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2007 LEONARDO AW139
Starts from the median asking price of 478 comparable Helicopter listings ($461,499), then adjusts for:
- Year -1 vs comparable listings -1.5%
- Airframe time +1,628 hr vs comps -3.3%
- Engine time +2,578 hr vs comps -7.7%
- Autopilot (uncommon in comps) +2.0%
Shown as a range. An estimate from asking-price comparables and FAA supply data — not an appraisal.
Overview
| Make / Model | LEONARDO AW139 |
|---|---|
| Type | Helicopter |
| Airframe time | 3,228 hrs |
| Engine time | 3,228 SNEW |
Description
YOM 31/1/2007 Total time 3,228 hours/15,018 cycles Configuration VIP Flight rule IFR Crew/passengers 2 crew/8 passenger Avionics phase 4 Highlights •LH and RH electrically operated passengers steps •Super silent soundproofing •Vibration absorber (3rd mass) •Emergency floats provision •Air conditioning system •Ripple damper •Moquette finishing on cabin floor •TCAS I, EGPWS, HF Antenna •Autopilot 4-axis software FDR enhanced
Modifications
•LH and RH electrically operated passengers steps with light •Standard passenger cabin ceiling liners •Composite liners leather/leatherette covered •Dome lights •Moquette finishing on cabin floor •Cabin handles •Cabin loudspeakers •Passenger cabin thermo acustic double layer windows •Ripple damper •Vibration absorber (3rd mass) •Nose landing gear door •Super silent soundproofing •ICS in cabin for all passengers •Air conditioning system •Coat hangers x3 •Emergency floats provision •Crew crashworthy seats with inertial reels and safety belts •Cockpit dome/storm light •Cockpit utility lights x2 •28 V DC cockpit/cabin power outlet •Cockpit panel sun-glare shields •Overhead cockpit windows sun shades •Floor provisions for 15 seat configuration •Fluorescent lighted emergency exit signs •Cockpit map and data case in central console •Two flash lights for pilot and co-pilot •Map and data cases in pilot and co-pilot doors •ICS panel with plug for one headset •Air ventilation system •First aid kit
Avionics
•Autopilot 4-axis software FDR enhanced •EGPWS Honeywell Mark 22 •Weather radar Primus 660 •TCAS I Honeywell KTA-970 model •Kit auxiliary battery 27 AH •HF Antenna •PFD and MFD x2 •ESIS (attitude, airspeed, altitude, vertical speed, compass and ILS data) •AHRS x2 •Air data module x2 •Flux valve x2 •Display controller x2 •Cursor control device x2 •Reversion control panel •Display dimming control panel •stability augmentation system control panel •Remote instrument controller x2 •Vehicle monitoring system x2 •Monitoring warning system x2 •Aural warning generator •Central maintenance computer •Provision for CVR/FDR data interface •Flight director system x2 •Pilot and co-pilot interphone control (cyclic grip and floor switches) •VHF/HF Comm x2 •Mode S diversity transponder •VOR/LOC/GS/MB x2 •ADF •DME •MCDU x2 •Radar altimeter RT – 300 x2 •ELT – 121.5/243/406 MHz •Flight guidance controller •Honeywell GPS module with FPMS •Pilot and co-pilot digital audio panels remote ICS audio port for ground operation •Digital clock x2 •One magnetic compass •Master Warning Lights x2 •Master Caution Lights x2 •Engine 1 & 2 Fire Light x2 •Baggage compartment smoke detector light •Dual electrical power connection for CVR/FDR •CVR/FDR with ULB
How this aircraft compares
Where this LEONARDO AW139 lands versus other LEONARDO AW139 listings on fyiAero.
Airframe time
58th pct3,228 hours total (TTAF) · 58th percentile of 12 listings
Engine time (Engine 1)
99th pct3,228 hours since new · 99th percentile of 5 listings
Engine time (Engine 2)
99th pct2,924 hours since new · 99th percentile of 5 listings
Percentile = share of comparable listings at or below this value. Lower airframe/engine hours are generally fresher; price reflects the asking price only.
