Taylorcraft · 1946–2008
Taylorcraft BC-12D Twosome
Specifications
MOSAIC eligiblePerformance
Cruise
83KTAS
Range
260nm
Climb
500fpm
Ceiling
12,000ft
Fuel Burn
4.2gph
Fuel Cap.
18gal
MPG
22.7mpg
Stall (Vs0)
30KIAS
T/O roll
500ft
Ldg roll
350ft
Size & weight
Seats
2
Useful Load
450lbs
Full-fuel payload
342lbs
Max gross
1,200lbs
Wingspan
36ft
Length
22ft
Engine
Engine
Continental A-65-8
Power
65hp
TBO
1,800hrs
Overhaul
$16k
Owning it
Hull insurance
$1k/yr
Parts
good
Mechanics
common
Gear
Fixed
IFR
No
Category
certified
Full specification
V-speeds
Airframe
- Empty weight
- 750 lbs
- Max fuel weight
- 108 lbs
- Height
- 6.7 ft
- Wing position
- high
Obstacle performance
- Takeoff over 50 ft
- 900 ft
- Landing over 50 ft
- 750 ft
Paperwork
- Type certificate
- A-696
- Certification basis
- CAR 04
These figures are typical for the model, not a specification for any individual aircraft. Real-world numbers vary with year, installed equipment, weight, modifications and engine condition — often by more than you would expect. Use them to compare types, and confirm anything you would act on against the Pilot's Operating Handbook for that specific airframe and a prebuy inspection.
Pricing
Typical
$28k
Range
$18k – $45k
Annual all-in
~$16k/yr
All-in at ~100 flying hours a year, using the midpoint of each range — the same figures broken out under “Cost to own” below. Your number will differ, and mostly for two reasons. Experience sets your insurance: a 2,000-hour pilot with recent training pays 30–40% less than a 200-hour owner, and student owners pay 20–40% more — on the same aircraft that is often a doubling. Location sets your hangar: a T-hangar runs $200–400 a month in the Midwest against $400–1,500 in a coastal metro, and an outside tie-down is less again. Engine reserves move too — a local shop reusing your serviceable cylinders can come in 30–50% under the national specialty-shop pricing we quote, though you trade the warranty and turnaround that comes with it. Reserves are money set aside toward a future overhaul, not a bill this year, and the annual inspection figure is the shop’s labor to look — whatever they find is separate.
Cost to own — estimate
Set your yearly hours and local fuel price. Fixed costs (insurance, hangar, annual inspection) don't change with hours; fuel, maintenance and the engine reserve do.
- Fuel (4.2 gph)
- $2,730
- Engine reserve
- $889
- Maintenance, parts & wear items ($12/hr)
- $1,200
- Insurance
- $900–$1,800
- Hangar
- $4,752–$11,880
- Annual inspection (labor only)
- $1,200
- Databases & subscriptions
- $400
- Total per year
- $16,085
- Per flight hour
- $161
- Miles flown / year (at cruise)
- 9,551 mi
- Cost per mile
- $1.68/mi
- Time in the air
- 3 hr 37 min
- Fuel burned
- 15 gal
- Out of pocket
- $174
Fuel, engine reserve and wear only. Insurance, hangar and the annual are already paid whether you make the trip or not, so they are not charged here.
Estimate, not a quote. Where a line shows a range, the total, per-hour and per-mile figures use its midpoint— insurance moves most with your experience and time in type, hangar with where you base the aircraft, so your own number could sit at either end. Annual inspection is the shop's labor to open and inspect — what they find is the maintenance line, which covers oil changes, plugs, tires, brakes, hoses, lights, a battery and vacuum pump amortised over their life, and the unscheduled squawks that are the largest and least predictable part of it. Reserves are sinking funds toward an overhaul, not a bill you pay this year — and note that a propeller is due on hours or calendar time, typically six years, so flying less does not put it off forever.
