Developed for Training Purposes Only Maintenance Training Manual ABBREVIATIONS AND SYMBOLS EMBRAER ERJ-170 / 175 / 190 / 195 (GE CF34) ABBREVIATIONS / ELECTRICAL / ELECTRONIC & MECHANICAL SYMBOLS Copyright 2015 by EMBRAER – Empresa Brasileira de Aeronáutica S.A. All rights reserved. This document shall not be copied or reproduced in whole or in part, In any form or by any means without the express written Authorization of Embraer. The information, technical data, designs and drawings disclosed in this document are proprietary information of Embraer or third parties and shall not be used or disclosed to any third party without permission of Embraer FRONT MATTER This manual is issued by Embraer Customer Training and SHALL BE USED FOR TRAINING PURPOSES ONLY. The data contained herein, although its update to the revision date, does not replace or supersede the information contained in the Embraer ERJ-170/190 (GE CF34) airframe or engine maintenance manuals or other official publications. This Maintenance Training Manual (MTM) contains all necessary information to fulfill the needs as a printed/electronic publication to support the theoretical training activities in aircraft maintenance training. Where possible, duplication of information has been avoided, however, certain data may be repeated where it has been necessary to include such data to preserve the continuity of subject matter. This edition of the Maintenance Training Manual is based on the last version of Embraer Technical Publications. No further revisions will be added to this current issue, if printed. MANUAL STRUCTURE All manual contents are organized as follows: TITLE PAGE A title page with its identification as "Training Manual" and copyright information. FRONT MATTER BLOCK The purpose of the front matter block is to explain the way this manual is organized, and to inform which publications were used as source of information. TABLE OF CONTENT The table of content shows a list of relevant items/pages contained in the actual volume in an “Index” format. CHAPTER DESCRIPTION BLOCK The chapter description block has the technical information derived from the Embraer Technical Publications and follows the modularity concept, thus its contents may vary according to the course purpose (rating and the applicable training level). It is organized in a didactic manner to facilitate the learning process with rearranged sequence of the applicable sub-chapters. The body of each ATA chapter has a Title Page. For additional information concerning this manual, contact EMBRAER CUSTOMER TRAINING. Copyright 2014 by EMBRAER – Empresa Brasileira de Aeronáutica S.A. All rights reserved. This document shall not be copied or reproduced in whole or in part, In any form or by any means without the express written Authorization of Embraer. The information, technical data, designs and drawings disclosed in this document are proprietary information of Embraer or third parties and shall not be used or disclosed to any third party without permission of Embraer 2 Developed for Training Purposes Only Developed for Training Purposes Only DISCLAIMER The data and any other information contained herein (“Embraer Data”) are only and exclusive property of Embraer S.A. and they cannot be disclosed without the previous consent of Embraer S.A. The use of the Embraer Data is exclusive for the specific purpose of training which is merely informative and any other use of Embraer Data is expressly forbidden. Embraer does not represent or endorse the accuracy or reliability of any advice, opinion, statement, recommendation, guidance or any other information displayed or established herein. Nothing contained in this authorization shall be deemed to diminish or eliminate any right or remedy Embraer S.A may have at law or in equity. Developed for Training Purposes Only Developed for Training Purposes Only THIS PAGE INTENTIONALLY LEFT BLANK Copyright 2014 by EMBRAER – Empresa Brasileira de Aeronáutica S.A. All rights reserved. This document shall not be copied or reproduced in whole or in part, In any form or by any means without the express written Authorization of Embraer. The information, technical data, designs and drawings disclosed in this document are proprietary information of Embraer or third parties and shall not be used or disclosed to any third party without permission of Embraer 3 Developed for Training Purposes Only Developed for Training Purposes Only ABBREVIATIONS / ELECTRICAL / ELECTRONIC & MECHANICAL SYMBOLS Copyright 2014 by EMBRAER – Empresa Brasileira de Aeronáutica S.A. All rights reserved. This document shall not be copied or reproduced in whole or in part, In any form or by any means without the express written Authorization of Embraer. The information, technical data, designs and drawings disclosed in this document are proprietary information of Embraer or third parties and shall not be used or disclosed to any third party without permission of Embraer 4 Developed for Training Purposes Only Percent Plus or minus is less than is greater than Differential Degrees Degrees Celsius Degrees Fahrenheit Liter Ohm Microampere Ampere Aircraft Anti-Ice, Approach Idle