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Embraer 170 LR Airplane Operations Manual Volume 2 AOM-1502-002 PDF

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Complete Embraer 170 LR Airplane Operations Manual Volume 2 (AOM-1502-002, Revision 1) covering all aircraft systems for CF34-8E5-equipped LR models under FAA certification. Instant PDF download.

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Description

Embraer 170 LR Airplane Operations Manual Volume 2 – AOM-1502-002

The Embraer 170 LR Airplane Operations Manual Volume 2 is the systems-focused half of the complete AOM set published by Empresa Brasileira de AeronΓ‘utica S.A. This volume applies specifically to the EMBRAER 170 LR model equipped with CF34-8E5 engines operating under FAA certification, and it covers every major aircraft system from air management and automatic flight through to warning systems and oxygen.

This is Revision 1 of document AOM-1502-002, dated February 20, 2004, superseding the original release of December 10, 2003. Every page in this PDF carries the revision coding and list-of-effective-pages data so you can verify exactly what is current.

File Details

  • Manual Type: Airplane Operations Manual (AOM), Volume 2
  • Manufacturer: Empresa Brasileira de AeronΓ‘utica S.A. (Embraer)
  • Applicable Aircraft: EMBRAER 170 LR model
  • Applicable Engines: General Electric CF34-8E5
  • Certification Basis: FAA
  • Document Number: AOM-1502-002
  • Edition: Revision 1
  • Original Issue Date: December 10, 2003
  • Revision Date: February 20, 2004
  • Language: English
  • File Format: PDF
  • Page Count: 820+ pages

Important note: As stated on the cover page, this publication is incomplete without Airplane Operations Manual AOM-1502 Volume 1. Volume 1 contains the operating limitations, normal and non-normal procedures, and performance data that complement the systems descriptions in this volume.

Chapters Covered

This volume is organised into fifteen ATA-style system sections, each with its own table of contents, controls and indications, system description, and EICAS messages:

  • 14-01 Airplane General β€” Basic data, external dimensions, three-view drawing, airplane antennas, cockpit general, cockpit philosophy, display system overview, cockpit lighting, passenger cabin, galley, PSU, lavatory, external and internal lighting, doors, escape slides, reinforced cockpit door, water and waste, cargo compartment, EICAS messages
  • 14-02 Air Management System β€” Pneumatic system, engine bleed, APU bleed, ground connections, overheat detection, ECS packs, recirculation fans, gasper ventilation, electronic bay ventilation, emergency ram air, pressurisation system, CPCS flight modes, EICAS messages
  • 14-03 Automatic Flight β€” Guidance panel, lateral and vertical guidance controls, AFCS, autopilot, flight director, yaw damper, FMA indications, lateral and vertical modes, ILS approach sequences, thrust management system, autothrottle, thrust rating selection, EICAS messages
  • 14-04 Auxiliary Power Unit β€” APU fuel supply, APU bleed, APU operation, start and shutdown, APU protection, EICAS messages
  • 14-05 Electrical β€” AC and DC power controls, ram air turbine deployment, electrical synoptic page, IDG, APU generator, AC GPU, inverter, RAT, TRUs, batteries, DC GPU, ICC, SPDA, circuit breakers, AC/DC load distribution, system configurations, EICAS messages
  • 14-06 Engine β€” Control pedestal, thrust lever, fire handle, engine control panel, EICAS indications, fuel system, lubrication system, starting and ignition, thrust reverser, FADEC, ATTCS, flexible takeoff, engine ratings, takeoff dataset, engine protection, EICAS messages
  • 14-07 Fire Protection β€” Fire protection control panel, engine fire detection and extinguishing, APU fire protection, cargo compartment fire protection, lavatory fire protection, fire detection system test, EICAS messages
  • 14-08 Flight Controls β€” Control wheel, slat/flap selector lever, speed brake lever, trim panel, flight control mode panel, disconnect handle, flight controls synoptic page, EICAS indications, fly-by-wire, pitch control, roll control, yaw control, slat-flap system, spoiler system, EICAS messages
  • 14-09 Flight Instruments, Communication, Navigation, FMS β€” PFD, ADI, HSI, MFD, weather radar, lightning sensor, MCDU, display controller panel, IESS, clock, standby compass, communication, VHF, interphone, PA, attendant call, audio control panel, DVDR, CMF, ACARS, IRS, GPS, radio navigation, transponder, preview mode, weather radar system, FMS, EICAS messages
  • 14-10 Fuel β€” Fuel control panel, fuel synoptic page, EICAS indication, refuelling/defuelling control panel, fuel tanks, quantity indication, fuel pumps, fuel crossfeed, engine fuel shutoff valve, refuelling and defuelling, EICAS messages
  • 14-11 Hydraulic β€” Hydraulic system panel, hydraulic synoptic page, hydraulic system 1, 2, and 3, reservoirs, engine driven pumps, electric hydraulic pumps, accumulators, power transfer unit, pump unloader valve, flow limiter valve, EICAS messages
  • 14-12 Ice and Rain Protection β€” Ice protection control panel, windshield wiper control panel, synoptic page, ice detectors, engine anti-ice, wing anti-ice, anti-ice system operation, windshield heating, ADSP/TAT heating, water and waste heating, windshield wiper system, ice detection system test, EICAS messages
  • 14-13 Landing Gear and Brakes β€” Landing gear control panel, alternate gear extension, warning inhibition, position indication, brakes, emergency parking brake, MFD status page, steering, towing lights, air/ground positioning, landing gear operation, brakes, nosewheel steering system, EICAS messages
  • 14-14 Oxygen β€” Oxygen control panel, mask stowage box and crew mask, synoptic page, flight crew oxygen system, protective breathing equipment, passenger oxygen system, portable oxygen cylinder, EICAS messages
  • 14-15 Warning System β€” Glareshield panel, takeoff config check, stall warning panel, EGPWS panel, TCAS, visual warnings, aural warnings, voice messages, takeoff configuration warning, stall protection system, EGPWS, windshear detection and escape guidance, TCAS, EICAS messages

