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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 190-100 STD,
ERJ 190-100 IGW, ERJ 190-200 STD, ERJ 190-200 LR AND ERJ 190-
200 IGW.
NOTE: - THE ERJ 190-100 AND ERJ 190-200 MODELS HAVE THE
COMMERCIAL
EMBRAER 195, RESPECTIVELY.
- THE ERJ 190-100 IGW AND ERJ 190-200 IGW HAVE THE
COMMERCIAL
EMBRAER 195 AR, RESPECTIVELY.
- SOME MANUAL VERSIONS MAY NOT PRESENT ALL LISTED
MODELS. FOR SPECIFIC CONFIGURATION, REFER TO LEP
APPLICABILITY.
CTA APPROVAL:_______________________
DATE
SEPTEMBER 02, 2005
:
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 190/195
FAA
Embraer S.A.
ERJ 190-100 LR,
DESIGNATION
DESIGNATION
GERALDO CURCIO NETO – TEN CEL AV
DIVISÃO DE CERTIFICAÇÃO DE
TEMPORARY REVISION 12.5 – MARCH 31, 2016
all pages of this document.
Copyright © 2016 by Embraer S.A. All rights reserved.
ERJ 190-100 ECJ,
OF
EMBRAER 190
OF
EMBRAER 190 AR
AVIAÇÃO CIVIL
RELEASE 12.A
AND
AND
AFM–1912
CODE 031

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Summary of Contents for Embraer 190

  • Page 1 RELEASE 12.A TEMPORARY REVISION 12.5 – MARCH 31, 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 2 RELEASE 12-A REVISION 12 – APRIL 15, 2015 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 24 AIRPLANE LOG OF REVISIONS FLIGHT MANUAL ANAC APPROVED AIRPLANE FLIGHT MANUAL (AFM–1912) LOG OF REVISIONS REVISION REVISED DESCRIPTION NUMBER BLOCKS ANAC APPROVAL OF REVISION AND DATE /PAGES S-TOC Included optional page 1 Supplement 11 - codes 01 to “Radial Tires Supplement Performance”.
  • Page 25 S6-15 page performance 1 code 01 information. Corrected CG envelope in 2-05 page 2 pounds for code 54 EMBRAER 190 ECJ model. JUN 15, 12 Included new Alternate CG 2-05 pages Envelope codes 1, 2 codes related to 55, 56 EMBRAER 190 ECJ model.
  • Page 26: Description Of Revision

    51 ECJ model. Removed Quick Turn Around S1-15 page Weight penalty 1 code 51 for EMBRAER JUN 15, 12 190 ECJ model. Included EMBRAER 190 S10-05 ECJ model in pages 1, 2 code 01 Supplement 10 applicability. Included ADS-B...
  • Page 27 S3-10 page adjustment, and 7 code 01 updated S5-15 page performance 1 codes 01, information. Also S6-15 page included 1 code 01 EMBRAER 190 ECJ in the Supplement 6 applicability. 0-LOR ANAC APPROVED Page 24 code 01 REVISION 11...
  • Page 28 (MZWFW) to 2-05 page 1 Maximum Zero codes 53, Fuel Weight 54, 55, 56 (MZFW) and included SBs numbers to change EMBRAER 190 ECJ MZFW. Included Alternate CG 2-06 pages Envelopes 1, 2 codes MAR 14, 14 applicable to 11, 12 EMBRAER 195 models.
  • Page 29 DESCRIPTION NUMBER BLOCKS/ ANAC APPROVAL OF REVISION AND DATE PAGES Updated Normal Procedures for 3-09 page 3 EMBRAER 190 code 55 3-13 page 1 ECJ model with code 55 EMBRAER interior. 4-30 pages Updated Table 1, 3, 7 code of Contents and...
  • Page 30 Eastern Europe Supplement Fuels Operation. Included new CAFM version S1-05 with CAT III pages 1, 2 operation for the code 51 EMBRAER 190 ECJ. S1-15 page Updated Takeoff 1 codes 01, selection mode. 0-LOR ANAC APPROVED code 01 Page 27...
  • Page 31 MAR 14, 14 Updated S6-05 page Autoland 1 code 01 S6-10 page supplement 1 code 01 limitation. Included EMBRAER 190 S6-15 page ECJ in the 1 code 01 Supplement applicability. Included the main landing AP1-32 gear wheel page 1 code fairing in the CDL.
  • Page 32 LOG OF REVISIONS AIRPLANE FLIGHT MANUAL ANAC APPROVED AIRPLANE FLIGHT MANUAL (AFM–1912) LOG OF REVISIONS REVISION REVISED DESCRIPTION NUMBER BLOCKS/ ANAC APPROVAL OF REVISION AND DATE PAGES Updated Abbreviations 1-20 page 7 and Acronyms code 01 table. Included action related to “No Smoking”...
  • Page 33 CAFM CAT II pages 1, 2 option must be codes 01, selected to EMBRAER 195 models. Included EMBRAER S13-00 190/195 all page 2 code models in the applicability of Supplement 13. 0-LOR ANAC APPROVED Page 30 code 01 REVISION 12...
  • Page 34 LOG OF REVISIONS AIRPLANE FLIGHT MANUAL ANAC APPROVED AIRPLANE FLIGHT MANUAL (AFM–1912) LOG OF REVISIONS REVISION REVISED DESCRIPTION NUMBER BLOCKS/ ANAC APPROVAL OF REVISION AND DATE PAGES AP1-00 pages 1, 4 code 01 AP1-32 page 1 code AP1-33 page 1 code AP1-34 pages 1, 2 Included...
  • Page 35 LOG OF REVISIONS AIRPLANE FLIGHT MANUAL ANAC APPROVED AIRPLANE FLIGHT MANUAL (AFM–1912) LOG OF REVISIONS REVISION REVISED DESCRIPTION NUMBER BLOCKS/ ANAC APPROVAL OF REVISION AND DATE PAGES AP1-33 pages 1, 2 code 01 AP1-34 Included LED page 1 code light lens and miscellaneous AP1-55 items in the...
  • Page 36 3 code 01 extension from SEP 25, 15 S14-10 page 1 code 01 -40°C to -45°C to ERJ 190-200. 0-LOR ANAC APPROVED code 01 Page 33 TEMPORARY REVISION 12.3 Copyright © by Embraer. Refer to cover page for details.
  • Page 37 S-TOC page Supplement – 2 codes 01 EFVS to 08, 10 to (Enhanced 14, 16, 17, Flight Vision Supplement System) Operation. 0-LOR ANAC APPROVED Page 34 code 01 TEMPORARY REVISION 12.5 Copyright © by Embraer. Refer to cover page for details.
  • Page 38: Airplane Flight Manual

    May 30/07 Oct 04/07 Revision 2 Supplements 1, 4 and 5 Sections 2, 3, 4, 5 and Oct 22/07 Apr 10/08 Revision 3 Supplement 1 code 01 Page 1 REVISION 12 Copyright © by Embraer. Refer to cover page for details.
  • Page 39 Supplements 1 and 7 Section 1 and Supplements 1 Sep 28/09 Apr 08/10 Revision 6 and 2 Section 2 Nov 06/09 Apr 08/10 Revision 6 Page 2 code 01 REVISION 12 Copyright © by Embraer. Refer to cover page for details.
  • Page 40 3, 5, 6, 9 and 13 10.2 Appendix 1 Nov 25/13 Mar 14/14 Revision 11 10.3 Supplement 2 Dec 06/13 Mar 14/14 Revision 11 code 01 Page 3 REVISION 12 Copyright © by Embraer. Refer to cover page for details.
  • Page 41 Jun 19/15 12.2 Section 4 Sep 08/15 12.3 Supplement 14 Sep 25/15 Supplements 1 12.4 Dec 01/15 and 15 12.5 Supplement 1 Mar 31/16 Page 4 code 01 TEMPORARY REVISION 12.5 Copyright © by Embraer. Refer to cover page for details.
  • Page 42 Sections 1 and 3, 11.2 and Supplement Oct 10/14 Apr 15/15 Revision 12 Supplements 1, 11.3 Nov 20/14 Apr 15/15 Revision 12 5 and 6 Page 4 code 01 REVISION 12 Copyright © by Embraer. Refer to cover page for details.
  • Page 43 TEMP. REVISION ....12.2....SEP 08, 2015 TEMP. REVISION ....12.3....SEP 25, 2015 TEMP. REVISION ....12.4....DEC 01, 2015 TEMP. REVISION ....12.5....MAR 31, 2016 TR-LEP code 031 Page 1 TEMPORARY REVISION 12.5 Copyright © by Embraer. Refer to cover page for details.
  • Page 44: Intentionally Blank

    TR LIST OF AIRPLANE EFFECTIVE PAGES FLIGHT MANUAL INTENTIONALLY BLANK TR-LEP Page 2 code 031 TEMPORARY REVISION 12.5 Copyright © by Embraer. Refer to cover page for details.
  • Page 45 Takeoff and Landing up to -45°C S14-10 TR12.3 Takeoff and Landing up to -45°C * Asterisk indicates pages revised, added or deleted by the current revision. TR-LEP code 031 Page 3 TEMPORARY REVISION 12.5 Copyright © by Embraer. Refer to cover page for details.
  • Page 46 TR LIST OF AIRPLANE EFFECTIVE PAGES FLIGHT MANUAL INTENTIONALLY BLANK TR-LEP Page 4 code 031 TEMPORARY REVISION 12.5 Copyright © by Embraer. Refer to cover page for details.
  • Page 47: List Of Effective Pages

    REVISION....10 ....JUN 03, 2013 REVISION....11 ....MAR 14, 2014 REVISION....12 ....APR 15, 2015 RELEASE ....12-A ....OCT 08, 2015 0-LEP code 031 Page 1 RELEASE 12-A Copyright © by Embraer. Refer to cover page for details.
  • Page 48 LIST OF AIRPLANE EFFECTIVE PAGES FLIGHT MANUAL INTENTIONALLY BLANK 0-LEP Page 2 code 031 RELEASE 12-A Copyright © by Embraer. Refer to cover page for details.
  • Page 49 REVISION 12 0-LOR REVISION 12 0-LOR REVISION 12 REVISION 12 CC 01 * Asterisk indicates pages revised, added or deleted by the current revision. 0-LEP code 031 Page 3 RELEASE 12-A Copyright © by Embraer. Refer to cover page for details.
  • Page 50 REVISION 12 1-20 REVISION 12 1-20 REVISION 12 1-20 REVISION 12 * Asterisk indicates pages revised, added or deleted by the current revision. 0-LEP Page 4 code 031 RELEASE 12-A Copyright © by Embraer. Refer to cover page for details.
  • Page 51 2-40 REVISION 2 2-48 ORIGINAL ALL with 8000 ft Cabin Altitude * Asterisk indicates pages revised, added or deleted by the current revision. 0-LEP code 031 Page 5 RELEASE 12-A Copyright © by Embraer. Refer to cover page for details.
  • Page 52 ORIGINAL ALL except ECJ with Embraer 3-17 ORIGINAL Interior 3-19 ORIGINAL * Asterisk indicates pages revised, added or deleted by the current revision. 0-LEP Page 6 code 031 RELEASE 12-A Copyright © by Embraer. Refer to cover page for details.
  • Page 53 4-01 REVISION 2 ALL, except ECJ 4-01 REVISION 3 4-01 ORIGINAL * Asterisk indicates pages revised, added or deleted by the current revision. 0-LEP code 031 Page 7 RELEASE 12-A Copyright © by Embraer. Refer to cover page for details.
  • Page 54 REVISION 2 4-02 ORIGINAL 4-02 ORIGINAL 4-02 ORIGINAL 4-02 ORIGINAL 4-04 ORIGINAL * Asterisk indicates pages revised, added or deleted by the current revision. 0-LEP Page 8 code 031 RELEASE 12-A Copyright © by Embraer. Refer to cover page for details.
  • Page 55 4-12 ORIGINAL 4-12 ORIGINAL 4-12 REVISION 3 4-12 ORIGINAL 4-12 ORIGINAL * Asterisk indicates pages revised, added or deleted by the current revision. 0-LEP code 031 Page 9 RELEASE 12-A Copyright © by Embraer. Refer to cover page for details.
  • Page 56 ORIGINAL 4-20 REVISION 3 ALL, except ECJ 4-20 ORIGINAL 4-20 ORIGINAL * Asterisk indicates pages revised, added or deleted by the current revision. 0-LEP Page 10 code 031 RELEASE 12-A Copyright © by Embraer. Refer to cover page for details.
  • Page 57 REVISION 11 4-30 ORIGINAL 5-00 ORIGINAL 5-00 REVISION 2 5-01 ORIGINAL * Asterisk indicates pages revised, added or deleted by the current revision. 0-LEP code 031 Page 11 RELEASE 12-A Copyright © by Embraer. Refer to cover page for details.
  • Page 58 ORIGINAL 5-10 ORIGINAL 5-10 ORIGINAL 5-10 ORIGINAL 5-10 ORIGINAL 5-10 ORIGINAL * Asterisk indicates pages revised, added or deleted by the current revision. 0-LEP Page 12 code 031 RELEASE 12-A Copyright © by Embraer. Refer to cover page for details.
  • Page 59 Primus Epic FMS S2-10 REVISION 6 S2-10 REVISION 6 S2-10 REVISION 6 * Asterisk indicates pages revised, added or deleted by the current revision. 0-LEP code 031 Page 13 RELEASE 12-A Copyright © by Embraer. Refer to cover page for details.
  • Page 60 REVISION 8 Radial Tires Performance S11-00 REVISION 8 190/195 except ECJ * Asterisk indicates pages revised, added or deleted by the current revision. 0-LEP Page 14 code 031 RELEASE 12-A Copyright © by Embraer. Refer to cover page for details.
  • Page 61 REVISION 12 AP1-00 REVISION 12 AP1-00 REVISION 12 AP1-00 REVISION 12 * Asterisk indicates pages revised, added or deleted by the current revision. 0-LEP code 031 Page 15 RELEASE 12-A Copyright © by Embraer. Refer to cover page for details.
  • Page 62 REVISION 1 AP1-71 REVISION 1 AP1-78 REVISION 12 AP1-78 REVISION 12 * Asterisk indicates pages revised, added or deleted by the current revision. 0-LEP Page 16 code 031 RELEASE 12-A Copyright © by Embraer. Refer to cover page for details.
  • Page 63 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 ORIGINAL...
  • Page 64 AIRPLANE TABLE OF CONTENTS FLIGHT MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 0-TOC CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 65 GENERAL AIRPLANE FLIGHT MANUAL 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 CTA APPROVED code 01 Page 1 ORIGINAL...
  • Page 66 55 12 3927-2477 E-MAIL: opereng@embraer.com.br 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 67: Temporary Revisions

    GENERAL AIRPLANE FLIGHT MANUAL TEMPORARY REVISIONS Temporary revisions may be issued when the need arises. The temporary revision will be clearly identified and will be replaced as soon as possible. Temporary revisions will not be included in the List of Effective Pages. LIST OF EFFECTIVE PAGES A List of Effective Pages for all the sections is located at the beginning of this Manual.
  • Page 68 GENERAL AIRPLANE FLIGHT MANUAL SECTION 3 - NORMAL PROCEDURES This Section contains the required normal procedures. 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...
  • Page 69: Definition Of Terms

    AIRPLANE GENERAL FLIGHT MANUAL DEFINITION OF TERMS The following definitions apply to the terms below: WARNING: OPERATING PROCEDURES, TECHNIQUES OTHER RELATED INFORMATION WHICH RESULT IN PERSONAL INJURY OR LOSS OF LIFE, IF NOT FOLLOWED. CAUTION: OPERATING PROCEDURES, TECHNIQUES OTHER RELATED INFORMATION WHICH MAY RESULT IN DAMAGE OR DESTRUCTION OF EQUIPMENT, IF NOT FOLLOWED.
  • Page 70 AIRPLANE GENERAL FLIGHT MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 1-10 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 71 Automatic Direction Finder Air Data System All Engines Operating Automatic Dependant Surveillance ADS-B Broadcast Above Field Elevation Airplane Flight Manual Above Ground Level 1-20 ANAC APPROVED code 01 Page 1 REVISION 12 Copyright © by Embraer. Refer to cover page for details.
  • Page 72 Category II Operation Circuit Breaker Cursor Control Device Course Deviation Indicator Center of Gravity Configuration, Maintenance and Procedures COMM Communication Continuous 1-20 ANAC APPROVED Page 2 code 01 REVISION 12 Copyright © by Embraer. Refer to cover page for details.
  • Page 73 Engine Indication and Crew Alerting EICAS System EMG or EMERG Emergency Engine Essential ETOPS Extended Operations Federal Aviation Administration FADEC Full Authority Digital Electronic Control 1-20 ANAC APPROVED code 01 Page 3 REVISION 12 Copyright © by Embraer. Refer to cover page for details.
  • Page 74 Heading High Frequency High Initial Approach Fix IESS Integrated Electronic Standby System Instrument Flight Rules Instrument Landing System Inertial Reference System 1-20 ANAC APPROVED Page 4 code 01 REVISION 12 Copyright © by Embraer. Refer to cover page for details.
  • Page 75 Mean Aerodynamic Chord Manual Modular Acquisition Unit Maximum MCDU Multi-Function Control Display Unit Minimum Enroute Altitude Multifunction Display Minimum Microwave Landing System 1-20 ANAC APPROVED code 01 Page 5 REVISION 12 Copyright © by Embraer. Refer to cover page for details.
  • Page 76 One Engine Inoperative OVHT Overheat Passenger Atmospheric Pressure at Airport Elevation Radio Altimeter, Resolution Advisory RAIM GPS Receiver Integrity Monitoring Ram Air Turbine 1-20 ANAC APPROVED Page 6 code 01 REVISION 12 Copyright © by Embraer. Refer to cover page for details.
  • Page 77 Traffic and Collision Avoidance System TDZE Touchdown Zone Elevation Thrust Lever Angle Takeoff Takeoff Distance Top of Descent TODA Takeoff Distance Available 1-20 ANAC APPROVED code 01 Page 7 REVISION 12 Copyright © by Embraer. Refer to cover page for details.
  • Page 78 Lift Off Speed Maximum Brake Energy Speed Minimum Control Speed in the Air Minimum Control Speed on Ground Minimum Control Speed During Landing 1-20 ANAC APPROVED Page 8 code 01 REVISION 12 Copyright © by Embraer. Refer to cover page for details.
  • Page 79 Maximum Operating Speed Minimum Unstick Speed VNAV Vertical Navigation Mode VHF Omnidirectional Range Rotation Speed Maximum Turbulent Air Penetration Speed Landing Reference Speed 1-20 ANAC APPROVED code 01 Page 9 REVISION 12 Copyright © by Embraer. Refer to cover page for details.
  • Page 80: Intentionally Blank

