FOR SALE MOONEY M2Oe SUPER 21

Transcription

1 FOR SALE MOONEY M2Oe SUPER 21 TTAF: SMOH: (C) (H)

2 OPTIONS AND HIGHLIGHTS Ovation Paint scheme Tan Interior Great Glass Numerous Airframe STC upgrades documented (See Below) Garmin Panel STEC30 Autopilot EI Engine Monitor Zaon PCAS (will include AV8OR Ace and WxWorx XM) Over $60K in upgrades (not including labour) Great documentation and Information and.. MAPA Best in Show Winner This is a beautiful flying and great looking aircraft. I have had it for the last 7 years but do not fly enough to justify the expense (so my wife says!). This aircraft is fast (over 150kt cruise), Economical (10-11 gph), and has a lot of bells and whistles a button pushing pilot would ever want. Following pages highlight upgrade work done on AC in (Note Original Engine Gauges removed and storage box in place) Aircraft also has the following: GAMI injectors HID landing light system EI MVP-50 Engine analyzer STC KR87 ADF Running with Garmin Pilot

3 STC s INSTALLED Under STC SA615EA & SA800EA & type certificate 2A3 Whelen strobe kit part # S was installed. Under STC SA4443NM Lake Aero Styling and Repair Disc brake calipers reversing kit # 103-B was installed. Under STC SA4443NM Lake Aero Styling and Repair Dorsal fin fairings kit # 104 was installed. Under STC SA4443NM Lake Aero Styling and Repair Tail root horizontal fairings kit # 105 was installed. Under STC SA4443NM Lake Aero Styling and Repair Wing Tip Fairings kit # 107 was installed. Under STC SA4443NM Lake Aero Styling and Repair Wing root leading edge fairings kit # 108 was installed. Under STC SA4535NM Lake Aero Styling and Repair Cowl closure fairing kit # 131was installed.. Under PMA # PQ0939SW Plane Plastics Ltd. all interior plane plastics were replaced (see form tracking number 38603) Under PMA # PQ876SW by Nu Lite the following instruments were modified with Part # LW3028: Directional gyro, artificial horizon, airspeed indicator, manifold pressure / fuel pressure, altimeter and vertical speed indicator. ENGINE: Removed firewall forward pressure hoses based on 10-year replacement. Teflon hoses were supplied by Precision Hose Technologies Invoice # Mooney part numbers listed below are for reference for location purposes; One only # SF oil hose from oil cooler to engine. Replacement # 124J002-8CR0500 / SF D50. One only # SF oil hose from engine to oil cooler. Replacement # 124J002-8CR0470 / SF D50. One only # MS oil hose from engine to oil pressure firewall termination fitting. Replacement # 124J001-3CR0190 / MS One only # MS /2 from injector assembly to fuel pressure gauge firewall termination fitting. Replacement # 124J001-3CR0454 / MS One only # MS engine driven fuel pump hose to firewall stand off box. Replacement # 124J001-6CR0254 / LW One only engine driven fuel pump hose to injector assembly. Replacement # 124J001-4CR0172 / LW One only engine driven fuel pump hose to injector assembly. Replacement # 124J001-6CR0170 / MS In doing the above hose replacement, pilot side exhaust and induction tubes were removed and reinstalled. New gaskets were installed. Induction o-ring seal Part # Exhaust to cylinder gasket Part # Replaced missing broken engine induction plenum metal fuel drain line part # c/w connection hose part # from drain pipe to attachment fitting on bottom engine fuselage panel. Installed new slick ignition upgrade kit c/w magnetos LH Part # 4373 Serial # RH Part # 4370 Serial # and harness assemblies LH Part # 2989 and RH Part # Installed new sparkplugs UREM38E Unison sparkplugs. AIRFRAME: Replaced damaged belly panel stiffener doubler part # Riveted aluminum panel behind rear seat with # 6 sheet metal screws. No access required. Riveted aluminum circular panels under rear seat with # 6 sheet metal screws. No access required.

