Embraer 175 - User Manual

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Copyright © 2016 by Embraer S.A. All rights reserved.
EMBRAER 170/175
FAA
AIRPLANE FLIGHT MANUAL
Embraer S.A.
THIS MANUAL IS APPROVED IN ACCORDANCE WITH FAR 21.29 FOR
U.S. REGISTERED AIRCRAFT, AND IS APPROVED BY THE CTA ON
BEHALF OF THE FEDERAL AVIATION ADMINISTRATION.
THIS DOCUMENT IS APPLICABLE TO THE FOLLOWING AIRPLANE
MODELS: ERJ 170-100 STD, ERJ 170-100 LR, ERJ 170-100 SE, ERJ 170-
100 SU, ERJ 170-200 STD, ERJ 170-200 LR AND ERJ 170-200 SU.
NOTE: - EMBRAER 170 AND EMBRAER 175 ARE COMMERCIAL
DESIGNATIONS USED IN THIS MANUAL TO REFER TO THE
ERJ 170-100 AND ERJ 170-200 MODELS, RESPECTIVELY.
- SOME MANUAL VERSIONS MAY NOT PRESENT ALL LISTED
MODELS. FOR SPECIFIC CONFIGURATION, REFER TO LEP
APPLICABILITY.
CTA APPROVAL: _______________________
CLAUDIO PASSOS SIMÃO – TEN.-CEL.-ENG.
CHEFE DA DIVISÃO DE HOMOLOGAÇÃO
AERONÁUTICA
DATE:________________________________
REGISTRATION NUMBER:_______________
SERIAL NUMBER:______________________
AFM–1385
CODE 003
FEBRUARY 20, 2004
REVISION 15 – OCTOBER 03, 2016

Summary

EMBRAER 170;175 FAA AIRPLANE FLIGHT MANUAL

SECTION 3 NORMAL PROCEDURES

Internal Safety Inspection

Checklist for internal safety inspection before flight.

Power Up

Procedures for powering up aircraft systems.

External Inspection

Checklist for external safety inspection of the aircraft.

Before Start

Procedures to perform before starting the engines.

Engine Start

Procedures and indications for engine start.

After Start

Procedures to perform after engine start.

Before Takeoff

Checklist and procedures before takeoff.

Takeoff

Procedures for takeoff, including pitch angle guidance.

After Takeoff

Procedures to perform after takeoff.

Descent

Procedures for aircraft descent.

Approach

Procedures to perform during the approach phase.

Before Landing

Procedures to perform before landing.

Go Around

Procedure for performing a go-around.

After Landing

Procedures to perform after landing.

Shutdown

Procedures for shutting down the aircraft.

Leaving the Airplane

Procedures for securing the aircraft before leaving.

Buffet Onset Envelope

Information on buffet onset data from CAFM.

Enhanced;Ground Proximity Warning

Limitations applicable to EGPWS and TCAS.

Windshear Prevention;Recovery

Procedures for windshear prevention and recovery.

Traffic and Collision Avoidance

Procedures for managing traffic and collision avoidance.

Transponder

Checks for transponder status in compliance with airworthiness directives.

Simoperation in Icing Conditions

Procedures for operation in icing conditions.

Turbulent Air Penetration

Procedures for penetrating turbulent air.

SECTION 4 EMERGENCY AND ABNORMAL PROCEDURES

Non-annunciated procedures

Procedures not related to EICAS messages but to conditions.

Emergency Procedures

List of emergency procedures.

DUAL ENGINE FAILURE

ENGINE FIRE, SEVERE DAMAGE OR SEPARATION

FORCED LANDING

Procedure for forced landing.

FUEL LEAK

JAMMED CONTROL COLUMN (PITCH)

JAMMED CONTROL WHEEL (ROLL)

JAMMED RUDDER PEDALS

PITCH TRIM RUNAWAY

REJECTED TAKEOFF

ROLL (YAW) TRIM RUNAWAY

STEERING RUNAWAY

TAKEOFF WITH ENGINE FAILURE AT OR ABOVE V1

ABNORMAL LANDING GEAR EXTENSION

ENGINE ABNORMAL VIBRATION

ENGINE AIRSTART

ENGINE ITT OVERTEMPERATURE

ENGINE SHUTDOWN

GEAR LEVER CAN NOT BE MOVED UP

IMPAIRED OR CRACKED WINDSHIELD

LOSS OF AUXILIARY POWER UNIT INDICATIONS

LOSS OF HYDRAULIC SYSTEM 1

LOSS OF HYDRAULIC SYSTEM 2

LOSS OF HYDRAULIC SYSTEM 1 AND 2

LOSS OF HYDRAULIC SYSTEM 1 AND 3

LOSS OF HYDRAULIC SYSTEM 2 AND 3

LOSS OF PRESSURIZATION INDICATION

ONE ENGINE INOPERATIVE APPROACH AND LANDING

PARTIAL OR GEAR UP LANDING

STRUCTURAL DAMAGE

AIRPLANE GENERAL (DOORS;LIGHTING;CARGO COMPARTMENT)

AMS (PNEUMATICS, AIR CONDITIONING;PRESSURIZATION)

CABIN ALTITUDE HIGH

Procedure for high cabin altitude.

