embraer 19x simulator - aviation for all€¦ · embraer 19x flight simulator training device...

Copyright © 2014

Aviation For All Company

All Rights Reserved

Document Number A2-14001-PTR

July 13, 2011

Revision Number: 06

Revision Date: March 10, 2014

Embraer 19X

Flight Simulator Training

Device

Manual

Embraer 19X Simulator

Manual

Mar 10, 2014 A2-14001-PTR

EMBRAER 19X SIMULATOR

MANUAL

Elaboration:

_______________________________________

LUIZ F FARRET

Endorsement:

_______________________________________

LUIZ F FARRET

Review:

_______________________________________

LUIZ F FARRET


Manual

Mar 10, 2014 A2-14001-PTR

Review

Nº Reviser Date Signature

ORIGINAL - Jul/2011 -

REV-1 L. F. F. Apr/2012

REV-2 L. F. F. Aug/2012

REV-3 L. F. F. Aug/2012

REV-4 L. F. F. Nov/2012

REV-5 L. F. F. May/2013

REV-6 L. F. F. Mar/2014


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Intentionally

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1. Table of Contents

Table of Contents 1.

Preface 2. Model Identification 2.1

Introduction 2.2

Manual Information 2.3

Abbreviations 2.4

Bulletin Record 2.5

Limitations 3. Operating Limitations 3.1

Normal Procedures 4. Power up 4.1

Shutdown 4.2

Supplementary Procedures 5. Non-normal procedures 5.1

Overheat 5.1.1

Electric Failure 5.1.2

Fan Malfunction 5.1.3

Lights Malfunction 5.1.4

Standby Gauges not working 5.1.5

Instrument window wrong size 5.1.6

General Information 6. General Overview 6.1

Peripheral Connections 6.2

Maintenance 7. Hardware 7.1

Software 7.2


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Mar 10, 2014 A2-14001-PTR

2. Preface

2.1 Model Identification

The simulators listed in the table below are covered in this

manual. The table information is used to distinguish data peculiar

to one or more, but not all of the simulators. Where data applies

to all simulators listed, no reference is made to individual

simulators.

Simulator number is supplied by the operator. Serial and

tabulation number are supplied by Aviation For All.

Simulator Number Serial Number Tabulation Number

003 A2-14001-PTR 19X


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Mar 10, 2014 A2-14001-PTR

Preface

2.2 Introduction

This manual has been prepared by the Aviation For All Company.

The purpose of this manual is to:

• provide the necessary operating limitations, procedures,

performance, and systems information the user needs to safely

and efficiently operate the 19X simulator;

• serve as a comprehensive reference for use during training for

the 19X simulator;

• serve as a review guide for use in recurrent training and

proficiency checks in the 19X simulator;

• establish standardized procedures and practices to enhance the

simulator operational philosophy and policy;

This manual is prepared for the owner/operator named on the title

page specifically for the simulators listed in the "Model

Identification" section. It contains operational procedures and

information, which apply only to these simulators. Changes to the

delivered configuration are incorporated when covered by

contractual revision agreements between the owner/operator and

The Aviation For All Company.

This manual is not suitable for use for any simulators not listed in

the "Model Identification" section. Further, it may not be suitable

for simulators that have been transferred to other

owners/operators.

Owners/operators are solely responsible for ensuring the

operational documentation they are using is complete and

matches the current configuration of the listed simulators. This

includes the accuracy and validity of all information furnished by

the owner/operator or any other party. Owners/operators receiving

active revision service are responsible to ensure that any


Manual

Mar 10, 2014 A2-14001-PTR

modifications to the listed simulators are properly reflected in the

operational procedures and information contained in this manual.

The manual is periodically revised to incorporate pertinent

procedural and systems information. Items of a more critical

nature will be incorporated in operational bulletins and distributed

in a timely manner. In all cases, such revisions and changes must

remain compatible with the approved AFM with which the

operator must comply. In the event of conflict with the AFM, the

AFM shall supersede.

This manual is written under the assumption that the user has had

previous multi–engine jet aircraft experience and is familiar with

basic jet airplane systems and basic pilot techniques common to

airplanes of this type. Therefore, the operations manual does not

contain basic flight information that is considered prerequisite

training.

This manual can not be used to real flight or real airplane

operation, it is restricted to be used in the simulators listed on the

“Model Identification” section.

Any questions about the content or use of this manual can be

directed to:

Commercial Aviation Simulators Services

Aviation For All Simulators Group

[email protected]


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Mar 10, 2014 A2-14001-PTR

Preface 2.3 Manual Information

Page Numbering

The manual uses a decimal page numbering system. The page

number is divided into three fields; chapter, section, and page.

Warnings, Cautions, and Notes

The following levels of written advisories are used throughout the

manual.

WARNING: An operating procedure, technique, etc., that

may result in personal injury or loss of life if not carefully

followed.

CAUTION: An operating procedure, technique, etc., that may

result in damage to equipment if not carefully followed.

Operations Manual Configuration

The material in this manual is not customized to a specific

airplane configuration. The user must ascertain that this material

is applicable for the intended use.

Schematic Symbols

Symbols shown are those which may not be identified on

schematic illustrations.


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Preface 2.4 Abbreviations

The following abbreviations may be found throughout the

manual. Some abbreviations may also appear in lowercase letters.

Abbreviations having very limited use are explained in the

chapter where they are used.

