Grumman · 1941–1955
Grumman G-44 Widgeon

Specifications
Performance
Cruise
120KTAS
Range
800nm
Climb
700fpm
Ceiling
14,600ft
Fuel Burn
23gph
Fuel Cap.
108gal
MPG
6.0mpg
Stall (Vs0)
55KIAS
T/O roll
1100ft
Ldg roll
900ft
Size & weight
Seats
5
Useful Load
1285lbs
Full-fuel payload
637lbs
Max gross
4,525lbs
Wingspan
40ft
Length
31.1ft
Engine
Engine
Ranger L-440-5 (original) / Lycoming GO-480-B1D (Super Widgeon)
Power
400hp
TBO
1,200hrs
Overhaul
$55keach
Engines
2
Owning it
Hull insurance
$10k/yr
Parts
fair
Mechanics
specialist
Gear
Retractable
IFR
Yes
Category
certified
Full specification
V-speeds
Airframe
- Empty weight
- 3,240 lbs
- Max fuel weight
- 648 lbs
- Height
- 11.5 ft
- Wing position
- high
Obstacle performance
- Takeoff over 50 ft
- 1,750 ft
- Landing over 50 ft
- 1,550 ft
Paperwork
- Type certificate
- A-734
- 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
$325k
Range
$180k – $525k
Annual all-in
~$61k/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 (23 gph)
- $14,950
- Engine reserve
- $9,167
- Propeller reserve
- $600
- Maintenance, parts & wear items ($45/hr)
- $4,500
- Insurance
- $8,150–$17,900
- Hangar
- $7,464–$18,660
- Annual inspection (labor only)
- $4,500
- Databases & subscriptions
- $900
- Total per year
- $60,704
- Per flight hour
- $607
- Miles flown / year (at cruise)
- 13,809 mi
- Cost per mile
- $4.40/mi
- Time in the air
- 2 hr 30 min
- Fuel burned
- 58 gal
- Out of pocket
- $730
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
- Amphibious capability opens water and backcountry venues unavailable to wheeled twins
- Rugged, honest design with short takeoff/landing distances on land and water
- Twin-engine safety over remote water; strong community support and parts pool
- Head-turning aesthetic and exceptional fun factor for adventure flying
Weaknesses
- High maintenance costs ($35k–$45k annual + $16k fuel for typical 100-hour year)
- Ranger L-440 engines now obsolete; parts supply dire; most owners convert to GO-480
- Hull corrosion is existential risk—saltwater ops without meticulous care destroy airframe value
- Marginal single-engine performance and poor glide characteristics demand pilot discipline
Overview
The Grumman G-44 Widgeon is a five-place, twin-engine amphibious flying boat designed by Grumman in 1940 as a smaller, more affordable civil companion to the Grumman G-21A Goose. It first flew in 1940 and entered production in 1941. During WWII, the civilian line was diverted to the U.S. Navy (as the J4F-2) and the Coast Guard (J4F-1) for anti-submarine patrol and utility work. Postwar production resumed briefly as the improved G-44A (1944–1949), and the French firm SCAN built a license version (the SCAN 30) using inline engines and later Continental conversions.
A total of 317 Widgeons were built (276 Grumman + 41 SCAN), making it one of the rarer general-aviation twins still flying. The Widgeon earned a reputation as a rugged, honest, strikingly pretty amphibian that can land on fairly short runways or open water, carry five people plus baggage, and cruise faster than many single-engine bush planes. Today it is primarily flown by owner-operators who use it for adventure travel, remote cabin access, and lake country touring — it occupies a niche between single-engine floatplanes and the much larger Goose and Grumman G-73 Mallard.
The vast majority of airworthy Widgeons today have been converted away from the cranky 200 hp inverted-inline Ranger engines to 260–295 hp flat-six Lycoming GO-480 engines under the McKinnon "Super Widgeon" STC or similar conversions (Gannet, Magnum). Unconverted Ranger Widgeons are now uncommon outside of museum-quality restorations.
Variants & History
| Variant | Years | Engines | HP (ea) | Gross Wt | Notes |
|---|---|---|---|---|---|
| G-44 | 1941–1945 | 2× Ranger L-440-5 | 200 | 4,500 lb | Original civil version, 41 built pre-war |
| J4F-1 | 1941–1942 | 2× Ranger L-440-5 | 200 | 4,500 lb | USCG anti-sub/utility, 25 built |
| J4F-2 | 1942–1945 | 2× Ranger L-440-5 | 200 | 4,500 lb | USN utility transport, 131 built |
| Gosling / Widgeon I | 1943 | 2× Ranger L-440-5 | 200 | 4,500 lb | Royal Navy lend-lease, 15 transferred |
| G-44A | 1944–1949 | 2× Ranger L-440-5 | 200 | 4,525 lb | Redesigned deeper hull, better water handling, 76 built |
| SCAN 30 | 1948–1955 | 2× Salmson 8 AS-00 / Mathis | 240 | 4,700 lb | French license-built, 41 built; many later re-engined with Continental IO-470 or Lycoming |
| Super Widgeon (McKinnon STC SA4-576) | 1957–onward | 2× Lycoming GO-480-B1D | 260–270 | 5,500 lb | Most common conversion; 70+ performed |
| Gannet Super Widgeon (PACE) | 1960s | 2× Lycoming GO-480 variants | 295 | 5,500 lb | Higher-HP Texas-built conversion |
| Magnum Widgeon | 1990s–2000s | 2× Lycoming O-540 | 260 | 5,500 lb | Smaller modern conversion; rare |
The G-44A's revised hull profile — deeper V forward, more rise of floor aft — cured the original G-44's tendency to porpoise on takeoff and is considered materially superior on the water. Most Super Widgeon conversions are based on G-44A airframes, though some G-44s have also been converted.
