Flight-Testing of the FAA Onboard Inert Gas Generation System on ...

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APPENDIX B—FOUR-BOLT FLANGE ENGINEERING SPECIFICATION B-1/B-2
APPENDIX C—THE <str<strong>on</strong>g>FAA</str<strong>on</strong>g> OBIGGS WIRING DIAGRAM C-1/C-2
Page 1 and 2: DOT/FAA/AR-03/58 O
Page 3 and 4: 1. Report No. DOT/FAA</stro
Page 5 and 6: TABLE OF CONTENTS EXECUTIVE SUMMARY
Page 7 and 8: 10 Correlation of
Page 9 and 10: EXECUTIVE SUMMARY Significant empha
Page 11 and 12: Other previous stu
Page 13 and 14: 2.1.2.1 Center Wing Tank. The CWT <
Page 15 and 16: 2.2 TEST PROCEDURES. All tests were
Page 17 and 18: After passing through the</
Page 19 and 20: amount of flow (10
Page 21 and 22: 5. DISCUSSION OF RESULTS. The resul
Page 23 and 24: of the</st
Page 25 and 26: Figure 12 gives the</strong
Page 27 and 28: 5.2 FUEL TANK INERTING. The fuel ta
Page 29 and 30: the ullage would b
Page 31 and 32: Oxygen Concentration (% vol) 25 20
Page 33 and 34: 6. “A Review of
Page 35: Interface Description: Interface 1:
Page 39: APPENDIX D—CALCULATION OF BLEED A

Flight-Testing of the FAA Onboard Inert Gas Generation System on ...

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