ACTT:
| Total Airframe Hours: |
28 |
| Total Landings: |
22 |
| Year of Manufacture: |
2008 |
|
Engines |
Hours |
Cycles |
Serial # |
Misc. |
| GE CF34-3B1 |
43 |
54 |
|
|
| GE CF34-3B1 |
43 |
54 |
|
|
Engine Notes:
APU:
Honeywell GTCP 36-150
Avionics:
Collins ADC-850A ADC
Collins VHF-422C VHF COM
Collins GPS-4000A GPS
Collins DME-422 DME
Collins VIR-432 VHF NAV
Honeywell Mark V EGPW Computer
Collins DCU-4000 DCU
L3 Communication SPS
Collins TTR-921 TCAS
Collins ADF-462 ADF Receiver
Collins ICC-4004 IAP
AVTECH Audio Control Panel
AVTECH CSD-714 SELCAL
Collins ALT-1000 Radio Altimeter
L3 Communication FA2100 CVR
L3 Communication FA2100 Flight Data Computer
Collins RTA-844 WX Radar Antenna
Collins FMC-4200 FMC
Collins TDR-94D ATC Transponder
Collins RTU-4000 Radio Tuning Unit
Collins MDC-4000 Maint. Diagnostic Computer
Collins DBU-4000 FMS-CDUArtex C406-2 ELT
Collins FCC-4000 Computer Flight Control
MFD Electronic Flight Display
EICAS Electronic Flight Display
Thales ISIS
Thales QAR
Additional Features:
Ice ShieldGround Air Service Connection (Less APU) Enhanced Range Option Full Manufacturer’s Warranty Engines and airframe can be enrolled on Smart Parts Program Aircraft fully certified to EASA commercial standards (EU-OPS)
Maintenance:
On CAMP
Interior:
Fourteen-passenger interior plus 2 crew (one jump seat) configured with a four-place club arrangement in the forward and middle cabin, each club arrangement includes a pull-out table. The aft cabin is comprised of a four-place dining/conference group opposite a two-place club arrangement with table. Other: Jeppesen under floor storageForward and aft lavatoryCrew wardrobe compartment
Exterior:
Overall dark red and beige with white accent stripes.
Weights:
Maximum Take-Off Mass = 52,900 lbs or 23,995 kg.
Maximum Landing Mass = 46,750 lbs or 21,205 kg.
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