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Equipment Specifications
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Year
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2005
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Manufacturer
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BEECHCRAFT
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Model
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A36 BONANZA
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Price
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US $430,000
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Location
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Fort Myers, Florida
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Condition
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USED
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Serial Number
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E-3607
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Registration Number
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N946AJ
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Total Time
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325 Hours
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Flight Rules
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IFR
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Number Of Seats
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6
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General Information
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GNS 530W/430W, MX-20, Skywatch, WSI Weather, EDM-700, Avionics Warranty-SUPERB! Video.
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Detailed Description
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Truly a 9.8 in and out, this remarkably well equipped, superbly well maintained aircraft shows care it has received; having never spent a night outside and having been thoroughly wiped down after each flight (interior and exterior!). Annuals by two of the most respected Beech Factory Authorized shops, logs are squeaky clean. All AD's current. Nary a blemish on either the paint or interior. Allied Signal/Honeywell/King warranty until April, 2010.
Airframe:
325 TOTAL TIME, ANNUAL MARCH, 2009 HAWKER BEECHCRAFT, TAMPA, TIM BACKLUND
Engine Specs:
Teledyne Continental/Raytheon Special Edition six cylinder IO-550-B fuel injected engine rated at 300 horsepower
325 TOTAL TIME, ALL COMPRESSIONS 68 OR BETTER LAST ANNUAL
Prop(s):
Hartzell three blade, aluminum alloy, 80” diameter, constant speed propeller with polished spinner
325 TOTAL TIME
Avionics/Radios:
HONEYWELL/BENDIX/KING AVIONICS WARRANTY THROUGH APRIL, 2010 MFD - GARMIN MX20; TRAFFIC - L3 COMMUNICATIONS SKY WATCH 497; WEATHER - WSI AV-300 DATA LINK WEATHER SYSTEM AND WX-500 STORMSCOPE; BOSE HARDWIRING PILOT AND COPILOT
No. 1 Nav/Comm/GPS - Garmin GNS 530W Comm transceiver, Nav/glideslope, GPS and moving map with course information displayed on KI 525A indicator
No. 2 Nav/Comm/GPS - Garmin GNS 430W Comm transceiver, Nav/glideslope, GPS and moving map with course information displayed on Garmin GI 106A VOR/ILS/GPS indicator
Transponder - KT 76C Mode A/Mode C with pilot’s control wheel Ident button
Encoding altimeter - Honeywell KEA 130A with three pointer display (feet/inches/millibars)
Audio control system - PS Engineering PMA7000B audio amplifier/intercom/marker beacon receiver includes: pilot’s and copilot’s control wheel microphone buttons; pilot’s and copilot’s microphone and headphone jacks; microphone and headphone jacks at no. 3, no. 4, no. 5, and no. 6 cabin chair locations; interphone between pilot, copilot, and passengers; two miniature audio inputs (these jacks have the capability to accept external stereo CD audio which will then provide stereo output at all headphone locations); two split comm modes provided; digital audio playback of previous 1 minute of incoming radio transmissions controlled through pilot’s control wheel mounted switch
Remote marker beacon light panel
KFC 225 autopilot system (includes altitude preselect, vertical speed select, and altitude alerter features) KI 256 flight command indicator/gyro horizon
KCS 55A compass system includes KA 51B slaving meter, KI 525A 07 horizontal situation indicator, KA 285A remote autopilot annunciator
Yaw damper
KA 33 cooling blower
L3 Communications WX-500 Stormscope weather mapping system (displayed/controlled through either the GNS 530 or GNS 430 with remote storm clear function also available through pilot’s control wheel mounted switch)
Shadin ADC 200+ fuel/airdata computer (displayed on either the GNS 530 or GNS 430)
Hand-held microphone (mounted on end of armrest between pilot's chair)
Cockpit speaker
Static wicks
Avionics master switch
Emergency locator transmitter (ELT) with cockpit switch
Additional Equipment:
AIR CONDITIONING; ELECTRO-THERMAL PROPELLER DEICE SYSTEM; JPI EDM-700 ENGINE MONITOR; PILOT/COPILOT SHEEP SKIN COVERS
Landing Gear And Brakes Tricycle type with electro-mechanical extension and retraction system; Steerable nose landing gear with shimmy damper and Beech oil-air strut; Main wheel tires (tube type) - 7.00 x 6 Nose wheel
tire (tube type) - 5.00 x 5; Two-spot hydraulic disc brakes; Fully enclosed nose and main landing gear; Auxiliary landing gear extension control; Throttle and flap controlled, landing gear-up warning horn, and
