Attach_4_Boeing_STL_00A0060.pdf
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- Attached to
- Aircraft Components and Accessories
- Solicitation number
- FA8505-13-R-31129
About this file
Attach 4 Boeing STL 00A0060 (BOEING REPORT STL00A0060)
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Other files
| File | Type | Posted |
|---|---|---|
| FA850513R31129______0002.pdf | ||
| Q A_6_PAD.docx | DOCX document | |
| Passive_Attack_Display_(PAD)_X201122867_Rev-11_Jun_13.pdf | ||
| FA850513R31129______0001_11_Jun_13.pdf | ||
| Q A_5_PAD.docx | DOCX document | |
| Q A_4_PAD.docx | DOCX document | |
| Q A_3_PAD.docx | DOCX document | |
| Attach_5_97X0011.pdf | ||
| Attach_3_Boeing_G667-E.pdf | ||
| Attach_1_MDC_A4246_Rev_C_-_F15_Dynamic_Load_Requirements.pdf | ||
| Q A_2.docx | DOCX document | |
| Attach_2_Boeing_H417-D.pdf | ||
| PAD_Q A__1_23_May_13.docx | DOCX document | |
| PADSOW7May13.docx | DOCX document | |
| PADPkg.pdf | ||
| PADSPECX201122867.docx | DOCX document | |
| CDRLSPAD.pdf | ||
| FA850513R31129.pdf |
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Cover/Signature Page
| Table of Contents |
| 1.0 Introduction |
| 2.0 Applicable Documents |
| 3.0 Definition |
| 4.0 CAST Prerequisites |
| 5.0 Test Description |
| 6.0 Test Procedures |
| 7.0 CAST Criteria |
| Appendix A - Sample Omni-Axial Vibration PSD Plots |
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