“These C340A Turbo high altitude high speed pressurized 6 passenger planes w 1 ton carrying capacity.



Item specifics Condition: Seller Notes:
Make: Cessna Model Year: 1979

1979 Cessna 340A with RAM Continental TSIO-520NB Engines, Robertson STOL kit and only 4,447 airframe hours and engine hours still well below TBO.
 TRUE NO RESERVE AUCTION - WOW!!! CRAZY LOW OPENING BID PRICE!!! FOR A CORPORATE OR VIP AIRCRAFT RECENTLY APPRAISED AT $281,580.00 FULL CERTIFIED APPRAISAL IS AVAILABLE BELOW. READ ON!
This aircraft is equipped with several significant upgrades including the RAM Turbo 235 hp Engine Upgrades on the Continental TSIO-520NB Engines and the highly sought after Robertson STOL kit (R-STOL - Robertson Short Take Off and Landing Kit) which enables take off and landing on much shorter runways than a factory spec Cessna 340A and which was over $40,000 upgrade at the time of installation. Full inspection report is available in the Certified Appraisal below.
Both engines are over TBO (Factory Recommended Time Between Overhaul) as measured by years since overhaul, but still a few hundred hours away from TBO as measured by flight hours. This is because the previous owner has not actively used the aircraft for several years. TBO is rated at 1600hrs or 12 years of service for these powerplants. Right engine has 1329 hours remaining until 1600hrs and left engine has 257 hours remaining. As for the McCauley Propellers - Right prop has 1809 hours remaining and left has 659 remaining, but as with the engines both props are over TBO for their years since overhaul.
Right engine does not currently achieve full spec. power and needs diagnostic service to determine whether the reduced power is an issue with the turbo waste gate actuator or a fuel pump issue. In either case this should be a relatively cheap fix and the plane should be ferriable once full power is restored to the right engine. Directly across from the current airport are two FAA A and P certified repair facilities who may be hired to do this diagnostic work if the new buyer is not an A and P FAA mechanic.
 These C340A Turbo high-altitude high speed pressurized 6-passenger planes w/ 1 ton carrying capacity are serious overkill for the average doctor or lawyer who is hunting for hundred dollar hamburgers on the weekend. They are a serious airplane that fits the niche between personal aircraft & corporate jet --much cheaper than a corporate jet to maintain & fly--but much more expensive than a single prop piston 4 or 6 seat family aircraft that flies lower & slower and consumes less fuel & is cheaper to maintain. Despite their vintage C340As look and fly like multi-million dollar modern planes. With a little investment in new interior, modern paint job and regular TBO service, this sleek twin engine can give a growing company or high profile individual almost the same peer/client respect as owning a million+ dollar aircraft at a tiny fraction of that expense. Unless they are a pilot themselves, most clients don"t realize these planes can be as affordable as they are.
 PLEASE READ TERMS OF SALE CAREFULLY
THERE IS A SINGLE NON-REFUNDABLE $650.00 DEPOSIT FEE DUE VIA PAYPAL AT THE END OF THE AUCTION IN ADDITION TO THE PURCHASE PRICE. We are eager to discuss this aircraft with you by telephone and physical inspections are available with appointment.
 We are a nationwide charity focused on restoring coral reefs and preventing plastic contamination of the oceans. A very generous supporter has donated this valuable airplane to support our vital mission for the oceans. Their tax write-off can be your opportunity to acquire an incredible aircraft for potentially a deep, deep discount off fair market value.

This is a serious airplane! If you are a corporate CEO or high profile individual looking to acquire your own affordable aircraft to shuttle business executives to areas without major airports or to deliver vital supplies thousands of miles at a moments notice, this aircraft could be the opportunity you have been looking for. Or it could be a family aircraft if you are a high net worth individual who can afford to own and maintain an aircraft capable of taking off and landing on very short runways while carrying a family of six with luggage with a range of nearly 1500 miles per fueling and a top airspeed rating of 235 miles per hour (205 kts).
With the ability to fly in a pressurized cabin at 21,000 feet of altitude, this aircraft is a very specialized global tool.