Complete PDF Bookmark Tree

Complete Bookmarks

The complete bookmarks in the β€œEmbraer 170 LR Airplane Operations Manual Volume 2 AOM-1502-002 PDF” are as follows:

Table of Contentsp. 31
Section 14-01 Airplane Generalp. 33
14-01-00 Introductionp. 38
14-01-05 Airplane Basic Datap. 39
14-01-10 Cockpit Generalp. 45
14-01-15 Cockpit Philosophyp. 55
14-01-20 Main/Glareshield/Control Pedestal Panelsp. 57
Auto Reversion Logicp. 60
14-01-25 Electronic Display System (EDS)p. 59
Modular Avionics Unit (MAU)p. 73
14-01-30 Controls and Indicationsp. 79
Doors Synoptic Pagep. 99
14-01-35 Passenger Cabinp. 103
14-01-40 Lightingp. 111
Rainbow Lightsp. 117
14-01-45 Doorsp. 127
Passenger and Service Doorsp. 127
Emergency Exitsp. 141
Cargo Doorsp. 143
Access Doorsp. 146
14-01-50 Escape Slidep. 149
14-01-60 Reinforced Cockpit Doorp. 155
14-01-65 Water and Wastep. 161
14-01-70 Cargo Compartmentp. 165
14-01-80 EICAS Messagesp. 167
Section 14-02 Air Management Systemp. 171
14-02-00 Introductionp. 174
14-02-05 Controls and Indicationsp. 175
14-02-10 Pneumatic Systemp. 187
Pneumatic System Schematicp. 188
Overheat Detection Systemp. 190
14-02-15 Environmental Control System (ECS)p. 193
14-02-20 Pressurization Systemp. 197
Pressurization Differentialp. 198
Dump Functionp. 199
APU Bleed Source Prioritizationp. 200
Bleed Valve Logicp. 200
Engine Bleedp. 200
APU Bleedp. 200
Cross Bleedp. 201
ECS Packsp. 201
Smoke Detectionp. 202
CPCS Flight Modesp. 203
Groundp. 203
Takeoffp. 203
Climbp. 204
Cruisep. 204
Descentp. 205
Abortp. 205
14-02-25 EICAS Messagesp. 209
Section 14-03 Automatic Flightp. 211
14-03-00 Introductionp. 214
14-03-05 Control Indicationsp. 215
14-03-10 Flight Guidance Control Systemp. 231
Preview Featurep. 251
14-03-20 Thrust Management Systemp. 253
14-03-30 EICAS Messagesp. 261
Section 14-04 Auxiliary Power Unitp. 265
14-04-00 Introductionp. 266
14-04-05 Controls and Indicationsp. 267
14-04-10 APU Fuel Supplyp. 269
APU Protectionp. 271
14-04-15 EICAS Messagesp. 273
Section 14-05 Electricalp. 275
14-05-00 Introductionp. 277
14-05-05 Controls and Indicationsp. 279
14-05-10 AC Electrical Power Descriptionp. 289
14-05-15 DC Electrical Power Descriptionp. 293
14-05-20 Electrical Power Distribution and Controlp. 295
Integrated Control Center (ICC)p. 295
Secondary Power Distribution Assemblies (SPDA)p. 296
14-05-30 Circuit Breakersp. 299
14-05-35 AC/DC Bus Load Distributionp. 303
14-05-40 Electrical Distribution and System Configurationsp. 313
Electrical Source Priorityp. 313
System Configurationsp. 314
Batteries Only/APU Start in Progressp. 315
AC GPUp. 316
APU Powerp. 317
Ground Service Modep. 318
Two IDG Powerp. 319
IDG Failed and APU Generator in Usep. 320
IDG Failed and APU Generator not in Usep. 321
RAT Powerp. 322
TRU Failedp. 323
14-05-45 EICAS Messagesp. 327
Section 14-06 Enginep. 329
14-06-00 Introductionp. 333
14-06-05 Controls and Indicationsp. 337
14-06-10 Engine Fuel Systemp. 347
14-06-20 Starting and Ignition Systemsp. 351
14-06-25 Thrust Reverser Systemp. 353
14-06-30 Engine Control Systemp. 355
Engine Fadec Protectionp. 364
Engine Thrust Ratingsp. 359
14-06-35 EICAS Messagesp. 365
Section 14-07 Fire Protectionp. 369
