aom-1502-017-rev.04_apr-30-10

AIRPLANE OPERATIONS MANUAL VOLUME 1EMPRESA BRASILEIRA DE AERONUTICA S.A.

TACAThis manual is applicable to the EMBRAER 190 airplanes AR model equipped with CF34-10E6 engines and operating under FAA certification.

THIS PUBLICATION IS INCOMPLETE WITHOUT AIRPLANE OPERATIONS MANUAL AOM-1502 VOLUME 2.

AOM-1502-017 MARCH 25, 2008REVISION 4 - APRIL 30, 2010

Copyright 2010 by EMBRAER - Empresa Brasileira de Aeronautica S.A. All rights reserved. This document shall not be copied or reproduced, whether 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.

CUSTOMER COMMENT FORMAirplane Operations Manual AOM-1502-017

Please use this Customer Comment Form to notify us of any discrepancies or problems you find in the Airplane Operations Manual. We would also welcome constructive suggestions on how we can further improve our documentation or service.

Your feedback will be acknowledged, and we will advise you of the action we intend to take.

Sincerely, Embraer Flight Operations Support

Please return this form to: Embraer - Flight Operations Support - PC176 Av. Brigadeiro Faria Lima, 2170 CEP 12227-901 So Jos dos Campos - SP - BRASIL Phone: +55 12 3927-1706 Fax: +55 12 3927-2477 E-mail: [email protected]

Airplane Operations Manual AOM-1502-017Section/Page: Name: Position: Company: Fax Number: E-mail: Comment/Suggetion: Page Revision Number:

Phone Number:

Space Reserved for EmbraerCCF No. Comment received: Person in Charge: Action to be taken: Date Acknowledged:

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Implemented:

AIRPLANE OPERATIONS MANUAL HIGHLIGHTS OF CHANGE REVISION 4 APRIL 30, 2010

HIGHLIGHTS OF CHANGE

Editorial revisions (for example, spelling corrections) may have revision bars with no associated highlight. Block 1-20 1-25 1-35 1-40 2-05 2-10 2-36 2-40 2-57 2-64 2-68 3-01 3-03 3-09 3-11 3-13 3-15 3-16 3-23AOM-1502-017

Change Description Update of abbreviations and acronyms list. Update of Units Conversion table. Update of Service Bulletin Table. Deletion of CDL item. Replacement of Weight and Balance Manual reference by Airplane Operations Manual sections reference. Update of Wind Limitations for operation with tailwind up to 15 kt. Deletion of Russian and Ukrainian fuels. Update of thrust assurance check information and thrust reverser limitation (Pre-Mod. SB 170-73-0003 or Pre-Mod. SB 190-73-0010). Update of information for CAT II operation. Update of Navigation Limitation. Inclusion of block title. Update of Cockpit Safety Inspection procedure title and Power Up procedure. Update of block title. Update of Before Start procedure. Update of Engine Start procedure. Update of After Start Procedure. Update of recommendation to turn off nose taxi lights. Inclusion of Takeoff with tailwind above 10 kt procedure. Update of recommendation to keep nose taxi lights turned off.

Copyright by Embraer. Refer to cover page for details.

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AIRPLANE OPERATIONS MANUAL Change Description Update of Engine Battery Start Procedure. Update of Icing Conditions, Cold Weather and Cold Soak Operations. Deletion of Windshear information included in SOPM. Update of turbulent air penetration procedure. Inclusion of QFE operation. Update of Flight Patterns pictures. SMOKE, FIRE, FUMES - Organizes the list of relevant inoperative items in alphabetical order. Inclusion of Unreliable Airspeed procedure. ABNORMAL LANDING GEAR EXTENSION Includes note regarding completely pulling the alternate extension lever. LOSS OF HYDRAULIC SYSTEM 1 - Organizes the list of relevant inoperative items in alphabetical order. LOSS OF HYDRAULIC SYSTEM 2 - Organizes the list of relevant inoperative items in alphabetical order. LOSS OF HYDRAULIC SYSTEM 1 AND 2 Organizes the list of relevant inoperative items in alphabetical order. LOSS OF HYDRAULIC SYSTEM 1 AND 3 Organizes the list of relevant inoperative items in alphabetical order, and includes Outboard Aileron actuators in the list. LOSS OF HYDRAULIC SYSTEM 2 AND 3 Organizes the list of relevant inoperative items in alphabetical order. JAMMED CONTROL WHEEL ROLL - Organizes the list of relevant inoperative items in alphabetical order. BRK LH (RH) FAIL - Corrects landing distance factor for EMBRAER 190 TCCA. AC BUS 1 OFF - Organizes the list of relevant inoperative items in alphabetical order. AC BUS 2 OFF - Organizes the list of relevant inoperative items in alphabetical order.AOM-1502-017

Block 3-70 3-75 3-75 3-75 3-80 3-95 4-01-01 4-02-01 4-02-01 4-02-01 4-02-01 4-02-01

4-02-01

4-02-01 4-02-01 4-03-03 4-03-05 4-03-05

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AIRPLANE OPERATIONS MANUAL Block 4-03-05 4-03-05 4-03-05 4-03-05 4-03-05 4-03-05 4-03-06


Change Description DC BUS 1 OFF - Organizes the list of relevant inoperative items in alphabetical order. DC BUS 2 OFF - Organizes the list of relevant inoperative items in alphabetical order and includes autobrake in the list. DC ESS BUS 1 OFF - Organizes the list of relevant inoperative items in alphabetical order. DC ESS BUS 2 OFF - Organizes the list of relevant inoperative items in alphabetical order. DC ESS BUS 3 OFF - Organizes the list of relevant inoperative items in alphabetical order. ELEC EMERGENCY - Organizes the list of relevant inoperative items in alphabetical order. ENGINE 1 (2) REV DEPLOYED Includes the instruction to set the transponder to TA only. Includes APU bleed button action according to OB170-001/09. ENGINE 1 (2) CONTROL FAULT Includes the instruction to move associated Thrust Lever to IDLE and set the transponder to TA only, if engine thrust is stable at IDLE. ENGINE 1 (2) FAIL Includes the instruction to set the transponder to TA only, if engine is not restarted. Includes APU bleed button action according to OB170-001/09. ENGINE 1 (2) TLA FAIL Includes the instruction to set the transponder to TA only, if thrust is at IDLE. Also includes scenario where engine thrust control is not lost. ENGINE 1 (2) FIRE Includes the instruction to set the transponder to TA only. Includes APU bleed button action according to OB170-001/09. RUDDER FAIL - Organizes the list of relevant inoperative items in alphabetical order. SPOILER FAULT - Allows the use of the spoilers after the Flight Controls Mode reset. FLAP FAIL - Includes one additional unloking attempt. SLAT FAIL - Includes one additional unloking attempt.

4-03-06

4-03-06

4-03-06

4-03-07 4-03-08 4-03-08 4-03-08 4-03-08AOM-1502-017


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AIRPLANE OPERATIONS MANUAL Change Description RUDDER NML MODE FAIL - Organizes the list of relevant inoperative items in alphabetical order. SPOILER NML MODE FAIL - Organizes the list of relevant inoperative items in alphabetical order. AVNX MAU 1A FAIL - Organizes the list of relevant inoperative items in alphabetical order. AVNX MAU 1B FAIL - Organizes the list of relevant inoperative items in alphabetical order. AVNX MAU 2A FAIL - Organizes the list of relevant inoperative items in alphabetical order. AVNX MAU 2B FAIL - Organizes the list of relevant inoperative items in alphabetical order, and corrects which autopilot channel is failed. AVNX MAU 3A FAIL - Organizes the list of relevant inoperative items in alphabetical order. AVNX MAU 3B FAIL - Organizes the list of relevant inoperative items in alphabetical order. DISPLAY CTRL FAIL - Organizes the list of relevant inoperative items in alphabetical order. A-I ENG LEAK - Removes the message for EMBRAER 190/195 (Message is applicable only to EMBRAER 170/175). Update of Geometric Height to Pressure Height example. Update of flexible temperature determination flowchart. Inclusion of Unfactored Landing Distance tables for contaminated runway. Update of Economic Cruise Speed introduction. Inclusion of a guideline when flying over mountainous area. Update of overwing door clearances. Update of Fire Extinguisher operation. Text improved. Update of Towbarless Towing procedure.AOM-1502-017

Block 4-03-08 4-03-08 4-03-09 4-03-09 4-03-09 4-03-09 4-03-09 4-03-09 4-03-09 4-03-12 5-10 5-20 5-35 6-15 6-35 8-10 11-15 11-30 13-11

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AIRPLANE OPERATIONS MANUAL Block 13-25 13-40 13-60 14-01-05 14-01-10 14-01-10 14-01-22 14-01-25 14-01-37 14-01-45 14-02-05 14-02-10 14-02-15 14-02-20 14-03-05 14-03-05


Change Description Inclusion of recommendations for refueling with APU running. Language review. Improvement of FUEL 1 (2) FEED FAULT procedure. Inclusion of QRH 1(2) TIME OUT message. Update of Airplane Antennas picture with TDR1 and TDR2 correction position. Deletion of emergency equipment information from cockpit partition. For emergency equipment information refer to section 11. Inclusion of Observer seat fold procedure. Inclusion of Interphone Handset/Cradle Assembly description. Update of CMF2 information. Inclusion of description of red indication of LED at the outlet. Inclusion of maximum wind limitation for operating doors. Update of cabin altitude, cabin rate of change and differential pressure indications. Update of table "Bleed Source Prioritization Logic". Text improvement. Change from TDS to T/O Dataset. Text improvement to describe OFV logic. Update of FD button note according to Load 23.1 and Autothrottle Indications on FMA. Deletion of FLARE label on Vertical Mode Indications on FMA. Inclusion of AFCS logic regarding maximum bank angles while in LOC mode. Update of Preview Feature description according to Load 23.1. Update of Altitude Select note. Update of CRZ mode description according to Load 23.1. Update of APU START procedure. Update of DC BUS tie toggle switch description. Update of Ram Air Turbine description.