ºC . . . . . . . . . .Degree Celsius

ºF . . . . . . . . . .Degree Fahrenheit

ft . . . . . . . . . . .Feet

g . . . . . . . . . . .Gravity Acceleration

h . . . . . . . . . . .Hour

Hz . . . . . . . . . .Hertz

in . . . . . . . . . . .Inches

in.Hg . . . . . . . .Inches of Mercury

kg . . . . . . . . . .Kilogram

km . . . . . . . . . .Kilometer

kt . . . . . . . . . . .Knot

lb . . . . . . . . . . .Pounds

m . . . . . . . . . . .Meter

mb . . . . . . . . . .Millibar

min . . . . . . . . .Minute

mm . . . . . . . . .Millimeter

nm . . . . . . . . . .Nautical Mile

psi . . . . . . . . . .Pound per Square Inch

sec . . . . . . . . .Second

A . . . . . . . . . . .Ampere

A/I . . . . . . . . . .Anti-Ice

ABM . . . . . . . .Auto Brake Control Module

A/C . . . . . . . . .Aircraft

AC . . . . . . . . . .Alternating Current

ACARS . . . . . .Aircraft Communication

Addressing and Reporting System

ACE . . . . . . . .Actuator Control Electronics

ACMP . . . . . . .AC Motor Pump

ACP . . . . . . . .Audio Control Panel

ACT . . . . . . . . .Altitude Compensated Tilt

ADA . . . . . . . .Air Data Application

ADC . . . . . . . .Air Data Computer

ADF . . . . . . . . .Automatic Direction Finder

ADI . . . . . . . . .Altitude Direction Indication

ADS . . . . . . . .Air Data System

ADS-B . . . . . . .Automatic Dependence

Surveillance Broadcast

ADSP . . . . . . .Air Data Smart Probe

AFCS . . . . . . .Automatic Flight Control System

AFE . . . . . . . . .Above Field Elevation

AFM . . . . . . . .Airplane Flight Manual

AFU . . . . . . . . .Artificial Feel Unit

AGB . . . . . . . .Accessory Gear Box

AGL . . . . . . . . .Above Ground Level

AICC . . . . . . .Auxiliary Integrated Control Center

AH . . . . . . . . . .Alert Height

AIL . . . . . . . . .Aileron

ALT .................Altitude

AM . . . . . . . . . Amplitude Modulation

AMM . . . . . . . . Aircraft Maintenance Manual

AMS . . . . . . . . Air Management System

ANR . . . . . . .Automatic Navigation Realignment

AOA . . . . . . . . .Angle of Attack

AOC . . . . . .Airline Operational Communications

AOM . . . . . . . . .Airplane Operations Manual

AP . . . . . . . . . .Autopilot

APM . . . . . . . . .Aircraft Personality Module

APPR . . . . . . . .Approach

APU . . . . . . . . .Auxiliary Power Unit

ASCB . . . .Avionics Standard Communication Bus

ASEL . . . . . . . .Altitude Select

ASTM . . . . .American Society of Testing Material

AT . . . . . . . . . . .Auto Throttle

ATC . . . . . . . . .Air Traffic Control

ATIS .. . .Automatic Terminal Information Service

ATS . . . .Air Turbine Starter, Air Traffic Services

ATT . . . . . . . . .Attitude

ATTCS . . . . . . .Automatic Takeoff Thrust Control

System

ATTND . . . . . . .Attendant

AZFW . . . . . . . .Actual Zero Fuel Weight

AUTO . . . . . . . .Automatic

AUX . . . . . . . . .Auxiliary

AVAIL . . . . . . . .Available

AVNX . . . . . . . .Avionics

BATT . . . . . . . .Battery

BC . . . . . . . . . .Back Course

BCM . . . . . . . . .Brake Control Module

BCN . . . . . . . . .Beacon

BEW . . . . . . . . .Basic Empty Weight

BFO . . . . . . . . .Beat Frequency Oscillator

BIT . . . . . . . . . .Built-In Test

BRG . . . . . . . . .Bearing

BRT . . . . . . . . .Bright

BTC . . . . . . . . .Bus Tie Contactor

BTL . . . . . . . . .Bottle


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CAB . . . . . . . . .Cabin

CAN . . . . . . . . .Controller Area Network

CAS . . . . . . . . .Calibrated Airspeed, Crew

Alerting System

CB . . . . . . . . . .Circuit Breaker

CCD . . . . . . . . .Cursor Control Device

CDL . . . . . . . . .Configuration Deviation List

CFIT . . . . . . . . .Controlled Flight Into Terrain

CG . . . . . . . . . .Center of Gravity

CGD . . . . . . . . .Corrected Ground Distance

CHR . . . . . . . . Chronometer

CKPT . . . . . . . Cockpit

CLB . . . . . . . . Climb

CLK . . . . . . . . Clock

CLR . . . . . . . . Clear

CMC . . . . . . Central Maintenance Computer

CMD . . . . . . . .Command

CMF . .Communication Management Function

CMS. . . . .Configuration Management System

COMM . . . . . .Communication

CON . . . . . . . .Continuous

CONN . . . . . . .Connection

CPC . . . . . . . .Cabin Pressure Controller

CPCS . . . . . .Cabin Pressure Control System

CRFL . . . . . . .Cruise Flight Level

CRG . . . . . . . .Cargo

CRZ . . . . . . . .Cruise

CSS. . . . . . . . .Cabin Surveillance System

CTRL . . . . . . .Control

CVR . . . . . . . .Cockpit Voice Recorder

DC . . . . . . . . . .Direct Current

DCTC . . . . . . .Direct Current Tie Contactor

DDPM . . . . . . .Dispatch Deviation Procedures

Manual

DET . . . . . . . . .Detector

DGRAD . . . . . .Degraded

DH . . . . . . . . . .Decision Height

DISC . . . . . . . .Disconnect

DIM . . . . . . . . .Dimmer

DLK . . . . . . . . .Datalink

DME . . . . . . . .Distance Measuring Equipment

DMU . . . . . . . .Data Management Unit

DN . . . . . . . . . .Down

DOW . . . . . . . .Dry Operating Weight

DR . . . . . . . . . .Dead Reckoning

DU . . . . . . . . . .Display Unit

DVDR . . . . . . .Digital Voice and Data Recorder

EADI . . . . . Electronic Attitude Director Indicator

E-BAY . . . . . . . Electronic Bay

EBV . . . . . . . . . Engine Bleed Valve

ECS . . . . . . . . Environmental Control System

EDP . . . . . . . . Engine Driven Pump

EDS . . . . . . . . Electronic Distribution System

EEW . . . . . . . . Equipped Empty Weight

EFB . . . . . . . . . Electronic Flight Bag

EGPWM . . . . . Enhanced Ground Proximity

Warning Module

EGPWS . . . . . Enhanced Ground Proximity

Warning System

EGT . . . . . . . . Exhaust Gas Temperature

EHSI. . . Electronic Horizontal Situation Indicator

EICAS . . . . . . . Engine Indication and Crew

Alerting System

EICC . . . .. . Emergency Integrated Control Circuit

ELEC . . . . . . . Electrical

