U.S. Special Operations Command, Attn: AMSAM-AR-Z-A-K, Bldg 401, Lee Blvd., Fort Eustis, VA 23604-5577

16 -- STANDBY ATTITUDE INDICATOR SOL USZA95-98-R-0005 DUE 022898 POC Teresa Dansberry, 757-878-5223, Ext. 243 E-MAIL: contact the Contract Specialist via e-mail, tdansber@tapo.eustis.army.mil. This is a synopsis for 60 each Standby Attitude Indicators to be installed on the MH-60K and MH-60E Aircraft. This system must be totally self-contained and be able to display the following information simultaneously: Pitch, Roll, Side Slip, Heading, Airspeed, and Vertical Speed. This will be a fully competitive unrestricted contract action. This is not a request for a developmental item. Contractor may modify existing commercial off the shelf items to meet the Specification outlined below: 1. The system must totally self-contained and be able to display the following information simultaneously: a. Pitch b. Roll. c. Side Slip. d. Heading. e. Airspeed. f. Vertical Speed. 2. Must be NVIS compatible per MIL-L-85762. 3. The system must be qualified to ADS-37A-PRF (Aeronautical Design Standard, Electromagnetic Environmental Effects (E3) Performance and Verification Requirements for a Flight Critical Component. 4. The system must be qualified to operate in the environment (temperature, altitude, vibration, dust/sand, etc.) that an Army Aircraft must operate. (will be provided with the solcitation). 5. The system must operate on 28 VDC aircraft power per MIL-STD-704. 6. The display is to be 3ATI size, no longer than 9.0 inches (without connectors) and weigh less than 4.0 lbs. 7. The indicator must be capable of being mounted on various instrument panels (18 for the MH-47E and 30 for the MH-60K) without changes to the box. 8. Total system shall weigh less than 10 lbs. 9. The Roll Pointer (Bank Index Pointer) shall indicate the degree of bank in the direction of the bank (i.e. the roll pointer shall move clockwise when the aircraft enters a right bank and indicate the degree of bank. 10. The system shall have the following accuracy: a. Attitude: 1) Static 0.5 degrees max 2) Dynamic 4.0 degrees max b. Airspeed: 1) 60 KIAS 6.0 KIAS 2) >60 KIAS 2.0 KIAS c. Altitude: 1) Sea Level 15 feet 2) 10,000 feet 20 feet d. Data Latency < 20 msece. Lateral Acceleration 0.02 g 11. Display shall meet the following: a. Display size of 2.4 x 2.4 viewing area. b. 240 x 240 colors. c. Minimum of 20 Hz refresh rate. d. Display colors are to be a standard FAA color set. 12. System to be certified to the following Federal Aviation Administration Technical Standard Orders or their equivalents: a. TSO-C2d, Airspeed Instruments. b. TSO-C4c, Bank and Pitch Instruments. c. TSO-C10b, Aircraft Altimeter. d. TSO-C113, Airborne Multipurpose Electronic Displays. 13. Baro set must be pilot selectable in either Hg or milibars and must be capable of being set and transmitting its setting over an ARINC 429. 14. The unit must have 5 VDC lighting for its bezel. 15. Reliability: a. Magnetometer > 50,000 hours b. Air Data Computer >100,000 hours c. Attitude Indicator > 10,000 hours 16. System must be able to have the aircraft reference symbol adjusted in flight to correct for difference in aircraft attitude during straight and level flight. Interested sources may contact Teresa Dansberry at 757-878-5223, Ext. 243 or Fax your request to 757-878-4199 please reference the solicitation number. (0020)

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