AIRFRAME

In Service Date / Warranty Start Date – 24th June 2006
CAMP Maintenance Tracking – Available Upon Request

ENGINES

Description Pratt & Whitney 305A

ENGINE #1 ENGINE #2
Total Time 1938 1938
Cycles 1041 1041

AVIONICS & CONNECTIVITY

Collins Proline 4 – Four Liquid Crystal Flight Displays (EFIS)
Dual Collins VHF COMM (VHF-422C with 8.33 Spacing)
Collins Dual VOR/ILS Navigation Receivers (VIR-432 with FM Immunity)
Collins Dual Mode S Transponders (TDR-94D)
Dual Universal FMS with GPS, PRNAV Compliant (UNS-1E)
Dual Rockwell Automatic Direction Finder (ADF-462)
Dual Distance Measuring Equipment (DME-442)
Universal Cockpit Voice Recorder (CVR-120)
Dual Collins Air Data System (ADC-850D)
Integrated Flight Instrument System (IFIS)Autopilot
Collins Weather Radar System (RTA-854)
Dual Honeywell HF Comms (KTR953)
Collins Radio Altimeter (ALT-4000)
Collins TCAS II with Change 7.1 (TTR-4000)
Honeywell MK-V EGWPS
Artex ELT (C-406-2) with NAV interface
SELCAL (JETCALL-5)
L3 Comm Lighting Sensor (WX-1000)
L3 Comm Flight Data Recorder (FA2100FDR)

WEIGHT
Gross Weight — 23,500 lbs
Empty Weight — 16,500 lbs
Max Landing Weight — 19,500 lbs
Max Take-off Weight — 22,750 lbs
Fuel Capacity — 7,912 lbs