ELEV . . . . . . . . Elevator

ELPU . . . . . . . Emergency Lights Power Unit

ELT . . . . . . . . . Emergency Locator Transmitter

EMER . . . . . . . Emergency

ENG . . . . . . . . Engine

EOAH . . . . . . . Engine Out Acceleration Height

EPOP . . . . Embraer Portable Operational Package

ET . . . . . . . . . Elapsed Time

ETC . . . . . . . . Essential Tie Contactor

EXT . . . . . . . . Extension

FADEC . . . Full Authority Digital Engine Control

FAP . . . . . . . . Flight Attendant Panel

FAR . . . . . . . . .Federal Aviation Regulation

FBW . . . . . . . . .Fly by Wire

FCM . . . . . . . . .Flight Control Module

FCOC . . . . . . . .Fuel Cooled Oil Cooler

FCU . . . . . . . . .Fuel Conditioning Unit, Flight

Control Unit

FCV. . . . . . . . . .Flow Control Valve

FD . . . . . . . . . .Flight Director

FDR . . . . . . . . .Flight Data Recorder

FGCS . . . . . . . .Flight Guidance Control System

FLCH . . . . . . . .Flight Level Change

FLEX . . . . . . . .Flexible

FMA . . . . . . . . .Flight Mode Annunciator

FMS . . . . . . . . .Flight Management System

FMU . . . . . . . . .Fuel Metering Unit

FOQA . . . . .Flight Operational Quality Assurance

FPA . . . . . . . . .Flight Path Angle

FPL . . . . . . . . .Flight Plan

FPR . . . . . . . . .Flight Path Reference

FPV . . . . . . . . .Flight Path Vector

FSBY OVRD . . . . .Forced Standby Override

FSTN . . . . . . . .Fasten

FWD . . . . . . . . .Forward


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Mar 10, 2014 A2-14001-PTR

GA . . . . . . . . . Go-Around

GCU . . . . . . . . Generator Control Unit

GD . . . . . . . . . Ground Distance

GEN . . . . . . . . Generator

GMAP . . . . . . Ground Mapping

GMT . . . . . . . . Greenwich Mean Time

GND . . . . . . . . Ground

GP . . . . . . . . . Guidance Panel, Glide Path

GPS . . . . . . . . Global Positioning System

GPU . . . . . . . . Ground Power Unit

G/S . . . . . . . . . Glide Slope

GS . . . . . . . . . Ground Speed

HDG . . . . . . . . Heading

HDPH . . . . . . . Headphone

HF . . . . . . . . . High Frequency

HGS . . . . . . . . Heads-Up Guidance System

HI . . . . . . . . . . High

HP . . . . . . . . . High Pressure

HPT . . . . . . . . High Pressure Turbine

HSA . . . . . . . . Horizontal Stabilizer Actuator

HS-ACE . . . . . Horizontal Stabilizer Actuator

Controls Electronics

HSI . . . . . . . . . Horizontal Situation Indicator

HUD. . . . . . . . . Heads-Up Display

IAS . . . . . . . . . Indicated Airspeed

IATA . . . . International Air Transport Association

IAW . . . . . . . . . In Accordance With

ICAO . . .International Civil Aviation Organization

ICC . . . . . . . . . Integrated Control Center

ID . . . . . . . . . . Identification

IDG . . . . . . . . . Integrated Drive Generator

IESS . . . . . Integrated Electronic Standby System

IFE. . . . . . . . . . In-Flight Entertainment

IFR . . . . . . . . . Instrument Flight Rules

IGN . . . . . . . . . Ignition

ILS . . . . . . . . . Instrument Landing System

INBD . . . . . . . . Inboard

INHIB . . . . . . . Inhibition / Inhibited

INOP . . . . . . . . Inoperative

INPH . . . . . . . . Interphone

INSP . . . . . . . . Inspection

INT . . . . . . . . . Initialization

I/O . . . . . . . . . . Input/Output

IRS . . . . . . . . .Inertial Reference System

ISA . . . . . . . . .International Standard Atmosphere

ITT . . . . . . . . .Interturbine Temperature

KCAS . . . . . . .Calibrated Airspeed in Knots

kHz . . . . . . . . .Kilohertz

KIAS . . . . . . . .Indicated Airspeed in Knots

KPH . . . . . . . .Kilograms per Hour

LAV . . . . . . . . .Lavatory

LCD . . . . . . . . .Liquid Crystal Display

LEMAC…..Leading Edge Mean Aerodynamic

Chord

LFE . . . . . . . . .Landing Field Elevation

LG . . . . . . . . . .Landing Gear

LH . . . . . . . . . .Left Hand

LICC . . . . . . . .Left Integrated Control Circuit

LIM . . . . . . . . .Limited Thrust

LNAV . . . . . . . .Lateral Navigation

LOC . . . . . . . .Localizer

LOGO . . . . . . .Logotype

LP . . . . . . . . . .Low Pressure

LPT . . . . . . . . .Low Pressure Turbine

LRC . . . . . . . . .Long Range Cruise

LRM . . . . . . . .Line Replaceable Module

LRU . . . . . . . . .Line Replaceable Unit

LSK . . . . . . . . .Line Select Key

LSS . . . . . . . . .Lighting Sensor System

LT . . . . . . . . . .Light

LVDT . . .Linear Variable Differential Transducer

LVTO. . . . . . . . Low-Visibility Takeoff

LX . . . . . . . . . . Lightning Detection

M . . . . . . . . . . Mach

MAC . . . . . . . . Mean Aerodynamic Chord

MAN . . . . . . . . Manual

MAU . . . . . . . . Modular Avionics Unit

MAX . . . . . . . . Maximum

MaxAT . . . . . . Maximum Assumed Temperature

MB . . . . . . . . . Marker Beacon

MCDU . . . . . . Multifunction Control Display Unit

MDA . . . . . . . . Minimum Descent Altitude

MEA . . . . . . . . Minimum Enroute Altitude

MEW . . . . . . . Manufacturer Empty Weight

MFD . . . . . . . . Multifunction Display

MFP . . . . . . . . Multifunction Probe

MGT . . . . . . . . Management

MHz . . . . . . . . Megahertz

MIN . . . . . . . . Minimum, minutes

MinAT . . . . . . . Minimum Assumed Temperature

MKR . . . . . . . . Marker

MLG . . . . . . . . Main Landing Gear

MLS . . . . . . . . Microwave Landing System

MLW . . . . . . .Maximum Design Landing Weight

MMEL . . . . . . . Master Minimum Equipment List

MMO . . . . . . . Maximum Operating Mach

MOW . . . . . .Maximum Design Operating Weight

MPP . . . . . Maintenance Practices and Procedures

MRC . . . . . . . . Modular Radio Cabinet

MRW . . . . . . . Maximum Design Ramp Weight

MSA . . . . . . . . Minimum Safety Altitude

MTOW . . . . . . Maximum Design Takeoff Weight

MZFW . . . . . Maximum Design Zero Fuel Weight


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N1 . . . . . . . . . Fan Speed

