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ics Suite Air Data Computer: Dual Air Data Computers Attitude Heading Reference System: Dual Litef LCR-92s AHRS Automatic Direction Finder: Single Collins ADF-462 ADF Receiver Cockpit Voice Recorder: Universal CVR--I20 Communications: Dual Collins VHF-22a VHF Radios Distance Measuring Equipment: Dual
Page: EFTA00022720 →uipment: Dual Collins Dme-42 DME Transceiyeri Electronic Flight Instrumentation System: Honeywell Ed-800 EFIS System Emergency Locator Transmitter. Artex C406-N ELT With Nav Interface Flight Control System / Autopilot: Dual Honeywell FZ-706 Flight Control Computers Flight Management System: Universal
Page: EFTA00022720 →Autopilot: Triple Collins 701 Communication Radios: Dual Collins VHF-7008w18.33 spacing CVR: Fairchld A100 DME: Dual Collins DME-700 EFTS: Collins EFIP-701E FDR: Sundstrand Flight Director: Tnplc Collins EFIP-701E Flight Phone: MagnaStar w/Aerocom interface FMS: Dual Honeywell PEG-009 G
RT-701X ADDITIONAL EQUIPMENT Cockpit: Dual Honeywell 906 air data systems. forward looking windshear, ADS-8 Out. FANS-1/A. triple Collins ILS 700, Artex C406 N ELT. CPDCL. Modification: Wnglets General: Crew Accessories: PATS auxiliary fuel system. Stage 3 compliant. Aerocon airstairs. belly qua
ing Unit (RTU), receiving navigation inputs from Triple Honeywell Inertial Reference Sensors (IRS), dual internal GPS sensors, and VORIDME from the Collins No. 1 and No. 2 VORIDME systems in accordance with manufacture's InstalatIon and Checkout Manual No. 34-60-09, Rev. 2, dated August 15, 1997 or lat
is 337 is for the work performed on N908JE undo Banyan Air Service, Avionics • Division work order #68062. A. Installed an Artex ELT406-2Hivl per Artex installation document number 570.5000, Rev. A, dated 12/10/02 mounted in unpressurized aft compartment. The antenna is mounted in the aft tail sect
Entities connected to both Collins and Artex