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AIRPLANE FLIGHT MANUAL
THIS MANUAL IS APPROVED IN ACCORDANCE WITH FAR 21.29 FOR
U.S. REGISTERED AIRCRAFT, AND IS APPROVED BY THE CTA ON
BEHALF OF THE FEDERAL AVIATION ADMINISTRATION.
THIS DOCUMENT IS APPLICABLE TO THE FOLLOWING AIRPLANE
MODELS: ERJ 170-100 STD, ERJ 170-100 LR, ERJ 170-100 SE, ERJ 170-
100 SU, ERJ 170-200 STD, ERJ 170-200 LR AND ERJ 170-200 SU.
NOTE: - EMBRAER 170
DESIGNATIONS USED IN THIS MANUAL TO REFER TO THE
ERJ 170-100 AND ERJ 170-200 MODELS, RESPECTIVELY.
- SOME MANUAL VERSIONS MAY NOT PRESENT ALL LISTED
MODELS. FOR SPECIFIC CONFIGURATION, REFER TO LEP
APPLICABILITY.
CTA APPROVAL: _______________________
DATE:________________________________
REGISTRATION NUMBER:_______________
SERIAL NUMBER:______________________
In connection with the use of this document, Embraer does not provide any express or implied warranties
and expressly disclaims any warranty of merchantability or fitness for a particular purpose.
This document contains trade secrets, confidential, proprietary information of Embraer and technical data subject to
U.S. Export Administration Regulation ("EAR") and other countries export control laws and regulations. Diversion
contrary to the EAR and other laws and regulations is strictly forbidden. The above restrictions may apply to data on
EMBRAER 170/175
FAA
Embraer S.A.
AND
EMBRAER 175
CLAUDIO PASSOS SIMÃO – TEN.-CEL.-ENG.
CHEFE DA DIVISÃO DE HOMOLOGAÇÃO
REVISION 15 – OCTOBER 03, 2016
all pages of this document.
Copyright © 2016 by Embraer S.A. All rights reserved.
ARE
COMMERCIAL
AERONÁUTICA
FEBRUARY 20, 2004
AFM–1385
CODE 003

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Summary of Contents for Embraer 170

  • Page 1 FEBRUARY 20, 2004 REVISION 15 – OCTOBER 03, 2016 In connection with the use of this document, Embraer does not provide any express or implied warranties and expressly disclaims any warranty of merchantability or fitness for a particular purpose. This document contains trade secrets, confidential, proprietary information of Embraer and technical data subject to U.S.
  • Page 3 AIRPLANE REVISION APPROVAL FLIGHT MANUAL code 01 Page 1 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 4 REVISION APPROVAL AIRPLANE FLIGHT MANUAL Page 2 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 5 AIRPLANE REVISION APPROVAL FLIGHT MANUAL code 01 Page 3 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 6 REVISION APPROVAL AIRPLANE FLIGHT MANUAL Page 4 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 7 AIRPLANE REVISION APPROVAL FLIGHT MANUAL code 01 Page 5 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 8 REVISION APPROVAL AIRPLANE FLIGHT MANUAL Page 6 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 9 AIRPLANE REVISION APPROVAL FLIGHT MANUAL code 01 Page 7 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 10 REVISION APPROVAL AIRPLANE FLIGHT MANUAL Page 8 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 11 AIRPLANE REVISION APPROVAL FLIGHT MANUAL code 01 Page 9 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 12 REVISION APPROVAL AIRPLANE FLIGHT MANUAL Page 10 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 13 AIRPLANE REVISION APPROVAL FLIGHT MANUAL code 01 Page 11 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 14 REVISION APPROVAL AIRPLANE FLIGHT MANUAL INTENTIONALLY BLANK Page 12 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 15 Revision 4 Section 2 Dec 23/05 May 02/07 Revision 4 Sections 1, 2, 4, 5 and Oct 03/06 May 02/07 Revision 4 Supplement 1 code 01 Page 1 REVISION 14 Copyright © by Embraer. Refer to cover page for details.
  • Page 16 Nov 10/08 Revision 7 Supplements 4 Section 4 Apr 02/09 Jul 02/09 Revision 8 Section 1, Sep 28/09 Apr 08/10 Revision 9 Supplement 4 Page 2 code 01 REVISION 14 Copyright © by Embraer. Refer to cover page for details.
  • Page 17 Supplement 1 Feb 19/16 Oct 03/16 Revision 15 Sections 1, 3, 14.5 Supplements 4, Jul 04/16 Oct 03/16 Revision 15 10, 12, and 13 code 01 Page 3 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 18 RECORD OF AIRPLANE TEMPORARY FLIGHT REVISIONS MANUAL INTENTIONALLY BLANK Page 4 code 01 REVISION 14 Copyright © by Embraer. Refer to cover page for details.
  • Page 19 REVISION....12 ....JUN 03, 2013 REVISION....13 ....MAR 14, 2014 REVISION....14 ....APR 29, 2015 REVISION....15 ....OCT 03, 2016 0-LEP code 003 Page 1 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 20 LIST OF AIRPLANE EFFECTIVE PAGES FLIGHT MANUAL INTENTIONALLY BLANK 0-LEP Page 2 code 003 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 21 REVISION 15 0-LOR REVISION 15 0-LOR REVISION 15 0-LOR REVISION 15 * Asterisk indicates pages revised, added or deleted by the current revision. 0-LEP code 003 Page 3 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 22 REVISION 15 1-10 REVISION 15 1-10 REVISION 15 1-20 REVISION 15 * Asterisk indicates pages revised, added or deleted by the current revision. 0-LEP Page 4 code 003 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 23 REVISION 15 170 + 8000 ft 2-10 REVISION 15 2-10 REVISION 15 * Asterisk indicates pages revised, added or deleted by the current revision. 0-LEP code 003 Page 5 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 24 2-58 ORIGINAL 3-00 REVISION 14 3-00 REVISION 14 3-00 REVISION 14 * Asterisk indicates pages revised, added or deleted by the current revision. 0-LEP Page 6 code 003 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 25 3-25 ORIGINAL 3-27 ORIGINAL 3-27 ORIGINAL 3-29 REVISION 4 3-29 ORIGINAL * Asterisk indicates pages revised, added or deleted by the current revision. 0-LEP code 003 Page 7 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 26 REVISION 15 4-01 REVISION 15 4-01 REVISION 15 4-01 REVISION 15 * Asterisk indicates pages revised, added or deleted by the current revision. 0-LEP Page 8 code 003 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 27 REVISION 15 4-08 REVISION 6 4-08 ORIGINAL 4-08 REVISION 6 4-08 ORIGINAL * Asterisk indicates pages revised, added or deleted by the current revision. 0-LEP code 003 Page 9 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 28 REVISION 15 4-16 REVISION 15 4-16 REVISION 15 4-16 REVISION 15 * Asterisk indicates pages revised, added or deleted by the current revision. 0-LEP Page 10 code 003 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 29 REVISION 15 4-24 REVISION 15 4-24 REVISION 15 4-24 REVISION 15 * Asterisk indicates pages revised, added or deleted by the current revision. 0-LEP code 003 Page 11 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 30 REVISION 6 5-01 REVISION 6 5-01 REVISION 6 5-01 REVISION 6 * Asterisk indicates pages revised, added or deleted by the current revision. 0-LEP Page 12 code 003 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 31 175 EWT – CF34-8E5 CAFM-175-FAA-006 VERSION S1-05 REVISION 15 S1-10 ORIGINAL * Asterisk indicates pages revised, added or deleted by the current revision. 0-LEP code 003 Page 13 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 32 REVISION 15 S4-10 REVISION 15 S5-00 REVISION 6 CAT II Operation * Asterisk indicates pages revised, added or deleted by the current revision. 0-LEP Page 14 code 003 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 33 REVISION 3 AP1-28 REVISION 4 AP1-28 REVISION 4 AP1-32 REVISION 14 * Asterisk indicates pages revised, added or deleted by the current revision. 0-LEP code 003 Page 15 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 34 REVISION 2 AP2-10 REVISION 4 170 Supplemental Noise AP2-10 REVISION 2 * Asterisk indicates pages revised, added or deleted by the current revision. 0-LEP Page 16 code 003 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 35 AIRPLANE TABLE OF CONTENTS FLIGHT MANUAL TABLE OF CONTENTS 1 - GENERAL 2 - LIMITATIONS 3 - NORMAL PROCEDURES 4 - EMERGENCY AND ABNORMAL PROCEDURES 5 - PERFORMANCE SUPPLEMENTS APPENDICES 0-TOC CTA APPROVED Page 1 code 01 REVISION 3...
  • Page 36 AIRPLANE TABLE OF CONTENTS FLIGHT MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 0-TOC CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 37 SECTION 1 GENERAL TABLE OF CONTENTS Block Page Introduction ................ 1-00..02 Definition of Terms............. 1-10..01 Abbreviations and Acronyms Used........1-20..01 1-00 code 01 Page 1 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 38 Av. Brigadeiro Faria Lima, 2170 - PC 176 São José dos Campos - São Paulo - BRASIL CEP 12227-901 PHONE: 55 12 3927-1706 E-MAIL: opereng@embraer.com.br 1-00 Page 2 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 39 FLIGHT MANUAL REVISIONS EMBRAER may periodically revise this manual as required to update information or provide information not available at the time of printing. Revised data may result from EMBRAER approved airplane modifications or from improved techniques gained through operational experience.
  • Page 40 Both cover and LEP (of normal and temporary revision) must be replaced with those transmitted by the configuration release, and the content pages inserted or removed accordingly. 1-00 Page 4 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 41 SECTION 4 - EMERGENCY AND ABNORMAL PROCEDURES This Section contains the actions in the event of failures. SECTION 5 - PERFORMANCE This section contains performance general information configurations. 1-00 code 01 Page 5 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 42 AFM for the operator convenience. Such portions are presented in segregated Sections, Supplements or Appendices, and their pages do not bear the notation "ANAC APPROVED". 1-00 Page 6 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 43 OTHER RELATED INFORMATION WHICH MAY RESULT IN DAMAGE OR DESTRUCTION OF EQUIPMENT, IF NOT FOLLOWED. NOTE: Operating procedures, techniques other related information which are considered essential to emphasize. 1-10 code 01 Page 1 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 44 GENERAL AIRPLANE FLIGHT MANUAL INTENTIONALLY BLANK 1-10 Page 2 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 45 Airplane Flight Manual Above Ground Level Anti-Ice Air Management System Angle of Attack AP or A/P Autopilot Auxiliary Power Unit Armed Accelerate Stop Distance 1-20 code 01 Page 1 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 46 Environmental Control System Enhanced Ground Proximity Warning EGPWS System Exhaust Gas Temperature Engine Indication and Crew Alerting EICAS System EMG or EMERG Emergency 1-20 Page 2 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 47 Integrated Driven Generator IESS Integrated Electronic Standby System Instrument Flight Rules Instrument Landing System Inertial Reference System Inertial Reference Unit International Standard Atmosphere 1-20 code 01 Page 3 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 48 Maximum Turbulent Air Penetration Speed (Mach) Maintenance Review Board Maximum Ramp Weight MTOW Maximum Takeoff Weight Maximum Reserve Fan Speed High Pressure Rotor Shaft Speed 1-20 Page 4 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 49 Reduced Vertical Separation Minimum Static Air Temperature Simplified Directional Monitoring Shutoff Valve Standard Traffic Advisory Total Air Temperature TCAS Traffic and Collision Avoidance System 1-20 code 01 Page 5 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 50 Minimum Control Speed on Ground Minimum Control Speed During Landing Maximum Operating Speed Minimum Unstick Speed VNAV Vertical Navigation Mode VHF Omnidirectional Range 1-20 Page 6 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 51 GENERAL AIRPLANE FLIGHT MANUAL ABBREVIATIONS OR MEANING ACRONYMS Rotation Speed Maximum Turbulent Air Penetration Speed Landing Reference Speed 1-20 code 01 Page 7 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 52 GENERAL AIRPLANE FLIGHT MANUAL INTENTIONALLY BLANK 1-20 Page 8 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 53 LIMITATIONS AIRPLANE FLIGHT MANUAL SECTION 2 LIMITATIONS TABLE OF CONTENTS Block Page Introduction ................ 2-00..02 Weight................2-05..01 Loading ................2-05..01 Center of Gravity Envelope..........2-06..01 Operational Limitations ............2-10..01 Systems: Electronic Display System ..........2-20..01 Warning ................
  • Page 54 LIMITATIONS AIRPLANE FLIGHT MANUAL INTRODUCTION This airplane must be operated in accordance with the limitations presented in this Section. These limitations also apply to operations in accordance with an approved Supplement or Appendix to this AFM, except as altered by such Supplement or Appendix. 2-00 CTA APPROVED Page 2...
  • Page 55 82364 82011 72310 65256 (1) NOTE: 1) For airplanes S/N 170-0059, 170-0065 and on, or Post-Mod. SB170-00-0024, the MZFW is 66446 lb. To comply with the performance and operating limitations of the regulations, the maximum allowable takeoff and landing operational weights may be equal to, but not greater than design limits.
  • Page 56 LIMITATIONS AIRPLANE FLIGHT MANUAL DELETED 2-05 ANAC APPROVED Page 2 code 02 REVISION 13...
  • Page 57 82364 82011 72310 65256 (1) NOTE: 1) For airplanes S/N 170-0059, 170-0065 and on, or Post-Mod. SB170-00-0024, the MZFW is 66446 lb. To comply with the performance and operating limitations of the regulations, the maximum allowable takeoff and landing operational weights may be equal to, but not greater than design limits.
  • Page 58 LIMITATIONS AIRPLANE FLIGHT MANUAL DELETED 2-05 ANAC APPROVED Page 2 code 03 REVISION 13...
  • Page 59 82364 82011 72310 65256 (1) NOTE: 1) For airplanes S/N 170-0059, 170-0065 and on, or Post-Mod. SB170-00-0024, the MZFW is 66446 lb. To comply with the performance and operating limitations of the regulations, the maximum allowable takeoff and landing operational weights may be equal to, but not greater than design limits.
  • Page 60 LIMITATIONS AIRPLANE FLIGHT MANUAL DELETED 2-05 ANAC APPROVED Page 2 code 04 REVISION 13...