N2 . . . . . . . . . High-Pressure-Rotor Shaft Speed

NAT. . . . . . . . . North Atlantic

NAV . . . . . . . . Navigation

NBPT . . . . . . . No Break Power Transfer

NLT. . . . . . . . . No(t) Later Than

NM . . . . . . . . . Nautical Miles

NOTAM . . . . . Notice to Airman

NPRV . . . . . . . Negative Pressure Relief Valve

OAT . . . . . . . . Outside Air Temperature

OBV . . . . . . . . Operating Bleed Valve

ODS . . . . . . . . Overheat Detection System

OEI . . . . . . . . . One Engine Inoperative

OET. . . . . . . . . One Engine Taxi

OEW . . . . . . . Operating Empty Weight

OFV . . . . . . . . Outflow Valve

OGV . . . . . . . . Outlet Guide Vane

OUTBD . . . . . Outboard

OVHT . . . . . . . .Overheating

OVRD . . . . . . . Override

OVSP . . . . . . . Overspeed

OXY . . . . . . . . Oxygen

PA . . . . . . . . . . Passenger Address

P-ACE . . . . . . . Primary Actuator Controls

Electronics

PAX . . . . . . . . . Passenger

PBE . . . . . . . . . Protective Breathing Equipment

PCU . . . . . . . . Power Control Unit

PDU . . . . . . . . Power Drive Unit

PERF . . . . . . . Performance

PF . . . . . . . . . . Pilot Flying

PFD . . . . . . . . . Primary Flight Display

PLI . . . . . . . . . Pitch Limit Indicator

PMA . . . . . . . . Permanent Magnet Alternator

PPH . . . . . . . . Pounds per Hour

PRESN . . . . . . Pressurization

PRESS . . . . . . Pressure

PROX . . . . . . . Proximity

PSEM . . . . . Proximity Sensor Electronic Module

PSI . . . . . . . . . Pounds per Sq. Inch

PSU . . . . . . . . Passenger Service Unit

PTU . . . . . . . . . Power Transfer Unit

PTT . . . . . . . . . Press-To-Talk

PUV . . . . . . . . Pump Unloader Valve

PV . . . . . . . . . . Priority Valve

PWR . . . . . . . . Power

QFE . . . . . . . . Field Elevation

QNE . . . . . . . . Normal Elevation

QNH. . . . . . . . . Normal Height

QRC. . . . . . . . . Quick Reference Checklist

QRH . . . . . . . . Quick Reference Handbook

QTY. . . . . . . . . Quantity

RA . . . . . . . . . . Radio Altimeter

RAIM . . . . . . . . Receiver Autonomous Integrity

Monitoring

RAR . . . . . . . . Radio Altimeter Receiver

RAT . . . . . . . . . Ram Air Turbine

REACT . . . . . . Rain Echo Attenuation

Compensation Technique

RECIRC . . . . . Recirculation

REF . . . . . . . . . Reference

REV . . . . . . . . Reverse

RH . . . . . . . . . . Right Hand

RICC . . . . . . . . Right Integrated Control Center

RLY . . . . . . . . . Relay

RNAV. . . . . . . . Area Navigation

RON. . . . . . . . . Remaining Overnight

RPM . . . . . . . . Revolution Per Minute

RSV . . . . . . . . Reserve

RTA . . . . . . . . .Receiver/Transmitter/Antenna

RTO. . . . . . . . . Rejected Takeoff

RVSM . . .Reduced Vertical Separation Minimum

SAD . . . . . . . . Still Air Distance

SAT . . . . . . . . Static Air Temperature

SCV . . . . . . . . Starter Control Valve

SEC . . . . . . . . Seconds

SELCAL . . . . . Selective Call

SERV . . . . . . . Service

SF-ACE . . .Slat/Flap Actuator Control Electronics

SL . . . . . . . . . . Sea Level

SLD . . . . . . . . Supercooled Large Droplets

SMK . . . . . . . . Smoke

SMKG . . . . . . Smoking

SMPL . . . . . . . Sample

SOV . . . . . . . . Shutoff Valve

SPDA . . . . . . . Secondary Power Distribution

Assembly

SPDE . . . . . . . Speed on Elevator

SPDT . . . . . . . Speed on Thrust

SPKR . . . . . . . Speaker

SPLT . . . . . . . Split

SPS . . . . . . . . Stall Protection System

SRC . . . . . . . . Source

SSPC . . . . . . . Solid State Power Controller

STAB . . . . . . . Stabilizer

STBY . . . . . . . Stand By

SVC . . . . . . . . Service

SW . . . . . . . . . Switch


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T/O . . . . . . . . . Takeoff

