NSN 1560-01-280-1924 of Door Access Aircraft - Parts Details
| Alternative NSN: 1560012801924 |
| Item Name: Door Access Aircraft |
| FSG: 15 Aircraft and Airframe Structural Components |
| Federal Supply Class (FSC): 1560 Airframe Structural Components |
| NIIN: 012801924 |
| NCB Code: USA (01) |
| Manufacturers: Aerospace And Commerical Technologies , Cyclone Aviation Services 1972 Ltd , Elbit Systems Ltd |
ASAP Aviation Procurement, owned and operated by ASAP Semiconductor, is the latest parts procurement platform for the aerospace and aviation industry. Check out high demanding part numbers 16P1524-813 under NSN 1560-01-280-1924 of Door Access Aircraft manufactured by Aerospace And Commerical Technologies, Cyclone Aviation Services 1972 Ltd, Elbit Systems Ltd.
Federal Supply Class of NSN 1560-01-280-1924 is FSC 1560 contains part details of Airframe Structural Components. Quote for your desired part numbers.
Part Number's List for NSN 1560-01-280-1924, 1560012801924
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Part No Manufacturer Item Name QTY RFQ 16P1524-813 Aerospace And Commerical Technologies door access aircraft Avl RFQ 16P1524-813 Cyclone Aviation Services 1972 Ltd door access aircraft Avl RFQ 16P1524-813 Elbit Systems Ltd door access aircraft Avl RFQ
Characteristics Data of NSN 1560012801924MRC Criteria Characteristic AAGR CROSS-SECTIONAL SHAPE STYLE ARCHED ABGL WIDTH 7.222 INCHES NOMINAL ABMW PERIPHERAL SHAPE STYLE RECTANGLE, MULTI HOLES ABRY LENGTH 11.900 INCHES NOMINAL ADNU CORNER RADIUS 0.750 INCHES NOMINAL ADNV HOLE QUANTITY ALONG LENGTH 11 ADNW HOLE QUANTITY ALONG WIDTH 11 ADNY DISTANCE BETWEEN HOLES ALONG LENGTH 1.478 INCHES NOMINAL ADNZ DISTANCE BETWEEN HOLES ALONG WIDTH 1.630 INCHES NOMINAL ADPA DISTANCE BETWEEN HOLE CENTERLINE AND FIRST HOLE ALONG LENGTH 1.478 INCHES NOMINAL ADPB DISTANCE BETWEEN HOLE CENTERLINE AND FIRST HOLE ALONG WIDTH 1.630 INCHES NOMINAL ADPC DISTANCE FROM FIRST HOLE CENTERLINE TO END ALONG LENGTH 2.108 INCHES NOMINAL ADPD DISTANCE FROM FIRST HOLE CENTERLINE TO END ALONG WIDTH 2.070 INCHES NOMINAL ADPK CORNER HOLE CENTERLINE RADIUS 0.114 INCHES NOMINAL ADPQ INSIDE CORNER RADIUS 56.000 INCHES NOMINAL ADPR BODY THICKNESS 1.730 INCHES NOMINAL ADQB SECURING DEVICE TYPE HINGE AND THREADED FASTENER AGAV END ITEM IDENTIFICATION F-16 CXCY PART NAME ASSIGNED BY CONTROLLING AGENCY DOOR,EXHAUST-JET ENGINE FUEL STARTER,ASSY FEAT SPECIAL FEATURES JET FUEL STARTER EXHAUST; C/O: 1 SHAFT, 1 SKIN, 6 SHIMS, 1 AR PRIMER, 5 BUSHINGS, 1 HOUSING, 1 HINGE, 1 CAM, 3 FLANGES, 79 WASHERS, 2 PINS, 59 NUTS, 8 RIVETS, AND 33 BOLTS MATT MATERIAL STEEL COMP 321 MDCL MATERIAL DOCUMENT AND CLASSIFICATION MIL-S-6721 MIL SPEC SINGLE MATERIAL RESPONSE
| MRC | Criteria | Characteristic |
|---|---|---|
| AAGR | CROSS-SECTIONAL SHAPE STYLE | ARCHED |
| ABGL | WIDTH | 7.222 INCHES NOMINAL |
| ABMW | PERIPHERAL SHAPE STYLE | RECTANGLE, MULTI HOLES |
| ABRY | LENGTH | 11.900 INCHES NOMINAL |
| ADNU | CORNER RADIUS | 0.750 INCHES NOMINAL |
| ADNV | HOLE QUANTITY ALONG LENGTH | 11 |
| ADNW | HOLE QUANTITY ALONG WIDTH | 11 |
| ADNY | DISTANCE BETWEEN HOLES ALONG LENGTH | 1.478 INCHES NOMINAL |
| ADNZ | DISTANCE BETWEEN HOLES ALONG WIDTH | 1.630 INCHES NOMINAL |
| ADPA | DISTANCE BETWEEN HOLE CENTERLINE AND FIRST HOLE ALONG LENGTH | 1.478 INCHES NOMINAL |
| ADPB | DISTANCE BETWEEN HOLE CENTERLINE AND FIRST HOLE ALONG WIDTH | 1.630 INCHES NOMINAL |
| ADPC | DISTANCE FROM FIRST HOLE CENTERLINE TO END ALONG LENGTH | 2.108 INCHES NOMINAL |
| ADPD | DISTANCE FROM FIRST HOLE CENTERLINE TO END ALONG WIDTH | 2.070 INCHES NOMINAL |
| ADPK | CORNER HOLE CENTERLINE RADIUS | 0.114 INCHES NOMINAL |
| ADPQ | INSIDE CORNER RADIUS | 56.000 INCHES NOMINAL |
| ADPR | BODY THICKNESS | 1.730 INCHES NOMINAL |
| ADQB | SECURING DEVICE TYPE | HINGE AND THREADED FASTENER |
| AGAV | END ITEM IDENTIFICATION | F-16 |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | DOOR,EXHAUST-JET ENGINE FUEL STARTER,ASSY |
| FEAT | SPECIAL FEATURES | JET FUEL STARTER EXHAUST; C/O: 1 SHAFT, 1 SKIN, 6 SHIMS, 1 AR PRIMER, 5 BUSHINGS, 1 HOUSING, 1 HINGE, 1 CAM, 3 FLANGES, 79 WASHERS, 2 PINS, 59 NUTS, 8 RIVETS, AND 33 BOLTS |
| MATT | MATERIAL | STEEL COMP 321 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | MIL-S-6721 MIL SPEC SINGLE MATERIAL RESPONSE |