  • Page 61 (MTOW) (MLW) (MZFW) (lb) (lb) (lb) (lb) EMBRAER 175 LR 85870 85517 74957 69886 To comply with the performance and operating limitations of the regulations, the maximum allowable takeoff and landing operational weights may be equal to, but not greater than design limits.
  • Page 62 LIMITATIONS AIRPLANE FLIGHT MANUAL DELETED 2-05 ANAC APPROVED Page 2 code 11 REVISION 13...
  • Page 63 89000 75177 70547 EMBRAER 175-LR NOTE: (1) For airplanes Post-Mod. SB 170-00-0016 or equipped with an equivalent modification factory incorporated. To comply with the performance and operating limitations of the regulations, the maximum allowable takeoff and landing operational weights may be equal to, but not greater than design limits.
  • Page 64 LIMITATIONS AIRPLANE FLIGHT MANUAL DELETED 2-05 ANAC APPROVED Page 2 code 20 REVISION 13...
  • Page 65 FLIGHT MANUAL CENTER OF GRAVITY ENVELOPE EMBRAER 170 STANDARD, LR, SE AND SU MODELS PRE-MOD SB 170-00-0003 AND PRE-MOD 170-00-0016 NOTE: The data below must be used in conjunction with the maximum weight values (ramp, takeoff, landing and zero fuel) associated to each model and found in the Maximum Weight table.
  • Page 66 LIMITATIONS AIRPLANE FLIGHT MANUAL EMBRAER 170 STANDARD, LR, SE AND SU MODELS POST-MOD 170-00-0003 EQUIPPED WITH EQUIVALENT MODIFICATION FACTORY INCORPORATED AND PRE-MOD SB 170-00-0016 NOTE: The data below must be used in conjunction with the maximum weight values (ramp, takeoff, landing and zero fuel) associated to each model and found in the Maximum Weight table.
  • Page 67 LIMITATIONS AIRPLANE FLIGHT MANUAL EMBRAER 170 STANDARD, LR, SE AND SU MODELS POST-MOD 170-00-0016 EQUIPPED WITH EQUIVALENT MODIFICATION FACTORY INCORPORATED NOTE: The data below must be used in conjunction with the maximum weight values (ramp, takeoff, landing and zero fuel) associated to each model and found in the Maximum Weight table.
  • Page 68 LIMITATIONS AIRPLANE FLIGHT MANUAL INTENTIONALLY BLANK 2-06 ANAC APPROVED Page 4 code 01 REVISION 13...
  • Page 69 FLIGHT MANUAL CENTER OF GRAVITY ENVELOPE EMBRAER 175 STANDARD, LR AND SU MODELS NOTE: The data below must be used in conjunction with the maximum weight values (ramp, takeoff, landing and zero fuel) associated to each model and found in the Maximum Weight table.
  • Page 70 LIMITATIONS AIRPLANE FLIGHT MANUAL INTENTIONALLY BLANK 2-06 ANAC APPROVED Page 2 code 03 REVISION 13...
  • Page 71 MANUAL CENTER OF GRAVITY ENVELOPE (ALTERNATE 1 – CENTER OF GRAVITY – 16%) EMBRAER 170 STANDARD, LR, SE AND SU MODELS PRE-MOD SB 170-00-0003 AND PRE-MOD SB 170-00-0016 NOTE: The data below must be used in conjunction with the maximum weight values (ramp, takeoff, landing and zero fuel) associated to each model and found in the Maximum Weight table.
  • Page 72 LIMITATIONS AIRPLANE FLIGHT MANUAL EMBRAER 170 STANDARD, LR, SE AND SU MODELS POST-MOD 170-00-0003 EQUIPPED WITH EQUIVALENT MODIFICATION FACTORY INCORPORATED AND PRE-MOD SB 170-00-0016 NOTE: The data below must be used in conjunction with the maximum weight values (ramp, takeoff, landing and zero fuel) associated to each model and found in the Maximum Weight table.
  • Page 73 LIMITATIONS AIRPLANE FLIGHT MANUAL EMBRAER 170 STANDARD, LR, SE AND SU MODELS POST-MOD 170-00-0016 EQUIPPED WITH EQUIVALENT MODIFICATION FACTORY INCORPORATED NOTE: The data below must be used in conjunction with the maximum weight values (ramp, takeoff, landing and zero fuel) associated to each model and found in the Maximum Weight table.
  • Page 74 LIMITATIONS AIRPLANE FLIGHT MANUAL INTENTIONALLY BLANK 2-06 ANAC APPROVED Page 4 code 05 REVISION 13...
  • Page 75 EMBRAER 175 STANDARD, MODELS CF34-8E5 ENGINES - POST-MOD SB 170-57-0058 (ENHANCED WING TIP) OR WITH AN EQUIVALENT FACTORY MODIFICATION NOTE: The data below must be used in conjunction with the maximum weight values (ramp, takeoff, landing and zero fuel) associated to each model and found in the Maximum Weight table.
  • Page 76 LIMITATIONS AIRPLANE FLIGHT MANUAL INTENTIONALLY BLANK 2-06 ANAC APPROVED Page 2 code 11 REVISION 13...
  • Page 77 STATIC AIR TEMPERATURE − °C NOTE: In the event of a landing below -40°C, the airplane may not takeoff without further maintenance inspection. 2-10 ANAC APPROVED code 01 Page 1 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 78 - V LE is the maximum speed at which the airplane can be safely flown with the landing gear extended and locked. 2-10 ANAC APPROVED Page 2 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 79 CHANGES IN PITCH, ROLL, OR YAW (E.G. LARGE SIDE SLIP ANGLES) RESULT STRUCTURAL FAILURES AT ANY SPEED, EVEN BELOW V A . 2-10 ANAC APPROVED code 01 Page 3 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 80 200 210 220 230 240 250 260 270 280 290 300 310 320 330 340 350 AIRSPEED − KIAS NOTE: V may not be deliberated exceeded in any regime of flight (climb, cruise, or descent). 2-10 ANAC APPROVED Page 4 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 81 − Visual (VFR). − Instrument (IFR). − Icing conditions. − Category I and II. − RVSM. − Extended Over-Water Operation. 2-10 ANAC APPROVED code 01 Page 5 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 82 Runway Surface Type ........... PAVED TOWING Towbarless towing is prohibited, unless it is conducted in accordance with the procedures presented in the AMM chapter 9. 2-10 ANAC APPROVED Page 6 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 83 STATIC AIR TEMPERATURE − °C NOTE: In the event of a landing below -40°C, the airplane may not takeoff without further maintenance inspection. 2-10 ANAC APPROVED code 03 Page 1 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 84 - V LE is the maximum speed at which the airplane can be safely flown with the landing gear extended and locked. 2-10 ANAC APPROVED Page 2 code 03 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 85 CHANGES IN PITCH, ROLL, OR YAW (E.G. LARGE SIDE SLIP ANGLES) RESULT STRUCTURAL FAILURES AT ANY SPEED, EVEN BELOW V A 2-10 ANAC APPROVED code 03 Page 3 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 86 200 210 220 230 240 250 260 270 280 290 300 310 320 330 340 350 AIRSPEED − KIAS NOTE: V may not be deliberated exceeded in any regime of flight (climb, cruise, or descent). 2-10 ANAC APPROVED Page 4 code 03 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 87 − Visual (VFR). − Instrument (IFR). − Icing conditions. − Category I and II. − RVSM. − Extended Overwater Operation. 2-10 ANAC APPROVED code 03 Page 5 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 88 Runway Surface Type ........... PAVED TOWING Towbarless towing is prohibited, unless it is conducted in accordance with the procedures presented in the AMM chapter 9. 2-10 ANAC APPROVED Page 6 code 03 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 89 ELECTRONIC CHECKLIST Operational approval is required in order to load database into the airplane and use the electronic checklist. For airplanes Pre-Mod. SB 170-31-0019 or with an equivalent modification factory incorporated, the use of the Electronic Checklist is prohibited. 2-20...
  • Page 90 LIMITATIONS AIRPLANE FLIGHT MANUAL INTENTIONALLY BLANK 2-20 ANAC APPROVED Page 2 code 01 REVISION 4...
  • Page 91 AIRPLANE LIMITATIONS FLIGHT MANUAL WARNING ENHANCED GROUND PROXIMITY WARNING The following limitations are applicable to the Enhanced Ground Proximity Warning System (EGPWS): Navigation is not to be predicated on the use of the Terrain Awareness Display. The use of predictive EGPWS functions should be manually inhibited when landing to an airport that is not in the airport database to avoid unwanted alerts.
  • Page 92 AIRPLANE LIMITATIONS FLIGHT MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 2-30 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 93 American Specification ..........MIL-T-83133A- FUEL TANK TEMPERATURE Minimum ............... -37°C CROSSFEED OPERATION Crossfeed Selector Knob must be set OFF during takeoff and landing. 2-36 ANAC APPROVED code 01 Page 1 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 94 LIMITATIONS AIRPLANE FLIGHT MANUAL INTENTIONALLY BLANK 2-36 ANAC APPROVED Page 2 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 95 LIMITATIONS AIRPLANE FLIGHT MANUAL AUXILIARY POWER UNIT SUNDSTRAND APS 2300 OPERATIONAL LIMITS PARAMETER START: TEMPERATURE -54° C ALTITUDE 30000 ft OPERATION: TEMPERATURE ALTITUDE: 33000 ft ELECTRICAL GEN 33000 ft BLEED 15000 ft TO ASSIST ENGINE START 21000 ft ROTOR SPEED 108% EGT (1) (2): START...
  • Page 96 LIMITATIONS AIRPLANE FLIGHT MANUAL INTENTIONALLY BLANK 2-38 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 97 2) Time limited to the remaining 3 minutes of the total 5 minutes limit. 3) Transient operation above 155°C limited to 15 minutes. 2-40 ANAC APPROVED code 02 Page 1 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 98 90 seconds (monitoring plus start time). - For in-flight starts, the maximum cumulative starter run time per start attempt is 120 seconds (monitoring plus start time). 2-40 ANAC APPROVED Page 2 code 02 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 99 After applying thrust reverser, do not move the throttle back to the forward thrust range, unless the REV icon on the EICAS is shown in amber or green. 2-40 ANAC APPROVED code 02 Page 3 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 100 LIMITATIONS AIRPLANE FLIGHT MANUAL INTENTIONALLY BLANK 2-40 ANAC APPROVED Page 4 code 02 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 101 Maximum differential overpressure ......8.8 psi Maximum differential negative pressure....... -0.5 psi Maximum differential pressure for Takeoff and Landing ............. 0.2 psi 2-48 ANAC APPROVED code 01 Page 1 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 102 LIMITATIONS AIRPLANE FLIGHT MANUAL INTENTIONALLY BLANK 2-48 ANAC APPROVED Page 2 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 103 ON when icing conditions exist or are anticipated below 10°C TAT with visible moisture. 2-50 ANAC APPROVED code 01 Page 1 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 104 THE COCKPIT MAY RESULT IN ICE INGESTION AND POSSIBLE ENGINE DAMAGE OR FLAMEOUT. WINDSHIELD WIPER OPERATION Maximum Airspeed for Windshield Wiper Operation..253 KIAS 2-50 ANAC APPROVED Page 2 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 105 - For airplanes Post-Mod. SB 170-34-0035 (ADS-B Out) or equipped with an equivalent modification factory incorporated, the ADS-B Out system complies with AMC 20-24 and was implemented according to DO-260A, change 1 and change 2.
  • Page 106 LIMITATIONS AIRPLANE FLIGHT MANUAL (Continued from the previous page) MAGNETIC CUT-OUT LATITUDE LONGITUDE REGIONS Between 60°S and Between 120°E South 82°S 160°E South of 82°S Between 0° and 180°W/E NOTE: Whenever operating within North or South magnetic polar cut- out regions, current airplane heading must be referenced to true heading, if not already selected.
  • Page 107 AIRPLANE LIMITATIONS FLIGHT MANUAL OZONE CONCENTRATION The tables below show the airplane altitude limitations due to ozone concentration in atmosphere for airplanes not equipped with the Ozone Converters. NOTE: - These tables are based on FAA ADVISORY CIRCULAR 120.38. - The tables show altitude limitations calculated for constant ozone concentration and cabin stabilized at 8000 ft.
  • Page 108 AIRPLANE LIMITATIONS FLIGHT MANUAL NORTH AMERICA - MAXIMUM OZONE CRITERIA FLIGHT LEVEL LATITUDE 80°N 75°N 70°N 65°N 356 346 333 326 328 327 328 321 326 321 338 336 60°N 376 356 347 336 338 334 327 326 327 326 341 336 55°N 394 362 376 346 347 341 327 334 327 327 347 356 50°N...
  • Page 109 AIRPLANE LIMITATIONS FLIGHT MANUAL NORTH AMERICA - TWA OZONE CRITERIA NOTE: Values below are the altitude limitations which the airplane is allowed to fly more than 3 continuous hours. FLIGHT LEVEL LATITUDE 80°N 75°N 70°N 65°N 273 292 60°N 291 274 55°N 291 270 50°N...
  • Page 110 AIRPLANE LIMITATIONS FLIGHT MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 2-58 CTA APPROVED Page 4 code 01 ORIGINAL...
  • Page 111 Traffic and Collision Avoidance ......... 3-39..01 Transponder ..............3-40..01 Operation in Icing Conditions..........3-41..01 Turbulent Air Penetration ........... 3-43..01 3-00 ANAC APPROVED code 01 Page 1 REVISION 14 Copyright © by Embraer. Refer to cover page for details.
  • Page 112 NORMAL AIRPLANE PROCEDURES FLIGHT MANUAL INTENTIONALLY BLANK 3-00 ANAC APPROVED Page 2 code 01 REVISION 14 Copyright © by Embraer. Refer to cover page for details.
  • Page 113 The actions identified with φ are recall items. They must be performed expeditiously and from memory. 3-00 ANAC APPROVED code 01 Page 3 REVISION 14 Copyright © by Embraer. Refer to cover page for details.
  • Page 114 NORMAL AIRPLANE PROCEDURES FLIGHT MANUAL INTENTIONALLY BLANK 3-00 ANAC APPROVED Page 4 code 01 REVISION 14 Copyright © by Embraer. Refer to cover page for details.
