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Copyright © 2015
Aviation For All Company
All Rights Reserved
Document Number P1-14001-PTR
August 29, 2014
Revision Number: 02
Revision Date: March 17, 2015
Prop Sim
Flight Simulator Training
Device
Manual
Prop Sim Simulator
Manual
Mar 17, 2015 P1-14001-PTR
PROP SIM SIMULATOR
MANUAL
Elaboration:
_______________________________________
AVIATION FOR ALL
Endorsement:
_______________________________________
AVIATION FOR ALL
Review:
_______________________________________
AVIATION FOR ALL
Prop Sim Simulator
Manual
Mar 17, 2015 P1-14001-PTR
Review
Nº Reviser Date Signature
ORIGINAL - Aug/2014 -
REV 1 L.F.F. Mar/2015
Prop Sim Simulator
Manual
Mar 17, 2015 P1-14001-PTR
Intentionally
Blank
Prop Sim Simulator
Manual
Mar 17, 2015 P1-14001-PTR
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
Simulator initialization 4.3
Simulator monitor indication 4.4
Monitor 1 4.4.1
Supplementary Procedures 5. Non-normal procedures 5.1
Overheat 5.1.1
Electric Failure 5.1.2
Lights Malfunction 5.1.3
Gauges not working 5.1.4
Instrument window wrong size 5.1.5
General Information 6. General Overview 6.1
Panel 6.1.1
Main panel 6.1.2
Selector panel 6.1.3
Switch panel 6.1.4
Rack 6.1.5
Peripheral Connections 6.2
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Mar 17, 2015 P1-14001-PTR
Monitor screen 6.2.1
Avionics 6.2.2
Maintenance 7. Request maintenance form 7.0.1
Replacement parts request form 7.0.2
Hardware 7.1
Knobs 7.1.1
Toggle switch 7.1.2
Rotary switch 7.1.3
Pushbutton 7.1.4
Encoder 7.1.5
Potentiometer 7.1.6
Software 7.2
Undock window 7.2.1
Out of scale screen 7.2.2
Windows workplace not config. 7.2.3
FSUIPC 7.2.4
Config. the panel display 7.2.5
Panel restore procedure 7.2.6
Using FSUIPC 7.2.7
Prop Sim Simulator
Manual
Mar 17, 2015 P1-14001-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
004 P1-14001 PRP
004 P1-14002 PRP
004 P1-14003 PRP
004 P1-14004 PRP
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Mar 17, 2015 P1-14001-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 Prop Sim simulator;
• serve as a comprehensive reference for use during training for the
Prop Sim simulator;
• serve as a review guide for use in recurrent training and
proficiency checks in the Prop Sim 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
Prop Sim Simulator
Manual
Mar 17, 2015 P1-14001-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 aircraft experience and is familiar with basic
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
Prop Sim Simulator
Manual
Mar 17, 2015 P1-14001-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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Mar 17, 2015 P1-14001-PTR
Prop Sim Simulator
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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
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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AICC . . . . . . .Auxiliary Integrated Control
Center
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 17, 2015 P1-14001-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
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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Manual
Mar 17, 2015 P1-14001-PTR
KPH . . . . . . . .Kilograms per Hour
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
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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Mar 17, 2015 P1-14001-PTR
QRH . . . . . . . . Quick Reference Handbook
QTY. . . . . . . . . Quantity
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
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
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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
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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.
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Nº Subject Ref. Nº Date Status
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Intentionally
Blank
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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.
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Electrical Power
The simulators listed in this manual require a DC power supply
supplied by the USB board.
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.
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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
USB CONNECTIONS CONNECTED
DISPLAY MONITOR ON
COMPUTER ON
FSX START
FLIGHT LOAD
PANEL RESTORE.EXE START
FLIGHT READY TO CONFIG
4.2 SHUTDOWN
FLIGHT
FINISHED
FSX CLOSED
COMPUTER OFF
ELETRICAL EQUIPMENT OFF
LIGHTS OFF
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4.3 Simulator initialization
Certify that all cables and connections are connected prior to turn
on the computer.
Once the computer is turned on follow the Power Up checklist in
the normal procedures section 4.1.
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. (See software
maintenance section of this manual).