Air/ Oil Autopilot Auto Throttle Auxiliary Power Unit Start Bus Contactor Auto Brake Control Module Absolute Value Alternating Current Aircraft Communication Addressing and Reporting System Aft Core Cowl, Active Clearance Control Actuator Control Electronics Aircraft Air Cycle Machine Aircraft Condition-Monitoring Function Alternating-Current Motor-Driven Pump Aircraft Condition Monitoring System Aircraft Classification Number Altitude Compensated Tilt Air-Cooled Oil Cooler Alternating Current Voltage Analogic/Digital Airworthiness Directive Air Data Application Air Data Computer ADF ADG ADI ADJ ADMS ADRAS ADS ADS-B ADSP AEO AETC AF AFCS AFH AFM AFT AGB AGCU AGL AGT A.h AICC AIL AIOP AIP AIPC ALC ALF ALT AM AMI AMLCD AMM AMS AMTOSS ANAC ANN ANR ANT Automatic Direction Finder Air Driven Generator Attitude Director Indicator Adjustment Aircraft Diagnostic and Maintenance System Aircraft Data Recovery and Analysis Software Air Data System, Automatic Dependent Surveillance Automatic Dependent Surveillance - Broadcast Air Data Smart Probe All Engines Operative AC Essential Transfer Contactor AICC Fuse Automatic Flight Control System Aircraft Flight Hours Airplane Flight Manual Afterward Accessory Gearbox Auxiliary Generator Control Unit Above Ground Level Agent Amp Hour Auxiliary Integrated Control Centre Aileron Actuator Input Output Processor Aeronautical Information Publication Aircraft Illustrated Parts Catalog Auxiliary Generator Line Contactor Aft Looking Forward Altitude Amplitude Modulation Airline Modifiable Information Active Matrix Liquid Crystal Display Aircraft Maintenance Manual Air Management System Aircraft Maintenance Task Oriented Support System Agência Nacional de Aviação Civil Annunciator Active Noise Reduction Antenna Copyright 2014 by EMBRAER – Empresa Brasileira de Aeronáutica S.A. All rights reserved. This document shall not be copied or reproduced in whole or in part, In any form or by any means without the express written Authorization of Embraer. The information, technical data, designs and drawings disclosed in this document are proprietary information of Embraer or third parties and shall not be used or disclosed to any third party without permission of Embraer Developed for Training Purposes Only SYMBOLS % +/< > ∆ ° °C °F ℓ Ω µA A A A/C A/I A/O A/P A/T ABC ABM ABS AC ACARS ACC ACE ACFT ACM ACMF ACMP ACMS ACN ACT ACOC ACV A/D AD ADA ADC 5 Developed for Training Purposes Only Angle of Attack Aircraft on Ground Airplane Operations Manual Automatic Pilot Aircraft Personality Module, Airport Planning Manual Approach Auxiliary Power Unit Advanced Range Aeronautical Radio Incorporated Aircraft Recovery Manual, Armed ATA Specification Breakdown Manual APU Start Contactor Avionics Standard Communication Bus (version D) Anti-Surge Control Valve Altitude Preselect Assembly Air Starter Valve Air Transport Association Air Traffic Control Air-Traffic Control-Radar Beacon-System Attendant Automatic Test Equipment Automatic-Terminal-Information Service Air Turbine Starter, Auto throttle System Attitude Automatic Takeoff Thrust Control System Attendant Automatic Auxiliary Auxiliary Generator Auxiliary Available Avionics Both Barometric Setting Barometric Altitude Battery Battery Contactor, Back Course BCD BCM BCS BCV BFE BFO BIC BIT BITE BLW BLWR BNC BOSC BPT BRG BRK BRT BSV BTC BTL BTM BTMS C C CAB CAN Cap CAS CAT CAT I, II, III, IIIa CB CBIT CBP CBT cc/h CCD CCDL CCP CCT Binary Coded Decimal Brake Control Module Brake Control System Brake Control Valve Buyer Furnished Equipment Beat Frequency Oscillator Bus Interface Controller Built-In Test Built-in Test Equipment Bellow Blower Bayonet Neil Concelman Bottom of Step Climb Break Power Transfer Bearing Brake Bright Brake Shutoff Valve Bus Tie Contactor Bottle Brake Temperature Monitor Brake Temperature Monitoring System Developed for Training Purposes Only AOA AOG AOM AP APM APP APU AR ARINC ARM ASBM ASC ASCB ASCV ASEL ASSY ASV ATA ATC ATCRBS ATDT ATE ATIS ATS ATT ATTCS ATTND AUTO AUX AUX GEN AUX AVAIL AVNX B B BARO BARO-ALT BATT BC Centigrade, Celsius, Capacitor Cabin Control Area Network Captain Crew Alerting System Category, Clear Air Turbulence Category, I, II, III, IIIa Operation Circuit Breaker Continuous Built-in Test Circuit Breaker Panel Computer-Based Training cubic centimeter per hour Cursor Control Device Cross Channel Data link Cockpit Control Panel Cockpit Control Transducer Copyright 2014 by EMBRAER – Empresa Brasileira de Aeronáutica S.A. All rights reserved. This document shall not be copied or reproduced in whole or in part, In any form or by any means without the express written Authorization of Embraer. The information, technical data, designs and drawings disclosed in this document are proprietary information of Embraer or third parties and shall not be used or disclosed to any third party without permission of Embraer 6 Developed for Training Purposes Only Counter clockwise Configuration Deviation List Compressor Discharge Pressure Control Display Unit Commercial Fan, Center Fuselage Carbon Fiber Composite Customer Furnished Equipment Controlled Flight into Terrain Code of Federal Regulations (USA) Centre