TA/RA . . .Traffic Advisory/ Resolution Advisory

TAS . . . . . . . . True Airspeed

TAT . . . . . . . . . Total Air Temperature

TCAS. . . Traffic and Collision Avoidance System

TCF . . . . . . . . Terrain Clearance Floor

THR. . . . . . . . . Threshold

TCS . . . . . . . . Touch Control Steering

TDR . . . . . . . . Transponder

TDS . . . . . . . . Takeoff Data Set

TEMP . . . . . . . Temperature

TERR . . . . . . . Terrain

TGT . . . . . . . . Target

THR . . . . . . . . Thrust

TK SEL . . . . . . Tank Selector

TLA . . . . . . . . Thrust Lever Angle

TMS. . . . Thrust Management System TO Takeoff

TOD . . . . . . . . Top of Descent

TO/GA . . . . . . Takeoff/Go-Around

TORA . . . . . . . Takeoff Runway Available

TR . . . . . . . . . Thrust Reverser

TRK. . . . . . . . . Track Mode

TRS . . . . . . . . Thrust Rating Selection

TRU . . . . . . . . Transformer Rectifier Unit

TWIP . . .Terminal Weather Information for Pilots

UNLK . . . . . . .Unlock

UTC . . . . . . . .Universal Time

V . . . . . . . . . . .Volt

V1 . . . . . . . . . .Takeoff Decision Speed

V2 . . . . . . . . . .Takeoff Safety Speed

VA . . . . . . . . . .Volt-Ampere

VA . . . . . . . . . .Design Maneuvering Speed

VAC . . . . . . . . .Approach Climb Speed

VALT . . . . . . . .VNAV altitude hold mode

VAP . . . . . . . . .Approach Speed

VASEL. . . . . . .VNAV altitude capture

VDP. . . . . . . . .Visual Descent Point

VDR . . . . . . . .VHF Digital Radio

VEF . . . . . . . . .Critical Engine Failure Speed

VFE . . . . . . . . .Maximum Flaps Extended Speed

VFS . . . . . . . . .Final Segment Speed

VFR . . . . . . . . .Visual Flight Rules

VFR . . . . . . . . .Flaps Retraction Speed

VHF . . . . . . . . .Very High Frequency

VLE . . .Maximum Landing Gear Extended Speed

VLF . . . . . . . . .Very Low Frequency

VLO . . . . . . . . .Maximum Landing Gear

Operating Speed

VLOF . . . . . . . Lift-Off Speed

VLV . . . . . . . . . Valve

VMBE . . . . . . . Maximum Brake Energy Speed

VMCA . . . . . . . Air Minimum Control Speed

VMCG . . . . . . . Minimum Control Speed Ground

VMCL . . . . . . . Minimum Control Speed Landing

VMO . . . . . . . . Maximum Operating Speed

VMU . . . . . . . . Minimum Unstick Speed

VNAV . . . . . . . Vertical Navigation

VOR . . . . . . . . VHF Omnidirectional Range

VPATH. . . . . . . VNAV vertical path mode

VR . . . . . . . . . . Rotation Speed

VREF . . . . . . . Reference Speed

VREFXX . . . . . Landing Reference Speed

associated with the flap setting of XX

VS . . . . . . . . . . Vertical Speed

VS . . . . . . . . . . Stall Speed

VTA . . . . . . . . . Vertical Track Alert

WX . . . . . . . . . Weather

WHCU . . . . . . .Windshield Heating Control Unit

WML . . . . . . . .Windmilling

WOW . . . . . . .Weight on Wheels

WRN . . . . . . . .Warning

WSHR . . . . . . .Windshear

XBLEED . . . . .Cross Bleed

XCHECK . . . . .Cross Check

XFEED . . . . . . Cross Feed

XPDR . . . . . . . Transponder

YD . . . . . . . . . Yaw Damper


Manual

Mar 10, 2014 A2-14001-PTR

Preface 2.5 Bulletin Record

The Aviation For All Company issues operations manual bulletins

as required. Bulletins transmit temporary information which must

be issued before the next formal revision to the manual or

information of interest to all operators.

Bulletins are numbered sequentially for each operator. Each new

bulletin is recorded in this record when received and filed as

instructed. A bulletin may not apply to all simulator models. Each

bulletin specifically identifies the simulator effectivity. When

appropriate, the next formal manual revision will include an

updated bulletin record page.

Temporary information is normally incorporated into the manual

at the next formal revision. When the condition remains

temporary after a bulletin incorporation, the temporary paragraphs

are identified by a heading referencing the originating bulletin.

When the temporary condition no longer exists, the bulletin is

cancelled and the original manual content is restored.

Bulletin status is defined as follows:

• In Effect (IE) - the bulletin contains pertinent information not

otherwise covered in the manual. The bulletin is recorded in this

record and filed as instructed. The bulletin is active and should be

retained in the manual.

• Incorporated (INC) - the bulletin material is incorporated into

the manual pages. The bulletin remains in effect.

• Cancelled (CANC) - the bulletin is no longer in effect. File the

bulletin as instructed and remove it from this section of the

manual. The record page should be modified to indicate the

CANC bulletin status.

The record below should be accomplished by the person revising

the material.


Manual

Mar 10, 2014 A2-14001-PTR

Nº Subject Ref. Nº Date Status


Manual

Mar 10, 2014 A2-14001-PTR

Intentionally

Blank


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Mar 10, 2014 A2-14001-PTR

3. Limitations 3.1 Operating Limitations

This chapter contains the simulator limitations and recommended

operating limitations. Limitations that are obvious, shown on

displays or placards, or incorporated within an operating

procedure are not contained in this chapter.

Before the initialization of the simulator verify that the following

conditions are within tolerance.

CAUTION: Operating the simulator in other conditions not

listed below or not within tolerance may cause malfunctions

and or damage to the simulator system.

Temperature

The operating temperature range for the simulators covered by

this manual is from +5°C to +30°C. Negative temperature

operations are not allowed.

Humidity

The simulator should not be operated in high humidity conditions.

It is strictly prohibited to energize the simulator systems under

humidity condensation conditions.

Gases

It is strictly prohibited to energize the simulator systems under

flammable gases or liquids condition.

WARNING: Energizing the simulator under the conditions

above listed may result in personal injury or loss of life.


Manual

Mar 10, 2014 A2-14001-PTR

Electrical Power

The simulators listed in this manual require a DC power supply of

12VDC 2A.

CAUTION: Operating the simulator in other current

conditions not listed may cause malfunctions and or damage

to the simulator system.

Radiation

Do not expose the simulator to any radiation conditions.


Manual

Mar 10, 2014 A2-14001-PTR

4. Normal Procedures

This chapter contains Normal Procedures applied only for the

simulator. This chapter does not cover the aircraft operation.

4.1 POWER UP

ELECTRICAL SOURCE CONNECTED

POWER SUPPLY ON

FAN ON

COMPUTER ON

EMB STANDBY INSTRUMENTS START

FSX START

FLIGHT READY TO CONFIG

4.2 SHUTDOWN

FLIGHT

FINISHED

FSX CLOSED

EMB STANDBY INSTRUMENTS CLOSED

COMPUTER OFF

ELETRICAL EQUIPMENT OFF

LIGHTS OFF

POWER SUPPLY OFF

FAN OFF

ELECTRICAL SOURCE OFF/DISCONNECTED


Manual

Mar 10, 2014 A2-14001-PTR

Software initialization

Once the computer is turned on, first open the Emb Standby

Gauges and then start FSX.

We do recommend that the FSX should be configured to have a

preloaded flight with all settings and panels configured to reduce

the configuration time before each flight. Any changes should be

made by the FSX menu after the flight is loaded.

It is recommended to save each flight that you desire to use again.

After configuration, the default view should be the following

shown below. In case that something is not in accordance or differ

from the picture bellow, refer to the non-normal procedures.