  • Page 115 Start/Stop Selectors ..........STOP Slat/Flap Lever............VERIFY POSITION Circuit Breakers ............CHECK Photoluminescent Escape Path Marking System (Passenger Cabin) ....CHARGED 3-03 ANAC APPROVED code 01 Page 1 REVISION 14 Copyright © by Embraer. Refer to cover page for details.
  • Page 116 NORMAL AIRPLANE PROCEDURES FLIGHT MANUAL INTENTIONALLY BLANK 3-03 ANAC APPROVED Page 2 code 01 REVISION 14 Copyright © by Embraer. Refer to cover page for details.
  • Page 117 Emergency Lights Selector Knob......ARMED Fire Extinguisher Panel..........CHECK APU Selector Knob ..........AS REQUIRED MCDU Electronic CBs ..........CHECK DVDR Panel............. CHECK 3-05 ANAC APPROVED code 01 Page 1 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 118 NORMAL AIRPLANE PROCEDURES FLIGHT MANUAL INTENTIONALLY BLANK 3-05 ANAC APPROVED Page 2 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 119 NORMAL AIRPLANE PROCEDURES FLIGHT MANUAL EXTERNAL INSPECTION Prior to start the external inspection, apply the Emergency/Parking Brake. Access Doors and Panels ........SECURED Air Inlets, Outlets and Vents ........NO OBSTRUCTION Antennas..............CONDITION APU................CONDITION Doors (Passenger, Service and Cargo) ....CHECK Drain Masts..............
  • Page 120 NORMAL AIRPLANE PROCEDURES FLIGHT MANUAL Pressurization Static Port......... NO OBSTRUCTION Radome..............CHECK Smart Probes/TAT Sensors/Ice Detectors ....CHECK Static Dischargers............ NUMBER AND CONDITION Thrust Reverser Cowls ..........FLUSHED WITH NACELLE Wing Water Drain Valves......... NO LEAKS Windshield Wipers ........... CHECK 3-07 CTA APPROVED Page 2/(3 to 6 deleted)
  • Page 121 Fire Extinguisher Panel..........CHECK APU Control Panel........... AS REQUIRED External Lights Panel ..........AS REQUIRED Engine 2 Fire Handle ..........STOWED Hydraulic Panel............SET 3-09 ANAC APPROVED code 01 Page 1 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 122 Clock ................ SET ELT................ARMED Gnd Prox G/S Inhib Button........CHECK LG Wrn Inhib Button ..........CHECK Flight Control Panel..........CHECK 3-09 ANAC APPROVED Page 2 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 123 Flight Controls Disconnect Handles......CHECK Alternate Gear Extension Compartment .......... CHECK MCDU ..............SET Insert route in the FMS according to the flight plan. 3-09 ANAC APPROVED code 01 Page 3 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 124 Takeoff Briefing............COMPLETED Red Beacon ............. ON Hydraulic Pump Sys 3A..........ON Ground Equipment ........... AS REQUIRED Steering Disengage Switch ........PRESS 3-09 ANAC APPROVED Page 4 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 125 - For airplanes Post-Mod. SB 170-73-0007 or equipped with Engine FADEC 5.60 or later versions, two additional engine starts are allowed in case of automatic abort due to engine hot start.
  • Page 126 NORMAL AIRPLANE PROCEDURES FLIGHT MANUAL INTENTIONALLY BLANK 3-11 ANAC APPROVED Page 2 code 01 REVISION 14 Copyright © by Embraer. Refer to cover page for details.
  • Page 127 N1 Target..............CHECK Slat/Flap..............SET Flight Controls............CHECK NOTE: The flight controls check must be performed with the flight controls synoptic page displayed. 3-13 ANAC APPROVED code 01 Page 1 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 128 NORMAL AIRPLANE PROCEDURES FLIGHT MANUAL INTENTIONALLY BLANK 3-13 ANAC APPROVED Page 2 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 129 − ATTCS (if selected). − FLEX TEMP (__ºC). --------------------------SHORTLY BEFORE TAKEOFF------------------------- Cabin Crew .............. ADVISE Transponder ............TA/RA Lights ............... ON 3-15 ANAC APPROVED code 01 Page 1 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 130 NORMAL AIRPLANE PROCEDURES FLIGHT MANUAL INTENTIONALLY BLANK 3-15 ANAC APPROVED Page 2 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 131 FLAPS POSITION PITCH ANGLE 11° 10° 12° For airplanes Post-Mod. SB 170-31-0019 or equipped with an − equivalent modification factory incorporated, rotate the airplane according to the takeoff pitch angle displayed on TAKEOFF page 3/3 on the MCDU. With positive rate of climb: Landing Gear ............
  • Page 132 NORMAL AIRPLANE PROCEDURES FLIGHT MANUAL INTENTIONALLY BLANK 3-16 ANAC APPROVED Page 2 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 133 NORMAL AIRPLANE PROCEDURES FLIGHT MANUAL AFTER TAKEOFF Air Conditioning & Press .......... CHECK APU................AS REQUIRED Slat/Flap..............UP Select Slat/Flap to up following the flap retraction speed reference indication. Altimeters ..............SET & XCHECK ------------------------------AFTER 10000 FT AFE-------------------------------- External Lights ............OFF No Smoking .............
  • Page 134 NORMAL AIRPLANE PROCEDURES FLIGHT MANUAL INTENTIONALLY BLANK 3-17 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 135 MANUAL DESCENT Approach Briefing ............ COMPLETE Landing Data............SET Select the LANDING page on the MCDU and set V and V 3-19 ANAC APPROVED code 01 Page 1 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 136 NORMAL AIRPLANE PROCEDURES FLIGHT MANUAL INTENTIONALLY BLANK 3-19 ANAC APPROVED Page 2 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 137 APPROACH Passenger Signs Panel..........SET Altimeters ..............SET & X-CHECK Autobrake (if applicable) .......... AS REQUIRED Approach Aids............SET & X-CHECK 3-21 ANAC APPROVED code 01 Page 1 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 138 NORMAL AIRPLANE PROCEDURES FLIGHT MANUAL INTENTIONALLY BLANK 3-21 ANAC APPROVED Page 2 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 139 NORMAL AIRPLANE PROCEDURES FLIGHT MANUAL BEFORE LANDING Landing Gear ............DOWN Slat/Flap..............SET_ Lights ............... AS REQUIRED 3-23 CTA APPROVED code 01 Page 1 ORIGINAL...
  • Page 140 NORMAL AIRPLANE PROCEDURES FLIGHT MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 3-23 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 141 AIRPLANE NORMAL PROCEDURES FLIGHT MANUAL GO AROUND Go Around button............. PRESS Thrust Levers............TOGA Rotate or verify that autopilot rotates the airplane following the flight director guidance. NOTE: In case of flight director is inoperative, rotate the airplane to 8º nose up.
  • Page 142 AIRPLANE NORMAL PROCEDURES FLIGHT MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 3-25 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 143 AIRPLANE NORMAL PROCEDURES FLIGHT MANUAL AFTER LANDING NOTE: Upon landing, thrust reversers should be set to MIN REV at 60 KIAS and be closed at 30 KIAS. During RTO the thrust reversers can be used until the airplane comes to a complete stop.
  • Page 144 AIRPLANE NORMAL PROCEDURES FLIGHT MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 3-27 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 145 NORMAL AIRPLANE PROCEDURES FLIGHT MANUAL SHUTDOWN Thrust Levers............IDLE Emergency/Parking Brake........SET Electrical ..............ON GPU/APU Start/Stop Selectors..........STOP Electric Hydraulic Pump 3A ........OFF Red Beacon ............. OFF Fasten Belts............. OFF 3-29 ANAC APPROVED code 01 Page 1 REVISION 4...
  • Page 146 NORMAL AIRPLANE PROCEDURES FLIGHT MANUAL INTENTIONALLY BLANK 3-29 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 147 NORMAL AIRPLANE PROCEDURES FLIGHT MANUAL LEAVING THE AIRPLANE Passenger Signs Panel ........... OFF Set the Emergency Lights and all switches to OFF. APU................OFF Turn the APU off selecting the APU selector to OFF and wait until the APU shuts down before turning off both batteries selectors. Batteries 1 &...
  • Page 148 NORMAL AIRPLANE PROCEDURES FLIGHT MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 3-31 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 149 NORMAL AIRPLANE PROCEDURES FLIGHT MANUAL BUFFET ONSET ENVELOPE The Buffet Onset data are provided by the CAFM presented in the Supplement 1. 3-33 CTA APPROVED code 01 Page 1 ORIGINAL...
  • Page 150 NORMAL AIRPLANE PROCEDURES FLIGHT MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 3-33 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 151 NORMAL AIRPLANE PROCEDURES FLIGHT MANUAL ENHANCED/GROUND PROXIMITY WARNING When an EGPWS alert occurs, use the flight controls and thrust as necessary to correct the airplane attitude, flight path and configuration, according to the voice message presented, to provide terrain clearance. WARNING: IF A TERRAIN AWARENESS WARNING OCCURS, IMMEDIATELY INITIATE AND CONTINUE A CLIMB...
  • Page 152 NORMAL AIRPLANE PROCEDURES FLIGHT MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 3-35 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 153 NORMAL AIRPLANE PROCEDURES FLIGHT MANUAL WINDSHEAR PREVENTION/RECOVERY φThrust Levers .............. MAX φGo Around Button ............PRESS Rotate the airplane smoothly following the Flight Director on EADI to minimize altitude loss. Pitch attitude may be well above normal angles. Maintain airplane configuration. Do not change gear and flap position until terrain clearance is assured.
  • Page 154 NORMAL AIRPLANE PROCEDURES FLIGHT MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 3-37 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 155 NORMAL AIRPLANE PROCEDURES FLIGHT MANUAL TRAFFIC AND COLLISION AVOIDANCE The pilot must not initiate evasive maneuvers using Traffic Advisory information (TA) only, without visually sighting conflicting traffic. The traffic display and advisories are intended for assistance in visually locating the indicated conflicting traffic. Compliance with TCAS resolution advisory is required unless the pilot considers it unsafe to do so.
  • Page 156 NORMAL AIRPLANE PROCEDURES FLIGHT MANUAL WARNING: IF STALL WARNING OCCURS DURING AN RA MANEUVER, IMMEDIATELY ABANDON THE RA AND EXECUTE STALL RECOVERY PROCEDURES. TCAS II WILL CONTINUE TO PROVIDE RAS DURING STALL WARNING AND RECOVERY PROCEDURE. WARNING: IF HIGH SPEED BUFFET IS ENCOUNTERED WHEN INITIALLY RESPONDING TO AN RA, RELAX PITCH FORCE AS NECESSARY TO REDUCE BUFFET, BUT STILL CONTINUE TO MANEUVER.
  • Page 157 NORMAL AIRPLANE PROCEDURES FLIGHT MANUAL TRANSPONDER In compliance with Airworthiness Directive 2006-19-04, during all flight phases, after completion of any 4096 ATC Code change (also referred to as Mode A Code), check the status of the transponder. If the transponder indicates that it is in the standby mode, re-select the desired mode (i.e., the transponder should be in the active mode).
  • Page 158 NORMAL AIRPLANE PROCEDURES FLIGHT MANUAL INTENTIONALLY BLANK 3-40 ANAC APPROVED Page 2 code 01 REVISION 4...
  • Page 159 3-41 ANAC APPROVED code 01 Page 1 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 160 HOLDING Landing Gear ..............UP Flaps ................UP Minimum Airspeed ............210 KIAS 3-41 ANAC APPROVED Page 2 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 161 AIRPLANE NORMAL PROCEDURES FLIGHT MANUAL TURBULENT AIR PENETRATION Adjust airspeed and disconnect the autothrottle. Set thrust for penetration and avoid large thrust variations. Set trim for target speed and do not change it. Use attitude indicator as the primary instrument. Allow altitude and airspeed to vary and maintain attitude.
  • Page 162 AIRPLANE NORMAL PROCEDURES FLIGHT MANUAL MAXIMUM RECOMMENDED TURBULENT PENETRATION SPEED 3-43 ANAC APPROVED Page 2 code 01 REVISION 7...
  • Page 163 AIRPLANE EMERGENCY & ABNORMAL FLIGHT PROCEDURES MANUAL SECTION 4 EMERGENCY AND ABNORMAL PROCEDURES TABLE OF CONTENTS Block Page Introduction .................4-00 ..03 Non-annunciated procedures ..........4-01 ..01 Emergency Procedures ..........4-01 ..03 Abnormal Procedures ............4-01 ..12 Airplane General (Doors/Lighting/Cargo Compartment) ..4-02 ..01 AMS (Pneumatics/Air Conditioning/Pressurization)....4-04 ..01 Autoflight ................4-06 ..01 Auxiliary Power Unit ............4-08 ..01 Electrical ................4-10 ..01...
  • Page 164 AIRPLANE EMERGENCY & ABNORMAL FLIGHT PROCEDURES MANUAL Block Page Landing Gear & Brakes............4-26..01 Oxygen ................4-28..01 Smoke Procedures ............4-30..01 4-00 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 165 AIRPLANE EMERGENCY & ABNORMAL FLIGHT PROCEDURES MANUAL INTRODUCTION The emergency and abnormal procedures contained in this manual have been developed by the airplane manufacturer and approved by the Certification Authority for use in the operation of this airplane. This section provides the emergency and abnormal procedures to be performed in case of a system malfunction or failure, in order to protect passengers and/or crew from serious harm and to maintain the airworthiness of the airplane.
  • Page 166 AIRPLANE EMERGENCY & ABNORMAL FLIGHT PROCEDURES MANUAL The procedures contained herein assume that: − Airplane systems are operating normally prior to the failure. − All emergency/abnormal checklists are performed in the order they are presented in the procedure. − Normal procedures have been properly accomplished. −...
