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Agusta AB139 |
cena na żądanie |
Przegląd
| Informacje podstawowe | | Typ: | Helikopter (Turbina) | | Producent: | Agusta | | Model: | AB139 | | Rok produkcji: | 2007 | | Cechy charakterystyczne: | Certyfikat IFR
Wpisany do rejestru handlowego | | Lokalizacja: | Nigeria | | Całkowity czas (TTAF): | 3228 h | | Cena: | cena na żądanie | | Wszystkie szczególy |
| Sprzedawca |
Rotortrade
7943 Woodley Ave, Van Nuys
Los Angeles, CA 91406
Stany Zjednoczone
Tel.: 1 818-686-2463 |
| Kontakt do Sprzedawcy |
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Szczególy
| Informacje podstawowe | | Typ: | Helikopter (Turbina) | | Producent: | Agusta | | Model: | AB139 | | Rok produkcji: | 2007 | | Cechy charakterystyczne: | Certyfikat IFR
Wpisany do rejestru handlowego | | Lokalizacja: | Nigeria | | Całkowity czas (TTAF): | 3228 h | | Cena: | cena na żądanie | | Liczba pasażerów: | 8 | | Lądowania: | 15018 |
| Silnik(i) | | Liczba silników: | 2 | | Producent/Model: | PT6C-67C | PT6C-67C | | Czas całkowity: | 3228 h | 2924 h | | TBO (hours): | 5000 h | 5000 h |
| Opis/Charakterystyka silnika | Engine 1 cycles 5,003 IMP/3,489 CT/4,095 PT
Engine 2 cycles 4,602 IMP/2,999 CT/4,090 PT |
| Awionika | •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 |
| Wyposażenie | •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 |
| Inne uwagi | YOM 31/1/2007
Configuration VIP
Flight rule IFR
Empty weight 4,643 kgs
MTOW 6,800 kgs
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 |
Zdjęcia
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