of Gravity Channel Chronometer Climb Climb 1, 2 rating Centimeter Cubic Centimeter Central Maintenance Computer Central Maintenance Computer Module Central Maintenance Computer Module Command Communications Management Function Component Maintenance Manual Configuration Management System Communications Compartment Maximum Continuous rating Configuration Cosmicheskaya Sistyema Poiska Avariynich Sudov Consumable Products Catalog Cabin Pressure Control System Controller - Pilot Data link Communication Corrosion Prevention Manual Central Processing Unit Cyclic Redundancy Check Corrosion Resisting Steel Cruise Flight Level Cargo Constant Resistance Heating Certification Review Item CRS CRZ CSD CSMU CSS CTRL CT CTR CVR CW D D D/A D/I D/LNA Da DA DAP DAU DB dB DBS DC DCTC DCU DCV DDPM DEOS DET DFDAU DH DIM DISAG DISC DLK DLS DME DMM DMU Course Cruise rating Constant Speed Drive Crash Survivable Memory Unit Cabin Surveillance System Control Current Transformer Centre Cockpit Voice Recorder Clockwise, Continuous Wave Developed for Training Purposes Only CCW CDL CDP CDU CF CFC CFE CFIT CFR CG CH CHR CLB CLB-1, 2 cm cm³ CMC CMCF CMCM CMD CMF CMM CMS COMM COMPT CON CONFIG COSPAS CPC CPCS CPDLC CPM CPU CRC CRES CRFL CRG CRH CRI Diode Digital/Analogic Descent Idle Diplexer/Low Noise Amplifier Double amplitude Decision Altitude Digital Audio Panel Data Acquisition Unit Database Decibel Direct Broadcast Satellite Direct Current, Display Controller DC Tie Contactor Direction Control Unit Direct Current Voltage Dispatch Deviation Procedures Manual Digital Engine Operating System Detailed Inspection, Detector Digital Flight Data Acquisition Unit Decision Height Dimmer Disagree Disconnect Data link Data Loading System Distance Measuring Equipment Data Memory Module Data Loader Management Unit Copyright 2014 by EMBRAER – Empresa Brasileira de Aeronáutica S.A. All rights reserved. This document shall not be copied or reproduced in whole or in part, In any form or by any means without the express written Authorization of Embraer. The information, technical data, designs and drawings disclosed in this document are proprietary information of Embraer or third parties and shall not be used or disclosed to any third party without permission of Embraer 7 Developed for Training Purposes Only Differential Current, Deactivation Procedures Differential Pressure Indicator (190) Bleed Bias Sensor Dole Pole Double Throw De-rotation Display Unit Digital Voice and Data Recorder Downlock Engine 1, 2 Engine Anti-Ice Engine Anti-Icing System European Aviation Safety Agency Electronic Bay Engine Built-up Unit Essential Contactor Electronic Checklist Engine Configuration Plug Environmental Control System Electronic Control Unit, Environmental Control Unit Engine Driven Pump Electronic Display Systems Electro-explosive Device Electronically Erasable Programmable Read Only Memory EICC Fuse Electronic Flight Bag Effectivity Enhanced Ground-Proximity Warning-Module Enhanced Ground Proximity Warning System Exhaust Gas Temperature Electro Hydraulic Cowl Lock Electro Hydraulic Servo Valve Engine Indicating and Crew Alerting System Emergency Integrated Control Centre Emergency Lights Power Unit Emergency Locator Transmitter Empresa Brasileira de Aeronáutica Electromagnetic Compability Emergency EMI ENG EPAC EPBS EPBV EPDC EPGDS EPLD EPM EPROM ESDS ER ERJ ESC ESD ESS ET ETA ETC ETE ETOPS ETTS EVM EXT PWR F F µF F/I F/O FAA FADEC FAF FAGB FAM FAN FAP FAR FBW FC Electro-Magnetic Interference Engine External Power AC Contactor Emergency Parking Brake System Emergency Parking Brake Valve External Power DC Contactor Electrical Power Generating and Distribution System Erasable Programmable Logic Device External Power Mode Erasable Programmable Read Only Memory Electrostatic Discharge Susceptible Extended Range Embraer Regional Jet Electronic Starter Control Electrostatic Discharge Essential (Power bus) Elapsed Time Estimated Time of Arrival Essential Tie Contactor, Elevator Thrust Compensation Estimated Time Enroute Extended Operations Electronic Thrust Trim system Engine Vibration Monitor External Power Developed for Training Purposes Only DP DPI DP3 DPDT D-ROT DU DVDR DWLK E E1, E2 EAI EAIS EASA E-BAY EBU EC ECL ECP ECS ECU EDP EDS EED EEPROM EF EFB EFF EGPWM EGPWS EGT EHCL EHSV EICAS EICC ELPU ELT EMB EMC EMERG Fahrenheit, Farad, Fuse Micro Farad Flight Idle Fuel/Oil Federal Aviation Administration Full Authority Digital Engine Control Final Approach Fix Flap Angle Gear Box Flight Attendant Manual Fan Flight Attendant Panel Federal Aviation Regulations (U.S.A.) Fly by Wire Flight Cycles, Functional Check Copyright 2014 by EMBRAER – Empresa Brasileira de Aeronáutica S.A. All rights reserved. This document shall not be copied or reproduced in whole or in part, In any form or by any means without the express written Authorization of Embraer. The information, technical data, designs and drawings disclosed in this document are proprietary information of Embraer or third parties and shall not be used or disclosed to any third party without permission of Embraer 8 Developed for Training Purposes Only Flight Control Module Fuel Cooled Oil Cooler Flight