Thank you for taking an interest in our selection of 1560-01-485-3955 parts here on Boost AOG. You are currently on the RFQ form for part number P00200-1, a Gkn Aerospace Transparency Systems product listed with the Windshield Panel Aircraft If part number P00200-1 catches your eye, be sure to use our online RFQ service to request quotes, with customized responses provided within 15 minutes of us receiving and reviewing a completed submission.
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To ensure the quality of our NSN components, we adhere to a strict NO CHINA SOURCING pledge, meaning every purchased item will be delivered alongside any pertinent qualifying certifications or manufacturing trace documentation for your benefit. Paired with numerous other commitments, we proudly operate with AS9120B, ISO 9001:2015, and FAA AC 00-56B accreditation. If you happen to be facing a time constraint and require NSN parts quickly, contact us at your earliest convenience, and we will discuss the expedited shipping options we have available for domestic and international customers alike. With our various dedications in mind, kick off procurement for Gkn Aerospace Transparency Systems part number P00200-1 and other Windshield Panel Aircraft products today.
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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