NOTE: It is recommended to save each flight that you desire to
use again.
After the flight is loaded you may need to drag and resize the
instrument panel window by using the mouse or the PANEL
RESTORE.EXE. (See software maintenance section of this manual).
After configuration, the default view should be the following
shown below. In case that something is not in accordance or differ
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from the picture bellow, refer to the non-normal procedures or
maintenance procedures.
NOTE: Refer to section 7.2 Software for the directions of how
configure the panels.
4.4 Simulator monitor indication
4.4.1 Monitor 1
The picture bellow show the image that should be displayed in the
Monitor 1. Make sure that this image is properly sized and
positioned in the screen area.
All the airplane instruments are displayed in this screen.
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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.
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
PANEL LIGHTS OFF
IF OVERHEAT CONDITION CONTINUES
ELECTRIC CONNECTIONS OFF/DISCONNECTED
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
ELECTRIC CONNECTIONS OFF/DISCONNECTED IF ELEC FAIL CONDITION CONTINUES
FIRE EXTINGUISHER USE IF NECESSARY
5.1.3 LIGHTS MALFUNCTION PANEL LIGHTS OFF
IF LIGHTS MALFUNCTION CONDITION CONTINUES
ELECTRIC SOURCE OFF/DISCONNECTED
ELECTRIC CONNECTIONS OFF/DISCONNECTED
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5.1.4 GAUGES NOT WORKING
Close and restart the FLIGHT SIMULATOR software.
5.1.5 INSTRUMENTS WINDOW WRONG SIZE
PANEL RESTORE.EXE
EXECUTE
IF INSTRUMENTS MALFUNCTION CONDITION CONTINUES
Manually resize the instruments window by using the mouse on
the edge of the window to resize it.
CAUTION: Do not touch the Power Plug, this may cause
damage and hurt.
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6. General Information
This section contains general information about the simulator
structure, components and display.
6.1 General overview
6.1.1 Panel
The front main panel is composed by the main panel, selector
panel, switch panel and the avionics rack.
6.1.2 Main panel
The main panel contains all flight and engine instruments, it
contains 3 push buttons in the clock, 2 in the RMI and 1 in the
DME.
The guide to properly configure the instruments display is in the
maintenance procedures in this manual.
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1 - EADI
2 - EHSI
3 - Airspeed Indicator
4 - Altimeter
5 - RMI
6 - VSI
7 - Flap Position Indicator
8 - Engine Indication
9 - Clock
10 - DME
11 - Turn Coordinator
12 - Fuel Gauges
6.1.3 Selector panel
The selector panel contains 4 rotary encoders, the primary use for
them is to select the barometric pressure in the altimeter, the course
selector, heading selector and altitude selector, but they can be
assigned to any other function to meet your requirements.
The pushbutton associated in the encoders are not operative in this
model.
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6.1.4 Switch panel
The switch panel is composed by 13 ON-OFF toggle switch, 2
(ON)-OFF spring-loaded toggle switch, 1 (ON)-OFF spring-loaded
pushbutton, 1 ON-OFF-ON toggle switch, 1 (ON)-OFF-(ON)
toggle switch and 4 LED indicators.
The switches listed bellow have specific operations:
BAT: Energizes the simulator BUS that enable the panel lights and
landing gear indicator lights.
GEAR: 3 position toggle switch, UP, DN and OFF, after the UP
selection is made the switch must be returned to the OFF position,
when selected the DN position it must remain in this position.
The indicator lights are not linked to the FSX, any faults simulated
in the software will not be shown in the hardware, any lights
malfunctions are hardware fault and must be taken into
maintenance procedure.
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FLAP: 3 position spring loaded toggle switch, one click per
operation dent for UP or DN operation, to verify the flap position
check the main panel indicator.
ENG STRT: 2 position spring loaded toggle switch, held in the ON
position to engage the engine starter.
NOTE: The Landing Gear Lever is very delicate and care
should be employ when operating it.
NOTE: To improve the panel utilization, turn the knobs and
switches slowly.
6.1.5 Rack
The rack is factory closed and can be used to hold avionics modules
from the GoFlight Inc™ that are not included in the simulator
packaged.