Strengths
- Exceptionally affordable and fun to fly—quintessential $100 hamburger airplane
- Simple, honest stick-and-rudder trainer; excellent for tailwheel endorsements
- Excellent parts support and active community (Univair, ITA, taylorcraft.org)
- Already LSA-compliant; lowest cost-of-ownership in certified GA
Weaknesses
- Tube-and-fabric airframe requires vigilant corrosion inspection and eventual re-cover ($15k–$30k+)
- 65 hp A-65 engine marginal at altitude and in hot/high conditions; density-altitude sensitive
- No electrical system on most examples; limited panel and no radio without retrofit
- Only ~260 nm range and 83 KTAS—fair-weather local flying only
Overview
This page's frontmatter describes the Model BC12-D specifically — Continental A-65-8, 65 hp, 1,200 lb max gross, 18 gal usable fuel, per FAA TCDS A-696 Revision 26, Section IV. The F-19, F-21, F-21A, F-21B and F-22 rows in the Variants table below are NOT covered by A-696 — confirmed against both the FAA's own model list for this certificate and the certificate PDF text directly, neither of which names any F-series model. Those later (1973-2008) Taylorcraft-revival airplanes were certificated separately; their figures below are retained for context but are not backed by the document this page cites.
The Taylorcraft BC-12D is a two-seat, side-by-side, high-wing, tube-and-fabric light airplane designed by C.G. Taylor — the same engineer who created the original Piper J-2 Cub before parting ways with William Piper in 1936. Taylor formed Taylorcraft Aviation in Alliance, Ohio, and the postwar Model B series became one of the archetypal classic lightplanes of American aviation. Over 2,800 BC-12Ds were built between 1946 and 1950, with the vast majority produced during the 1946 postwar boom year before the GA market collapse bankrupted Taylorcraft along with most of its competitors.
Unlike the tandem-seating Piper J-3 Cub, the Taylorcraft B series pioneered side-by-side seating in the ultralight category, offering a more social cockpit and better forward visibility. It competes directly with the Luscombe 8 Silvaire as a lightweight, economical classic two-seater. The company was resurrected multiple times — most notably to produce the F-19 Sportsman (1973-1980, 120 built) with a Continental O-200, and the F-21/F-21A/F-21B (1980-1990s, 43 built) with a Lycoming O-235. A final resurrection attempt ran until roughly 2008 under Taylorcraft Aviation LLC before folding again.
The BC-12D and its successors already met the pre-MOSAIC LSA definition (max gross at or below 1,320 lb for the BC-12D, max stall under 45 kt), making them sport-pilot legal without any weight-reduction gymnastics. Under the MOSAIC (Modernization of Special Airworthiness Certification) rule (effective for pilots October 2025, for aircraft certification July 2026), even the heavier F-19 and F-21 variants remain comfortably sport-pilot eligible. T-Crafts are revered as pure stick-and-rudder machines: light, responsive, honest, and cheap to fly. This page primarily covers the BC-12D; the F-19 and F-21 are treated in the Variants section.
Variants & History
| Variant | Years | Engine | HP | Gross Wt | Notes |
|---|---|---|---|---|---|
| BC-12D | 1946-1950 | Continental A-65-8 | 65 | 1,200 lb | Postwar production standard; ~2,800 built; 18 gal (12 gal header + 6 gal wing aux) |
| BC-12D-85 | late 1940s / field mod | Continental C-85 | 85 | 1,200-1,500 lb (STC dependent) | Common O-200/C-85 upgrade STC for real-world climb |
| F-19 Sportsman | 1973-1980 | Continental O-200 | 100 | 1,500 lb | 120 built; revived by Taylorcraft Inc.; 300 mi range; metalized struts, improved interior |
| F-21 | 1980-1985 | Lycoming O-235-L2C | 118 | 1,500 lb | 43 total F-21 series built; updated type certificate |
| F-21A | mid-1980s | Lycoming O-235 | 118 | 1,500 lb | Minor refinements |
| F-21B | late 1980s-1990s | Lycoming O-235 | 118 | 1,750 lb | Higher gross, 200 lb baggage, firewall battery, skylight option |
| F-22 | 1990s | Lycoming O-235 | 118 | 1,750 lb | Final production variant; few built under multiple resurrection attempts through ~2008 |
Most T-Crafts in the used market today are 1946 BC-12Ds; F-19s and F-21s are uncommon and typically command a premium.