Control Panel Flight Control System (primary and secondary) Flush Control Unit, Fuel Conditioning Unit Flow Control Valve Flight Director Flight-Data Acquisition Unit Flight Deck Effect Flight Data Recorder Forward Flight Attendant Panel Flight Guidance Control System Flight Hour Functional Hazard Assessment Fault History Database First In First Out Fault Isolation Manual Fire Extinguisher Fault-initiated Test Flight Level Flight Level Change Flexible take-off Flow Limiter Valve Flight Management Computer Flight Frequency Modulation Flight Mode Annunciator Flight Management System Fuel Metering Unit Fuel Metering Valve First Officer Foreign Object Damage Figure of Merit Forward Outer Seal Flap Power Drive-Unit Field Programmable Gate Array Fuel Quantity Gauging System Fuel Quantity Processor Frame FS FSBY FSBY OVRD FSD FSO ft, ft², ft³ FTA FTI FTP FUS FWD FWSOV G g G/I GA RSV GA GB GCR GCS GCU GE/ GEAE GE GEN GLC GIO GMAP GMO GMT GND GP GPM GPS GPU GS, G/S GSE GSTC GVI Fuselage Station Forced Standby Forced Standby Override Full Scale Deflection Full Scale Output Feet, Square Foot, Cubic Foot Fault Tree Analysis Flight Test Instrumentation File Transfer Protocol Fuselage Forward Fire-wall Shut-off Valve Developed for Training Purposes Only FCM FCOC FCP FCS FCU FCV FD FDAU FDE FDR FFAP FGCS FH FHA FHDB FIFO FIM FIREX FIT FL FLCH FLEX FLV FMC FLT FM FMA FMS FMU FMV F/O FOD FOM FOS FPDU FPGA FQGS FQP FR Gram, Gravity Acceleration Ground Idle Go-around reserve Go-around rating Gearbox, Gigabyte Generator Control Relay Generator Control Switch Generator Control Unit General Electric Aircraft Engines General Electric Company Generator Generator Line Contactor Generic Input/Output Ground Mapping Ground Maintenance Override Greenwich Mean Time Ground Guidance/Display Control Panel US Gallons per Minute Global Positioning System Ground Power Unit Ground Speed, Glide slope, Ground Spoilers Ground Support Equipment Ground Service Transfer Contactor General Visual Inspection Copyright 2014 by EMBRAER – Empresa Brasileira de Aeronáutica S.A. All rights reserved. This document shall not be copied or reproduced in whole or in part, In any form or by any means without the express written Authorization of Embraer. The information, technical data, designs and drawings disclosed in this document are proprietary information of Embraer or third parties and shall not be used or disclosed to any third party without permission of Embraer 9 Developed for Training Purposes Only Henry, hour Heading Headphone High Definition Data Link Control High Efficiency Particulate-Air High Frequency Head-up Guidance System Hand-Held Download Unit High Intensity Radiated Fields Hold Open Rod, Horizontal High Pressure, Horsepower High Power Amplifier Hectopascal High Pressure Compressor, Hydraulic Pump Contactor High Pressure Regulation Valve High Pressure Shut-Off Valve High Pressure Turbine (190) High Pressure Turbine Clearance Control Valve Horsepower Extraction Hour High Rate Discharge Horizontal Stabilizer Actuator Horizontal-Stabilizer Actuator-Control Electronics Horizontal Situation Indicator Hydraulic Synoptic Page Horizontal-Stabilizer Trim Actuator Heater High Thermal Stability Hardware Heat Exchanger Hydraulic Hertz (Cycles per second) Input/Output Indicated Air Speed International Air Transport Association Inboard International Civil Aviation Organization ICC ICU ID IDG IESS IEVM IFE IFS IFSD IGA IGB IGFER IGN IGV ILS IM IMP In, in², in³ INBD INFO in.Hg INHIB INIT INMARSAT INOP INPH IOM IPV IRS IRU ISA ISO ITEM ITT ITU J J JAA JAR Integrated Control-Center Isolation Control Unit Identification Integrated Drive Generator Integrated Electronic Standby System Integrated Engine Vibration Monitor In Flight Entertainment Inner Fixed Structure (Forward Core Cowl) In-flight Shutdown Intermediate Gain Antenna (190) Inlet Gearbox Instructions for Ground Fire Extinguishing and Rescue Ignition Inlet Guide Vane Instrument Landing System Inner Marker Impending Inch, Square Inch, Cubic Inch Inboard Information Inch of Mercury Inhibition Initialization International Maritime Satellite Organization Inoperative Interphone Input/Output Module (190) Inlet Pressurizing Valve Inertial Reference System Inertial Reference Unit International Standard Atmosphere International Standards Organization Illustrated Tool and Equipment Manual Inter-Turbine Temperature International Telecommunication Union Developed for Training Purposes Only H H, h HDG HDPH HDLC HEPA HF HGS HHDLU HIRF HOR HP HPA hPa HPC HPRSOV HPSOV HPT HPTCC HPX Hr HRD HSA HS-ACE HSI HSP HSTA HTR HTS HW HX/ Hex HYD Hz I I/O IAS IATA IB ICAO Joule Joint Aviation Authorities Joint Aviation Regulations (Europe) Copyright 2014 by EMBRAER – Empresa Brasileira de Aeronáutica S.A. All rights reserved. This document shall not be copied or reproduced in whole or in part, In any form or by any means without the express written Authorization of Embraer. The information, technical data, designs and drawings disclosed in this document are proprietary information of Embraer or third parties and shall not be used or disclosed to any third party without permission of Embraer 10 Developed for