Fastening Devices: GS501APD10A, GS501APD10D, GS501A-SD6B
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| GS501APD10A | 5325-00-717-9697 | Insert, Panel Fastener | Shoulder Diameter: 0.309 inches nominal Flange Diameter: 0.625 inches nominal Material Accommodated Thickness: 0.250 inches nominal | Northrop Grumman Systems Corporation (26512) | |
| GS501APD10C | 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) | |
| GS501A-PD10D GS501APD10D | 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) | |
| GS501APD10D | 5325-00-522-4882 | Insert, Panel Fastener | Material: Aluminum alloy 2024 overall Surface Treatment: Anodize overall Material Accommodated Thickness: 0.312 inches nominal | Alcoa Global Fasteners Inc. (29372) Young Engineers Inc., The (56958) | |
| GS501A-PD25A GS501APD25A | 5325-01-513-5495 | Insert, Panel Fastener | Material: Aluminum alloy overall Surface Treatment: Chromate overall Material Accommodated Thickness: 0.250 inches nominal | Northrop Grumman Systems Corporation (26512) | |
| GS501A-PD6A GS501APD6A | 5325-01-513-5496 | Insert, Panel Fastener | Material: Aluminum alloy overall Surface Treatment: Chromate overall Material Accommodated Thickness: 0.250 inches nominal | Northrop Grumman Systems Corporation (26512) | |
| GS501A-PD8A GS501APD8A | 5325-01-440-5249 | 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) | |
| GS501A-PF10B GS501APF10B | 5325-00-574-3373 | Insert, Panel Fastener | Material: Aluminum alloy 2024 overall Surface Treatment: Anodize overall Material Accommodated Thickness: 0.531 inches nominal | Northrop Grumman Systems Corporation (26512) | |
| GS501A-PF10C GS501APF10C | 5325-00-522-4881 | Insert, Panel Fastener | Material: Aluminum alloy 2024 overall Surface Treatment: Anodize overall Material Accommodated Thickness: 0.562 inches nominal | Northrop Grumman Systems Corporation (26512) | |
| GS501A-PF8A GS501APF8A | 5325-01-293-6713 | Insert, Panel Fastener | Material: Aluminum alloy 2024 overall Surface Treatment: Chromate overall Material Document and Classification: QQ-A-225/6, T4 or T351 fed spec single material response overall | Alcoa Global Fasteners Inc. (29372) Northrop Grumman Systems Corporation (26512) Young Engineers Inc., The (56958) | |
| GS501APP10A | 5325-00-717-9697 | Insert, Panel Fastener | Shoulder Diameter: 0.309 inches nominal Flange Diameter: 0.625 inches nominal Material Accommodated Thickness: 0.250 inches nominal | Northrop Grumman Systems Corporation (26512) | |
| GS501A-SD10A GS501ASD10A | 5325-00-911-8222 | 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) Young Engineers Inc., The (56958) | |
| GS501A-SD10B GS501ASD10B | 5325-00-701-2552 | 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) Young Engineers Inc., The (56958) | |
| GS501A-SD10C GS501ASD10C | 5325-00-574-3379 | Insert, Panel Fastener | Material: Aluminum alloy overall Surface Treatment: Anodize overall Special Features: 0.375 inches long | Northrop Grumman Systems Corporation (26512) | |
| GS501A-SD10D GS501ASD10D | 5325-00-704-0704 | 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) Young Engineers Inc., The (56958) | |
| GS501A-SD10E GS501ASD10E | 5325-00-566-4247 | Insert, Panel Fastener | Material: Aluminum alloy 2024 overall Surface Treatment: Anodize overall Material Document and Classification: MIL-C-5541 mil spec single material response overall | Northrop Grumman Systems Corporation (26512) | |
| GS501A-SD10G GS501ASD10G | 5325-01-320-7261 | Insert, Panel Fastener | Material: Aluminum alloy 2024 overall Surface Treatment: Chromate overall Material Document and Classification: QQ-A-225/6, T4 or T351 fed spec single material response overall | Northrop Grumman Systems Corporation (26512) | |
| GS501A-SD25B GS501ASD25B | 5325-01-513-5498 | Insert, Panel Fastener | Material: Aluminum alloy overall Surface Treatment: Chromate overall Hole Type: Unthreaded-counterbored | Northrop Grumman Systems Corporation (26512) | |
| GS501A-SD25D GS501ASD25D | 5325-00-983-7393 | Insert, Panel Fastener | Material: Aluminum alloy 2024 overall Surface Treatment: Anodize overall Surface Treatment Document and Classification: MIL-A-8625 mil spec single treatment response overall | Alcoa Global Fasteners Inc. (29372) Northrop Grumman Systems Corporation (26512) Young Engineers Inc., The (56958) | |
| GS501A-SD6B GS501ASD6B | 5325-01-513-5499 | Insert, Panel Fastener | Material: Aluminum alloy overall Surface Treatment: Chromate overall Hole Type: Unthreaded-counterbored | Northrop Grumman Systems Corporation (26512) |