General
| Year | 2007 |
|---|---|
| Manufacturer | LEONARDO |
| Model | AW139 |
| Condition | Used |
| FlightRules | IFR |
Airframe
| Total Time | 3,228 |
|---|---|
| Max Takeoff Weight | 6,800 lb |
| Basic Empty Weight | 4,643 lb |
Engine 1
| Engine 1 Make/Model | PRATT & WHITNEY PT6C-67C |
|---|---|
| Engine 1 Time | 3,228 SNEW |
| Engine 1 TBO | 5000 |
Engine 2
| Engine 2 Make/Model | PRATT & WHITNEY PT6C-67C |
|---|---|
| Engine 2 Time | 2,924 SNEW |
| Engine 2 TBO | 5000 |
Avionics
| Radar Altimeter | Yes |
|---|---|
| Auto Pilot | Yes |
| ELT | Yes |
| Airborne Weather Radar | Yes |
| Traffic Avoidance System | Yes |
| Avionics/Radios | •Autopilot 4-axis software FDR enhanced •EGPWS Honeywell Mark 22 •Weather radar Primus 660 •TCAS I Honeywell KTA-970 model •Kit auxiliary battery 27 AH •HF Antenna •PFD and MFD x2 •ESIS (attitude, airspeed, altitude, vertical speed, compass and ILS data) •AHRS x2 •Air data module x2 •Flux valve x2 •Display controller x2 •Cursor control device x2 •Reversion control panel •Display dimming control panel •stability augmentation system control panel •Remote instrument controller x2 •Vehicle monitoring system x2 •Monitoring warning system x2 •Aural warning generator •Central maintenance computer •Provision for CVR/FDR data interface •Flight director system x2 •Pilot and co-pilot interphone control (cyclic grip and floor switches) •VHF/HF Comm x2 •Mode S diversity transponder •VOR/LOC/GS/MB x2 •ADF •DME •MCDU x2 •Radar altimeter RT – 300 x2 •ELT – 121.5/243/406 MHz •Flight guidance controller •Honeywell GPS module with FPMS •Pilot and co-pilot digital audio panels remote ICS audio port for ground operation •Digital clock x2 •One magnetic compass •Master Warning Lights x2 •Master Caution Lights x2 •Engine 1 & 2 Fire Light x2 •Baggage compartment smoke detector light •Dual electrical power connection for CVR/FDR •CVR/FDR with ULB |
Additional Equipment
| Dual Controls | Yes |
|---|---|
| A/C | Yes |
| Baggage Compartment | Yes |
| Additional Equipment | •LH and RH electrically operated passengers steps with light •Standard passenger cabin ceiling liners •Composite liners leather/leatherette covered •Dome lights •Moquette finishing on cabin floor •Cabin handles •Cabin loudspeakers •Passenger cabin thermo acustic double layer windows •Ripple damper •Vibration absorber (3rd mass) •Nose landing gear door •Super silent soundproofing •ICS in cabin for all passengers •Air conditioning system •Coat hangers x3 •Emergency floats provision •Crew crashworthy seats with inertial reels and safety belts •Cockpit dome/storm light •Cockpit utility lights x2 •28 V DC cockpit/cabin power outlet •Cockpit panel sun-glare shields •Overhead cockpit windows sun shades •Floor provisions for 15 seat configuration •Fluorescent lighted emergency exit signs •Cockpit map and data case in central console •Two flash lights for pilot and co-pilot •Map and data cases in pilot and co-pilot doors •ICS panel with plug for one headset •Air ventilation system •First aid kit |
Interior
| Configuration | Corporate |
|---|---|
| Number of Seats | 8 |
| Soundproofing | Yes |
Exterior
| Door Type | Sliding |
|---|
Rotor
| Main Rotor Blade Time Remaining | 16772 |
|---|---|
| Main Rotor Gearbox Time Remaining | 1910 |
| Tail Rotor Gearbox Time Remaining | 4272 |