  • Page 167 ENGINE ABNORMAL VIBRATION ........4-01 ..13 ENGINE AIRSTART ............4-01 ..14 ENGINE AIRSTART ENVELOPE........4-01 ..15 ENGINE ITT OVERTEMPERATURE .........4-01 ..16 ENGINE SHUTDOWN............4-01 ..16 4-01 ANAC APPROVED code 01 Page 1 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 168 ONE ENGINE INOPERATIVE APPROACH AND LANDING ............. 4-01..21 OXYGEN LEAKAGE ............4-01..21 PARTIAL OR GEAR UP LANDING........4-01..21 STRUCTURAL DAMAGE ..........4-01..22 4-01 ANAC APPROVED Page 2 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 169 After ditching, set thrust levers to idle, set the start/stop selectors to stop, pull fire-extinguishing handles, announce emergency evacuation and set batteries to off. 4-01 ANAC APPROVED code 01 Page 3 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 170 If a go around is required, maintain slat/flap to 3 and V REF FULL 20 KIAS until the acceleration altitude is reached. 4-01 ANAC APPROVED Page 4 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 171 If applicable, accomplish the One Engine Inoperative Approach and Landing Procedure. 4-01 ANAC APPROVED code 01 Page 5 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 172 After landing, set thrust levers to idle, start/stop selectors to stop, pull and rotate the fire-extinguishing handles, announce emergency evacuation and set batteries to off. 4-01 ANAC APPROVED Page 6 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 173 If a go around is required, maintain V + 15 KIAS (limited to REF FULL 175 KIAS) until the acceleration altitude is reached. 4-01 ANAC APPROVED code 01 Page 7 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 174 If a go around is required, maintain V + 15 KIAS (limited to REF FULL 175 KIAS) until the acceleration altitude is reached. 4-01 ANAC APPROVED Page 8 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 175 NOTE: As assymetric thrust may be required to help controlling the airplane, maximum thrust on both engines may not be possible. 4-01 ANAC APPROVED code 01 Page 9 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 176 NOTE: During RTO the thrust reversers can be used until the airplane comes to a complete stop. When airplane has stopped: Emerg/Parking Brake ..........ON If applicable: EMERGENCY EVACUATION Procedure....ACCOMPLISH 4-01 ANAC APPROVED Page 10 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 177 CTRL → ROLL TRIM PWR or YAW TRIM PWR) and release the A/P disc button. STEERING RUNAWAY φSteer Disc Switch............PRESS φSteer the airplane using differential braking and rudder. 4-01 ANAC APPROVED code 01 Page 11 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 178 FLAPS POSITION PITCH ANGLE 11° 10° 12° - For airplanes Post-Mod. SB 170-31-0019 or equipped with an equivalent modification factory incorporated, rotate the airplane according to the takeoff pitch angle displayed on TAKEOFF page 3/3 on the MCDU. φWith positive climb: φLanding Gear ............
  • Page 179 If unable to keep vibration within limits and engine parameters become abnormal or exceed operating limits, consider an engine shutdown. 4-01 ANAC APPROVED code 01 Page 13 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 180 One Engine Inoperative Approach and Landing Procedure. 4-01 ANAC APPROVED Page 14 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 181 SAT is hotter that -26°C. 21000 20000 15000 Started assist windmill only if N2 greater than 7.2%. 10000 8000 5000 INDICATED AIRSPEED − KIAS 4-01 ANAC APPROVED code 01 Page 15 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 182 (Continues on the next page) 4-01 ANAC APPROVED Page 16 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 183 For landing configuration, set slat/flap to full and set V REF FULL CAUTION: MULTIPLY THE FULL FLAPS UNFACTORED LANDING DISTANCE BY 1.90. 4-01 ANAC APPROVED code 01 Page 17 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 184 If a go around is required, maintain landing gear down, set slat/flap to 4, and maintain V + 10 KIAS until the acceleration REF FULL altitude is reached. 4-01 ANAC APPROVED Page 18 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 185 If a go around is required, maintain landing gear down, set slat/flap to 4, and maintain V + 10 KIAS until the acceleration REF FULL altitude is reached. 4-01 ANAC APPROVED code 01 Page 19 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 186 6000 32000 6300 33000 6700 34000 7000 35000 7300 36000 7600 37000 8000 38000 8000 39000 8000 40000 8000 41000 8000 4-01 ANAC APPROVED Page 20 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 187 If a go around is required, maintain landing gear down. 4-01 ANAC APPROVED code 01 Page 21 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 188 If the fuselage is damaged, limit altitude to 10000 ft or MEA (whichever is higher) and press the pressurization dump button in when reaching 10000 ft. Establish landing configuration early. 4-01 ANAC APPROVED Page 22 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 189 AIRPLANE EMERGENCY & ABNORMAL FLIGHT PROCEDURES MANUAL AIRPLANE GENERAL (DOORS/LIGHTING/CARGO COMPARTMENT) TABLE OF CONTENTS Block Page WARNING DOOR CARGO FORWARD (AFT) OPEN......4-02 ..03 DOOR PASSENGER (SERVICE) FORWARD (AFT) OPEN..........4-02 ..03 CAUTION DOOR FORWARD (CENTER) ELECTRONIC BAY OPEN ........... 4-02 ..04 DOOR HYDRAULIC OPEN..........
  • Page 190 EMERGENCY & AIRPLANE ABNORMAL FLIGHT PROCEDURES MANUAL INTENTIONALLY BLANK 4-02 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 191 AIRPLANE EMERGENCY PROCEDURES FLIGHT MANUAL DOOR CARGO FORWARD (AFT) OPEN If pressurization is normal, continue the flight monitoring the pressurization. If pressurization is abnormal, LAND AT THE NEAREST SUITABLE AIRPORT, limit the altitude to 10000 ft or MEA (whichever is higher). At 10000 ft, push the pressurization dump button in.
  • Page 192 ABNORMAL AIRPLANE PROCEDURES FLIGHT MANUAL DOOR FORWARD (CENTER) ELECTRONIC BAY OPEN If pressurization is abnormal, limit the altitude to 10000 ft or MEA (whichever is higher). DOOR HYDRAULIC OPEN Limit the airspeed to 250 KIAS maximum. EMERGENCY LIGHT NOT ARMED Arm the emergency lights.
  • Page 193 AIRPLANE ABNORMAL PROCEDURES FLIGHT MANUAL EMERGENCY LIGHT BATTERY FAULT Do not takeoff. 4-02 CTA APPROVED code 01 Page 5 REVISION 3...
  • Page 194 ABNORMAL AIRPLANE PROCEDURES FLIGHT MANUAL INTENTIONALLY BLANK 4-02 CTA APPROVED Page 6 code 01 REVISION 3...
  • Page 195 RECIRCULATION SMOKE DETECTION FAILURE ..4-04 ..06 ADVISORY BLEED 1 (2) OFF ...............4-04 ..07 PACK 1 (2) OFF ..............4-04 ..07 4-04 ANAC APPROVED code 01 Page 1 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 196 EMERGENCY & AIRPLANE ABNORMAL FLIGHT PROCEDURES MANUAL INTENTIONALLY BLANK 4-04 ANAC APPROVED Page 2 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 197 If the cabin altitude reaches 14500 ft, set the passenger oxygen selector to OVRD. At 10000 ft or MEA, press the pressurization dump button. 4-04 ANAC APPROVED code 01 Page 3 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 198 APU bleed button out and limit the altitude to 10000 ft or MEA (whichever is higher). At 10000 ft push the pressurization dump button in. 4-04 ANAC APPROVED Page 4 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 199 LAND AT THE NEAREST SUITABLE AIRPORT. FORWARD ELECTRONIC BAY FANS FAILURE If the TRU 1 (2) FAIL is displayed, LAND AT THE NEAREST SUITABLE AIRPORT. 4-04 ANAC APPROVED code 01 Page 5 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 200 At 25000 ft, turn one pack off. At 10000 ft, turn the remaining pack off. RECIRCULATION SMOKE DETECTION FAILURE Turn off the recirculation fan. 4-04 ANAC APPROVED Page 6 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 201 BLEED 1 (2) OFF Limit the altitude to 31000 ft maximum. PACK 1 (2) OFF Limit the altitude to 31000 ft maximum. 4-04 ANAC APPROVED code 01 Page 7 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 202 ABNORMAL AIRPLANE PROCEDURES FLIGHT MANUAL INTENTIONALLY BLANK 4-04 ANAC APPROVED Page 8 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 203 STALL PROTECTION FAILURE ........4-06 ..04 ADVISORY AUTO FLIGHT CONTROL SYSTEM FAULT ....4-06 ..05 STALL PROTECTION FAULT........... 4-06 ..05 4-06 ANAC APPROVED code 01 Page 1 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 204 EMERGENCY & AIRPLANE ABNORMAL FLIGHT PROCEDURES MANUAL INTENTIONALLY BLANK 4-06 ANAC APPROVED Page 2 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 205 FLIGHT DIRECTOR LATERAL MODE OFF Select a flight director lateral mode. FLIGHT DIRECTOR VERTICAL MODE OFF Select a flight director vertical mode. 4-06 ANAC APPROVED code 01 Page 3 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 206 For landing with slat/flap full, set V + 10 KIAS. REF FULL CAUTION: MULTIPLY FULL FLAPS UNFACTORED LANDING DISTANCE BY 1.22. 4-06 ANAC APPROVED Page 4 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 207 ABNORMAL AIRPLANE PROCEDURES FLIGHT MANUAL AUTO FLIGHT CONTROL SYSTEM FAULT Do not takeoff. STALL PROTECTION FAULT Do not takeoff. 4-06 ANAC APPROVED code 01 Page 5 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 208 ABNORMAL AIRPLANE PROCEDURES FLIGHT MANUAL INTENTIONALLY BLANK 4-06 ANAC APPROVED Page 6 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 209 EMERGENCY & AIRPLANE ABNORMAL FLIGHT PROCEDURES MANUAL AUXILIARY POWER UNIT TABLE OF CONTENTS Block Page CAUTION APU ALTITUDE EXCEEDNACE ........4-08 ..03 APU FAILURE ..............4-08 ..03 APU FAULT ............... 4-08 ..03 APU OIL HIGH TEMPERATURE ........4-08 ..03 APU OIL LOW PRESSURE..........
  • Page 210 EMERGENCY & AIRPLANE ABNORMAL FLIGHT PROCEDURES MANUAL INTENTIONALLY BLANK 4-08 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 211 ABNORMAL AIRPLANE PROCEDURES FLIGHT MANUAL APU ALTITUDE EXCEEDANCE If APU is not essential for the flight, turn it off. If APU is essential for the flight, descend to an altitude where the message is no longer displayed. APU FAILURE If the APU FAIL message was displayed during APU start, the APU can be restarted according to the starter limitations.
  • Page 212 ABNORMAL AIRPLANE PROCEDURES FLIGHT MANUAL INTENTIONALLY BLANK 4-08 CTA APPROVED Page 4 code 01 ORIGINAL...