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6.2 Peripheral connections
This simulator device uses the following peripheral components:
N Item Serial Number
1 AC/DC Adapter Samsung
1 Samsung Monitor
CAUTION: Before turning on the equipment make sure that
all peripheral devices are properly connected.
6.2.1 Monitor screen
The simulator is composed of ONE monitor.
Monitor 1 represents the aircraft instruments.
6.2.2 Avionics
The avionics rack may be used to assembly the GoFlight Inc™
modules.
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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 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.
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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.
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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 panels 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
NOTE: TO REQUEST A REPLACEMENT PART PLEASE
FILL THE REPLACEMENT PART FORM SHOWN
BELLOW AND SEND IT TO
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7.0.1 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]
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7.0.2 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]
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7.1 HARDWARE
7.1.1 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
4° Step Insert the procedure done in the maintenance
record
End
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7.1.2 Toggle switch
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
8° Step Insert the procedure done in the maintenance
record
End
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To install a toggle switch:
NOTE: To install a switch it may be necessary to remove the front
panel.
Tool Wrench (Size varies from switch model)
Reference material Switch datasheet
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
8° Step Insert the procedure done in the maintenance
record
End
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7.1.3 Rotary switch
To remove a rotary 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 knob, see 7.1.1
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
8° Step Insert the procedure done in the maintenance
record
End
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To install a rotary switch:
NOTE: To install a switch it may be necessary to remove the front
panel.
Tool Wrench (Size varies from switch model)
Reference material Switch datasheet
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 knob, see 7.1.1
6º Step Re-connect the switch
7° Step Test the circuit
8° Step Insert the procedure done in the maintenance
record
End
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7.1.4 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
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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
1° Step Prepare the area (must be clean, right hole
diameter, right position)
2° Step Insert the push button
3° Step Press the push button abs and push it in
4° Step Re-connect the push button
5° Step Test the circuit
6º Step Insert the procedure done in the maintenance
record
End
7.1.5 Encoder
NOTE: The procedures for Encoders are the same for Rotary
Switches.
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7.1.6 Potentiometer
NOTE: The procedures for Potentiometers are the same for
Rotary Switches.
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7.2 SOFTWARE
7.2.1 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”.
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3 – Resize and move the window as necessary using the mouse.
7.2.2 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.
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2 – Use the following commands as needed to reset the eye point if
using the 3D panel view.
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
7.2.3 Windows work place not configured
1 – Right click over the Windows Work Place, select “Screen
resolution”.
2 – Reorganize the monitors as shown bellow.
MONITOR REAL POSITION
A MONITOR 1
B MONITOR 2
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NOTE: The work place is extended from Monitor A to Monitor
B.
7.2.4 FSUIPC
All commands, including switches, pushbuttons and potentiometer
axis are processed by the FSUIPC software. It is important to know
that NO switch or axis assignment are processed by FSX, 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.
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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.
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You can access the FSUIPC control panel in the “Add-ons” menu.
7.2.5 Configuring the panel display
1- Start the FSX, select the desired aircraft, location, weather and
date;
2- In this simulator guide we will use the default King Air 350;
3- It is necessary to organize the screens in order to your simulator
work properly;
4- The image bellow shows the default 3D view when using the
PROPSIM_PANEL.cfg, right click the screen and select Cockpit -
> Cockpit to open the 2D panel;
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5- The image bellow shows the default 2D view, right click one of
the instruments and select Undock Window;
6- Once the main panel is undocked, it is necessary to move it to
the main instrument panel monitor, simply use the mouse to move
and resize according to the necessity to match the instruments
image to the instrument position in the hardware panel;
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7- Open the Auxiliary instruments panel, View -> Instrument Panel
-> TQ;
MOVE
RESIZE
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8- Once open, move the panel to the left hand bottom of the screen.
9- Save this configuration as a new flight and use it for all the
simulator normal operations. If you need to make any changes in
the flight, first open the saved flight and then make the necessary
changes. Save as many flights as you need for your operation.
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NOTE: There is a FSX bug that in every software startup that
the user uses the saved flight the windows will show up out of
scale, adopt the procedure bellow in order to fix the bug.
7.2.6 Panel restore procedure
Unzip and open the Panel_position folder. There will be two exec
files, one for save the panel position and other to restore the
position and size of the panel. One file will be created for each
aircraft.