If you are a private pilot you would need to get a twin engine certification to fly this plane, but most company owners will typically hire their own charter pilot to do the flying while the executives meet in the back or have a pilot do global deliveries of medical supplies, custom critical equipment, perishable items etc. A certified pilot can deliver people or goods in a aircraft like this one from a tiny airport on the US East Coast to a tiny airport on the US West Coast with only one or two fuel stops and arrive in half the time as a air priority courier service or taking a commercial jet and renting a car and driving. And the payload capacity for fuel, people,luggage and cargo is a very impressive 2000 lb...more than twice the carrying capacity of a standard single prop six-seater aircraft.

If you are new to aircraft ownership please call to discuss this airplane prior to bidding. There are a lot of hidden expenses to aircraft ownership and owning and maintaining a large dual engine aircraft such as this one (even in relatively good condition as this one is) is an expensive proposition for a private salary budget.

Your bid is a legally binding purchase contract to purchase this aircraft at the final auction bid price, so please call before bidding to arrange a physical inspection if that is a requirement to you for completing the transaction and please call and discuss the full details of this plane, the auction transaction and entire your legally binding bid/purchase contract as a fully informed buyer. I am available via text or direct call during standard business hours 7 days per week at 970 319-6408. -Will
EVEN IF YOU ARE ALREADY A TWIN PROP CERTIFIED PILOT WITH A LOT OF EXPERIENCE THEIR ARE A LOT MORE DETAILS TO GO OVER THAN I CAN EASILY TYPE OUT EVEN IN THIS LONG DESCRIPTION.
THERE IS A SINGLE NON-REFUNDABLE $650.00 DEPOSIT FEE DUE AT THE END OF THE AUCTION IN ADDITION TO THE PURCHASE PRICE.
I HAVE 40 MORE PICTURES THAT TELL AN EVEN BETTER STORY OF THIS AIRCRAFT TO REQUEST THE EXTRA PICTURES TEXT YOUR EMAIL ADDRESS TO WILL 970 319 6408 AND THEY WILL BE EMAILED TO YOU Appointments may be made to inspect the aircraft prior to close of the auction by calling the number above.
The Cessna 340 is one of the most popular and identifiable pressurized, light twin-engine aircraft in general aviation. It’s a great airplane for those wishing to transition from a high-performance single, or those wishing to add some small commuters to their business fleet. There’s not much to flying the Cessna 340. Takeoffs and landings will almost make a pilot complacent. Landing doesn’t even really require a flare, set the attitude early, pull the power, and the airplane settles itself onto the runway. What really makes this aircraft great is the pressurized cabin. The rear four seats are arranged in a club configuration, with the middle row facing backward, giving passengers a little more legroom when they’re not knocking knees or feeling cramped. A typical cruising altitude in the Cessna 340 is around 18,000-21,000’. Above the little guys but below the big guys! At this altitude, you’ll be cruising between 190-205 knots consuming between 30-36 gallons per hour. A family of four can hop in a 340 and get out of town for the weekend, with standard full fuel tanks, and have a range of 1,000 miles with reserves.Cessna 340A SpecificationsEngine: 2 x Continental TSIO-520-NBHorsepower: 310 hp eachPropellers: McCauley CS/76in. 3-bland-constant-speedLength: 34 feet 4 inchesHeight: 12 feet 7 inchesWing Span: 38 feet 1 inchWing Area: 184 square feetWing Loading: 32.6 pounds/square footPower Loading: 9.7 pounds/horsepowerSeats: 1 pilot and 5 passengersCabin Height: 49 inchesCabin Width: 46.5 inchesEmpty Weight: 4,142 poundsMaximum Gross Weight: 5,990 poundsMaximum Takeoff Weight: 5,990 poundsUseful Load: 1,848 poundsBaggage Capacity: 950/53Fuel Capacity: 100 gallons plus 63-gallon reserveCessna 340A Performance(PLEASE NOTE - THESE ARE THE SPECS BEFORE INSTALLATION 0F THE ROBERTSON SHORT TAKE OFF AND LANDING KIT SO ACTUAL NUMBERS MAY BE EVEN CONSIDERABLY BETTER THAN THESE)
Takeoff Distance Ground Roll: 1,615 feetTakeoff Over 50 ft. Obstacle: 2,175 feetRate of Climb, Sea Level: 1,650 feet per minuteTop Speed: 281 miles per hourCruise Speed: 230 miles per hourStall Speed: 94 mphFuel Consumption: 34 gallons per hour at 75% powerEndurance (65% power with 1 hr reserve): 5.5 hoursRange: 1,618 milesService Ceiling: 29,800 feet MSLLanding Ground Roll: 770 feetLanding Over 50 ft. Obstacle: 1,850 feet