Refer to section 7.2 Software for the directions of how configure

the panels.


Manual

Mar 10, 2014 A2-14001-PTR

5. Supplementary Procedures

This section contains procedures that are accomplished as

required rather than routinely performed on each flight.

Supplementary procedures may be required because of

unscheduled maintenance or as a result of a procedure referenced

in a Non–Normal Checklist. Additionally, some may be

performed if the flight crew must accomplish preflight actions

normally performed by maintenance personnel.


Manual

Mar 10, 2014 A2-14001-PTR

5.1 Non-normal procedures

This chapter contains non-normal procedures applied only for the

simulator, this chapter does not cover the aircraft operation.

5.1.1 OVERHEAT

FAN ON

PANEL LIGHTS OFF IF OVERHEAT CONDITION CONTINUES

ELECTRIC CONNECTIONS OFF/DISCONNECTED

FAN OFF

ELECTRIC SOURCE OFF/DISCONNECTED IF OVERHEAT CONDITION CONTINUES

FIRE EXTINGUISHER USE IF NECESSARY

5.1.2 ELECTRIC FAILURE

ELECTRIC SOURCE OFF/DISCONNECTED IF ELEC FAIL CONDITION CONTINUES


IF ELEC FAIL CONDITION CONTINUES

FIRE EXTINGUISHER USE IF NECESSARY

5.1.3 FAN MALFUNCTION

FAN OFF

PANEL LIGHTS OFF IF FAN MALFUNCTION CONDITION CONTINUES

ELECTRIC SOURCE OFF/DISCONNECTED


5.1.4 LIGHTS MALFUNCTION PANEL LIGHTS OFF

FLOOD LIGHTS OFF

MAP LIGHT OFF IF LIGHTS MALFUNCTION CONDITION CONTINUES

ELECTRIC SOURCE OFF/DISCONNECTED


5.1.5 STANDBY GAUGES NOT WORKING


Manual

Mar 10, 2014 A2-14001-PTR

Close and restart the Emb Standby Gauges software.

5.1.6 INSTRUMENTS WINDOW WRONG SIZE

Manually resize the instruments window by using the mouse on

the edge of the window to resize it.


Manual

Mar 10, 2014 A2-14001-PTR

6. General Information

6.1 General overview

Overhead panel

Not available (S/N A2-14001-PTR)

Upper overhead panel


Cooling panel


AIR COND annunciator not available (S/N A2-14001-PTR)

OVERHEAT annunciator not available (S/N A2-14001-PTR)

CAUTION: If the OVERHEAT annunciator lit, proceed to

the non-normal procedure.

CAUTION: If there is no air coming out of the ventilation

exhaust after 15 seconds, proceed to the non-normal

procedure.

CAUTION: One Fan operation is only certified when ambient

temperature is between +5°C and +15°C.


CAUTION: Before energizing other systems of the simulator

make sure that the FAN is working properly and that FAN1

and FAN2 annunciators lit.

FAN1/FAN2 annunciator not available (S/N A2-14001-PTR)


Manual

Mar 10, 2014 A2-14001-PTR

Advisory Panel


Main overhead panel


Front overhead panel


Front main panel.

The front main panel is composed by 6 system panels plus 2

pushbuttons.

Glareshield Lights Control Panel

Master Warning and Master Caution Pushbutton

Guidance Panel

Primary Flight Display (PFD)

Multi Function Display (MFD)

Integrated Electronic Standby System (IESS)

Clock

Engine Indication and Crew Alerting System Display (EICAS)

Autobrake panel

Landing Gear Panel

1 2 3

4 5

6

7

8 9

10


Manual

Mar 10, 2014 A2-14001-PTR

Multi Function Display (MFD)

Use the computer mouse to navigate through the MFD functions.

Integrated Electronic Standby System (IESS)

The Integrated Electronic Standby System (IESS) provides

attitude, indicated airspeed and altitude indications.

The IAS is displayed in knots on the left scale.

The altitude is displayed on the right scale in hundreds of feet. It

uses the FSUIPC standby altimeter info as well. Same shortcuts

ton increase or decrease hpa than the analog altimeters, and if you

press "M" you set the standard pressure (1013.25hpa).

You can switch on/off the display of the localizer and glide path

deviation by pushing "L".

You can input airspeed and altitude "bugs" (references) via the

"bugs menu" accessible by pushing "B".

Inside the "bugs menu", use the "+"and "-" keys to select a bug

box then modify the value with "O" or "P" keys. Press "M" on a

key to activate/deactivate the box. The bug will appear as a cyan

dash on the scales. Push "B" again to exit "bugs menu". Before

using any of the Keyboard Functions bellow make sure to click

over the IESS display with the computer mouse to activate the

functions and to not be mistaken by the FSX as other commands.

Keyboard Function

"M" standard pressure (1013.25hpa)

"L" switch on/off the display of the LOC and GP

"B" "bugs menu"


Manual

Mar 10, 2014 A2-14001-PTR

Clock

Only the RST and CHR pushbuttons contained in the Clock panel

are connected to the simulator, the chronometer information of

those pushbuttons is displayed in the PFD. All the other

pushbuttons do not have functions assigned. However the

functions can be controlled by keyboard as shown bellow.

The clock uses FS Zulu time to display the hour or the date.

Before using any of the Keyboard Functions bellow make sure to

click over the Clock display with the computer mouse to activate

the functions and to not be mistaken by the FSX as other

commands.

Keyboard Function

"D" switch between date and hour

"C" start/stop the chronometer

"R" reset the chronometer

"S" run ET

"T" pause ET

"A" reset ET

Autobrake panel

The Autobrake knob controls the following functions: Autobrake

increase when placed in the Low position and Autobrake decrease

when placed in the RTO position, select the desired position by

moving the knob until the desired position is shown in the

EICAS.

Landing Gear Panel

The Landing Gear Lever controls the position of the Landing

Gear. To operate it simply move it up or down according to the

desired function.


Manual

Mar 10, 2014 A2-14001-PTR

NOTE: The Landing Gear Lever is very delicate and care

should be employ when operating it.

CAUTION: Do not touch the Fans while operating, this may

cause damage and hurt.

CAUTION: Do not touch the Power Plug, this may cause

damage and hurt.

Guidance panel

Only the functions listed below are not available:

Push Dir

Push Sync

Push Ft-M

To turn on the Guidance Panel Backlight turn on the BACK

LIGHT switch located on the left light panel.

