Nuts and Washers: 749B208P1BFR, 74A120612-2003, 74A170717-2001
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 749B208P1BFR | 5310-01-331-8121 | Nut, Plain, Hexagon | Criticality Code Justification: ZZZY Reference Number Differentiating Characteristics: Material will be in accordance with navicp mech; activity hx quality control, manufacturing and testing specifications. | General Electric Co. (24446) Naval Inventory Control Point (03950) | |
| 749B208REVBPCALL | 5310-00-613-9831 | Nut, Covered | Criticality Code Justification: ZZZY Reference Number Differentiating Characteristics: Material will be in accordance with navicp mech; activity hx quality control, manufacturing and testing specifications. | General Electric Co. (24446) | |
| 749-D-6 749D6 | 5310-01-309-2568 | Washer, Flat | Lawler Manufacturing Co. Inc. (75545) | ||
| 749PC18 | 5310-00-627-5676 | Washer | Clark-Reliance Corporation (95094) | ||
| 74A10534-2001 74A105342001 | 5310-01-116-1422 | Nut, Plain, Slotted, Hexagon | Material: Aluminum alloy 7075 overall Material Document and Classification: QQ-A-225/9 fed spec single material response overall Hardness Rating: Not rated | Associated Aircraft Manufacturing (56540) | |
| 74A10551 | 5310-01-121-8528 | Washer, Shouldered and Recessed | Hole Diameter: 2.9700 inches minimum and 2.9750 inches maximum Shoulder Diameter: 3.1900 inches minimum and 3.1915 inches maximum Outside Diameter: 3.504 inches minimum and 3.506 inches maximum | Goodrich Corporation (13002) | |
| 74A110681-2001 74A1106812001 | 5310-01-131-2957 | Washer, Shouldered and Recessed | Hole Diameter: 0.312 inches minimum and 0.319 inches maximum Shoulder Diameter: 1.750 inches nominal Outside Diameter: 2.900 inches nominal | Boeing Company, The (76301) Steelville Manufacturing Co. (25989) Triumph Structures - Wichita Inc. (1U854) | |
| 74A110681-2003 74A1106812003 | 5310-01-131-2958 | Washer, Shouldered and Recessed | Hole Diameter: 0.312 inches minimum and 0.319 inches maximum Shoulder Diameter: 1.830 inches nominal Outside Diameter: 2.900 inches nominal | Boeing Company, The (76301) Steelville Manufacturing Co. (25989) Triumph Structures - Wichita Inc. (1U854) | |
| 74A110896-2001 74A1108962001 | 5310-01-132-2195 | Washer, Convex | Material: Aluminum alloy 7075 overall Hole Diameter: 0.312 inches minimum and 0.319 inches maximum Material Thickness: 0.480 inches nominal | Boeing Company, The (76301) Calaine Enterprises (7M356) Pioneer Machine Products Inc. (12829) | |
| 74A110934-1001 74A1109341001 | 5310-01-265-2442 | Nut Assembly, Self-Locking, Gang C | Material: Aluminum alloy 7076 overall Material Document and Classification: QQ-A-250/13, cond T6 fed spec single material response overall Special Features: Consist of 1 plate P/N 74A110934-2001, 2 platenut P/N ST3M442-3A1, 14 platenut P/N ST3M443-4A2, 28 rivet P/N rivet P/N ST3M793-3-2 | Boeing Company, The (76301) | |
| 74A110934-1007 74A1109341007 | 5310-01-265-2441 | Nut Assembly, Self-Locking, Gang C | Material: Aluminum alloy 7076 overall Material Document and Classification: QQ-A-250/13, cond T6 fed spec single material response overall Special Features: Consist of 1 plate P/N 74A110934-2007, 2 platenut P/N ST3M442-3A1, 14 platenut P/N ST3M443-4A2, 28 rivet P/N NAS1097AD3 | Boeing Company, The (76301) | |
| 74A120612-2001 74A1206122001 | 5310-01-477-5945 | Nut Assembly, Retainer Ring | III End Item Identification: Fairing, aircraft F/a 18 E-F | Boeing Company, The (76301) | |
| 74A120612-2003 74A1206122003 | 5310-01-477-5946 | Nut Assembly, Retainer Ring | III End Item Identification: F/A18 E-F, fairing aircraft Special Features: Item previously known as nut assembly, self-locking | Boeing Company, The (76301) | |
| 74A120913-2001 74A1209132001 | 5310-01-477-5579 | Washer, Shouldered | III End Item Identification: Wing installation F/a 18E model code to support ECP6038 Special Features: Item also known as washer, shouldered, aircraft Criticality Code Justification: AGAV | Boeing Company, The (76301) | |
| 74A120914-2001 74A1209142001 | 5310-01-477-5580 | Washer, Shouldered | III End Item Identification: Wing installation F/a 18E-F model code to support ECP6038 Special Features: Item also known as washer, shouldered, aircraft Criticality Code Justification: AGAV | Boeing Company, The (76301) | |
| 74A150787-2005 74A1507872005 | 5310-01-131-2946 | Nut, Self-Locking, Plate | Material: Aluminum alloy 7075 base iron alloy 660 nut Material Document and Classification: QQ-A-250/13, temper T6 fed spec single material response base ams 5525 assn std single material response or ams 5732 assn std single material response nut Surface Treatment: Nickel and copper or copper nut | Boeing Company, The (76301) | |
| 74A150790-2001 74A1507902001 | 5310-01-193-4516 | Nut, Plain, Hexagon | Boeing Company, The (76301) | ||
| 74A150791-2001 74A1507912001 | 5310-01-193-0165 | Washer, key | Boeing Company, The (76301) | ||
| 74A16L | 5310-00-264-1106 | Washer, Flat | Material: Copper alloy overall Hole Diameter: 0.284 inches nominal Peripheral Shape Style: 1 round | Hewlett-Packard Co. (52983) Philips Electronics North America (0ZBJ4) | |
| 74A170717-2001 74A1707172001 | 5310-01-272-5471 | Washer, Recessed | Material: Plastic acetal overall Hole Diameter: 0.098 inches nominal Material Thickness: 0.054 inches nominal | Boeing Company, The (76301) |