Flight-Testing of the FAA Onboard Inert Gas Generation System on ...
Flight-Testing of the FAA Onboard Inert Gas Generation System on ...
Flight-Testing of the FAA Onboard Inert Gas Generation System on ...
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Interface Descripti<strong>on</strong>:<br />
Interface 1: 2” Flexible Coupling<br />
Interface 2: 2” Dia SS Pipe with 4-Bolt flange with Face Mating Seal<br />
Static Pressure (28-14)<br />
Temperature (28-15)<br />
NEA [O2] (28-73)<br />
Interface 3:<br />
<str<strong>on</strong>g>System</str<strong>on</strong>g> NEA<br />
Output<br />
Interface 2:<br />
<str<strong>on</strong>g>System</str<strong>on</strong>g> Bleed<br />
Air C<strong>on</strong>necti<strong>on</strong><br />
Interface 3: 1” Dia Al tube with Hydra-flow 14T02 Sleeve, Coupling, Seal, and Clamp Assy<br />
Interface 1:<br />
OEA Exhaust<br />
Heat Exchanger<br />
Cooling Air<br />
Exhaust<br />
(No Interface)<br />
Temperature<br />
(28-5)<br />
Note:<br />
Static Pressure (28-8)<br />
Temperature (28-9)<br />
Spare Port<br />
Static Pressure (282)<br />
Temperature (28-1)<br />
OEA [O2] (28-74)<br />
Temperature<br />
(28-4)<br />
Heat Exchanger<br />
Cooling Air Inlet<br />
(No Interface)<br />
Instrumentati<strong>on</strong> Identified with Paren<str<strong>on</strong>g>the</str<strong>on</strong>g>tic Numbers Cited in Airbus Z-Mod XB 071 B<br />
Heat Exchanger Exhaust Deposited in Rear <str<strong>on</strong>g>of</str<strong>on</strong>g> Cargo Bay via 4” Flexible Duct C<strong>on</strong>nected with<br />
Flexible Copuling<br />
Static Pressure (28-6)<br />
Temperature (28-7)<br />
Temperature (<str<strong>on</strong>g>FAA</str<strong>on</strong>g> Reader)<br />
A-3/A-4
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