Avionics:
VHF-AM ROCKWELL COLLINS VHF-422C (2X).
INTER COMMUNICATION SYSTEM TEAM TB 31 WITH 3 CONTROL BOXES 1976 (1 IN CABIN.)
PA WITH 4 LOUDSPEAKERS BAKER M1050.
HEADSETS SILEC 4449-1 (2X).
THALES AHV-16 RADIO ALTIMETER.
ATC TRANSPONDER MST67A (MODE-S).
HF/SSB BENDIX KING KHF950.
VHF/FM MARITIME NAT NPX-138.
SSCVFDR HONEYWELL AR COMBI.
TCAS GOODRICH HP899.
TCAS RYAN TAS600.
ADF HONEYWELL KDF-806.
DME HONEYWELL KDM 706A.
VOR/ILS HONEYWELL KNR-634A (2X).
AIR DATA COMPUTER SHADIN ADC-2000.
FLIGHT MANAGEMENT SYSTEM UNIVERSAL UNS-1K (INCLUDING GPS).
SFIM CDV 85 D3 FLIGHT DIRECTOR COUPLER.
TELEPHONICS RDR1400 WEATHER/SEARCH RADAR.
UMS.
HUMS FULL (M’ARMS).
JEPPENSEN MAP HONEYWELL KMD850.
JEPPENSEN MAP SKYFORCE SKYMAP IIIC.
Interior:
1 CABIN FLOOR CAPABLE OF THE VARIOUS OPTIONAL TYPES OF ARRANGEMENTS.
2 REMOVABLE PILOT AND CO-PILOT HIGH BACK-REST SEATS, ADJUSTABLE IN REACH AND HEIGHT EACH FITTED WITH A SAFETY BELT AND SHOULDER 4-POINT HARNESS.
11 STANDARD SEAT LAY-OUT.
4 POINTS HARNESSES FOR 11 STANDARD SEAT LAYOUTS.
2 PILOT AND CO-PILOT JETTISON ABLE DOORS, EACH FITTED WITH A BAD WEATHER WINDOW AND AN INTERNAL STORAGE UNIT. DOORS WITH AIR INLETS.
2 HINGED JETTISON ABLE CABIN FRONT DOORS.
2 ENLARGED AND BUBBLED REAR SLIDING DOORS WITH JETTISON ABLE WINDOW FROM INSIDE AND OUTSIDE.
2 RETRACTABLE FOOTSTEPS.
CABIN UPHOLSTERY WITH SOUND PROVING.
1 INSTRUMENT PANEL, ONE CONSOLE AND ONE CEILING PANEL.
DUAL FLIGHT CONTROL.
ENGINE CONTROLS.
ROTOR BRAKE CONTROL.
1 HEATING/DEMISTING/VENTILATION SYSTEM.
2 UPPER TINTED PANES.
2 FRONT PLEXIGLASS PANES.
2 WINDSHIELD WIPERS.
2 ILLUMINATED CHART HOLDERS.
2 HEADSET HOLDERS (SILEX).
1 PORTABLE FIRE-EXTINGUISHER.
1 FLIGHT MANUAL.
FIRST-AID KIT JAR-OPS COMPLIANT
Other comments:
EMERGENCY FLOATATION WITH AFDS.
INTERNAL AERAZUR (SR-8) LIFE RAFT INSTALLATION.
HELICOPTER EMERGENCY EGRESS LIGHTING (HEEL).
HR-SMITH CPI-503 ADELT.
DUKANE DK120 ULB.
AVAD RACAL V694 100FT, CH, UC WARNING.
ELT KANNAD 406AF
