NSN 1560-01-100-1701 B40809105, B40-809105, SB7301103
Product Details | AIRCRAFT STRUCTURAL COMPONENT FITTING
1560-01-100-1701 An item of unique shapes and cross-sectional configurations specifically designed with dimensional tolerances and finishes. It may be metallic and/or nonmetallic and must be able to mate with or join to like items with aircraft application. The item may consist of more then one (1) piece to form an assembly. Do not use if a more specific item name exists. Excludes BRACKET (1), STRUCTURAL COMPONENT, AIRCRAFT.
Part Alternates: B40809105, B40-809105, SB7301103, SB7301-103, LB9103471, LB9-1034-7-1, 1560-01-100-1701, 01-100-1701, 1560011001701, 011001701
Aircraft and Airframe Structural Components | Airframe Structural Components
| Supply Group (FSG) | NSN Assign. | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 15 | 29 AUG 1980 | 01-100-1701 | 41018 ( FITTING, STRUCTURAL COMPONENT, AIRCRAFT ) |
Demand History | NSN 1560-01-100-1701
| Part Number | Request Date | QTY | Origin |
|---|---|---|---|
| 1560-01-100-1701 | 2023-11-311 | 10 | United States |
| 1560-01-100-1701 | 2021-06-154 | 50 | MANUAL |
| 1560-01-100-1701 | 2020-11-330 | 1 | DIBBS-RFPs |
| B40-809105 | 2020-11-322 | 238 | DIBBS |
| LB9-1034-7-1 | 2020-11-322 | 238 | DIBBS |
| 1560-01-100-1701 | 2020-06-153 | 4 | Poland |
| 1560-01-100-1701 | 2020-03-70 | 50 | TR |
| SB7301-103 | 2019-11-323 | 4 | Poland |
| 1560-01-100-1701 | 2019-02-39 | 50 | TR |
| 1560-01-100-1701 | 2018-11-332 | 50 | United States |
| SB7301103 | 2018-05-129 | 8 | MX |
| 1560-01-100-1701 | 2017-05-124 | 1 | DIBBS-RFPs |
| 1560-01-100-1701 | 2017-01-06 | 1 | DIBBS-RFPs |
| 1560-01-100-1701 | 2016-12-348 | 300 | DIBBS |
| 1560-01-100-1701 | 2016-11-318 | 300 | DIBBS |
| 1560-01-100-1701 | 2016-11-306 | 40 | DIBBS |
| 1560-01-100-1701 | 2016-10-301 | 40 | DIBBS |
| 1560-01-100-1701 | 2016-10-300 | 38 | DIBBS |
| 1560-01-100-1701 | 2016-10-290 | 41 | DIBBS |
| 1560-01-100-1701 | 2016-09-250 | 1 | DIBBS-RFPs |
| 1560-01-100-1701 | 2015-11-327 | 1 | DIBBS-RFPs |
| 1560-01-100-1701 | 2015-08-223 | 311 | DIBBS |
| 1560-01-100-1701 | 2015-07-190 | 35 | TR |
| 1560-01-100-1701 | 2015-07-189 | 35 | MANUAL |
| 1560-01-100-1701 | 2015-05-141 | 230 | DIBBS |
| 1560-01-100-1701 | 2015-04-119 | 242 | DIBBS |
| 1560-01-100-1701 | 2015-04-98 | 109 | DIBBS |
| 1560-01-100-1701 | 2015-03-88 | 133 | DIBBS |
| 1560-01-100-1701 | 2015-01-12 | 133 | DIBBS |
| 1560-01-100-1701 | 2014-11-315 | 213 | DIBBS |
| 1560-01-100-1701 | 2014-10-288 | 411 | DIBBS |
| 1560-01-100-1701 | 2014-08-216 | 245 | DIBBS |
| SB7301103 | 2014-05-148 | 22 | US |
| 1560-01-100-1701 | 2014-03-83 | 167 | DIBBS |
| 1560-01-100-1701 | 2013-11-308 | 4 | US |
| 1560-01-100-1701 | 2013-08-227 | 1 | DIBBS-RFPs |
| 1560-01-100-1701 | 2013-04-119 | 21 | US |
| 1560-01-100-1701 | 2013-04-97 | 20 | Israel |
| 1560-01-100-1701 | 2013-03-70 | 139 | DIBBS |
| 1560-01-100-1701 | 2013-02-55 | 181 | DIBBS |
| 1560-01-100-1701 | 2012-08-227 | 227 | DIBBS |
| SB7301103 | 2012-05-132 | 52 | us |
| 1560-01-100-1701 | 2011-09-259 | 2 | DIBBS |
| 1560-01-100-1701 | 2011-08-213 | 297 | DIBBS |
| 1560-01-100-1701 | 2011-07-195 | 222 | DIBBS |
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Related Products | NSN 1560-01-100-1701
Technical Data | NSN 1560-01-100-1701
| Characteristic | Specifications |
|---|---|
| MATERIAL | ALUMINUM ALLOY 2024 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/4 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 2.875 INCHES NOMINAL |
| OVERALL WIDTH | 2.000 INCHES NOMINAL |
| HEIGHT | 1.362 INCHES NOMINAL |
| III END ITEM IDENTIFICATION | H-60A |
| III PART NAME ASSIGNED BY CONTROLLING AGENCY | PIVOT ASSEMBLY, TAIL ROTOR BLADE |
| MANUFACTURERS CODE | 78286 |
| MFR SOURCE CONTROLLING REFERENCE | SB7301-103 |
Restrictions/Controls & Freight Information | NSN 1560-01-100-1701
| Category | Code | Description |
|---|---|---|
| Shelf-Life Code: | S | 60 months |
| Hazardous Material Indicator Code | P | There is no information in the HMIS; however, the NSN is in an FSC in Table II of Federal Standard 313 and an MSDS may be required by the user. The requirement for an MSDS is dependent on a hazard determination of the supplier or the intended end use of the product |
| Demilitarization Code: | B | Munitions List Item - Mutilation (MUT) to the point of scrap required. (Formerly: Demilitarization not required. Trade Security Controls (TSCs) required at disposition.) |
| Controlled Inventory Item Code: | U | UNCLASSIFIED |
| Precious Metals Indicator Code: | A | Item does not contain precious metal |
| Criticality Code: | F | The item is an Aviation Critical Safety Item/Flight Safety Critical Aircraft Part ((ACSI/FSCAP). |
| Automatic Data Processing Equipment: | 0 | Represents items with no ADP components. NOTE: Codes 1 through 6 are only to be used when the item is Automatic Data Processing Equipment (ADPE) in its entirety and is limited to the type meeting only one of the definitions for codes 1 through 6. (See code 9) |
| Category | Code | Description |
|---|---|---|
| No Freight Information | ||