14-03-10

14-03-20 14-04-10 14-05-05 14-05-10AOM-1502-017


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AIRPLANE OPERATIONS MANUAL Change Description Update of DC ESS BUS 1 and 2 lists including brake control module 1 and 2. Improvement of amber indication of oil level on MFD. Inclusion of comment about igniters life reduction when OVRD position is continued used. Update of Ground Start description to include no light off logic. Update of ENG 1 (2) OIL SW FAIL meaning. Inclusion of details about lavatory smoke sensor. Inclusion note about SLAT/FLAP readout according to Load 23.1. Update Speedbrake Indication description. Update of Tail Strike avoidance function description. Update of Slat/Flap system interlocks description. Update of EICAS MESSAGES table according to Load 23.1. Update of VNAV altitude constraint annunciation. Update of CMF information. Delete CMF2 information. Language review. Inclusion of XPDR 1 (2) IN STBY EICAS message according to Load 23.1. Change the maximum fuel tank capacity to maximum fuel indicated to flight crew. Update of block title on footer. Inclusion of Handwheel Steering Mode for Airplanes equipped with NWSCM-04. Update of portable oxygen cylinder components description. Inclusion of inhibition phases for RAAS messages. Inclusion of TAIL STRIKE AVOID FAIL and XPDR 1 (2) IN STBY EICAS messages according to Load 23.1. Update of inhibition phase to ENG REF ECS DISAG EICAS message according to Load 23.1. Update of CAUTION definition on EICAS messages categorization.AOM-1502-017

Block 14-05-35 14-06-05 14-06-20 14-06-20 14-06-35 14-07-25 14-08-05 14-08-15 14-08-30 14-08-45 14-09-05 14-09-15 14-09-25 14-09-35 14-10-10 14-12-15 14-13-25 14-14-15 14-15-10

14-15-10

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AIRPLANE OPERATIONS MANUAL

LIST OF EFFECTIVE PAGES

LIST OF EFFECTIVE PAGES (VOLUME 1)ORIGINAL ...................................0 ................................... MAR 25, 2008 REVISION ...................................1 ................................... APR 29, 2008 REVISION ...................................2 ................................... OCT 31, 2008 REVISION ...................................3 ................................... AUG 03, 2009 REVISION ...................................4 ................................... APR 30, 2010

AOM-1502-017

Vol.1-LEPCopyright by Embraer. Refer to cover page for details.

REVISION 4

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REVISION 4

AOM-1502-017

AIRPLANE OPERATIONS MANUALBLOCK Vol.1-LEP Vol.1-LEP Vol.1-LEP Vol.1-LEP Vol.1-LEP Vol.1-LEP Vol.1-LEP Vol.1-LEP Vol.1-LEP Vol.1-LEP Vol.1-LEP Vol.1-LEP Vol.1-LEP Vol.1-LEP Vol.1-LEP Vol.1-LEP Vol.1-TOC Vol.1-TOC 1-TOC 1-TOC 1-01 1-01 1-01 1-01 1-01 1-01 1-10 1-10 1-20 (rev) 1-20 (rev) 1-20 (rev) 1-20 (rev) 1-20 (rev) 1-20 (rev) 1-20 (rev) 1-20 (rev) 1-20 (rev) 1-20 (rev) 1-20 (rev) 1-20 (rev) 1-20 (rev) 1-20 (rev)AOM-1502-017


(rev) (rev) (rev) (rev) (rev) (rev) (rev) (rev) (rev) (rev) (rev) (rev) (rev) (rev) (rev) (rev)

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REVISION Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Original Original Rev. 2 Rev. 2 Rev. 3 Rev. 3 Rev. 3 Rev. 3 Rev. 3 Rev. 3 Rev. 1 Rev. 1 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4

BLOCK 1-20 (rev) 1-20 (rev) 1-25 (rev) 1-25 (rev) 1-35 (rev) 1-35 (rev) 1-40 (rev) 1-40 (rev) 1-40 (rev) 1-40 (rev) 1-40 (rev) 1-40 (rev) 1-40 (rev) 1-40 (rev) 1-40 (rev) 1-40 (rev) 1-40 (rev) 1-40 (rev) 1-40 (rev) 1-40 (rev) 2-TOC (rev) 2-TOC (rev) 2-TOC (rev) 2-TOC (rev) 2-INTRO 2-INTRO 2-05 (rev) 2-05 (rev) 2-05 (add) 2-05 (add) 2-10 (rev) 2-10 (rev) 2-10 (rev) 2-10 (rev) 2-10 (rev) 2-10 (rev) 2-10 (add) 2-10 (add) 2-20 2-20 2-30 2-30

PAGE * 15 * 16 *1 *2 *1 *2 *1 *2 *3 *4 *5 *6 *7 *8 *9 * 10 * 11 * 12 * 13 * 14 *1 *2 *3 *4 1 2 *1 *2 *3 *4 *1 *2 *3 *4 *5 *6 *7 *8 1 2 1 2

REVISION Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 1 Rev. 1 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 3 Rev. 3 Rev. 1 Rev. 1

* Asterisk indicates pages revised (rev), added (add), or deleted (del), by the current revision.


REVISION 4

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AIRPLANE OPERATIONS MANUALREVISION Rev. 2 Rev. 2 Rev. 2 Rev. 2 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 3 Rev. 3 Rev. 1 Rev. 1 Rev. 1 Rev. 1 Rev. 4 Rev. 4 Rev. 3 Rev. 3 Rev. 1 Rev. 1 Rev. 1 Rev. 1 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 1 Rev. 1 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 1 Rev. 1 Rev. 4 Rev. 4 Rev. 4 Rev. 4 BLOCK 3-03 (rev) 3-03 (rev) 3-05 (rev) 3-05 (rev) 3-05 (rev) 3-05 (rev) 3-07 3-07 3-07 3-07 3-07 3-07 3-07 3-07 3-09 (rev) 3-09 (rev) 3-09 (rev) 3-09 (rev) 3-09 (rev) 3-09 (rev) 3-11 (rev) 3-11 (rev) 3-13 (rev) 3-13 (rev) 3-15 (rev) 3-15 (rev) 3-16 (rev) 3-16 (rev) 3-17 3-17 3-19 3-19 3-21 3-21 3-23 (rev) 3-23 (rev) 3-25 3-25 3-27 3-27 3-29 3-29 PAGE *1 *2 *1 *2 *3 *4 1 2 3 4 5 6 7 8 *1 *2 *3 *4 *5 *6 *1 *2 *1 *2 *1 *2 *1 *2 1 2 1 2 1 2 *1 *2 1 2 1 2 1 2 REVISION Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 3 Rev. 3 Rev. 3 Rev. 3 Rev. 3 Rev. 3 Rev. 3 Rev. 3 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 3 Rev. 3 Rev. 3 Rev. 3 Rev. 3 Rev. 3 Rev. 4 Rev. 4 Rev. 1 Rev. 1 Rev. 2 Rev. 2 Rev. 3 Rev. 3AOM-1502-017

BLOCK 2-36 2-36 2-38 2-38 2-40 (rev) 2-40 (rev) 2-40 (rev) 2-40 (rev) 2-48 2-48 2-50 2-50 2-56 2-56 2-57 (rev) 2-57 (rev) 2-57 (del) 2-57 (del) 2-60 2-60 2-60 2-60 2-64 (rev) 2-64 (rev) 2-64 (rev) 2-64 (rev) 2-64 (rev) 2-64 (rev) 2-64 (rev) 2-64 (rev) 2-66 2-66 2-68 (rev) 2-68 (rev) 3-TOC (rev) 3-TOC (rev) 3-INTRO 3-INTRO 3-01 (rev) 3-01 (rev) 3-01 (rev) 3-01 (rev)

PAGE 1 2 1 2 *1 *2 *3 *4 1 2 1 2 1 2 *1 *2 3 4 1 2 3 4 *1 *2 *3 *4 *5 *6 *7 *8 1 2 *1 *2 *1 *2 1 2 *1 *2 *3 *4



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REVISION 4

AIRPLANE OPERATIONS MANUALBLOCK 3-31 3-31 3-68 3-68 3-70 (rev) 3-70 (rev) 3-70 (rev) 3-70 (rev) 3-70 (rev) 3-70 (rev) 3-70 (rev) 3-70 (rev) 3-72 3-72 3-75 (rev) 3-75 (rev) 3-75 (rev) 3-75 (rev) 3-75 (rev) 3-75 (rev) 3-75 (rev) 3-75 (rev) 3-75 (rev) 3-75 (rev) 3-75 (rev) 3-75 (rev) 3-75 (rev) 3-75 (rev) 3-75 (rev) 3-75 (rev) 3-75 (rev) 3-75 (rev) 3-75 (rev) 3-75 (rev) 3-75 (rev) 3-75 (rev) 3-75 (rev) 3-75 (rev) 3-75 (rev) 3-75 (rev) 3-75 (rev) 3-75 (rev)AOM-1502-017


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BLOCK 3-75 (del) 3-75 (del) 3-75 (del) 3-75 (del) 3-75 (del) 3-75 (del) 3-80 (rev) 3-80 (rev) 3-80 (rev) 3-80 (rev) 3-80 (rev) 3-80 (rev) 3-80 (rev) 3-80 (rev) 3-80 (rev) 3-80 (rev) 3-80 (rev) 3-80 (rev) 3-94 3-94 3-95 (rev) 3-95 (rev) 3-95 (rev) 3-95 (rev) 3-95 (rev) 3-95 (rev) 3-95 (rev) 3-95 (rev) 3-97 3-97 3-97 3-97 3-97 3-97 4-TOC 4-TOC 4-INTRO (rev) 4-INTRO (rev) 4-INTRO (rev) 4-INTRO (rev) 4-01-01-TOC (rev) 4-01-01-TOC (rev)

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AIRPLANE OPERATIONS MANUALREVISION Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 BLOCK 4-02-01 (rev) 4-02-01 (rev) 4-02-01 (rev) 4-02-01 (rev) 4-02-01 (rev) 4-02-01 (rev) 4-02-01 (rev) 4-02-01 (rev) 4-02-01 (rev) 4-02-01 (rev) 4-02-01 (rev) 4-02-01 (rev) 4-02-01 (rev) 4-02-01 (rev) 4-02-01 (rev) 4-02-01 (rev) 4-02-01 (rev) 4-02-01 (rev) 4-02-01 (rev) 4-02-01 (rev) 4-02-01 (rev) 4-02-01 (rev) 4-02-01 (add) 4-02-01 (add) 4-02-01 (add) 4-02-01 (add) 4-03-01-TOC 4-03-01-TOC 4-03-01 4-03-01 4-03-01 4-03-01 4-03-01 4-03-01 4-03-02-TOC 4-03-02-TOC 4-03-02 (rev) 4-03-02 (rev) 4-03-02 (rev) 4-03-02 (rev) 4-03-02 (rev) 4-03-02 (rev) PAGE * 29 * 30 * 31 * 32 * 33 * 34 * 35 * 36 * 37 * 38 * 39 * 40 * 41 * 42 * 43 * 44 * 45 * 46 * 47 * 48 * 49 * 50 * 51 * 52 * 53 * 54 1 2 1 2 3 4 5 6 1 2 *1 *2 *3 *4 *5 *6 REVISION Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 3 Rev. 3 Rev. 3 Rev. 3 Rev. 3 Rev. 3 Rev. 3 Rev. 3 Original Original Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4AOM-1502-017

BLOCK 4-01-01 (rev) 4-01-01 (rev) 4-01-01 (rev) 4-01-01 (rev) 4-01-01 (rev) 4-01-01 (rev) 4-01-01 (rev) 4-01-01 (rev) 4-01-01 (rev) 4-01-01 (rev) 4-01-01 (del) 4-01-01 (del) 4-02-01-TOC (rev) 4-02-01-TOC (rev) 4-02-01 (rev) 4-02-01 (rev) 4-02-01 (rev) 4-02-01 (rev) 4-02-01 (rev) 4-02-01 (rev) 4-02-01 (rev) 4-02-01 (rev) 4-02-01 (rev) 4-02-01 (rev) 4-02-01 (rev) 4-02-01 (rev) 4-02-01 (rev) 4-02-01 (rev) 4-02-01 (rev) 4-02-01 (rev) 4-02-01 (rev) 4-02-01 (rev) 4-02-01 (rev) 4-02-01 (rev) 4-02-01 (rev) 4-02-01 (rev) 4-02-01 (rev) 4-02-01 (rev) 4-02-01 (rev) 4-02-01 (rev) 4-02-01 (rev) 4-02-01 (rev)

