionics Pilot's Guide
Chelton Avionics Inc. A Chelton Group Company 6400 Wilkinson Drive Prescott, AZ 86305 U.S.A. 150-041074 Rev. B i Wulfsberg Electronics Division, located in Prescott, Arizona, designs and manufactures the
AIRFRAME Status as of November 13, 2007 Total Airframe Hours Since New : 60,488 Hours Total Airframe Cycles Since New : 26,881 Cycles
2715 Reynolda Road, Winston-Salem, NC 27106 USA Phone 1-336-722-1616 Fax 1-336- 722-1655 Admin@SkyQuestInternational.com www.skyquestinternational.com Aircraft Specifications AIRCRAFT Type and Model :
Rockwell Collins ADS-B Perspective Bangkok March 2005
Rockwell Collins ADS-B Perspective Bangkok March 2005 Arnold Oldach aoldach@rockwellcollins.com NOTICE: The contents of this document are proprietary to Rockwell Collins, Inc. and shall not be disclosed,
SD3-60 AIRCRAFT MAINTENANCE MANUAL - DESCRIPTION AND OPERATION (POST-MOD A8062)
SD3-60 AIRCRAFT MAINTENANCE MANUAL z AMM 55.0.0.0DME SYSTEM - DESCRIPTION AND OPERATION (POST-MOD A8062) 1. General A. The DME systems provides a visual indication of the distance, in nautical miles, the
G U L F S T R E A M G S / N 1 4 6
MAX CRUISE SPEED 470 ktas PASSENGERS 8 RANGE (NM) 2,790 HIGHLIGHTS NEW CUSTOM PAINT IN PROCESS ENGINES & APU ENROLLED ON JSSI CUSTOM INTERIOR BY DUNCAN UPGRADED FMS W/ WAAS & LPV WI FI OVERVIEW Best G100
CIRRUS AIRPLANE MAINTENANCE MANUAL
UNIVERSAL ACCESS TRANSCEIVER. GENERAL This section covers the GDL UAT/ADS-B Transceiver. A. GDL UAT/ADS-B Transceiver - Serials w/ GDL The optionally installed GDL UAT/ADS-B Transceiver system consists
Dash8-200/300 - Automatic Flight AUTOMATIC FLIGHT CONTROLS AND INDICATORS. Page 1
AUTOMATIC FLIGHT CONTROLS AND INDICATORS FLIGHT GUIDANCE MODE SELECTORS (alternate action) - Engages flight director modes of operation. - Flight director command bars display lateral and/or vertical guidance
HAZARD AVOIDANCE. Displaying traffic on the Navigation Map. Displaying traffic information (PFD Inset Map):
HAZARD AVOIDANCE Displaying traffic on the Navigation Map 1) Ensure that the TAS system is operating. With the Navigation Map displayed, select the MAP Softkey. 2) Select the TRAFFIC Softkey. Traffic is
LOG OF REVISIONS Rev 1 RFMS, Eurocopter EC130 B4 G500H System. Page Date Number Description FAA Approved.
Revision Number LOG OF REVISIONS Page Date Number Description FAA Approved 1 05/15/2014 All Complete Supplement See page 1 190-01527-16 Rev 1 RFMS, Eurocopter EC130 B4 G500H System Page 2 of 25 FAA APPROVED
Services Information Ordering Procedure and Pool Locations... 1
Table of Contents Services Information Ordering Procedure and Pool Locations... 1 Exchange Services General Terms and Conditions... 3 Exchange Billing Procedures... 3 High Price Repair To Exchange Policy...
SECTION 2-19 AUTOPILOT
AIRPLANE SECTION 2-19 Block General...2-19-05...01 Automatic Flight Control System...2-19-05...02 Flight Guidance System...2-19-05...04 Flight Director...2-19-05...04 Autopilot...2-19-05...04 Flight Director
Heterogeneous Control of Small Size Unmanned Aerial Vehicles
Magyar Kutatók 10. Nemzetközi Szimpóziuma 10 th International Symposium of Hungarian Researchers on Computational Intelligence and Informatics Heterogeneous Control of Small Size Unmanned Aerial Vehicles
EMBRAER 135/145 Autopilot
EMBRAER 135/145 Autopilot GENERAL The Primus 1000 (P-1000) Automatic Flight Control System (AFCS) is a fully integrated, fail passive three-axis flight control system which incorporates lateral and vertical
Fundamentals of HF Data Link
Fundamentals of HF Data Link 2014 Rockwell 2014 Collins. Rockwell Collins. Framework for Discussion General Overview Propagation The Ground Component Architecture HFDL Ground Station The Airborne Component
AT01 AIRPLANE FLIGHT MANUAL
Table of Contents Supplement AVE12 1. Section 1 General AVE12 3 2. Section 2 Operating Limitations AVE12 3 3. Section 3 Emergency Procedures AVE12 3 4. Section 4 Normal Procedures AVE12 4 5. Section 5
Train for Tomorrow...TODAY
Train for Tomorrow...TODAY AeroTrain Corp. Aircraftt Maintenance Training Products Powerplant Trainers Aircraft Systems Trainers Avionics & Instruments Trainers Computer Based Training Courseware Catalog
G1000 Integrated Flight Deck. Pilot s Guide
G1000 Integrated Flight Deck Pilot s Guide Copyright 2006-2011 Garmin Ltd. or its subsidiaries. All rights reserved. This manual reflects the operation of System Software version 0435.23 or later for
This document is an unpublished work. Copyright 2002, 2009 Honeywell International Inc. All rights reserved.
