You have reached the quote request page for part number P00200-1 of Gkn Aerospace Transparency Systems, we have in stock that is listed alongside the description Windshield Panel Aircraft. If you would like to learn more about this NSN part and your purchasing options, please fill out and submit the Request the Quote (RFQ) page presented on this page. By offering us important details like your target price and expected fulfillment time frame, our team can best offer you a tailored solution for your consideration. As we have staff available at all times, responses to any submission will be offered within 15 minutes of our review.
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To make exploring our expansive inventory simple, we have chosen to list all offerings alongside as much information as we can for an ease of identification. For example, part number P00200-1 is specifically produced under CAGE Code 86175, denoting the specific Gkn Aerospace Transparency Systems facility it traces back to. Furthermore, with the NSN 1560-01-485-3955, this item also belongs to FSC 1560 Airframe Structural Components, further ensuring that you only purchase your exact needs. If you have any questions or concerns regarding our offerings or service, be sure to call or email us at your convenience. Otherwise, we look forward to serving you as your strategic sourcing partner for part number P00200-1 and more.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
1560-01-485-3955 Item PartTypeName: WINDSHIELD PANEL,AIRCRAFT | 1560 | 014853955 | 0 | P | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
65206-01009-106 | 6 | 9 | 5 |
MRC | Criteria | Characteristic |
---|---|---|
AGAV | End Item Identification | CH-53;WINDSHIELD CENTER COCKPIT CANOPY |
MDCL | Material Document And Classification | MIL-P-25690 MIL SPEC SINGLE MATERIAL RESPONSE |
CZDJ | Aircraft Location | WINDSHIELD CENTER COCKPIT CANOPY |
CXCY | Part Name Assigned By Controlling Agency | INAVY:WINDSHIELD, PANEL AIRCRAFT |
CRTL | Criticality Code Justification | AGAV |
FEAT | Special Features | ABRASION RESISTANT COATING (PILKINGTON ARC SS-6590) IS TO BE APPLIED TO THE ENTIRE OUTER SURFACE OF THE OUTER PANEL AND TO THE ENTIRE INNER SURFACE OF THE INNER PANEL;INNER PANEL THICKNESS IS 0.190 INCHES AND THE OUTER PANEL THICKNESS IS 0.063 INCHES. |
MRC | Decoded Requirement | Clear Text Reply |
CZEK | Aircraft Mission Design Series | H-53 |
MATT | Material | PLASTIC ACRYLIC |
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