1- Unzip the Panel_position.zip;
2- Open the Panel_position folder;
3- Start the FSX in the window mode;
4- Open all the panels that are required, undock them, resize and
position them in the correct locations;
5- Execute the ¨Panel_Store.exe¨ and wait 5 seconds;
6- A new file will be created for this aircraft. Keep this file in the
Panel_position folder;
7- After the file is created, go back to the FSX and modify all the
windows size, save it again and use it as the standard flight. (it is
important to modify the windows size in order to the
¨Panel_restore.exe¨ correct and update all the graphics);
8- Exit and restart the FSX;
9- When the flight is started again the windows will be out of their
positions and scale;
10- Certify that all the windows that you need are open and
undocked;
11- Execute the ¨Panel_restore.exe¨;
12- All the windows should go back to their original and correct
position that you saved in the first moment.
When starting a new flight (EVERYDAY USE PROCEDURE)
1- Certify that all windows that will be used are open and
undocked;
2- Execute the ¨Panel_restore.exe¨.
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NOTE: The program will remember the size and position of
the panels.
More details
When the ¨Panel_store.exe¨ is executed, the program verify all the
open windows, it only keeps the panels and store the information
in an .ini file. The name of this .ini file must be the same name of
the panel that the program saves.
When the ̈ Panel_restore.exe¨ is executed, it search the name of the
aircraft, verify the .ini file to access the panels size, scale and
position and if the panels are open and undocked (the program
don´t open the panels, just modify them).
If you execute the ̈ Panel_store.exe¨ and there is a file for the same
aircraft it automatically delete the old file and create a new one.
Tips
Create a shortcut in the work place to make easier the access to the
program.
Only after executing the ¨Panel_restore.exe¨ make the changes in
the scenery and flight situation.
7.2.7 Using FSUIPC
This tutorial will guide you in the process of assigning functions
for all switches.
Now that the panels are adjusted, it is time to configure the
functions in the FSUIPC, start by opening the FSUIPC in the Adds-
on menu;
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7.2.8 Create mouse macro
1- Open the Buttons + Switches menu and click the Create Mouse
Macro button;
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2- Name the new mouse macro 00-SIM and click OK;
3- Using the mouse click in the Aux Panel switches in order to
create a new mouse macro, once you click in one switch a new
window will pop-up, you must give a name to the function selected,
bellow there is a table with all functions names that you need to
assign;
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NOTE: When using the default FSX King Air 350 model it is
not necessary to create mouse macros in the FSUIPC, all the
necessary commands are in the FS control list.
The table below displays the commands associated to each switch
that need to be connected.
FS LIST – FSUIPC ASSOCIATED SWITCH FSUIPC
ANTI_ICE_TOGGLE 65571 ANTI ICE *
AP_ALT_VAR_DEC 65893 ALT – ROTATE L **
AP_ALT_VAR_INC 65892 ALT – ROTATE R **
AXIS_AILERONS_SET 65763 JOYSTICK AILERON ***
AXIS_ELEVATOR_SET 65762 JOYSTICK ELEVATOR ***
AXIS_LEFT_BRAKE_SET 66387 JOYSTICK BRAKES LEFT ***
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AXIS_MIXTURE_SET 66292 JOYSTICK MIXTURE (IF
USING SINGLE HANDLE FOR
BOTH ENGINES)
***
AXIS_MIXTURE1_SET 66422 JOYSTICK MIXTURE ENG 1 ***
AXIS_MIXTURE2_SET 66425 JOYSTICK MIXTURE ENG 2 ***
AXIS_PROPELLER_SET 66291 JOYSTICK PROPELLER (IF
USING SINGLE HANDLE FOR