4 Metal skin work being fill antennae holes and adding doublers performed by Commuter & General Aviation Services Ltd. as per Invoice # Chemically stripped complete aircraft of paint. Corrosion protected complete exterior surfaces. Painted aircraft with DuPont aircraft approved paint with 3 coats of clear finish. Balanced all control surface and all were within specified limits in Maintenance Manual. Replaced all exterior access panel fasteners with stainless steel fasteners. WINDOWS: Installed pilot side front window by LP Aero plastics ¼ Plexiglas Part # SG. Supplied by API Invoice # Installed pilot side hinged vent window by LP Aero plastics ¼ Plexiglas Part # SG. Supplied by API Invoice # Installed pilot side rear window by LP Aero plastics ¼ Plexiglas Part # SG. Supplied by API Invoice # Installed co-pilot door window by LP Aero plastics ¼ Plexiglas Part # SG. Supplied by API Invoice # Installed co-pilot rear window by LP Aero plastics ¼ Plexiglas Part # SG. Supplied by API Invoice # Under STC SA4332SW Southwest Texas Aviation Inc. removed and installed new ¼ thick one piece windshield kit serial # 585 INTERIOR: Remove interior plastics, removed and replaced cavity insulation with approved foil back 1 insulation and replace with new painted plastic from Plane Plastics under Invoice # Remove all wall upholstery, removed and replaced cavity insulation with approved foil back 1 insulation and replace with new upholstery supplied by J. Ennis Fabrics with proper flame spread rating specifications FAA requirements Fire Code. Removed all rugs and replaced with new approved rugs from Airtex Products Inc. Part # Invoice # Installed new approved seat belts supplied by Aircraft Spruce under Invoice # , Invoice # and Invoice # INSTRUMENTS removed, rebuilt and/or replaced Removed Rate of Climb indicator manufactured by Garwin Model # G A Serial # B-420 and installed United Instruments Rate of Climb indicator Model # 7000C.31 Serial # Removed Encoding Altimeter by Aero Mechanism Model # 8140-B Serial # 1600 and installed reconditioned United Instruments Altimeter Part # 5934P-3 Serial # Removed Directional Gyro indicator Part # 1U Serial # T50485K and replace with EDO Part # 1U Serial # Work order # by IFR Instruments Ltd. Removed Turn & Bank indicator Part # Serial # 4137 and installed S TEC 30 turn coordinator Part # Serial # D. Removed Artificial Horizon indicator by Sigma Tek Inc. Part # Serial # T71526M for overhaul under work order # by IFR Instruments Ltd. Removed Airspeed indicator by Garwin Part # Serial # Replace with United Instruments Part # 8000 Serial # Work order # by IFR Instruments Ltd. Removed Suction indicator Model # AW 1 7/8-21-W Serial # N-1 AT. Replaced with Varga Enterprises Inc.1 suction gauge Part # 5001 Serial # 14941by Aircraft Spruce. Removed EGT indicator by Aerospace Logic c/w all sending units. Removed Compass original factory unit. Installed Precision Aviation Inc. Vertical card compass Model # PAI-700 Serial # v

5 MISCELLANEOUS: Remove instrument panel shocks and installed new instrument panel shock rubbers Part # from aircraft spruce. Removed pilot instrument panel and replaced with Southwest Texas Aviation standard instrument layout. Removed non essential factory radio cooling grill and scat tube. Swung new vertical card compass supplied by Aircraft Spruce Invoice # as per directions and attached new compass deviation card. Installed new vacuum regulator Tempest air filter by Tempest Model # ARB3-5-1 Part # Installed all new approved Klixon circuit breakers supplied by Aircraft Spruce under Invoice # Removed faulty vacuum gear safety switch and installed new Whitman vacuum gear safety switch Part # VEP Serial # 1145 purchased from Lake Aero Styling & Repair. Installed new tubes and new tires to main and nose gear. Parts supplied by API under Invoice # and # Installed new brake pads. Parts supplied by Goulet Invoice # Installed new wheel bearings on main gear and nose wheel gear. Replaced heavy duty steering arm Part # Southwest Texas Aviation Inc. was installed.. Installed new 3M wing walk. Installed new 2 ½ lb approved A-B-C fire extinguisher and bracket assembly. Mounted unit between pilot and copilot seats. Installed approved new first aid kit in hat shelf area. Aircraft was jacked and weighed: Nose wheel 548 lb., Pilot side main 600 lb., Co- Pilot side main 548 lb. New aircraft empty weight 1735 lb. C of G is now 44.5 inches aft of datum. Maximum allowable gross weight as per factory lb. Aircraft new useful load 840 lb. With full fuel of 336 lb. payload capacity passengers and baggage is 504 lb. 100 hour annual inspection completed as per CAR 625 appendix B part 1 and C, using Mooney check sheet as a guide. Aircraft subject to satisfactory test flight. AVIONICS removed: Removed King KR-86 ADF Part # Serial # Removed Collins ComVHF-251 Part # Serial # Removed Collins Com VHF-251 Part # Serial # Removed Collins Nav VIR-351Part # Serial # Removed Collins Nav VIR-351 Part # Serial # Removed Collins Nav Indicator IND-350A Part # Serial # Removed King KT-76A Transponder Part # Serial # Removed Collins AMR-350 Audio Panel Part # Serial # Removed Collins DME IND-450 indicator Part # Serial # Removed Collins DME TCR-451 Controller and tray Part # Serial # Removed Soft COM 4 place Intercom serial # Removed original cabin speaker.

