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Beechcraft King Air A100 Aircraft

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ATTENTION: This item is no longer available.
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Quantity: 1 Aircraft
Manufacturer: Beechcraft
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Model: KingAir A100
Product Location: Canada

Seller Description

This Beechcraft King Air A100 Aircraft ­­­­­is no longer needed for company's own operation and is being sold as an asset liquidation for its owner.

General
Manufacturer: Beechcraft
Model: KingAir A100
TTSN : 28,870 Hrs
TCSN : 27,666 Cycles
Flight Rules: IFR
Wind and Prop De-Ice: Yes

 

Propellers
No. P/N REMAINING OH Due
PROP #1 HC-D4N-3C 1695 Hrs Aug-23
PROP #2 HC-D4N-3C 229 Hrs Jul-22

 

Gears
GEAR P/N REMAINING OH Due
LH Strut 99-810000-651 1425 Cycles Jan-20
LH Drag Brace 50-810335-13 7942 Cycles Mar-25
RH Strut 99-810000-652 7319 Cycles Feb-24
RH Drag Brace 50-810335-13 3980 Cycles May-21
Nose Strut 97-820000-671 1700 Cycles Apr-20
Nose Drag Brace 50-820010-609 6600 Cycles Jul-22

 

AVIONICS
Dual Garmin GNS 430AW
Dual Garmin G600 Primary Flight Display
Dual ADF-60
Garmin GTS855 TCAS
Dual GTX 330ES transponder
Garmin GWX68 Weather Radar

 

STC’S INSTALLED
Cockpit Voice Recorder (Solid State) System installed IAW LSTC O-LSA00-854/D
Stretcher System installed IAW LSTC O-LSA00-875/D
Electrical Provisions for Air-Vac Transport Incubator P/N 304-3226-900 installed IAW LSTC O-LSA01- 370/D
Commuter Interior(Passenger Seats C/W Underseat Restraint System) installed IAW LSTC O-LSA02- 597
L/H Cabin Cargo System installed IAW LSTC O-LSA03-244/D
Crew Quick Donning O2 Mask installed IAW LSTC O-LSA03-252/D
Tanis Engine Heaters Model TAS-300 installed IAW Manufacturer’s Instructions #112
Tanis Battery Heaters Model TAS-200 installed IAW Manufacturer’s instructions #114
Noise  Cancelling  Headset  Model  H10-13XP  (12507G-53)  installed  IAW  David  Clark  Installation Manual
Wing Tip Recognition Lights installed IAW Beech Aircraft Drawing 101-3063-3
Exhaust  Stack  Fairings  installed  IAW  FAA-Approved  Raisbeck  Engineering  List  R81-1003  and  STC SA3683NM
Nacelle Overwing  Stowage Lockers and  Lower Flap  Fairing installed  IAW FAA-Approved  Raisbeck Engineering List 86-1001 and STC SA3819NM
Lower Aft Fuselage Strakes installed IAW FAA-Approved Raisbeck Engineering List 87-1004 and STC SA3828NM
Fully Enclosed Main  Landing Gear Door System High-Flotation-Gear-Equipped installed  IAW FAA- Approved Raisbeck Engineering List 90-1008 and STC SA4952NM
Hartzell Quiet Turbofan Propellers and Increased Takeoff Gross Weight installed IAW FAA-Approved Raisbeck Engineering List 91-2500 and STC SA5661NM
S-TEC Autopilot installed IAW FAA STC SA7198SW-D
S-TEC Yaw Damper installed IAW FAA STC SA7199SW-D
Hot Brake Deice System installed as per Beechcraft Drawing No.100-8003, SI 0722-456
Cleveland Nose Wheel installed IAW STC SA1061GL
Latitude Technologies SKYNODE S200 Satellite Phone System carried out IAW STC SA04-59(System to be removed prior to Sale)
Artex  C406-2  ELT  Installation  carried  out  IAW  Manufacturer’s  Instructions  of  Artex  Installation Manual, MC2 Drawing 09-A100-25-60-01 R.B
Pitot Heat Failure Warning System Indication carried out IAW STC SA08-16 Issue 2
Installation of Flap Gravel Guard carried out IAW LSTC O-LSA08-161/D Issue 1
Installation  of  Stretcher,  Patient  Loading  and  Support  System  (Lifeport)  carried  out  IAW  STC SA00273WI(System to be removed prior to Sale)
Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System carried out IAW SA02153LA-D
Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System carried out IAW STC SA09-26(SA01933LA-D).
ESI-2000 Standby Instrument Installation carried out IAW SA02738CH
GWX-68 Weather Radar Upgrade installed
GTX-330 Transponder Upgrade installed
Installation of Ballast Weights carried out IAW LSTC Q-12-031/D
Inverter and Voltage Regulator Replacement carried out IAW STC O-LSA11-198/D
Installation  of  Garmin  GTS  855  (TCAS  1)  system  carried  out  IAW  STC  SA14-72  Issue  1,  FAA  STC S02121SE
Installation of the Concorde RG-380E/60L Battery carried out IAW STC SA0126W1
Installation of TI500 Incubator carried out IAW LSTC C-LSA16-122/D Issue 1

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