AMS CONTROLLER FAILURE

Procedure for AMS controller failure.

BLEED APU LEAKAGE

Procedure for APU bleed leakage.

BLEED 1 (2) FAILURE

Procedure for bleed 1 or 2 failure.

BLEED 1 (2) LEAKAGE

Procedure for bleed 1 or 2 leakage.

BLEED 1 (2) OVERPRESSURE

Procedure for bleed 1 or 2 overpressure.

CABIN DIFFERENTIAL PRESSURE FAILURE

Procedure for cabin differential pressure failure.

CARGO FORWARD VENTILATION FAILURE

Procedure for cargo forward ventilation failure.

CENTER ELECTRONIC BAY FANS FAILURE

Procedure for center electronic bay fans failure.

FORWARD ELECTRONIC BAY FANS FAILURE

Procedure for forward electronic bay fans failure.

PACK 1 (2) FAILURE

Procedure for pack 1 or 2 failure.

PACK 2 LEAKAGE

Procedure for pack 2 leakage.

PRESSURIZATION AUTO FAILURE

Procedure for pressurization auto failure.

PRESSURIZATION MANUAL FAILURE

Procedure for pressurization manual failure.

RECIRCULATION SMOKE DETECTION FAILURE

Procedure for recirculation smoke detection failure.

AUTOFLIGHT

SHAKER ANTICIPATED

Procedure for shaker anticipated.

STALL PROTECTION FAILURE

Procedure for stall protection failure.

ENGINE

ENGINE 1 (2) FAILURE

Procedure for engine failure.

ENGINE 1 (2) FUEL IMPENDING BYPASS

Procedure for engine fuel impending bypass.

ENGINE 1 (2) FUEL LOW PRESSURE

Procedure for engine fuel low pressure.

ENGINE 1 (2) REVERSER THRUST LEVER ANGLE FAILURE

Procedure for engine reverser thrust lever angle failure.

ENGINE 1 (2) STARTER VALVE OPENED

Procedure for engine starter valve opened.

ENGINE 1 (2) THRUST LEVER ANGLE FAILURE

Procedure for engine thrust lever angle failure.

FIRE PROTECTION

APU FIRE

Procedure for APU fire.

ENGINE 1 (2) FIRE

Procedure for engine 1 or 2 fire.

FLIGHT CONTROLS

ELEVATOR LH (RH) FAILURE

Procedure for elevator left/right failure.

FLAP (SLAT) FAILURE

Procedure for flap/slat failure.

PITCH TRIM FAILURE

Procedure for pitch trim failure.

RUDDER FAILURE

Procedure for rudder failure.

RUDDER LIMITER FAILURE

Procedure for rudder limiter failure.

SPOILER FAULT

Procedure for spoiler fault.

STABILIZER LOCK FAULT

Procedure for stabilizer lock fault.

AILERON RH (LH) FAILURE

Procedure for aileron right/left failure.

FMS;NAV;COM & FLIGHT INSTRUMENTS

SECTION 5 PERFORMANCE

Performance Configuration

Applicable configurations for each performance phase.

SUPPLEMENT 5 CAT II OPERATION

SUPPLEMENT 6 RVSM OPERATION

APPENDICES

CONFIGURATION DEVIATION LIST

List of configuration deviations.

APPENDIX 1 CONFIGURATION DEVIATION LIST

APPENDIX 2 GUIDANCE INFORMATION

Introduction

Introduction to guidance information for EMBRAER 170.

Embraer 175 Specifications

General

Manufacturer	Embraer
Model	175
Length	31.68 m (103 ft 11 in)
Wingspan	26.00 m (85 ft 4 in)
Engine Type	General Electric CF34-8E
Service Ceiling	12, 497 m (41, 000 ft)
Seating Capacity	76-88
Cruise Speed	828 km/h
Maximum Speed	0.82 Mach (871 km/h)
Range	3, 704 km
Thrust per Engine	14, 200 lbf (63 kN)
Maximum Takeoff Weight	38, 790 kg