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 |