2011 DIAMOND DA20 C-1 “ECLIPSE” 125hp. Garmin G-500 Glass Panel. Beautiful condition. Location VERO BEACH, FL. ONE OWNER, DRY COUNTRY OPERATED, ALWAYS HANGARED, NO DAMAGE ALL LOGS. (Fresh annual to be performed early March.) Perfect modern and economical training and cross country aircraft. Real performaner, with a real engine (not underpowered like many other two seat aircraft). Best priced G-500 C-1 on the market, and you will not find a cleaner one. Please call or email for more information.
Avionics / Equipment
Avionics/RadiosGarmin G500 Glass with Safe Taxi, Terrain warning and more.Dual 6.5” diagonal color LCD displays with RGB backlighting technology, direct sunlight readable.Garmin GMA-340 Audiopanel.Garmin GNS 430 GPS/NAV/COM with glideslope receiver # 1 Com.Garmin SL40 VHF COM # 2 Com.Garmin 327 Transponder.Additional EquipmentExternal power unit receptacleWheel fairings, (like new)Second altimeter, airspeed indicator and more.Electric trim and flaps
Airframe
Total Time since new: 1493 hours
Interior / Exterior
ExteriorWhite with Diamond Blue and Gray custom striping. Close to factory new condition.InteriorPremium Leather interior with foldable Headrests. No wear or tear. Close to new condition.Four-way seat belts Extended glare shieldEngraved aluminum throttle quadrant cover plates
Price
Contact Details
(772) 766-4917 Contact:Carl Bondesson Vero Beach, FL USA
2011, 186 TT, Experimental S2S from factory made sub assemblies (fuselage, wings, empenage, gear, motor mount, etc.) Airframe mod for easier maintenance. 8:1 pistons, spin on oil filter. Built for competitive aerobatics.
In the early ’80s, the Pitts factory made a limited number of S2S “kits” available for sale. They included just about everything needed to complete the airframe including the fuselage, wings, empennage, gear, wires, cowl, cabanes, motor mount, controls, push rods, bearings, bell cranks,etc. They were either a manufactured or supplied by the Pitts Factory. Most everything had factory serial numbers or a factory stamp. Both the fuselage and all three wing assemblies were completed and have factory serial numbers. When I bought it, it was stored in a heated hangar. Some major assembly had been completed. An IO-540 and a Hartzell aerobatic propeller was installed. Every nut, bolt, hose, screw, etc. is new. The fuel tanks, windscreen and canopy are from other aircraft. It was professionally finished and painted.
Engines / Mods / Prop
The engine has ~185hours TT since first major. It had 1940hours TT prior to MOH in this configuration. It is a lycoming IO-540: parallel valve cylinders, heavy crankshaft, impulse coupling Bendix 1200 series Magnetos, complete Christen inverted fuel and oil system including vac pad pickup. 8.5 to 1 pistons were installed at major. It performs flawlessly, oil changed every 10 to 15 hours. After approximately 80 hours TT, a spin on oil filter was installed. It puts out more than 260hp, probably around 300. The Hartzell aerobatic prop has ~185hours SMOH.
Interior / Exterior
See Pics.
Remarks
In the early ’80s, the Pitts factory made a limited number of S2S “kits”available for sale. They included just about everything needed to complete the airframe including the fuselage, wings, empennage, gear, wires, cowl, cabanes, motor mount, controls, push rods, bearings, bell cranks,etc. They were either a manufactured or supplied by the Pitts Factory. Most everything had factory serial numbers or a factory stamp. Both the fuselage and all three wing assemblies were completed and have factory serial numbers.When I bought it, it was stored in a heated hangar. Some major assembly had been completed. An IO-540 and a Hartzell aerobatic propeller was installed.Both the engine and prop were 0 SMOH (the engine was pickled.) I started the fabrication process by essentially taking everything apart and starting the build from scratch. Every nut, bolt, hose, screw, etc. is new. The fuel tanks and windscreen came out of Sean Tucker’s Pitts, the canopy was Jim Leroy’s. I completed the fabrication. The airframe was then sent to George Taylor at Old School Aviation for final fabrication, finish and painting. On 10/15/2011 an Experimental Airworthiness Certificate was issued. The wings were covered when I purchased the project. In 2014, all of the wing fabric was removed, the wings inspected and recovered professionally. There is presently 185hours TT on the aircraft.The engine has ~185hours TT since first major. It had 1940hours TT prior to MOH in this configuration. It is a lycoming IO-540: parallel valve cylinders, heavy crankshaft, impulse coupling Bendix 1200 series Magnetos, complete Christen inverted fuel and oil system including vac pad pickup. 8.5 to 1 pistons were installed at major. It performs flawlessly, oil changed every 10 to 15 hours. After approximately 80 hours TT, a spin on oil filter was installed. It puts out more than 260hp, probably around 300. The Hartzell aerobatic prop has ~185hours SMOH. Oil temp is aprox 180-190 even after sustained aerobatics. Weight & Balance Data Pitts S2S N65AG Total Net Weight ( includes 12 quarts oil, 1 gallon unuseable fuel in main and auxillary tanks) 1145 lbs CG= 86.61 in. Moment= 99157 in-lb
Entry into Service: March 2011, Engines on Rolls-Royce CorporateCare, Forward Crew Rest – 16 Pax Interior, BBML, Direct TV, Enhanced Avionics including CPDLC, FANS-1A, ADS-B Out & TCAS 7.1, Avionics Covered by Honeywell HAPP, One Experienced Gulfstream Owner Since New
