2014 Agusta AW139

(2) Pratt & Whitney Canada PT6C-67C (Hard Time)
ENGINE 1: ENGINE 2:
S/N: PCE-KB1485 S/N: PCE-KB1490
ENG Time: 3,172ENG Time: 3,172
ENG Cycles: 5,504 ENG Cycles: 5,504
Engines Enrolled on Pratt & Whitney ESP Gold Program

Inspection: Last Complied: Next Due:
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

•Airworthiness Date: March 28, 2014
•Maintenance Tracking by CAMP
•All recent major maintenance performed by Sterling Helicopters

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

CAPABILITIES:
WAAS
TCAS 7.1
EGPWS
QAR
CVR
FLIR
HUMS
EMERGENCY FLOATS
FAST SYSTEM
SBAS
GPS
ADS-B OUT
AUX FUEL TANK
AVC (3+1)

2014 Paint – SureFlight, Coatesville, PA
Arista Blue Base with Gray and Matterhorn White Accent Striping

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 Configuration 3
•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
•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 Cameras