NOTE: To improve the panel utilization, turn the knobs

slowly.


Manual

Mar 10, 2014 A2-14001-PTR

6.2 Peripheral connections

This simulator device uses the following peripheral components:

N Item Serial Number

1 Energy source SK02G-1200200V

1 AC/DC Adapter Samsung BN44-00394D

021012ABRLF-B/SB

1 Samsung LS22B300 Monitor 0292HQBD401146A

CAUTION: Before turning on the equipment make sure that

all peripheral devices are properly connected.

Monitor screen

The simulator is composed of ONE monitor.

Monitor 1 represents the aircraft instruments, it is a Samsung

LS22B300 LED model.


Manual

Mar 10, 2014 A2-14001-PTR

7. Maintenance

General

This Publication contains information required to check, repair,

adjust or test units or assemblies for all systems and equipment

installed in the 19X simulators listed on this manual.

NOTE: THIS MANUAL WAS PREPARED SPECIFICALLY

TO COVER THE AVIATION FOR ALL SIMULATORS

LISTED IN THE LIST OF EFFECTIVE SIMULATORS. IT

CONTAINS INSTRUCTIONS AND INFORMATION

APPLICABLE SOLELY TO THOSE SPECIFIC

SIMULATORS.

Systems Description Section

Manual describes the functions, operation, configuration, and

control of the airplane systems. The SDS explains how the

systems and components operate, and how to operate the systems.

The SDS shows how the systems are constructed, and the

interfaces to other systems.

Component Location

The location of each major component is shown by a component

locator illustration on the graphic(s) that address this major

component. The physical location is shown in reference to

structural features.

Fault Isolation

Fault isolation provides the information used to identify, locate

and correct any fault that is predicted to occur on the airplane

from time to time.


Manual

Mar 10, 2014 A2-14001-PTR

Testing

Explain a test procedure.

How To Use The Maintenance Manual

CAUTION: MAKE SURE THAT YOU DO ALL OF THE

STEPS TO THE END OF THE PROCEDURE. LARGE

BLANK SPACES CAN OCCUR AT THE BOTTOM OF

PAGES WHICH DO NOT ALWAYS INDICATE THAT

YOU ARE AT THE END OF THE PROCEDURE. IF YOU

DO NOT MAKE SURE THAT YOU HAVE COMPLETED

THE PROCEDURE, DAMAGE TO EQUIPMENT OR

SYSTEM MALFUNCTION MAY OCCUR.

Identify the material of the damaged part. Refer to the applicable

material identification data in this manual.

NOTE: The material identification tables and some of the figures

give reference drawing numbers. Refer to these reference

drawings when the applicable structure is not identified.

Find the allowable damage data for the damaged structure.

Unless specified differently, all dimensions in this manual are

given in millimeters.

Standard Tools

Tools in this manual that are identified with an ST prefix are

designed by The Aviation For All Company. Detail drawings of

these tools are available by request.


Manual

Mar 10, 2014 A2-14001-PTR

Service Bulletins

The service bulletins that have been used to make or change the

data contained in this manual are given in the Service Bulletin

List.

Maintenance record

Every fault, system discrepancy or schedule maintenance should

be noted in the Maintenance Record. Following that, should be

described the work that need to be done and the work performed.

Maintenance procedures

All maintenance procedures must follow what is described in this

manual or newer service bulletins. If the procedure is not listed in

this manual or in any service bulletin, contact Aviation For All

maintenance sector.

CAUTION: When removing the Overhead Main Panel or the

Cooling Panel beware of the electronic components cables, as

they might disconnect or break.

NOTE: THE MAINTENANCE PROCEDURES NOT

LISTED IN THIS MANUAL SHOULD BE REQUESTED AS

NEEDED.

NOTE: TO REQUEST A MAINTENANCE PROCEDURE

PLEASE FILL THE REQUEST MAINTENANCE

PROCEDURE FORM SHOWN BELLOW AND SEND IT TO

[email protected].

NOTE: TO REQUEST A REPLACEMENT PART PLEASE

FILL THE REPLACEMENT PART FORM SHOWN

BELLOW AND SEND IT TO

[email protected].


Manual

Mar 10, 2014 A2-14001-PTR

REQUEST MAINTENANCE PROCEDURE FORM COMPANY/OPERATOR NAME SIMULATOR SERIAL NUMBER

DATE OF REQUEST MAINTENANCE DEPARTMENT (NAME, E-MAIL, PHONE)

PROCEDURE REQUEST

MAINTENANCE PROBLEM DESCRIPTION

SIMULATOR ACTUAL CONDITION

OPERATIONAL

( )

PARTIALY

OPERATIONAL

( )

NOT OPERATIONAL

( )

OTHER:

( )

TO THE AVIATIONFORALL MAINTENANCE DEPARTMENT WE REQUEST THE

PROCEDURES LISTED ABOVE CONCERNING THE SIMULATOR DEVICE INFORMED

ABOVE IN THE SERIAL NUMBER BOX.

NAME DATE CONTACT INFORMATION (E-MAIL/PHONE)

IF THERE IS ANY IMAGE/PHOTO TO BE SEND WITH THIS FORM PLEASE PLACE IT AS

AN ANNEX IN JPEG FORMAT UP TO 2MB PER FILE. DO NOT EXCEED 20MB TOTAL.

SEND THIS FORM FILLED TO [email protected]


Manual

Mar 10, 2014 A2-14001-PTR

REPLACEMENT PARTS REQUEST FORM

COMPANY/OPERATOR NAME SIMULATOR SERIAL NUMBER

DATE OF REQUEST MAINTENANCE DEPARTMENT (NAME, E-MAIL, PHONE)

PARTS REQUEST

QUANTY PART NUMBER DESCRIPTION RMK

MAINTENANCE PROBLEM DESCRIPTION SHIPPING INFORMATION

ADRESS

CITY COUNTRY ZIP CODE

SHIPPING METHOD

SIMULATOR ACTUAL CONDITION

OPERATIONAL

( )

PARTIALY

OPERATIONAL

( )

NOT OPERATIONAL

( )

OTHER:

( )

TO THE AVIATIONFORALL MAINTENANCE/STOCK DEPARTMENT WE REQUEST THE

PARTS LISTED ABOVE CONCERNING THE SIMULATOR DEVICE INFORMED ABOVE IN

THE SERIAL NUMBER BOX.