  • Page 213 IDG 1 (2) OFF BUS ............4-10..10 IDG 1 (2) OIL ..............4-10..10 TRU 1 (2) FAILURE............4-10..10 TRU ESSENTIAL FAILURE ..........4-10..10 4-10 ANAC APPROVED code 01 Page 1 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 214 EMERGENCY & AIRPLANE ABNORMAL FLIGHT PROCEDURES MANUAL INTENTIONALLY BLANK 4-10 ANAC APPROVED Page 2 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 215 NOTE: Do not start the APU. BATTERY 1-2 OFF LAND AT THE NEAREST SUITABLE AIRPORT. NOTE: APU start is not available. 4-10 ANAC APPROVED code 01 Page 3 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 216 If a go around is required, maintain slat/flap 3 and V + 20 KIAS REF FULL or 130 KIAS (whichever is higher) until the acceleration altitude is reached. 4-10 ANAC APPROVED Page 4 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 217 AC ESSENTIAL BUS OFF NOTE: - The flaps and slats will operate at low rate. - Fuel Crossfeed Low 1 is not available. 4-10 ANAC APPROVED code 01 Page 5 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 218 NOTE: If battery 1 selector is off, APU start is not available. BATTERY 2 OFF Verify battery 2 is set to auto. 4-10 ANAC APPROVED Page 6 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 219 LAND AT THE NEAREST SUITABLE AIRPORT. Exit and avoid icing conditions and set battery 1 to off. (Continues on the next page) 4-10 ANAC APPROVED code 01 Page 7 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 220 For landing configuration, set slat/flap to full and V REF FULL On ground, apply brakes normally. CAUTION: MULTIPLY THE FULL FLAPS UNFACTORED LANDING DISTANCE BY 1.70. 4-10 ANAC APPROVED Page 8 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 221 Turn the APU off. For landing configuration, set slat/flap to full and REF FULL On ground, apply brakes normally. CAUTION: MULTIPLY THE FULL FLAPS UNFACTORED LANDING DISTANCE BY 1.80. 4-10 ANAC APPROVED code 01 Page 9 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 222 If the TRU 1 (2) FAIL message persists, select the affected TRU to off. TRU ESSENTIAL FAILURE Select the TRU ESS to off. 4-10 ANAC APPROVED Page 10 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 223 ENGINE REFERENCE ECS DISAGREE ......4-12..07 ENGINE THRUST LEVER ANGLE NOT TOGA ....4-12..07 ENGINE THRUST RATING DISAGREE ......4-12..07 4-12 ANAC APPROVED code 01 Page 1 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 224 EMERGENCY & AIRPLANE ABNORMAL FLIGHT PROCEDURES MANUAL INTENTIONALLY BLANK 4-12 ANAC APPROVED Page 2 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 225 Landing Procedure. ENGINE 1 (2) OIL LOW PRESSURE If the affected oil pressure indication is abnormal, accomplish the Engine Shutdown Procedure. 4-12 ANAC APPROVED code 01 Page 3 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 226 If fuel leak is not suspected and a restart is not considered, accomplish the One Engine Inoperative Approach and Landing Procedure. 4-12 ANAC APPROVED Page 4 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 227 ENGINE 1 (2) REVERSER THRUST LEVER ANGLE FAILURE On ground, the associated thrust reverser is not available. Inflight, do not move the thrust levers below idle. 4-12 ANAC APPROVED code 01 Page 5 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 228 ENGINE REFERENCE ANTI-ICE DISAGREE Configure the airplane according to takeoff data or re enter the takeoff data according to airplane configuration. 4-12 ANAC APPROVED Page 6 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 229 ENGINE THRUST LEVER ANGLE NOT TOGA Move the thrust levers to TOGA position. ENGINE THRUST RATING DISAGREE Do not takeoff. 4-12 ANAC APPROVED code 01 Page 7 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 230 ABNORMAL AIRPLANE PROCEDURES FLIGHT MANUAL INTENTIONALLY BLANK 4-12 ANAC APPROVED Page 8 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 231 APU FIRE-EXTINGUISHING FAILURE ......4-14..04 CARGO AFT (FORWARD) FIRE SYSTEM FAILURE ..4-14..04 ENGINE 1 (2) FIRE DETECTION FAILURE ..... 4-14..04 4-14 ANAC APPROVED code 01 Page 1 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 232 EMERGENCY & AIRPLANE ABNORMAL FLIGHT PROCEDURES MANUAL INTENTIONALLY BLANK 4-14 ANAC APPROVED Page 2 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 233 Use the APU, the autothrottle and fuel crossfeed as required. When appropriate, accomplish the One Engine Inoperative Approach and Landing Procedure. 4-14 ANAC APPROVED code 01 Page 3 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 234 ENGINE 1 (2) FIRE DETECTION FAILURE If fire is suspected in the affected engine, accomplish the Engine Fire, Severe Damage or Separation Procedure. 4-14 ANAC APPROVED Page 4 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 235 SPOILER FAULT ............... 4-16..09 STABILIZER LOCK FAULT ..........4-16..10 ADVISORY AILERON RH (LH) FAILURE..........4-16..10 FLIGHT CONTROL FAULT ..........4-16..10 4-16 ANAC APPROVED code 01 Page 1 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 236 EMERGENCY & AIRPLANE ABNORMAL FLIGHT PROCEDURES MANUAL INTENTIONALLY BLANK 4-16 ANAC APPROVED Page 2 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 237 For landing configuration, set slat/flap to full and set V REF FULL CAUTION: MULTIPLY THE FULL FLAPS UNFACTORED LANDING DISTANCE BY 1.45. 4-16 ANAC APPROVED code 01 Page 3 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 238 If a go around is required, set slat/flap to 4 and maintain + 15 KIAS until the acceleration altitude is reached. REF FULL 4-16 ANAC APPROVED Page 4 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 239 1.31 1.29 Ldg Coef USABLE REF FULL REF FULL FULL (KIAS) 1.06 NOT APPLICABLE Ldg Coef (Continues on the next page) 4-16 ANAC APPROVED code 01 Page 5 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 240 3, 4 and 5 (KIAS) 1.31 1.29 Ldg Coef USABLE REF FULL REF FULL (KIAS) FULL 1.06 NOT APPLICABLE Ldg Coef 4-16 ANAC APPROVED Page 6 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 241 If a go around is required, set slat/flap to 4 and maintain + 15 KIAS until the acceleration altitude is reached. REF FULL 4-16 ANAC APPROVED code 01 Page 7 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 242 If the RUDDER FAULT message persists and is associated with the RUDDER LIMITER FAIL message, reset (push in, then out) the flight controls mode rudder button once again. 4-16 ANAC APPROVED Page 8 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 243 If all spoiler panels are closed, for landing configuration set slat/flap to full and set V REF FULL CAUTION: MULTIPLY FULL FLAPS UNFACTORED LANDING DISTANCE BY 1.45. 4-16 ANAC APPROVED code 01 Page 9 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 244 5 and maintain V + 10 KIAS. REF FULL CAUTION: MULTIPLY FULL FLAPS UNFACTORED LANDING DISTANCE BY 1.30. FLIGHT CONTROL FAULT Do not takeoff. 4-16 ANAC APPROVED Page 10 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 245 AVIONICS MAU 1 (2) (3) A (B) OVERHEAT..... 4-18..07 AVIONICS MAU 1 (2) (3) FAN FAILURE ......4-18..07 COMMUNICATION MANAGEMENT SYSTEM FAILURE............4-18..07 4-18 ANAC APPROVED code 01 Page 1 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 246 VHF 1 (2) (3) OVERHEAT ..........4-18 ..10 WINDSHEAR FAILURE.............4-18 ..10 ADVISORY ADS PROBE 1 (2) (3) (4) FAILURE........4-18 ..11 4-18 ANAC APPROVED Page 2 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 247 EMERGENCY AIRPLANE PROCEDURES FLIGHT MANUAL NO TAKEOFF CONFIGURATION Configure the airplane for takeoff. 4-18 ANAC APPROVED code 01 Page 3 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 248 Monitor visual indications. NOTE: Aural warnings, including EGPWS callouts, are lost. TCAS aural will be operative. AVIONICS ASCB FAULT Do not takeoff. 4-18 ANAC APPROVED Page 4 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 249 CAUTION: MULTIPLY THE FULL FLAPS UNFACTORED LANDING DISTANCE BY 1.15. AVIONICS MAU 2A FAILURE On ground, steer the airplane using rudder and differential braking. 4-18 ANAC APPROVED code 01 Page 5 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 250 For landing configuration, set slat/flap to full and set V REF FULL CAUTION: MULTIPLY THE FULL FLAPS UNFACTORED LANDING DISTANCE BY 1.20. 4-18 ANAC APPROVED Page 6 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 251 Setting will be locked at the last setting position prior to the failure. - Disregard altitude callouts from aural system. - Use IESS for barometric setting and ILS approach. 4-18 ANAC APPROVED code 01 Page 7 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 252 Pull the associated circuit breaker. For MCDU 1 OVHT, pull the B16 CB. For MCDU 2 OVHT, pull the B31 CB. 4-18 ANAC APPROVED Page 8 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 253 Altitude, FMA, FPA, Minimuns, Baro setting, Nav-Com radios frequencies, HDG and CRS) with the opposite side PFD display information. Disregard any non-reliable information from the affected PFD. 4-18 ANAC APPROVED code 01 Page 9 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 254 For VHF 3 OVHT, pull the VHF 3 Electronic CB. WINDSHEAR FAILURE Increase awareness in relation to weather, wind and speed variations. 4-18 ANAC APPROVED Page 10 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 255 ABNORMAL AIRPLANE PROCEDURES FLIGHT MANUAL ADS PROBE 1 (2) (3) (4) FAILURE Do not takeoff. 4-18 ANAC APPROVED code 01 Page 11 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 256 ABNORMAL AIRPLANE PROCEDURES FLIGHT MANUAL INTENTIONALLY BLANK 4-18 ANAC APPROVED Page 12 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 257 (POST-MOD. SB 170-31-0017 OR EQUIVALENT MODIFICATION FACTORY INCORPORATED) ..4-20..04 FUEL TANK LOW TEMPERATURE (PRE-MOD. SB 170-31-0017) ........4-20..05 4-20 ANAC APPROVED code 01 Page 1 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 258 EMERGENCY & AIRPLANE ABNORMAL FLIGHT PROCEDURES MANUAL INTENTIONALLY BLANK 4-20 ANAC APPROVED Page 2 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 259 If fuel leak is suspected, accomplish the Fuel Leak Procedure. If fuel leak is not suspected, operate fuel crossfeed as required. 4-20 ANAC APPROVED code 01 Page 3 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 260 FUEL AC PUMP 1 (2) FAILURE Select the crossfeed selector to OFF. FUEL DC PUMP FAILURE Turn the fuel DC pump off. 4-20 ANAC APPROVED Page 4 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 261 Increase airspeed as much as possible up to V and wait 3 minutes. If the FUEL TANK LO TEMP message persists, descend to lower altitudes. 4-20 ANAC APPROVED code 01 Page 5 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 262 If fuel crossfeed is set to LOW 1 or LOW 2 and fuel quantity is not being equalized, set the fuel crossfeed to OFF and use asymmetric thrust as required. 4-20 ANAC APPROVED Page 6 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 263 EMERGENCY & AIRPLANE ABNORMAL FLIGHT PROCEDURES MANUAL HYDRAULICS TABLE OF CONTENTS Block Page WARNING HYDRAULIC SYSTEM 1 OR 2 OVERHEAT..... 4-22..03 HYDRAULIC SYSTEM 3 OVERHEAT ......4-22..03 CAUTION HYDRAULIC PTU FAILURE ..........4-22..04 HYDRAULIC 1 (2) EDP NOT D-PRESSED ...... 4-22..04 HYDRAULIC 1 (2) HIGH TEMPERATURE .......
  • Page 264 EMERGENCY & AIRPLANE ABNORMAL FLIGHT PROCEDURES MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 4-22 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 265 EMERGENCY AIRPLANE PROCEDURES FLIGHT MANUAL HYDRAULIC SYSTEM 1 OR 2 OVERHEAT Set the associated electric hydraulic pump to off and push the associated engine pump shutoff button in. If HYD 1 (2) SOV FAIL message is presented, LAND AT THE NEAREST SUITABLE AIRPORT and accomplish the Engine Shutdown Procedure.
  • Page 266 ABNORMAL AIRPLANE PROCEDURES FLIGHT MANUAL HYDRAULIC PTU FAILURE Turn the PTU on. If the message HYD PTU FAIL persists, turn the PTU to OFF. NOTE: During cruise flight, if PTU is commanded ON, it may be turned to AUTO. HYDRAULIC 1 (2) EDP NOT D-PRESSED An engine windmill restart will not be available.
  • Page 267 ABNORMAL AIRPLANE PROCEDURES FLIGHT MANUAL HYDRAULIC TEMPERATURE SENSORS FAILURE Do not takeoff. 4-22 CTA APPROVED code 01 Page 5 REVISION 3...
  • Page 268 ABNORMAL AIRPLANE PROCEDURES FLIGHT MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 4-22 CTA APPROVED Page 6 code 01 REVISION 3...
  • Page 269 ANTI-ICE WING FAILURE ..........4-24 ..04 ICE DETECTOR 1 (2) FAILURE ........4-24 ..05 WINDSHIELD 1 (2) HEATER FAILURE......4-24 ..05 4-24 ANAC APPROVED code 01 Page 1 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 270 EMERGENCY & AIRPLANE ABNORMAL FLIGHT PROCEDURES MANUAL INTENTIONALLY BLANK 4-24 ANAC APPROVED Page 2 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 271 31000 ft maximum. If bleed 1 is the affected bleed, push out the APU bleed button. 4-24 ANAC APPROVED code 01 Page 3 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 272 V REF FLAP 5 ICE CAUTION: MULTIPLY THE FULL FLAPS UNFACTORED LANDING DISTANCE BY 1.30. Limit bank angle to 20° maximum. 4-24 ANAC APPROVED Page 4 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 273 Push the affected windshield-heating button out and then push in. If the WINDSHIELD 1 (2) HTR FAIL message persists, push the affected windshield-heating button out. 4-24 ANAC APPROVED code 01 Page 5 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 274 ABNORMAL AIRPLANE PROCEDURES FLIGHT MANUAL INTENTIONALLY BLANK 4-24 ANAC APPROVED Page 6 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 275 SYSTEM FAILURE ............4-26..05 STEERING FAILURE ............4-26..05 ADVISORY BRAKE CONTROL FAULT..........4-26..06 BRAKE LH (RH) FAULT ............ 4-26..06 4-26 ANAC APPROVED code 01 Page 1 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 276 EMERGENCY & AIRPLANE ABNORMAL FLIGHT PROCEDURES MANUAL INTENTIONALLY BLANK 4-26 ANAC APPROVED Page 2 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 277 If the LG LEVER DISAG message persists and it was displayed after a landing gear retraction, maintain landing gear down and avoid/exit icing conditions. 4-26 ANAC APPROVED code 01 Page 3 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 278 EMERGENCY BRAKE FAILURE When parking the airplane, use wheel chocks. LANDING GEAR NO DISPATCH Do not takeoff. 4-26 ANAC APPROVED Page 4 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 279 NOTE: Thrust Reversers, Steering, Ground Spoilers, Wing Anti-Ice and Ground Idle may not be available. STEERING FAILURE Steer the airplane using differential braking and rudder. 4-26 ANAC APPROVED code 01 Page 5 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 280 During landing run, expect a slight directional tendency. Apply brakes normally. CAUTION: MULTIPLY THE FULL FLAPS UNFACTORED LANDING DISTANCE BY 1.28. 4-26 ANAC APPROVED Page 6 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 281 AIRPLANE EMERGENCY & ABNORMAL FLIGHT PROCEDURES MANUAL OXYGEN TABLE OF CONTENTS Block Page CAUTION CREW OXYGEN LOW PRESSURE ......... 4-28..03 PASSENGER OXYGEN NOT DEPLOYED....... 4-28..03 ADVISORY OBSERVER OXYGEN LOW PRESSURE ......4-28..03 4-28 CTA APPROVED Page 1 code 01 ORIGINAL...
  • Page 282 AIRPLANE EMERGENCY & ABNORMAL FLIGHT PROCEDURES MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 4-28 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 283 AIRPLANE ABNORMAL PROCEDURES FLIGHT MANUAL CREW OXYGEN LOW PRESSURE Limit altitude to 10000 ft or MEA (whichever is higher) maximum, whichever is higher. PASSENGER OXYGEN NOT DEPLOYED If required, deploy the passenger oxygen masks manually. OBSERVER OXYGEN LOW PRESSURE If the observer seat is occupied, limit altitude to 10000 ft or MEA (whichever is higher) maximum.
  • Page 284 AIRPLANE ABNORMAL PROCEDURES FLIGHT MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 4-28 CTA APPROVED Page 4 code 01 ORIGINAL...
