SPECIAL NOTICE
69 -- T57 Graphical Trainer
- Notice Date
- 5/14/2009
- Notice Type
- Special Notice
- NAICS
- 334111
— Electronic Computer Manufacturing
- Contracting Office
- Department of the Navy, Naval Air Systems Command, Naval Air Warfare Center Training Systems Division, 12350 Research Parkway, Code 253, Orlando, Florida, 32826-3224
- ZIP Code
- 32826-3224
- Solicitation Number
- T57001
- Archive Date
- 4/29/2010
- Point of Contact
- Gerald F Hooper,, Phone: 407-380-4266
- E-Mail Address
-
gerald.f.hooper@navy.mil
- Small Business Set-Aside
- N/A
- Description
- Key Dates Release Date: 14 May 2009 Response Date: 5 June 2009 Issued By NAWC TSD Background Chief of Naval Air Training (CNATRA) has a requirement for a Graphical Training Device (GTD) part task trainer, (integrated systems and procedures trainer, or virtual / integrated procedures trainer), to support the TH-57 Intermediate and Advanced Helicopter training syllabus. The TH-57 is a Bell 206 helicopter that has been modified for helicopter training of US Military pilots. The target aircraft for the GTD is the “D” model which has been upgraded to a glass cockpit. The avionics suite used is the Integrated Avionics System (IAS) consisting of a Chelton Flight Systems synthetic vision EFIS featuring five 4” x 5” Integrated Display Units (IDUs). This 5-screen architecture will include one Primary Flight Display (PFD) and one Multi-Function Display (MFD) installed on the pilot’s (right side) instrument panel, one PFD and one MFD installed on the copilot’s (left side) instrument panel, and one dedicated Engine Instruments and Crew Alerting System (EICAS) display installed in the center of the instrument panel. The display units will interface with engine and aircraft system sensors by means of the dual channel Airframe and Engine Data Concentrator (AEDC). The primary interface between the AEDC and the Display Units will be via an ARINC-429 data bus. The subject training device objective is to familiarize the pilot with all aircraft systems and related instruments, as well as allow for “hands on” practice to gain experience in the operational functions and procedures of the aircraft systems in all phases of operation. Also desired is the ability to demonstrate all aircraft systems including related malfunctions and normal and emergency procedures. It would allow hands-on with switches, knobs, levers, etc. that could reinforce the systems knowledge taught in the classroom portion of the systems course. The device also requires the ability to enter data through the Primary Flight Display (PFD) and Multi-Function Display (MFD), resulting in the correct display indications and the proper interface with related avionics equipment such as the VHF/UHF Comm. The training sequence envisioned would have morning systems training (Mediated Interactive Lecture) followed by afternoon GTD sessions Computer Aided Instruction (CAI) to reinforce the systems lessons and to introduce malfunctions and failures of the various systems and recovery options. The device should be capable of utilizing self-paced lessons that are similar to the capability of higher level computer based training modules. The functions shall have automated and interactive modes to reinforce the training objectives. The ability to familiarize the student with system behaviors and functions is the primary objective of this device. It is not to be confused with higher fidelity Cockpit Procedure Trainers (CPTs) where aircraft procedures are executed and graded, but to teach the systems and what happens within the systems when switches/circuit breakers are manipulated. This device shall be capable of being configured in a flight mode to step through the actions and reactions of the systems due to airborne emergencies. Actual cockpit instruments are not required, but accurate graphical depictions should be displayed on touch sensitive (where appropriate) screens. The following modules will be taught to include components/operating limits/emergency procedures for each: Electrical (DC/Battery) Hydraulic Main Rotor/Transmission Tail Rotor Flight Controls Fuel System Power Plant and associated systems Flight Controls/HeliSas (automated flight control stabilization) Navigation/Avionics (Chelton EFIS, IDU-450, EICAS, Garmin GTX-330 Transponder, COBHAM COM/NAV, COBHAM VHF/UHF) Information Requested 1. Existing solutions to the subject requirement 2. Proposed architecture of the GFT to include hardware, software, technical documentation, system drawings, physical dimensions and power requirements. 3. Challenges and risks of developing a GFT 4. Cost estimate for one or more of the following areas: i. Training requirements analysis to include development of a requirements traceability matrix that considers the current syllabus and improvements that could be made to the syllabus with the introduction of this device ii. Software design documentation. Software and hardware development and procurementcost iii.Proposed delivery schedule iv.Companion instructional materials v.Operators manual / instructor guide vi.Maintenance manual / troubleshooting guide vii.Interface documentation viii.Drawings ix.Spare parts x.COMS/ISEO training xi.Data rights xii.Development for Test Procedures to verify and validate functionalities of the PFD/MFD. 5.Proposed schedule for delivery of a minimum of four devices Response submission Please direct all responses in Microsoft Office 2007 viewable format no later than COB, 5:00PM 5 June 2009. POC: Gerald Hooper NAWC TSD Contracting 12350 Research Parkway Orlando, FL 32826 gerald.f.hooper@navy.mil (407) 380-4266
- Web Link
-
FedBizOpps Complete View
(https://www.fbo.gov/spg/DON/NAVAIR/N61339/T57001/listing.html)
- Place of Performance
- Address: 12350 Research Parkway, Orlando, Florida, 32826, United States
- Zip Code: 32826
- Zip Code: 32826
- Record
- SN01817118-W 20090516/090514220112-039d1961f08f89914d98fa3c4d03b7fa (fbodaily.com)
- Source
-
FedBizOpps Link to This Notice
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