PAGE *1 *2 *3 *4 *5 *6 *7 *8 *9 * 10 * 11 * 12 *1 *2 *1 *2 *3 *4 *5 *6 *7 *8 *9 * 10 * 11 * 12 * 13 * 14 * 15 * 16 * 17 * 18 * 19 * 20 * 21 * 22 * 23 * 24 * 25 * 26 * 27 * 28



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REVISION 4

AIRPLANE OPERATIONS MANUALBLOCK 4-03-02 (rev) 4-03-02 (rev) 4-03-02 (rev) 4-03-02 (rev) 4-03-02 (rev) 4-03-02 (rev) 4-03-02 (rev) 4-03-02 (rev) 4-03-03-TOC 4-03-03-TOC 4-03-03 4-03-03 4-03-03 4-03-03 4-03-03 4-03-03 4-03-03 (del) 4-03-03 (del) 4-03-04-TOC 4-03-04-TOC 4-03-04 4-03-04 4-03-04 4-03-04 4-03-05-TOC 4-03-05-TOC 4-03-05 (rev) 4-03-05 (rev) 4-03-05 (rev) 4-03-05 (rev) 4-03-05 (rev) 4-03-05 (rev) 4-03-05 (rev) 4-03-05 (rev) 4-03-05 (rev) 4-03-05 (rev) 4-03-05 (rev) 4-03-05 (rev) 4-03-05 (rev) 4-03-05 (rev) 4-03-05 (rev) 4-03-05 (rev)AOM-1502-017


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BLOCK 4-03-05 (rev) 4-03-05 (rev) 4-03-06-TOC (rev) 4-03-06-TOC (rev) 4-03-06 (rev) 4-03-06 (rev) 4-03-06 (rev) 4-03-06 (rev) 4-03-06 (rev) 4-03-06 (rev) 4-03-06 (rev) 4-03-06 (rev) 4-03-06 (rev) 4-03-06 (rev) 4-03-06 (add) 4-03-06 (add) 4-03-07-TOC 4-03-07-TOC 4-03-07 (rev) 4-03-07 (rev) 4-03-07 (rev) 4-03-07 (rev) 4-03-07 (rev) 4-03-07 (rev) 4-03-08-TOC (rev) 4-03-08-TOC (rev) 4-03-08 (rev) 4-03-08 (rev) 4-03-08 (rev) 4-03-08 (rev) 4-03-08 (rev) 4-03-08 (rev) 4-03-08 (rev) 4-03-08 (rev) 4-03-08 (rev) 4-03-08 (rev) 4-03-08 (rev) 4-03-08 (rev) 4-03-08 (rev) 4-03-08 (rev) 4-03-08 (rev) 4-03-08 (rev)

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REVISION 4

Page 5


AIRPLANE OPERATIONS MANUALREVISION Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 3 Rev. 3 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 BLOCK 4-03-11-TOC 4-03-11-TOC 4-03-11 (rev) 4-03-11 (rev) 4-03-11 (rev) 4-03-11 (rev) 4-03-11 (rev) 4-03-11 (rev) 4-03-12-TOC 4-03-12-TOC 4-03-12 (rev) 4-03-12 (rev) 4-03-12 (rev) 4-03-12 (rev) 4-03-12 (rev) 4-03-12 (rev) 4-03-12 (rev) 4-03-12 (rev) 4-03-12 (rev) 4-03-12 (rev) 4-03-13-TOC 4-03-13-TOC 4-03-13 (rev) 4-03-13 (rev) 4-03-13 (rev) 4-03-13 (rev) 4-03-13 (rev) 4-03-13 (rev) 4-03-13 (rev) 4-03-13 (rev) 4-03-14-TOC 4-03-14-TOC 4-03-14 4-03-14 4-04-54-TOC 4-04-54-TOC 4-04-54 4-04-54 4-04-54 4-04-54 4-04-54 4-04-54 PAGE 1 2 *1 *2 *3 *4 *5 *6 *1 *2 *1 *2 *3 *4 *5 *6 *7 *8 *9 * 10 *1 *2 *1 *2 *3 *4 *5 *6 *7 *8 1 2 1 2 1 2 1 2 3 4 5 6 REVISION Rev. 3 Rev. 3 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Original Original Rev. 1 Rev. 1 Original Original Rev. 1 Rev. 1 Rev. 1 Rev. 1 Rev. 1 Rev. 1AOM-1502-017

BLOCK 4-03-08 (rev) 4-03-08 (rev) 4-03-08 (rev) 4-03-08 (rev) 4-03-08 (rev) 4-03-08 (rev) 4-03-08 (add) 4-03-08 (add) 4-03-09-TOC (rev) 4-03-09-TOC (rev) 4-03-09-TOC (rev) 4-03-09-TOC (rev) 4-03-09 (rev) 4-03-09 (rev) 4-03-09 (rev) 4-03-09 (rev) 4-03-09 (rev) 4-03-09 (rev) 4-03-09 (rev) 4-03-09 (rev) 4-03-09 (rev) 4-03-09 (rev) 4-03-09 (rev) 4-03-09 (rev) 4-03-09 (rev) 4-03-09 (rev) 4-03-09 (rev) 4-03-09 (rev) 4-03-09 (rev) 4-03-09 (rev) 4-03-09 (rev) 4-03-09 (rev) 4-03-10-TOC 4-03-10-TOC 4-03-10 (rev) 4-03-10 (rev) 4-03-10 (rev) 4-03-10 (rev) 4-03-10 (rev) 4-03-10 (rev) 4-03-10 (rev) 4-03-10 (rev)

PAGE * 17 * 18 * 19 * 20 * 21 * 22 * 23 * 24 *1 *2 *3 *4 *1 *2 *3 *4 *5 *6 *7 *8 *9 * 10 * 11 * 12 * 13 * 14 * 15 * 16 * 17 * 18 * 19 * 20 1 2 *1 *2 *3 *4 *5 *6 *7 *8

(rev) (rev)

(rev) (rev)



Page 6

REVISION 4

AIRPLANE OPERATIONS MANUALBLOCK 4-04-56-TOC 4-04-56-TOC 4-04-56 4-04-56 4-04-57-TOC 4-04-57-TOC 4-04-57 4-04-57 5-TOC (rev) 5-TOC (rev) 5-01 5-01 5-01 5-01 5-10 (rev) 5-10 (rev) 5-10 (rev) 5-10 (rev) 5-10 (rev) 5-10 (rev) 5-10 (rev) 5-10 (rev) 5-15 5-15 5-15 5-15 5-15 5-15 5-15 5-15 5-15 5-15 5-15 5-15 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev)AOM-1502-017


PAGE 1 2 1 2 1 2 1 2 *1 *2 1 2 3 4 *1 *2 *3 *4 *5 *6 *7 *8 1 2 3 4 5 6 7 8 9 10 11 12 *1 *2 *3 *4 *5 *6 *7 *8

REVISION Original Original Rev. 1 Rev. 1 Rev. 2 Rev. 2 Rev. 2 Rev. 2 Rev. 4 Rev. 4 Rev. 1 Rev. 1 Rev. 1 Rev. 1 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 3 Rev. 3 Rev. 3 Rev. 3 Rev. 3 Rev. 3 Rev. 3 Rev. 3 Rev. 3 Rev. 3 Rev. 3 Rev. 3 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4

BLOCK 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev)

PAGE *9 * 10 * 11 * 12 * 13 * 14 * 15 * 16 * 17 * 18 * 19 * 20 * 21 * 22 * 23 * 24 * 25 * 26 * 27 * 28 * 29 * 30 * 31 * 32 * 33 * 34 * 35 * 36 * 37 * 38 * 39 * 40 * 41 * 42 * 43 * 44 * 45 * 46 * 47 * 48 * 49 * 50




REVISION 4

Page 7


AIRPLANE OPERATIONS MANUALREVISION Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 1 Rev. 1 Rev. 1 Rev. 1 Rev. 1 Rev. 1 Rev. 1 Rev. 1 BLOCK 5-30 (rev) 5-30 (rev) 5-30 (rev) 5-30 (rev) 5-30 (rev) 5-30 (rev) 5-30 (rev) 5-30 (rev) 5-30 (rev) 5-30 (rev) 5-30 (rev) 5-30 (rev) 5-30 (rev) 5-30 (rev) 5-30 (rev) 5-30 (rev) 5-30 (rev) 5-30 (rev) 5-35 (rev) 5-35 (rev) 5-35 (rev) 5-35 (rev) 5-35 (rev) 5-35 (rev) 5-35 (rev) 5-35 (rev) 5-35 (rev) 5-35 (rev) 5-35 (rev) 5-35 (rev) 5-35 (rev) 5-35 (rev) 5-35 (rev) 5-35 (rev) 5-35 (rev) 5-35 (rev) 5-35 (rev) 5-35 (rev) 5-35 (rev) 5-35 (rev) 5-35 (rev) 5-35 (rev) PAGE *1 *2 *3 *4 *5 *6 *7 *8 *9 * 10 * 11 * 12 * 13 * 14 * 15 * 16 * 17 * 18 *1 *2 *3 *4 *5 *6 *7 *8 *9 * 10 * 11 * 12 * 13 * 14 * 15 * 16 * 17 * 18 * 19 * 20 * 21 * 22 * 23 * 24 REVISION Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4AOM-1502-017

BLOCK 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-20 (rev) 5-25 5-25 5-25 5-25 5-25 5-25 5-25 5-25

PAGE * 51 * 52 * 53 * 54 * 55 * 56 * 57 * 58 * 59 * 60 * 61 * 62 * 63 * 64 * 65 * 66 * 67 * 68 * 69 * 70 * 71 * 72 * 73 * 74 * 75 * 76 * 77 * 78 * 79 * 80 * 81 * 82 * 83 * 84 1 2 3 4 5 6 7 8



Page 8

REVISION 4

AIRPLANE OPERATIONS MANUALBLOCK 5-35 (rev) 5-35 (rev) 5-35 (rev) 5-35 (rev) 5-35 (rev) 5-35 (rev) 5-35 (rev) 5-35 (rev) 5-35 (rev) 5-35 (rev) 5-35 (add) 5-35 (add) 5-35 (add) 5-35 (add) 5-35 (add) 5-35 (add) 5-35 (add) 5-35 (add) 5-35 (add) 5-35 (add) 5-35 (add) 5-35 (add) 5-35 (add) 5-35 (add) 5-35 (add) 5-35 (add) 5-35 (add) 5-35 (add) 5-35 (add) 5-35 (add) 5-35 (add) 5-35 (add) 5-35 (add) 5-35 (add) 5-40 5-40 6-TOC (rev) 6-TOC (rev) 6-05 6-05 6-05 6-05AOM-1502-017