  • Page 285 LAVATORY SMOKE............4-30..03 SMOKE EVACUATION ............. 4-30..03 SMOKE, FIRE OR FUMES..........4-30..04 CAUTION RECIRCULATION SMOKE ..........4-30..08 4-30 ANAC APPROVED code 01 Page 1 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 286 EMERGENCY & AIRPLANE ABNORMAL FLIGHT PROCEDURES MANUAL INTENTIONALLY BLANK 4-30 ANAC APPROVED Page 2 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 287 If cabin rate is less than 1000 ft/min, set the pressurization to manual and turn the recirculation fan and both packs off. Accomplish the Emergency Descent Procedure. 4-30 ANAC APPROVED code 01 Page 3 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 288 CAUTION: MULTIPLY THE FULL FLAPS UNFACTORED LANDING DISTANCE BY 2.10. NOTE: On ground, steer the airplane using differential braking and rudder. (Continues on the next page) 4-30 ANAC APPROVED Page 4 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 289 Landing configuration: Emergency Lights........ ARMED Ground Proximity Flap Override Button ......PUSH IN Slat/flap Lever........3 (Continues on the next page) 4-30 ANAC APPROVED code 01 Page 5 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 290 Set V + 20 KIAS. REF FULL CAUTION: MULTIPLY FULL FLAPS UNFACTORED LANDING DISTANCE BY 2.10. (Continues on the next page) 4-30 ANAC APPROVED Page 6 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 291 (Continued from the previous page) If a go around is required: Slat/flap Lever......3 + 20 KIAS until the acceleration altitude REF FULL is reached. 4-30 ANAC APPROVED code 01 Page 7 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 292 ABNORMAL AIRPLANE PROCEDURES FLIGHT MANUAL RECIRCULATION SMOKE LAND AT THE NEAREST SUITABLE AIRPORT Recirc Fan Button ............PUSH OUT 4-30 ANAC APPROVED Page 8 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 293 PERFORMANCE AIRPLANE FLIGHT MANUAL SECTION 5 PERFORMANCE TABLE OF CONTENTS Block Page Introduction ................ 5-00..02 Performance Configuration..........5-01..01 Definitions ................5-01..02 Demonstrated Crosswind ..........5-01..21 Noise Levels ..............5-03..01 Position Error Corrections..........5-05..01 Airspeed Position Error Correction Chart ..... 5-05..01 Altitude Position Error Correction Chart......
  • Page 294 PERFORMANCE AIRPLANE FLIGHT MANUAL INTRODUCTION The performance information given in this Section is applicable and common to all EMBRAER 170 and EMBRAER 175 models. For performance information related EMBRAER 170 EMBRAER 175 equipped with specific engine model, refer to the Supplement 1 - CAFM.
  • Page 295 AIRPLANE PERFORMANCE FLIGHT MANUAL PERFORMANCE CONFIGURATION The configurations applicable to each performance phase are shown below. OPERATING FLAPS GEAR AIRSPEED ENGINES TAKEOFF 2 until V TOGA 1, 2, or 4 DOWN 0 TO V 1 after V DOWN TO SEGMENT TOGA 1, 2, or 4 TO V...
  • Page 296 AIRPLANE PERFORMANCE FLIGHT MANUAL DEFINITIONS TEMPERATURES OUTSIDE AIR TEMPERATURE - OAT or SAT Free static air (ambient) temperature. INTERNATIONAL STANDARD ATMOSPHERE - ISA As accepted by the International Civil Aviation Organization. ISA DEVIATION - r r ISA Temperature deviation from the standard temperature defined for ISA, at the specified altitude.
  • Page 297 AIRPLANE PERFORMANCE FLIGHT MANUAL AIRPORT DECLARED FIELD DATA TAKEOFF RUN AVAILABLE - TORA The runway length declared available and suitable for the ground run of an airplane taking off. TAKEOFF DISTANCE AVAILABLE - TODA The length of the runway plus the length of any available clearway, except that the length of any clearway included must not be greater than one-half the length of the runway.
  • Page 298 AIRPLANE PERFORMANCE FLIGHT MANUAL CLEARWAY It is an area beyond the runway, not less than 500 ft wide, centrally located about the extended centerline of the runway, and under the control of the airport authorities. It is expressed in terms of a clear way plane extending from the end of the runway with an upward slope not exceeding 1.25%, above which no object or terrain protrudes.
  • Page 299 PERFORMANCE AIRPLANE FLIGHT MANUAL TAKEOFF RUN ONE ENGINE INOPERATIVE (DRY RUNWAY) It is the gross distance along the takeoff path from the start of takeoff to the mid point between lift off and the point at which the airplane is 35 ft above the takeoff surface, the critical engine having failed at V TAKEOFF ENGINE...
  • Page 300 PERFORMANCE AIRPLANE FLIGHT MANUAL ALIGNMENT ALLOWANCE It is the runway length distance that is lost when the airplane maneuvers into the runway prior to takeoff. There are two alignments distances: − ASDA Alignment: is the distance from the airplane nose landing gear to the start of the runway surface.
  • Page 301 PERFORMANCE AIRPLANE FLIGHT MANUAL CONTAMINATED RUNWAY - STANDING WATER A runway is considered contaminated by standing water when covered by more than 3 mm deep water. CONTAMINATED RUNWAY - SLUSH A runway is considered contaminated by slush, when covered by partly melted snow or ice with high water content, such that it cannot significantly resist compression by hand, and of an assumed specific gravity of 0.85.
  • Page 302 PERFORMANCE AIRPLANE FLIGHT MANUAL MINIMUM CONTROL SPEED IN THE AIR - V It is the minimum speed at which, when the critical engine is suddenly made inoperative, it is possible to maintain control of the airplane with the remaining engine at takeoff thrust, and maintain a straight flight with an angle of bank of not more than 5°.
  • Page 303 PERFORMANCE AIRPLANE FLIGHT MANUAL OPTIMUM V It is the V speed that assures the greatest V dependent takeoff weight. ROTATION SPEED - V It is the speed at which the pilot starts to rotate the airplane during the takeoff ground run. TAKEOFF SAFETY SPEED - V It is the target speed to be attained at 35 ft height above runway surface, the critical engine having failed at V...
  • Page 304 PERFORMANCE AIRPLANE FLIGHT MANUAL APPROACH CLIMB SPEED It is the go-around speed in the approach configuration, with one engine inoperative, approach flaps, and landing gear retracted. LANDING CLIMB SPEED It is the go-around speed in the landing configuration, with all engines operating, landing flaps, and landing gear extended.
  • Page 305 PERFORMANCE AIRPLANE FLIGHT MANUAL TAKEOFF PATH The takeoff path assumes failure of one engine at V and extends from a standing start to a point in takeoff at which the airplane is at least 1500 ft above takeoff surface and has achieved the enroute configuration and final segment climb speed.
  • Page 306 PERFORMANCE AIRPLANE FLIGHT MANUAL MAXIMUM LEVEL-OFF HEIGHT It is the height where the takeoff thrust time limit occurs at the end of the acceleration segment. The maximum level-off height cannot be lower than the minimum level-off height. FIRST SEGMENT Starts at 35 ft above the takeoff surface, at the end of the one-engine- inoperative takeoff distance (TOD/OEI), and extends to the point where the landing gear is fully retracted using a constant V speed and...
  • Page 307 PERFORMANCE AIRPLANE FLIGHT MANUAL MAXIMUM TAKEOFF WEIGHT - MTOW It is the maximum structural takeoff weight. CLIMB LIMITED TAKEOFF WEIGHT (OR TAKEOFF WAT) It is the maximum allowed takeoff weight for the airport altitude and temperature, and complying with the takeoff and go-around climb gradient requirements.
  • Page 308 PERFORMANCE AIRPLANE FLIGHT MANUAL ENGINE RATINGS CRITICAL ENGINE It is the engine whose failure would most adversely affect the performance or handling qualities of the airplane. TAKEOFF THRUST It is the maximum thrust available for takeoff, usually time limited. NORMAL TAKEOFF THRUST - NTO It is the maximum thrust available for the all-engine-operating takeoff, or for the one-engine-inoperative takeoff when ATTCS is not used.
  • Page 309 PERFORMANCE AIRPLANE FLIGHT MANUAL NORMAL GO-AROUND THRUST It is the maximum thrust available for the all-engine-operating go- around, or for the one-engine-inoperative go-around when ATTCS is not used. It is usually time limited. MAXIMUM CONTINUOUS THRUST It is the maximum thrust that may be used continuously, not time limited.
  • Page 310 PERFORMANCE AIRPLANE FLIGHT MANUAL LOAD FACTOR It is the ratio between the aerodynamic force component acting normal to the longitudinal axis of the airplane and the airplane weight. A positive load factor is one in which the aerodynamic force acts upward with respect to the airplane.
  • Page 311 PERFORMANCE AIRPLANE FLIGHT MANUAL The input and range V values are “label” values in the sense that they usually occur in the low thrust to weight ratio region, where the airplane is at or close to the climb limiting condition. At high thrust to weight ratio regions the airplane has better accelerating capabilities, which leads to higher speeds achieved at the takeoff screen height, thus increasing the output V...
  • Page 312 PERFORMANCE AIRPLANE FLIGHT MANUAL REVERSE THRUST PERFORMANCE CREDIT Reverse thrust performance credit can be granted according to operational regulations. Usually, reverse thrust credit can be taken for: Takeoff field length performance: wet and contaminated runways; Landing field length performance: contaminated runway. Regulations also require that the reverse thrust system reliability be demonstrated to a certain degree.
  • Page 313 PERFORMANCE AIRPLANE FLIGHT MANUAL Maximum stopping margin allows the user to limit the calculation of MIN as follows: as actual takeoff weight is reduced below the FLLW, the calculation of V MIN proceeds normally; at the point where the specified stopping margin is reached, the calculation of V MIN is governed by the stopping margin, i.e., V MIN is increased in order to...
  • Page 314 PERFORMANCE AIRPLANE FLIGHT MANUAL The speed is incremented as following: Bank Angle Takeoff Flaps Flaps Retracted from 0° to 15° from 15° up to 20° + 5 KIAS + 5 KIAS from 20° up to 25° + 10 KIAS + 10 KIAS Once bank angle is known, the speed is set according to table above and the climb gradients are calculated for both wings level and the specified bank angle.
  • Page 315 PERFORMANCE AIRPLANE FLIGHT MANUAL The effect of the overspeed required by AFM procedures for landing in emergency or abnormal configurations has been already taken into account in the landing distance factors therein presented. Therefore, the CAFM V OVERSPEED feature is not to be used for calculation of the landing performance for the AFM emergency or abnormal cases, due to the different airplane configurations involved.
  • Page 316 PERFORMANCE AIRPLANE FLIGHT MANUAL INTENTIONALLY BLANK 5-01 ANAC APPROVED Page 22 code 01 REVISION 6...
  • Page 317 • Thrust Reverser LH assemblies P/N 15G0002-012. • Thrust Reverser RH assemblies P/N 15G0003-012. NOISE LEVEL IN EPNdB CONDITION Airplane Model Flyover Lateral Approach EMBRAER 170 STD 83.0 92.3 94.9 EMBRAER 170 LR 84.1 92.3 94.9 84.1 92.3 94.9 EMBRAER 170 SU EMBRAER 170 SE 84.1...
  • Page 318 83.2 92.0 94.9 EMBRAER 170 SE NOTE: (1) For airplanes Post-Mod. SB 170-00-0003 or with an equivalent modification factory incorporated, the noise levels remain the same. The noise levels for EMBRAER 170 equipped with APU Hamilton Sundstrand APS 2300 and two GE CF34-8E5 engines were established as follows: −...
  • Page 319 EMBRAER 170 SE 81.9 90.6 95.1 NOTE: (1) For airplanes Post-Mod. SB 170-00-0003 or with an equivalent modification factory incorporated, the noise levels remain the same. The noise levels for EMBRAER 170 equipped with APU Hamilton Sundstrand APS 2300 and two GE CF34-8E5 engines were established as follows: −...
  • Page 320 PERFORMANCE AIRPLANE FLIGHT MANUAL INTENTIONALLY BLANK 5-03 ANAC APPROVED Page 4 code 02 REVISION 12...
  • Page 321 95.0 84.4 91.9 95.0 EMBRAER 175 SU The noise levels for EMBRAER 175 equipped with APU Hamilton Sundstrand APS 2300 and two GE CF34-8E5 engines were established as follows: − Flyover: at maximum takeoff weight, flap setting 1 and thrust power cutback;...
  • Page 322 95.2 EMBRAER 175 SU 83.3 90.5 95.2 The noise levels for EMBRAER 175 equipped with APU Hamilton Sundstrand APS 2300 and two GE CF34-8E5 engines were established as follows: − Flyover: at maximum takeoff weight, flap setting 1 and thrust power cutback;...
  • Page 323 91.9 95.0 EMBRAER 175 LR NOTE: (1) For airplanes Post-Mod. SB 170-00-0016 or equipped with an equivalent modification factory incorporated. The noise levels for EMBRAER 175 equipped with APU Hamilton Sundstrand APS 2300 and two GE CF34-8E5, were established as follows: −...
  • Page 324 95.2 EMBRAER 175 SU EMBRAER 175 LR NOTE: (1) For airplanes Post-Mod. SB 170-00-0016 or equipped with an equivalent modification factory incorporated. The noise levels for EMBRAER 175 equipped with APU Hamilton Sundstrand APS 2300 and two GE CF34-8E5 engines were established as follows: −...
  • Page 325 PERFORMANCE AIRPLANE FLIGHT MANUAL POSITION ERROR CORRECTIONS The corrections to be applied to indicated airspeed or altitude in order to eliminate the effect of location of the static port on instrument readings are shown in the Airspeed Position Error Correction charts and in the Altitude Position Error Correction charts.
  • Page 326 PERFORMANCE AIRPLANE FLIGHT MANUAL AIRSPEED POSITION ERROR CORRECTION AIR DATA SYSTEM 3 FLAPS 0, 1, 2, 3, 4, 5 AND FULL NOTE: ALL ALTITUDES FLAPS 0 FLAPS 1 FLAPS 2 FLAPS FULL FLAPS 3, 4 AND 5 INDICATED AIRSPEED - kt 5-05 CTA APPROVED Page 2...
  • Page 327 PERFORMANCE AIRPLANE FLIGHT MANUAL ALTITUDE POSITION ERROR CORRECTION CHART Enter the appropriate chart with indicated airspeed, the indicated pressure altitude considering the appropriate airplane configuration to read the altimetric correction. The true pressure altitude will be the indicated pressure altitude minus the altimetric correction. EXAMPLE Given: ADSP 3...
  • Page 328 PERFORMANCE AIRPLANE FLIGHT MANUAL ALTITUDE POSITION ERROR CORRECTION AIR DATA SYSTEM 3 FLAPS 0,1, 2, 3, 4, 5 AND FULL NOTE: ALL ALTITUDES FLAPS 3, 4 AND 5 FLAPS 2 FLAPS 1 FLAPS FULL FLAPS 0 INDICATED AIRSPEED - kt 5-05 CTA APPROVED Page 4...