Performance
Only two performance figures are stored in frontmatter, and that reflects a
real gap rather than an oversight. The certificate publishes no performance
at all. AOPA's aircraft guide is the only secondary source found with any
numbers (see raw/press/press-taylorcraft-bc12d-aopa-2026-09-11.md), and most
of its own spec-table rows are blank. Its cruise row states 90-95 mph at 75%
power — midpoint converts to 80 KTAS at 75% power, stored with the
arithmetic in the field comment — but names no fuel burn, so fuel_burn_gph
is not stored. A free period Taylorcraft Foundation "Model B & B12" Service
Manual was checked and ruled out: it never names the BC-12D and has no
performance section regardless (see the same passage). A genuine BC-12D
Flight Manual exists commercially (Essco/PilotMall, part TABC12DF) and would
close this gap if purchased.
No stall speed, climb rate, service ceiling, or runway distance is stored — none is published by either source. Reputation among owners (not a stored figure) is that the airplane is docile at low speed with a gentle, low-drama stall, floats in ground effect on a full-flap-less wing, and is a genuine density-altitude performer at only 65 hp — a hot, high afternoon with two adults aboard is where owners report climb performance getting thin, which is also why the C-85/O-200 upgrade is common. Landing is more demanding than a J-3 because of the side-by-side cockpit's narrower tread and a comparatively brisk approach, but it remains in the "friendly classic tailwheel" category rather than the "squirrely" one.
The F-19 and F-21 improve every practical number: 100-120 mph cruise, 600-800 fpm climb, and meaningful useful load with two adults plus fuel and baggage. The F-21B's 1,750 lb gross with a 118 hp O-235 makes it a genuinely capable two-place cruiser rather than a fair-weather local hopper.
Payload & Range
The BC-12D is payload-limited before it is range-limited. Useful load is 425 lb (AOPA's published 400-450 lb range, midpoint, single-sourced — no certificated empty weight exists to derive it from, see Performance Notes).
- Two 170 lb pilots + full 18 gal fuel (108 lb): 340 lb + 108 lb = 448 lb — over the 425 lb midpoint figure, though within AOPA's own stated 400-450 lb band. Zero to no margin for baggage depending on where in that band the actual airplane sits.
- Two 200 lb pilots + full fuel: 400 + 108 = 508 lb. Over gross either way. Fuel must be reduced to ~10 gal (60 lb) to have any chance of legal weight.
- Solo + full fuel + 40 lb baggage: ~148 lb + 40 = 188 lb, comfortably under useful load either way.
- Two 170 lb pilots + 10 gal fuel: 340 + 60 = 400 lb, within the useful-load band with little to no margin for baggage.
No certificated range figure exists for this page (see Performance Notes), so these scenarios are worked in weight only, not in nautical miles.
The F-19 (1,500 lb gross, 100 hp, still 18 gal) roughly doubles the margin, allowing two adults, reasonable fuel, and real baggage — though its own figures are not backed by TCDS A-696 (see Overview) and are not sourced on this page. The F-21B (1,750 lb gross, 118 hp, 200 lb baggage area) is the only variant that is genuinely a "two adults plus stuff" cross-country airplane, subject to the same caveat.
The honest summary: the BC-12D is a one-adult-or-one-couple fair-weather local airplane. Treat it as such and it is delightful; demand more and it disappoints.
Related: Piper J-3 Cub | Luscombe 8 Silvaire | Piper Vagabond | MOSAIC (Modernization of Special Airworthiness Certification) | Aircraft Valuation Methodology | Avionics Pricing Reference | GA Insurance Underwriting | Maintenance Ecosystem
1980 Cessna 152
Honest Trainer · Mid-Time Engine · Fresh Annual
Mission Suitability
- Local fun flying (9/10): Exactly what this airplane exists for. Low stall, benign handling, panoramic visibility, fuel-sipper economics, nostalgic grin factor. A superb Sunday-morning $100 hamburger airplane and the quintessential "just fly" platform.
- Flight training (6/10): Excellent stick-and-rudder and tailwheel trainer for pilots who want to genuinely learn coordination and energy management. Not suited for primary students targeting PPL/IFR because there's no electrical system on most BC-12Ds, no radio without retrofit, and no modern instrument panel. Outstanding for tailwheel endorsements and LSA transition training.
- Backcountry (5/10): Short-field numbers are respectable and weight is low, but 65 hp is marginal at altitude, the gear is not bush-rated, and tire/prop clearance is modest. F-19/F-21 variants with more horsepower score higher here but still fall well short of a Piper Super Cub or Maule.