    GENERAL AIRPLANE FLIGHT MANUAL INTENTIONALLY BLANK 1-20 ANAC APPROVED Page 10 code 01 REVISION 12 Copyright © by Embraer. Refer to cover page for details.
  • Page 81: Table Of Contents

    AIRPLANE LIMITATIONS 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..........2-05..02 Operational Limitations ............2-10..01 Systems: Electronic Display ............2-20..01 Warning ................
  • Page 82: Introduction

    AIRPLANE LIMITATIONS 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 83: Airplane Flight Manual

    (MTOW) (MLW) (MZFW) (kg) (kg) (kg) (kg) EMBRAER 195 AR 52450 52290 45800 42600 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 84 LIMITATIONS AIRPLANE FLIGHT MANUAL DELETED 2-05 ANAC APPROVED Page 2 code 20 REVISION 11...
  • Page 85: Center Of Gravity Envelope

    FLIGHT MANUAL CENTER OF GRAVITY ENVELOPE EMBRAER 195 STANDARD, LR AND AR 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 86 LIMITATIONS AIRPLANE FLIGHT MANUAL INTENTIONALLY BLANK 2-06 ANAC APPROVED Page 2 code 04 REVISION 11...
  • Page 87 CENTER OF GRAVITY ENVELOPE (ALTERNATE 1 – CENTER OF GRAVITY – 17%) EMBRAER 195 STANDARD, LR AND AR 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 88 LIMITATIONS AIRPLANE EMBRAER 190 ECJ FLIGHT MANUAL INTENTIONALLY BLANK 2-06 ANAC APPROVED Page 2 code 12 REVISION 11...
  • Page 89: Operational Limitations

    LIMITATIONS AIRPLANE FLIGHT MANUAL OPERATIONAL LIMITATIONS OPERATIONAL ENVELOPE 55000 REGION − TAKEOFF , LANDING & GROUND START 50000 45000 −65°C −21.5°C 41000 ft 40000 35000 30000 25000 ISA + 35°C 20000 15000 10000 ft 10000 5000 −1000 ft −54°C −40°C 52°C −5000 −80 −70 −60 −50 −40 −30 −20 −10 0...
  • Page 90: Minimum Control Speeds

    LIMITATIONS AIRPLANE FLIGHT MANUAL MAXIMUM ALTITUDE FOR FLAP EXTENTED Maximum Altitude For Flap Extended......20000 ft AIRSPEEDS LANDING GEAR OPERATION/EXTENDED SPEED (V LO AND V LE ) V LO for retraction............235 KIAS V LO for extension ............265 KIAS V LE ................
  • Page 91: Maximum Operating Speed

    LIMITATIONS AIRPLANE FLIGHT MANUAL MAXIMUM OPERATING SPEED 45000 40000 = 0.82 35000 30000 25000 20000 15000 10000 5000 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).
  • Page 92 LIMITATIONS AIRPLANE FLIGHT MANUAL EMBRAER 195 MANEUVERING SPEED (V A ) 45000 40000 =0.82 35000 30000 25000 20000 15000 10000 5000 AIRSPEED - KIAS NOTE: Maneuvers that involve angle of attack near the stall or full application of rudder, elevator, and aileron controls should be confined to speeds below V .
  • Page 93: Kinds Of Operation

    AIRPLANE LIMITATIONS FLIGHT MANUAL MAXIMUM FLAP EXTENDED SPEED (V FE ) Flaps 1 ................230 KIAS Flaps 2 ................215 KIAS Flaps 3 ................200 KIAS Flaps 4 ................180 KIAS Flaps 5 ................180 KIAS Flaps Full ..............165 KIAS MAXIMUM TIRE GROUND SPEED Maximum Tire Ground Speed ........
  • Page 94 AIRPLANE LIMITATIONS FLIGHT MANUAL MANEUVERING FLIGHT LOAD FACTORS These corresponding accelerations limit the bank angle during turns and limit the pull-up maneuvers. FLAPS DOWN (1, 2, 3, 4, 5 AND LOAD FACTOR LIMIT FLAPS UP FULL) Positive 2.5 g 2.00 g Negative - 1.00 g RUNWAY...
  • Page 95: Electronic Display

    ELECTRONIC CHECKLIST Operational approval is required in order to load database into the airplane and use the electronic checklist. For airplanes Pre-Mod. SB 190-31-0009 or with an equivalent modification factory incorporated, the use of the Electronic Checklist is prohibited. 2-20...
  • Page 96 LIMITATIONS AIRPLANE FLIGHT MANUAL INTENTIONALLY BLANK 2-20 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 97: Warning

    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 System. The use of predictive EGPWS functions should be manually inhibited when landing at an airport that is not in the airport database to avoid unwanted alerts.
  • Page 98 AIRPLANE LIMITATIONS FLIGHT MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 2-30 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 99: Fuel

    LIMITATIONS AIRPLANE FLIGHT MANUAL FUEL EMBRAER 190/195 AIRPLANE MODEL STD/LR/AR 8076.3 l Maximum usable quantity per tank (6550 kg) 56.7 l Unusable quantity per tank (46 kg) NOTE: Maximum fuel capacity is 16266 l (13192 kg). Maximum permitted imbalance between tanks .... 360 kg NOTE: The weights above have been determined for an adopted fuel density of 0.811 kg/l.
  • Page 100 LIMITATIONS AIRPLANE FLIGHT MANUAL INTENTIONALLY BLANK 2-36 ANAC APPROVED Page 2 code 02 REVISION 3...
  • Page 101: Apu

    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 1032°C...
  • Page 102 LIMITATIONS AIRPLANE FLIGHT MANUAL INTENTIONALLY BLANK 2-38 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 103: Power Plant

    LIMITATIONS AIRPLANE FLIGHT MANUAL POWER PLANT ENGINES Two General Electric CF34-10E6A1. OPERATIONAL LIMITS PARAMETER 100% 59.3% 100% ITT: Ground Start 740° C Inflight Start 875° C Normal and Maximum Takeoff 983° C (1) (2) and Go Around Maximum Continuous 960° C OIL PRESSURE 25 psi (3) OIL TEMPERATURE:...
  • Page 104 LIMITATIONS AIRPLANE FLIGHT MANUAL STARTER LIMITS DRY MOTORING DUTY CYCLE LIMITS: Motoring Number Maximum Time Cool-Down Time 90 Seconds 5 Minutes 2 through to 5 (1) 30 Seconds 5 Minutes NOTE: 1) After five sequential motorings, cycle may be repeated following a 15-minute cool-down period.
  • Page 105 THRUST REVERSER (APPLICABLE ONLY TO AIRPLANES PRE- MOD. SB 190-73-0010) 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.
  • Page 106 LIMITATIONS AIRPLANE FLIGHT MANUAL INTENTIONALLY BLANK 2-40 ANAC APPROVED Page 4 code 02 REVISION 1...
  • Page 107 LIMITATIONS AIRPLANE FLIGHT MANUAL POWER PLANT ENGINES General Electric CF34-10E7 General Electric CF34-10E7-B. OPERATIONAL LIMITS PARAMETER 100% 100% ITT: Ground Start 740° C Inflight Start 875° C Normal Takeoff and Go Around 943° C (1) (3) 983° C (1) (2) Maximum Takeoff and Go Around Maximum Continuous 960°...
  • Page 108 LIMITATIONS AIRPLANE FLIGHT MANUAL STARTER LIMITS DRY MOTORING DUTY CYCLE LIMITS: Motoring Number Maximum Time Cool-Down Time 90 Seconds 5 Minutes 2 through to 5 (1) 30 Seconds 5 Minutes NOTE: After five sequential motorings, cycle may be repeated following a 15-minute cool-down period. STARTING DUTY CYCLE LIMITS: Motoring Number Maximum Time...
  • Page 109 LIMITATIONS AIRPLANE FLIGHT MANUAL ENGINE THRUST Operation at reduced takeoff thrust based on the assumed temperature higher than the actual ambient temperature as calculated by CAFM is permissible if the airplane meets all applicable performance requirements at the planned takeoff weight and reduced thrust setting.
  • Page 110 LIMITATIONS AIRPLANE FLIGHT MANUAL INTENTIONALLY BLANK 2-40 ANAC APPROVED Page 4 code 09 REVISION 2...
  • Page 111: Pneumatic, Air Conditioning And Pressurization

    AIRPLANE LIMITATIONS FLIGHT MANUAL PNEUMATIC, CONDITIONING PRESSURIZATION PRESSURIZATION Maximum differential pressure Up to 37000 ft ............7.80 psi Above 37000 ft............8.34 psi Maximum differential overpressure ......8.77 psi Maximum differential negative pressure....... - 0.5 psi Maximum differential pressure for Takeoff and Landing ..............
  • Page 112 AIRPLANE LIMITATIONS FLIGHT MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 2-48 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 113: Ice And Rain Protection

    AIRPLANE LIMITATIONS FLIGHT MANUAL ICE AND RAIN PROTECTION OPERATION IN ICING CONDITIONS There is no temperature limitation for anti-icing system automatic operation. On ground: - The TO DATASET MENU on the MCDU must be set to ENG when SAT is between 5°C and 10°C with visible moisture. - The TO DATASET MENU on the MCDU must be set to ALL when SAT is below 5°C with visible moisture In flight:...
  • Page 114 AIRPLANE LIMITATIONS FLIGHT MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 2-50 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 115: Autopilot

    - For airplanes Post-Mod. SB 190-34-0026 (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 116 AIRPLANE LIMITATIONS FLIGHT MANUAL (Continued from the previous page) MAGNETIC CUT-OUT LATITUDE LONGITUDE REGIONS Between 60°S and Between 120°E and 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 117: Ozone Concentration

    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 118 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 119 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 291 270 298 270...
  • Page 120 AIRPLANE LIMITATIONS FLIGHT MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 2-58 CTA APPROVED Page 4 code 01 ORIGINAL...
  • Page 121 NORMAL AIRPLANE PROCEDURES FLIGHT MANUAL SECTION 3 NORMAL PROCEDURES TABLE OF CONTENTS Block Page Introduction ................ 3-00..03 Internal Safety Inspection ..........3-03..01 Power Up ................3-05..01 External Inspection ............3-07..01 Before Start................ 3-09..01 Engine Start ............... 3-11..01 Abnormal Engine Start Indications .......
  • Page 122 NORMAL AIRPLANE PROCEDURES FLIGHT MANUAL Transponder...............3-40 ..01 Operation in Icing Conditions ..........3-41 ..01 Turbulent Air Penetration ...........3-45 ..01 3-00 ANAC APPROVED Page 2 code 01 REVISION 1...
  • Page 123: Introduction

    The normal procedures contained in this manual have been developed and recommended by the manufacturer and approved by the certification authorities for use during the operation of the EMBRAER 190 and EMBRAER 195. Indented explanations (lines beginning further from the margin than the others) may follow a main item regarded as not being self-explanatory or lacking further details.
  • Page 124: Intentionally Blank

    NORMAL AIRPLANE PROCEDURES FLIGHT MANUAL INTENTIONALLY BLANK 3-00 CTA APPROVED Page 4 code 01 ORIGINAL...
  • Page 125: Internal Safety Inspection

    RAT Command ............STOWED Slat/Flap Lever............VERIFY POSITION Circuit Breakers ............CHECK Photoluminescent Escape Path Marking System (Passenger Cabin) (if installed) ......CHARGED 3-03 ANAC APPROVED code 01 Page 1 REVISION 12 Copyright © by Embraer. Refer to cover page for details.
  • Page 126 NORMAL AIRPLANE PROCEDURES FLIGHT MANUAL INTENTIONALLY BLANK 3-03 ANAC APPROVED Page 2 code 01 REVISION 12 Copyright © by Embraer. Refer to cover page for details.
  • Page 127: Power Up

    NORMAL AIRPLANE PROCEDURES FLIGHT MANUAL POWER UP Battery 1 ..............ON Battery 2 ..............AUTO CAUTION: VERIFY THAT ONLY DISPLAYS 2 AND 3 ARE AVAILABLE. IF MORE THAN DISPLAYS 2 AND 3 ARE AVAILABLE, AIRPLANE MUST DISPATCHED. Batteries Voltage ............. CHECK CAUTION: EACH BATTERY VOLTAGE MUST BE AT LEAST 22.5 VOLTS.
  • Page 128 NORMAL AIRPLANE PROCEDURES FLIGHT MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 3-05 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 129: External Inspection

    AIRPLANE NORMAL 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 130 AIRPLANE NORMAL PROCEDURES FLIGHT MANUAL Oxygen Discharge Indicator........GREEN DISC Pressure Relief Valves..........CHECK 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 ...........
  • Page 131: Before Start

    NORMAL AIRPLANE PROCEDURES FLIGHT MANUAL BEFORE START Airplane Manuals & Documents ......ON BOARD Jump Seat Oxy Masks & Regulators....... CHECK Electrical Panel ............SET Cockpit Lights Panel..........AS REQUIRED Push the annunciators test button and verify all associated lights. Engine 1 Fire Handle..........
  • Page 132 NORMAL AIRPLANE PROCEDURES FLIGHT MANUAL Oxygen Masks & Regulators ........CHECK/100% Check masks for supply of oxygen and for microphone − functionality. The MFD Status page must be checked and the available − oxygen supply and pressure must be adequate for use. Glareshield Lights Control Panel ......
  • Page 133 AIRPLANE NORMAL PROCEDURES FLIGHT MANUAL Speedbrake Lever............ CLOSED Thrust Levers ............IDLE Gnd Prox Flap Ovrd ..........CHECK Audio Control Panel ..........AS REQUIRED Trims ................ CHECK/SET Flight Controls Disconnect Handles ......CHECK Alternate Gear Extension Compartment .......... CHECK MCDU ..............SET Insert route in the FMS according to the flight plan.
  • Page 134 AIRPLANE NORMAL PROCEDURES FLIGHT MANUAL − Select the LANDING page on the MCDU and set the landing speeds for the takeoff weight. Speed Selector Knob..........SET TOGA Button............PRESS Doors and Windows ..........CLOSED Pitch Trim ..............SET Takeoff Briefing ............COMPLETED Red Beacon..............ON Hydraulic Pump Sys 3A..........ON Ground Equipment ...........AS REQUIRED Emergency/Parking Brake........AS REQUIRED Steering Disengage Switch ........PRESS...
  • Page 135: Engine Start

    - For airplanes Post-Mod. SB 190-73-0016 or equipped with Engine FADEC 5.50 or later versions, two additional engine starts are allowed in case of automatic abort due to engine hot start.
  • Page 136 NORMAL AIRPLANE PROCEDURES FLIGHT MANUAL INTENTIONALLY BLANK 3-11 ANAC APPROVED Page 2 code 01 REVISION 12 Copyright © by Embraer. Refer to cover page for details.
  • Page 137: After Start

    NORMAL AIRPLANE PROCEDURES FLIGHT MANUAL AFTER START APU................AS REQUIRED Ground Equipment ..........REMOVED Autobrake (if applicable).......... RTO N1 Target..............CHECK Slat/Flap..............SET_ Flight Controls............CHECK NOTE: - The flight controls check must be performed with the flight controls synoptic page displayed. - Flight control full travel indication on the flight controls synoptic page is not required when full control deflection is reached.
  • Page 138 NORMAL AIRPLANE PROCEDURES FLIGHT MANUAL INTENTIONALLY BLANK 3-13 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 139: Before Takeoff

    AIRPLANE NORMAL FLIGHT PROCEDURES MANUAL BEFORE TAKEOFF Take Off Configuration ..........CHECK Brake Temperature..........CHECK NOTE: Brake temperature indication must be in the green range for takeoff. EICAS ..............CHECK Check: − No Warning and Caution EICAS messages displayed. − Thrust Rate Mode (TO-1, TO-2 or TO-3).
  • Page 140 AIRPLANE NORMAL PROCEDURES FLIGHT MANUAL INTENTIONALLY BLANK 3-15 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 141: Takeoff

    11° 11° 9° 12° - For airplanes Post-Mod. SB 190-31-0009 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 142 11° 11° 9° 11° - For airplanes Post-Mod. SB 190-31-0009 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 143: After Takeoff

    AIRPLANE NORMAL PROCEDURES FLIGHT MANUAL AFTER TAKEOFF Air Conditioning & Press .......... CHECK APU................AS REQUIRED Slat/Flap..............UP Select slat/flap to up following the ideal slat/flap selection speed reference (flap retraction speed bug). Altimeters ..............SET & X-CHECK 3-17 CTA APPROVED Page 1 code 01 ORIGINAL...
  • Page 144 AIRPLANE NORMAL PROCEDURES FLIGHT MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 3-17 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 145: Descent

