Simulator General Description
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1 Garuda MD11 Full Flight Simulator Technical Description Simulator General Description Operator/Sponsor Location Manufacturer Garuda Airlines Jakarta, Indonesia CAE, Montreal Canada Original In-Service Date 1996 Current Status Not currently operating Simulated Aircraft Aircraft Manufacturer / Model Engine Manufacturer / Model MD-11 GECF6-80C2 DIF; PW4060/4460 Tail # Still in Operator's Fleet PK-GIG (not in fleet) Qualification / Certification Authority: Country: Regulation or Standard: Designation & ID # Dept. of Transport Canada FAA Level D / Phase 3
2 DGAC Indonesia FAA Level D DSKU/0322/APP/98 Certification Event: Certifying Authority: Date: Initial Qualification DoT Canada January 1996 Last Recurrent Evaluation DGAC April 1998 Next Recurrent Evaluation Not Current April 2008 Aircraft Avionics Unit / System: Manufacturer / Model: Flight Management Software model - Honeywell FMC Rehost Computer IBM Risc/6000 J30 Model, FMC load 909, MCDU load 903, and DEU load 908 MCDU Honeywell GPWS / EGPWS Sundstrand Mk V Warning Computer EICAS / ECAM EFIS Symbol Generator Engine Instrument Spec MDC K ,02 MD11 CAE hardware Software System Spec Honeywell C Rev D Flight Compartment Primary Flight Instrument Type Engine Instrument Type Electronic Electronic Unit / System: Manufacturer / Model:
3 ADI EADI PFD HSI EHSI NFD PFD CAE built MA ND CAE built MA CDU MCDU Honeywell INS GPS EGPWS Sundstrand Autopilot Honeywell TCAS IVSI RDDMI Simulated TCAS II, TTR-920 Weather Radar Simulated WX Radar and WR Landmass System ACARS AlliedSignals (Boeing) ATIS CAE simulated ATIS/Digital Voice System Auto Throttles Installed Thrust Control Module, ABH7760-1, Honeywell Heads Up Display Simulator Upgrades A1 update engine update to include PW4060/PW4460 Motion System Manufacturer / Model CAE series 600 Type (Hyd/Elec) Motion System Drive Hydraulic Digital DN1 (DMC16, FPMC-30, ADIO)
4 Number of Axis Jack Stroke Length HPU Pump(s) 6 Axis 60 inch Stroke 2 Motion Pumps 1 Control Loading Pump 1 Cooling Pump Control Loading System Primary Controls: Manufacturer / Model Type (Hyd/Elec) Control System Drive CAE Hydraulic Digital DN1 (DMC16, FPMC-30, ADIO) No. of Primary Channels 13 Loaded Primary Controls: Capt Aileron (Wheel) Capt Elevator (Column) Capt Rudder (Pedals) FO Aileron (Wheel) FO Elevator (Column) FO Rudder (Pedals) Nosewheel (Tiller) Celevevator, Felevator, Stabtrim, Caileron, Faileron, Rudder, NWS, Ltoebrake, Rtoebrake, Speedbrake, Autospoiler, Flaps, Altlndgear
5 Toe Brakes (L & R) Secondary Controls Loaded Secondary Controls: Installed: Stab Trim Speed Brake Primary (as above) Primary (as above) Auto Throttles Thrust Mode Control Unit (Aircraft) Visual System - Image Generator IG Manufacturer / Model CAE Maxvue (Not operable), Enhance A+ Number of Channels Y2K Compliant 3 Channels Visual System - Display System Display Type WIDE Mirror Field of View 180 Degrees x 40 Degrees (+20/-20) Projector Manufacturer / Model EIS Barco 5043 Window Display Configuration Cross Cockpit AutoCal Visual Scenes Jakarta, Bali, Surabaya, Solo, Yogyakarta, Padang, Medan, Balikpapan, Manado, Singapore, Darwin, Bangkok (old), Kuala Lumpur (old), Hong Kong (old), Amsterdam, Seattle, San Fran, LAX.
