Airframe Structural Components: AMC-1500-1, AN-19W, AND10134-1006X9.50
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| AMC-1500-1 AMC15001 | 1560-01-532-2296 | Insulation Pipe Covering, Thermal | Layer Quantity: 1 Fabrication Method: Woven Jacket Material: Aluminum and cloth | Hydraulics International Inc. (2N386,56529) | |
| AMC-1500-2 AMC15002 | 1560-01-532-2291 | Insulation Pipe Covering, Thermal | Layer Quantity: 1 Fabrication Method: Woven Jacket Material: Aluminum and cloth | Hydraulics International Inc. (2N386,56529) | |
| AME 95117-1 AME951171 | 1560-01-471-8602 | Fitting, Structural Component, Air | American Manufacturing & Engineering (0P291) | ||
| AMS-C-7438 AMSC7438 | 1560-01-293-7810 | Core Material | Special Features: Nominal foil thickness 0.0015; designed transverse and transverse direction dimension 96.000 in.; designed ribbon and ribbon direction 48.000 in.; 350.0 deg F max service temp limit; 4.4 lbs per cubic foot density rating; cell perforation not included; 0.980 in. cell depth; 3/16 in. cell size; expanded cell condition; material aluminum alloy, 5056 | Society of Automotive Engineers Inc. (81343) | |
| AN100038 | 1560-00-680-8602 | Cover, Access | Material: Magnesium alloy AZ63A Special Features: GRAY Material Document AND Classification: Ams 4424 assn std single material response | Aeronautical Standards Group (88044) | |
| AN12700-102A AN12700102A | 1560-00-163-3089 | Lever, Stair Ladder | III End Item Identification: Aircraft model C5A | Lockheed Martin Corporation (98897) | |
| AN-19W AN19W | 1560-01-457-8396 | Covering, External Surface, Aircra | End Item Identification: Aircraft C-17A | Orcon Corporation (23788) | |
| AN3437-1-11 AN3437111 | 1560-01-413-2236 | Insulation, Thermal, Special Purpo | Special Features: C-130 aircraft | Aeronautical Standards Group (88044) Lockheed Martin Corporation (98897) | |
| AN4043-2 AN40432 | 1560-00-090-4484 | Cock-Water Detector, Fuel Tank | General Characteristics Item Description: Potassium chromate purified crystals req for water detection, O/a dim 3.880 in. max lg incl cock and cylinder, 1.260 in. max dia, W/ shrink fit secured cap, W/integral screen, 100 mesh psi, 0.0253 in. min, 0.0263 in. max dia wire, thd mtd 1 IN.-14 size, uns class 3A thd, 0.406 in. lg, rh thd, sq wrenching 0.750 in. W across flats, drilled for lock wire, self-locking poppet drain cock, body style 7 drilled for lock wire | Aeronautical Standards Group (88044) | |
| AN4122-3 AN41223 | 1560-00-564-1315 | Adapter, Filler cap | General Characteristics Item Description: Steel, QQ-S-698, cadmium-plated, 7.000 in. dia, 3.000 in. dia of aperture | Aeronautical Standards Group (88044) | |
| AN5766-40 AN576640 | 1560-01-456-7325 | Fitting, Structural Component, Aircraft | Aeronautical Standards Group (88044) | ||
| AN775-4 AN7754 | 1560-00-780-3755 | Retainer, Seal, Meergency Exit | III End Item Identification: Aircraft model C141 General Characteristics Item Description: Aluminum alloy, AMS4156 | Aeronautical Standards Group (88044) | |
| ANAAR-45 ANAAR45 | 1560-01-052-0309 | Pod Assembly | III End Item Identification: Aircraft model A-7E | Joint Electronics Type Designation (80058) | |
| ANB7203-1 ANB72031 | 1560-01-552-3692 | Frame, Aircraft | III End Item Identification: KDC-10 tanker aircraft | The Boeing Company (81205) | |
| ANCRA4-0000-11 ANCRA4000011 | 1560-01-286-1030 | Plate, Structural, Aircraft | III End Item Identification: Acft model HH65A cabin floor, rh, P/N 366A21-0105-1001 Special Features: Overall DIA.1.750 in.;overall thickness 0.438 in.;includes two drilled countersunk holes 0.188 in.dia.;locking or anchoring feature included | Ancra Southwest Inc. (2X618) | |
| AND10132-2002 7075T6511 AND1013220027075T6511 | 1560-01-528-0311 | Support, Structural Component, Air | III End Item Identification: UH1 aircraft III Part Name Assigned BY Controlling Agency: Extrusion Criticality Code Justification: AGAV | Bell Helicopter Textron Inc. (97499) | |
| AND10133-1002 AND101331002 | 1560-01-206-5119 | Support, Structural Component, Air | III End Item Identification: 1520-00-859-2670 Special Features: Aluminum alloy 7075 QQ-A-200/11, T6; 0.094 in. matl thk; 1.000 in. W both legs; 12.200 in. O/a lg; l cross section; W/O rivet holes III Part Name Assigned BY Controlling Agency: Type/model DESIGNATION:UH-1D | Airforce-Navy Aeronautical Design (99237) | |
| AND10133-1002 AND101331002 | 1560-01-207-2514 | Support, Structural Component, Air | III End Item Identification: 1520-00-859-2670 Special Features: Aluminum alloy 7075 QQ-A-200/11, T6; 0.094 in. matl thk; 1.000 in. W both legs; 13.000 in. O/a lg; l cross section; W/O rivet holes III Part Name Assigned BY Controlling Agency: Type/model DESIGNATION:UH-1D | Airforce-Navy Aeronautical Design (99237) | |
| AND10133-1201 AND101331201 | 1560-01-206-5118 | Support, Structural Component, Air | III End Item Identification: 1520-00-859-2670 Special Features: Aluminum alloy 7075 QQ-A-200/11, T6; 0.063 in. matl thk; 1.250 in. W both legs; 18.500 in. lg; l cross section; W/O rivet holes III Part Name Assigned BY Controlling Agency: Type/model DESIGNATION:UH-1D | Airforce-Navy Aeronautical Design (99237) | |
| AND10134-1003 AND101341003 | 1560-01-208-3210 | Support, Structural Component, Air | Airforce-Navy Aeronautical Design (99237) | ||
| AND10134-1003 AND101341003 | 1560-01-208-3211 | Support, Structural Component, Air | Airforce-Navy Aeronautical Design (99237) | ||
| AND10134-1006X9.50 AND101341006X950 | 1560-01-221-6649 | Support, Structural Component, Air | Airforce-Navy Aeronautical Design (99237) | ||
| AND10134-1006X9.50 AND101341006X950 | 1560-01-221-6650 | Support, Structural Component, Air | Airforce-Navy Aeronautical Design (99237) | ||
| AND10134-1006X9.50 AND101341006X950 | 1560-01-221-6652 | Support, Structural Component, Air | Airforce-Navy Aeronautical Design (99237) |