PAGE * 25 * 26 * 27 * 28 * 29 * 30 * 31 * 32 * 33 * 34 * 35 * 36 * 37 * 38 * 39 * 40 * 41 * 42 * 43 * 44 * 45 * 46 * 47 * 48 * 49 * 50 * 51 * 52 * 53 * 54 * 55 * 56 * 57 * 58 1 2 *1 *2 1 2 3 4


BLOCK 6-05 6-05 6-05 6-05 6-05 6-05 6-05 6-05 6-05 6-05 6-05 6-05 6-05 6-05 6-05 6-05 6-07 6-07 6-10 6-10 6-10 6-10 6-10 6-10 6-10 6-10 6-10 6-10 6-10 6-10 6-10 6-10 6-10 6-10 6-10 6-10 6-10 6-10 6-10 6-10 6-10 6-10

PAGE 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 1 2 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24




REVISION 4

Page 9


AIRPLANE OPERATIONS MANUALREVISION Rev. 2 Rev. 2 Rev. 2 Rev. 2 Rev. 2 Rev. 2 Rev. 2 Rev. 2 Rev. 2 Rev. 2 Rev. 2 Rev. 2 Rev. 2 Rev. 2 Rev. 2 Rev. 2 Rev. 2 Rev. 2 Rev. 2 Rev. 2 Rev. 2 Rev. 2 Rev. 2 Rev. 2 Rev. 2 Rev. 2 Rev. 2 Rev. 2 Rev. 2 Rev. 2 Rev. 2 Rev. 2 Rev. 2 Rev. 2 Rev. 2 Rev. 2 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 BLOCK 6-15 (rev) 6-15 (rev) 6-15 (rev) 6-15 (rev) 6-15 (rev) 6-15 (rev) 6-15 (rev) 6-15 (rev) 6-15 (rev) 6-15 (rev) 6-15 (rev) 6-15 (rev) 6-15 (rev) 6-15 (rev) 6-15 (rev) 6-15 (rev) 6-15 (rev) 6-15 (rev) 6-15 (rev) 6-15 (rev) 6-15 (rev) 6-15 (rev) 6-15 (rev) 6-15 (rev) 6-15 (rev) 6-15 (rev) 6-15 (rev) 6-15 (rev) 6-15 (rev) 6-15 (rev) 6-15 (rev) 6-15 (rev) 6-15 (rev) 6-15 (rev) 6-15 (rev) 6-15 (rev) 6-15 (rev) 6-15 (rev) 6-15 (del) 6-15 (del) 6-15 (del) 6-15 (del) PAGE *7 *8 *9 * 10 * 11 * 12 * 13 * 14 * 15 * 16 * 17 * 18 * 19 * 20 * 21 * 22 * 23 * 24 * 25 * 26 * 27 * 28 * 29 * 30 * 31 * 32 * 33 * 34 * 35 * 36 * 37 * 38 * 39 * 40 * 41 * 42 * 43 * 44 * 45 * 46 * 47 * 48 REVISION Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4AOM-1502-017

BLOCK 6-10 6-10 6-10 6-10 6-10 6-10 6-10 6-10 6-10 6-10 6-10 6-10 6-10 6-10 6-10 6-10 6-10 6-10 6-10 6-10 6-10 6-10 6-10 6-10 6-10 6-10 6-10 6-10 6-10 6-10 6-10 6-10 6-10 6-10 6-10 6-10 6-15 (rev) 6-15 (rev) 6-15 (rev) 6-15 (rev) 6-15 (rev) 6-15 (rev)

PAGE 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 *1 *2 *3 *4 *5 *6



Page 10

REVISION 4

AIRPLANE OPERATIONS MANUALBLOCK 6-15 (del) 6-15 (del) 6-15 (del) 6-15 (del) 6-15 (del) 6-15 (del) 6-15 (del) 6-15 (del) 6-15 (del) 6-15 (del) 6-15 (del) 6-15 (del) 6-15 (del) 6-15 (del) 6-15 (del) 6-15 (del) 6-15 (del) 6-15 (del) 6-20 6-20 6-20 6-20 6-20 6-20 6-25 6-25 6-25 6-25 6-25 6-25 6-25 6-25 6-25 6-25 6-25 6-25 6-25 6-25 6-30 6-30 6-30 6-30AOM-1502-017


PAGE * 49 * 50 * 51 * 52 * 53 * 54 * 55 * 56 * 57 * 58 * 59 * 60 * 61 * 62 * 63 * 64 * 65 * 66 1 2 3 4 5 6 1 2 3 4 5 6 7 8 9 10 11 12 13 14 1 2 3 4


BLOCK 6-30 6-30 6-30 6-30 6-30 6-30 6-30 6-30 6-30 6-30 6-30 6-30 6-30 6-30 6-30 6-30 6-30 6-30 6-30 6-30 6-30 6-30 6-30 6-30 6-30 6-30 6-35 (rev) 6-35 (rev) 6-35 (rev) 6-35 (rev) 6-35 (add) 6-35 (add) 7-TOC (rev) 7-TOC (rev) 7-INTRO 7-INTRO 7-05 7-05 7-05 7-05 7-10 (rev) 7-10 (rev)

PAGE 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 *1 *2 *3 *4 *5 *6 *1 *2 1 2 1 2 3 4 *1 *2




REVISION 4

Page 11


AIRPLANE OPERATIONS MANUALREVISION Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Original Original Rev. 1 Rev. 1 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 1 Rev. 1 Rev. 2 Rev. 2 Rev. 2 Rev. 2 Rev. 3 Rev. 3 Rev. 3 Rev. 3 Rev. 3 Rev. 3 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 3 Rev. 3 BLOCK 8-60 8-60 8-60 8-60 8-60 8-60 8-60 8-60 8-70 8-70 8-70 8-70 8-70 8-70 8-70 (del) 8-70 (del) 8-90 8-90 8-90 8-90 9-TOC 9-TOC 9-01 9-01 10-TOC 10-TOC 10-01 10-01 11-TOC 11-TOC 11-INTRO 11-INTRO 11-05 (rev) 11-05 (rev) 11-05 (rev) 11-05 (rev) 11-05 (rev) 11-05 (rev) 11-06 11-06 11-06 11-06 PAGE 3 4 5 6 7 8 9 10 1 2 3 4 5 6 7 8 1 2 3 4 1 2 1 2 1 2 1 2 1 2 1 2 *1 *2 *3 *4 *5 *6 1 2 3 4 REVISION Rev. 3 Rev. 3 Rev. 3 Rev. 3 Rev. 3 Rev. 3 Rev. 3 Rev. 3 Rev. 2 Rev. 2 Rev. 2 Rev. 2 Rev. 2 Rev. 2 Rev. 2 Rev. 2 Rev. 1 Rev. 1 Rev. 1 Rev. 1 Original Original Rev. 1 Rev. 1 Original Original Rev. 1 Rev. 1 Rev. 3 Rev. 3 Rev. 1 Rev. 1 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 2 Rev. 2 Rev. 2 Rev. 2AOM-1502-017

BLOCK 7-10 (rev) 7-10 (rev) 7-10 (rev) 7-10 (rev) 7-10 (rev) 7-10 (rev) 7-10 (del) 7-10 (del) 7-15 (rev) 7-15 (rev) 7-15 (rev) 7-15 (rev) 7-15 (rev) 7-15 (rev) 7-15 (rev) 7-15 (rev) 8-TOC 8-TOC 8-INTRO 8-INTRO 8-10 (rev) 8-10 (rev) 8-10 (rev) 8-10 (rev) 8-20 8-20 8-30 8-30 8-30 8-30 8-40 8-40 8-40 8-40 8-40 8-40 8-50 (rev) 8-50 (rev) 8-50 (rev) 8-50 (rev) 8-60 8-60

PAGE *3 *4 *5 *6 *7 *8 *9 * 10 *1 *2 *3 *4 *5 *6 *7 *8 1 2 1 2 *1 *2 *3 *4 1 2 1 2 3 4 1 2 3 4 5 6 *1 *2 *3 *4 1 2



Page 12

REVISION 4

AIRPLANE OPERATIONS MANUALBLOCK 11-08 11-08 11-08 11-08 11-08 11-08 11-10 (rev) 11-10 (rev) 11-12 (rev) 11-12 (rev) 11-12 (rev) 11-12 (rev) 11-15 (rev) 11-15 (rev) 11-20 11-20 11-20 11-20 11-25 11-25 11-30 (rev) 11-30 (rev) 12-TOC 12-TOC 12-INTRO 12-INTRO 12-05 12-05 12-40 12-40 12-40 12-40 12-40 12-40 12-40 12-40 12-40 12-40 12-40 12-40 12-40 12-40AOM-1502-017


PAGE 1 2 3 4 5 6 *1 *2 *1 *2 *3 *4 *1 *2 1 2 3 4 1 2 *1 *2 1 2 1 2 1 2 1 2 3 4 5 6 7 8 9 10 11 12 13 14

REVISION Rev. 1 Rev. 1 Rev. 1 Rev. 1 Rev. 1 Rev. 1 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 3 Rev. 3 Rev. 3 Rev. 3 Rev. 1 Rev. 1 Rev. 4 Rev. 4 Original Original Rev. 1 Rev. 1 Rev. 3 Rev. 3 Rev. 3 Rev. 3 Rev. 3 Rev. 3 Rev. 3 Rev. 3 Rev. 3 Rev. 3 Rev. 3 Rev. 3 Rev. 3 Rev. 3 Rev. 3 Rev. 3

BLOCK 12-40 12-40 13-TOC 13-TOC 13-INTRO 13-INTRO 13-05 13-05 13-05 13-05 13-05 13-05 13-05 (del) 13-05 (del) 13-10 (rev) 13-10 (rev) 13-10 (rev) 13-10 (rev) 13-10 (rev) 13-10 (rev) 13-10 (rev) 13-10 (rev) 13-10 (rev) 13-10 (rev) 13-11 (rev) 13-11 (rev) 13-11 (rev) 13-11 (rev) 13-11 (rev) 13-11 (rev) 13-11 (del) 13-11 (del) 13-11 (del) 13-11 (del) 13-15 13-15 13-15 13-15 13-25 (rev) 13-25 (rev) 13-25 (rev) 13-25 (rev)

