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Quality guaranteed We sell only warrantied and traceable partsThank you for your interest in our available NSN parts 103E4151G14 and components on Purchasing Union. 103E4151G14 is described as a Processor Flight Co part, and it is manufactured by Federal Specifications Promulgat. This component is readily available for purchase today, and our team of industry experts are on standby 24/7x365 to provide you with rapid-lead times and competitive pricing on all that we carry. To begin the purchasing process, you may submit an Instant RFQ form as provided through our website. Once it is received, a member of our staff will reach out to you in 15 minutes or less to provide a personalized quote that is crafted to fit your individual needs.
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Purchasing Union is a state of the art purchasing platform, and we are a leading independent distributor of 103E4151G14 that cater to a diverse set of industries and applications. To ensure the quality of our inventory for our customers, we choose to only source our parts from top global manufacturers that we trust, such as Federal Specifications Promulgat. We also ensure that every part is rigorously tested, inspected, and cross-referenced before being shipped. Peruse our inventory at your leisure to find a multitude of top requested parts like 6615014482341, and our team is ready to serve as your strategic sourcing partner today. (CAGE Code 88277).
| MRC | Criteria | Characteristic |
|---|---|---|
| AJAF | Unpackaged Unit Length | 16.30 INCHES NOMINAL |
| SUPP | Supplementary Features | MANUFACTURERS NAME: COMPUTER,FLIGHT CONTROL |
| AJAG | Unpackaged Unit Width | 10.10 INCHES NOMINAL |
| ACUR | Direct Current Voltage Rating In Volts | 22.0 AND 29.5 |
| CBBL | Features Provided | ELECTROSTATIC SENSITIVE |
| AJAH | Unpackaged Unit Height | 7.60 INCHES NOMINAL |
| FEAT | Special Features | EFFECTIVITY P41 TO SUBSEQUENT ACFT; P/N 103E4151G14 IS THE HARDWARE ONLY |
| 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 AUGMENATION SYSTEM, AUTOPILOT, AUTOTHROTTLE, FLIGHT DIRECTOR, HEADS UP DISPLAY CONTROL AND GROUND PROXIMITY WARNING SYSTEM |
| AGAV | End Item Identification | C-17 AIRCRAFT |
| CRTL | Criticality Code Justification | CBBL |
| AXQJ | Intelligence Input Method | ELECTRICAL |
| AWZJ | Power Source | EXTERNAL |
| MRC | Decoded Requirement | Clear Text Reply |
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