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Samantha Power
PERSONTHE STATIC LOADING OF THE INSTALLED EQUIPMENT MEETS THE REQUIREMENTS OF AC
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n AIRFRAME (As described In Item 1 above) X POWER PLANT PROPELLER • APPLIANCE Type Manufacture
CHECKED FOR ACCURACY AND COMPENSATED AS NECESSARY PER AC 43.13-IB, CHAPTER 12, SECTION 3, PARAGRAPH 12- 37 AND AC 43.13-2A, CHAPTER 2 PARAGRAPH 234 THE STATIC LOADING OF THE INSTALLED EQUIPMENT MEETS THE REQUIREMENTS OF AC 43.I3-2A. CHAPTER 1. PARAGRAPH 3 AND WAS FOUND TO MEET THE REQUIREMENTS OF PARAGRAPH 2. MATERIALS AND PRACTICES COMPLY WITH PARAGRAPHS 4 THROUGH 12
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AUDIO PANEL TO RS232 DATA TERMINAL TO AIRCRAFT POWER (2.8 Vdc) AIRCRAFT FUSELAGE Figure 2.1-1 Bloc
CHECKED FOR ACCURACY AND COMPENSATED AS NECESSARY PER AC 43.13-1B, CHAPTER 12, SECTION 3, PARAGRAPH 12- 37 AND AC 43.13-2A, CHAPTER 2 PARAGRAPH 23f. THE STATIC LOADING OF THE INSTALLED EQUIPMENT MEETS THE REQUIREMENTS OF AC 43.13-2A, CHAPTER 1, PARAGRAPH 3 AND WAS FOUND TO MEET THE REQUIREMENTS OF PARAGRAPH 2. MATERIALS AND PRACTICES COMPLY WITH PARAGRAPHS 4 THROUGH 12
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EL UC-28-14, 28 VDC TO 14 VDC CONVERTER AND THREE POWER OUTLETS IN THE COCKPIT IN ACCORDANCE WITH KGS EL
CHECKED FOR ACCURACY AND COMPENSATED AS NECESSARY PER AC 43.13-1B, CHAPTER 12, SECTION 3, PARAGRAPH 12- 37 AND AC 43.13-2A, CHAPTER 2 PARAGRAPH 23f. THE STATIC LOADING OF THE INSTALLED EQUIPMENT MEETS THE REQUIREMENTS OF AC 43.13-2A, CHAPTER 1, PARAGRAPH 3 AND WAS FOUND TO MEET THE REQUIREMENTS OF PARAGRAPH 2. MATERIALS AND PRACTICES COMPLY WITH PARAGRAPHS 4 THROUGH•12
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8) Modified the existing Cabin 14VDC Accessory Power Distribution System as per International Jet Inte
REPANCIES. AN EMI TEST, REPORT NO.: G2B-20895-080 WAS CONDUCTED AND THE INSTALLED EQUIPMENT DOES NOT INTERFERE WITH ANY OTHER INSTALLED EQUIPMENT. THE STATIC LOADING OF THE INSTALLED EQUIPMENT MEETS THE REQUIREMENTS OF AC 43.13-2A, CHAPTER 1, PARAGRAPH 3 AND WAS FOUND TO MEET THE REQUIREMENTS OF PARAGRAPH 2. MATERIALS AND PRACTICES COMPLY WITH PARAGRAPHS 4 THROUGH 12
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Jeffrey Epstein
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George W. Bush
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United States
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Ghislaine Maxwell
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