Mfg Part Number: P00201 2 | Alternate P/N: P002012 | NSN : 1560-01-485-3954 |
NIIN : 014853954 | CAGE Code : 86175 | Manufacturer: Gkn Aerospace Inc |
Item Name : Windshield Panel Ai | FSC : 1560 Airframe Structural Components |
At Aerospace and Defence Parts, we offer high-quality NSN Part P00201 2 that you can steadily rely on for your applications. NSN 1560-01-485-3954 of P00201 2 is listed alongside and it has been manufactured by Gkn Aerospace Inc. As we have availability for Windshield Panel Ai parts now, we invite you to fill out and submit the form provided below to request a quote for your comparisons. As you complete our form, we recommend that you provide us with as much information as you can regarding your desired P00201 2 Part, quantities, target price, expected shipping time frame, and more so that we may best tailor a solution fit for you.
NSN 1560-01-485-3954 with NIIN is manufactured under the CAGE Code 05305, and we list our parts with such information to ensure that you always procure the exact items that you require. Additionally, our industry experts offer person-to-person communication every step of the purchasing process so that your requirements are thoroughly met. If you are facing a time constraint and need components quickly, our supply chain network stretching across the United States, Canada, and the United Kingdom enables us to provide rapid shipping times for your benefit. Experience the future of part procurement today when you get in contact with one of our representatives.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
1560-01-485-3954 Item Description: Windshield Panel Ai | 1560 | 014853954 | 0 | P | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
P00201 2 | 6 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
FEAT | SPECIAL FEATURES | ABRASION RESISTANT COATING (PILKINGTON ARC SS-6590) IS TO BE APPLIED TO THE ENTIRE OUTER AND INNER SURFACE OF THE OUTER AND INNER PANEL.WINDSHEILD SHALL BE CAPABLE OF WITHSTANDING SETTINGS OF 110 DEGREES F, MEASURED AT THE TEMPERATURE SENSORS; WINDSHEILD SHALL BE CAPABLE OF OPERATING AT AMBIENT AIR TEMPERATURES OF -65 DEGREES F. |
CZEJ | AIRCRAFT STATION NUMBER | BL24.0 |
BWJF | SIDE FOR WHICH DESIGNED | RIGHT SIDE |
CXCY | III PART NAME ASSIGNED BY CONTROLLING AGENCY | INAVY:WINDSHEILD, COCKPIT CANOPY |
SR-1 | MANUFACTURERS CODE | 78286 |
SR-1 | MFR SOURCE CONTROLLING REFERENCE | 65206-01003-114 |
SR-1 | SPEC/STD CONTROLLING DATA | |
CZEK | AIRCRAFT MISSION DESIGN SERIES | H-53 |
AGAV | III END ITEM IDENTIFICATION | WINDSHEILD,COCKPIT CANOPY;CH-53E,MH-53E;S-80E-1;S-80M-1 |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | MIL-P-25690 MIL SPEC SINGLE MATERIAL RESPONSE |
MATT | MATERIAL | PLASTIC ACRYLIC |
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