PAGE 15 16 1 2 1 2 1 2 3 4 5 6 7 8 1 * *2 *3 *4 *5 *6 *7 *8 *9 * 10 *1 *2 *3 *4 *5 *6 *7 *8 *9 * 10 1 2 3 4 *1 *2 *3 *4




REVISION 4

Page 13


AIRPLANE OPERATIONS MANUALREVISION Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 1 Rev. 1 Rev. 1 Rev. 1 Rev. 1 Rev. 1 Rev. 1 Rev. 1 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 2 Rev. 2 Rev. 1 Rev. 1 Rev. 1 Rev. 1 Rev. 1 Rev. 1 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 BLOCK 13-60 (rev) 13-60 (rev) 13-60 (rev) 13-60 (rev) 13-60 (rev) 13-60 (rev) 13-60 (rev) 13-60 (rev) 13-60 (rev) 13-60 (rev) 13-60 (rev) 13-60 (rev) 13-60 (rev) 13-60 (rev) 13-60 (rev) 13-60 (rev) 13-60 (rev) 13-60 (rev) 13-60 (rev) 13-60 (rev) 13-60 (rev) 13-60 (rev) 13-60 (rev) 13-60 (rev) 13-60 (rev) 13-60 (rev) 13-60 (rev) 13-60 (rev) 13-60 (rev) 13-60 (rev) 13-60 (rev) 13-60 (rev) 13-60 (rev) 13-60 (rev) 13-60 (rev) 13-60 (rev) 13-60 (rev) 13-60 (rev) 13-60 (rev) 13-60 (rev) 13-60 (del) 13-60 (del) PAGE *7 *8 *9 * 10 * 11 * 12 * 13 * 14 * 15 * 16 * 17 * 18 * 19 * 20 * 21 * 22 * 23 * 24 * 25 * 26 * 27 * 28 * 29 * 30 * 31 * 32 * 33 * 34 * 35 * 36 * 37 * 38 * 39 * 40 * 41 * 42 * 43 * 44 * 45 * 46 47 48 REVISION Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 3 Rev. 3AOM-1502-017

BLOCK 13-25 (rev) 13-25 (rev) 13-25 (rev) 13-25 (rev) 13-25 (rev) 13-25 (rev) 13-25 (rev) 13-25 (rev) 13-30 13-30 13-30 13-30 13-35 13-35 13-35 13-35 13-40 (rev) 13-40 (rev) 13-40 (rev) 13-40 (rev) 13-40 (rev) 13-40 (rev) 13-45 (rev) 13-45 (rev) 13-45 (rev) 13-45 (rev) 13-45 (rev) 13-45 (rev) 13-45 (del) 13-45 (del) 13-50 13-50 13-50 13-50 13-55 13-55 13-60 (rev) 13-60 (rev) 13-60 (rev) 13-60 (rev) 13-60 (rev) 13-60 (rev)

PAGE *5 *6 *7 *8 *9 * 10 * 11 * 12 1 2 3 4 1 2 3 4 *1 *2 *3 *4 *5 *6 *1 *2 *3 *4 *5 *6 7 8 1 2 3 4 1 2 *1 *2 *3 *4 *5 *6



Page 14

REVISION 4

AIRPLANE OPERATIONS MANUALBLOCK 13-70 (rev) 13-70 (rev) 13-70 (rev) 13-70 (rev) 13-70 (rev) 13-70 (rev) 13-70 (rev) 13-70 (rev) 13-70 (rev) 13-70 (rev) 13-70 (rev) 13-70 (rev) PAGE *1 *2 *3 *4 *5 *6 *7 *8 *9 * 10 * 11 * 12 REVISION Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4 Rev. 4


AOM-1502-017



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REVISION 4

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TABLE OF CONTENTS

VOLUME 1 TABLE OF CONTENTS

SECTION 1 SECTION 2 SECTION 3 SECTION 4 SECTION 5 SECTION 6 SECTION 7 SECTION 8 SECTION 9 SECTION 10 SECTION 11 SECTION 12 SECTION 13

GENERAL INFORMATION AND DEFINITION OF TERMS LIMITATIONS NORMAL PROCEDURES EMERGENCY AND ABNORMAL PROCEDURES PERFORMANCE FLIGHT PLANNING WEIGHT AND BALANCE LOADING CONFIGURATION DEVIATION LIST MINIMUM EQUIPMENT LIST EMERGENCY INFORMATION EMERGENCY EVACUATION GROUND SERVICING

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ORIGINAL

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GENERAL INFORMATION AND DEFINITION OF TERMS

SECTION 1 GENERAL INFORMATION AND DEFINITION OF TERMSTABLE OF CONTENTS Block Page 1 1 1 2 2 2 3 4 4 1 1 1 1 1 1 1 1 1 1

General Information............................................. 1-01 ........... GENERAL.............................................................. 1-01 ........... REVISIONS............................................................ 1-01 ........... TEMPORARY REVISIONS.................................... 1-01 ........... LIST OF EFFECTIVE PAGES............................... 1-01 ...........Effectivity range to which this information is applicable

EFFECTIVITY........................................................ 1-01 ........... OPERATIONAL REQUIREMENTS AND THE AIRPLANE OPERATIONS MANUAL............... 1-01 ........... EMBRAER AIRPLANE OPERATIONS MANUAL. . 1-01 ........... AIRPLANE OPERATIONS MANUAL STRUCTURE................................................... 1-01 ........... Definition of Terms.............................................. 1-10 ........... DEFINITION OF TERMS....................................... 1-10 ........... Abbreviations and Acronyms............................. 1-20 ........... ABBREVIATIONS AND ACRONYMS.................... 1-20 ........... Units Conversion................................................. 1-25 ........... UNITS CONVERSION........................................... 1-25 ........... Service Bulletins.................................................. 1-35 ........... SERVICE BULLETIN TABLE................................. 1-35 ........... Airplane Models Differences............................... 1-40 ........... EMBRAER 170/175 X 190/195.............................. 1-40 ...........

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AOM-1502-017



GENERALThis Airplane Operations Manual provides useful information to complement the Airplane Flight Manual, Weight and Balance Manual and the Master Minimum Equipment List. It must be used in conjunction with those publications to safe and efficiently operate the airplane. Any difference found between the data in the Airplane Operations Manual and the approved manuals is attributable to airplane modifications and scheduling of amendments to publications. In the event of such a difference, the data contained in the approved manuals must prevail.

REVISIONSEmbraer may periodically revise this manual as required to update information or to provide information not available at the time of last issue. Revised data may result from either airplane modifications or improved techniques gained through operational experience. Changes to the content are indicated by a vertical line in the outside page margin, at the direction of revised text, graphic or table. A deleted text, graph or table is marked by a vertical line in the outside margin, at the direction of immediate previous line. A deleted table row is marked by a vertical line in the outside margin, at the direction of immediate next row. For relocated or rearranged contents, the vertical line marker is drawn adjacent to the page number. The basic issue date of this Manual is presented on the title page. Subsequent revisions are sequentially numbered (Revision 1, Revision 2, and so forth). The last Revision number is presented on the title page and on the footer of every page affected, replacing the former number. The status of each page is presented in the List of Effective Pages (LEP).

AOM-1502-017

1-01Copyright by Embraer. Refer to cover page for details.

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General Information

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TEMPORARY REVISIONSTemporary revisions may be issued when the need arises. The temporary revision pages will be clearly identified and they are to be inserted adjacent to the affected page. Temporary revisions description are presented at the Log of Temporary Revisions. Temporary revision pages status is not included in the List of Effective Pages. Temporary revision pages shall be removed when the changed content is either incorporated or canceled by a Revision.

LIST OF EFFECTIVE PAGESA List of Effective Pages (LEP) for all the sections is located at the beginning of this Manual. The LEP presents the list of revision numbers with the corresponding revision date, as well as the roll of pages with the current revision number. The LEP is updated at every revision, and it is the reference to verify each Manual page for its proper updating status.

EFFECTIVITY

!Effectivity range to which this information is applicable

Texts, tables and graphics applicable to a specific airplane range are identified by: a preceding start tag and text (presented in a different font type) and an end tag at the final of the marked element. This paragraph constitutes an example of effectivity text.

SUB-EFFECTIVITY

!!Sub-effectivity range to which this information is applicable

When the information is applicable to a specific range within a marked range, they are identified by: a double start tag and text and a double end tag at the final of the marked element. This paragraph constitutes an example of sub-effectivity text."" "


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General Information

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AOM-1502-017



OPERATIONAL REQUIREMENTS AND AIRPLANE OPERATIONS MANUAL

THE

The existence of fleets composed of airplanes or other aircraft types built by different manufacturers, led the Airworthiness Authorities to require operators certification, in addition to the airplanes certification. The idea is to standardize manuals, training and operation, so as to make it easier for a pilot to change equipment. As an example, if a pilot used to fly an EMBRAER airplane (ERJ-145) is scheduled to fly another EMBRAER airplane (EMBRAER 170/175/190/195), the training syllabus required for both airplane families/models needs to be very similar; the operators normal, abnormal and emergency procedures presentation must be similar for all airplanes even when there are different AFMs with different presentation for those procedures, as well as the manuals for both airplanes. By doing so, the operator will assure that human factors/errors are minimized. Some Operation Requirements just define the main subjects that must be presented in an Airplane Operations Manual. However, even detailing the AOM at that level, all the requirements let the operators free to use different Airplane Operations Manual structures, depending on the manuals that have been already issued. Therefore, EMBRAER has developed this AOM in an attempt to cover, in the best possible manner, the most currently used requirements. By doing so, it is possible for an operator to use the EMBRAER AOM by just adding some missing information that is specific to that operator. Below is a suggested Airplane Operations Manual structure to comply with most of the Operation Requirements:

PART APresents operators administrative information, such as who are the president, vice-president, the managers, who is the chief pilot for the fleet, who is the responsible for revising manuals, where the offices and bases are located, etc.

PART BPresents airplane related information, such as procedures, performance, dispatch, Weight and Balance, bulletins and systems description.AOM-1502-017


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PART CPresents the operators airport and route information (performance and navigation).

PART DPresents training information.

EMBRAER AIRPLANE OPERATIONS MANUALThis Embraer Airplane Operations Manual covers only Part B. Parts A and D should be generated by the operator only. Part C can be generated by the operator with the help of Embraer operations softwares (runway analysis, driftdown, and route analysis).

AIRPLANE OPERATIONS MANUAL STRUCTUREThe Embraer Airplane Operations Manual is organized in two volumes, with the following contents: Volume 1: 1 General 2 Limitations 3 4 5 6 7 8 Normal Procedures Emergency and Abnormal Procedures Performance Flight Planning Weight and Balance Loading

9 Configuration Deviation List 10 Minimum Equipment List 11 Emergency Information 12 Emergency Evacuation 13 Ground Servicing Volume 2: 14-01 Airplane Description 14-02 Air Management System 14-03 Automatic Flight


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AOM-1502-017

AIRPLANE OPERATIONS MANUAL 14-04 Auxiliary Power Unit 14-05 Electrical 14-06 Engine


14-07 Fire Protection 14-08 Flight Controls 14-09 Flight Instruments, Communication, Navigation and Flight Management System 14-10 Fuel 14-11 Hydraulic 14-12 14-13 14-14 14-15 Ice and Rain Protection Landing Gear and Brakes Oxygen Warning System

Each of the above sections may be divided into smaller parts, called blocks. The number of the section followed by a two-digit number identifies such blocks. For example: Section 14-03 can be divided as follows: 14-03-01 General Description 14-03-05 14-03-10 14-03-20 14-03-30 Controls and Indications Flight Guidance Control System Thrust Management EICAS Messages

The page numbering restarts at each block.