APPRAISAL BELOW:
LET"S START WITH THE APPRAISER"S CONCLUSION COMMENT ABOUT THIS 1979 CESSNA 340A "The subject Cessna 340A described within this appraisal report was built in 1979 andbears the manufacturer serial number 340A0791. With a total of 4,447.0 hours of utilizationsince new, it has less than average total time as compared to the world wide Cessna 340A fleet. The subject aircraft is equipped with a variety of popular modifications, above average paint,overall average avionics, and instruments and well documented maintenance. However, itsengines and propellers have exceeded their TBO (time before overhaul) calendar service lifelimitation, its interior is in below average condition and it has a history of repaired damage. All considered, the subject Cessna 340A is viewed as an overall well above average example of its make, model and year of manufacture."
AIRCRAFT IDENTIFICATION & GENERAL INFORMATION Manufacturer: Cessna Aircraft Company Model: 340A Serial Number: 340A0791 U.S.A. Registration: N340CC Year of Manufacture: 1979 Engine Make & Model: Continental TSIO-520NB Piston Total Airframe Hours: 4,447.0 hours Configuration: Passenger; seating for 5 (incl. pilot) Type Aircraft: Fixed wing, land, multiengine piston powered. Airworthiness Certification: Certification Date: 09-27-1979 Classification: Standard Category: Normal Registration: Country of Registration: U.S.A. Registration Date: 12-17-2018 Expiration Date: 12-31-2021 Total Airframe Hours: 4,447.0 hours
Aircraft Identification & General Information Summary: The subject aircraft, Cessna 340A bearing serial number 340A0791 was manufactured in 1971 and is currently registered in the U.S.A. as N340CC. Its original and current FAA Standard Airworthiness Certificate was issued on 09-27-1979 and its current FAA Registration is dated 12-17-2018 with an expiry date of 12-31-2021. The aircraft has accumulated a total of 4,447.0 hours on its airframe since new. Recordings from the Hobbs hour meter is the method in which the airframe, engine and propeller times are recorded. The aircraft is currently authorized to operate privately in accordance with Federal Aviation Administration Regulations
MAINTENANCE RECORDS & TECHNICAL MANUALS Maintenance Records: The maintenance records for the subject aircraft were presented to the appraiser. The aircraft maintenance records consist of three (3) airframe logs, one (1) engine log for each of the two engines, one (1) propeller log for each of the two propellers and associated records relative to modifications, and airworthiness release certification.Airframe log number 1 begins on 02-16-1979 at 31.7 hours total airframe time with record of miscellaneous servicing and ends on 09-17-1986 at an unrecorded total airframe time with record of log book closure.Airframe log number 2 begins on 07-31-1986 at 1,410.9 hours total airframe time with record of a Ram Industries modification and ends on 06-10-2000 at 3,186.4 hours total airframe time with record of air conditioning servicing.Airframe log number 3 begins on 02-04-2000 at 3,111.2 hours total airframe time with record of an annual inspection and ends on 10-01-2018 at 4,447.0 hours total airframe time with record of an annual inspection.The left engine log begins on 12-04-2000 at 0.0 hours total engine time since overhaul with record of its installation to the airframe and ends on 10-01-2018 at 1,342.3 hours total engine time since overhaul with record of an annual inspection.The right engine log begins on 07-09-2007 at 0.0 hours total engine time since overhaul with record of its installation to the airframe and ends on 10-01-2018 at 270.8 hours total engine time since overhaul with record of an annual inspection.The left propeller log begins on 02-04-2000 at 0.0 hours total propeller time since new with record of its installation to the left engine and ends on 10-01-2018 at 1,340.3 hours total propeller time since new with record of an annual inspection.The right propeller log begins on 08-27-2007 at 0.0 hours total propeller time since new with record of its installation to the right engine and ends on 10-01-2018 at 190.8 hours total propeller time since new with record of an annual inspection.