- Cross-country (3/10): ~80 KTAS at 75% power (AOPA, single-sourced — no certificated cruise or range figure exists, see Performance Notes), minimal panel, and no electrical system on most airframes makes XC a fair-weather day-trip proposition. F-19/F-21 variants nudge this up to 4/10.
- Surveying (4/10): Slow speed and good visibility are surveying-friendly, but lack of electrical system and single door limit utility for camera mounts and sensor packages.
- Business travel (1/10), Aerobatics (1/10), Cargo (1/10): Not remotely the mission. BC-12D is placarded against intentional spins and is not certified for aerobatics.
Avionics Ecosystem
Most BC-12Ds were delivered without an electrical system — no starter, no battery, no lights, no radio. Hand-propping is normal and expected. Typical panels are airspeed, altimeter, compass, oil pressure, oil temp, tach, and perhaps a slip-skid ball. Period.
Modern owner upgrades tier roughly as:
- Bare-bones vintage ($0 extra): Stock 1946 panel. Handheld com and handheld GPS velcroed to the panel. Sport-pilot friendly.
- Light electrical retrofit ($3,000-$6,000): B&C or Plane-Power small alternator and battery kit, panel-mount com radio (Val, Icom A220), LED position lights. Transponder optional.
- ADS-B compliant ($6,000-$12,000): uAvionix tailBeacon or skyBeacon, Garmin GTR-200 or Val com, portable ADS-B In (Sentry/GDL-50), iPad nav. Enough to operate in Mode C veils and near Class B/C/D without issue.
- F-19/F-21: Most were factory-delivered with electrical systems and basic Narco/King radios; panel refreshes follow the same logic as any 1970s-80s trainer.
Certified avionics pricing details are in Avionics Pricing Reference.
STCs & Modifications
- Continental C-85 / C-90 / O-200 engine upgrade STCs: The most common and most value-added mod. Restores adequate climb, raises gross weight to 1,500 lb on some STCs, and greatly improves density-altitude performance. Install cost varies widely; a running C-85 or O-200 plus STC paperwork and firewall-forward work typically runs $15,000-$30,000 above the cost of an overhaul.
- Metalized lift struts: Univair and others supply sealed or PMA-replacement struts to address the chronic corrosion AD on original vented struts. $2,000-$4,000 per pair plus labor. Essentially mandatory on any BC-12D still running original struts.
- Electrical system retrofit: B&C small alternator and lightweight battery kits are common, enabling radios and lights without giving up too much useful load.
- Cleveland brake conversion: Replaces original heel brakes with toe brakes and modern Cleveland hardware — widely done for better directional control.
- Extended baggage compartment, skylight, door windows: Period owner-preference mods.
- Tundra tires / bush tires: Possible but not transformative on 65 hp.
1989 Aviat Husky
Husky A-1 · Tundra Tires · Backcountry Ready
Maintenance & Support
- Parts availability: good. Univair is the single most important supplier, holding extensive Taylorcraft PMA parts (struts, windshields, fairings, hardware, steel tubing, fabric kits, fuel system components). Wag-Aero, Aircraft Spruce, and the Taylorcraft Foundation also stock or source common items. The International Taylorcraft Association and taylorcraft.org are active communities providing technical support, parts leads, and restoration help.
- Mechanic familiarity: common. Any A&P comfortable with tube-and-fabric classics can work on a BC-12D — this is a simple, forgiving airplane for a competent mechanic. Finding an A&P willing to do the strut AD inspections and re-cover work is the main filter.
- Engine: Continental A-65 parts and overhaul shops (Continental Engine Services, Aircraft Specialties, Poplar Grove, etc.) remain well-supported because the same engine family powers Cubs, Aeronca Champs, Ercoupes, Luscombes, and countless others. Overhaul runs $14,000-$18,000 for a straight-up rebuild; a C-85/O-200 upgrade is a popular alternative when the A-65 is due.
- Annual inspection cost: Typically $800-$1,500 for an owner-assisted annual if the airplane is in good condition; $2,500-$4,000+ if fabric issues, strut work, or tubing repair is uncovered.
- Re-cover cost: $15,000-$30,000 for a full fabric job depending on whether the owner assists and which covering system (Ceconite, Stits/Poly-Fiber, Oratex) is used.
