Epstein Secrets

l/Installation 29 3.2 Access Location 29 4 POWER DISTRIBUTION 30 4.1 Circuit Breakers by Bus 3

ociated 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 Warning System (TAWS)

gement Computer PWR-4000 (4) 622.9945.021 IAPS Power Card GPS-4000 822-0931-003 GPS Receiver Mount

ociated 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 Warning System (TAWS)

ine Discussion Verification Step(s) Symptom I Power is not available to ASE The handset display shou

8JE BOEING 20115 3) Press the APP-65A Autopilot Control Panel [AP ENG]-button to couple the AP to the selected FD. The Autopilot will track pseudo-Localizer and pseudo-Glidesbpe signals from the FMS. b. Advanced Approach Operations 1) Advanced approaches may be identified in the data base by the prefi

al/Installation 29 3.2 Access Location 29 4 POWER DISTRIBUTION 30 4.1 Circuit Breakers by Bus 3

ociated 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 Warning System (TAWS)

gement Computer PWR-4000 (4) 622-9945-021 !APS Power Card GPS•4000 822-0931-003 GPS Receiver Mount

ociated 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 Warning System (TAWS)

AUDIO PANEL TO RS232 DATA TERMINAL TO AIRCRAFT POWER (2.8 Vdc) AIRCRAFT FUSELAGE Figure 2.1-1 Bloc

8JE BOEING 20115 3) Press the APP-65A Autopilot Control Panel [AP ENG]-button to couple the AP to the selected FD. The Autopilot will track pseudo-Localizer and pseudo-Glideslope signals from the FMS. b. Advanced Approach Operations 1) Advanced approaches may be identified in the data base by the pref