14-07-00 Introductionp. 370
14-07-05 Controls and Indicationsp. 371
14-07-10 Engine Fire Protectionp. 373
14-07-15 APU Fire Protectionp. 375
14-07-20 Cargo Compartment Fire Protectionp. 377
14-07-25 Lavatory Fire Protectionp. 379
14-07-30 Fire Detection System Testp. 383
14-07-35 EICAS Messagesp. 385
Section 14-08 Flight Controlsp. 387
14-08-00 Introductionp. 389
14-08-05 Controls and Indicationsp. 391
Slat/Flap Intermediate Positionsp. 392
14-08-10 Fly By Wirep. 405
Normal and Direct Modesp. 407
14-08-15 Pitch Controlp. 411
Stabilizer Trimp. 416
14-08-20 Roll Controlp. 419
Aileron Trimp. 421
14-08-25 Yaw Controlp. 423
Rudder Trim Systemp. 425
14-08-30 Slat/Flap Systemp. 427
14-08-35 Spoiler Systemp. 431
Auto Speed Brake Retractionp. 433
14-08-45 EICAS Messagesp. 435
Section 14-09 Flight Instruments/Comm/Nav/FMSp. 439
14-09-00 Introductionp. 444
14-09-05 Controls and Indicationsp. 445
14-09-10 Flight Instrumentsp. 507
Integrated Electronic Standby System (IESS)p. 513
Air Data System (ADS)p. 507
14-09-15 Communication Systemp. 517
Digital Voice Data Recorder (DVDR)p. 527
14-09-20 Navigation Systemp. 535
Inertial Reference System (IRS)p. 535
Preview Modep. 545
14-09-25 Flight Management Systemp. 557
Section 14-10 Fuelp. 625
14-10-00 Introductionp. 626
14-10-05 Controls and Indicationsp. 627
14-10-10 Fuel Tanksp. 637
14-10-15 EICAS Messagesp. 645
Section 14-11 Hydraulicsp. 647
14-11-00 Introductionp. 649
14-11-05 Controls and Indicationsp. 651
14-11-10 Hydraulic Systemsp. 659
Hydraulic System 1p. 659
Hydraulic System 1 Accumulatorp. 659
Hydraulic System 2p. 661
Power Transfer Unit (PTU)p. 662
Hydraulic System 2 Accumulatorp. 662
Hydraulic System 3p. 663
Hydraulic System 3 Accumulatorp. 664
Pump Unloader/Limiter Valvep. 664
Hydraulic System Schematicp. 665
14-11-15 EICAS Messagesp. 667
Section 14-12 Ice and Rain Protectionp. 669
14-12-00 Introductionp. 670
14-12-05 Controls and Indicationsp. 671
Windshield Wiper Controlp. 673
14-12-10 Ice Detectorsp. 677
Windshield Heating Systemp. 682
Engine and Wing Anti-Ice Systemp. 680
14-12-15 Ice Protection System Testp. 683
14-12-20 EICAS Messagesp. 685
Section 14-13 Landing Gear and Brakesp. 687
14-13-00 Introductionp. 689
14-13-05 Controls and Indicationsp. 691
14-13-10 Air/Ground Positioning Systemp. 705
14-13-15 Landing Gear Operationp. 707
Landing Gear Aural Warningsp. 711
14-13-20 Brakesp. 713
14-13-25 Nosewheel Steering Systemp. 719
14-13-30 EICAS Messagesp. 723
Section 14-14 Oxygenp. 725
14-14-00 Introductionp. 726
14-14-05 Controls and Indicationsp. 727
14-14-10 Flight Crew Oxygen Systemp. 733
14-14-15 Passenger Oxygen Systemp. 737
Auto Mask Deploymentp. 737
14-14-20 EICAS Messagesp. 741
Section 14-15 Warning Systemp. 743
14-15-00 Introductionp. 746
14-15-05 Controls and Indicatorsp. 747
14-15-10 Visual Warningsp. 763
14-15-15 Aural Warningsp. 787
14-15-20 Takeoff Configuration Warningp. 791
14-15-25 Stall Protection Systemp. 793
14-15-30 Enhanced Ground Proximityh Warning System (EGPWS)p. 795
14-15-35 Windshear Detection and Escape Guidance Systemp. 807
14-15-40 Traffic Alert and Collision Avoidance Sytem (TCAS)p. 811
14-15-45 EICAS Messagesp. 819