Training Purposes Only Japan Civil Aviation Bureau Kelvin Kilobit Kilogram Kilo Hertz Indicated Airspeed in Knots Kilometers kilo-ohm Kilo-Pascal kilograms per hour Knot Kilo Volt Amp Kilowatt Liter Landing Idle Local Area Network Latitude Lavatory Lbs Pound Pounds-force pounds per hour pounds per minute pounds per second Liquid Crystal Display Landing (Gear) Loadable Diagnostic Information Light-Emitting Diode Landing Gear System Left Hand Engine Left Integrated Control Centre Low Limit Valve Load Management System Lateral Navigation Low Localizer Localizer-Back Course Logotype LON LOP LPTACC LOTC LP LPT LRD LRM LRN LRU LSA LSB LSK LSS LT LVDT LVTO LX M µm M m m², m³ mA MAU MAX mB, MB, Mb MCDU MCOEI MEL MFD MFEP MFP MFS Mg MHz Mi MIC MID Longitude Low Oil Pressure Low Pressure Turbine Active Clearance Control Loss of Thrust Control Low Pressure Low Pressure Turbine (190) Low Rate Discharge Line Replaceable Module Long Range Navigation Line Replaceable Unit Low Speed Awareness Low Significant Bit Line Select Key Lightning Sensor System Light Linear Variable Differential Transducer Low Visibility Takeoff Lightning Processor Developed for Training Purposes Only JCAB K K Kb Kg kHz KIAS km kohm KPa KPH Kt KVA kW L L L/I LAN LAT LAV lb lbf lbs/hr Lbs/min Lbs/sec LCD LDG LDI LED LGS LHE LICC LLV LMS LNAV LO LOC LOC-BC LOGO Micrometer Mach Meter Square Meter, Cubic Meter milli-amperes Modular Avionics Unit Maximum milli Bar, Marker Beacon, Megabits Multi-Function Control Display Unit Max Continuous One Engine Inoperative Minimum Equipment List Multi-Function Display Maintenance Facility and Equipment Planning Multi-Function Probe Multi-Function Spoiler Milligram Megahertz Mile Microphone Middle Copyright 2014 by EMBRAER – Empresa Brasileira de Aeronáutica S.A. All rights reserved. This document shall not be copied or reproduced in whole or in part, In any form or by any means without the express written Authorization of Embraer. The information, technical data, designs and drawings disclosed in this document are proprietary information of Embraer or third parties and shall not be used or disclosed to any third party without permission of Embraer 11 Developed for Training Purposes Only Measuring unit. equivalent to 1/1000 inch Minimum, Minutes Marker Beacon Main Landing Gear Magnetic Level Indicators Maximum Landing Weight Maintenance Manual, Middle Marker Millimeter Master Minimum Equipment List Monitor Warning Function Maximum Mach Operation Mini Modular Radio-Cabinet Mach Number Monitor Maintenance Planning Document Maximum Permissible Explore-Level Maintenance Practices and Procedures Maintenance Review Board Magnetic Pickup Unit Modular Radio Cabinet Member System millisecond Minimum Shift Key Mean Sea Level Motor Starting Relay Maintenance Task Oriented Support System Millivolt Monitor Warning Function Rotation Speed, Newton, North Not Applicable, Not Available Nose Wheel Engine Low Pressure Rotor Speed/ Physical Fan Speed Engine High Pressure Rotor Speed/ Physical Core Speed Corrected High Pressure Rotor Speed National Advisory Committee for Aeronautics Nacelle Anti Ice Nacelle Pressure Regulating and Shut off Valve National Aerospace Standard NAV NB NBPT NC NDB NDI NDT NIC NIM NLG nmi Notam NPRV NTO NVM NWS NWSCM O O/P OAT OB OBV OC OD ODS OEI OEM OF OFV OGV OM OOOI OUTBD OV OVHT OVLD oz P P Navigation Narrow Band No Break Power Transfer No Change Navigation Data Base, Non-Directional Beacon Nondestructive Inspection Nondestructive Testing Manual Network Interface Controller Network Interface Module Nose Landing Gear Nautical Mile Notices to Airmen Negative Pressure Relief Valve Normal Takeoff Non Volatile Memory Nose Wheel Steering Nose Wheel Steering Control Module Developed for Training Purposes Only Mils MIN, min MKR BCN MLG MLI MLW MM mm MMEL MMF Mmo MMRC MN MON MPD MPEL MPP MRB MPU MRC MS ms MSK MSL MSR MTOSS mV MWF N N N/A, NA N/W N1 N2 N2S NACA NAI NAPRSOV NAS Output Outside Air Temperature Outboard Operational (Operability) Bleed Valve Over current Outside Diameter Overheat Detection System One Engine Inoperative Original Equipment Manufacturer Over frequency Outflow Valve Outlet Guide Vane Outer Marker Out, Off, On and In Outboard Over voltage Overheat Overload Ounce Pressure Port Copyright 2014 by EMBRAER – Empresa Brasileira de Aeronáutica S.A. All rights reserved. This document shall not be copied or reproduced in whole or in part, In any form or by any means without the express written Authorization of Embraer. The information, technical data, designs and drawings disclosed in this document are proprietary information of Embraer or third parties and shall not be used or disclosed to any third party without permission of Embraer 12 Developed for Training Purposes Only Pascal Part number Ambient Pressure Primary Actuator Control Electronic Passenger Address & Cabin Interphone System Passenger Address and Cabin Interphone System Programmable Array Logic Passenger Push Button Actuator, Push Button Annunciator Protective Breathing Equipment Power Up Built In Test Personal Computer Printed Circuit Board Personal Comp. Memory Card International Association Pavement Classification