    NORMAL AIRPLANE PROCEDURES FLIGHT MANUAL DESCENT Approach Briefing ............ COMPLETE Landing Data ............SET Select the PERFORMANCE LANDING page on the MCDU and set and V 3-19 CTA APPROVED code 01 Page 1 ORIGINAL...
  • Page 146 NORMAL AIRPLANE PROCEDURES FLIGHT MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 3-19 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 147: Approach

    NORMAL AIRPLANE PROCEDURES FLIGHT MANUAL 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 1...
  • Page 148 NORMAL AIRPLANE PROCEDURES FLIGHT MANUAL INTENTIONALLY BLANK 3-21 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 149: Before Landing

    AIRPLANE NORMAL PROCEDURES FLIGHT MANUAL BEFORE LANDING Landing Gear ............DOWN Slat/Flap..............SET_ Lights ............... AS REQUIRED 3-23 CTA APPROVED Page 1 code 01 ORIGINAL...
  • Page 150 AIRPLANE NORMAL PROCEDURES FLIGHT MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 3-23 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 151: Go-Around

    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. Select flaps according to the table below: Landing Slat/Flap Go Around Slat/Flap...
  • Page 152 AIRPLANE NORMAL PROCEDURES FLIGHT MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 3-25 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 153: After Landing

    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 at maximum reverse thrust until the airplane comes to a complete stop.
  • Page 154 AIRPLANE NORMAL PROCEDURES FLIGHT MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 3-27 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 155: Shutdown

    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 1...
  • Page 156 NORMAL AIRPLANE PROCEDURES FLIGHT MANUAL INTENTIONALLY BLANK 3-29 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 157: Leaving The Airplane

    AIRPLANE NORMAL PROCEDURES FLIGHT MANUAL LEAVING THE AIRPLANE Passenger Signs Panel..........OFF Set the Emergency Lights and all switches to OFF. Electrical ..............OFF GPU/APU Batteries 1 & 2 ............OFF 3-31 CTA APPROVED Page 1 code 01 ORIGINAL...
  • Page 158 AIRPLANE NORMAL PROCEDURES FLIGHT MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 3-31 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 159: Buffet Onset Envelope

    AIRPLANE NORMAL PROCEDURES FLIGHT MANUAL BUFFET ONSET ENVELOPE The Buffet Onset data are provided by the CAFM presented in the Supplement 1. 3-33 CTA APPROVED Page 1 code 01 ORIGINAL...
  • Page 160 AIRPLANE NORMAL PROCEDURES FLIGHT MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 3-33 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 161: Enhanced/Ground Proximity Warning

    AIRPLANE NORMAL 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. IF A TERRAIN AWARENESS WARNING OCCURS, WARNING: IMMEDIATELY INITIATE AND CONTINUE A CLIMB...
  • Page 162 AIRPLANE NORMAL PROCEDURES FLIGHT MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 3-35 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 163: Windshear Prevention/Recovery

    AIRPLANE NORMAL 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 164 AIRPLANE NORMAL PROCEDURES FLIGHT MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 3-37 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 165: Traffic And Collision Avoidance

    AIRPLANE NORMAL 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. Maneuvers that are in the opposite direction of the Resolution Advisory (RA) are extremely hazardous, especially RAs involving altitude crossing, and thus are prohibited unless it is visually determined to be...
  • Page 166 AIRPLANE NORMAL PROCEDURES FLIGHT MANUAL WARNING: IF HIGH SPEED BUFFET IS ENCO UNTERED WHEN INITIALLY RESPONDING TO AN RA, RELAX PITCH FORCE AS NECESSARY TO REDUCE BUFFET, BUT STILL CONTINUE TO MANEUVER. NOTE: - The consequences of not following an RA may result in additional RA's in which aural alert and visual annunciations may not agree with each other.
  • Page 167 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 standby mode, re-select the desired mode (i.e., the transponder should be in the active mode).
  • Page 168 NORMAL AIRPLANE PROCEDURES FLIGHT MANUAL INTENTIONALLY BLANK 3-40 ANAC APPROVED Page 2 code 01 REVISION 1...
  • Page 169 AIRPLANE NORMAL PROCEDURES FLIGHT MANUAL OPERATION IN ICING CONDITIONS The procedures below complement or change the remaining procedures presented in this Section. For emergency and abnormal procedures related to operation in icing conditions, refer to Section 4. NOTE: - Icing conditions may exist whenever the Static Air Temperature (SAT) on the ground or for takeoff, or Total Air Temperature (TAT) inflight, is 10°C or below and visible moisture in any form is present (such as clouds, fog with...
  • Page 170 AIRPLANE NORMAL PROCEDURES FLIGHT MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 3-41 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 171: Turbulent Air Penetration

    NORMAL AIRPLANE 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 172 NORMAL AIRPLANE PROCEDURES FLIGHT MANUAL MAXIMUM RECOMMENDED TURBULENT AIR PENETRATION SPEED 3-45 ANAC APPROVED Page 2 code 01 REVISION 4...
  • Page 173 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 ..13 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 174 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 175 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 176 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 177 OR SEPARATION ..............4-01 ..06 FORCED LANDING............4-01 ..06 FUEL LEAK.................4-01 ..07 JAMMED CONTROL COLUMN (PITCH) (EMBRAER 190 MODELS)..........4-01 ..08 JAMMED CONTROL COLUMN (PITCH) (EMBRAER 195 MODELS)..........4-01 ..09 JAMMED CONTROL WHEEL (ROLL) (EMBRAER 190 MODELS)..........4-01 ..10 JAMMED CONTROL WHEEL (ROLL) (EMBRAER 195 MODELS)..........4-01 ..
  • Page 178 LOSS OF HYDRAULIC SYSTEM 2 ........4-01..22 LOSS OF HYDRAULIC SYSTEM 3 ........4-01..22 LOSS OF HYDRAULIC SYSTEM 1 AND 2 (EMBRAER 190 MODELS)..........4-01..23 LOSS OF HYDRAULIC SYSTEM 1 AND 2 (EMBRAER 195 MODELS)..........4-01..24 LOSS OF HYDRAULIC SYSTEM 1 AND 3 (EMBRAER 190 MODELS)..........
  • Page 179: Cargo Compartment Fire

    EMERGENCY AIRPLANE PROCEDURES FLIGHT MANUAL CARGO COMPARTMENT FIRE LAND AT THE NEAREST SUITABLE AIRPORT. Push the associated cargo fire-extinguishing button. After CRG AFT (FWD) FIREX HI ARM message is displayed and the associated cargo fire-extinguishing button is illuminated, push again the associated cargo fire-extinguishing button.
  • Page 180: Dual Engine Failure

    3 and set + 20 KIAS. REF FULL CAUTION: FOR THE EMBRAER 190, MULTIPLY THE FULL FLAPS UNFACTORED LANDING DISTANCE BY 1.35. FOR THE EMBRAER 195, MULTIPLY THE FULL FLAPS UNFACTORED LANDING DISTANCE BY 2.30.
  • Page 181: Emergency Descent

    EMERGENCY AIRPLANE PROCEDURES FLIGHT MANUAL EMERGENCY DESCENT φFasten Belts Signs ............ON φAltitude ................ 10000 ft or MEA WHICHEVER IS HIGHER φThrust Levers .............. IDLE φSpeedBrake Lever ............FULL OPEN φAirspeed..............MAX/ APPROPRIATE φTransponder..............7700 φATC................NOTIFY EMERGENCY EVACUATION φEmergency/Parking Brake .......... ON φSlat/Flap Lever ............
  • Page 182: Engine Fire, Severe Damage Or Separation

    EMERGENCY AIRPLANE PROCEDURES FLIGHT MANUAL ENGINE FIRE, SEVERE DAMAGE OR SEPARATION φAutothrottle ..............DISENGAGE φThrust Lever (affected engine) ........IDLE φStart/Stop Selector (affected engine) ......STOP φFire Extinguishing Handle (affected engine) ....PULL LAND AT THE NEAREST SUITABLE AIRPORT. Rotate the fire-extinguishing handle (to left or right). Wait 30 seconds.
  • Page 183: Fuel Leak

    EMERGENCY AIRPLANE PROCEDURES FLIGHT MANUAL FUEL LEAK LAND AT THE NEAREST SUITABLE AIRPORT. NOTE: An unexpected difference between the total fuel quantity indicated on EICAS and the total fuel quantity indicated on the FMS Fuel Management page may indicate a fuel leak condition.
  • Page 184: Jammed Control Column (Pitch) (Embraer 190 Models)

    PROCEDURES FLIGHT MANUAL JAMMED CONTROL COLUMN (PITCH) (EMBRAER 190 MODELS) φElevator Disconnection Handle ........PULL Identify the unrestricted control column. If the failure occurs above 175 KIAS, the current airspeed is the maximum speed for the remainder of the flight.
  • Page 185: Jammed Control Column (Pitch) (Embraer 195 Models)

    AIRPLANE PROCEDURES FLIGHT MANUAL JAMMED CONTROL COLUMN (PITCH) (EMBRAER 195 MODELS) φElevator Disconnection Handle........PULL Identify the unrestricted control column. If the failure occurs above 175 KIAS, the current airspeed is the maximum speed for the remainder of the flight.
  • Page 186: Jammed Control Wheel (Roll) (Embraer 190 Models)

    PROCEDURES FLIGHT MANUAL JAMMED CONTROL WHEEL (ROLL) (EMBRAER 190 MODELS) φAileron Disconnection Handle ........PULL Identify the unrestricted control column. If the failure occurs above 175 KIAS, the current airspeed is the maximum speed for the remainder of the flight.
  • Page 187: Jammed Control Wheel (Roll) (Embraer 195 Models)

    AIRPLANE PROCEDURES FLIGHT MANUAL JAMMED CONTROL WHEEL (ROLL) (EMBRAER 195 MODELS) φAileron Disconnection Handle........PULL Identify the unrestricted control column. If the failure occurs above 175 KIAS, the current airspeed is the maximum speed for the remainder of the flight.
  • Page 188 EMERGENCY AIRPLANE PROCEDURES FLIGHT MANUAL JAMMED RUDDER PEDALS If the failure occurs above 175 KIAS, the current airspeed is the maximum speed for the remainder of the flight. If the failure occurs below 175 KIAS, the maximum speed for the remainder of the flight is 175 KIAS.
  • Page 189 EMERGENCY AIRPLANE PROCEDURES FLIGHT MANUAL PITCH TRIM RUNAWAY φA/P Disc Button............PRESS AND HOLD φPitch Trim Systems 1 and 2 Cutout Button .............. PUSH IN Release the A/P Disc button. WARNING: DO NOT OPEN THE SPEEDBRAKE. Push the pitch trim system 1 cutout button out and actuate the pitch trim switch.
  • Page 190: (Embraer 190 Models)

    PITCH ANGLE 11° 11° 9° 12° - For airplanes Post-Mod. SB 190-31-0009 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 191 PITCH ANGLE 11° 11° 9° 11° - For airplanes Post-Mod. SB 190-31-0009 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 192: Abnormal Landing Gear Extension

    ABNORMAL AIRPLANE PROCEDURES FLIGHT MANUAL ABNORMAL LANDING GEAR EXTENSION Move landing gear lever to down and select the electrical override switch to gear down. If landing gear indications are not confirmed down, pull the alternate gear extension lever. Check landing gear indications. If landing gear indications are still not confirmed down, accomplish the Partial or Gear Up Landing Procedure.
  • Page 193: Engine Airstart

    ABNORMAL AIRPLANE PROCEDURES FLIGHT MANUAL ENGINE AIRSTART Disengage the autothrottle and check the airstart envelope. If an engine assisted airstart is considered, set the operative engine N2 to 80% minimum, set the inoperative engine ignition to override and the start/stop selector to start, then run. If the engine was restarted, set the ignition to auto after engine stabilizes at idle.
  • Page 194: Engine Airstart Envelope

    ABNORMAL AIRPLANE PROCEDURES FLIGHT MANUAL ENGINE AIRSTART ENVELOPE 30000 REGION 1 − REQUIRED MAXIMUM ITT FOR START IS 90°C. REGION 2 − REQUIRED MINIMUM ITT FOR START IS 50°C. 25000 21000 20000 17500 15000 ASSISTED OR WINDMILLING START 10000 8000 ASSISTED START ONLY 5000...
  • Page 195: Engine Itt Overtemperature

    If a go around is required, press the downlock override button and move the landing gear lever up. 4-01 ANAC APPROVED Page 19 code 01 TEMPORARY REVISION 12.2 Copyright © by Embraer. Refer to cover page for details.
  • Page 196 ABNORMAL AIRPLANE PROCEDURES FLIGHT MANUAL ENGINE ITT OVERTEMPERATURE The ITT pointer and digits will be flashing in red. Disengage the autothrottle and reduce the affected engine thrust lever in order to keep ITT within limits. ENGINE SHUTDOWN LAND AT THE NEAREST SUITABLE AIRPORT. Disengage the autothrottle.
  • Page 197: Impaired Or Cracked Windshield

    ABNORMAL AIRPLANE PROCEDURES FLIGHT MANUAL IMPAIRED OR CRACKED WINDSHIELD Turn off the affected windshield heating and close the cockpit door. If only the outer layer is cracked, continue the flight. NOTE: There is a windshield heating wire between the middle and outer layers that can be used as a reference to determine which layer is cracked.
  • Page 198: Loss Of Hydraulic System 2

    Plan a long final approach. For landing configuration, set slat/flap to full and set V REF FULL CAUTION: FOR THE EMBRAER 190, MULTIPLY THE FULL FLAPS UNFACTORED LANDING DISTANCE BY 1.76. FOR THE EMBRAER 195, MULTIPLY THE FULL FLAPS UNFACTORED LANDING DISTANCE BY 1.82.
  • Page 199: Loss Of Hydraulic System 3

    For landing configuration, set the landing gear lever to down, pull the alternate gear extension lever, set slat/flap to full and set V REF FULL CAUTION: FOR THE EMBRAER 190, MULTIPLY THE FULL FLAPS UNFACTORED LANDING DISTANCE BY 1.66. FOR THE EMBRAER 195, MULTIPLY THE FULL FLAPS UNFACTORED LANDING DISTANCE BY 1.74.
  • Page 200: Loss Of Hydraulic System 1 And 2

    AIRPLANE PROCEDURES FLIGHT MANUAL LOSS OF HYDRAULIC SYSTEM 1 AND 2 (EMBRAER 190 MODELS) LAND AT THE NEAREST SUITABLE AIRPORT. NOTE: - Expect lower roll and pitch rates. - Do not accomplish the Elevator Fault and the Spoiler Fault Procedures.
  • Page 201: Loss Of Hydraulic System 1 And 2

    AIRPLANE PROCEDURES FLIGHT MANUAL LOSS OF HYDRAULIC SYSTEM 1 AND 2 (EMBRAER 195 MODELS) LAND AT THE NEAREST SUITABLE AIRPORT. NOTE: - Expect lower roll and pitch rates. - Do not accomplish the Elevator Fault and the Spoiler Fault Procedures.
  • Page 202: Loss Of Hydraulic System 1 And 3

    PROCEDURES FLIGHT MANUAL LOSS OF HYDRAULIC SYSTEM 1 AND 3 (EMBRAER 190 MODELS) LAND AT THE NEAREST SUITABLE AIRPORT. NOTE: - Expect lower roll rates and lower speedbrake efficiency. - Do not accomplish the Spoiler Fault Procedure. Relevant Inoperative Items: −...
  • Page 203: Loss Of Hydraulic System 1 And 3

    PROCEDURES FLIGHT MANUAL LOSS OF HYDRAULIC SYSTEM 1 AND 3 (EMBRAER 195 MODELS) LAND AT THE NEAREST SUITABLE AIRPORT. NOTE: - Expect lower roll rates and lower speedbrake efficiency. - Do not accomplish the Spoiler Fault Procedure. Relevant Inoperative Items: −...
  • Page 204: Loss Of Hydraulic System 2 And 3

    PROCEDURES FLIGHT MANUAL LOSS OF HYDRAULIC SYSTEM 2 AND 3 (EMBRAER 190 MODELS) LAND AT THE NEAREST SUITABLE AIRPORT. NOTE: - Expect lower roll and pitch rates and lower speedbrake efficiency. - Do not accomplish the Elevator Fault and the Spoiler Fault Procedures.
  • Page 205: Loss Of Hydraulic System 2 And 3

    PROCEDURES FLIGHT MANUAL LOSS OF HYDRAULIC SYSTEM 2 AND 3 (EMBRAER 195 MODELS) LAND AT THE NEAREST SUITABLE AIRPORT. NOTE: - Expect lower roll and pitch rates and lower speedbrake efficiency. - Do not accomplish the Elevator Fault and the Spoiler Fault Procedures.
  • Page 206: Loss Of Pressurization Indication

    ABNORMAL AIRPLANE PROCEDURES FLIGHT MANUAL LOSS OF PRESSURIZATION INDICATION Use the remaining indications to maintain cabin altitude below 10000 ft, according to the table below: AIRPLANE CABIN DIFFERENTIAL ALTITUDE (ft) ALTITUDE (ft) PRESSURE (PSID) 10000 11000 1000 12000 1200 13000 1300 14000 1500...
  • Page 207: One Engine Inoperative Approach And Landing

    For landing configuration, set landing gear down, set slat/flap to 5 and set V + 20 KIAS. REF FULL CAUTION: FOR THE EMBRAER 190, MULTIPLY THE FULL FLAPS UNFACTORED LANDING DISTANCE BY 1.37. FOR THE EMBRAER 195, MULTIPLY THE FULL FLAPS UNFACTORED LANDING DISTANCE BY 1.50.
  • Page 208: Structural Damage

    ABNORMAL AIRPLANE PROCEDURES FLIGHT MANUAL STRUCTURAL DAMAGE LAND AT THE NEAREST SUITABLE AIRPORT. Limit the airspeed to 200 KIAS maximum. If the fuselage is damaged, limit altitude to 10000 ft or MEA (whichever is higher) and press the pressurization dump button when reaching 10000 ft.
  • Page 209: Intentionally Blank