- Annual total cost of ownership (hangared, flown 75-100 hr/yr): Roughly $4,500-$7,000/year including fuel, insurance, annual, reserves for engine/fabric, and tie-down/hangar. This is among the cheapest genuine certified GA airplanes to own.
Valuation Factors
- Price floor (~$18,000-$22,000): Needs-work BC-12Ds with tired fabric, mid-to-high-time A-65, original struts still pending AD compliance, and cosmetic issues.
- Driver-quality ($25,000-$32,000): Good fabric (under 10 years), mid-time A-65, AD-compliant metalized struts, honest logs, basic handheld-friendly panel. This is the market sweet spot.
- Show-quality / low-time BC-12D ($35,000-$45,000): Recent re-cover, low-time engine, fresh paint, original or high-quality restoration.
- BC-12D with C-85/O-200 STC: Add $6,000-$12,000 above equivalent A-65 airframe.
- F-19 Sportsman: Typically $30,000-$55,000 given low production (120 units), electrical system, and O-200 power.
- F-21 / F-21B: Rare (43 total); typically $45,000-$75,000 when they appear on the market, driven by scarcity and the O-235 performance delta.
- Fresh fabric is king. A re-cover done within the last 5-10 years can be worth $15,000+ of the asking price on a classic T-Craft. Tired fabric is the single biggest negative value driver.
See Aircraft Valuation Methodology for engine time and avionics valuation deltas.
ADs & Common Problems
- AD 2007-26-08 / 2008-04-25 (lift strut corrosion): The recurring AD on Taylorcraft A, B, and F series requiring inspection (and often replacement) of front and aft wing lift struts for corrosion and cracks. Multiple in-flight wing separations traced to through-the-thickness internal corrosion of the original vented struts drove this AD. This is the single biggest BC-12D pre-buy item. Replacement with sealed or PMA struts makes the AD a non-issue going forward.
- Wing strut attach fitting corrosion: A documented fatal accident on a BF12-65 involved ~70% corrosion of the wing strut attach fitting on the fuselage, where fabric wrap had plugged the drain hole and trapped water. Inspection of these fittings (and confirmation that the drain path is clear) is a mandatory pre-buy item.
- Header tank cork floats: Original fuel gauge floats in the 12 gal fuselage header tank are cork and deteriorate after a couple of decades. Standard owner fix is dual Ford Model A rubber floats on the welding-rod gauge arm.
- Fabric condition: All BC-12Ds are tube-and-fabric. Re-cover jobs run $15,000-$30,000+. A fresh-fabric airplane is worth substantially more than one approaching re-cover.
- Tube frame corrosion: Steel fuselage tubing corrodes from the inside out, especially at the tailpost and cluster welds. Borescope inspection is essential on any pre-buy.
- A-65 wear items: Tired A-65s with weak compression, oil leaks, and stuck valves are common given the age of the fleet. Assume any mid-time A-65 is closer to overhaul than the logbook implies.
- Wood wing spars (very early airframes): Most BC-12Ds have metal spars, but a small number of very early or oddball variants had wood — confirm the TCDS type on any given airframe.
See Maintenance Ecosystem for general vintage fabric aircraft maintenance patterns.
Insurance Profile
The BC-12D is a benign vintage tailwheel from an underwriting perspective. Insurance is cheap by modern standards: AOPA Insurance Services has quoted as little as $600-$700/year in hull plus liability for experienced tailwheel pilots. Low hull values ($20K-$35K typical) keep premiums genuinely affordable.
Underwriting quirks:
- Tailwheel time required. Expect 5-15 hours of tailwheel dual and the 61.31(i) endorsement before solo coverage is bound. Low-time tailwheel pilots pay noticeably more in the first year and may face open-pilot restrictions.
- Older pilots: Most classic insurers still write the demographic that flies T-Crafts, but pilots 75+ should expect annual medical underwriting and possible CFI-accompanied restrictions.
- Hangar vs tie-down: Fabric airplanes outside are penalized — hangared BC-12Ds get better rates.
- Not-in-motion only coverage is a common budget option for owners who accept ground-loop risk in exchange for liability-only pricing.
See GA Insurance Underwriting for the broader vintage-category framework.
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1946 Taylorcraft BC-12D Twosome
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