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ine Control (FADEC) and associated systems. ST10959SC: Installation of Rockwell Collins Pro Line 21 Electronic Flight Instrument System (EFIS) with Rockwell Collins FMS-6100, Localizer Performance with Vertical Guidance (LPV) approach capability and Universal Avionics System Company (UASC) Terrain Awareness Wa
rsion Panel 0.2 88.0 Rev. Panel 373-91.3203.3 Co-pilot Reversion Panel 0.2 88.0 9-PED 373-91-3203-9 9-Pedestal Panel 1.8 92.89 345-6196 ELT Switch 0.2 88.0 Annunciator Led-42-12-BB-E0Y47 AUX BATT (1/2) Annunciator 0.05 88.0 Annunciator (2) Led-40-18-BB-EOY4S Pull Up/ Terrain Annunciato
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rsion Panel 0.2 88.0 Rev. Panel 373.91.3203-3 Co-pilot Reversion Panel 0.2 88.0 9-PED 373-91-3203-9 9-Pedestal Panel 1.8 92.89 345-6196 ELT Switch 0.2 88.0 Annunciator Led-42-12-BB-E0Y47 AUX BATT (1/2) Annunciator 0.05 88.0 Annunciator (2) Led-40-18-86-E0Y45 Pull Up/ Terrain Annunciato
ine Control (FADEC) and associated systems. ST10959SC: Installation of Rockwell Collins Pro Line 21 Electronic Flight Instrument System (EFIS) with Rockwell Collins FMS-6100, Localizer Performance with Vertical Guidance (LPV) approach capability and Universal Avionics System Company (UASC) Terrain Awareness Wa
rsion Panel 0.2 88.0 Rev. Panel 373-91-3203-3 Co-pilot Reversion Panel 0.2 88.0 9-PED 373-91-3203.9 9-Pedestal Panel 1.8 92.89 345-6196 ELT Switch 0.2 88.0 Annunciator Led-42-12-8B-E0Y47 AUX BATT (1/2) Annunciator 0.05 88.0 Annunciator (2) Led-40-18-88-E0Y4S Pull Up/ Terrain Annunciato
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rsion Panel 0.2 88.0 Rev. Panel 373-91-3203-3 Co-pilot Reversion Panel 0.2 88.0 9-PED 373-91-3203-9 9-Pedestal Panel 1.8 92.89 345.6196 ELT Switch 0.2 88.0 Annunciator led-42-12-BB-E0Y47 AUX BATT (1/2) Annunciator 0.05 88.0 Annunciator (2) Led-40-18-BB-E0Y45 Pull Up/ Terrain Annunciato
Entities connected to both Rockwell Collins and ELT Switch

Samantha Power
PERSON
Ghislaine Maxwell
PERSONRegistration Mark
PERSONPratt & Whitney
ORGANIZATIONRichmond Heights
LOCATIONFADEC
ORGANIZATIONthe Federal Aviation Administration
ORGANIZATIONthe Aircraft Maintenance Records
ORGANIZATIONFull Authority Digital Engine Control
ORGANIZATIONPropulsion Branch
ORGANIZATIONAssociated Systems
ORGANIZATIONElectrical Wiring Interconnection Systems
ORGANIZATIONSpecial Conditions No
ORGANIZATIONGPS Receiver
ORGANIZATIONS. Description of Work
PERSON
Cleveland
LOCATIONAir Data Computer
ORGANIZATIONIAW Ground Test
ORGANIZATION
Richmond
LOCATIONFAA Regional Office
ORGANIZATION