    ABNORMAL AIRPLANE PROCEDURES FLIGHT MANUAL INTENTIONALLY BLANK 4-01 ANAC APPROVED Page 32 code 01 REVISION 2...
  • Page 210 AIRPLANE EMERGENCY & FLIGHT ABNORMAL PROCEDURES MANUAL AIRPLANE GENERAL (DOORS/LIGHTING/CARGO COMPARTMENT) TABLE OF CONTENTS Block Page WARNING DOOR CARGO FORWARD (AFT) OPEN......4-02 ..03 DOOR EMERGENCY RH (LH) OPEN ......4-02 ..03 DOOR PASSENGER (SERVICE) FORWARD (AFT) OPEN..........4-02 ..03 CAUTION DOOR FORWARD (CENTER) ELECTRONIC BAY OPENED ........
  • Page 211: Airplane Flight Manual

    AIRPLANE EMERGENCY & FLIGHT ABNORMAL PROCEDURES MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 4-02 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 212 AIRPLANE EMERGENCY FLIGHT PROCEDURES 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 213 AIRPLANE ABNORMAL FLIGHT PROCEDURES MANUAL DOOR FORWARD (CENTER) ELECTRONI C BAY OPENED 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 214 AIRPLANE EMERGENCY & ABNORMAL FLIGHT PROCEDURES MANUAL AMS (PNEUMATICS/AIR CONDITIONING/PRESSURIZATION) TABLE OF CONTENTS Block Page WARNING CABIN ALTITUDE HIGH ............4-04 ..03 CAUTION AMS CONTROLLER FAILURE ..........4-04 ..04 BLEED APU LEAKAGE ............4-04 ..04 BLEED 1 (2) FAILURE............4-04 ..04 BLEED 1 (2) LEAKAGE ............4-04 ..04 BLEED 1 (2) OVERPRESSURE.........4-04 ..05 CABIN DIFFERENTIAL PRESSURE FAILURE ....4-04 ..05 CARGO FORWARD VENTILATION FAILURE....4-04 ..05...
  • Page 215 AIRPLANE EMERGENCY & ABNORMAL FLIGHT PROCEDURES MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 4-04 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 216 EMERGENCY AIRPLANE PROCEDURES FLIGHT MANUAL CABIN ALTITUDE HIGH φCrew Oxygen Masks........... DON, 100% φCrew Communication ..........ESTABLISH φAltitude ................ 10000 FT or MEA, WHICHEVER IS HIGHER φThrust Levers .............. IDLE φSpeed Brake ............... FULL OPEN φAirspeed..............MAX/ APPROPRIATE φTransponder..............7700 φATC ................
  • Page 217 ABNORMAL AIRPLANE PROCEDURES FLIGHT MANUAL AMS CONTROLLER FAILURE Exit and avoid icing conditions and limit the altitude to 10000 ft or MEA (whichever is higher) maximum. At 10000 ft, push the pressurization dump button in. NOTE: - Assisted crossbleed start is not available. - Pneumatic assisted engine start is not available.
  • Page 218: Bleed 1 (2) Overpressure

    AIRPLANE ABNORMAL PROCEDURES FLIGHT MANUAL BLEED 1 (2) OVERPRESSURE Push the affected bleed button out then in. If the Bleed 1 (2) OVERPRESSURE message persists push the affected bleed button and the crossbleed button out. For Bleed 1 Overpressure, push also the APU bleed button out. Exit and avoid icing conditions.
  • Page 219: Pack 1 (2) Failure

    AIRPLANE ABNORMAL PROCEDURES FLIGHT MANUAL PACK 1 (2) FAILURE Set the associated cabin temperature controllers to 12 o’clock position and turn the affected pack off. Wait 1 minute and turn the affected pack on. If the PACK 1 (2) FAIL message extinguishes, wait 1 minute and operate the associated temperature controller normally.
  • Page 220: Bleed 1 (2) Off

    AIRPLANE ABNORMAL PROCEDURES FLIGHT MANUAL BLEED 1 (2) OFF Limit the altitude to 31000 ft maximum. PACK 1 (2) OFF Limit the altitude to 31000 ft maximum. 4-04 CTA APPROVED Page 7 code 01 ORIGINAL...
  • Page 221 AIRPLANE ABNORMAL PROCEDURES FLIGHT MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 4-04 CTA APPROVED Page 8 code 01 ORIGINAL...
  • Page 222 EMERGENCY & AIRPLANE ABNORMAL FLIGHT PROCEDURES MANUAL AUTOFLIGHT TABLE OF CONTENTS Block Page CAUTION AUTOPILOT FAILURE ............4-06..03 AUTOPILOT PITCH MISTRIM .......... 4-06..03 AUTOPILOT PITCH TRIM FAILURE ........ 4-06..03 AUTOPILOT ROLL MISTRIM..........4-06..03 AUTOTHROTTLE FAILURE ..........4-06..03 AUTOTHROTTLE NOT IN HOLD ........
  • Page 223 EMERGENCY & AIRPLANE ABNORMAL FLIGHT PROCEDURES MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 4-06 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 224 ABNORMAL AIRPLANE PROCEDURES FLIGHT MANUAL AUTOPILOT FAILURE Fly the airplane manually. AUTOPILOT PITCH MISTRIM Hold the control wheel firmly, disengage the autopilot and trim the airplane. The autopilot may be available for reengagement. AUTOPILOT PITCH TRIM FAILURE Hold the control wheel firmly, disengage the autopilot and trim the airplane.
  • Page 225 For landing configuration, set slat/flap to 5 or set slat/flap to full. For landing with slat/flap 5, set V + 15 KIAS. REF FULL CAUTION: FOR THE EMBRAER 190, MULTIPLY THE FULL FLAPS UNFACTORED LANDING DISTANCE BY 1.29. FOR THE EMBRAER 195, MULTIPLY THE FULL FLAPS UNFACTORED LANDING DISTANCE BY 1.38.
  • Page 226 AIRPLANE EMERGENCY & ABNORMAL FLIGHT PROCEDURES MANUAL AUXILIARY POWER UNIT TABLE OF CONTENTS Block Page CAUTION APU ALTITUDE EXCEEDANCE ........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 227: Intentionally Blank

    EMERGENCY & AIRPLANE ABNORMAL FLIGHT PROCEDURES MANUAL INTENTIONALLY BLANK 4-08 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 228 AIRPLANE ABNORMAL 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 229 ABNORMAL AIRPLANE PROCEDURES FLIGHT MANUAL INTENTIONALLY BLANK 4-08 CTA APPROVED Page 4 code 01 ORIGINAL...
  • Page 230 EMERGENCY & AIRPLANE ABNORMAL FLIGHT PROCEDURES MANUAL ELECTRICAL TABLE OF CONTENTS Block Page WARNING BATTERY DISCHARGING..........4-10..03 BATTERY 1 (2) OVERTEMPERATURE ......4-10..03 BATTERY 1-2 OFF............4-10..03 ELECTRICAL EMERGENCY..........4-10..04 CAUTION AC BUS 1 OFF ..............4-10..06 AC BUS 2 OFF ..............
  • Page 231 EMERGENCY & AIRPLANE ABNORMAL FLIGHT PROCEDURES MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 4-10 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 232: Battery Discharging

    EMERGENCY AIRPLANE PROCEDURES FLIGHT MANUAL BATTERY DISCHARGING LAND AT THE NEAREST SUITABLE AIRPORT. BATTERY 1 (2) OVERTEMPERATURE φAssociated Battery ............OFF NOTE: Do not start the APU. BATTERY 1-2 OFF LAND AT THE NEAREST SUITABLE AIRPORT. NOTE: APU start is not available. 4-10 CTA APPROVED code 01...
  • Page 233: Electrical Emergency

    3 and set + 20 KIAS. REF FULL CAUTION: FOR THE EMBRAER 190, MULTIPLY THE FULL FLAPS UNFACTORED LANDING DISTANCE BY 1.35. FOR THE EMBRAER 195, MULTIPLY THE FULL FLAPS UNFACTORED LANDING DISTANCE BY 2.30.
  • Page 234 3 and maintain + 20 or 130 KIAS (whichever is higher). REF FULL CAUTION: FOR THE EMBRAER 190, MULTIPLY THE FULL FLAPS UNFACTORED LANDING DISTANCE BY 2.21. FOR THE EMBRAER 195, MULTIPLY THE FULL FLAPS UNFACTORED LANDING DISTANCE BY 2.30.
  • Page 235: Ac Bus 1 Off

    ABNORMAL AIRPLANE PROCEDURES FLIGHT MANUAL AC BUS 1 OFF Relevant Inoperative Items: − Fuel AC Pump 1. − Hydraulic System 2 Electrical Pump. − Windshield Wiper 2. − Windshield Heater 2. − Ice Detector 1. − Pitch Trim Indication. NOTE: - The slats will operate at low rate. - Fuel Crossfeed Low 2 is not available.
  • Page 236: Ac Standby Bus Off

    ABNORMAL AIRPLANE PROCEDURES FLIGHT MANUAL AC STANDBY BUS OFF Monitor electrical system. Relevant Inoperative Items: − Ignition 1A − Ignition 2A NOTE: Engine Start with batteries only is not available. APU GENERATOR OFF BUS Turn the APU generator off, then on. If the APU GEN OFF message persists, turn the APU generator off.
  • Page 237: Dc Bus 1 Off

    For landing configuration, arm the emergency lights, set slat/flap to full and V REF FULL CAUTION: FOR THE EMBRAER 190, MULTIPLY THE FULL FLAPS UNFACTORED LANDING DISTANCE BY 1.07. FOR THE EMBRAER 195, MULTIPLY THE FULL FLAPS UNFACTORED LANDING DISTANCE BY 1.17.
  • Page 238: Dc Essential Bus 1 Off

    For landing configuration, set slat/flap to full and V REF FULL On ground, use differential braking and rudder to steer the airplane. CAUTION: FOR EMBRAER 190, MULTIPLY THE FULL FLAPS UNFACTORED LANDING DISTANCE BY 1.10. FOR EMBRAER 195, MULTIPLY THE FULL FLAPS UNFACTORED LANDING DISTANCE BY 1.22.
  • Page 239: Dc Essential Bus 2 Off

    • WHEN THE EMERGENCY/PARKING BRAKE LIGHT IS ON, MAINTAIN STEADY PRESSURE SINCE THE ANTI- SKID PROTECTION IS NOT AVAILABLE. • FOR THE EMBRAER 190, MULTIPLY THE FULL FLAPS UNFACTORED LANDING DISTANCE BY 1.58. FOR THE EMBRAER 195, MULTIPLY THE FULL FLAPS UNFACTORED LANDING DISTANCE BY 1.65.
  • Page 240: Dc Essential Bus 3 Off

    • WHEN THE EMERGENCY/PARKING BRAKE LIGHT IS ON, MAINTAIN STEADY PRESSURE SINCE THE ANTI- SKID PROTECTION IS NOT AVAILABLE. • FOR THE EMBRAER 190, MULTIPLY THE FULL FLAPS UNFACTORED LANDING DISTANCE BY 1.66. FOR THE EMBRAER 195, MULTIPLY THE FULL FLAPS UNFACTORED LANDING DISTANCE BY 1.72.
  • Page 241: Gpu Connected

    ABNORMAL AIRPLANE PROCEDURES FLIGHT MANUAL GPU CONNECTED Disconnect GPU before starting taxi. IDG 1 (2) OFF BUS Select the affected IDG to off and then to auto. If the IDG 1 (2) OFF message persists, select the affected IDG to off and use APU as required.
  • Page 242 AIRPLANE EMERGENCY & ABNORMAL FLIGHT PROCEDURES MANUAL ENGINE TABLE OF CONTENTS Block Page WARNING ENGINE 1 (2) REVERSER DEPLOYED ......4-12..03 ENGINE 1 (2) OIL LOW PRESSURE........ 4-12..03 CAUTION ENGINE 1 (2) CONTROL FAULT ........4-12..04 ENGINE 1 (2) FADEC OVERTEMPERATURE ....4-12..04 ENGINE 1 (2) FAILURE ............
  • Page 243: Cta Approved

    AIRPLANE EMERGENCY & ABNORMAL FLIGHT PROCEDURES MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 4-12 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 244: Airplane Flight Manual

    AIRPLANE EMERGENCY PROCEDURES FLIGHT MANUAL ENGINE 1 (2) REVERSER DEPLOYED LAND AT THE NEAREST SUITABLE AIRPORT. Disengage the autothrottle and set the affected thrust lever to idle. If any buffeting is noticed, set the start stop selector (affected engine) to stop, start the APU and balance the fuel. When appropriate, accomplish the One Engine Inoperative Approach and Landing Procedure.
  • Page 245: Engine 1 (2) Control Fault

    AIRPLANE ABNORMAL PROCEDURES FLIGHT MANUAL ENGINE 1 (2) CONTROL FAULT Disengage the autothrottle. CAUTION: AVOID QUICK THRUST LEVER MOVEMENT, HIGH ENGINE THRUST OPERATION THRUST REVERSER. If it is not possible to control engine thrust for the affected engine, accomplish the Engine Shutdown Procedure. ENGINE 1 (2) FADEC OVERTEMPERATURE If the respective engine parameters are abnormal, accomplish the Engine Shutdown Procedure.
  • Page 246: Engine 1 (2) Fuel Impending Bypass

    ABNORMAL AIRPLANE PROCEDURES FLIGHT MANUAL ENGINE 1 (2) FUEL IMPENDING BYPASS If both ENG 1 FUEL IMP BYPASS and ENG 2 FUEL IMP BYPASS messages are displayed, LAND AT THE NEAREST SUITABLE AIRPORT. ENGINE 1 (2) FUEL LOW PRESSURE Verify the fuel crossfeed is off. Disengage the autothrottle and monitor the affected engine parameters.
  • Page 247: Engine 1 (2) Starter Valve Opened

    ABNORMAL AIRPLANE PROCEDURES FLIGHT MANUAL ENGINE 1 (2) STARTER VALVE OPENED Turn the crossbleed and the associated bleed off. If the airplane is on ground and engine 1 is the affected engine, turn off APU bleed, reduce the engine 1 thrust lever to idle and set the engine 1 start/stop selector to stop.
  • Page 248: Engine Reference Ecs Disagree

    AIRPLANE ABNORMAL PROCEDURES FLIGHT MANUAL ENGINE REFERENCE ECS DISAGREE Configure the aircraft according to takeoff data or reenter the takeoff data according to aircraft configuration. NOTE: The EICAS message ENG REF ECS DISAG will be always displayed when the following conditions apply simultaneously: the REF ECS is set to ON, the APU is running and the engine thrust levers are set to idle.
  • Page 249 AIRPLANE ABNORMAL PROCEDURES FLIGHT MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 4-12 CTA APPROVED Page 8 code 01 ORIGINAL...
  • Page 250: Fire Protection

    AIRPLANE EMERGENCY & FLIGHT ABNORMAL PROCEDURES MANUAL FIRE PROTECTION TABLE OF CONTENTS Block Page WARNING APU FIRE ................4-14..03 ENGINE 1 (2) FIRE ............4-14..03 CAUTION APU FIRE DETECTION FAILURE ........4-14..04 APU FIRE-EXTINGUISHING FAILURE ......4-14..04 CARGO AFT (FORWARD) FIRE SYSTEM FAILURE ..
  • Page 251 AIRPLANE EMERGENCY & FLIGHT ABNORMAL PROCEDURES MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 4-14 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 252 AIRPLANE EMERGENCY PROCEDURES FLIGHT MANUAL APU FIRE φAPU Emergency Stop Button ........PUSH IN Turn the APU OFF. If the APU FIRE message persists, push the APU fire-extinguishing button. ENGINE 1 (2) FIRE φAutothrottle..............DISENGAGE φThrust Lever (affected engine)........IDLE φStart/Stop Selector (affected engine) ......
  • Page 253 ABNORMAL AIRPLANE PROCEDURES FLIGHT MANUAL APU FIRE DETECTION FAILURE Turn the APU OFF. APU FIRE-EXTINGUISHING FAILURE Turn the APU OFF. CARGO AFTER (FORWARD) FIRE SYSTEM FAILURE If aft (forward) cargo compartment is not empty, LAND AT THE NEAREST SUITABLE AIRPORT. ENGINE 1 (2) FIRE DETECTION FAILURE If fire is suspected in the affected engine, accomplish the Engine Fire, Severe Damage or Separation Procedure.
  • Page 254 ELEVATOR THRUST COMPENSATOR FAILURE ..4-16..05 ELEVATOR FAULT ............4-16..05 ELEVATOR LH (RH) FAILURE ......... 4-16..05 FLAP (SLAT) FAILURE (EMBRAER 190 MODELS) ..4-16..06 FLAP (SLAT) FAILURE (EMBRAER 195 MODELS) ..4-16..08 FLIGHT CONTROL BIT EXPIRED........4-16..09 FLIGHT CONTROL NO DISPATCH .........
  • Page 255 AIRPLANE EMERGENCY & ABNORMAL FLIGHT PROCEDURES MANUAL ADVISORY AILERON RH (LH) FAILURE (EMBRAER 190 MODELS) ..........4-16 ..14 AILERON RH (LH) FAILURE (EMBRAER 195 MODELS) ..........4-16 ..14 FLIGHT CONTROL FAULT ..........4-16 ..14 4-16 ANAC APPROVED Page 2 code 01 REVISION 7...
  • Page 256: Elevator Normal Mode Failure

    Close the speed brake. For landing configuration, set slat/flap to full and set V REF FULL CAUTION: FOR THE EMBRAER 190, MULTIPLY THE FULL FLAPS UNFACTORED LANDING DISTANCE BY 1.10. FOR THE EMBRAER 195, MULTIPLY THE FULL FLAPS UNFACTORED LANDING DISTANCE BY 1.22.
  • Page 257: Spoiler Normal Mode Failure