  • Page 329 PRIMUS EPIC - FLIGHT MANAGEMENT SYSTEM CATEGORY II OPERATION RVSM OPERATION NOT APPLICABLE NOT APPLICABLE NOT APPLICABLE NOT APPLICABLE NOT APPLICABLE NOT APPLICABLE S-TOC ANAC APPROVED code 02 Page 1 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 330 SUPPLEMENTS AIRPLANE FLIGHT MANUAL NOT APPLICABLE S-TOC ANAC APPROVED Page 2 code 02 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 331 SUPPLEMENT 1 AIRPLANE COMPUTERIZED AFM FLIGHT MANUAL SUPPLEMENT 1 COMPUTERIZED AIRPLANE FLIGHT MANUAL TABLE OF CONTENTS Block Page Introduction ................ S1-00 ..02 Software Presentation ............S1-02 ..01 Limitations................S1-05 ..01 Configuration ..............S1-05 ..01 Normal Procedures............S1-10 ..01 Emergency and Abnormal Procedures ......
  • Page 332 SUPPLEMENT 1 AIRPLANE COMPUTERIZED AFM FLIGHT MANUAL INTRODUCTION This Supplement presents the Computerized Airplane Flight Manual CAFM - for EMBRAER 170 and EMBRAER 175 performance calculation. S1-00 ANAC APPROVED Page 2 code 01 REVISION 4...
  • Page 333 SUPPLEMENT 1 AIRPLANE COMPUTERIZED AFM FLIGHT MANUAL SOFTWARE PRESENTATION The Computerized Airplane Flight Manual - CAFM performance calculation software has been developed employing a modular concept and in a manner that allows the user to run only the specific configuration applicable to his/her airplane. Among the many modules that compose the software, three kinds are worth emphasizing: −...
  • Page 334 SUPPLEMENT 1 AIRPLANE COMPUTERIZED AFM FLIGHT MANUAL INTENTIONALLY BLANK S1-02 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 335 (LOAD 19.3) MUST SELECT FIXED V OPTION AND MUST USE THE FOLLOWING VALUES: FLAPS POSITION FIXED V 1.20 1.20 1.19 CONTINUES ON NEXT PAGE S1-05 ANAC APPROVED code 02 Page 1 REVISION 14 Copyright © by Embraer. Refer to cover page for details.
  • Page 336 AFM. - This version incorporates all capabilities of the previous versions. S1-05 ANAC APPROVED Page 2 code 02 REVISION 14 Copyright © by Embraer. Refer to cover page for details.
  • Page 337 (LOAD 19.3) MUST SELECT FIXED V OPTION AND MUST USE THE FOLLOWING VALUES. FLAPS POSITION FIXED V 1.20 1.17 to 1.21 1.19 CONTINUES ON NEXT PAGE S1-05 ANAC APPROVED code 05 Page 1 REVISION 14 Copyright © by Embraer. Refer to cover page for details.
  • Page 338 AFM. - This version incorporates all capabilities of the previous versions. S1-05 ANAC APPROVED Page 2 code 05 REVISION 14 Copyright © by Embraer. Refer to cover page for details.
  • Page 339 CAFM-175-FAA-006 is constituted by specific Software Module part numbers and Engine Database to allow performance calculations for airplanes with the following configuration: − EMBRAER 175 airplanes Post-Mod. SB 170-57-0058 or with an equivalent factory modification (Enhanced Wing Tip). − CF34-8E5 Engines.
  • Page 340 AFM. - This version incorporates all capabilities of the previous versions. S1-05 ANAC APPROVED Page 2 code 07 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 341 SUPPLEMENT 1 AIRPLANE COMPUTERIZED AFM FLIGHT MANUAL NORMAL PROCEDURES Normal procedures presented in the basic AFM remain unchanged. EMERGENCY AND ABNORMAL PROCEDURES Emergency and abnormal procedures presented in the basic AFM remain unchanged. S1-10 CTA APPROVED code 01 Page 1 ORIGINAL...
  • Page 342 SUPPLEMENT 1 AIRPLANE COMPUTERIZED AFM FLIGHT MANUAL THIS PAGE INTENTIONALLY LEFT BLANK S1-10 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 343 SUPPLEMENT 1 AIRPLANE COMPUTERIZED AFM FLIGHT MANUAL PERFORMANCE The data obtained from the software is calculated considering the basic performance configurations presented Section Performance, and the procedures presented in Section 3 - Normal Procedures and Section 4 - Emergency and Abnormal Procedures. ENGINE DATA The CAFM calculates the engine power readings used to obtain the installed engine power on which the airplane’s certified performance is...
  • Page 344 SUPPLEMENT 1 AIRPLANE COMPUTERIZED AFM FLIGHT MANUAL INTENTIONALLY BLANK S1-15 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 345 Dead Reckoning ............S4-10 ..10 Engine Failure............... S4-10 ..11 FMS Failure ..............S4-10 ..11 Performance (Load prior to 27.1)........S4-10 ..12 S4-00 ANAC APPROVED code 01 Page 1 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 346 RNP AR instrument approach procedures. Refer to the PERFORMANCE section of this supplement for more details regarding RNP operations. S4-00 ANAC APPROVED Page 2 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 347 NOTE: The term RNP 10 must be understood as RNAV 10 as per ICAO nomenclature. S4-00 ANAC APPROVED code 01 Page 3 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 348 Supplement. S4-00 ANAC APPROVED Page 4 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 349 Supplement. S4-00 ANAC APPROVED code 01 Page 5 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 350 SUPPLEMENT 4 AIRPLANE PRIMUS EPIC - FLIGHT FLIGHT MANAGEMENT SYSTEM MANUAL INTENTIONALLY BLANK S4-00 ANAC APPROVED Page 6 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 351 4 Display units. 1 TAT sensor. 2 RVSM Compliant Air Data Systems. 1 Flight Director. EGPWS. RNP AR compliant Navigation Database. S4-05 ANAC APPROVED ode 01 Page 1 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 352 - RNP AR approach operations with Missed Approaches requiring RNP less than 1.0 are not approved. - For airplanes Pre-Mod. SB 170-31-0040 (LOAD 23.1), RNP AR 0.3 procedures with RF legs smaller than 1.25 NM radius are prohibited. - The use of VNAV requires the respective FD vertical guidance mode to be active.
  • Page 353 - FMS LNAV may command bank angles above the local regulations limits (i.e. There is no automatic protection for engine out situation). S4-05 ANAC APPROVED ode 01 Page 3 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 354 - Use of VNAV for a constant glide path approach procedures to a Decision Altitude prohibited airplanes Pre-Mod. SB 170-31-0019 (LOAD 19.3). S4-05 ANAC APPROVED Page 4 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 355 - For airplanes Pre-Mod. SB 170-31-0034 (LOAD 21.4), when using VGP, use of Temperature Compensation is prohibited. - For airplanes Post-Mod. SB 170-31-0028 (LOAD 21.2) or with an equivalent modification factory incorporated, Pre-Mod.
  • Page 356 FMS back to the correct position almost instantaneously; - If synchronous operation was in use, select “RETURN TO SELECTED CONFIG”. S4-05 ANAC APPROVED Page 6 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 357 HDG mode, accomplish the procedure above to activate the new runway and only then reengage LNAV. S4-05 ANAC APPROVED code 01 Page 7 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 358 In this case, the ACTIVE FLT PLAN will display the information correctly and the HSI pointer will be no longer reliable. S4-05 ANAC APPROVED Page 8 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 359 If RNP AR operations are intended: RNP predictive performance capability ....CHECK PFD NAV Source ............SELECT FMS For airplanes Post-Mod. SB 170-31-0028 (LOAD 21.2 and on) or with an equivalent modification factory incorporated: Speed Selector Knob..........AS REQUIRED LNAV................SELECT VNAV ................
  • Page 360 Alt Selector Knob ............SET NOTE: After an aborted takeoff, the performance must be reinitialized in order to the VNAV become available. After Takeoff: For airplanes Pre-Mod. SB 170-31-0028 (prior to LOAD 21.2): Speed Selector Knob ..........AS REQUIRED CRUISE AT TOC Thrust Rating Selection (TRS) ........
  • Page 361 FMS. The FMS maps may be used during these approach types to provide supplemental data. S4-10 ANAC APPROVED code 01 Page 3 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 362 NOTE: FMS does not correct Approach and Go Around speeds for non-standard conditions. Baro Altitude..............SET Minimums..............SET LNAV................SELECT VNAV ................SELECT S4-10 ANAC APPROVED Page 4 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 363 NOTE: FMS does not correct Approach and Go Around speeds for non-standard conditions. Preview LOC..............SELECT Baro Altitude ..............SET Minimums ..............SET S4-10 ANAC APPROVED code 01 Page 5 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 364 Speed Selector Knob ..........MAN Speed............... AS REQUIRED Localizer on PFD............VERIFY ACTIVE NAV SOURCE FGCS APPR1 Mode ..........CONFIRM ACTIVE S4-10 ANAC APPROVED Page 6 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 365 If a miscompare occurs that results in lack of ability to select independent sources, APPR2 will not be possible. S4-10 ANAC APPROVED code 01 Page 7 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 366 Approach Climb Speed. If landing speeds are not entered, GA mode will provide continued fixed pitch. S4-10 ANAC APPROVED Page 8 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 367 Hold fix. The Hold fix will then be automatically sequenced. S4-10 ANAC APPROVED code 01 Page 8A REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 368 SUPPLEMENT 4 AIRPLANE PRIMUS EPIC - FLIGHT FLIGHT MANAGEMENT SYSTEM MANUAL INTENTIONALLY BLANK S4-10 ANAC APPROVED Page 8B code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 369 Declare Missed Approach. Approach Non-RNP Remote Crosscheck FMS data with raw data from GPS, IRS. De-select error causing sensor, if detectable. S4-10 ANAC APPROVED code 01 Page 9 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 370 DR condition, using reference point fly-over techniques, to minimize the navigation error. In this case, ATC must be notified of the loss of navigation capability on the airplane. S4-10 ANAC APPROVED Page 10 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 371 RNP-0.3 or GPS required Declare Missed Approach. approach Remote Operations Contact ATC and declare loss of long range navigation capability. S4-10 ANAC APPROVED code 01 Page 11 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 372 Load 25.1.0.1 (Pre-Mod. SB 170-31-0044); 4 for airplanes equipped with Load 25.1.0.1 and on (Post-Mod. SB 170-31-0044 or with an equivalent modification factory incorporated). S4-10 ANAC APPROVED Page 12 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 373 The FMS computes an Estimate of Position Uncertainty (EPU), which is displayed with the current position determination mode on the PROGRESS page on the MCDU. S4-10 ANAC APPROVED code 01 Page 13 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 374 RNP for future flight plan legs. Refer to the Honeywell Primus Epic FMS Pilot’s Operating Manual for further details regarding system features and annunciations. S4-10 ANAC APPROVED Page 14 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 375 SUPPLEMENT 5 AIRPLANE CAT II FLIGHT OPERATION MANUAL SUPPLEMENT 5 CAT II OPERATION TABLE OF CONTENTS Block Page General ................S5-00 ..02 Cat II Engagement Logic ..........S5-00 ..02 Cat II Warnings............. S5-00 ..03 Limitations................S5-05 ..01 Minimum Equipment Required ........
  • Page 376 SUPPLEMENT 5 AIRPLANE CAT II FLIGHT OPERATION MANUAL GENERAL This supplement provides information required for CAT II operation when the appropriate equipment and instruments are approved, installed and in an operable condition. The information herein presented replaces or complements the equivalent information in the basic AFM.
  • Page 377 SUPPLEMENT 5 AIRPLANE CAT II FLIGHT OPERATION MANUAL Both Flight Directors operational. − Attitude and Heading valid on both PFD’s. − Glide slope and Localizer deviation valid on both PFD’s. − No reversions (IRS and ADC) modes selected on both PFD’s. −...
  • Page 378 SUPPLEMENT 5 AIRPLANE CAT II FLIGHT OPERATION MANUAL APR mode selected on Flight Guidance Panel. − Flaps 5. − CAT II Decision Height setting on both Display Control Panels. − On-side VOR/LOC active course valid. − Cross-side data valid. − Go-around not selected on either side.
  • Page 379 SUPPLEMENT 5 AIRPLANE CAT II FLIGHT OPERATION MANUAL On-side glide slope valid. − No back course selected. − Go-around not selected on either side. − Localizer excessive deviation: If a localizer deviation greater than approximately 1/3 dot is detected, the HSI lateral deviation bar on the PFD’s HSI will change from green to amber, the lateral deviation scale will change from white to amber, and flash.
  • Page 380 SUPPLEMENT 5 AIRPLANE CAT II FLIGHT OPERATION MANUAL INTENTIONALLY BLANK S5-00 CTA APPROVED Page 6 code 01 ORIGINAL...
  • Page 381 − 1 Autopilot System Channel must be operative. − Manual FD (Flight Director) Category II ILS approaches are prohibited. For CAT II operation with airplanes Pre-Mod. SB 170-31-0010, the following also applies: − The one engine inoperative CAT II operation is prohibited.
  • Page 382 SUPPLEMENT 5 AIRPLANE CAT II FLIGHT OPERATION MANUAL AUTOPILOT SYSTEM Minimum Use Height (MUH) ......... 50 ft NOTE: Coupled go-around height loss may be 50 ft. APPROACH AND LANDING FLAPS CAT II approach and landing must be performed with flaps 5. S5-05 ANAC APPROVED Page 2...
