| Product name | Description | |||
|---|---|---|---|---|
| 70104 | Appearance | Red Liquid | ||
| Boeing Number | 100A | |||
| Boeing Process Specification | BAC5008 | Application of Lubricants | ||
| BAC5054 | Taper Shank Fastener Installation | |||
| BAC5063 | Fastener Installation in Composite Structures | |||
| BAC5492 | Machining and Cutting Titanium | |||
| BAC5540 | Hole Preparation, Machining, and Grinding of Steels | |||
| BAC5578 | Manufacture of Advanced Carbon Fiber Reinforced Advanced Composite Structure with Toughened Epoxy Systems, +350 F Cure | |||
| BAC5657 | Manufacture of Carbon Fiber Reinforced Composite Structure by Automated Fiber Placement, +350 F Cure Epoxy Systems | |||
| 70106 | Appearance | Clear Liquid | ||
| Boeing Number | 100F | |||
| Boeing Process Specification | BAC5008 | Application of Lubricants | ||
| Boeing Process Specification | BAC5008 | Application of Lubricants | ||
| BAC5054 | Taper Shank Fastener Installation | |||
| BAC5063 | Fastener Installation in Composite Structures | |||
| BAC5492 | Machining and Cutting Titanium | |||
| BAC5540 | Hole Preparation, Machining, and Grinding of Steels | |||
| BAC5578 | Manufacture of Advanced Carbon Fiber Reinforced Advanced Composite Structure with Toughened Epoxy Systems, +350 F Cur | |||
| BAC5768 | Mandrel Coldworking of Holes in Aluminum | |||
| BAC5657 | Manufacture of Carbon Fiber Reinforced Composite Structure by Automated Fiber Placement, +350 F Cure Epoxy Systems | |||
| 70305 | Appearance | |||
| Boeing Number | 50B50A | |||
| Boeing Process Specification | BAC5008 | Application of Lubricants | ||
| BAC5054 | Taper Shank Fastener Installation | |||
| BAC5063 | Fastener Installation in Composite Structures | |||
| BAC5540 | Hole Preparation, Machining, and Grinding of Steels | |||
| BAC5768 | Mandrel Coldworking of Holes in Aluminum | |||
| 70307 | Appearance | Blue Medium Paste | ||
| Boeing Process Specification | BAC5008 | Application of Lubricants | ||
| BAC5054 | Taper Shank Fastener Installation | |||
| BAC5063 | Fastener Installation in Composite Structures | |||
| BAC5540 | Hole Preparation, Machining, and Grinding of Steels | |||
| BAC5768 | Mandrel Coldworking of Holes in Aluminum | |||
| 70302 | Appearance | Blue Soft Paste | ||
| Boeing Process Specification | BAC5008 | Application of Lubricants | ||
| BAC5054 | Taper Shank Fastener Installation | |||
| BAC5063 | Fastener Installation in Composite Structures | |||
| BAC5540 | Hole Preparation, Machining, and Grinding of Steels | |||
| 70200 | Appearance | White Solid | ||
| Boeing Number | 16B4F | |||
| Boeing Process Specification | BAC5008 | Application of Lubricants | ||
| BAC5063 | Fastener Installation in Composite Structures | |||
| BAC5540 | Hole Preparation, Machining, and Grinding of Steels | |||
| BAC5578 | Manufacture of Advanced Carbon Fiber Reinforced Advanced Composite Structure withToughened Epoxy Systems, +350 F Cure | |||
| BAC5657 | Manufacture of Carbon Fiber Reinforced Composite Structure by Automated Fiber Placement, +350 F Cure Epoxy Systems | |||
| 70206 | Appearance | White Solid | ||
| Boeing Number | 16B4F | |||
| Boeing Process Specification | BAC5008 | Application of Lubricants | ||
| BAC5063 | Fastener Installation in Composite Structures | |||
| BAC5540 | Hole Preparation, Machining, and Grinding of Steels | |||
| BAC5578 | Manufacture of Advanced Carbon Fiber Reinforced Advanced Composite Structure with Toughened Epoxy Systems, +350 F Cure | |||
| BAC5768 | Mandrel Coldworking of Holes in Aluminum | |||
| BAC5657 | Manufacture of Carbon Fiber Reinforced Composite Structure by Automated Fiber Placement, +350 F Cure Epoxy Systems | |||
| 70201 | Appearance | Pink Solid | ||
| Boeing Number | 16B1A | |||
| Boeing Process Specification | BAC5578 | Manufacture of Advanced Carbon Fiber Reinforced Advanced Composite Structure with Toughened Epoxy Systems, +350 F Cure | ||
| BAC5657 | Manufacture of Carbon Fiber Reinforced Composite Structure by Automated Fiber Placement, +350 F Cure Epoxy Systems | |||
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