annunciator light Throttle controlled, landing gear retract prevention system; Systems And Controls--Conventional dual column, three axis control system with adjustable pilot's (left side) rudder pedals, Adjustable copilot's (right side) rudder pedals; Individual toe operated pilot's and
copilot's brakes; Parking brake with hand control; Electronic stall warning horn; Adjustable aileron and dual elevator trim tabs; Pedestal mounted throttle, propeller and mixture control levers; Defroster control and ventilation and heating controls; Electrically actuated three position Fowler type flap controls; Manual cowl flap control; Standby instrument air pressure system; Alternate static air source; Heated pitot tube; Dual static air ports; Engine Instruments-- Manifold pressure gauge, Tachometer, Fuel flow gauge with electronic fuel flow transducer, Cylinder head temperature/exhaust gas temperature gauge Oil pressure/oil temperature
gauge; Dual fuel quantity gauges; Alternator load meter Bus voltmeter; Cockpit Instruments--True airspeed indicator, Instantaneous vertical speed indicator, Electric turn coordinator, Standby magnetic compass, Outside air
temperature gauge, Pilot's control wheel LCD digital chronometer clock; Instrument air pressure gauge, Flight hour recorder. Electrical--28 Volt System 100 ampere alternator, Standby alternator - (20 amp continuous),
15.5 ampere/hour battery Voltage regulator, Over-voltage regulator, External power receptacle, Electrical circuit protection. Internal Lights--Internally lighted flight and engine instruments, Electroluminescent subpanel lighting, Instrument panel floodlighting in glareshield. Annunciator light panel in glareshield. Landing gear position lights, Flap position indicator lights, Trim tab position indicator lights. Pilot's and copilots white control wheel map lights, Adjustable reading lights above all passenger seats. Entrance door and rear step courtesy lights and
timer. Outside air temperature gauge light, Fuel tank selector light; External Lights--Landing light in cowling, Taxi light on steerable nose landing gear, Wing tip and tail navigation lights, Anti-collision red flashing lights on vertical tail, Bottom mounted white oscillating beacon,
Wing tip and tail strobe lights. Cabin Ventilation--blower Fresh air, ventilation system with eight individual outlets. One piece windshield, Pilot's openable storm window, Windshield and windows with ultraviolet
protection. Windows tinted in light gray. Center club seating window openable for ground ventilation, has positive lock to prevent opening in flight, and may be used as emergency exit. Super soundproofing, Glove compartment in instrument subpanel, Adjustable front seat sun visors,
Cabin fire extinguisher* (Halon) *Warning - contains Halon substance which harms public health and environment by destroying ozone in the upper atmosphere. Large double doors for easy passenger boarding or cargo loading. Four coat hooks, Four cupholders, Six ashtrays, Extended aft
baggage compartment with clothes hanger bar, Removable nylon hat shelf in aft baggage area, Removable nylon webbing in aft baggage area. Capable of cargo storage on aft cabin floor. Matching black baggage restraint webs
and 5th and 6th seat support straps. Seats And Interior Furnishings--Vertically adjustable pilot's and copilot's seats, Pilot's sidewall storage pocket, Pilot's and copilot's seat with headrest, lumbar support, shared armrest, inertia reel shoulder harness with matching lap belt, and four position cam lever seat back adjustment. Club seating arrangement: Aft facing 3rd and 4th seats with headrests, lumbar support, shared armrest, inertia reel shoulder harnesses with matching lap belts and four position cam lever seat back adjustment. Forward
facing 5th and 6th seats with reading lights, air outlets, headrests,inertia reel shoulder harnesses with matching lap belts. Executive writing desk on left side with Acajou Mahogany laminate. Loose Equipment--One Telex
Twinset headset (emergency backup), Tow bar, Pitot tube cover, Gust lock assembly, Engine winter baffles, Flight bag, Oil drain probe, Fuel tester and drain tool, First aid kit, Aircraft log book, Engine log book, Engine manuals, Propeller log book, Service and safety information materials, Avionics wiring diagrams and avionics pilot guides, Passenger briefing cards, Pilot's Operating Handbook and FAA approved Airplane Flight Manual,
Aft cabin cargo web. Additional Features--Exterior high solids urethane paint, Complete internal polyamide epoxy corrosion proofing, Quick removable fuel tank
caps, Stainless steel cabin assist step.
Year Painted:
2005
Exterior:
Exterior Paint Scheme
Paint design 99A-IDV-A36-1
#1 Color (overall) Matterhorn White
#2 Color (stripe) Regimental Blue
#3 Color (stripe) Clarette
#4 Color (stripe) Silver Metallic
Registration Number
Registration number N946AJ
Slanted, Chamfered Regimental Blue
Drop Shadowed Clarette
9.8--TRULY!
Interior:
Interior
Headliner Pale Beige Ultrasuede
Vertical trim panels Platinum leather
Horizontal trim panels Acajou Mahogany
Sidewall and armrests Sesame leather
Floor covering Thatch Galaxy carpet
Seat inserts and trim Sesame leather
Seat belts Fawn
Instrument panel Castle Tan
9.8--TRULY!
Inspection Status:
ANNUAL MARCH, 2009 HAWKER BEECHCRAFT, TAMPA, BY TIM BACKLUND
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Contact:
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Bob LaFerriere Aircraft, Inc.
Bob La Ferriere
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Aircraft Located in:
Fort Myers, Florida
Phone: (727)709-2704
Fax: (727)935-4606
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