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Rotortrade - ÎÒÃǵ±Ç°µÄ¹©Ó¦
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¸Å¿ö | ÀàÐÍ: | Ö±Éý»ú (ÎÐÂÖ»ú) | Æ·ÅÆ: | Agusta | ÐͺŠ1: | AW139 | ÖÆÔìÄê: | 2007 | ÊôÐÔ: | ±»IFR¼ø¶¨µÄ ±»IFR×°±¸µÄ ÉÌÓÃ×¢²áµÄ | µØµã: | ÃÀ¹ú | ʱ¼ä×ܼÆ: | 6833 h | ¼Û¸ñ: | ѯ¼Û | ϸ½Ú |
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Rotortrade 7943 Woodley Ave, Van Nuys Los Angeles, CA 91406 ÃÀ¹ú
µç»°: 1 818-686-2463 |
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¸Å¿ö | ÀàÐÍ: | Ö±Éý»ú (ÎÐÂÖ»ú) | Æ·ÅÆ: | Agusta | ÐͺŠ1: | AW139 | ÖÆÔìÄê: | 2007 | ÊôÐÔ: | ±»IFR¼ø¶¨µÄ ±»IFR×°±¸µÄ ÉÌÓÃ×¢²áµÄ | µØµã: | ÃÀ¹ú | ʱ¼ä×ܼÆ: | 6833 h | ¼Û¸ñ: | ѯ¼Û | ³Ë¿ÍÊýÁ¿: | 12 | µÇ½: | 13745 |
·¢¶¯»ú£¨¶à¸ö£© | ·¢¶¯»úÊýÁ¿: | 2 | Æ·ÅÆ/ÐͺÅ: | PT6C-67C | PT6C-67C | ×Üʱ¼ä: | 4398 h | 3180 h | Time Between Overhaul ???
´óÐÞ¼ä¸ôʱ¼ä (hours): | 5000 h | 5000 h |
º½¿Õµç×Óѧ | •GE Smith HUMS
•Honeywell TCAS KTA 970 TCAS I system
•Honeywell EGPWS Mark XXII system
•QAR flight data monitoring
•Skyconnect satellite phone/tracking system
•HR Smith series 503 ADELT
•Weather radar Honeywell Primus 660
•ICS
•TFM550G FM radio
•DMP100 MP3 cabin briefing system
•Radar altimeter RT-300 x2
•4-axis dual DAFCS
•Flight director system x2
•GPS module GNSS/SBAS with FPMS x2
•Mode S Diversity Transponder with ES ADS- B Out 1,090 MHz
•CVR/FDR with ULB
•PFD x2
•MFD x2
•ESIS
•AHRS x2
•Air data modules x2
•Flux valves x2
•Display controllers x2
•Cursor control devices x2
•Reversion control panel
•Display dimming control panel
•Stability augmentation system control panel
•Remote instrument controllers x2
•Vehicle monitoring system x2
•Monitor warning system x2
•Aural warning generator
•Central maintenance computer
•Provision for CVR/FDR data interface
•Pilot and co-pilot interphone control
•VHF COMM x2
•VOR/LOC/GS/MB x2
•ADF
•DME
•MCDU x2
•ELT
•Flight guidance controller
•Pilot and co-pilot digital audio panels with remote ICS audio port for ground operation
•Clock x2
•Magnetic compass
•Outside air temperature indicator
•Master warning lights x2
•Master caution lights x2
•Engine fire light x2
•Baggage compartment smoke detector light
•Dual electrical power connection for CVR/FDR |
×°±¸ | •Nose landing gear doors
•28 VDC auxiliary heavy duty battery
•Cabin footsteps
•300 kg baggage Increase
•Baggage compartment anchor system
•Emergency floats provisions
•Transversal auxiliary fuel tank 132 US gal
•BT-200 tail reinforcement
•Rigid liner cabin
•Dome lights
•Crashworthy seats x12
•HEELS
•Air conditioning system
•Forced fan ventilation
•Bleed air heater and defroster with air noise suppressions
•Cockpit air ventilation system
•Rotor brake
•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
•Fluorescent emergency exit signs
•Cockpit map and data case in central console
•Flash lights for pilot and co-pilot
•Map and data cases in pilot and co-pilot doors
•ICS panel with plug for one headset LH side
•First aid kit
•44 Ah main battery
•13 Ah auxiliary battery
•Navigation lights x3
•Anticollision light
•External emergency landing lights on the sponsons x2
•Landing/taxing lights x2
•Baggage compartment lights x3
•Smoke sensor |
ÆäËû | YOM June 2007
Configuration Offshore
Flight rules DP IFR
Registration FAA
Crew/passengers 2 crew/12 passengers
Empty weight 4,433 kgs
MTOW 6,800 kgs
Avionics phase 4.8
Highlights
•Leonardo airframe warranty 3 months/250 hours
•Floats provisions
•Auxiliary fuel tank
•Air conditioning
•HUMS, ADELT, EGPWS
•4-axis dual DAFCS
•CVR/FDR with ULB, HEELS |
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