6 AVIONICS installed equipment installed as per instructions, drawings and tested Installed Garmin GMA-347 AUDIO PANEL Part # Serial # Installed Garmin GNS-430 GPS/WAAS Part # Serial # c/w Data Cards Part # for TAWS/Terrain and IFR. Installed Garmin SL-40 COM Part # Serial # Installed Garmin GTX-327 TRANSPONDER Part # Serial # Installed King KR-87 ADF Part # Serial # 10827c/w indicator serial #. Installed ACK Technologies ALTITUDE ENCODER Model # A-30 Serial # Installed Part # SPEAKER from Aircraft Spruce Installed secondary FRC components transponder antennae Part # AH-3000 Serial # on top of fuselage non-operating, for future 330 Mode S. Installed primary GPS GA-56 ANTENNAE Part # Serial # for Garmin-430 on top of fuselage. Installed secondary GPS GA-56 ANTENNAE Part # Serial # for portable Garmin 296 on top of fuselage. Installed new ACK ELT Part # E-01 Serial # Installed CO Guardian CARBON MONOXIDE DETECTOR Part # Serial # AUTOPILOT equipment installed as per instructions, drawings and tested Under STC SA09309AC-D, S Tec Corporation S TEC 30 Altitude Hold Part # ST A was installed c/w pitch computer Part # Serial # A, pitch servo Part # 0107-P56 Serial # CDEFGJK, transducer Part # 0111 Serial # AA and cable harness Part # HK A. Under STC SA09308AC-D, S Tec Corporation, S TEC 30 Roll Control Kit Part # ST was installed c/w Turn coordinator roll computer Part # Serial # D, roll servo Part # R2 Serial # CEFGJ, cable harness Part # Serial # and cable harness Part # Serial # Under STC SA09308AC-D, S Tec Corporation, S TEC System 30 GPSS Converter Part # ST-901 was installed c/w remote switch Part # Serial # and GPSS remote interface Part # Serial # E/A. MISCELLANEOUS equipment installed as per instructions, drawings and tested Under STC SA615EA & SA800EA & type certificate 2A3 Whelen strobe kit part # S was installed which included power pack assembly Part # A413AHDACF, left wing nav/strobe Part # A650PG14, right wing nav/strobe combo Part # A650PR14 and tail nav/strobe combo. Installation of a COWL CLOSURE FAIRING under STC SA-4535-NM installed in accordance with Lake Aero Styling & Repair drawing list report # 131 dated June 14, Installation of DORSAL FIN FAIRING under STC SA-4443-NM installed in accordance with Lake Aero Styling & Repair drawing list report # 104 dated July 1, Installation of BRAKE ROTATION under STC SA-4443-NM installed in accordance with Lake Aero Styling & Repair drawing list report # 103-B dated June 14, Installation of TAIL ROOT HORIZONTAL FAIRING under STC SA-4443-NM installed in accordance with Lake Aero Styling & Repair drawing list report # 105 dated May 17, Installation of WING ROOT LEADING EDGE FAIRINGS under STC SA-4443-NM installed in accordance with Lake Aero Styling & Repair drawing list report # 108 dated March 1, Installation of WING TIP FAIRINGS under STC SA-4443-NM installed in accordance with Lake Aero Styling & Repair drawing list report # 107 dated July 1, 1997.

7 Installation of 201 style ¼ inch single piece windshield under STC SA-4332-SW installed in accordance with Southwest Texas Aviation Inc. drawing list report # dated February 19, Installation of S-TEC SYSTEM 20/30, Model # ST /30, under STC SA AC- D, according to bulletin # 845, Revision 3, dated June 15, 2000 and master drawing list # , Revision C, dated March 15, 2000 or later. Installation of S-TEC SYSTEM 30 ALT ALTITUDE HOLD system, Model # ST-746, under STC SA AC-D, according to bulletin # 846, Revision 2, dated July 31, 2000 and master drawing list # , Revision B, dated July 31, 2000 or later. Installation of WHELEN ANTI-COLLISION STROBE LIGHT SYSTEM Model # HD, HR, HR-CF-A, or HS as replacement for originally installed anti-collision lights, under STC SA-615-EA when installed in accordance with Whelen installation and service manual dated January 1, 1985 or later. NOW FOR THE FINE PRINT CHECK ALL THE INFORMATION ABOVE BEFORE ASKING ANY QUESTIONS. IT IS QUITE DESCRIPTIVE & EXPLANATORY. PLANE FLIES BEAUTIFULLY. AIRCRAFT IS SOLD WITH NO IMPLIED WARRANTIES. TO THE BEST OF MY KNOWLEDGE ALL AD'S AND SERVICE BULLETINS HAVE BEEN COMPLETED TO THIS DATE. SERIOUS INQUIRIES ONLY AND NO LOGS WILL BE PHOTOCOPIED OR SENT OUT UNLESS AN OFFER IS SUBMITTED. NON REFUNDABLE 5% DEPOSIT BY PAYPAL, BANK DRAFT, CASHIERS CHECK SENT VIA OVERNIGHT COURIER. IF YOU RE LOCAL CASH IS FINE. BALANCE OF FUNDS MUST BE BANK DRAFT, CASHIERS CHECK OR CASH. AIRCRAFT CAN BE DELIVERED FOR THE COST OF FUEL, LODGING, MEALS AND A RETURN FLIGHT IN CANADA ONLY. IF YOU SUBMIT AND OFFER, BUT IF UPON INSPECTION YOU FIND SOMETHING MAJOR (within reason) TO CAUSE A COLLAPSE OF THE SALE, THEN THE DEPOSIT WILL BE RETURNED LESS $ I HAVE NO REASON TO BELIEVE THAT A PROBLEM SHOULD BE FOUND BUT BETTER TO HAVE IT IN THE WIDE OPEN THEN NOT. NO TEST FLIGHTS UNLESS CASH IS IN HAND.

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