6 Host Computer / Linkage Manufacturer / Model IBM Risc 6000 model 590 Operating System / Version AIX 3.2 Y2K Compliant Upgrades Linkage (I/O) Interface CAE C-bus interface Instructor Station Manufacturer / Model CAE Xterm Touchscreens IOS Display Computer Y2K Compliant Remote Control Unit Independent Crew Training Features JCC XfaceC-N-7A-2 JCC Internal to Touchscreens CAE PCU (Portable Control Unit) Multi engine Multi operator kgs/lbs meters/feet Aural Cue System Manufacturer / Model CAE
7 Type / Description Digital Simulated Special Effects Feature: FAA / JAA Approved Windshear Profile(s) Microburst Model(s) Simulated Oxygen System Installed: FAA Windshear profiles 3.3A, 3.3B1, 3.3B2, 3.3B3, 3.3C, 3.3D Smoke Generation System CO2 Bottle Type CAT I, II, III CAT 1, CAT 2, CAT III DH = 0 ft ETOPS Data Package (Installed and Certified in the Simulator) Category: Documentation: Revision: Aerodynamic Model MDC K / K D Flight Controls Model MDC K / K / K D Ground Handling MDC K D Engine Model Engine Model GE CF6-80C2-DIF (MD11/GE80C2-DIF FADEC Rev 8.3F) PW 4060/4460 (PW4000 engine PWA- PPS-1931 scn 4E)
8 Documentation Source: Amounts Present (Selection is Bold and Underlined) Equipment Manufacturer (Boeing & CAE) Vendor (Computer, Visual, Peripherals, etc.) Operator (Airline, etc) Spare Parts Source: Amounts Present (Selection is Bold and Underlined) Aircraft Parts Simulator Manufacturer Visual Manufacturer Vendor
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The Federal Aviation Administration (FAA) has evaluated the Flight Simulation Training Device (FSTD) listed below. This FSTD has been found to meet the standards set forth in the qualification document
Statement of Qualification
Statement of Qualification The Federal Aviation Administration (FAA) has evaluated the Flight Simulation Training Device (FSTD) listed below. This FSTD has been found to meet the standards set forth in
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Statement of Qualification The Federal Aviation Administration (FAA) has evaluated the Flight Simulation Training Device (FSTD) listed below. This FSTD has been found to meet the standards set forth in
Statement of Qualification
The Federal Aviation Administration (FAA) has evaluated the Flight Simulation Training Device (FSTD) listed below. This FSTD has been found to meet the standards set forth in the qualification document
Statement of Qualification
The Federal Aviation Administration (FAA) has evaluated the Flight Simulation Training Device (FSTD) listed below. This FSTD has been found to meet the standards set forth in the qualification document
Statement of Qualification
Statement of Qualification The Federal Aviation Administration (FAA) has evaluated the Flight Simulation Training Device (FSTD) listed below. This FSTD has been found to meet the standards set forth in
Statement of Qualification
Statement of Qualification The Federal Aviation Administration (FAA) has evaluated the Flight Simulation Training Device (FSTD) listed below. This FSTD has been found to meet the standards set forth in
Statement of Qualification
Statement of Qualification The Federal Aviation Administration (FAA) has evaluated the Flight Simulation Training Device (FSTD) listed below. This FSTD has been found to meet the standards set forth in
Statement of Qualification
Statement of Qualification The Federal Aviation Administration (FAA) has evaluated the Flight Simulation Training Device (FSTD) listed below. This FSTD has been found to meet the standards set forth in
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Statement of Qualification
Statement of Qualification The Federal Aviation Administration (FAA) has evaluated the Flight Simulation Training Device (FSTD) listed below. This FSTD has been found to meet the standards set forth in
Statement of Qualification
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