Avionics / Equipment
Honeywell’s Primus Epic Integrated Avionics System – Covered by Honeywell HAPP – Gulfstream PlaneView Avionics Certification HotelNAV/COM: TripleVHF: COM TripleMAUs: Modular Avionics Units – TripleDUs: Electronic Display Units Flat-Panel LCD-FourDC: Dual Display Controllers MCDUs: Three Multi-Function Control Display Units CCDs: Dual Cursor Control DevicesCMC: Central Maintenance ComputerADMs: Three Air Data Modules Primary SensorsIRS: Triple Inertial Reference SystemsGPS: Dual Global Positioning SystemsAFGs: Dual Automatic Flight Guidance Functions HUD: Heads Up-Display SystemEVSFADEC: Full Authority Digital Engine Control Dual-Four Channels, while two of the channels are in operational and controlling the engines two more are in standby mode for back upHF: Radio Transceivers DualADF: Receivers DualXPDR: Dual (MODE S) ATC transponders with advanced surveillance capabilities w/ TCASTCAS: Traffic Alert & Collision Avoidance (Change 7.1 incorporated)DME: Dual DME transceivers are co-tuned with the VHF omni-directional receivers (VOR)RADALT: Dual Radio Altimeters are installed to present accurate Above Ground Level (AGL) altitude informationSATCOM: Satellite Communication System A multi-channel Aero H+ satellite communication sys with a digital interface to the AirCell Axxess sys.EGPWS: Two EGPWS computers and controls, with wind shear and terrain avoidance displaysELT: One 406.028 MHz Emergency Locator Transmitter (ELT) also both Life Raft have one each 406 ELTISI: LCD Integrated Standby Instrument and Standby Bearing Distance Instrument (EBDI-4000)CVR/FDRGuidance PanelAuto-throttle SystemTriple audio controls are installed which interconnect the Aircraft communication flight interphone system to allow the pilot and co-pilot two-way voice communication Guidance PanelAvionics Upgrades:Major ASC’s ListASC 49 Lightning Sensor System (LSS)ASC 61A Synthetic Vision-Primary Flight Display (SV-PFD)ASC 71 Micro Quick Access Recorder InstallationASC 84B & C Enhanced NavigationASC 92 Communication Management Function (CMF) – Satcom Direct – Datalink Service ProviderASC 96 CPDLC – FANS 1/AASC 103 TCAS 7.1 InstallationASC 105A Automatic Dependent Surveillance – Broadcast (ADS-B) Out InstallationASC 113A PlaneView Avionics EnhancementASC 911A PlaneView Master Operating System Software Update (Certification Hotel)Equipment:RVSM – B-RNAV (RNP 5) – MNPS – RNP 4 – RNP 10 – P-RNAV – RNAV 1 – (P-RNAV) RNAV 2 – CPDLC/ADS-C – FANS-1A – ADS-B OUT – (DO-260-B) – LVTO – Minimum RVR: 150 meters – L3 QAR (Micro Quick Access Recorder) – EVAS (Emergency Vision Assurance System): Vision Safe Corporation – Three External Camera System: Securaplane 500 – Security System: Securaplane 500. Certified Part 91 – Satellite TV: Honeywell AIS-2000 Multi-Region Coverage Direct TV with four (4) Receivers – Internet: Broadband Multilink (BBML) High Speed Data System – Two (2) Life Rafts w/ 406 ELT – 16 Passenger Vests and four (4) Crew Vests – AirCell Axxess Iridium Satellite – Communication System provides two (2) channels of digital-voice or facsimile w/ six (6) handsets. Also can be used with AeroV app with any smartphone – Analog: Handset-voice – Printer: Multi-Function Machine – Blu-Ray/DVD: two (2) Players – Airshow: 4000 – Galley: One (1) Rockwell Collins 8.4” touchscreen monitor to control the entire cabin with headphone audio jack also has a Secondary Galley Switch Panel – Two (2) MX-3000: Touchscreen Cabin Remote Controllers – Auxiliary: Seven (7) Audio/Video AUX input panels.
Airframe
2,155 TSN – 534 CSNFirst Certificate of Airworthiness Date: October 2010Entry into Service: March 2011Maintenance Tracking: CMP
Interior:16 Pax seats configuration – Six (6) can be configured for sleeping with bedding/mattresses, three (3) singles and two (2) doubles sky loungers seat grouping mattress – Forward galley includes one (1) high temperature oven, one (1) microwave oven, one (1) refrigerator, coffee and espresso/cappuccino maker – Forward crew rest: One single seat – One 7’’ LCD Monitor – Crew lavatory – Main Cabin: Eight (8) executive seats in double club configuration – Four (4) dining tables – Two (2) Forward Cabin 20” LCD TV monitors, eight (8) 7” LCD cabin TV monitors – Mechanical pocket door to aft cabin – Aft Cabin features two (2) fold down divans turns in to sleeping bed with one (1) 20” LCD TV monitor –– Aft executive lavatory with vacuum toilet – Vanity cabinet – Forward lavatory –– One single seat -– Baggage compartment: exterior door access cover – Hinged baggage shelf. Exterior:Matterhorn-white Upper FuselageSlate-Gray Lower FuselageCharcoal Gray Pearl and Gray StripesNew Paint April 2013.
PRICE REDUCTION! Clean, well maintained corporate aircraft always professionally flown. Only 1750 Hours TT! Extremely well equipped PC-12 NG with a fantastic choice of exterior paint color and interior features! Give us a call for a full spec sheet and more details.
Avionics / Equipment
Flight Management System (FMS) Connected Flight DeckCursor Control Device (CCD)StormScope (WX500)Four 10.4” Flat PanelsDual TranspondersDual ADAHRS w/ Air DataCoupled VNAVRVSM Capable TAWS Class B & TCAS IHoneywell ChartLink – Jepp Chart DisplayDual WAAS GPSWAAS LPV Capable