Number Power Control Unit Periodic Device Driver Power Drive Unit Performance Pilot Flying, Pico farad Primary Flight Display Power For Take Off Pitch Power Lever Angle (TLA) Programmable Logic Device Processing Module Permanent Magnet Alternator Permanent Magnet Generator Pump Permanent Magnet Starter Ambient Pressure Point of Regulation pounds per hour Present Position Prerecorded Announcement Predictive Receiver Autonomous Integrity Monitor Processor Protection Pressure Regulating and Shut off Valve PS Ps PS3 PSEM Psia, psid psig PSM PSS PSU Pt PTO PTT PTU PUIGST PV PWM PWR Q QAD QAR QD QFE QNE QNH QRH qt QTY R R Rad Alt, RA RAAS R/I RAIM RAM RAT RB RBHA RCT RCB Phase Sequence Static Pressure Engine Compressor Discharge Pressure Proximity Sensor Evaluation Module Pounds per Square Inch, Absolute, Differential Pounds per square inch, gauge Power Supply Module Proximity Sensing System Passenger Service Unit Total Pressure Power Takeoff Assembly Push-to-Talk, to Transmit Power Transfer Unit Power-up Initiated Ground Self-test Priority Valve Pulse-Width Modulated Power Developed for Training Purposes Only Pa P/N P0 P-ACE PACIC PACIS PAL PAX PBA PBE P-BIT PC PCB PCMCIA PCN PCU PDD PDU Perf PF, pF PFD PFTO PIT PLA PLD PM PMA PMG PMP PMS PO POR PPH PPOS PRA PRAIM PROC PROT PRSOV Quick Attach / Detach Quick Access Recorder Quick Disconnect Local Station Barometric Pressure Standard Altimeter Setting (29.92 in.Hg, 1013.25 hPa) Local Altimeter Setting Quick Reference Handbook Quart Gallon Quantity Return Port/ Roller Radar Altimeter, Resolution Advisory Runway Awareness and Advisory System Reverse Idle Receiver Autonomous Integrity Monitor Random Access Memory Ram Air Turbine Report Builder Regulamentos Brasileiros de Homologação Aeronáutica Rain Echo Attenuation Radio Control Bus Copyright 2014 by EMBRAER – Empresa Brasileira de Aeronáutica S.A. All rights reserved. This document shall not be copied or reproduced in whole or in part, In any form or by any means without the express written Authorization of Embraer. The information, technical data, designs and drawings disclosed in this document are proprietary information of Embraer or third parties and shall not be used or disclosed to any third party without permission of Embraer 13 Developed for Training Purposes Only Receiver Radial Drive Shaft Refuel Defuel Panel Rain Echo Attenuation Compensation Technique Reference Retard Reverser / Reverse Thrust Radio Frequency RAT Generator Control Unit Right-Hand Right Hand Engine Remote Image Bus Right Integrated Control Centre RAT Line Contactor Load Resistance Relay Ramp Maintenance Manual Root Mean Square Area Navigation System Required Navigation Performance Rate-of-Change Roll Read Only Memory Output Resistance Revolution per Minute Root Sum Square Reserve Radio Technical Commission for Aeronautics Remote Terminal Receiver/Transmitter Antenna Resistive Thermal Device Ready to Load Rejected Take Off Return To Service Rotary Variable Differential Transducer Reduced Vertical Separation Minimum Rearward Second S1, S2 SAC S-ACE SAE SARSAT SAT SATCOM SAV SCL SCU SCV SDI SDS SDU Sec SECT SELCAL SFA SF-ACE SFC SHP SID SIL SL SLA SLS SM SMK SOV SPD SPDA SPDT SPKR SPM SPST SQ SRAM SRD SRM Solenoid1, 2 Single Annular Combuster Slat Actuator Control Electronics Society of Automotive Engineers Search and Rescue Satellite-Aided Tracking Static Air Temperature Satellite Communications (190) Starter Air Valve Software Critical Level Signal Control Unit Starter Control Valve Source Destination Identifier System Description Section Satellite Data Unit Second Sector Selective Call Synchronized Feedback Actuator Slat/Flap Actuator Control Electronics Specific Fuel Consumption Shaft Horsepower Standard Instrument Departures Service Information Letter Sea Level Synchronized Locking Actuators Sea Level Static Standard Manual Smoke Shut Off Valve, Solenoid Operated Valve Speed Secondary Power Distribution Assembly Single Pole Double Throw Speaker Seat Power Module Single Pole Single Throw Squelch Static Random Access Memory System Requirements Document Structural Repair Manual Copyright 2014 by EMBRAER – Empresa Brasileira de Aeronáutica S.A. All rights reserved. This document shall not be copied or reproduced in whole or in part, In any form or by any means without the express written Authorization of Embraer. The information, technical data, designs and drawings disclosed in this document are proprietary information of Embraer or third parties and shall not be used or disclosed to any third party without permission of Embraer Developed for Training Purposes Only RCVR RDS RDP REACT REF RETD REV RF RGCU RH RHE RIB RICC RLC Rload RLY RMM RMS RNAV RNP ROC ROL ROM Rout Rpm RSS RSV RTCA RT RTA RTD RTL RTO RTS RVDT RVSM RWD S s 14 Developed for Training Purposes Only System Requirement Specifications System Safety Assessment Single Sideband Static Source Error Correction Sign Status Matrix Solid State Power Controller Stabilizer Standard Instrument Arrivals Stand-by Stand-by Contactor Standard Day Store Key System Test Specification Service Software, Switch Standard Wiring Practices Manual Stall Warning Protection System