Fastening Devices: GS500G3-48T5, GS501A-PC8A, GS501APD100
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| GS500G3-48T5 GS500G348T5 | 5325-00-076-2214 | Insert, Panel Fastener | Material: Aluminum alloy overall Surface Treatment: Chromate overall Special Features: 0.480 in. core thk and thru-threads | Alcoa Global Fasteners Inc. (29372) Northrop Grumman Systems Corporation (26512) | |
| GS500G3-50-5 GS500G3505 | 5325-00-027-0481 | Fastener Assy, Panel | General Characteristics Item Description: Body, aluminum alloy, QQ-A-225/6, comp 2024, T4, sleeve, aluminumalloy, WW-T-700/6, comp 6061, T6, insert, nylon /zytel/ or equivalent, THD0.190-32, unf, 0.500 in. core thk, 0.500 in. min, 0.599 in. max panel thkrange | Northrop Grumman Systems Corporation (26512) | |
| GS500G3-64-7 GS500G3647 | 5325-01-090-7308 | Insert, Panel Fastener | Material: Aluminum alloy overall Surface Treatment: Chromate overall Special Features: 0.640 in. core thk | Alcoa Global Fasteners Inc. (29372) Northrop Grumman Systems Corporation (26512) | |
| GS500G3-78-8 GS500G3788 | 5325-01-067-8683 | Insert, Panel Fastener | Material: Aluminum alloy overall Surface Treatment: Chromate overall Special Features: 0.780 in. core thk | Northrop Grumman Systems Corporation (26512) | |
| GS500G3-82-8 GS500G3828 | 5325-00-497-0282 | Insert, Screw Thread | Surface Treatment: Chromate overall Length: 0.750 inches nominal Surface Treatment Document and Classification: MIL-C-5541 mil spec single treatment response overall | Northrop Grumman Systems Corporation (26512) | |
| GS500G4-48-50 GS500G44850 | 5325-00-076-2215 | Insert, Panel Fastener | Material: Aluminum alloy overall Surface Treatment: Chromate overall Special Features: 0.480 in. core thk | Northrop Grumman Systems Corporation (26512) | |
| GS500G4-48T50 GS500G448T50 | 5325-00-204-5454 | Insert, Panel Fastener | Material: Aluminum alloy 2024 overall Surface Treatment: Chromate overall Material Document and Classification: QQ-A-225/6, T4 fed spec single material response overall | Northrop Grumman Systems Corporation (26512) | |
| GS500G4-81-8 GS500G4818 | 5325-00-240-1867 | Insert, Panel Fastener | Material: Aluminum alloy overall Surface Treatment: Chromate overall Special Features: 0.810 in. core thk | Northrop Grumman Systems Corporation (26512) | |
| GS500G4-86-9 GS500G4869 | 5325-01-253-3761 | Insert, Panel Fastener | Material: Aluminum alloy 6061 eyelet aluminum alloy 2024 overall Surface Treatment: Chromate eyelet chromate overall Material Document and Classification: WW-T-789, T6 fed spec single material response eyelet QQ-A-225/6, T4 fed spec single material response overall | Northrop Grumman Systems Corporation (26512) | |
| GS500G5-48-5 GS500G5485 | 5325-01-116-1637 | Insert, Screw Thread | Surface Treatment: Chromate overall Length: 0.450 inches nominal Surface Treatment Document and Classification: MIL-C-5541 mil spec single treatment response overall | Northrop Grumman Systems Corporation (26512) | |
| GS500H04C12 | 5325-01-127-7235 | Fastener, Panel | General Characteristics Item Description: Steel, aisi 303, passivated; internal thread size 4-40 unc 2B; 0.160 in. min, 0.165 in. max od; 0.380 in. lg | Northrop Grumman Systems Corporation (26512) | |
| GS500V1032-10 GS500V103210 | 5325-00-915-2389 | Insert, Panel Fastener | Material: Steel comp 1006 or steel comp 1008 or steel comp 1010 or steel comp 1012 or steel comp 1015 or steel comp 1016 or steel comp 1017 or steel comp 1018 or steel comp 1019 or steel comp 1020 or steel comp 1021 or steel comp 1022 or steel comp 1025 or steel comp 1030 or steel comp 1035 or steel comp 1040 overall Surface Treatment: Cadmium and chromate overall Material Document and Classification: 66 fed std all material responses overall | Alcoa Global Fasteners Inc. (29372) Northrop Grumman Systems Corporation (26512) | |
| GS501A | 5325-00-972-3357 | Insert, Panel Fastener | Material: Aluminum alloy overall Surface Treatment: Anodize overall Special Features: 0.531 in. panel thk | Northrop Grumman Systems Corporation (26512) | |
| GS501AP10D | 5325-00-253-8711 | Insert, Panel Fastener | Material: Aluminum alloy 2024 overall Surface Treatment: Anodize overall Material Accommodated Thickness: 0.344 inches nominal | Northrop Grumman Systems Corporation (26512) | |
| GS501APC10A | 5325-00-716-3561 | Insert, Panel Fastener | Shoulder Diameter: 0.309 inches nominal Flange Diameter: 0.625 inches nominal Hole Type: Plain | Northrop Grumman Systems Corporation (26512) Young Engineers Inc., The (56958) | |
| GS501A-PC10B GS501APC10B | 5325-00-972-3357 | Insert, Panel Fastener | Material: Aluminum alloy overall Surface Treatment: Anodize overall Special Features: 0.531 in. panel thk | Northrop Grumman Systems Corporation (26512) | |
| GS501A-PC10-C GS501APC10C | 5325-00-522-4883 | Insert, Panel Fastener | Material: Aluminum alloy 2024 overall Surface Treatment: Anodize overall Material Accommodated Thickness: 0.312 inches nominal | Northrop Grumman Systems Corporation (26512) | |
| GS501A-PC10D GS501APC10D | 5325-01-066-9534 | Insert, Panel Fastener | Material: Aluminum alloy 2024 overall Surface Treatment: Anodize overall Material Document and Classification: QQ-A-225/6, T4 fed spec single material response overall | Northrop Grumman Systems Corporation (26512) | |
| GS501A-PC8A GS501APC8A | 5325-01-440-5248 | Insert, Panel Fastener | Material: Aluminum alloy 2024 overall Surface Treatment: Anodize overall Material Document and Classification: QQ-A-225/6 fed spec single material response overall | Northrop Grumman Systems Corporation (26512) | |
| GS501APD100 | 5325-00-522-4882 | Insert, Panel Fastener | Material: Aluminum alloy 2024 overall Surface Treatment: Anodize overall Material Accommodated Thickness: 0.312 inches nominal | Northrop Grumman Systems Corporation (26512) |