    Speed brake. For landing configuration, set slat/flap to full and set V REF FULL CAUTION: FOR THE EMBRAER 190, MULTIPLY THE FULL FLAPS UNFACTORED LANDING DISTANCE BY 1.30. FOR THE EMBRAER 195, MULTIPLY THE FULL FLAPS UNFACTORED LANDING DISTANCE BY 1.50.
  • Page 258: Angle Of Attack Limit Failure

    Auto Configuration Trim. Elevator Thrust Compensation. ELEVATOR LH (RH) FAILURE (EMBRAER 190 MODELS) If the failure occurs above 175 KIAS, the current airspeed is the maximum speed for the remainder of the flight. If the failure occurs below 175 KIAS, the maximum speed for the remainder of the flight is 175 KIAS.
  • Page 259: Flap (Slat) Failure (Embraer 190 Models)

    REF FULL until the acceleration altitude is reached. FLAP (SLAT) FAILURE (EMBRAER 190 MODELS) Cycle the slat/flap lever (up to three cycles may be attempted). If the FLAP (SLAT) FAIL message persists, use the position indicated on the EICAS as a reference to select landing data presented on the tables below.
  • Page 260 AIRPLANE ABNORMAL FLIGHT PROCEDURES MANUAL (Continued from the previous page) FLAP/SLAT FAIL LANDING TABLE SLAT FULL FLAP + 60 + 50 + 50 REF FULL REF FULL REF FULL (KIAS) Ldg Coef 1.90 1.77 1.81 + 35 + 35 + 35 REF FULL REF FULL REF FULL...
  • Page 261: Flap (Slat) Failure (Embraer 195 Models)

    FLIGHT MANUAL FLAP (SLAT) FAILURE (EMBRAER 195 MODELS) Cycle the slat/flap lever (up to three cycles may be attempted). If the FLAP (SLAT) FAIL message persists, use the position indicated on the EICAS as a reference to select landing data presented on the tables below.
  • Page 262 AIRPLANE ABNORMAL FLIGHT PROCEDURES MANUAL (Continued from the previous page) FLAP/SLAT FAIL LANDING TABLE WITH SHAKER ANTICIPATED SLAT FULL FLAP + 60 + 60 + 60 REF FULL REF FULL REF FULL (KIAS) Ldg Coef 1.80 1.82 1.85 + 40 + 40 + 40 REF FULL...
  • Page 263: Pitch Trim Failure (Embraer 190 Models)

    FLIGHT MANUAL PITCH TRIM FAILURE (EMBRAER 190 MODELS) If the failure occurs above 175 KIAS, the current airspeed is the maximum speed for the remainder of the flight. If the failure occurs below 175 KIAS, the maximum speed for the remainder of the flight is 175 KIAS.
  • Page 264: Pitch Trim Failure (Embraer 195 Models)

    PROCEDURES MANUAL PITCH TRIM FAILURE (EMBRAER 195 MODELS) If the failure occurs above 175 KIAS, the current airspeed is the maximum speed for the remainder of the flight. If the failure occurs below 175 KIAS, the maximum speed for the remainder of the flight is 175 KIAS.
  • Page 265: Rudder Fault

    AIRPLANE ABNORMAL PROCEDURES FLIGHT MANUAL (Continued from the previous page) If a go around is required, proceed as a normal go around limiting the airspeed to 175 KIAS. NOTE: As asymmetric thrust may be required to help controlling the airplane, maximum thrust on both engines may not be possible.
  • Page 266: Spoiler Fault

    + 15 KIAS. REF FULL CAUTION: FOR THE EMBRAER 190, MULTIPLY THE FULL FLAPS UNFACTORED LANDING DISTANCE BY 1.63. FOR THE EMBRAER 195, MULTIPLY THE FULL FLAPS UNFACTORED LANDING DISTANCE BY 1.86. If all spoiler panels are closed, set slat/flap to full and set V...
  • Page 267 ABNORMAL PROCEDURES FLIGHT MANUAL AILERON RH (LH) FAILURE (EMBRAER 190 MODELS) On ground, do not takeoff. Inflight: Avoid abrupt and large aileron inputs and limit bank angle to 25°. Establish landing configuration early. For landing configuration, set slat/flap 5 and maintain V + 10 KIAS.
  • Page 268 EMERGENCY & AIRPLANE ABNORMAL FLIGHT PROCEDURES MANUAL FMS/NAV/COM & FLIGHT INSTRUMENTS TABLE OF CONTENTS Block Page WARNING NO TAKEOFF CONFIGURATION ........4-18..03 CAUTION ADS 1 (2) FAILURE ............4-18..04 ADS 3 FAILURE ..............4-18..04 ADS 1 (2) (3) HEATER FAILURE........4-18..04 ADS 4 HEATER FAILURE..........
  • Page 269 IRS EXCESSIVE MOTION ..........4-18 ..10 IRS 1 (2) FAILURE.............4-18 ..10 MCDU 1 (2) OVERHEAT (PRE-MOD. SB 190-31-0007) ........4-18 ..10 MFD 1 (2) FAULT...............4-18 ..10 MFD 1 (2) OVERHEAT ............4-18 ..11 NAVCOM 1 (2) FAILURE...........4-18 ..11 NAVCOM 1 (2) OVERHEAT ..........4-18 ..
  • Page 270: No Takeoff Configuration

    EMERGENCY AIRPLANE PROCEDURES FLIGHT MANUAL NO TAKEOFF CONFIGURATION Configure the airplane for takeoff. 4-18 CTA APPROVED code 01 Page 3 ORIGINAL...
  • Page 271: Ads 1 (2) Failure

    ABNORMAL AIRPLANE PROCEDURES FLIGHT MANUAL ADS 1 (2) FAILURE Confirm the affected ADS automatic reversion. If necessary, revert the affected ADS. ADS 3 FAILURE If necessary, revert ADS 3. ADS 1 (2) (3) HEATER FAILURE Revert the affected ADS. ADS 4 HEATER FAILURE Disregard IESS altitude and airspeed indication.
  • Page 272: Avionics Mau 1A Failure

    • WHEN THE EMERGENCY/PARKING BRAKE LIGHT IS ON, MAINTAIN STEADY PRESSURE SINCE THE ANTI- SKID PROTECTION IS NOT AVAILABLE. • FOR THE EMBRAER 190, MULTIPLY THE FULL FLAPS UNFACTORED LANDING DISTANCE BY 1.58. FOR THE EMBRAER 195, MULTIPLY THE FULL FLAPS UNFACTORED LANDING DISTANCE BY 1.65.
  • Page 273: Avionics Mau 2A Failure

    • WHEN THE EMERGENCY/PARKING BRAKE LIGHT IS ON, MAINTAIN STEADY PRESSURE SINCE THE ANTI- SKID PROTECTION IS NOT AVAILABLE. • FOR THE EMBRAER 190, MULTIPLY THE FULL FLAPS UNFACTORED LANDING DISTANCE BY 1.51. FOR THE EMBRAER 195, MULTIPLY THE FULL FLAPS UNFACTORED LANDING DISTANCE BY 1.58.
  • Page 274: Avionics Mau 3A Failure

    Autopilot 2. For landing configuration, set slat/flap to full and set V REF FULL CAUTION: FOR THE EMBRAER 190, MULTIPLY THE FULL FLAPS UNFACTORED LANDING DISTANCE BY 1.30. FOR THE EMBRAER 195, MULTIPLY THE FULL FLAPS UNFACTORED LANDING DISTANCE BY 1.22.
  • Page 275: Avionics Mau 2A (2B) Overheat

    ABNORMAL AIRPLANE PROCEDURES FLIGHT MANUAL AVIONICS MAU 2A (2B) OVERHEAT Pull the associated circuit breaker. For MAU 2A OVHT, pull the B25 CB. For MAU 2B OVHT, pull the B26 and B35 CBs. Refer to AVIONICS MAU 2A (2B) FAIL Procedure to be aware of relevant inoperative items.
  • Page 276: Display Control Failure

    ABNORMAL AIRPLANE PROCEDURES FLIGHT MANUAL DISPLAY CONTROL FAILURE NOTE: - PFD selections of VOR, FMS, RA/BARO Minimums and Baro 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. Relevant Inoperative Items on both Pilot and Copilot Display Controllers: −...
  • Page 277: Fms Position Disagree

    Stop the airplane until the alignment is completed. IRS 1 (2) FAILURE Revert the affected IRS. MCDU 1 (2) OVERHEAT (PRE-MOD. SB 190-31-0007) Pull the associated circuit breaker. For MCDU 1 OVHT, pull the B16 CB. For MCDU 2 OVHT, pull the B31 CB.
  • Page 278: Mfd 1 (2) Overheat

    ABNORMAL AIRPLANE PROCEDURES FLIGHT MANUAL MFD 1 (2) OVERHEAT Pull the associated circuit breaker and revert the affected MFD if necessary. For MFD 1 OVHT, pull the B29 CB. For MFD 2 OVHT, pull the B20 CB. NAVCOM 1 (2) FAILURE Select and use the remaining NAVCOM (VHF, VOR, DME, Transponder).
  • Page 279: System Configuration Failure

    ABNORMAL AIRPLANE PROCEDURES FLIGHT MANUAL SYSTEM CONFIGURATION FAILURE Do not takeoff. TERRAIN FAILURE Increase awareness in relation to terrain proximity. VALIDATE CONFIGURATION Do not takeoff. VHF 3 FAILURE Select another VHF source. VHF 1 (2) (3) OVERHEAT Pull the associated circuit breaker. For VHF 1 OVHT, pull the C11 CB.
  • Page 280 FUEL IMBALANCE............4-20..04 FUEL CROSSFEED FAILURE.......... 4-20..05 FUEL CROSSFEED OVERRIDE FAILURE...... 4-20..05 ADVISORY FUEL AC PUMP 1 (2) FAILURE (POST-MOD. SB 190-31-0007 OR WITH EQUIVALENT MODIFICATION FACTORY INCORPORATED)..4-20..04 FUEL TANK LOW TEMPERATURE ......... 4-20..06 4-20 ANAC APPROVED...
  • Page 281: Airplane Flight Manual

    EMERGENCY & AIRPLANE ABNORMAL FLIGHT PROCEDURES MANUAL INTENTIONALLY BLANK 4-20 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 282: Fuel 1 (2) Low Level

    EMERGENCY AIRPLANE PROCEDURES FLIGHT MANUAL FUEL 1 (2) LOW LEVEL LAND AT THE NEAREST SUITABLE AIRPORT. CAUTION: AVOID ATTITUDES IN EXCESS OF 15° NOSE UP OR DOWN, UNCOORDINATED MANEUVERS NEGATIVE G´S. Turn ON the associated fuel AC pump. If fuel leak is suspected, accomplish the Fuel Leak Procedure. If fuel leak is not suspected, operate fuel crossfeed as required.
  • Page 283: Apu Fuel Shutoff Valve Failure

    ABNORMAL AIRPLANE PROCEDURES FLIGHT MANUAL APU FUEL SHUTOFF VALVE FAILURE Do not restart the APU. ENG 1 (2) FUEL SHUTOFF VALVE FAILURE If the ENG 1 (2) FUEL SOV FAIL message was displayed after pulling the associated engine fire handle, select the associated fuel AC electric pump and the fuel crossfeed to OFF.
  • Page 284: Fuel Crossfeed Failure

    ABNORMAL AIRPLANE PROCEDURES FLIGHT MANUAL FUEL CROSSFEED FAILURE If fuel crossfeed is set to LOW 1 or LOW 2 and fuel quantity is being equalized, set the fuel crossfeed to OFF when appropriate. If fuel crossfeed is set to LOW 1 or LOW 2 and fuel quantity is not being equalized: If Fuel XFeed Ovrd button is available, push it in and use crossfeed selector as required.
  • Page 285: Fuel Tank Low Temperature

    ABNORMAL AIRPLANE PROCEDURES FLIGHT MANUAL FUEL TANK LOW TEMPERATURE Increase airspeed to 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 CTA APPROVED Page 6 code 01 ORIGINAL...
  • Page 286 AIRPLANE EMERGENCY & 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 287 AIRPLANE EMERGENCY & ABNORMAL FLIGHT PROCEDURES MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 4-22 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 288 AIRPLANE EMERGENCY 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...
  • Page 289 AIRPLANE ABNORMAL 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 290 EMERGENCY & AIRPLANE ABNORMAL FLIGHT PROCEDURES MANUAL ICE & RAIN PROTECTION TABLE OF CONTENTS Block Page WARNING ANTI-ICE WING 1 (2) LEAKAGE ........4-24 ..03 CAUTION ANTI-ICE ENGINE 1 (2) FAILURE ........4-24 ..04 ANTI-ICE LOW CAPACITY ..........4-24 ..04 ANTI-ICE WING FAILURE ..........4-24 ..
  • Page 291 EMERGENCY & AIRPLANE ABNORMAL FLIGHT PROCEDURES MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 4-24 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 292: Anti-Ice Wing 1 (2) Leakage

    EMERGENCY AIRPLANE PROCEDURES FLIGHT MANUAL ANTI-ICE WING 1 (2) LEAKAGE Push out the ice protection wing button and avoid/exit icing conditions. If A-I WING 1 (2) LEAK message persists, push the affected side bleed button out, push the crossbleed button out and limit the altitude to 31000 ft maximum.
  • Page 293: Anti-Ice Engine 1 (2) Failure

    5 landing and maintain V REF FLAP 5 ICE CAUTION: FOR THE EMBRAER 190, MULTIPLY THE FULL FLAPS UNFACTORED LANDING DISTANCE BY 1.25. FOR THE EMBRAER 195, MULTIPLY THE FULL FLAPS UNFACTORED LANDING DISTANCE BY 1.35.
  • Page 294: Ice Detector 1 (2) Failure

    ABNORMAL AIRPLANE PROCEDURES FLIGHT MANUAL ICE DETECTOR 1 (2) FAILURE When flying in icing conditions, select the ice protection mode to on and select it to auto 2 minutes after exiting icing conditions. WINDSHIELD 1 (2) HEATER FAILURE 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.
  • Page 295 ABNORMAL AIRPLANE PROCEDURES FLIGHT MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 4-24 CTA APPROVED Page 6 code 01 ORIGINAL...
  • Page 296: Landing Gear & Brakes

    EMERGENCY & AIRPLANE ABNORMAL FLIGHT PROCEDURES MANUAL LANDING GEAR & BRAKES TABLE OF CONTENTS Block Page WARNING LANDING GEAR LEVER DISAGREE ....... 4-26..03 CAUTION AUTOBRAKE FAILURE ............ 4-26..04 BRAKE LH (RH) FAILURE ..........4-26..04 BRAKE OVERHEAT ............4-26..04 EMERGENCY BRAKE FAILURE ........
  • Page 297: Intentionally Blank

    EMERGENCY & AIRPLANE ABNORMAL FLIGHT PROCEDURES MANUAL INTENTIONALLY BLANK 4-26 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 298: Landing Gear Lever Disagree

    EMERGENCY AIRPLANE PROCEDURES FLIGHT MANUAL LANDING GEAR LEVER DISAGREE Cycle the landing gear lever. If the LG LEVER DISAG message persists and it was displayed after a landing gear extension, accomplish the Abnormal Landing Gear Extension Procedure. 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.
  • Page 299: Autobrake Failure

    • WHEN THE EMERGENCY/PARKING BRAKE LIGHT IS ON, MAINTAIN STEADY PRESSURE SINCE THE ANTI- SKID PROTECTION IS NOT AVAILABLE. • FOR THE EMBRAER 190, MULTIPLY THE FULL FLAPS UNFACTORED LANDING DISTANCE BY 1.51. FOR THE EMBRAER 195, MULTIPLY THE FULL FLAPS UNFACTORED LANDING DISTANCE BY 1.58.
  • Page 300: Landing Gear Nose Door Opened

    Exit and avoid icing conditions. For landing configuration, set slat/flap to full and set V REF FULL CAUTION: FOR THE EMBRAER 190, MULTIPLY THE FULL FLAPS UNFACTORED LANDING DISTANCE BY 1.30. FOR THE EMBRAER 195, MULTIPLY THE FULL FLAPS UNFACTORED LANDING DISTANCE BY 1.22.
  • Page 301: Brake Control Fault

    • WHEN THE EMERGENCY/PARKING BRAKE LIGHT IS ON, MAINTAIN STEADY PRESSURE SINCE THE ANTI- SKID PROTECTION IS NOT AVAILABLE. • FOR THE EMBRAER 190, MULTIPLY THE FULL FLAPS UNFACTORED LANDING DISTANCE BY 1.19. FOR THE EMBRAER 195, MULTIPLY THE FULL FLAPS UNFACTORED LANDING DISTANCE BY 1.30.
  • Page 302 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 303 AIRPLANE EMERGENCY & ABNORMAL FLIGHT PROCEDURES MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 4-28 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 304: Airplane Flight Manual

