Airframe Structural Components: A51B13127-73, A51B13532-11, A51B13534-11
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| A51B13127-73 A51B1312773 | 1560-00-421-8464 | Skin, Aircraft | III End Item Identification: Aircraft, F-14 Aircraft Mission Design Series: F-14 Material: Aluminum alloy 2024 | Northrop Grumman Systems Corporation (26512,61174) | |
| A51B13128-3 A51B131283 | 1560-00-351-6872 | Radome | III FSC Application Data: Fuselage, airframe Radome Flexibility: Rigid Pressurizing Device: Not included | Northrop Grumman Systems Corporation (26512,61174) | |
| A51B13128-4 A51B131284 | 1560-00-351-6874 | Radome | III FSC Application Data: Fuselage, airframe Radome Flexibility: Rigid Pressurizing Device: Not included | Northrop Grumman Systems Corporation (26512,61174) | |
| A51B13129-1 A51B131291 | 1560-00-411-0959 | Pan, Antenna Mounting | General Characteristics Item Description: Aluminum alloy, QQ-A-250/4, composition 2024, temper T4, irregular shape, 14.00 in. l, 13.00 in. W, 0.032 in. thk | Aero Components Inc. (59213) Maven Engineering Corporation (65273) Northrop Grumman Systems Corporation (26512,61174) | |
| A51B13129-3 A51B131293 | 1560-00-411-1047 | Pan, Antenna Mounting | General Characteristics Item Description: Aluminum alloy, QQ-A-250/4, composition 2024, temper T4, irregular shape, 14.00 in. l, 13.00 in. W, 0.032 in. thk | Aero Components Inc. (59213) Maven Engineering Corporation (65273) Northrop Grumman Systems Corporation (26512,61174) | |
| A51B13130-19 A51B1313019 | 1560-01-327-1111 | Stiffener, Aircraft | Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/4 fed spec single material response | Northrop Grumman Systems Corporation (26512,61174) | |
| A51B13132-23 A51B1313223 | 1560-01-327-1118 | Web, Structural Component, Aircraf | Material: Aluminum alloy | Northrop Grumman Systems Corporation (26512,61174) | |
| A51B13133-13 A51B1313313 | 1560-01-327-1110 | Frame, Aircraft | Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/4 fed spec single material response | Northrop Grumman Systems Corporation (26512,61174) | |
| A51B13140-3 A51B131403 | 1560-01-039-0945 | Skin, Aircraft | Special Features: Aluminum alloy filler QQ-A-250/4, type 2024, temper T81, cres skin MIL-S-25043, type 17-7PH, passivated MIL-S-5002, rockwell scale C 38-45 | Northrop Grumman Systems Corporation (26512,61174) | |
| A51B13143-15 A51B1314315 | 1560-01-242-2127 | Skin, Aircraft | III End Item Identification: Aircraft model F-14A Special Features: Steel, MIL-S-25043, comp 17-7PH, passivate, MIL-S-5002, epoxy polyamide, GP111V1, cagec 26512; 0.090 in. thk | Northrop Grumman Systems Corporation (26512,61174) | |
| A51B13143-3 A51B131433 | 1560-01-239-9556 | RIB | III End Item Identification: Aircraft model F-14A General Characteristics Item Description: Steel, corrosion resisting, MIL-S-25043, 17-7PH, passivate, MIL-S-5002, epoxy polyamide; 0.090 in. thk; furnished W/ solid rivets, clips | Northrop Grumman Systems Corporation (26512,61174) | |
| A51B13500-15 A51B1350015 | 1560-01-240-8239 | Panel, Structural, Aircraft | III End Item Identification: Acft model F-14A | Northrop Grumman Systems Corporation (26512,61174) | |
| A51B13513-13 A51B1351313 | 1560-00-421-8478 | Fitting | General Characteristics Item Description: Aluminum, 7.615 in. lg, 2.700 in. W, 1.126 in. H | Northrop Grumman Systems Corporation (26512,61174) | |
| A51B13514-13 A51B1351413 | 1560-00-413-2183 | Fitting, Splice Longeron Dome | III End Item Identification: Aircraft model F-14A General Characteristics Item Description: Aluminum, 7.590 in. O/a lg, 1.131 in. O/a H | Northrop Grumman Systems Corporation (26512,61174) | |
| A51B13514-14 A51B1351414 | 1560-00-413-2190 | Fitting, Splice Longeron Dome | III End Item Identification: Aircraft model F-14A General Characteristics Item Description: Aluminum, 7.590 in. O/alg, 1.131 in. O/a H | Northrop Grumman Systems Corporation (26512,61174) | |
| A51B13520-11 A51B1352011 | 1560-00-406-5295 | Support, Actuator | General Characteristics Item Description: 3.160 in. lg, 2.090 in. H, 2.600 in. W, material aluminum | Northrop Grumman Systems Corporation (26512,61174) | |
| A51B13531-13 A51B1353113 | 1560-00-411-1348 | Fitting, Splice Longeron | General Characteristics Item Description: Aluminum alloy, composition 2024-T6, GM2015 fscm 26512, 7.620 in. lg 2.700 in. W, 1.200 in. thk | Northrop Grumman Systems Corporation (26512,61174) | |
| A51B13532-11 A51B1353211 | 1560-01-272-5165 | Frame Segment, Radome | General Characteristics Item Description: Aluminum alloy, GM2007, grumman aerospace corp, alloy 2024, T851; gloss polyurethane, MIL-P-23377; color white | Northrop Grumman Systems Corporation (26512,61174) | |
| A51B13533-11 A51B1353311 | 1560-00-413-2173 | Fitting, Shear | General Characteristics Item Description: Steel MIL-S-8844, comp 4340, 1.72 in. W, 2.75 in. lg, 0.66 in.thk | Howe Machine & Tool Corp. (65777) Maven Engineering Corporation (65273) Northrop Grumman Systems Corporation (26512,61174) | |
| A51B13534-11 A51B1353411 | 1560-00-413-2174 | Fitting, Shear | General Characteristics Item Description: 3.250 in. approx lg, 1.700 in. O/a W, 0.660 in. O/a H, material steel, finish cadmium plated | Northrop Grumman Systems Corporation (26512,61174) |