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AOM-1502-017



DEFINITION OF TERMSThe following definitions apply to the terms below: WARNING: OPERATING PROCEDURES, TECHNIQUES AND OTHER RELATED INFORMATION, WHICH MAY RESULT IN PERSONAL INJURY OR LOSS OF LIFE, IF NOT FOLLOWED. CAUTION: OPERATING PROCEDURES, TECHNIQUES AND OTHER RELATED INFORMATION, WHICH MAY RESULT IN DAMAGE OR DESTRUCTION OF EQUIPMENT, IF NOT FOLLOWED. NOTE: Operating procedures, techniques and other related information, which are considered essential to emphasize the safety of flight.

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Definition of Terms

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Definition of Terms

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ABBREVIATIONS AND ACRONYMSABBREVIATION C F A A/C A/I ABM ABV AC ACARS ACE ACMP ACN ACP ACT ADA ADC ADF ADI ADS ADSP AFCS AFE AFM AFU AGL AICC AIOP AIP ALTAOM-1502-017

DESCRIPTION Degree Degree Celsius Degree Fahrenheit Liter Ampere Aircraft Anti-Ice Auto Brake Control Module Auxiliary Power-Unit Bleed-Valve Advisory Circular Aircraft Communication Addressing and Reporting System Actuator Control Electronics Alternating-Current Motor-Driven Pump Aircraft Classification Number Audio Control Panel Altitude Compensated Tilt Air Data Application Air Data Computer Automatic Direction Finder Attitude Director Indicator Air Data System Air Data Smart Probe Automatic-Flight Control System Above Field Elevation Airplane Flight Manual Artificial Feel Unit Above Ground Level Auxiliary Integrated Control-Center Actuator Input-Output Processor Aeronautical Information Publication Altitude


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Abbreviations and Acronyms

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ABBREVIATION AMM AMS ANAC ANR AOA AOC AOM AP APM APP APPR APR APU ARINC ASCB ASEL ASTM AT ATA ATC ATIS ATS ATTCS ATTND AUTO AVAIL AVOD AWS AZFW BARO BATT BC BCM BEW

DESCRIPTION Aircraft Maintenance Manual Air Management System Agncia Nacional de Aviao Civil Automatic Navigation Realignment Angle of Attack Airline Operational Communications Airplane Operations Manual Automatic Pilot Aircraft Personality Module Autopilot Panel Approach Approach Auxiliary Power Unit Aeronautical Radio Incorporated Avionics Standard-Communication Bus Altitude Preselect American Society of Testing Material Autothrottle Air Transport Association of America Air Traffic Control Automatic-Terminal-Information Service Air Turbine Starter Automatic Takeoff-Thrust Control-System Attendant Automatic Available Audio and Video on Demand Aural Warning System Actual Zero Fuel Weight Barometric Setting Battery Back Course Brake Control Module Basic Empty Weight


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AOM-1502-017

AIRPLANE OPERATIONS MANUAL ABBREVIATION BFO BIT BITE BOD BRG BRT BTC CAB CAFM CAGE CAS CAT I CAT II CB CCD CDL CFR CG CGD CH CLR cm CMC CMF CMS COMM CON CPC CPCS CRS CRZ CTRL CVR DBAOM-1502-017


DESCRIPTION Beat Frequency Oscillator Built-in Test Built-in Test Equipment Bottom of Descent Bearing Bright Bus Tie Contactor Cabin Computerized Airplane Flight Manual Commercial and Government Entity Calibrated Airspeed Category I Operation Category II Operation Circuit Breaker Cursor Control Device Configuration Deviation List Code of Federal Regulations Center of Gravity Corrected Ground Distance Channel Clear Centimeter Central Maintenance Computer Communications Management Function Configuration Management System Communications Continuous Cabin Pressure Controller Cabin Pressure Control-System Course Cruise Control Cockpit Voice Recorder Database


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ABBREVIATION DC DDPM DET DGRAD DH DIM DLK DME DMU DN DO DOW DR DU DVDR E-BAY EADI EBV ECAFM ECEF ECL ECS EDP EDS EDU EFB EGPWM EGPWS EGT EHSI EICAS EICC ELPU ELT

DESCRIPTION Direct Current Dispatch-Deviation Procedures Manual Detector Degraded Decision Height Dimmer Datalink Distance Measuring Equipment Data-Loader Management Unit Down RTCA Document Dry Operating Weight Dead Reckoning Display Unit Digital Voice-Data Recorder Electronic Bay Electronic Attitude Director Indicator Engine Bleed Valve Electronic Computerized AFM Earth-Centered Earth-Fixed Electronic Checklist Environmental Control System Engine Driven Pump Electronic Display System Electronic Display Unit Electronic Flight Bag Enhanced Ground-Proximity Warning-Module Enhanced Ground-Proximity Warning-System Exhaust Gas Temperature Electronic Horizontal Situation-Indicator Engine Indicating and Crew Alerting System Emergency Integrated Control-Center Emergency Lights Power Unit Emergency Locator Transmitter


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AOM-1502-017

AIRPLANE OPERATIONS MANUAL ABBREVIATION EMERG ENG EPNL EPU ESS ETA ETC ETE ETP FAA FADEC FAF FAP FAR FAWP FBW FCM FCOC FCP FCU FCV FD FDR FGCS FIM FIREX FLCH FLEX FMA FMS FMU FOM FPA FPLAOM-1502-017


DESCRIPTION Emergency Engine Effective Perceived Noise Level Estimated Position Uncertainty Essential Estimated Time of Arrival Elevator Thrust Compensation Estimated Time Enroute Equal Time Point Federal Aviation Authority Full-Authority Digital Electronic-Control Final Approach Fix Flight Attendant Panel Federal Aviation Regulations Final Approach Waypoint Fly-by-wire Flight Control Module Fuel Cooled Oil Cooler Flight Control Panel Fuel Conditioning Unit Flow Control Valve Flight Director Flight Data Recorder Flight Guidance Control System Fault Isolation Manual Fire Extinguisher Flight Level Change Flexible Flight Mode Annunciator Flight Management System Fuel Metering Unit Figure of Merit Flight Path Angle Flight Plan


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ABBREVIATION FPR FSTN ft ft/min ft3 FWD g G/A GA GB GCU GD GEN GMAP GMT GND GNSS GP GPS GPU GPWS GS h HDG HDOP HDPH HF HGS HI HP hPa HPC HPT HPU

DESCRIPTION Flight Path Reference Fasten Foot Foot per Minute Cubic Foot Forward Gravity Acceleration Go-Around Go Around Gigabyte Generator Control Unit Ground Distance Generator Ground Map Greenwich Mean Time Ground Global Navigation Satellite System Guidance Panel Global Positioning System Ground Power Unit Ground-Proximity Warning System Glide Slope Hour Heading Horizontal Dilution of Precision Headphone High Frequency Head-up Guidance System High High Pressure Hectopascal High Pressure Compressor High Pressure Turbine High Pressure Unit


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AOM-1502-017

AIRPLANE OPERATIONS MANUAL ABBREVIATION HS-ACE HSA HSI HYD Hz I/O IAS IATA IBIT ICAO ICC ID IDG IESS IFE IFR IGN ILS in in3 INBD inHg INHIB INOP INPH INT IRS IRU ISA ITT IU IU/kg KCASAOM-1502-017


DESCRIPTION Horizontal-Stabilizer Actuator-Control Electronics Horizontal Stabilizer Actuator Horizontal Situation Indicator Hydraulic Hertz Input/Output Indicated Air Speed International Air Transport Association Inflight Built In Test International Civil Aviation Organization Integrated Control-Center Identification Integrated Drive Generator Integrated Electronic Standby System In Flight Entertainment Instrument Flight Reference Ignition Instrument Landing System Inch Cubic Inch Inboard Inch of Mercury Inhibition Inoperative Interphone Initialization Inertial Reference System Inertial Reference Unit International Standard Atmosphere Interstage Turbine Temperature Index Unit Index Unit per Kilogram Calibrated Airspeed in Knots


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ABBREVIATION kg kg/ kg/m2 kg.m KIAS km km/h kPa KPH kt kVA LAT LAV lb lb/ft2 lbf LCD LDA LDG LED LEMAC LFE LG LH LICC LIM LNAV LO LOC LOC-BC LON LP LRC LRM

DESCRIPTION Kilogram Kilogram per Liter Kilogram per Square Meter Kilogram Meter Indicated Airspeed in Knots Kilometer Kilometer per Hour Kilopascal Kilograms per Hour Knot Kilovolt-Ampere Latitude Lavatory Pound Pound per Square Foot Pound Force Liquid-Crystal Display Localizer Directional Aid Landing Gear Light-Emitting Diode Leading Hedge Aerodynamic Chord Landing Field Elevation Landing Gear Left-Hand Left Integrated Control-Center Limited Thrust Lateral Navigation Low Localizer Localizer-Back Course Longitude Low Pressure Long Range Cruise Line Replaceable Module


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AOM-1502-017

AIRPLANE OPERATIONS MANUAL ABBREVIATION LRU LSK LSS LT LX m m3 MAC MAP MAU MAX MaxAT mbar MCDU MDA MEA MEL MEW MFD MHz MIC MID min MLG MLS MLW mm MMEL MMO MOW MPEG mph MRC MRWAOM-1502-017


DESCRIPTION Line Replaceable Unit Line Select Key Lightning Sensor System Light Lightning Detection Meter Cubic Meter Mean Aerodynamic Chord Multiple Alarm Panel Modular Avionics Unit Maximum Maximum Assumed Temperature Milibar Multifunction Control Display Unit Minimum Descent Altitude Minimum Enroute Altitude Minimum Equipment List Manufacture Empty Weight Multi-Function Display Megahertz Microphone Middle Minute Main Landing Gear Microwave Landing System Maximum Landing Weight Millimeter Master Minimum Equipment List Maximum Mach Operation Maximum Design Operating Weight Moving Picture Experts Group Mile per Hour Modular Radio Cabinet Maximum Ramp Weight


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ABBREVIATION MSA MSL MTOW MTP MZFW N1 N2 NAD-83 NAS NAV NAVCOM NBPT NDB NIC NLG NM NOTAM NPRV OAT OBV ODS OEI OEW OFV OUTBD OVHT OVRD OVSP OWE OXY P-ACE P-RNAV PA PAX

DESCRIPTION Minimum Safety Altitude Mean Sea Level Maximum Takeoff Weight Maintenance Test Panel Maximum Zero Fuel Weight Fan Rotor Speed Core Rotor Speed North American Datum 1983 National Airspace System Navigation Navigation & Communication No-Break Power Transfer Non-Directional Beacon Network Interface Controller Nose Landing Gear Nautical Miles Notice to Airmen Negative Pressure Relief Valve Outside Air Temperature Operability Bleed Valve Overheat Detection System One Engine Inoperative Operational Empty Weight Outflow Valve Outboard Overheat Override Overspeed Overwing Emergency Exit Oxygen Primary Actuator Control Electronics Precision Required Navigation Passenger Address Passenger