    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 305 AIRPLANE ABNORMAL PROCEDURES FLIGHT MANUAL THIS PAGE IS LEFT BLANK INTENTIONALLY 4-28 CTA APPROVED Page 4 code 01 ORIGINAL...
  • Page 306 EMERGENCY & AIRPLANE ABNORMAL FLIGHT PROCEDURES MANUAL SMOKE PROCEDURES TABLE OF CONTENTS Block Page WARNING CARGO FORWARD (AFT) SMOKE ......... 4-30..03 LAVATORY SMOKE............4-30..03 SMOKE EVACUATION ............. 4-30..03 SMOKE FIRE OR FUMES ..........4-30..04 CAUTION IFE RACK SMOKE ............4-30..07 RECIRCULATION SMOKE ..........
  • Page 307 EMERGENCY & AIRPLANE ABNORMAL FLIGHT PROCEDURES MANUAL INTENTIONALLY BLANK 4-30 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 308 EMERGENCY AIRPLANE PROCEDURES FLIGHT MANUAL CARGO FORWARD (AFT) SMOKE φAssociated Cargo Fire Extinguishing Button ....PUSH LAND AT THE NEAREST SUITABLE AIRPORT. Confirm the CRG AFT (FWD) FIREX HI ARM message extinguishes and the CRG AFT (FWD) FIREX LO ARM message is displayed. After 1 minute, confirm the CRG FWD (AFT) FIREX LO ARM message and cargo fire-extinguishing button light extinguish.
  • Page 309 Slat/Flap Lever............ 3 Set V + 20 KIAS or 130 KIAS (whichever is higher). REF FULL CAUTION: FOR THE EMBRAER 190, MULTIPLY THE FULL FLAPS UNFACTORED LANDING DISTANCE BY 2.21. FOR THE EMBRAER 195, MULTIPLY THE FULL FLAPS UNFACTORED LANDING DISTANCE BY 2.30.
  • Page 310 Ground Proximity Flap Override Button ... PUSH IN Slat/Flap Lever ......... 3 Set V + 20 KIAS. REF FULL CAUTION: FOR THE EMBRAER 190, MULTIPLY THE FULL FLAPS UNFACTORED LANDING DISTANCE BY 2.37. FOR THE EMBRAER 195, MULTIPLY THE FULL FLAPS UNFACTORED LANDING DISTANCE BY 2.14.
  • Page 311 Emergency Lights........ ARMED Ground Proximity Flap Override Button ..........PUSH IN Slat/Flap Lever ........3 Set V + 20 KIAS. REF FULL CAUTION: FOR THE EMBRAER 190, MULTIPLY FULL FLAPS UNFACTORED LANDING DISTANCE BY 2.55. FOR THE EMBRAER 195, MULTIPLY FULL...
  • Page 312 Landing configuration: Emergency Lights ..... ARMED Ground Proximity Flap Override Button ....PUSH IN Slat/Flap Lever......3 Set V + 20 KIAS. REF FULL CAUTION: FOR EMBRAER 190, MULTIPLY FULL FLAPS UNFACTORED LANDING DISTANCE BY 1.35. EMBRAER 195, MULTIPLY FULL...
  • Page 313 ABNORMAL AIRPLANE PROCEDURES FLIGHT MANUAL INTENTIONALLY BLANK 4-30 CTA APPROVED Page 8 code 01 ORIGINAL...
  • Page 314 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 Temperatures ............... 5-01..02 Airspeed................ 5-01..02 Airport Declared Field Data .......... 5-01..03 Takeoff and Landing Distances ........5-01..04 Takeoff and Landing Runway Conditions .....
  • Page 315: Introduction

    INTRODUCTION The performance information given in this Section is applicable and common to all EMBRAER 190 and EMBRAER 195 models. For performance information related to an airplane equipped with a specific engine model, refer to the Supplement 1 - CAFM.
  • Page 316 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, 3 or 4 DOWN 0 TO V 1 after V DOWN TO SEGMENT TOGA 1, 2, 3 or 4...
  • Page 317: Definitions

    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 - ! ! ! ! ISA Temperature deviation from the standard temperature defined for ISA, at the specified altitude.
  • Page 318: Airport Declared Field Data

    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 319: Takeoff And Landing Distances

    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 320 AIRPLANE PERFORMANCE 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 321: Takeoff And Landing Runway Conditions

    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 322: Takeoff And Landing Speeds

    AIRPLANE PERFORMANCE 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 323 AIRPLANE PERFORMANCE 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 324 AIRPLANE PERFORMANCE 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 325 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 326: Takeoff Path

    AIRPLANE PERFORMANCE 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 327: Weights

    PERFORMANCE AIRPLANE FLIGHT MANUAL 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 takeoff flaps.
  • Page 328: Engine Ratings

    AIRPLANE PERFORMANCE FLIGHT MANUAL DEPENDENT TAKEOFF WEIGHT It is the takeoff weight affected by V selection. The V dependent takeoff weights are those limited by field length (TOD/OEI, ASD/OEI, ASD/AEO), brake energy and obstacle clearance. The non-V dependent takeoff weights are those limited by TOD/AEO, climb gradients, tire speed and structure.
  • Page 329 AIRPLANE PERFORMANCE FLIGHT MANUAL 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. It is usually time limited. AUTOMATIC TAKEOFF THRUST CONTROL SYSTEM - ATTCS It is the system that increases the Normal Takeoff Thrust on the live engine to Reserved Takeoff Thrust, when the other engine fails.
  • Page 330: Enroute And Turn Performance

    AIRPLANE PERFORMANCE FLIGHT MANUAL MAXIMUM CLIMB THRUST It is the maximum thrust available for use during climb to cruise flight level, step climb, or for acceleration to cruise speed, with all engines operating, not time limited. MAXIMUM CRUISE THRUST It is the maximum thrust available for cruise with all engines operating, not time limited.
  • Page 331: Performance Information

    AIRPLANE PERFORMANCE FLIGHT MANUAL PERFORMANCE INFORMATION INPUT DATA ADJUSTMENT TO ENVELOPE Input data outside the airplane operational envelope is usually adjusted by the CAFM. This is particularly frequent for input temperatures, but can also occur for input altitudes and speeds. A message indicating that input values have been adjusted to the AFM limits will be shown in the “Messages”...
  • Page 332 AIRPLANE PERFORMANCE FLIGHT MANUAL The minimum or the fixed level-off height cannot be lower than 400 ft AGL, but the user can define higher figures. The maximum level-off height will never be lower than the minimum level-off height. The fixed level-off height is not changed during flight path calculation. Therefore, for airport analysis mode, airplane weight will be reduced as required for obstacle clearance with fixed level-off height.
  • Page 333 AIRPLANE PERFORMANCE FLIGHT MANUAL TAKEOFF MAXIMUM STOPPING MARGIN The use of minimum V has long been understood to be a valuable aid in the prevention of rejected takeoff (RTO) overrun accidents. The minimum V provided by the CAFM will be the lowest V for the RTOW.
  • Page 334 AIRPLANE PERFORMANCE FLIGHT MANUAL TAKEOFF FIELD LENGTH - WET AND CONTAMINATED RUNWAY When “Airport Analysis” calculation type is selected, the wet or contaminated runway takeoff performance is compared to the dry runway takeoff performance, and the lesser takeoff weight is taken as the maximum field length limited takeoff weight.
  • Page 335: Demonstrated Crosswind

    AIRPLANE PERFORMANCE FLIGHT MANUAL ATTCS FOR GO-AROUND ATTCS selection is not available for Go-Around, both in the Landing module and in the Takeoff module. CAFM assumes ATTCS always set to ON for Go-Around, due to airplane system design characteristics. AIR CONDITIONING SYSTEM FOR GO-AROUND Air Conditioning selection is not available for Go-Around, both in the Landing module and in the Takeoff module.
  • Page 336: Noise Levels

    For the airplanes equipped with both right and left hand side engines with the following reference: − EBUCF34-10E6A1G07 The noise levels are presented in the following table: NOISE LEVELS IN EPNdB CONDITION Airplane Model Flyover Lateral Approach EMBRAER 195-STD 83.0 92.6 92.5 EMBRAER 195-LR 84.0 92.5 92.5 EMBRAER 195-AR 84.9 92.4 92.6...
  • Page 337 AIRPLANE PERFORMANCE FLIGHT MANUAL The noise levels for EMBRAER 195 equipped with APU Hamilton Sundstrand APS 2300 and two GE CF34-10E6A1, were established as follows: − Flyover: at maximum takeoff weight, flap setting 1 and + 12 KIAS; − Lateral: at maximum takeoff weight, flap setting 1 and with all engines at maximum takeoff power setting;...
  • Page 338 For the airplanes equipped with both right and left hand side engines with the following reference: − EBUCF34-10E7G07 The noise levels are presented in the following table: NOISE LEVELS IN EPNdB CONDITION Airplane Model Flyover Lateral Approach EMBRAER 195-STD 83.0 92.6 92.5 EMBRAER 195-LR 84.0 92.5 92.5 EMBRAER 195-AR 84.9 92.4 92.6...
  • Page 339 AIRPLANE PERFORMANCE FLIGHT MANUAL The noise levels for EMBRAER 195 equipped with APU Hamilton Sundstrand APS 2300 and two GE CF34-10E7, were established as follows: − Flyover: at maximum takeoff weight, flap setting 1 and + 12 KIAS; − Lateral: at maximum takeoff weight, flap setting 1 and with all engines at maximum takeoff power setting;...
  • Page 340: Position Error Corrections

    AIRPLANE PERFORMANCE 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 341 AIRPLANE PERFORMANCE FLIGHT MANUAL AIRSPEED POSITION ERROR CORRECTION AIR DATA SYSTEM 3 - FLAPS 0 PRESSURE ALTITUDE - ft 20000 AND BELOW 30000 AND ABOVE -1.0 -2.0 -3.0 CALIBRATED AIRSPEED = INDICATED AIRSPEED + DV -4.0 -5.0 INDICATED AIRSPEED - kt 5-10 CTA APPROVED Page 2...
  • Page 342 AIRPLANE PERFORMANCE FLIGHT MANUAL AIRSPEED POSITION ERROR CORRECTION AIR DATA SYSTEM 3 - FLAPS 1 PRESSURE ALTITUDE - ft -0.5 10000 AND BELOW -1.0 -1.5 -2.0 20000 -2.5 CALIBRATED AIRSPEED = INDICATED AIRSPEED + DV -3.0 INDICATED AIRSPEED - kt 5-10 CTA APPROVED Page 3...
  • Page 343 AIRPLANE PERFORMANCE FLIGHT MANUAL AIRSPEED POSITION ERROR CORRECTION AIR DATA SYSTEM 3 - FLAPS 2 PRESSURE ALTITUDE - ft -0.5 -1.0 10000 AND BELOW -1.5 -2.0 -2.5 20000 -3.0 CALIBRATED AIRSPEED = INDICATED AIRSPEED + DV -3.5 -4.0 INDICATED AIRSPEED - kt 5-10 CTA APPROVED Page 4...
  • Page 344 AIRPLANE PERFORMANCE FLIGHT MANUAL AIRSPEED POSITION ERROR CORRECTION AIR DATA SYSTEM 3 - FLAPS 3, 4 and 5 PRESSURE ALTITUDE - ft -0.5 -1.0 10000 AND BELOW -1.5 -2.0 -2.5 20000 -3.0 CALIBRATED AIRSPEED = INDICATED AIRSPEED + DV -3.5 -4.0 INDICATED AIRSPEED - kt 5-10...
  • Page 345 AIRPLANE PERFORMANCE FLIGHT MANUAL AIRSPEED POSITION ERROR CORRECTION AIR DATA SYSTEM 3 - FLAPS FULL PRESSURE ALTITUDE - ft -0.5 10000 AND BELOW -1.0 -1.5 -2.0 -2.5 20000 -3.0 CALIBRATED AIRSPEED = INDICATED AIRSPEED + DV -3.5 -4.0 INDICATED AIRSPEED - kt 5-10 CTA APPROVED Page 6...
  • Page 346: Altitude Position Error Correction Charts

    AIRPLANE PERFORMANCE FLIGHT MANUAL ALTITUDE POSITION ERROR CORRECTION CHARTS Enter the appropriate chart with indicated airspeed, the indicated pressure altitude considering the appropriate airplane configuration to read the altimetric correction. 5-10 CTA APPROVED Page 7 code 01 ORIGINAL...
  • Page 347 AIRPLANE PERFORMANCE FLIGHT MANUAL ALTITUDE POSITION ERROR CORRECTION AIR DATA SYSTEM 3 - FLAPS 0 PRESSURE ALTITUDE - ft 20000 AND BELOW CORRECTED ALTITUDE = INDICATED ALTITUDE - DH 30000 AND ABOVE INDICATED AIRSPEED - kt 5-10 CTA APPROVED Page 8 code 01 ORIGINAL...
  • Page 348 AIRPLANE PERFORMANCE FLIGHT MANUAL ALTITUDE POSITION ERROR CORRECTION AIR DATA SYSTEM 3 - FLAPS 1 PRESSURE ALTITUDE - ft 20000 10000 AND BELOW CORRECTED ALTITUDE = INDICATED ALTITUDE - DH INDICATED AIRSPEED - kt 5-10 CTA APPROVED Page 9 code 01 ORIGINAL...
  • Page 349 AIRPLANE PERFORMANCE FLIGHT MANUAL ALTITUDE POSITION ERROR CORRECTION AIR DATA SYSTEM 3 - FLAPS 2 PRESSURE ALTITUDE - ft 20000 10000 AND BELOW CORRECTED ALTITUDE = INDICATED ALTITUDE - DH INDICATED AIRSPEED - kt 5-10 CTA APPROVED Page 10 code 01 ORIGINAL...
  • Page 350 AIRPLANE PERFORMANCE FLIGHT MANUAL ALTITUDE POSITION ERROR CORRECTION AIR DATA SYSTEM 3 - FLAPS 3, 4 AND 5 PRESSURE ALTITUDE - ft 20000 10000 AND BELOW CORRECTED ALTITUDE = INDICATED ALTITUDE - DH -100 INDICATED AIRSPEED - kt 5-10 CTA APPROVED Page 11 code 01 ORIGINAL...
  • Page 351 AIRPLANE PERFORMANCE FLIGHT MANUAL ALTITUDE POSITION ERROR CORRECTION AIR DATA SYSTEM 3 - FLAPS FULL PRESSURE ALTITUDE - ft 20000 10000 AND BELOW CORRECTED ALTITUDE = INDICATED ALTITUDE - DH INDICATED AIRSPEED - kt 5-10 CTA APPROVED Page 12 code 01 ORIGINAL...
  • Page 352 NOT APPLICABLE NOT APPLICABLE NOT APPLICABLE NOT APPLICABLE NOT APPLICABLE NOT APPLICABLE RADIAL TIRES PERFORMANCE CONTROLLER PILOT DATA LINK COMMUNICATIONS (CPDLC) S-TOC ANAC APPROVED code 16 Page 1 REVISION 12 Copyright © by Embraer. Refer to cover page for details.
  • Page 353: Not Applicable

    SUPPLEMENTS AIRPLANE FLIGHT MANUAL EASTERN EUROPE FUELS OPERATION TAKEOFF AND LANDING OPERATIONS BELOW -40°C DOWN TO -45°C NOT APPLICABLE S-TOC ANAC APPROVED code 16 Page 2 TEMPORARY REVISION 12.4 Copyright © by Embraer. Refer to cover page for details.
  • Page 354 SUPPLEMENTS AIRPLANE FLIGHT MANUAL EASTERN EUROPE FUELS OPERATION TAKEOFF AND LANDING OPERATIONS BELOW -40°C DOWN TO -45°C S-TOC ANAC APPROVED Page 2 code 16 REVISION 12 Copyright © by Embraer. Refer to cover page for details.
  • Page 355 Software Presentation............S1-02 ..01 Limitations................S1-05 ..01 Configuration ..............S1-05 ..01 Presentation..............S1-05 ..01 Media P/N: CAFM-190-FAA-001 VERSION 1.0 ... S1-05 ..01 Normal Procedures............S1-10 ..01 Emergency and Abnormal Procedures......S1-10 ..01 Performance ..............S1-15 ..01 Engine Data ..............
  • Page 356 SUPPLEMENT 1 AIRPLANE COMPUTERIZED AFM FLIGHT MANUAL INTRODUCTION This Supplement presents the Computerized Airplane Flight Manual CAFM - for EMBRAER 190 and EMBRAER 195 performance calculation. S1-00 ANAC APPROVED Page 2 code 01 REVISION 2...
  • Page 357: Software Presentation

    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 358: Intentionally Blank

    SUPPLEMENT 1 AIRPLANE COMPUTERIZED AFM FLIGHT MANUAL INTENTIONALLY BLANK S1-02 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 359 21.2) MUST SELECT FIXED V OPTION AND MUST USE ONE OF THE FOLLOWING VALUES: FLAPS POSITION 1.18 1.17 1.17 1.21 CONTINUES ON NEXT PAGE S1-05 ANAC APPROVED code 06 Page 1 REVISION 12 Copyright © by Embraer. Refer to cover page for details.
  • Page 360 AFM. - This version incorporates all capabilities of the previous versions. S1-05 ANAC APPROVED Page 2 code 06 REVISION 12 Copyright © by Embraer. Refer to cover page for details.
  • Page 361 21.2) MUST SELECT FIXED V OPTION AND MUST USE ONE OF THE FOLLOWING VALUES: FLAPS POSITION 1.18 1.17 1.17 1.21 CONTINUES ON NEXT PAGE S1-05 ANAC APPROVED code 09 Page 1 REVISION 12 Copyright © by Embraer. Refer to cover page for details.
  • Page 362 AFM. - This version incorporates all capabilities of the previous versions. S1-05 ANAC APPROVED Page 2 code 09 REVISION 12 Copyright © by Embraer. Refer to cover page for details.
  • Page 363: Emergency And Abnormal Procedures

