2012 Agusta AW109 SP GrandNew

Description

ENVIRONMENTAL CONTROL SYSTEM
CATEGORY “A”
IN-FLIGHT ENTERTAINMENT SYSTEM (IES)
EXTERNAL VIDEO CAMERA SYSTEM (EVS-1500)
FRESH 3200 HOUR INSPECTION


ENGINES

ENGINE TYPE PW207C X2
TIME SINCE NEW
CYCLES
COMPONENT TIMES
ITEM TBO/SLL HOURS REMAINING % REMAINING
MAIN ROTOR BLADE 1 8,800 6,006.58 68.25%
MAIN ROTOR BLADE 2 8,800 5,668.50 64.41%
MAIN ROTOR BLADE 3 8,800 6,253.16 71.05%
MAIN ROTOR BLADE 4 8,800 5,623.50 63.89%
TAIL ROTOR BLADE X2 10,000 8,485.25 84.85%
MAIN TRANSMISSION 4,800 1,343.09 27.98%
90-DEGREE GEARBOX 3,000 1,098.08 36.60%
MAIN SERVO 1 TBO 1,800 1,368.66 76.03%
MAIN SERVO 1 SLL 8,000 7,568.66 94.60%
MAIN SERVO 2 TBO 1,800 1,407.50 78.19%
MAIN SERVO 2 SLL 8,000 5,741.51 71.76%
MAIN SERVO 3 TBO 1,800 1,368.66 76.03%
MAIN SERVO 3 SLL 8,000 6,030.58 75.75%
TAIL SERVO TBO 1,800 1,368.66 76.03%
TAIL SERVO SLL 11,000 9,005.07 81.86%
STARTER GENERATOR 1 1,000 568.66 56.86%
STARTER GENERATOR 2 1,000 944.33 94.43%
ENGINE 1 3,500 874.91 24.99%
ENGINE 2 3,500 821.08 23.45%
ENGINE 2
2,678 HOURS
2955IMP/1913 N1/ 5259N2
ENGINE 1
2,565 HOURS
2033 IMP / 1693 N1 / 5349 N2

Avionics

NAVIGATION SYSTEM WITH EFIS (PILOT AND CO-PILOT)
VHF/COM/NAV/GPS
AUTOMATIC FLIGHT CONTROL SYSTEM (3 AXIS DUPLEX)
MULTIFUNCTION DISPLAY
TRANSPONDER TDR-94D MODE S
EMERGENCY LOCATOR TRANSMITTER (ELT) SYSTEM
WEATHER RADAR RDR2000
COCKPIT CENTRAL MONITOR 8.4’’
TAS, DIGITAL MAP GENERATOR

Additional Info

ELECTRICAL STEP BAR RIGHT SIDE WITH SINGLE ACTUATOR
SOUND PROOFING KIT
PASSIVE VIBRATION ABSORBER
INTERCOMMUNICATION SYSTEM (ICS), VIP VERSION
ROTOR BRAKE SYSTEM
AUXILIARY FUEL TANKS
BAGGAGE COMPARTMENT EXTENSION
EMERGENCY FLOATS PROVISION ONLY
INSTALLATION OF THE 20 CELLS BATTERY KIT
PILOT/CO-PILOT STEPS
RIPPLE DAMPER, HYDRAULIC SYSTEM
CABIN SUNBLINDS (NOT NVG COMPATIBLE)
ENGINE INLET PARTICLE SEPARATOR SYSTEM
CABIN FOLDABLE FOOTSTEP (LEFT/RIGHT SIDE)

Pacific Airhub Aircraft Sales Ltd

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