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| NIIN: | 01-414-3174 | Item Name: | INC: | 53048 |
| FSC: | 6615 | Assignment Date: | Jun-05-1995 | CRIT: | X | IIG: | 53048 |
| ISC: | 2 | Date Standardized: | Jan-27-1998 | HMIC: | N | DODIC: |
| NSC: | 8 | Cancellation Date: | Apr-30-2010 | PMIC: | A | FIIG: | A30800 |
| ESD: | B | Schedule B: | DEMIL: | A | DEMIL INT: |
| TIIC: | 1 | Originator: | TU | ADPEC: | 0 | RPDMRC: |
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The full version of LogiQuest has information related to NSN 6615-01-414-3174 in each of the following databases.
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PROCUREMENT - Procurement History
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WHEREUSED - Where NIIN Used
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CAGE - Commercial And Government Entity
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H6 - Federal Item Name Directory
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FSC - Federal Supply Class
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| Part Number | CAGE | Company | Status | RN CC | RN VC | DAC | RN AAC | RN FC | RN SC | RN JC | SADC | HCC | MSDS |
| 17B1U6001-545 | 88277 | THE BOEING COMPANY | H | 5 | 9 | 5 | ZZ | B | |||||
| 17B1U6001-553 | 88277 | THE BOEING COMPANY | H | 3 | 2 | 5 | ZZ |
| MOEC | SOS | A A C | R C | S L C | CIIC | U P Q | U S C | Unit Price | UI | UICF | MCD | Action Date | C/H |
| DF | FPZ | Y | T | 0 | U | 1 | L | $329,186.68 | EA | SF8LD-N | Jan-01-1999 | H |
| MRC | Requirement Statement | Reply Statement |
| ACUR | DIRECT CURRENT VOLTAGE RATING IN VOLTS | 22.0 AND 29.5 |
| AGAV | END ITEM IDENTIFICATION | C-17 ACFT |
| AJAF | UNPACKAGED UNIT LENGTH | 16.30 INCHES NOMINAL |
| AJAG | UNPACKAGED UNIT WIDTH | 10.10 INCHES NOMINAL |
| AJAH | UNPACKAGED UNIT HEIGHT | 7.60 INCHES NOMINAL |
| AWJN | UNPACKAGED UNIT WEIGHT | 38.90 POUNDS |
| AWZJ | POWER SOURCE | EXTERNAL |
| AXQJ | INTELLIGENCE INPUT METHOD | ELECTRICAL |
| CBBL | FEATURES PROVIDED | ELECTROSTATIC SENSITIVE |
| FEAT | SPECIAL FEATURES | OPERATING TEMP -40 TO 131 DEG F; ALTITUDE UP TO 50,000 FEET; MEMORY 314K; BASIC PROCESSOR UNIT WITHOUT SOFTWARE IS PART NUMBER 103E415G14; PART NUMBER 17B1U6001-553 IS THE BASIC UNIT WITH SOFTWARE VERSION 3.0 INSTALLED |
| FTLD | FUNCTIONAL DESCRIPTION | USED TO COMPUTE PRIMARY FLIGHT CONTROL, STABILITY AND CONTROL AUGMENTATION AND AUTOMATIC FLIGHT CONTROL FUNCTIONS; PERFORMS ALL CALCULATIONS NECESSARY TO IMPLEMENT FUNCTIONS OF THE STABILITY AND CONTROL AUGMENTATION SYSTEM, AUTOPILOT, AUTOTHROTTLE, FLIGHT DIRECTOR, HEAD UP DISPLAY CONTROL AND GROUND PROXIMITY WARNING SYSTEM |
| RDAL | REFERENCE DATA AND LITERATURE | T.O. 5A7-3-45-2 |
| SUPP | SUPPLEMENTARY FEATURES | MANUFACTURERS NAME: COMPUTER,FLIGHT CONTROL |
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