manufacturer
Leonardo
configuration
Corporate
condition
Used
year
2014
time
2965
helicopter location
United States
serial number
41364
registration number
N978V
listing ID
HT18270
Description
AW139, YOM 2014, TT 2965hours,
Seven (7) Passenger Interior with 8 or 9 Pax option, Airframe Enrolled on JSSI, Engines Enrolled on ESP Gold, Avionics Enrolled on MSP, Honeywell Primus 2.0 Phase 7, 6800 KG MTOW SB, Cabin Steps & DART MX Step System
avionics
AVIONICS: Honeywell Primus 2.0 Phase 7 Version 7.12 (Enrolled on Honeywell MSP)
AIR DATA MODULES: Dual Honeywell AZ-200 ADM
ATTITUDE HEADING REFERENCE SYSTEM: Dual LiteF LCR-100
AUTOMATIC DIRECTION FINDER: Single Honeywell DF-855 ADF AUTOPILOT
CONTROLLER: Single Honeywell PC-770
COMMUNICATIONS: Honeywell AV-900 Audio Panel
DISPLAY UNITS: Four Honeywell DU-1080-3
DISTANCE MEASURING EQUIPMENT: Dual Honeywell DM-855 DME
ENHANCED GROUND PROXIMITY WARNING SYSTEM: Honeywell MK XXII EGPWS
EMERGENCY LOCATOR TRANSMITTER: Single ARC/Artex C406-2HM ELT
FLIGHT GUIDANCE CONTROLLER: Single Honeywell GC-810 FGC
GLOBAL POSITIONING SYSTEM: Dual Honeywell GPM-XXX
MULTI-FUNCTION CONTROL DISPLAY UNIT: Dual Upgraded MCDU-R Units
MULTI-PURPOSE FLIGHT RECORDER: Single Penny & Giles FDR/CVR (w/ ULB)
RADIO ALTIMETER: Dual Honeywell RT-300 ALT
STANDBY INSTRUMENT: Meggitt Avionics TRANSPONDERS:
Dual Honeywell XS-858B
TRAFFIC COLLISION ALERT AVOIDANCE SYSTEM: BendixKing KTA-910 TCAS I
VERY-HIGH FREQUENCY COMMUNICATION: Cobham NPX138N VHF COMM
VOICE DATA RADIO MODULE: Dual Honeywell TR-865A VDR
VOR / ILS / DATA LINK: Dual Honeywell NV-875A VDL
WEATHER RADAR: Single Honeywell WU-660
equipment
• Environmental Control System (ECS)
• Inlet Barrier Filter (IBF) system
• Two (2) Cockpit Ipad Mounts
• LH and RH ACI Cabin Door Steps
• Dart Aerospace Maintenance Step Kit
• Flightcell DZMx with Satellite
• Pratt & Whitney Flight-Data Acquisition Storage Transmission
(FAST) system Additional Features:
• Curtis Wright Quick Access Recorder (QAR)
• Honeywell LP-860 Lightning Detection Processor
4
AVIONICS
• Health and Usage Monitoring System (HUMS)
• Active Vibration Control System (3+1)
• Aerazur Emergency Floats System
• Auxiliary Fuel Tank
• Pulsation Dampener Kit
• Sagem 5th Display
• Fwd Looking, Aft Looking, and Belly Mounted Camera
interior
VIP Executive s even (7) passenger interior with additional seats for 8 or 9 pax with optional conference table.
Features f our (4) aft facing seats and three (3) forward facing seats.
The cabin features include:
• Custom Executive VIP Cabin Interior
• Cockpit / Cabin Separation Bulkhead with sliding privacy windows
• 3 - Forward Facing VIP seats with arm rests – drawers beneath for additional storage
• 4 - Aft Facing VIP seats with two exterior armrests -– drawers beneath for additional storage
• Optional seats that can swapped in for 8 or 9 passenger configuration
• Optional Cabin conference table
• Cabin Interior Sound Reduction Wall Panels System
• Drawers beneath seats to store life vests and smoke hoods
• 4 – 110 volt power outlets
inspection details
MAINTENANCE & INSPECTIONS
• Airworthiness Date: March 28, 2014
• Maintenance Tracking by CAMP
• All recent major maintenance
performed by Sterling Helicopters
Inspection: Last Complied: Next Due:
6 Month c/w Jan 2024 July 2024
12 Month c/w Jan 2024 Jan 2025
4 Year c/w Jan 2022 Jan 2026
100 Hour c/w Jan 2024 3,025 Hours
300 Hour c/w Jan 2024 3,225 Hours
600 Hour c/w Jan 2024 2,958 Hours
Eng 1&2 PI c/w Jan 2024 Jan 2025
remarks
Service Bulletins:
• SB-BR-139-140 Rev C – MTOW increase to 6,800 KG
• SB-BR-139-191 – Search Light installation
• SB-BR-139-424 – Replaced NIMS and Epic Software to 7.10
• SB-BR-139-427 – Power Control Module
• SB-BR-139-417 – Replaced Elastomeric T/R Dampers
• SB-BR-139-414 – Replaced Avionics Brackets in Nose
• SB-BR-139-137 Rev B – Part III Powered Parking Brake
• SB-BR-139-115 Rev D – Mast Vibration Kit
• SB-BR-139-500 Primus Epic Software 7.12 & 7.14 Upgrade
Modifications:
• Forward Looking Infrared (FLIR) System Camera