Maintenance Records & Technical Manuals Summary: The maintenance records for the subject aircraft areconsidered to be authentic, unaltered and complete.The minimum required technical manuals manuals areincluded with the aircraft.
MAINTENANCE STATUS Serviceability Status: Aircraft is conditionally serviceable due to an expired annual inspection and, pitot static, altimeter and transponder certification requirements. Maintenance Program: FAA approved manufacturer’s maintenance program. Maintenance Tracking Program: Maintenance log book record tracking system. Airworthiness Directives Status: Applicable ADs reported as complied with. Annual Inspection Status: Date Completed: 10-01-2018 Next due: 10-31-2019 (Expired) Pitot Static System/Altimeter Certification Status: Date Completed: 04-20-2018 Next due: 04-30-2020 (Expired) Transponder Certification Status: Date Completed: 04-20-2018 Next due: 04-30-2020 (Expired) Maintenance Status Summary: According to available maintenance records and reports,this aircraft is conditionally serviceable due to expiredannual inspection and, pitot static, altimeter andtransponder certification requirements.
AIRFRAME COMPONENTS Fuselage Skins: The fuselage skins are considered to be in above average condition absent of significant defects. All skins are pulled tight, rivets flush and secure, with no current evidence of defects or damage. Wing Assembly Skins: The wing assembly skins are considered to be in above average condition absent of significant defects. Both wings are equipped with R/STOL vortex generators. All skins are pulled tight, rivets flush and secure, with no current evidence of defects or damage. Empennage Skins: The empennage skins are considered to be in above average condition absent of significant defects. The vertical stabilizer is equipped with R/STOL vortex generators. The skins on the vertical and horizontal stabilizer components are pulled tight, rivets flush and secure, with no current evidence of defects or damage. Control Surfaces: All control surfaces are properly aligned and securely attached to the wing and empennage structure. All control surfaces are considered to be in average condition absent of defects or damage. AIRFRAME COMPONENTS Fuselage Skins: The fuselage skins are considered to be in above average condition absent of significant defects. All skins are pulled tight, rivets flush and secure, with no current evidence of defects or damage. Wing Assembly Skins: The wing assembly skins are considered to be in above average condition absent of significant defects. Both wings are equipped with R/STOL vortex generators. All skins are pulled tight, rivets flush and secure, with no current evidence of defects or damage. Empennage Skins: The empennage skins are considered to be in above average condition absent of significant defects. The vertical stabilizer is equipped with R/STOL vortex generators. The skins on the vertical and horizontal stabilizer components are pulled tight, rivets flush and secure, with no current evidence of defects or damage. Control Surfaces: All control surfaces are properly aligned and securely attached to the wing and empennage structure. All control surfaces are considered to be in average condition absent of defects or damage. Fuselage Access Doors & Seal Assemblies: All fuselage access doors and seal assemblies are considered to be in average condition absent of significant defects or damage. The cabin entry door and both nose baggage storage doors open properly and fit flush with fuselage when closed. All door seal assemblies are undamaged and serviceable. Fuselage Storage Compartments: The nose baggage storage compartment is considered to be in above average condition absent of defects or damage. Windshield & Windows: The two windshield panels, 11 side fuselage windows and 2 cockpit DV windows are considered to be in above average condition absent of significant scratches, crazing or delamination. Fuselage cabin window 1R additionally serves as an emergency exit hatch. Landing Gear Components: The landing gear components are considered to be in average condition absent of significant defects. All landing gear and brake assemblies are clean with no evidence of excessive fluid leakage. All landing gear door assemblies are in above average condition absent of significant defects or damage. All tires have approximately 80 