FSC 5340 Commercial Hardware: 5340-01-509-4488, 5340-01-509-4703, 5340-01-509-4755
| NSN | MFG SKU | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 5340-01-509-4488 5340015094488 | 70243 | Catch, Magnetic | Special Features: Need to order two III End Item Identification: For curing system, light model: triad 2000 | Dentsply International Inc. (16969) | |
| 5340-01-509-4490 5340015094490 | 6392233 | Bracket, Double Angle | Material: Nickel alloy 625 Style Designator: 13 adjacent angles Material Document and Classification: ASTM-B443, grade 1 assn std single material response | Naval SEA Systems Command (53711) | |
| 5340-01-509-4529 5340015094529 | 11463353-3 | Frame, Air Inlet-Outlet | Material: Steel comp 304 overall Style Designator: F1 rectangular Material Document and Classification: QQ-S-766, class 304, cond a fed spec single material response overall | U S Army Aviation and Missile (18876) | |
| 5340-01-509-4550 5340015094550 | 23052508 | Holder, Special | General Characteristics Item Description: Item used on AE2100 aircraft engine on the C-130J aircraft | Rolls-Royce Corporation (63005) | |
| 5340-01-509-4551 5340015094551 | 23052509 | Holder, Special | General Characteristics Item Description: Item used on AE2100 aircraft engine on the C-130J aircraft | Rolls-Royce Corporation (63005) | |
| 5340-01-509-4552 5340015094552 | 23052511 | Support, Special | General Characteristics Item Description: Item used on AE2100 aircraft engine on the C-130J aircraft | Rolls-Royce Corporation (63005) | |
| 5340-01-509-4553 5340015094553 | 23052512 | Pedestal | General Characteristics Item Description: Item used on AE2100 aircraft engine on the C-130J aircraft | Rolls-Royce Corporation (63005) | |
| 5340-01-509-4556 5340015094556 | 23052515 | Holder, Special | General Characteristics Item Description: Item used on AE2100 aircraft engine on the C-130J aircraft | Rolls-Royce Corporation (63005) | |
| 5340-01-509-4564 5340015094564 | 23052520-7 | Gripper | General Characteristics Item Description: Item used on AE2100 aircraft engine on the C-130J aircraft | Rolls-Royce Corporation (63005) | |
| 5340-01-509-4566 5340015094566 | 23060631 | Alignment Wedge | Rolls-Royce Corporation (63005) | ||
| 5340-01-509-4588 5340015094588 | 3220-01-0004 | Cover, Protective, Dust and Moistu | End Item Identification: MRC-85 Open End Inside Diameter: 0.765 inches nominal | McDowell Research Co. Inc. (0VJU1) | |
| 5340-01-509-4651 5340015094651 | 17G690777-15 | Pad, Cushioning | Boeing Company, The (88277) | ||
| 5340-01-509-4687 5340015094687 | 12369740 | Bracket, Mounting | U S Army Tank Automotive Command (19207) | ||
| 5340-01-509-4703 5340015094703 | 7004108 | Cap, Protective, Dust and Moisture | Marine Corps Systems Command (0MLM6) | ||
| 5340-01-509-4712 5340015094712 | 7326452-4 | Bracket, Angle | Material: Aluminum alloy 5052 Style Designator: 6 angle Special Features: Has two additional slots directly in line with others on leg 2 center positioned 1.750 inches and 3.750 inches from slot 3 respectfully; portion of bracket beginning at 1.480 inches from outside corner of where leg one and two are joined and extending 2.730 inches down leg one is angled back to a distance of 0.880 inches | Naval SEA Systems Command (53711) Northrop Grumman Systems Corporation (31442) | |
| 5340-01-509-4719 5340015094719 | POP-1000 BLACK | Cap, Protective, Dust and Moisture | Material: Plastic polyhexamethylene adipamide End Item Identification: Cbil/D Design Type: Friction | Heyco Inc. (28520) | |
| 5340-01-509-4724 5340015094724 | 7326347-01 | Bracket Assembly, Weldment, Type 1 | Material: Titanium alloy Special Features: Made up of 1 base plate and 8 variable shaped sheets, welded together and then painted Overall Width: 8.750 inches nominal | Northrop Grumman Systems Corporation (31442) Naval SEA Systems Command (53711) | |
| 5340-01-509-4734 5340015094734 | 6391073 | Bracket, Mounting | Material: Aluminum alloy 5086 Special Features: Bottom front edge is cut off 0.500 X 0.500 inch on each side; mounting holes on front are centered 0.515 from top edge and 1.625 from each side; top has 2 holes thd for 0.375-16 UNC-2B helical coil insert (per MS33537, assembled wet) centered 0.985 from front edge and 0.750 from each side Material Document and Classification: Astm B209, temper H32 assn std single material response | Naval SEA Systems Command (53711) Northrop Grumman Systems Corporation (31442) | |
| 5340-01-509-4740 5340015094740 | 7326298-1 | Plate, T | Material: Aluminum alloy 6061 Style Designator: 85 tee Special Features: Has additional mounting holes with 0.281 inch diameters | Northrop Grumman Systems Corporation (31442) Naval SEA Systems Command (53711) | |
| 5340-01-509-4755 5340015094755 | 6393032 | Bracket, Angle | Material: Steel Style Designator: 6 angle Special Features: Second leg has arched cutout on right edge with radius of 0.266 centered 1.056 from bottom and 0.434 from right edge | Northrop Grumman Systems Corporation (31442) Naval SEA Systems Command (53711) |