Synchronous System Traffic Advisory Thrust Asymmetry Compensation Traffic Advisory/ Resolution Advisory Thrust Reverser Tactical Air Navigation Static Air Temperature True Airspeed Total Air Temperature To be advised To be Calculated/Confirmed To be defined (190) Transient Bleed Valve Thermocouple Traffic Alert and Collision Avoidance System Terrain Clearance Floor Task Card Manual Transfer Control Protocol/internet Protocol Temperature Compensated Pressure Switch Thrust Control Quadrant TCS TDZE TDC TDS TE TEMP TGB TGT THS TIU TLA TLD TM TMS TO TO/GA TOLD TQA TR TRAS TRB TRF TRS TRU TRUC TRUEC TRU1C, 2C TRX TS TSO U UF UHF ULB UNLK UPLK USB US G UTC Touch Control Steering Touchdown Zone Elevation Top Dead Centre Takeoff Data Set Trailing Edge Temperature (190) Transfer Gearbox Target Trimmable Horizontal Stabilizer Test Interface Unit Throttle Lever Angle / Thrust Lever Angle Time Limited Dispatch Torque Motor Thrust Management System Take-off Take Off and Go Around Takeoff and Landing Data Throttle Quadrant Assembly Thrust Reverser Thrust Reverser Actuation System Turbulence (190) Turbine Rear Frame Thrust Rating Selector Transformer Rectifier Unit Transformer Rectifier Unit Contactor Transformer Rectifier Unit Essential Contactor Transformer Rectifier Unit 1, 2 Contactor Thrust Reverser Position Technical Specification Technical Standard Order Developed for Training Purposes Only SRS SSA SSB SSEC SSM SSPC STAB STAR STBY STBYC STD STO STS SVC SW SWPM SWPS SYNC SYS T TA TAC TA/RA T/R TACAN TAMB TAS TAT TBA TBC TBD TBV TC TCAS TCF TCM TCP/IP TCPS TCQ Under frequency Ultra High Frequency Underwater Locator Beacon Unlock Uplock Universal Serial Bus US Gallon Universal Time Coordination Copyright 2014 by EMBRAER – Empresa Brasileira de Aeronáutica S.A. All rights reserved. This document shall not be copied or reproduced in whole or in part, In any form or by any means without the express written Authorization of Embraer. The information, technical data, designs and drawings disclosed in this document are proprietary information of Embraer or third parties and shall not be used or disclosed to any third party without permission of Embraer 15 Developed for Training Purposes Only Under voltage Microvolt Volts Volt Ampere the minimum speed in the takeoff Volts Alternating Current Vertical Altitude Variable Vertical Altitude Select Virtual Backplane Peripheral Component (190) Variable Bleed Valve Valve Control Unit Volts Direct Current VHF Data Link VHF Data Radio Variable Differential Transducer Vertical Vertical Flight Level Change Variable Geometry Video Graphics Array Vertical Guidance Path Variable Guide Vane Variable Geometry Actuator Position Feedback Very High Frequency Vibration VOR/ILS Data link Maximum Operating Speed Vertical Navigation Volume Very High Frequency Omni directional Radio VOR Localizer VOR and UHF Tactical Air Navigation Vertical Path Voltage Reference Volts Root Mean Square Vertical Speed Variable Stator Vane Vacuum Waste System W W WADL WAI WAIV WF WHCU WHS WM WOFFW WOW WOWA WOWB WPS WPT WQAR WRN WS WSHR WWS WWSC WX X XBLEED XCHECK XDCR XFEED XFER XMTR XPDR XTK Y YD Z ZWF Watt, West Wireless Aircraft Data Link Wing Anti-Ice Wing Anti-Ice Valve Fuel Flow Windshield Heating Control-Unit Windshield Heating System Wiring Manual Weight-off-Wheels Weight On Wheels Weight On Wheels PSEM1 Weight On Wheels PSEM2 Words per Second Waypoint Wireless Quick Access Recorder Warning Wheel Spin, Wind shear Wind shear Windshield Wiper System Water Waste System Controller Weather Developed for Training Purposes Only UV V µV V VA V1 VAC VALT VAR VASEL VBPCI VBV VCU VDC VDL VDR VDT VERT VFLCH VG VGA VGP VGV VGX VHF Vibe VIDL VMO VNAV VOL VOR VOR/LOC VORTAC VPATH VREF VRMS VS VSV VWS Cross Bleed Cross Check Transducer Cross feed Transfer Transmitter Transponder Cross track Yaw Damper Zero Weight Fuel Copyright 2014 by EMBRAER – Empresa Brasileira de Aeronáutica S.A. All rights reserved. This document shall not be copied or reproduced in whole or in part, In any form or by any means without the express written Authorization of Embraer. The information, technical data, designs and drawings disclosed in this document are proprietary information of Embraer or third parties and shall not be used or disclosed to any third party without permission of Embraer 16 ELECTRICAL/ELECTRONIC AND MECHANICAL SYMBOLS The illustrations in the MTM and other Technical Publications show graphic symbols to represent electrical/electronic and mechanical components. Developed for Training Purposes Only Developed for Training Purposes Only The symbols are identified in the following pages: Copyright 2014 by EMBRAER – Empresa Brasileira de Aeronáutica S.A. All rights reserved. This document shall not be copied or reproduced in whole or in part, In any form or by any means without the express written Authorization of Embraer. The information, technical data, designs and drawings disclosed in this document are proprietary information of Embraer or third parties and shall not be used or disclosed to any third party without permission of Embraer 17 Developed for Training Purposes Only Developed for Training Purposes Only