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1993-07-25
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5KB
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137 lines
============================================================================
AIRBUS A310-300
for
Microsoft Fightsimulator IV
Design from
Oliver Pabst
Finkenstr. 4
D-63263 Neu-Isenburg
Germany
Version 2.0 of Juli 1993
=============================================================================
This aircraft for the Microsoft Fightsimulator is a try to use the
possibility of the Aircraft Designers from Mallard in the best way.
Installation:
-------------
Copy the following files in the Flugsimulator-Directory:
PA313xxx - Grafik Aircraft-Information
PA313xxx.SIM - Aircraft - Technical-Data
PA313xxx.SC0 - Object-Database for SEE 4.0
You can use this aircraft with the Flightsimulator menu No 1, part E.
You can change the technical Information with the Aircraft-Designer (Menu 1,
Part I).
Technical Information:
======================
ENHANCED AIRCRAFT DESIGNER - MAIN MENU
Menus Main Wings
A STABILIZER SYSTEMS... J Span In Feet;00144
K Chord In Feet;00016
C WGT/BAL/INSTRUM/STRUCT... L Aspect Ratio;008.80
D AERODYNAMICS/CONTROLS... M Angle Of Incidence;357.99
N Induced Drag Adj.;10000
O Dihedral (Degrees);00002
Files P Dihedral Scale;00100
F Write Flight Parameter File Q Gyro Dihedral;00050
G Filename; PA313DLH R +Winglets
H Aircraft Name; PA313DLH A310-300 d DLH
I Save Aircraft To Disk Airframe And Propulsion
S Type: JET
T Power: LBS 00100 x 1000
U Altitude Derate;00400
STABILIZER SYSTEMS
Horizontal Stabilizer Damping Effects
A Position;01575 G Pitch Damper;00400
B Surface Area;00688 H Roll Damper;30000
C Angle Of Incidence;000.00 I Yaw Damper;65000
D Lift Coefficient Scale;15000 J Pitch Vel. Hyst.;00040
Tail Stability Augmentation
E Position;01500 K Pitch Stabilizer Easy;32000
F Surface Area;00486 L Pitch Stabilizer Real;32000
COLOR AND VISUAL DESIGN
VISUAL EFFECTS
K Aircraft Numbers ;
WEIGHT/BALANCE/INSTRUMENTS/STRUCTURE
Weight And Balance Instruments
A Dry Weight LBS x 1000;00176 H Overspeed Warning;00450
B Fuel Tanks LBS x 1000;00070 I Sim Switches;00002
C Center Of Gravity;00780 J Stall Warning Angle;011.99
D Center Of Lift;00860 K +Enhanced Instrument Panel
E Pitch Inverse Moment;01000
F Roll Inverse Moment;00500 Structure
G Yaw Inverse Moment;05000 L Gear: Fixed
M Canard Configuration
AERODYNAMICS/CONTROLS N Crash Resistance;00020
Surface Areas Control Sensitivities
A Frontal Area (Sq. Ft.);00100 M Rudder Sens.;08000
B Frontal Area Scale;00200 N Rudder Half;00180
C Body Side Area;02000 O Rudder Eighth;00300
P Ailer. Sens.;02000
Flaps Lift/Drag Coefficients Q Ailer. Half;00180
D Flaps Lift Coef.;03000 R Ailer. Eighth;00300
E Flaps Drag Coef.;00020 S Elev. Half;00180
T Elev. Eighth;00300
Drag Coefficients U Ground Steering;60000
F Gear Drag Coef.;00050
G Slow Speed Drag;00015 Miscellaneous.
H Spoiler Drag;00300 V Stall Synthesize;00044
I Touchdown Drag;00200 W +Heavy Aircraft
J Slip Drag;00010 Y +Thrust Reversers
Dynamic Pressure Effects
K Max Velocity;00520
L Dynamic Pressure Limit;00200
Other available Airlines:
=========================
- AFR Air France
- AUA Austrian
- BBB Balair
- CFG Condor Flugdienst
- HLF Hapag Llyod
- KLM KLM Royal Dutch Airlines
- DLH Deutsche Lufthansa
- MPH Martinair
- SAB Sabena World Airlines
- TEA Transeuropean Airways
- THY Turkish Airlines
Happy fly hour.
=============================================================================