1965 MOONEY M20E SUPER 21

Description

Detailed Description 1965 Mooney M20E "Super 21" ' C-FCZB ' Modern Garmin Glass Panel Fast, efficient, and fully modernized. This M20E pairs the classic 200 HP fuel-injected Mooney airframe - roughly 160 kt cruise on about 9-10 gph - with a 2023 full Garmin glass panel that would cost tens of thousands to replicate today. What makes this one stand out: -2023 Garmin panel: dual GI 275 EFIS plus GI 275 engine display, GNC 355 WAAS/LPV GPS-COM, GTX 345 ADS-B In/Out, GNC 255A nav/com, GMA 345 Bluetooth audio -Lasar Mooney speed mods -GFC 500 digital autopilot (altitude hold, vertical speed, GPS/NAV coupling, LPV tracking) -Low airframe time: approx. 4,205 hrs TTSN -Fresh annual (Oct 2025) with strong compressions: 75 / 76 / 76 / 79 -Hartzell constant-speed prop overhauled 2020, low time since -BAS inertia-reel shoulder harnesses in both front seats Bonus: brand-new tinted windshields and a one-piece windshield convey with the aircraft (not yet installed - $5,000+ value) ADS-B compliant and IFR-ready - turn-key today Engine: Lycoming IO-360-A1A, 200 HP, approx. 1,228 hrs SMOH. Based at CYRC (Chicoutimi/St-Honoré), Quebec, Canada. Canadian registered. U.S. buyers welcome - export, ferry, and FAA import coordination available through Red Beacon Aeronautical. Asking: $149,000 USD A full 14-page aircraft report with logbook history, avionics list, and photos is available to serious buyers. Message or comment for the report and more pictures. Frederic Roy - Red Beacon Aeronautical ' Aircraft Brokerage, Acquisitions, Ferry Services PERFORMANCE (MOONEY M20E SUPER 21): The figures below are published/typical performance values for the Mooney M20E Super 21 (Lycoming IO-360-A1A, 200 HP, constant-speed propeller). Maximum Speed Approximately 171 KTAS Cruise Speed (75% power) Approximately 163 KTAS Rate of Climb (Sea Level) Approximately 1,110 fpm Service Ceiling Approximately 18,800 ft Stall Speed (dirty) Approximately 50 KIAS Takeoff Ground Roll Approximately 760 ft Landing Ground Roll Approximately 595 ft Fuel Capacity (Usable) Approximately 52 US gal Range Approximately 600 nm Maximum Gross Weight 2,575 lbs Useful Load (this aircraft) Approximately 947 lbs -No damage history was found in the maintenance records reviewed for this report. Two items are worth highlighting for transparency: Weight & Balance: Empty Weight (current) 1,627.6 lbs (re-weighed 4 October 2023, Brantford, ON) Empty CG 44.33 inches aft of datum Datum Nose gear trunnion Maximum Gross Weight 2,575 lbs Useful Load Approx. 947 lbs

Modifications

Engine: Lycoming IO-360-A1A, 200 HP, four-cylinder fuel-injected, serial L-14584-51A, direct drive (spec 1E10). • Overhaul: complete overhaul by Okanagan Aero Engine (Kelowna, BC), inspection release certificate dated 8 February 1985 at 2,202.9 hrs total time since new. • Time since overhaul: approximately 1,228 hrs (1,227.9 hrs recorded at the October 2025 annual), giving an engine total time of roughly 3,430 hrs since new. • Recent maintenance: at the October 2025 annual the engine was serviced with 7 qts Phillips 20W-50; oil filter (P/N AA48110-2) replaced and cut - no contaminants found; spark plugs cleaned, gapped and tested serviceable; engine washed, ground-run and leak-checked with normal operating parameters. A July 2025 entry (Eagle Aircraft) replaced the #4 cylinder lower spark plug and cleaned/reinstalled the #4 fuel injector. • Compressions: October 2025 differential compressions were 75, 76, 76, and 79 (over 80) - healthy and even across all four cylinders. Propeller: Hartzell HC-C2YR-1BF/F7497 two-blade constant-speed, hub serial CH45160B (blades K96384 / K96385). • History: installed new in 2010 under the Hartzell propeller STC (SA02414CH-D / SA01443CH), then overhauled 27 March 2020 by AMO 105-99 under work order E4037. • Current status: low time since the 2020 overhaul, well within the typical Hartzell calendar/hour TBO; propeller lubricated with Aeroshell 6 at the most recent annual

Avionics

The panel was comprehensively modernized in 2023 (Brant Aero, Brantford, ON) around a Garmin GI 275 / GFC 500 architecture, transforming this short-body Mooney into an ADS-B-compliant, LPV-capable IFR platform. The full equipment list: Primary Flight & Engine Displays • Garmin GI 275 ADI/PFD: primary attitude, airspeed, altitude, vertical speed and heading, with Synthetic Vision / Terrain enabled (S/N 5MZ103366). • Garmin GI 275 HSI: horizontal situation indicator with GPS/NAV course guidance and moving-map overlay. • Garmin GI 275 EIS: electronic engine information display (S/N 5MZ102587), with GEA 24 engine adapter, GTP 59 OAT probe and GMU 11 magnetometer. Navigation, Communication & Surveillance • Garmin GNC 355: WAAS GPS/COM with LPV approach capability and ADS-B position source. • Garmin GNC 255A: VHF NAV/COM with ILS/VOR and 8.33 kHz comm spacing. • Garmin GTX 345: ADS-B Out/In transponder (1090ES) with traffic and weather (S/N 3EG041526). • Garmin GMA 345: Bluetooth-capable audio panel with intercom. Autopilot • Garmin GFC 500: digital autopilot with GMC 507 mode controller and GSA 28 roll, pitch and pitch-trim servos - altitude hold, vertical speed, GPS/NAV coupling and LPV approach tracking. Surveillance equipment (GTX 345 transponder, encoder and ADS-B) was bench/integration-tested IAW CAR Standard 571 Appendix F at the time of installation; confirm currency of the recurring transponder/altimeter/ADS-B certification at pre-purchase inspection. C-FCZB's