For anyone maintaining, operating, or training on the EMBRAER 170 LR, this volume is the single most complete systems reference published by the manufacturer. It explains not just what each system does, but how it is controlled, what indications the crew sees on the EICAS and MFD synoptic pages, what the automatic logic does in each flight phase, and what every EICAS message means. The schematics, synoptic page diagrams, cockpit panel illustrations, and system interface drawings throughout the volume make it possible to trace signal flow, understand failure modes, and prepare for both normal and abnormal situations.

What This Manual Enables

This is not a generic training handout. It is the manufacturer’s own operations manual for a specific aircraft variant, and it supports real technical work:

  • System operation and theory β€” Understand exactly how the air management, electrical, hydraulic, fuel, flight control, ice protection, landing gear, and warning systems function on the EMBRAER 170 LR with CF34-8E5 engines.
  • EICAS message interpretation β€” Every section includes the full EICAS message table with type, message, meaning, and inhibition codes so you can identify what the aircraft is telling you and why.
  • Cockpit panel familiarisation β€” Detailed illustrations and descriptions of the overhead panel, glareshield, main instrument panel, control pedestal, and all associated controls.
  • Synoptic page understanding β€” Full colour-coded explanations of every MFD synoptic page for fuel, hydraulic, electrical, flight controls, anti-ice, doors, and oxygen.
  • System interface and schematics β€” Block diagrams and schematics showing how systems communicate, where data comes from, and what happens when a source fails.
  • Automatic flight logic β€” Detailed descriptions of the FGCS lateral and vertical modes, autothrottle modes, thrust rating selection, and the conditions that trigger each mode.
  • Engine and APU control β€” FADEC operation, ATTCS logic, flexible takeoff, thrust ratings, engine protection, APU start and shutdown, and APU protection.
  • Warning system coverage β€” EGPWS modes, TCAS annunciations, windshear detection and escape guidance, stall protection, takeoff configuration warning, and the full EICAS message inhibition table.

Having the correct systems information matters because the EMBRAER 170 LR is a fly-by-wire aircraft with highly integrated avionics. Procedures that work on conventional aircraft do not always apply. This manual tells you what the aircraft actually does, how the automatic systems will respond, and what indications to expect in every phase of flight.

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The Embraer 170 LR Airplane Operations Manual Volume 2 AOM-1502-002 is delivered as an instant PDF download after payment. No shipping, no waiting, no physical media. The file is printable and can be viewed on any device that reads PDFs β€” laptop, tablet, or smartphone. Whether you are a pilot, maintenance technician, flight dispatcher, simulator operator, or aviation enthusiast, this manual gives you direct access to the manufacturer’s system descriptions for the EMBRAER 170 LR with CF34-8E5 engines.

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