NAME DATE CONTACT INFORMATION (E-MAIL/PHONE)

IF THERE IS ANY IMAGE/PHOTO TO BE SEND WITH THIS FORM PLEASE PLACE IT AS

AN ANNEX IN JPEG FORMAT UP TO 2MB PER FILE. DO NOT EXCEED 20MB TOTAL.

SEND THIS FORM FILLED TO [email protected]


Manual

Mar 10, 2014 A2-14001-PTR

7.1 HARDWARE

Knobs

To remove a knob:

Tool Screwdriver (Size varies from knob model)

Reference material Knob datasheet

1° Step Loose the screw

2° Step Remove the knob

3° Step Check the knob for damages

4° Step If necessary replace the knob

5° Step Insert the procedure done in the maintenance

record

End

To install a knob:

Tool Screwdriver

Reference material Knob datasheet

1° Step Insert the knob in the right position

2° Step Tight the screw

3° Step Verify the integrity of the installation


record

End


Manual

Mar 10, 2014 A2-14001-PTR

Switches

Types of switches

Toggle

To remove a toggle switch:

NOTE: To remove a switch it may be necessary to remove the

front panel.

Tool Wrench (Size varies from switch model)

Reference material Switch datasheet

1° Step Disconnect the switch

2° Step Remove the switch cover (if installed)

3° Step Loose the screw nut

4° Step Remove the screw nut and the washer

5° Step Remove the switch

6º Step Check the switch for damages

7° Step If necessary replace the switch


record

End


Manual

Mar 10, 2014 A2-14001-PTR

To install a toggle switch:

NOTE: To install a switch it may be necessary to remove the

front panel.



1° Step Prepare the area (must be clean, right hole

diameter, right position)

2° Step Insert the switch

3° Step Insert the washer and the screw nut

4° Step Tight the screw nut

5° Step Insert the switch cover (if installed)

6º Step Re-connect the switch

7° Step Test the circuit


record

End


Manual

Mar 10, 2014 A2-14001-PTR

Rotary

To remove a rotary switch:

NOTE: To remove a switch it may be necessary to remove the

front panel.



1° Step Disconnect the switch

2° Step Remove the switch knob, see 00.00.00

3° Step Loose the screw nut

4° Step Remove the screw nut and the washer

5° Step Remove the switch

6º Step Check the switch for damages

7° Step If necessary replace the switch


record

End


Manual

Mar 10, 2014 A2-14001-PTR

To install a rotary switch:

NOTE: To install a switch it may be necessary to remove the

front panel.





2° Step Insert the switch

3° Step Insert the washer and the screw nut

4° Step Tight the screw nut

5° Step Insert the switch knob, see 00.00.00

6º Step Re-connect the switch



record

End


Manual

Mar 10, 2014 A2-14001-PTR

Push button

Model A Model B

NOTE: The procedures for Push Button Model B are the

same for Toggle Switches.

To remove a push button (Model A):

NOTE: To remove a push button it may be necessary to remove

the front panel.

Tool No tool required

Reference material Push button datasheet

1° Step Disconnect the push button

2° Step Press the push button abs and push it out

3° Step Remove the push button

4° Step Check the push button for damages

5° Step If necessary replace the push button

6º Step Insert the procedure done in the maintenance

record

End


Manual

Mar 10, 2014 A2-14001-PTR

To install a push button (Model A):

NOTE: To install a push button it may be necessary to remove the

front panel.

Tool No tool required

Reference material Push button datasheet



2° Step Insert the push button

3° Step Press the push button abs and push it in

4° Step Re-connect the push button


6º Step Insert the procedure done in the maintenance

record

End

Encoder

NOTE: The procedures for Encoders are the same for Rotary

Switches.


Manual

Mar 10, 2014 A2-14001-PTR

Potentiometer

NOTE: The procedures for Potentiometers are the same for

Rotary Switches.


Manual

Mar 10, 2014 A2-14001-PTR

7.2 SOFTWARE

Undock Window

To a FSX screen be suitable to be transferred between two

monitors it is necessary to follow the procedure bellow. The FSX

must not be in the full screen mode.

1 – Select the new view that you want to undock.

2 – Right click over it and select “Undock Window”.


Manual

Mar 10, 2014 A2-14001-PTR

3 – Resize and move the window as necessary using the mouse.

Out of scale screen

Just resize the window and change the eye point if necessary.

1 – Resize and move the window as necessary using the mouse.

2 – Use the following commands as needed to reset the eye point.


Manual

Mar 10, 2014 A2-14001-PTR

COMAND FUNCTION

- ZOOM OUT

= ZOOM IN

ROTATE THE EYE POINT HOLD SPACE + MOVE THE MOUSE

EYE POINT (LEFT) CTRL+SHIFT+BACKSPACE

EYE POINT (RIGHT) CTRL+SHIFT+ENTER

EYE POINT (UP) SHIFT+ENTER

EYE POINT (DOWN) SHIFT+BACKSPACE

EYE POINT (FOWARD) CTRL+BACKSPACE

EYE POINT (BACK) CTRL+ENTER

Windows work place not configured

1 – Right click over the Windows Work Place, select “Resolução

da tela”.

2 – Reorganize the three monitors as shown bellow. S/N A1-

11002-PTR

MONITOR REAL POSITION

A S19B300B MONITOR 3

B S19B300B MONITOR 2

C LG E1960T MONITOR 1


Manual

Mar 10, 2014 A2-14001-PTR

NOTE: The work place is extended from Monitor A to

Monitor B.

NOTE: In case that the Monitor C screen appear to be upside

down, just modify the screen orientation.

FSUIPC

All commands, including switches, pushbuttons and

potentiometer axis are processed by the FSUIPC software. It is

important to know that any switch or axis assignment are

processed by FSX, in fact it is strictly necessary to deny the FSX

the task of recognizing joysticks.

NOTE: Allowing FSX to recognize joysticks will lead to a

conflict between FSX and FSUIPC and all data may be lost.


Manual

Mar 10, 2014 A2-14001-PTR

Make sure that FSX will not recognize any joystick by the

procedure bellow.

1 – Open the “Controls” menu.

2 – Make sure that the “Enable Controller(s)” box is NOT check.


Manual

Mar 10, 2014 A2-14001-PTR

You can access the FSUIPC control panel in the “Add-ons”

menu.

NOTE: For more information about the FSUIPC, please

check the FSUIPC manual available in the

http://www.schiratti.com/dowson.html

http://www.schiratti.com/dowson.html

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