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AOM-1502-017

AIRPLANE OPERATIONS MANUAL ABBREVIATION PBE PBIT PC PCN PCU PDU PED Perf PF PFD PIT PMA PPH PPOS PRA PREV PRN PSEM psi psid psig PSU PTT PTU PWR QFE QNH QRH RA RAD RAIM RALT RAMP RATAOM-1502-017


DESCRIPTION Protective Breathing Equipment Power Up Built in Test Personal Computer Pavement Classification Number Power Control Unit Power Drive Unit Portable Electronic Device Performance Pilot Flying Primary Flight Display Pitch Permanent Magnet Alternator Pounds per Hour Present Position Prerecorded Announcement Previous Pseudo-Random Noise Proximity Sensor Electronic Module Pounds per Square Inch Pound per Square Inch Differential Pound per Square Inch Gauge Passenger Service Unit Press To Transmit Power Transfer Unit Power Question Field Elevation Local Altimeter Setting Quick Reference Handbook Resolution Advisory Radio Receiver Autonomous Integrity Monitor Radio Altitude Reliability Analysis and Motoring Program Ram Air Turbine


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ABBREVIATION RCT REACT RECIRC REF. RETD REV RH RICC RNAV RNP rpm RSV RTA RTO RVSM RWY s S-ACE SAD SAI SAT SCV SDF SECT SEL SELCAL SF-ACE SID SL SMKG SOV SPD SPDA

DESCRIPTION Rain Echo Attenuation Rain Echo Attenuation Compensation Technique Recirculation Reference Retard Reverse Right-Hand Right Integrated Control-Center Area Navigation System Required Navigation Performance Revolutions per Minute Reserve Receiver/Transmitter Antenna Rejected Takeoff Reduced Vertical Separation Minimum Runway Second Spoiler Actuator-Control Electronics Still Air Distance Slat Anti-Ice Static Air Temperature Starter Control Valve Simplified Directional Facility Sector Selector Selective Call Slat/Flap Actuator Control Electronics Standard Instrument Departures Sea Level Smoking Shutoff Valve Speed Secondary Power Distribution AssemblyAOM-1502-017


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REVISION 4

AIRPLANE OPERATIONS MANUAL ABBREVIATION SPKR SPS SSPC SSR STAB STAR STBY STD SVC SW SYS T/O T2 TA TA/RA TAS TAT TCAS TCS TDS TEMP TERM TGL TGT TLA TMS TO TOC TOD TOGA TOW TRS TRU TWIPAOM-1502-017


DESCRIPTION Speaker Stall Protection System Solid State Power Controller Secondary Surveillance Radar Stabilizer Standard Instrument Arrivals Standby Standard Service Switch System Takeoff Fan Inlet Temperature Traffic Advisory Traffic Advisory/ Resolution Advisory True Airspeed Total Air Temperature Traffic Alert and Collision Avoidance System Touch Control Steering Takeoff Data Set Temperature Terminal Temporary Guidance Leaflet Target Thrust Lever Angle Thrust Management System Takeoff Top of Climb Top of Descent Takeoff/Go Around Takeoff Weight Thrust Rating Selector Transformer Rectifier Unit Terminal Weather Information for Pilots


REVISION 4


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ABBREVIATION US gal USB UTC V V1 V2 VA VAC VALT VAPP VAR VARM VASEL VDC VDOP VDR VEF VFE VFLCH VFR VFS VGP VHF VLE VLO VMCA VMCG VMCL VMO VNAV VOR VOR/LOC VPATH VR

DESCRIPTION Gallon Universal Serial Bus Universal Time Coordinated Volt Takeoff Decision Speed Takeoff Safety Speed Design Maneuvering Speed Approach Climb Speed Vertical Altitude Approach Speed Variable Vertical ARM Vertical Altitude Select Volt Direct Current Vertical Dilution of Precision VHF Data Radio Critical Engine Failure Speed Maximum Flaps Extended Speed Vertical Flight Level Change Visual Flight Reference Final Segment Speed VNAV Glide Path Very High Frequency Maximum Landing Gear Extended Speed Maximum Landing Gear Operating Speed Air Minimum Control Speed Ground Minimum Control Speed Minimum Control Speed During Landing Maximum Operating Speed Vertical Navigation VHF Omnidirectional Range VOR Localizer Vertical Path Rotation Speed


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AOM-1502-017

AIRPLANE OPERATIONS MANUAL ABBREVIATION Vref VREFXX VS VSI VTA WGS-84 WML WOW WRN WSHR WX XBLEED XCHECK XFEED XPDR YD


DESCRIPTION Reference Speed Landing Reference Speed associated to the flap setting XX Vertical Speed Vertical Speed Indicator Vertical Track Alert World Geodetic System 1984 Windmilling Weight-on-Wheels Warning Windshear Weather Radar Cross Bleed Cross Check Cross Feed Transponder Yaw Damper

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AOM-1502-017



UNITS CONVERSIONTO CONVERT Degree Celsius (C) Degree Fahrenheit (F) Feet (ft) Inches (in) Inches of Mercury (inHg) Kilogram (kg) Kilogram force per Square meter (kg/m2) Kilometer (km) Kilometer per hour (km/h) Knot (kt) Pounds (lb) Meter (m) Millibar (mbar) Millimeter (mm) Nautical Mile (NM) INTO Degree Fahrenheit (F) Degree Celsius (C) Meter (m) Millimeter (mm) Millibar (mbar) Pounds (lb) Pound per Square Inch (psi) Nautical Mile (NM) Knot (kt) Kilometer per hour (km/h) Kilogram (kg) Feet (ft) Inches of Mercury (inHg) Inches (in) Kilometer (km) MULTIPLY BY 1.8000 0.5556 0.3048 25.4000 33.8636 2.2046 0.0014 0.5399 0.5399 1.852 0.4536 3.2808 0.0295 0.0394 1.852 703.0740 AND ADD +32 -17.7778

Kilogram force per Pound per Square Square meter Inch (psi) (kg/m2)

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Units Conversion

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Units Conversion

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SERVICE BULLETIN TABLEEMBRAER 190/195 models SB SB 190-00-0002 SUBJECT Installation of placard indicating the Maximum Takeoff Weight (MTOW) of 50000 kg. Installation of placard indicating the Maximum Takeoff Weight (MTOW) of 46000 kg. Installation of placard indicating the Maximum Takeoff Weight (MTOW) of 51800 kg. Installation of placard indicating the Maximum Takeoff Weight (MTOW) of 47790 kg. Installation of placard indicating the Maximum Takeoff Weight (MTOW) of 50300 kg. Installation of Dual active HF (High Frequency). Update of Load 4.3 to Load 4.5 version of the PRIMUS EPIC field-loadable software system into the Primus Epic Integrated Avionics System. Update of Load 4.5 to Load 19.3 version of the PRIMUS EPIC field-loadable software system into the Primus Epic Integrated Avionics System. Update of current Load to Load 21.2 version of the PRIMUS EPIC field-loadable software system into the Primus Epic Integrated Avionics System.

SB 190-00-0008

SB 190-00-0009

SB 190-00-0012

SB 190-00-0013 SB 190-23-0009

SB 190-31-0007

SB 190-31-0009

SB 190-31-0015

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Service Bulletins

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SB SB 190-32-0022 SB 190-34-0010 SB 190-34-0015 SB 190-49-0001 SB 190-52-0013 SB 190-73-0004 SB 190-73-0010

SUBJECT Installation of Nose Wheel Steering Control Module new version. Upgrade of HGS software version to 811. Installation of HGS software 811 version with CAT IIIa functionalities. Upgrade of APU FADEC software version to FADEC 02.00. Slide Mechanism Modification. Installation of placard in the cockpit with new time limit for maximum TO thrust. Upgrade of engine FADEC software version to 5.32.


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Service Bulletins

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AOM-1502-017



EMBRAER 170/175 X 190/195EMBRAER 170/175 and EMBRAER 190/195 models are classified as common type rating, thus have a high level commonality and may use almost the same AOM. The differences are customized in the manual according to each airplane model and configuration. The following table is presented to help identifying and finding the relevant differences between models EMBRAER 170/175 and EMBRAER 190/195.Difference Section/ Subsection Reference Block 2-05 LIMITATIONS Weight and CG 2-05 LIMITATIONS Weight and CG 2-36 Fuel 2-40 Powerplant 2-40 Powerplant 3-11 Engine Start 3-16 Takeoff Maximum Usable Fuel per Tank/Unusable Fuel per Tank Engine Parameter limits ENGINE Center of Gravity envelopes Embraer 170/175 Embraer 190/195 Topic SubTopic

MRW, MTOW, MLW and MZFW

LIMITATIONS

LIMITATIONS

LIMITATIONS NORMAL PROCEDURES NORMAL PROCEDURES EMERGENCY AND ABNORMAL PROCEDURES/ SMOKE

Noise Levels

NOISE LEVELS

Ground Start ITT limitation Pitch Trim table for FD inoperative Abnormal landing factors for

4-01-01 Smoke

ELECTRICAL SYSTEM FIRE OR SMOKE procedure

ELECTRICAL SYSTEM FIRE OR SMOKE

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Airplane Models Differences

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Difference Section/ Subsection EMERGENCY AND ABNORMAL PROCEDURES/ NON ANNUNCIATED EMERGENCY AND ABNORMAL PROCEDURES/ NON ANNUNCIATED EMERGENCY AND ABNORMAL PROCEDURES/ NON ANNUNCIATED EMERGENCY AND ABNORMAL PROCEDURES/ NON ANNUNCIATED EMERGENCY AND ABNORMAL PROCEDURES/ NON ANNUNCIATED EMERGENCY AND ABNORMAL PROCEDURES/ NON ANNUNCIATEDAOM-1502-017

Reference Block Embraer 170/175 Embraer 190/195

Topic

SubTopic

4-02-01 Non Annunciated

Abnormal Landing factors for DUAL ENGINE FAILURE procedure

DUAL ENGINE FAILURE


Abnormal Landing factors for JAMMED CONTROL COLUMN - PITCH procedure

JAMMED CONTROL COLUMN PITCH


Abnormal Landing factors for JAMMED CONTROL WHEEL - ROLL procedure

JAMMED CONTROL WHEEL - ROLL

4-02-01 Non Annunciated Engine Airstart envelope

ENGINE AIRSTART ENVELOPE


Abnormal Landing factors for LOSS OF HYDRAULIC SYSTEM 1 procedure

LOSS OF HYDRAULIC SYSTEM 1


Abnormal Landing factors for LOSS OF HYDRAULIC SYSTEM 2 procedure

LOSS OF HYDRAULIC SYSTEM 2


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Topic

SubTopic


Abnormal Landing factors for LOSS OF HYDRAULIC SYSTEM 1 AND 3 procedure

LOSS OF HYDRAULIC SYSTEM 1 AND 3


Abnormal Landing factors for LOSS OF HYDRAULIC SYSTEM 2 AND 3 procedure

LOSS OF HYDRAULIC SYSTEM 2 AND 3

4-03-03 Autoflight

Abnormal Landing factors for STALL PROT FAIL procedure

STALL PROT FAIL

Abnormal Landing factors 4-03-05 Electrical and Relevant Inoperative Items list for ELEC EMERGENCY procedure ELEC EMERGENCY