percent tread life remaining. Engine Nacelle Assemblies: The engine nacelle assemblies are considered to be in average condition absent of significant defects or damage. Both assemblies are secure, clean and undamaged. Pitot Tube & Static Ports: The pitot tubes and static ports are considered to be in average condition absent of significant defects. All components are secure, clean and unobstructed. Antenna & Static Wicks: The antenna and static wicks are considered to be in average condition absent of significant defects. All antenna installations are securely attached and appear to meet manufacturer specifications. A total of 7 static wicks are installed with none missing. Exterior Lights: The exterior light systems are considered to be in above average condition absent of significant defects. The exterior lights include the following components:• Standard navigation and beacon lights • Landing lights • Taxi light • Strobe lights • Ice detection light Airframe Components Summary: The external airframe components are considered to be in overall above average condition for its make, model, year of production and hours of utilization. There is no evidence of defects or damage to the external components. ENGINES Engine Manufacture: Continental Engine Type: Piston Model: TSIO-520NB Manufacturer TBO: 1,600 hours of operation / 12 years in service. Engine Position 1 (Left) Serial Number: G519659 Modifications: Ram Aircraft 235 h.p. modification. Serviceability: Reported as serviceable. Time Since New: 3,823.3 hours of operation Time Since Last Overhaul: 1,342.3 hours of operation / 21 years in service. Date of Last Overhaul: 02-04-2000 TBO/ Time Remaining: 257.7 hours of operation / 9 years overdue. Engine Position 1 Summary: This engine is considered to be an upgraded power plant installation to the make, model and year of production aircraft and is considered to be in serviceable condition. However, with a manufacture published overhaul requirement of 1,600 hours of operation or 12 years in service (whichever occurs first), this engine is currently 9 years overdue for an overhaul. Engine Position 2 (Right) Serial Number: 514068 Modifications: Ram Aircraft 235 h.p. power plant installation. Serviceability: Reported as serviceable. Time Since New: 5,303.0 hours of operation Time Since Last Overhaul: 270.8 hours of operation / 13 years, 7 months in service. Date of Last Overhaul: 07-09-2007 TBO/ Time Remaining: 1,329.2 hours of operation / 1 year, 7 months overdue. Engine Position 2 Summary: This engine is considered to be an upgraded power plant installation to the make, model and year of production aircraft and is considered to be in serviceable condition. However, with a manufacture published overhaul requirement of 1,600 hours of operation or 12 years in service (whichever occurs first), this engine is currently 1 year 7 months overdue for an overhaul. PROPELLERS Propeller Manufacture: McCauley
 Propeller Type: Controllable Model: PHC-C3YF Number of Blades: 3 Manufacturer TBO: 2,000 hours of operation / 6 years in service. Propeller Position 1 (Left) Hub Serial Number: 991988 Blade Serial Numbers: 1) TH212 2) TH217 3) TH219 Modifications: Hartzell Q-Tip series propeller installation. Serviceability: Reported as serviceable. Time Since New: 1,340.3 hours of operation / 21 years in service. Date of Installation: 02-04-2000 Time Since Last Overhaul: Not applicable. TBO/ Time Remaining: 659.7 hours of operation / 15 years overdue. Propeller Position 1 Summary: This propeller is considered to be an upgraded installation to the make, model and year of production aircraft and reported to be in serviceable condition. However, with a manufacture published overhaul requirement of 2,000 hours of operation or 6 years in service (whichever occurs first), this propeller is currently 15 years overdue for an overhaul. Propeller Position 2 (Right) Hub Serial Number: 060753 Blade Serial Numbers: 1) AAB26400 2) AAB26182 3) AAB26195 Serviceability: Reported as serviceable. Time Since New: 1,340.3 hours of operation / 21 years in service. Date of Installation: 02-04-2000 Time Since Last Overhaul: 190.8 hours of operation / 13 years, 5 months in service. Date of Last Overhaul: 08-27-2007 TBO/ Time Remaining: 1,809.2 hours of operation / 7 years, 5 months overdue. Propeller Position 2 Summary: This propeller is considered to be an upgraded