ELECTRICAL AND ELECTRONIC SYMBOLS 1 Copyright 2014 by EMBRAER – Empresa Brasileira de Aeronáutica S.A. All rights reserved. This document shall not be copied or reproduced in whole or in part, In any form or by any means without the express written Authorization of Embraer. The information, technical data, designs and drawings disclosed in this document are proprietary information of Embraer or third parties and shall not be used or disclosed to any third party without permission of Embraer 18 Developed for Training Purposes Only Developed for Training Purposes Only ELECTRICAL AND ELECTRONIC SYMBOLS 2 Copyright 2014 by EMBRAER – Empresa Brasileira de Aeronáutica S.A. All rights reserved. This document shall not be copied or reproduced in whole or in part, In any form or by any means without the express written Authorization of Embraer. The information, technical data, designs and drawings disclosed in this document are proprietary information of Embraer or third parties and shall not be used or disclosed to any third party without permission of Embraer 19 Developed for Training Purposes Only Developed for Training Purposes Only ELECTRICAL AND ELECTRONIC SYMBOLS 3 Copyright 2014 by EMBRAER – Empresa Brasileira de Aeronáutica S.A. All rights reserved. This document shall not be copied or reproduced in whole or in part, In any form or by any means without the express written Authorization of Embraer. The information, technical data, designs and drawings disclosed in this document are proprietary information of Embraer or third parties and shall not be used or disclosed to any third party without permission of Embraer 20 Developed for Training Purposes Only Developed for Training Purposes Only ELECTRICAL AND ELECTRONIC SYMBOLS 4 Copyright 2014 by EMBRAER – Empresa Brasileira de Aeronáutica S.A. All rights reserved. This document shall not be copied or reproduced in whole or in part, In any form or by any means without the express written Authorization of Embraer. The information, technical data, designs and drawings disclosed in this document are proprietary information of Embraer or third parties and shall not be used or disclosed to any third party without permission of Embraer 21 Developed for Training Purposes Only Developed for Training Purposes Only ELECTRICAL AND ELECTRONIC SYMBOLS 5 Copyright 2014 by EMBRAER – Empresa Brasileira de Aeronáutica S.A. All rights reserved. This document shall not be copied or reproduced in whole or in part, In any form or by any means without the express written Authorization of Embraer. The information, technical data, designs and drawings disclosed in this document are proprietary information of Embraer or third parties and shall not be used or disclosed to any third party without permission of Embraer 22 Developed for Training Purposes Only Developed for Training Purposes Only ELECTRICAL AND ELECTRONIC SYMBOLS 6 Copyright 2014 by EMBRAER – Empresa Brasileira de Aeronáutica S.A. All rights reserved. This document shall not be copied or reproduced in whole or in part, In any form or by any means without the express written Authorization of Embraer. The information, technical data, designs and drawings disclosed in this document are proprietary information of Embraer or third parties and shall not be used or disclosed to any third party without permission of Embraer 23 Developed for Training Purposes Only Developed for Training Purposes Only MECHANICAL SYMBOLS 1 Copyright 2014 by EMBRAER – Empresa Brasileira de Aeronáutica S.A. All rights reserved. This document shall not be copied or reproduced in whole or in part, In any form or by any means without the express written Authorization of Embraer. The information, technical data, designs and drawings disclosed in this document are proprietary information of Embraer or third parties and shall not be used or disclosed to any third party without permission of Embraer 24 Developed for Training Purposes Only Developed for Training Purposes Only MECHANICAL SYMBOLS 2 Copyright 2014 by EMBRAER – Empresa Brasileira de Aeronáutica S.A. All rights reserved. This document shall not be copied or reproduced in whole or in part, In any form or by any means without the express written Authorization of Embraer. The information, technical data, designs and drawings disclosed in this document are proprietary information of Embraer or third parties and shall not be used or disclosed to any third party without permission of Embraer 25 Developed for Training Purposes Only Developed for Training Purposes Only EMBRAER Empresa Brasileira de Aeronáutica S.A. Customer Training Phone: +55 (12) 3927-5827 Fax: +55 (12) 3927-7535 http://www.embraer.com.br Copyright 2014 by EMBRAER – Empresa Brasileira de Aeronáutica S.A. All rights reserved. This document shall not be copied or reproduced in whole or in part, In any form or by any means without the express written Authorization of Embraer. The E-mail: training@embraer.com.br information, technical data, designs and drawings disclosed in this document are proprietary information of Embraer or third parties and shall not be used or disclosed to any third party without permission of Embraer