  • Page 383 If no visual contact is made upon reaching the decision height − or if any malfunction could not be promptly identified during approach, a missed approach must be immediately initiated. S5-10 ANAC APPROVED code 01 Page 1 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 384 MISSED APPROACH GO-AROUND Procedure ..........APPLY LANDING Reaching the Decision Height with runway in sight: Autopilot ..............DISENGAGE Landing ..............PERFORM S5-10 ANAC APPROVED Page 2 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 385 1000 1200 1400 RUNWAY HORIZONTAL DISTANCE − m THRESHOLD NOTE: The maximum demonstrated altitude loss due to autopilot malfunction is 20 ft. S5-10 ANAC APPROVED code 01 Page 3 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 386 NOTE: Consider the possibility of continuing and performing the landing if under visual conditions and the airplane position and attitude assure a safe landing. S5-10 ANAC APPROVED Page 4 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 387 NOTE: Consider the possibility of continuing and performing the landing if under visual conditions and the airplane position and attitude assure a safe landing. S5-10 ANAC APPROVED code 01 Page 5 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 388 Roll angle in excess of 25°. − Pitch angle below - 5° or above 5°. − Rate of descent in excess of 1200 ft/min. − S5-10 ANAC APPROVED Page 6 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 389 DEMONSTRATED WIND COMPONENTS Headwind ..............25 kt Tailwind................. 10 kt Crosswind ..............12 kt These demonstrated values are not considered to be limiting. S5-10 ANAC APPROVED code 01 Page 7 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 390 SUPPLEMENT 5 AIRPLANE CAT II FLIGHT OPERATION MANUAL INTENTIONALLY BLANK S5-10 ANAC APPROVED Page 8 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 391 SUPPLEMENT 6 AIRPLANE RVSM OPERATION FLIGHT MANUAL SUPPLEMENT 6 RVSM OPERATION TABLE OF CONTENTS Block Page General ................S6-00 ..02 Introduction..............S6-00 ..02 Limitations................S6-05 ..01 Minimum Equipment Required ........S6-05 ..01 Normal Procedures............S6-10 ..01 External Safety Inspection..........
  • Page 392 This Supplement is provided to present the data required for operation in the RVSM (Reduced Vertical Separation Minimum) airspace. The RVSM operation reduces the EMBRAER 170 minimum vertical separation from 2000 ft to 1000 ft between FL 290 and FL 410.
  • Page 393 EMBRAER model Pre-Mod. SB 170-34-0009, only the ADS 1 and ADS 3 are compliant with RVSM operation, the ADS 2 must not be used for RVSM operation and the airspeed is limited to Mach 0.8. - The ADS 3 is not considered RVSM compliant in case of loss of sideslip compensation, i.e., with the EICAS message ADS...
  • Page 394 SUPPLEMENT 6 AIRPLANE RVSM OPERATION FLIGHT MANUAL INTENTIONALLY BLANK S6-05 ANAC APPROVED Page 2 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 395 When altitude difference between PFD 1 and PFD 2 exceeds 180 ft, select ADS 3 on the PFD that does not agree with IESS. S6-10 ANAC APPROVED code 01 Page 1 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 396 If unable to notify ATC and obtain an ATC clearance prior to − deviating from the cleared flight level, follow any established contingency procedures and obtain ATC clearance as soon as possible. S6-10 ANAC APPROVED Page 2 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 397 SUPPLEMENT 6 AIRPLANE RVSM OPERATION FLIGHT MANUAL PERFORMANCE Performance Data presented in the basic AFM remain unchanged. S6-10 ANAC APPROVED code 01 Page 3 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 398 SUPPLEMENT 6 AIRPLANE RVSM OPERATION FLIGHT MANUAL INTENTIONALLY BLANK S6-10 ANAC APPROVED Page 4 code 01 REVISION 15 Copyright © by Embraer. Refer to cover page for details.
  • Page 399 APPENDICES AIRPLANE FLIGHT MANUAL APPENDICES TABLE OF CONTENTS CONFIGURATION DEVIATION LIST GUIDANCE INFORMATION AP-TOC CTA APPROVED code 01 Page 1 REVISION 3...
  • Page 400 APPENDICES AIRPLANE FLIGHT MANUAL THIS PAGE INTENTIONALLY LEFT BLANK AP-TOC CTA APPROVED Page 2 code 01 REVISION 2...
  • Page 401 ATA 55 Stabilizers ............. AP1-55 ..01 ATA 57 Wings..............AP1-57 ..01 ATA 71 Powerplant ............AP1-71 ..01 ATA 78 Exhaust..............AP1-78 ..01 AP1-00 ANAC APPROVED code 01 Page 1 REVISION 14 Copyright © by Embraer. Refer to cover page for details.
  • Page 402 APPENDIX 1 AIRPLANE CONFIGURATION FLIGHT DEVIATION LIST MANUAL INTENTIONALLY BLANK AP1-00 ANAC APPROVED Page 2 code 01 REVISION 14 Copyright © by Embraer. Refer to cover page for details.
  • Page 403 100 lb (45 kg). Where performance penalties are listed as no penalty, any accumulative number of items listed as no penalty may be missing without further penalty. AP1-00 ANAC APPROVED code 01 Page 3 REVISION 14 Copyright © by Embraer. Refer to cover page for details.
  • Page 404 ATA Spec. 2200. The parts within each system are identified by its functional description and, when necessary, by door or panel identification. See Maintenance Manual, Chapter 06, for panel identification. AP1-00 ANAC APPROVED Page 4 code 01 REVISION 14 Copyright © by Embraer. Refer to cover page for details.
  • Page 405 APPENDIX 1 AIRPLANE CONFIGURATION FLIGHT DEVIATION LIST MANUAL CONFIGURATION DEVIATION LIST System & 1. 2. Number installed Sequence ITEM 3. Number required for dispatch Number 4. Remarks and/or exceptions 23 COMMUNICATIONS 61-00 Static Dischargers 32 24 A maximum of 8 (eight) static dischargers may be missing with no penalty.
  • Page 406 APPENDIX 1 AIRPLANE CONFIGURATION FLIGHT DEVIATION LIST MANUAL INTENTIONALLY BLANK AP1-23 CTA APPROVED Page 2 code 01 REVISION 3...
  • Page 407 APPENDIX 1 AIRPLANE CONFIGURATION FLIGHT DEVIATION LIST MANUAL CONFIGURATION DEVIATION LIST System & 1. 2. Number installed Sequence ITEM 3. Number required for dispatch Number 4. Remarks and/or exceptions 28 FUEL 42-01 Magnetic Level Any number or combination Indicators may be missing with no penalty provided: a) There is no evidence of leakage, and...
  • Page 408 APPENDIX 1 AIRPLANE CONFIGURATION FLIGHT DEVIATION LIST MANUAL INTENTIONALLY BLANK AP1-28 ANAC APPROVED Page 2 code 01 REVISION 4...
  • Page 409 Fairing is removed or missing associated supports must also removed. - Items 32-12-01 and 32-49-01 missing simultaneously with no additional penalty. AP1-32 ANAC APPROVED code 01 Page 1 REVISION 14 Copyright © by Embraer. Refer to cover page for details.
  • Page 410 APPENDIX 1 AIRPLANE CONFIGURATION FLIGHT DEVIATION LIST MANUAL INTENTIONALLY BLANK AP1-32 ANAC APPROVED Page 2 code 01 REVISION 14 Copyright © by Embraer. Refer to cover page for details.
  • Page 411 Halogen lights type) Cavity covered with blanking plate, and Affected light is deactivated and considered inoperative. Refer to MMEL 33-44-00. AP1-33 ANAC APPROVED code 01 Page 1 REVISION 14 Copyright © by Embraer. Refer to cover page for details.
  • Page 412 One or both may be missing (Airplanes with LED with negligible penalty provided lights type) affected lights are deactivated and considered inoperative. Refer to MMEL 33-47-00. AP1-33 ANAC APPROVED Page 2 code 01 REVISION 14 Copyright © by Embraer. Refer to cover page for details.
  • Page 413 Affected DME system is deactivated and considered inoperative, and b) Cavity covered with blanking plate. Refer to MMEL 34-51-00. AP1-34 ANAC APPROVED code 01 Page 1 REVISION 14 Copyright © by Embraer. Refer to cover page for details.
  • Page 414 APPENDIX 1 AIRPLANE CONFIGURATION FLIGHT DEVIATION LIST MANUAL INTENTIONALLY BLANK AP1-34 ANAC APPROVED Page 2 code 01 REVISION 14 Copyright © by Embraer. Refer to cover page for details.
  • Page 415 Procedures are established and used to ensure that the associated galley lavatory sink is not used. Refer to MMEL 30-71-02. AP1-38 ANAC APPROVED code 01 Page 1 REVISION 14 Copyright © by Embraer. Refer to cover page for details.
  • Page 416 APPENDIX 1 AIRPLANE CONFIGURATION FLIGHT DEVIATION LIST MANUAL INTENTIONALLY BLANK AP1-38 ANAC APPROVED Page 2 code 01 REVISION 14 Copyright © by Embraer. Refer to cover page for details.
  • Page 417 APPENDIX 1 AIRPLANE CONFIGURATION FLIGHT DEVIATION LIST MANUAL CONFIGURATION DEVIATION LIST System & 1. 2. Number installed Sequence ITEM 3. Number required for dispatch Number 4. Remarks and/or exceptions 52 DOORS 2 One door deflector from each 10-01 Door Deflectors fuselage side may be missing (Passenger and with negligible penalty provided...
  • Page 418 APPENDIX 1 AIRPLANE CONFIGURATION FLIGHT DEVIATION LIST MANUAL INTENTIONALLY BLANK AP1-52 ANAC APPROVED Page 2 code 01 REVISION 4...
  • Page 419 03-05 Hydraulic System 3 May be missing with no penalty. Ground Connector, Cover the cavity with speed Hydraulic Pressure tape. Gauge Access Door (314AR) AP1-53 ANAC APPROVED code 01 Page 1 REVISION 14 Copyright © by Embraer. Refer to cover page for details.
  • Page 420 1 One may be missing with no Ground Service penalty. Cover the cavity with Access Doors speed tape. (195 BR / 195 CL) AP1-53 ANAC APPROVED Page 2 code 01 REVISION 14 Copyright © by Embraer. Refer to cover page for details.
  • Page 421 31-01 APU Oil Cooler Inlet 0 May be missing with negligible penalty provided APU is not operated in flight. AP1-53 ANAC APPROVED code 01 Page 3 REVISION 14 Copyright © by Embraer. Refer to cover page for details.
  • Page 422 APPENDIX 1 AIRPLANE CONFIGURATION FLIGHT DEVIATION LIST MANUAL INTENTIONALLY BLANK AP1-53 ANAC APPROVED Page 4 code 01 REVISION 14 Copyright © by Embraer. Refer to cover page for details.
  • Page 423 -Avoid deicing and anti- icing fluid application directly to the cavity when speed tape is not applied. AP1-55 ANAC APPROVED code 01 Page 1 REVISION 14 Copyright © by Embraer. Refer to cover page for details.
  • Page 424 12 10 One or two seals may be Aerodynamic Seal partially or totally missing in any (Lower Side) combination with negligible penalty. AP1-55 ANAC APPROVED Page 2 code 01 REVISION 14 Copyright © by Embraer. Refer to cover page for details.
  • Page 425 - Up to 25% length of all right- hand vertical stabilizer seal (aerodynamic + access panel) may be missing. AP1-55 ANAC APPROVED code 01 Page 3 REVISION 14 Copyright © by Embraer. Refer to cover page for details.
  • Page 426 - One seal may be partially or totally missing, or; - Up to 25% length of all vertical stabilizer aerodynamic seal (LH) may be missing. AP1-55 ANAC APPROVED Page 4 code 01 REVISION 14 Copyright © by Embraer. Refer to cover page for details.
  • Page 427 Drag Index of 45 is applied. 50-02 Wing Trailing Edge 0 One or both may be missing or Seals (Spar 2) partially missing with penalty. AP1-57 ANAC APPROVED code 01 Page 1 REVISION 14 Copyright © by Embraer. Refer to cover page for details.
  • Page 428 CAFM Seals) performance calculation a Drag Index of 45 is applied. NOTE: Wing-to-fuselage flap track fairing seals must be installed. AP1-57 ANAC APPROVED Page 2 code 01 REVISION 14 Copyright © by Embraer. Refer to cover page for details.
  • Page 429 (2030 kg) for flaps FULL/ice condition. NOTE: - Items 57-20-01, 57-49-01 and 57-50-01 should not be missing simultaneously with inboard nacelle strake. (Continued) AP1-71 ANAC APPROVED code 01 Page 1 REVISION 14 Copyright © by Embraer. Refer to cover page for details.
  • Page 430 Aft NOTE: Item 71-13-01 may be Core Cowl P/N missing simultaneously 15F0020-021 or with item 71-11-01 15F0021-017) without additional penalty. AP1-71 ANAC APPROVED Page 2 code 01 REVISION 14 Copyright © by Embraer. Refer to cover page for details.
  • Page 431 4. Remarks and/or exceptions 78 EXHAUST 30-01 Thrust Reverser Any number or combination Inhibit Pin Cover may be missing with negligible Plate penalty. AP1-78 ANAC APPROVED code 01 Page 1 REVISION 14 Copyright © by Embraer. Refer to cover page for details.
  • Page 432 APPENDIX 1 AIRPLANE CONFIGURATION FLIGHT DEVIATION LIST MANUAL INTENTIONALLY BLANK AP1-78 ANAC APPROVED Page 2 code 01 REVISION 14 Copyright © by Embraer. Refer to cover page for details.
  • Page 433 AIRPLANE APPENDIX 2 GUIDANCE INFORMATION FLIGHT MANUAL APPENDIX 2 GUIDANCE INFORMATION TABLE OF CONTENTS Block Page Introduction ................ AP2-00 ..02 Noise Levels - ICAO ANNEX 16 Chapter 4 ....... AP2-10 ..01 AP2-00 Page 1 code 01 REVISION 2...
  • Page 434 GUIDANCE INFORMATION FLIGHT MANUAL INTRODUCTION This appendix presents information relevant to EMBRAER 170 operation which is not required by Airworthiness Regulation. This appendix is not approved by the Authority and must be used as a guidance information. Whenever necessary, the information contained herein shall be previously approved by the local authority.
  • Page 435 EMBRAER 170 models and engine versions are listed in the tables below. All the data herein presented is based on the EMBRAER 170 airplane noise certification test data base. Compliance to ICAO Annex 16 Section 4.4 is met when: 1.
  • Page 436 APPENDIX 2 AIRPLANE GUIDANCE INFORMATION FLIGHT MANUAL INTENTIONALLY BLANK AP2-10 Page 2 code 01 REVISION 2...

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