installation to the make, model and year of production aircraft and reported to be in serviceable condition. However, with a manufacture published overhaul requirement of 2,000 hours of operation or 6 years in service (whichever occurs first), this propeller is currently 7 years, 5 months overdue for an overhaul. ICE PROTECTION SYSTEMS Equipped for Known Icing: Equipped. Airframe: Equipped; pneumatic boots. Propellers: Equipped; electrically heated boots. Pitot Heat: Equipped; electrically heated. Stall Warning: Equipped; electrically heated. Windshield: Equipped; electrically heated panel. Ice Protection Systems Summary: This aircraft is equipped for flight into known icing conditions. The ice protection systems installed are reported to be serviceable and considered to be in above average condition with no significant defects noted. AVIONICS & INSTRUMENTS Full Instrument Panel: Equipped. Dual Flight Instrument Panel: Equipped; full left panel / partial right panel. Analog or EFIS: Analog. IFR Equipped: Equipped. GPS System: Equipped. Terrain Warning System: Equipped. Traffic Advisory System: Capable. ADS-B System: Not equipped. Condition of Avionics and Instruments: All components are reported to be in serviceable condition. INVENTORY OF AVIONICS & INSTRUMENTS ADI / Flight Director - L: Cessna - 400A Airspeed Indicator - L: Cessna - C661045 Altimeter - L : ARC - EA-401A Altimeter - R: United Instruments - 5934 Altitude Alerter: Cessna - AA-801A Attitude Indicator - R: Allen - 26AK Audio Selector Panel: PS Engineering - PMA-7000 MS Autopilot/AFCS: Cessna - 400A Course Deviation Indicator - L: Garmin - GI-106 Chronometer - L: Davtron - M-877 Compass - magnetic: Airpath - Not specified ELT: Not specified - Not specified Electronic Engine Data Monitor: JPI Instruments - EDM-760 Electronic OAT/ALT/Volt Indicator: Davtron - M655 Electronic Fuel Flow Indicator: Shadin - 910532 GPS/Nav/Com: Garmin - GNS-530 HSI - L: Bendix-King - KI-525 Intercom: PS Engineering - PMA-7000 MS Marker Beacon: PS Engineering - PMA-7000 MS Multifunction Display: Garmin - GMX-200 Nav/Com: Garmin - SL-30 Terrain Warning System: Garmin - GMX-200 Traffic Advisory System: Garmin - GMX-200 Transponder - 1: Garmin - GTX-330 Transponder - 2: Bendix-King - KT-760 Turn Coordinator Indicator - L: GAI - 509 Vertical Speed Indicator - L : Aerosonic - 30230 Weather Radar: Narco - KWX-56 Avionics & Instruments Summary: The avionics and instrument installations are considered to be average overall for this make, model and year of production aircraft. Additional upgraded components include a JPI Instruments EDM-760 engine monitor, Davtron M655 OAT/ALT/Volt indicator and a Shadin 910532 fuel flow indicator. However, the aircraft is not equipped with an ADS-B out system as required in accordance with F.A.R. 14 CFR § 91.225. All installed components are reported to be in serviceable condition. EXTERIOR PAINT Exterior Paint Colors: Overall Oyster White with accent stripes along both sides of the fuselage, tail section and wing tip tanks in wine and dark blue. The registration markings are painted in matching wine and dark blue. Age of Paint: 22 years, 4 months; applied on 10-27-1998. Condition of Paint: The exterior paint is considered to be in above average condition absent of significant wear or defects.Exterior Paint Summary: The paint on the exterior surfaces of the aircraft is an attractive design suitable to its make and model. The condition of the painted surfaces is considered to be above average relative to its age and hours of utilization. INTERIOR Interior Description & Condition: The interior furnishings consist of two forward cockpit area seats and three rear cabin passenger seats. All seats are upholstered in Sabrina red wine leather material. The two pilot seats are considered to be in poor condition with evidence of significant wear and tear to the leather materials. The three passenger seats are considered to be in overall average condition absent of excessive wear and tear. Flooring throughout the interior is covered in a red wine colored carpet considered to be in below average condition with evidence of moderate wear, tear and soiling.The ceiling headliner within the interior is upholstered in oyster white fabric and leather materials considered to be in average condition absent of significant wear and tear. Air vents, reading lights and