APPLICATION DASH NO. NEXT ASSY USED ON 018 965-1227 TITLE SHEET INDEX SHEET NO. TITLE SHEET 1 REVISIONS HISTORY 2 DOCUMENT 3 PRODUCTION - Release - 27 Jul 2009 09:17:23 MST - Printed on 08 Oct 2009 This
11 Traffic-alert and Collision Avoidance System (TCAS)
11 Traffic-alert and Collision Avoidance System (TCAS) INSTRUMENTATION 11.1 Introduction In the early nineties the American FAA stated that civil aircraft flying in US airspace were equipped with a Traffic-alert
F-104 Electronic Systems
Information regarding the Lockheed F-104 Starfighter F-104 Electronic Systems An article published in the Zipper Magazine # 49 March-2002 Author: Country: Website: Email: Theo N.M.M. Stoelinga The Netherlands
NAVIGATION (2) RADIO NAVIGATION
1 An aircraft is "homing" to a radio beacon whilst maintaining a relative bearing of zero. If the magnetic heading decreases, the aircraft is experiencing: A left drift B right drift C a wind from the
An Introduction to Airline Communication Types
AN INTEL COMPANY An Introduction to Airline Communication Types By Chip Downing, Senior Director, Aerospace & Defense WHEN IT MATTERS, IT RUNS ON WIND RIVER EXECUTIVE SUMMARY Today s global airliners use
HGS Model 5600 Pilot Guide
Head-Up Guidance System HGS Model 5600 Pilot Guide Dual HGS Installation Embraer 170/190 Registration Notice HGS is a registered trademark of Rockwell Collins. Proprietary Notice The information contained
Introduction...3. System Overview...4. Navigation Computer GPS Antenna...6. Speed Signal...6 MOST RGB Lines...6. Navigation Display...
Table of Contents E65 NAVIGATION SYSTEM Subject Page Introduction...............................................3 System Overview...........................................4 Components Navigation Computer.....................................
SA4550. Pilot s Guide Effectivity and Errata
SA4550 Pilot s Guide Effectivity and Errata Insert this update ahead of the cover page of the above referenced Pilot s Guide. The environmental categories in the Technical Specifications contained in Section
AP OLLO S L15M Audio Control Panel and Marker Beacon Receiver
SkyRentals INFO FOR VH-VMA Insert to SECTION 7 MODEL 182Q (1977) Audio Control Panel & Marker Receiver AP OLLO S L15M Audio Control Panel and Marker Beacon Receiver Audio Panel & Marker components 1A Apollo
Wulfsberg Electronics
Wulfsberg Electronics Nav/Com and Tactical Communications Products Table of Contents Table of Contents... 2 Contact List... 6 Section I: Wulfsberg FliteLine Nav/Com Products CVC-152 VHF Com Controls...
RECORD OF REVISIONS. Revisions to this Supplement are recorded in the following table.
Supplement D42L AFM RECORD OF REVISIONS Revisions to this Supplement are recorded in the following table. New or amended text will be indicated by a bold black vertical line in the left hand margin of
European Aviation Safety Agency. European Technical Standard Order. ED Decision 2016/013/R Annex II
European Aviation Safety Agency Date: 5.8.2016 European Technical Standard Order Subject: Next Generation Satellite Systems (NGSS) Equipment 1 Applicability This ETSO provides the requirements which Next
20283 STATE ROAD 7 SUITE 300 = BOCA RATON FL PHONE: (561) / (561)
20283 STATE ROAD 7 SUITE 300 = BOCA RATON FL 33498 PHONE: (561) 210-7951/ (561) 961-9399 WWW.JLMAIRCRAFTS.COM - EMAIL: JLMAVIATION@OUTLOOK.COM 2013 LINEAGE 1000E AIRFRAME: Airframe:... 255 Engines: General
Advisory Circular. U.S. Department of Transportation Federal Aviation Administration
U.S. Department of Transportation Federal Aviation Administration Advisory Circular Subject: Airworthiness Approval of Automatic Date: 11/07/12 AC No: 20-165A Dependent Surveillance - Broadcast (ADS-B)
AUTOMATIC FLIGHT CONTROL SYSTEM TABLE OF CONTENTS CHAPTER 4
TABLE OF CONTENTS CHAPTER 4 Page TABLE OF CONTENTS DESCRIPTION General Guidance Panel Autopilot System Autopilot Yaw Damper Autopilot Engage Autopilot Disengage PFD Annunciation Flight Director (FD) Flight
apply nose down control wheel force upon autopilot disconnect. Preflight system test has failed.
13.4 AFCS ALERTS System Status Annunciation System Status Annunciation The following alert annunciations appear in the AFCS System Status Annunciation on the PFD. Figure 13-5 AFCS System Status Annunciation
SIGMA TEK, INC. 1U /-003 COMM / NAV / DME / ATC RADIO CONTROL PANEL INSTALLATION MANUAL. Publication No. 86M072
SIGMA TEK, INC. 1U619-002/-003 COMM / NAV / DME / ATC CONTROL PANEL INSTALLATION MANUAL Publication No. 86M072 TABLE OF CONTENTS Section Title Page No. 1.0 General Information...1 1.1 Introduction...1
Inter- and Intra-Vehicle Communications
Inter- and Intra-Vehicle Communications Gilbert Held A Auerbach Publications Taylor 5* Francis Group Boca Raton New York Auerbach Publications is an imprint of the Taylor & Francis Croup, an informa business
NMEA Training Overview
NMEA Training Overview NMEA offers 4 classroom installer training courses Basic Marine Electronics Installer (MEI) Basic NMEA 2000 Network Installer Basic Marine Electronics Installer (MEI) Advanced NMEA
ADS-B Introduction Greg Dunstone
ADS-B Introduction Greg Dunstone Surveillance Program Lead, Airservices Australia SURVEILLANCE Basics Primary and Secondary radar Why do we need Surveillance? Why surveillance? Improved safety Reduced