    AIRPLANE SUPPLEMENT 1 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 Page 1 code 01 ORIGINAL...
  • Page 364 AIRPLANE SUPPLEMENT 1 COMPUTERIZED AFM FLIGHT MANUAL THIS PAGE INTENTIONALLY LEFT BLANK S1-10 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 365 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 366 SUPPLEMENT 1 AIRPLANE COMPUTERIZED AFM FLIGHT MANUAL INTENTIONALLY BLANK S1-15 ANAC APPROVED Page 2 code 02 REVISION 2...
  • Page 367 SUPPLEMENT 2 AIRPLANE PRIMUS EPIC - FLIGHT FLIGHT MANAGEMENT SYSTEM MANUAL SUPPLEMENT 2 PRIMUS EPIC FLIGHT MANAGEMENT SYSTEM TABLE OF CONTENTS Block Page General ................S2-00 ..02 Introduction..............S2-00 ..02 Navigation Operational Approvals........ S2-00 ..02 Limitations................S2-05 ..01 General Limitations............
  • Page 368 1.0 for missed approach, when equipped with the Honeywell Primus Epic FMS when operated compliance with recommended Embraer flight crew and operational procedures. − The temperature compensation function complies with RTCA/DO-236B, Appendix H.2. NOTE: Appropriate operational...
  • Page 369 SUPPLEMENT 2 AIRPLANE PRIMUS EPIC - FLIGHT FLIGHT MANAGEMENT SYSTEM MANUAL NOTE: The airplane capability does not constitute RNP operation approval. The operators must be granted local approval conduct operations. − Navigation using GPS - The FMS has been demonstrated compliant with the requirements of FAA AC90-94, regarding the use of GPS for IFR navigation in en-route, terminal, and non- precision approach operations.
  • Page 370 SUPPLEMENT 2 AIRPLANE PRIMUS EPIC - FLIGHT FLIGHT MANAGEMENT SYSTEM MANUAL RNP-10 Airspace - The FMS has been demonstrated compliant with the requirements of FAA Order 8400.12A when operated as a dual system, with dual installed FMS, GPS, and IRS operational prior to the start of flight. Enroute and Terminal Operation - The FMS has been demonstrated compliant with the requirements of AC 20-130A and AC25-15, regarding multi-sensor system IFR operation in...
  • Page 371 Supplement. − For airplanes Post-Mod. SB 190-31-0009 (LOAD 19.3) or with an equivalent modification factory incorporated with VGP enabled, the FMS has been demonstrated compliant with the...
  • Page 372 SUPPLEMENT 2 AIRPLANE PRIMUS EPIC - FLIGHT FLIGHT MANAGEMENT SYSTEM MANUAL INTENTIONALLY BLANK S2-00 ANAC APPROVED Page 6 code 01 REVISION 6...
  • Page 373: General Limitations

    SUPPLEMENT 2 AIRPLANE PRIMUS EPIC - FLIGHT FLIGHT MANAGEMENT SYSTEM MANUAL LIMITATIONS GENERAL LIMITATIONS - The FMS does not correct the speed targets, including approach and go around speeds, for ice conditions or non-normal conditions. It is the pilot responsibility to ensure that the speeds are within the limits in these conditions.
  • Page 374 AC 90-101 Appendix 4 item 3.i (2) and any speed restrictions published with the RF leg segments on individual RNP AR approach procedures. - For airplanes Pre-Mod. SB 190-31-0033 (LOAD 23.1), RNP AR 0.3 procedures with RF legs smaller than 1.25 NM radius are prohibited.
  • Page 375 - Use of VNAV guidance below the published approach minimums without the appropriate visibility indications is prohibited. - For airplanes Pre-Mod. SB 190-31-0024 (LOAD 21.4), when using VGP, use of Temperature Compensation is prohibited. - For airplanes Post-Mod. SB 190-31-0015 (LOAD 21.2) or with an equivalent modification factory incorporated, Pre-Mod.
  • Page 376 Flight Plan. - The FMS Disable selection on MCDU Radio Tune NAV page is prohibited for airplanes Pre-Mod. SB 190-31-0009 (LOAD 19.3). - The use of the Step Climb function is prohibited. - The selection of course interception to a conditional waypoint is prohibited.
  • Page 377 AIRPLANE SUPPLEMENT 2 PRIMUS EPIC - FLIGHT FLIGHT MANAGEMENT SYSTEM MANUAL FMS POSITION ANOMALY This limitation is applicable to airplanes equipped with Primus EPIC software version 23.1 or 23.2 and it is associated to the following conditions: Crossing the 180 degree meridian will cause FMS longitude position calculation to move by approximately 180 degrees.
  • Page 378 AIRPLANE SUPPLEMENT 2 PRIMUS EPIC - FLIGHT FLIGHT MANAGEMENT SYSTEM MANUAL RUNWAY CHANGE WHEN NO ARRIVAL OR APPROACH PROCEDURE IS SELECTED This limitation is applicable to airplanes equipped with Primus EPIC software version 23.1 or 23.2 and it is associated to the following conditions: −...
  • Page 379 AIRPLANE SUPPLEMENT 2 PRIMUS EPIC - FLIGHT FLIGHT MANAGEMENT SYSTEM MANUAL NOTE: Follow the procedure above for any subsequent runway change, otherwise the MOD FLT PLAN page will display the information correctly when a new runway is inserted via ARRIVAL page, but the described misbehavior will occur once the change is activated.
  • Page 380 AIRPLANE SUPPLEMENT 2 PRIMUS EPIC - FLIGHT FLIGHT MANAGEMENT SYSTEM MANUAL INTENTIONALLY BLANK S2-05 ANAC APPROVED Page 8 code 01 REVISION 8...
  • Page 381: Normal Procedures

    For airplanes Pre-Mod. SB 190-31-0015 (previous to LOAD 21.2): Fuel Used ..............RESET PFD NAV Source ............SELECT FMS For airplanes Post-Mod. SB 190-31-0015 (LOAD 21.2 and on) or with an equivalent modification factory incorporated: Speed Selector Knob..........AS REQUIRED LNAV................
  • Page 382 SUPPLEMENT 2 AIRPLANE PRIMUS EPIC - FLIGHT FLIGHT MANAGEMENT SYSTEM MANUAL APPROACH It is assumed that LNAV and VNAV are the active navigation modes, and the Speed Selector Knob is set to FMS. If RNP AR approach is intended: NOTE: - The procedure must be retrieved from the FMS database.
  • Page 383 SUPPLEMENT 2 AIRPLANE PRIMUS EPIC - FLIGHT FLIGHT MANAGEMENT SYSTEM MANUAL MISSED APPROACH LNAV ............... SELECT HOLD PATTERN Speed................AS REQUIRED For speeds above 210 kt, pilots must monitor the position throughout maneuver ensure protected airspace maintenance. Hold Entry Type ............VERIFY Hold Inbound Course ............
  • Page 384 SUPPLEMENT 2 AIRPLANE PRIMUS EPIC - FLIGHT FLIGHT MANAGEMENT SYSTEM MANUAL COMPLEMENTARY INFORMATION DEPENDING ON FMS CONFIGURATION The following information is also applicable and should be observed depending on the airplane configuration. FOR AIRPLANES EQUIPED WITH PRIMUS EPIC LOAD 4.0 AND ON Cruise: With FMS Cruise Schedules in MXR SPD or MAX SPD, the TRS does not automatically transition to CRZ.
  • Page 385: Emergency And Abnormal Procedures

    SUPPLEMENT 2 AIRPLANE PRIMUS EPIC - FLIGHT FLIGHT MANAGEMENT SYSTEM MANUAL EMERGENCY AND ABNORMAL PROCEDURES All FMS Action/Malfunction Messages are described in the Honeywell Flight Management System Pilot's Operating Manual. The airplane abnormal operating procedures are the same as those in the basic AFM except as follows: DEGRADED NAVIGATION The UNABLE RNP and GPS APPR RAIM UNAVAIL scratchpad...
  • Page 386: Dead Reckoning

    SUPPLEMENT 2 AIRPLANE PRIMUS EPIC - FLIGHT FLIGHT MANAGEMENT SYSTEM MANUAL DEAD RECKONING The pilot should discontinue use of the FMS when in it is in DR mode. If there is no alternative means of navigation (off-side FMS, VOR, etc.), the pilot may elect to perform manual position updates to the FMS, using reference point fly-over techniques, to minimize the navigation error.
  • Page 387 NOTE: 1) The default RNP value for Remote/Oceanic is: 10 for airplanes equipped with Load version previous than Load 25.1.0.1 (Pre-Mod. SB 190-31-0041); 4 for airplanes equipped with Load 25.1.0.1 and on (Post-Mod. SB 190-31-0041 or with an equivalent modification factory incorporated). S2-10 ANAC APPROVED...
  • Page 388 0009), performing any approach using FMS; 0.5 for airplanes equipped with Load 25.3 (Post-Mod. SB 190-31-0049 or Post-Mod. SB 190LIN-31-0012), Load 25.4 and on (Post-Mod. SB 190-31-0045 or Post- Mod. SB 190LIN-31-0009) or with an equivalent modification factory incorporated, performing radio- based approach.
  • Page 389 AIRPLANE SUPPLEMENT 2 PRIMUS EPIC - FLIGHT FLIGHT MANAGEMENT SYSTEM MANUAL GPS mode is given the highest priority for position determination, when GPS HIL is within limits. If GPS is not available, the FMS will utilize radio modes (DME-DME or VOR-DME) if they provide satisfactory accuracy.
  • Page 390 10 for airplanes equipped with Load version previous than Load 25.1.0.1 (Pre-Mod. SB 190-31-0041); 4 for airplanes equipped with Load 25.1.0.1 and on (Post-Mod. SB 190-31-0041 or with an equivalent modification factory incorporated). 2) The DO-236A Containment Limit for Remote/Oceanic is: 20 for airplanes equipped with Load version previous than Load 25.1.0.1 (Pre-Mod.
  • Page 391 0009), performing any approach using FMS; 0.5 for airplanes equipped with Load 25.3 (Post-Mod. SB 190-31-0049 or Post-Mod. SB 190LIN-31-0012), Load 25.4 and on (Post-Mod. SB 190-31-0045 or Post- Mod. SB 190LIN-31-0009) or with an equivalent modification factory incorporated, performing radio- based approach.
  • Page 392 AIRPLANE SUPPLEMENT 2 PRIMUS EPIC - FLIGHT FLIGHT MANAGEMENT SYSTEM MANUAL INTENTIONALLY BLANK S2-10 ANAC APPROVED Page 12 code 01 REVISION 10...
  • Page 393 SUPPLEMENT 3 AIRPLANE CAT II OPERATION FLIGHT MANUAL SUPPLEMENT 3 CAT II OPERATION TABLE OF CONTENTS Block Page General ................S3-00 ..02 CAT II Engagement Logic ..........S3-00 ..02 CAT II Warnings ............S3-00 ..03 Limitations................S3-05 ..01 Flight Controls ..............
  • Page 394 SUPPLEMENT 3 AIRPLANE CAT II OPERATION FLIGHT 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 395: Cat Ii Warnings

    SUPPLEMENT 3 AIRPLANE CAT II OPERATION FLIGHT MANUAL − Glide slope and Localizer deviation valid on both PFD’s. − No reversions (IRS and ADC) modes selected on both PFD’s. − Valid Airspeed and Baro Altitude on both PFD’s. − No comparison monitors are tripped (FPA, Attitude, Heading, Airspeed, Baro Altitude, Localizer, Glide slope and Radio altitude) on both PFD’s.
  • Page 396 SUPPLEMENT 3 AIRPLANE CAT II OPERATION FLIGHT MANUAL − 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. − No back course selected. For localizer, the following additional condition is required: −...
  • Page 397 SUPPLEMENT 3 AIRPLANE CAT II OPERATION FLIGHT MANUAL − On-side localizer tuned and valid. − 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 398 SUPPLEMENT 3 AIRPLANE CAT II OPERATION FLIGHT MANUAL INTENTIONALLY BLANK S3-00 CTA APPROVED Page 6 code 01 ORIGINAL...
  • Page 399: Limitations

    SUPPLEMENT 3 AIRPLANE CAT II OPERATION FLIGHT MANUAL LIMITATIONS FLIGHT CONTROLS CAT II is prohibited with the SPOILER FAULT EICAS message displayed. MINIMUM EQUIPMENT REQUIRED The performance of Category II approaches has been demonstrated to meet the airworthiness requirements of FAA AC 120-29A – Appendix 3 and CS AWO Subpart 2 requirement, when the following equipment are installed and operative: −...
  • Page 400: Autopilot System

    SUPPLEMENT 3 AIRPLANE CAT II OPERATION FLIGHT 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. MAXIMUM WIND COMPONENTS This limitation applies to manual FD (Flight Director) approaches only.
  • Page 401: Normal Procedures

    SUPPLEMENT 3 AIRPLANE CAT II OPERATION FLIGHT MANUAL NORMAL PROCEDURES CAT II APPROACH BEFORE INTERCEPTING LOCALIZER COURSE Set the RA/BARO Minimums Selector knob to RA. Perform the Descent/Approach/Before Landing checklists, as appropriate. Set the CAT II Decision Height on both Display Control Panels. Test Radio Altimeter if only one is available.
  • Page 402: Missed Approach

    SUPPLEMENT 3 AIRPLANE CAT II OPERATION FLIGHT MANUAL AFTER PASSING FAF The pilot flying should maintain the Landing Reference Speed REF 5 At 80 ft above the decision height setting the EGPWS will call out "APPROACHING MINIMUMS". NOTE: If the CAT II Instrument Approach Landing chart does not authorize the use of RA, set the RA to OFF.
  • Page 403: Emergency And Abnormal Procedures

    SUPPLEMENT 3 AIRPLANE CAT II OPERATION FLIGHT MANUAL EMERGENCY AND ABNORMAL PROCEDURES ALTITUDE LOSS The demonstrated altitude loss due to a pitch down hardover during flight test is presented in the graph below. Recovery initiated 1 second after failure recognition: FAILURE OCCURS AIRPLANE WHEEL FAILURE...
  • Page 404: Abnormal Procedures

    SUPPLEMENT 3 AIRPLANE CAT II OPERATION FLIGHT MANUAL ABNORMAL PROCEDURES HARDOVER If any unusual acceleration or motion is noticed on the airplane flight path the approach must be discontinued, and: Autopilot ..............DISENGAGE MISSED APPROACH Procedure......PERFORM AS REQUIRED Perform a normal MISSED APPROACH Procedure, unless the approach is continued under visual conditions and the airplane position and attitude assure a safe landing.
  • Page 405: Autopilot Malfunction

    SUPPLEMENT 3 AIRPLANE CAT II OPERATION FLIGHT MANUAL ENGINE FAILURE ON FINAL APPROACH OR DURING GO-AROUND Go-Around..............PERFORM AUTOPILOT MALFUNCTION BEFORE REACHING FAF If the autopilot disengages or has to be disengaged, try to reengage it. If the autopilot disengages again: MISSED APPROACH Procedure ......
  • Page 406 SUPPLEMENT 3 AIRPLANE CAT II OPERATION FLIGHT MANUAL DISPLAY WARNINGS DURING FINAL APPROACH Discontinue the approach if any of the following warnings occur: - APPR 1 ONLY displayed on Autopilot Approach Status Annunciator, - EICAS message APPR 2 NOT AVAIL presented, - RALT FAIL (cyan), - RA (amber), - GS (amber),...
  • Page 407 SUPPLEMENT 3 AIRPLANE CAT II OPERATION FLIGHT MANUAL PERFORMANCE The performance data required for Category II operations are presented by basic CAFM output tables and must be calculated previously. Operational regulations may require additional CAFM landing distance adjustment. ENGINES FLAPS GEAR AIRSPEED APPROACH...
  • Page 408 SUPPLEMENT 3 AIRPLANE CAT II OPERATION FLIGHT MANUAL INTENTIONALLY BLANK S3-10 CTA APPROVED Page 8 code 01 ORIGINAL...
  • Page 409 SUPPLEMENT 4 AIRPLANE RVSM OPERATION FLIGHT MANUAL SUPPLEMENT 4 RVSM OPERATION TABLE OF CONTENTS Block Page General ................S4-00 ..02 Introduction ..............S4-00 ..02 Limitations................S4-05 ..01 Minimum Equipment Required ........S4-05 ..01 Normal Procedures............S4-10 ..01 External Safety Inspection ..........
  • Page 410 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 190 and EMBRAER 195 minimum vertical separation from 2000 ft to 1000 ft between FL 290 and FL 410.
  • Page 411 SUPPLEMENT 4 AIRPLANE RVSM OPERATION FLIGHT MANUAL LIMITATIONS MINIMUM EQUIPMENT REQUIRED During RVSM operation it is necessary that the following equipment and instruments be in proper operating condition: − 2 RVSM Compliant Air Data Systems; − 1 Autopilot with Altitude Hold Mode operative; −...
  • Page 412 SUPPLEMENT 4 AIRPLANE RVSM OPERATION FLIGHT MANUAL THIS PAGE INTENTIONALLY LEFT BLANK S4-05 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 413 AIRPLANE SUPPLEMENT 4 RVSM OPERATION FLIGHT MANUAL NORMAL PROCEDURES The actions listed below must complement the procedures contained in the basic AFM. The remaining Normal Procedures section remains unchanged. EXTERNAL SAFETY INSPECTION NOSE SECTION Air Data Smart Probes..........NO DAMAGE OR OBSTRUCTION Particular attention should be paid to the condition of the pressure ports and to the marked area on the fuselage skin near each Air...
  • Page 414: After Landing

    AIRPLANE SUPPLEMENT 4 RVSM OPERATION FLIGHT MANUAL When altitude difference between PFD 1 and PFD 2 exceeds 100ft, select ADS 3 on the PFD that does not agree with IESS. AFTER LANDING In case of failure or malfunction, the following information should be recorded when appropriate: −...
  • Page 415 AIRPLANE SUPPLEMENT 4 RVSM OPERATION FLIGHT MANUAL PERFORMANCE Performance Data presented in the basic AFM remain unchanged. S4-10 CTA APPROVED Page 3 code 01 ORIGINAL...
  • Page 416 AIRPLANE SUPPLEMENT 4 RVSM OPERATION FLIGHT MANUAL THIS PAGE INTENTIONALLY LEFT BLANK S4-10 CTA APPROVED Page 4 code 01 ORIGINAL...
  • Page 417 AIRPLANE SUPPLEMENT 11 RADIAL TIRES FLIGHT PERFORMANCE MANUAL SUPPLEMENT 11 RADIAL TIRES PERFORMANCE TABLE OF CONTENTS Block Page General ................S11-00 ..02 Introduction..............S11-00 ..02 Limitations................S11-05 ..01 Operational Limitations..........S11-05 ..01 Normal Procedures............S11-10 ..01 Emergency and Abnormal Procedures ......
  • Page 418: Performance