air conditioning ventilation outlets are installed within the headliner throughout the interior.The interior side walls of the cabin interior are upholstered in red wine and oyster leather materials considered to be in average condition absent of significant wear and tear. Intercom communication ports are installed at each passenger seat location and a single, fold-out style burlwood convenience table is installed on the right cabin side wall.In addition to the windshield panels, there are nine passenger side fuselage windows, two cockpit side fuselage windows and two cockpit DV windows installed on the aircraft. All interior surface panels are considered to be in above average condition absent of significant scratches or the effects of crazing. Passenger window position 1R additionally serves as an emergency exit hatch. Each passenger window position is equipped with an adjustable fabric curtain.A baggage storage area is located at the most aft section of the interior. It is accessible from within the aircraft during flight as well as on the ground through the cabin access door. The baggage storage area is considered to be in overall average condition absent of excessive wear and tear.Cabinetry within the interior include a single wood laminate 3 drawer storage unit located in the forward section of the interior between the copilot seat and passenger seat 1R. The cabinet is considered to be in average condition absent of excessive wear and tear.Additional furnishings and equipment within the interior include a Keith air conditioning system, a supplemental oxygen system, an audio entertainment system with a CD player and XM radio connectivity, a single, hand-held portable fire extinguisher and all standard fixtures typically installed within the make and model aircraft. Age of Interior Furnishings: 22 years, 4 months; refurbished on 10-27-1998. Intercom System: Equipped Entertainment System: Equipped; CD player and XM radio availability. Interior Summary: The interior configuration and furnishings on this aircraft are considered to be generally standard for its make, model and year of production. The interior was refurbished during 1998 with new materials and considered to currently be in below average condition due to the poor condition of the pilot seat upholstery and the below average condition of the floor carpeting. MODIFICATIONS Only those modifications determined to have significant relevance to the value of the subject aircraft are included within this appraisal report. Modification 1: STC: SE4327SWModification: Installation of Ram Continental TSIO-52-NB engines. Modification 2: STC: SA4241SW Modification: Installation of Ram Hartzell PHC-c3YFQ-Tip propellers. Modification 3: STC: SA474NW Modification: Installation of Ram STOL vortex generators. Modification 4: STC: SA5796SW Modification: Installation of Hoskins fuel flow system. Modification 5: STC: SA2872SW Modification: Installation of wing nacelle auxiliary fuel tanks. Modification 6: STC: SA5137NM Modification: Installation of Rosen windshield sun visors. ADDITIONAL EQUIPMENT Only the additional installed equipment determined to have significant relevance to the value of the subject aircraft are included within this appraisal report. Equipment Item 1: Keith Air conditioning system. DAMAGE HISTORY Current Damage: None noted. Previous Damage History: Damage Record Number 1 Damage Repair Date: 05-25-1981 Classification of Damage: Moderate. Description of Damage: Records indicate the extent of damage required repair and/or replacement of the following components: Airframe; Right and left wing inboard leading edge skins, right and left lower wing skins, right and left inboard wing deice boots, main landing gear trunion and lower retract arm bolts.Records indicate that all repairs made I.A.W. manufacturer published procedures.Certified Fair Market Value as of February 26, 2021 1979 Cessna 340A Aircraft Serial Number 340A0791 $281,580.00 THIS AIRCRAFT IS LOCATED IN VENICE, FLORIDA
SHIPPING OR TRANSPORT SHIPPING IS THE RESPONSIBILITY OF THE BUYER. PLEASE SEEK YOUR TRANSPORTATION SOURCE AND SECURE YOUR QUOTES BEFORE BIDDING PAYMENTS INSTRUCTIONS THE DEPOSIT AND DOCUMENTATION FEE IS NOT REFUNDABLE, AND MUST BE MADE THRU PAYPAL WITHIN 24 HOURS OF THE AUCTION CLOSE. THE FINAL PURCHASE PRICE MUST BE PAID WITHIN 3 DAYS OF AUCTION CLOSE.
Current date: 2021-04-19