BOTH ENGINES)
***
AXIS_PROPELLER1_SET 66421 JOYSTICK PROPELLER ENG 1 ***
AXIS_PROPELLER2_SET 66424 JOYSTICK PROPELLER ENG 1 ***
AXIS_RIGHT_BRAKE_SET
66388 JOYSTICK BRAKES RIGHT ***
AXIS_RUDDER_SET 65764 JOYSTICK RUDDER ***
AXIS_THROTTLE_SET 65765 JOYSTICK THROTTLE (IF
USING SINGLE HANDLE FOR
BOTH ENGINES)
***
AXIS_THROTTLE1_SET 66420 JOYSTICK THROTTLE ENG 1 ***
AXIS_THROTTLE2_SET 66423 JOYSTICK THROTTLE ENG 2 ***
BRAKES 65588 JOYSTICK BRAKES ***
ELEV_TRIM_DN 65607 JOYSTICK ELV TRIM DN ***
ELEV_TRIM_UP 65615 JOYSTICK ELV TRIM UP ***
FLAPS_DECR 65759 FLAP – UP
FLAPS_INCR 65758 FLAP – DN
GEAR_DOWN 66080 GEAR – DN
GEAR_UP 66079 GEAR – UP
HEADING_BUG_DEC 65880 HDG – ROTATE L **
HEADING_BUG_INC 65879 HDG – ROTATE R **
KOHLSMAN_DEC 65884 BARO – ROTATE L **
KOHLSMAN_INC 65883 BARO – ROTATE R **
LANDING_LIGHTS_TOGGLE
65751
LIGHTS – LAND *
PITOT_HEAT_TOGGLE 65858 PITOT *
STROBES_TOGGLE 65560 LIGHTS – STRB *
TOGGLE_ALTERNATOR1 66363 GEN 1 *
TOGGLE_ALTERNATOR2 66364 GEN 2 *
TOGGLE_AUTOFEATHER_ARM
66297 AUTO FEATHER *
TOGGLE_AVIONICS_MASTER
66293 AVIONICS *
TOGGLE_BEACON_LIGHTS
66239 LIGHTS – BCN *
TOGGLE_DME 66286 DME – N1/N2
TOGGLE_MASTER_BATTERY
66241 BAT *
TOGGLE_NAV_LIGHTS 66379 LIGHTS – NAV *
TOGGLE_PROPELLER_SYNC
66287 PROP SYNC
TOGGLE_STARTER1 66300 ENG STRT – L **/****
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TOGGLE_STARTER2 66301 ENG STRT – R **/****
TOGGLE_TAXI_LIGHTS 66240 LIGHTS – TAXI *
VOR1_OBI_DEC 65662 CRS – ROTATE L **
VOR1_OBI_INC 65663 CRS – ROTATE R **
CLOCK – OAT/VOLTS
CLOCK – SELECT
CLOCK – CONTROL
RMI – 1 SWAP
RMI – 2 SWAP FSUIPC commands table.
*Toggle switch: All the toggle
switch inputs (except the landing
gear and flap lever) need to be
associated the same control when
pressed and when released in order
to the switch work properly.
**Encoder: Every encoder has two
operational commands, rotate left
and rotate right.
***Joystick: Commands associated
in this category are not included in
the simulator, it is necessary to have
a separate joystick to operate these
commands and calibrate them in the
FSUIPC in order to avoid conflict.
****Starter: The starters toggle
switch are spring loaded to OFF
position, it is necessary to check the
¨Control to repeat while held¨.
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7.2.9 How to add a command
Upon the first use of the simulator it is necessary to configure all
commands using the FSUIPC.
After the initialization of the simulator, open the FSUIPC and make
sure the simulator is connected to the computer.
Open the Buttons + Switches menu, make sure the Aircraft specific
box is checked, this will allow the commands to work specific with
the associated aircraft.
Use the FSUIPC commands table to start the switch configuration
following the order.
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Press, rotate or flip the associated switch/button in the simulator.
Once the switch is moved, the FSUIPC will recognize it and show
the board input. To select a command after the switch input, mark
the Select for FS control and select the associated FS command in
the list.
* All the toggle switch inputs (except the landing gear and flap
lever) need to be associated a control when pressed and when
released in order to the switch work properly.
TOGGLE_AUTOFEATHER_ARM
TOGGLE_AUTOFEATHER_ARM
*
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NOTE: Always before the simulator startup make sure all
switches are in the same position that in the simulator, to make
any changes before the simulator is initialized use the virtual
TQ panel to modify the switch position.
NOTE: For more information about the FSUIPC, please check
the FSUIPC manual available in the
http://www.schiratti.com/dowson.html