    PERFORMANCE MANUAL GENERAL INTRODUCTION This supplement provides information required for EMBRAER 190 and EMBRAER 195 airplanes operation taking credit of radial tires improved takeoff and landing performance. The information herein presented replaces or complements the equivalent information in the basic AFM.
  • Page 419 MANUAL LIMITATIONS OPERATIONAL LIMITATIONS TIRE SPECIFICATION The performance herein stated applies to EMBRAER 190 and 195 with the following tires installed on both sides of each landing gear: Nose Landing Gear Tires: P/N: M18201 Main Landing Gear Tires: P/N: M18602 NOTE: For any tire configuration that differs from the configuration listed above, refer to the Supplement 1 –...
  • Page 420 AIRPLANE SUPPLEMENT 11 RADIAL TIRES FLIGHT PERFORMANCE MANUAL INTENTIONALLY BLANK S11-05 ANAC APPROVED Page 2 code 01 REVISION 8...
  • Page 421 AIRPLANE SUPPLEMENT 11 RADIAL TIRES FLIGHT PERFORMANCE 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. PERFORMANCE The performance calculations are presented by basic CAFM output tables and must be calculated previously with Tires model option set to Radial.
  • Page 422 AIRPLANE SUPPLEMENT 11 RADIAL TIRES FLIGHT PERFORMANCE MANUAL INTENTIONALLY BLANK S11-10 ANAC APPROVED Page 2 code 01 REVISION 8...
  • Page 423 AIRPLANE SUPPLEMENT 12 FLIGHT CPDLC MANUAL SUPPLEMENT 12 CONTROLLER TO PILOT DATA LINK COMMUNICATIONS (CPDLC) TABLE OF CONTENTS Block Page General ................S12-00 ..02 Introduction..............S12-00 ..02 Limitations................S12-05 ..01 Normal Procedures............S12-10 ..01 Emergency and Abnormal Procedures ......S12-10 ..02 Performance ..............
  • Page 424 FLIGHT MANUAL GENERAL INTRODUCTION This supplement is applicable to airplanes Post-Mod. SB 190-23-0011 or SB 190LIN-23-0014 or with an equivalent modification factory incorporated. FAA has approved the aircraft data link system to the criteria contained in AC20-140A for ATN B1 using VDL M2. The data link system meets the aircraft-allocated performance requirements for continental applications (ATN B1 using VDL M2).
  • Page 425 SUPPLEMENT 12 AIRPLANE CPDLC FLIGHT MANUAL LIMITATIONS The usage of ATN-CPDLC is restricted to supplementary means of communication for non time critical messages. The usage of ATN-CPDLC with one inoperative MCDU is prohibited. The ACARS can be disabled by the flight crew, but it will cause all data link communication to be unavailable.
  • Page 426 SUPPLEMENT 12 AIRPLANE CPDLC FLIGHT MANUAL INTENTIONALLY BLANK S12-05 ANAC APPROVED Page 2 code 01 REVISION 10...
  • Page 427 AIRPLANE SUPPLEMENT 12 FLIGHT CPDLC MANUAL NORMAL PROCEDURES AFTER TAKEOFF Air Conditioning & Press.......... CHECK APU................AS REQUIRED Slat/Flap..............UP Select slat/flap to up following the ideal flap selection speed reference (F) indication. Altimeters..............SET & X-CHECK CPDLC..............AS REQUIRED DESCENT Approach Briefing ............
  • Page 428 AIRPLANE SUPPLEMENT 12 CPDLC FLIGHT MANUAL EMERGENCY AND ABNORMAL PROCEDURES Emergency and abnormal procedures presented in the basic AFM and applicable supplements remain unchanged. S12-10 ANAC APPROVED Page 2 code 01 REVISION 10...
  • Page 429 AIRPLANE SUPPLEMENT 12 FLIGHT CPDLC MANUAL PERFORMANCE Performance presented in the basic AFM and applicable supplements remain unchanged. S12-15 ANAC APPROVED Page 1 code 01 REVISION 10...
  • Page 430 AIRPLANE SUPPLEMENT 12 CPDLC FLIGHT MANUAL INTENTIONALLY BLANK S12-15 ANAC APPROVED Page 2 code 01 REVISION 10...
  • Page 431 Normal Procedures............S13-10 ..01 Before Start..............S13-10 ..01 Emergency and Abnormal Procedures......S13-10 ..01 Performance ..............S13-10 ..01 S13-00 ANAC APPROVED code 01 Page 1 REVISION 12 Copyright © by Embraer. Refer to cover page for details.
  • Page 432 FLIGHT FUELS OPERATION MANUAL GENERAL This supplement provides information required for EMBRAER 190 and EMBRAER 195 airplanes operation with Russian and Ukrainian fuel grades. The information herein presented must replace or complement the equivalent information in the basic AFM. This supplement is only valid when the airplanes are fueled with Russian (TS-1 Regular, TS-1 Premium and RT) or Ukrainian (TS-1 and RT) fuel grades.
  • Page 433 SUPPLEMENT 13 AIRPLANE EASTERN EUROPE FLIGHT FUELS OPERATION MANUAL LIMITATIONS FUEL SPECIFICATION Russian Specification ........... GOST 10227- 86 RT, TS-1 Premium TS-1 Regular Ukrainian Specification ..........GSTU 320.00149943. 011 TS-1 and GSTU 320.00149943. 007 RT FUEL TANK TEMPERATURE Minimum ............... -37°C Maximum ..............
  • Page 434 SUPPLEMENT 13 AIRPLANE EASTERN EUROPE FLIGHT FUELS OPERATION MANUAL INTENTIONALLY BLANK S13-05 ANAC APPROVED Page 2 code 01 REVISION 11...
  • Page 435: Before Start

    SUPPLEMENT 13 AIRPLANE EASTERN EUROPE FLIGHT FUELS OPERATION MANUAL NORMAL PROCEDURES BEFORE START Fuel Tank Temperature ..........CHECK EMERGENCY AND ABNORMAL PROCEDURES The Emergency and Abnormal procedures of the basic AFM remain unchanged. PERFORMANCE The performance section of the basic AFM remains unchanged. S13-10 ANAC APPROVED code 01...
  • Page 436 SUPPLEMENT 13 AIRPLANE EASTERN EUROPE FLIGHT FUELS OPERATION MANUAL INTENTIONALLY BLANK S13-10 ANAC APPROVED Page 2 code 01 REVISION 11...
  • Page 437 Emergency and Abnormal Procedures......S14-10 ..02 Performance ..............S14-15 ..01 Takeoff and Landing Runway Conditions ..... S14-15 ..01 S14-00 ANAC APPROVED code 01 Page 1 REVISION 12 Copyright © by Embraer. Refer to cover page for details.
  • Page 438 SUPPLEMENT 14 AIRPLANE TAKEOFF AND LANDING FLIGHT OPERATIONS BELOW MANUAL -40°C DOWN TO -45°C INTENTIONALLY BLANK S14-00 ANAC APPROVED Page 2 code 01 REVISION 12 Copyright © by Embraer. Refer to cover page for details.
  • Page 439 -40°C DOWN TO -45°C GENERAL INTRODUCTION This Supplement provides information to EMBRAER 190 except ECJ and EMBRAER 195 airplanes to perform takeoff and landing operations below -40°C down to -45°C. The information herein presented replaces or complements the equivalent data in the basic AFM and applicable supplements.
  • Page 440 AFM and applicable supplements. For limitations, procedures and performance information not contained in this Supplement refer to the basic AFM and applicable Supplements. S14-00 ANAC APPROVED code 01 Page 3 REVISION 12 Copyright © by Embraer. Refer to cover page for details.
  • Page 441 SUPPLEMENT 14 AIRPLANE TAKEOFF AND LANDING FLIGHT OPERATIONS BELOW MANUAL -40°C DOWN TO -45°C INTENTIONALLY BLANK S14-00 ANAC APPROVED Page 4 code 01 REVISION 12 Copyright © by Embraer. Refer to cover page for details.
  • Page 442: Operational Limitations

    -45°C. NOTE: In the event of a landing below -45°C, the airplane may not takeoff without further maintenance inspection. S14-05 ANAC APPROVED code 01 Page 1 REVISION 12 Copyright © by Embraer. Refer to cover page for details.
  • Page 443 SUPPLEMENT 14 AIRPLANE TAKEOFF AND LANDING FLIGHT OPERATIONS BELOW MANUAL -40°C DOWN TO -45°C INTENTIONALLY BLANK S14-05 ANAC APPROVED Page 2 code 01 REVISION 12 Copyright © by Embraer. Refer to cover page for details.
  • Page 444: After Start

    At TOD, if the temperature at destination airport is lower than -40°C: Ice Protection Mode Selector ........ON AFTER LANDING Ice Protection Mode Selector ........AUTO S14-10 ANAC APPROVED Page 1 code 01 TEMPORARY REVISION 12.3 Copyright © by Embraer. Refer to cover page for details.
  • Page 445: Descent

    At TOD, if the temperature at destination airport is lower than -40°C: Ice Protection Mode Selector........ON AFTER LANDING Ice Protection Mode Selector........AUTO S14-10 ANAC APPROVED code 01 Page 1 REVISION 12 Copyright © by Embraer. Refer to cover page for details.
  • Page 446 OPERATIONS BELOW MANUAL -40°C DOWN TO -45°C EMERGENCY AND ABNORMAL PROCEDURES Emergency and Abnormal Procedures presented in the basic AFM remain unchanged. S14-10 ANAC APPROVED Page 2 code 01 REVISION 12 Copyright © by Embraer. Refer to cover page for details.
  • Page 447: Performance

    TAKEOFF AND LANDING RUNWAY CONDITIONS Operations below -40°C down to -45°C are limited to dry, wet, dry snow, and compacted snow runways surface condition. S14-15 ANAC APPROVED code 01 Page 1 REVISION 12 Copyright © by Embraer. Refer to cover page for details.
  • Page 448 SUPPLEMENT 14 AIRPLANE TAKEOFF AND LANDING FLIGHT OPERATIONS BELOW MANUAL -40°C DOWN TO -45°C INTENTIONALLY BLANK S14-15 ANAC APPROVED Page 2 code 01 REVISION 12 Copyright © by Embraer. Refer to cover page for details.
  • Page 449 APPENDICES AIRPLANE FLIGHT MANUAL APPENDICES TABLE OF CONTENTS APPENDIX 1 – CONFIGURATION DEVIATION LIST APPENDIX 2 – NOT APPLICABLE AP-TOC ANAC APPROVED code 02 Page 1 REVISION 1...
  • Page 450 APPENDICES AIRPLANE FLIGHT MANUAL INTENTIONALLY BLANK AP-TOC CTA APPROVED Page 2 code 02 ORIGINAL...
  • Page 451 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 12 Copyright © by Embraer. Refer to cover page for details.
  • Page 452 APPENDIX 1 AIRPLANE CONFIGURATION FLIGHT DEVIATION LIST MANUAL INTENTIONALLY BLANK AP1-00 ANAC APPROVED Page 2 code 01 REVISION 12 Copyright © by Embraer. Refer to cover page for details.
  • Page 453 100 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 12 Copyright © by Embraer. Refer to cover page for details.
  • Page 454: Component Location

    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 12 Copyright © by Embraer. Refer to cover page for details.
  • Page 455 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 36 26 A maximum of 10 (ten) static dischargers may be missing with no penalty.
  • Page 456 APPENDIX 1 AIRPLANE CONFIGURATION FLIGHT DEVIATION LIST MANUAL INTENTIONALLY BLANK AP1-23 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 457 AIRPLANE APPENDIX 1 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 458 APPENDIX 1 AIRPLANE CONFIGURATION FLIGHT DEVIATION LIST MANUAL INTENTIONALLY BLANK AP1-28 ANAC APPROVED Page 2 code 01 REVISION 1...
  • Page 459: Landing Gear

    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 12 Copyright © by Embraer. Refer to cover page for details.
  • Page 460 APPENDIX 1 AIRPLANE CONFIGURATION FLIGHT DEVIATION LIST MANUAL INTENTIONALLY BLANK AP1-32 ANAC APPROVED Page 2 code 01 REVISION 12 Copyright © by Embraer. Refer to cover page for details.
  • Page 461 LED lights type) a) Cavity is covered with speed tape, and b) Affected light is deactivated and considered inoperative. Refer to MMEL 33-44-00. AP1-33 ANAC APPROVED code 01 Page 1 REVISION 12 Copyright © by Embraer. Refer to cover page for details.
  • Page 462 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 12 Copyright © by Embraer. Refer to cover page for details.
  • Page 463 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 12 Copyright © by Embraer. Refer to cover page for details.
  • Page 464 APPENDIX 1 AIRPLANE CONFIGURATION FLIGHT DEVIATION LIST MANUAL INTENTIONALLY BLANK AP1-34 ANAC APPROVED Page 2 code 01 REVISION 12 Copyright © by Embraer. Refer to cover page for details.
  • Page 465: Water And Waste

    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 12 Copyright © by Embraer. Refer to cover page for details.
  • Page 466 APPENDIX 1 AIRPLANE CONFIGURATION FLIGHT DEVIATION LIST MANUAL INTENTIONALLY BLANK AP1-38 ANAC APPROVED Page 2 code 01 REVISION 12 Copyright © by Embraer. Refer to cover page for details.
  • Page 467 AIRPLANE APPENDIX 1 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 10-01 Door Deflectors 2 One door deflector from each (Passenger and fuselage side may be missing Service)
  • Page 468 APPENDIX 1 AIRPLANE CONFIGURATION FLIGHT DEVIATION LIST MANUAL INTENTIONALLY BLANK AP1-52 CTA APPROVED Page 2 code 01 ORIGINAL...
  • Page 469 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 53 FUSELAGE 03-01 Forward Ramp 0 May be missing with no penalty Handset, Steering provided: Disconnect Switch and...
  • Page 470 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 53 FUSELAGE 03-05 Hydraulic System 3 0 May be missing with no penalty. Ground Connector, Cover the cavity with speed Hydraulic Pressure...
  • Page 471 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 53 FUSELAGE 04-05 Ecological Bottles 1 One may be missing with Inspection and negligible penalty.
  • Page 472 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 53 FUSELAGE 05-02 APU Compartment 0 May be missing with negligible Drain (Gravity Drain) penalty provided APU is not operated in flight.
  • Page 473 54 NACELLES / PYLONS 50-01 Pylon Side Fairing Any number or combination Seals may be missing or partially missing with negligible penalty. AP1-54 ANAC APPROVED code 01 Page 1 REVISION 12 Copyright © by Embraer. Refer to cover page for details.
  • Page 474 APPENDIX 1 AIRPLANE CONFIGURATION FLIGHT DEVIATION LIST MANUAL INTENTIONALLY BLANK AP1-54 ANAC APPROVED Page 2 code 01 REVISION 12 Copyright © by Embraer. Refer to cover page for details.
  • Page 475 - Avoid deicing anti-icing fluid application directly to the cavity when speed tape is not applied. AP1-55 ANAC APPROVED code 01 Page 1 REVISION 12 Copyright © by Embraer. Refer to cover page for details.
  • Page 476 24-01 Elevator Root Fairing One or two seals may be Seal partially or totally missing with negligible penalty. AP1-55 ANAC APPROVED Page 2 code 01 REVISION 12 Copyright © by Embraer. Refer to cover page for details.
  • Page 477 - 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 12 Copyright © by Embraer. Refer to cover page for details.
  • Page 478 APPENDIX 1 AIRPLANE CONFIGURATION FLIGHT DEVIATION LIST MANUAL INTENTIONALLY BLANK AP1-55 ANAC APPROVED Page 4 code 01 REVISION 12 Copyright © by Embraer. Refer to cover page for details.
  • Page 479 0 Any number or combination Seals (Inboard and may be missing or partially Outboard Canoe Flap missing in any position with Seals) negligible penalty. AP1-57 ANAC APPROVED code 01 Page 1 REVISION 12 Copyright © by Embraer. Refer to cover page for details.
  • Page 480 53-01 Wing Root-Inboard 0 Any number or combination Flap Seal may be missing or partially missing in any position with negligible penalty. AP1-57 ANAC APPROVED Page 2 code 01 REVISION 12 Copyright © by Embraer. Refer to cover page for details.
  • Page 481 AIRPLANE APPENDIX 1 CONFIGURATION FLIGHT DEVIATION LIST MANUAL CONFIGURATION DEVIATION LIST System & 2. Number installed Sequence ITEM 3. Number required for dispatch Number 4. Remarks and/or exceptions 71 POWERPLANT 1 One may be missing with 11-01 Inboard Nacelle negligible penalty provided Strakes...
  • Page 482 APPENDIX 1 AIRPLANE CONFIGURATION FLIGHT DEVIATION LIST MANUAL INTENTIONALLY BLANK AP1-71 ANAC APPROVED Page 2 code 01 REVISION 1...
  • Page 483 4. Remarks and/or exceptions 78 EXHAUST 30-01 Thrust Reverser Inhibit 0 Any number or combination Pin Cover Plate may be missing with negligible penalty. AP1-78 ANAC APPROVED code 01 Page 1 REVISION 12 Copyright © by Embraer. Refer to cover page for details.
  • Page 484 APPENDIX 1 AIRPLANE CONFIGURATION FLIGHT DEVIATION LIST MANUAL INTENTIONALLY BLANK AP1-78 ANAC APPROVED Page 2 code 01 REVISION 12 Copyright © by Embraer. Refer to cover page for details.

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