4-03-05 Electrical

Relevant Inoperative Items list for AC BUS 1 OFF procedure AC BUS 1 OFF

4-03-05 Electrical

Relevant Inoperative Items list for AC ESS BUS OFF procedure

AC ESS BUS OFF


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Topic

SubTopic

4-03-05 Electrical

Abnormal Landing factors for DC BUS 1 OFF procedure DC BUS 1 OFF

4-03-05 Electrical

Abnormal Landing factors for DC BUS 2 OFF procedure DC BUS 2 OFF

4-03-05 Electrical

Abnormal Landing factors for DC ESS BUS 1 OFF procedure

DC ESS BUS 1 OFF

Abnormal Landing factors 4-03-05 Electrical and Relevant Inoperative Items list for DC ESS BUS 2 OFF procedure DC ESS BUS 2 OFF

4-03-05 Electrical

Relevant Inoperative Items list for DC ESS BUS 3 OFF procedure

DC ESS BUS 3 OFF

4-03-08 Flight Controls

Abnormal Landing factors for GROUND SPOILERS FAIL procedure

GROUND SPOILERS FAIL


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Topic

SubTopic


Abnormal Landing factors for SPOILERS NML MODE FAIL procedure

SPOILERS NML MODE FAIL


Abnormal Landing factors for ELEVATOR RH (LH) FAIL procedure

ELEVATOR RH (LH) FAIL


FLAP (SLAT) FAIL performance table

FLAP (SLAT) FAIL


Abnormal Landing factors for PITCH TRIM FAIL procedure

PITCH TRIM FAIL


Abnormal Landing factors for SPOILER FAULT procedure

SPOILER FAULT

4-03-09 FMS/Nav/ Com & Flight Instruments

Abnormal Landing factors for AVNX MAU 1A FAIL procedure

AVNX MAU 1A FAIL


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Difference Section/ Subsection EMERGENCY AND ABNORMAL PROCEDURES/ NON ANNUNCIATED EMERGENCY AND ABNORMAL PROCEDURES/ NON ANNUNCIATED EMERGENCY AND ABNORMAL PROCEDURES/ ANNUNCIATED EMERGENCY AND ABNORMAL PROCEDURES/ ANNUNCIATED EMERGENCY AND ABNORMAL PROCEDURES/ ANNUNCIATED EMERGENCY AND ABNORMAL PROCEDURES/ ANNUNCIATED 4-03-13 Landing Gear and Brakes Abnormal Landing factors for BRAKE LH (RH) FAIL procedure BRAKE LH (RH) FAIL 4-03-12 Ice and Rain Protection Abnormal Landing factors for A-I WING FAIL procedure A-I WING FAIL 4-03-09 FMS/Nav/ Com & Flight Instruments 4-03-09 FMS/Nav/ Com & Flight Instruments Abnormal Landing factors and Relevant Inoperative Items list for AVNX MAU 2B FAIL procedure AVNX MAU 2B FAIL 4-03-09 FMS/Nav/ Com & Flight Instruments Abnormal Landing factors for AVNX MAU 1B FAIL procedure Reference Block Embraer 170/175 Embraer 190/195 Topic SubTopic

AVNX MAU 1B FAIL

Abnormal Landing factors for AVNX MAU 3A FAIL procedure

AVNX MAU 3A FAIL

4-03-09 FMS/Nav/ Com & Flight Instruments

Abnormal Landing factors for AVNX MAU 3B FAIL procedure

AVNX MAU 3B FAIL


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Difference Section/ Subsection EMERGENCY AND ABNORMAL PROCEDURES/ ANNUNCIATED EMERGENCY AND ABNORMAL PROCEDURES/ ANNUNCIATED PERFORMANCE FLIGHT PLANNING WEIGHT AND BALANCE 5 6 Performance data Flight Planning data 4-03-13 Landing Gear and Brakes Abnormal Landing factors for BRAKE LH (RH) FAULT procedure BRAKE LH (RH) FAULT 4-03-13 Landing Gear and Brakes Abnormal Landing factors for LG WOW SYS FAIL procedure LG WOW SYS FAIL Reference Block Embraer 170/175 Embraer 190/195 Topic SubTopic

7 8-10

Weight and Balance data

LOADING

External Dimensions 8-10

External dimensions of the airplane

GROUND Ground clearances CLEARANCES GRAPHIC VERTICAL Ground clearances GROUND CLEARANCES TABLE Passenger, service and cargo compartment door clearances Interior arrangement of flight deck and passenger cabin Passenger balance arm and furnishings and equipment balance arms DOOR CLEARANCES

LOADING


LOADING


LOADING


LOADING

Interior Arrangement 8-30

LOADING

Interior Arrangement

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Difference Section/ Subsection Reference Block 8-50 LOADING Cargo Compartment Door 8-60 LOADING Cargo Compartment 8-60 LOADING Cargo Compartment 8-60 LOADING Cargo Compartment LOADING 8-70 Cargo Nets 11-05 Emergency Equipment 12-40 Doors and Exits 13-25 Fuel Cargo compartments dimensions DIMENSIONS AND LIMITS Cargo doors dimensions Embraer 170/175 Embraer 190/195 Topic SubTopic

Cargo compartments balance arms and volumes

DIMENSIONS AND LIMITS

Package size dimensions table Cargo nets limitation and positions Emergency equipment location

PACKAGE SIZE TABLES

EMERGENCY INFORMATION

EMERGENCY EVACUATION

Emergency evacuation exits for EMBRAER 190/195

GROUND SERVICING

Fuel quantity according to magnetic level indication

FUEL MAGNETIC LEVER ENGINE OIL

GROUND SERVICING

13-30 Engine Oil

Engine Oil Level Check

ENGINE OIL SERVICING

LEVEL CHECK ENGINE

SYSTEMS DESCRIPTION/ AIRPLANE GENERAL

14-01-05 Airplane Basic Data

Maximum seat capacity for EMBRAER 190/195 airplane models


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AOM-1502-017



Difference Section/ Subsection SYSTEMS DESCRIPTION/ AIRPLANE GENERAL SYSTEMS DESCRIPTION/ AIRPLANE GENERAL SYSTEMS DESCRIPTION/ AIRPLANE GENERAL SYSTEMS DESCRIPTION/ AIRPLANE GENERAL SYSTEMS DESCRIPTION/ AIRPLANE GENERAL Reference Block Embraer 170/175 14-01-05 Airplane Basic Data Embraer 190/195 Topic SubTopic

External dimensions of the airplane

EXTERNAL DIMENSIONS

14-01-05 Airplane Basic Data

Antennas positioning along the airplane

AIRPLANE ANTENNAS

14-01-05 Airplane Basic Data 14-01-25 Electronic Display System (EDS) 14-01-30 Controls and Indications Main service points location

MAIN SERVICE POINTS

OWE door pictorial status page on MFD, for EMBRAER 190/195

MULTI FUNCTION DISPLAY (MFD) STATUS PAGE

OWE door pictorial status page on MFD, for EMBRAER 190/195

SYNOPTIC PAGE ON MFD

WING SYSTEMS DESCRIPTION/ AIRPLANE GENERAL 14-01-40 Lighting Overwing emergency lights EXTERNAL LIGHTING INSPECTION, LOGOTYPE AND OVERWING EMERGENCY LIGHTS SYSTEMS DESCRIPTION/ AIRPLANE GENERAL SYSTEMS DESCRIPTION/ AIRPLANE GENERALAOM-1502-017

14-01-40 Lighting

Photoluminescent strips for EMBRAER 190/195

EMERGENCY LIGHTING

PHOTOLUMINESCENT STRIPS

14-01-40 Lighting

Cargo compartment lights quantity and location

CARGO COMPARTMENT LIGHTS


REVISION 4


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Difference Section/ Subsection SYSTEMS DESCRIPTION/ AIRPLANE GENERAL SYSTEMS DESCRIPTION/ AIRPLANE GENERAL SYSTEMS DESCRIPTION/ AIR MANAGEMENT SYSTEM SYSTEMS DESCRIPTION/ AUTOMATIC FLIGHT SYSTEMS DESCRIPTION/ AUTOMATIC FLIGHT SYSTEMS DESCRIPTION/ ELECTRICAL 14-05-35 Electrical Loads Distribution 14-05-35 Electrical Loads Distribution 14-05-35 Electrical Loads Distribution Right Smoke Detector A3/F4 Cargo Bay Pitch Trim 1 Control Reading lights MID Right/Left AC/DC BUSSES LOAD DISTRIBUTION DC BUS 2 14-03-10 Mach Trim Description of mach trim function 14-03-10 Flight Guidance Control System Airplane pitch angle guidance for flaps 2 TAKEOFF (TO) 14-02-10 Bleed Air System Engine bleed stage supply and precooler ENGINE BLEED SYSTEM 14-01-80 EICAS Messages EICAS messages applicable only for EMBRAER 190/195 14-01-45 Doors Overwing emergency exits for EMBRAER 190/195 EMERGENCY EXITS Reference Block Embraer 170/175 Embraer 190/195 Topic SubTopic

FGCS

SYSTEMS DESCRIPTION/ ELECTRICAL

AC/DC BUSSES LOAD DISTRIBUTION

DC ESS BUS 1


AC/DC BUSSES LOAD DISTRIBUTION

DC ESS BUS 1


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REVISION 4

AOM-1502-017



Difference Section/ Subsection Reference Block 14-05-35 Electrical Loads Distribution 14-05-35 Electrical Loads Distribution 14-05-35 Electrical Loads Distribution 14-05-35 Electrical Loads Distribution 14-05-35 Electrical Loads Distribution 14-06-01 General Description 14-06-10 Engine Fuel System 14-06-10 Engine Fuel System 14-06-10 Engine Fuel System 14-06-10 Engine Fuel System Fuel schematic Description of fuel flow into the fuel pump Variable Geometric Actuator Fuel system characteristics Engine model, graphic and schematic for EMBRAER 190/195 ENGINE FUEL SYSTEM Pitch Trim 2 AC power FAN AFT Avionics bay Pitch Trim 1 AC power AFT Lavatory Lights Pitch Trim 2 Control Embraer 170/175 SYSTEMS DESCRIPTION/ ELECTRICAL Embraer 190/195 AC/DC BUSSES LOAD DISTRIBUTION Topic SubTopic

DC ESS BUS 3


AC/DC BUSSES LOAD DISTRIBUTION DC GND SVC


AC/DC BUSSES LOAD DISTRIBUTION AC BUS 1


AC/DC BUSSES LOAD DISTRIBUTION AC BUS 2

aom-1502-017-rev.04_apr-30-10

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