We appreciate your interest in Boeing Company The part number L3226602-003, which is currently ready for procurement here on Prompt Aerospace. For your reference, part number L3226602-003 is listed with the NSN 1560-01-454-8127 and description “Skin Aircraft.” If this is the item you are seeking and you would like to request a quote for your comparisons, simply complete the form below with information like your desired quantity, budget, and anticipated fulfillment timeframe. We regularly respond to requests within 15 minutes of receiving them, using the details we are offered to curate the most ideal purchasing options.
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If you want to explore other items produced by Boeing Company The under the CAGE Code 43999 or that similarly fall under the FSC 1560 Airframe Structural Components, keep in mind that since we list everything with relevant information, you can easily locate related part numbers using our search engine or catalogs. We also excel at tracking down parts with long lead times or that are generally hard to find, meaning that we can serve you even if you do not see exactly what you need on our website. With all of this being said, we are ready to help you source any of the NSN 1560-01-454-8127 parts and Skin Aircraft items your operations require, so request a quote today.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 1560-01-454-8127 Item PartTypeName: SKIN,AIRCRAFT | 1560 | 014548127 | 0 | P | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| 7 | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| L3226602-003 | 6 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABHP | OVERALL LENGTH | 38.000 INCHES NOMINAL |
| ABMK | OVERALL WIDTH | 31.600 INCHES NOMINAL |
| ABNM | THICKNESS | 0.125 INCHES NOMINAL |
| CZDJ | AIRCRAFT LOCATION | NACELLE |
| CZEJ | AIRCRAFT STATION NUMBER | STA YN87.2 TO STA YN117.8 |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | B-1B |
| FEAT | SPECIAL FEATURES | NUCLEAR HARDNESS CRITICAL ITEM; MATL: 2024-T3 CLAD ALUM ALLOY SHT;HEAT TREAT TO TEMPER T81 PER ST0111LA0009; DWG NOTE: (HCP) GAP TOLERANCE BETWEEN THIS PART & ADJACENT PARTS:000 TO .060MAX; OPPOSITE -004; N/A:L3226010; U/O ACFT 1 & SUBQ |
| MATT | III MATERIAL | ALUMINUM ALLOY 2024 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5 FED SPEC SINGLE MATERIAL RESPONSE |
| NHCF | NUCLEAR HARDNESS CRITICAL FEATURE | HARDENED |
| ABHP | OVERALL LENGTH | 38.000 INCHES NOMINAL |
| ABMK | OVERALL WIDTH | 31.600 INCHES NOMINAL |
| ABNM | THICKNESS | 0.125 INCHES NOMINAL |
| CZDJ | AIRCRAFT LOCATION | NACELLE |
| CZEJ | AIRCRAFT STATION NUMBER | STA YN87.2 TO STA YN117.8 |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | B-1B |
| FEAT | SPECIAL FEATURES | NUCLEAR HARDNESS CRITICAL ITEM; MATL: 2024-T3 CLAD ALUM ALLOY SHT;HEAT TREAT TO TEMPER T81 PER ST0111LA0009; DWG NOTE: (HCP) GAP TOLERANCE BETWEEN THIS PART & ADJACENT PARTS:000 TO .060MAX; OPPOSITE -004; N/A:L3226010; U/O ACFT 1 & SUBQ |
| MATT | III MATERIAL | ALUMINUM ALLOY 2024 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5 FED SPEC SINGLE MATERIAL RESPONSE |
| NHCF | NUCLEAR HARDNESS CRITICAL FEATURE | HARDENED |
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