Performance
Book cruise for an unconverted Ranger G-44A is quoted as 133 KIAS at 75% and ~800 nm range on 138 gal, but real-world numbers are softer: owners routinely flight-plan 115–120 KTAS at 20 GPH total to preserve the aging Rangers. The Super Widgeon conversion brings a genuine 135–150 KTAS cruise, 1,750+ fpm climb (vs 700 fpm stock), and service ceiling near 18,000 ft. It also transforms single-engine performance from "barely positive at sea level" (stock Ranger) to a useful 200–300 fpm at light weights.
Water handling is honest but demands training. The hull gets onto the step relatively quickly and runs clean once up, but rough water above 18-inch chop is unwise — the Widgeon is a smaller hull than the Goose and will pound. Takeoff distances on smooth water at sea-level gross run 1,400–1,800 ft to liftoff. Land takeoff ground roll is roughly 1,000–1,200 ft, notably longer than a Baron given the draggy hull and smaller props. Glide is poor — the retracted gear still leaves a boat-shaped fuselage — so engine-out decisions must come quickly.
Density altitude hurts hard. At 6,000 ft DA and gross, even a Super Widgeon becomes a marginal twin; unconverted Rangers are essentially single-pilot-plus-fuel aircraft in mountain country in summer.
Payload & Range
Unconverted Ranger G-44A at 4,525 lb gross:
- Full fuel (108 gal × 6 lb = 648 lb) leaves 637 lb payload — pilot + 2 adults + bags, or pilot + 3 adults with no bags.
- Full cabin (4 adults + pilot + 100 lb bags = 1,000 lb payload) leaves 285 lb of fuel ≈ 47 gal ≈ 2.0 hours + reserve ≈ 230 nm usable.
- Realistic two-person adventure trip: 4 hours at 22 GPH = 88 gal, 528 lb fuel, leaves 757 lb for two occupants + 350 lb gear; range ~460 nm.
Super Widgeon at 5,500 lb gross:
- Full fuel (typically 160 gal long-range tanks × 6 lb = 960 lb) leaves 1,295 lb payload — four adults + 500 lb bags, or five adults with light bags.
- Five-adult mission (1,050 lb payload + 100 lb bags) leaves 1,110 lb of fuel ≈ 185 gal — but max fuel is 160 gal, so full cabin + full fuel is possible. Range with full fuel and full cabin at 140 KTAS and 26 GPH ≈ 820 nm with reserves.
The Super Widgeon conversion fundamentally changes the payload-range story: it is the difference between "two people and a weekend bag" and "family bush vacation with gear" — which is why the conversion is nearly universal in today's flying fleet.
Mission Suitability
- Backcountry / Bush Flying (8) — This is the Widgeon's core mission. Amphibious gear lets it access gravel strips, grass, and water in the same trip. Hull is rugged, takeoff/landing distances are short for a twin, and the cabin swallows camping gear and coolers. Only deducted from a 9/10 because it cannot handle truly rough water or boulder-field beaches the way a floatplane on skis/tundra tires can.
- local_fun (9) — Few aircraft deliver as much head-turning, venue-opening fun. Lake-hopping, island lunches, and cocktail-hour water landings are unmatched.
- cross_country (6) — A converted Super Widgeon cruises at respectable speeds with a 5-place cabin, but fuel burn (24–28 GPH total) and pressurization absence limit true XC utility vs a Baron or 310. Unconverted Ranger versions rate 4/10 here.
- surveying (6) — Good visibility from the high wing and slow minimum maneuvering speeds make it usable for photo and fisheries work; twin safety is a plus over water. Deducted because op costs are high vs purpose-built singles.
- cargo_hauling (4) — Useful load of ~1,300 lb (stock) to ~1,800 lb (Super Widgeon at 5,500 lb gross) is modest for a twin and space is cramped compared to a 206 on floats.
- business_travel (4) — Slower, louder, and more maintenance-intensive than a modern cabin-class twin; only relevant if destinations are waterfront.
- flight_training (2) — Complex, multi, amphibious, high-insurance: not a rational trainer. Only useful as a checkout/transition platform for seaplane-multi ratings.
- aerobatics (1) — No.
Avionics Ecosystem
Widgeon panels span a century of technology. Entry-level unrestored examples may still carry 1960s King radios, a single VOR, and ADF. Mid-market Super Widgeons ($300k–$400k) typically have a Garmin GNS 430W or GTN 650, one or two digital nav/comms, a Century or S-TEC autopilot, and a JPI or EI engine monitor. Top-of-market restorations carry dual GTN 750s, Garmin G500 TXi or dual G3X Touch, GFC 500/600 autopilot, ADS-B In/Out, and synthetic vision. Installation costs run 20–40% higher than a landplane twin because of panel access constraints and the need to route antennas to avoid water immersion of belly equipment. See Avionics Pricing Reference for baseline numbers.
STCs & Modifications
- McKinnon Super Widgeon (STC SA4-576) — Lycoming GO-480-B1D 270 hp conversion, three-blade props, 5,500 lb gross weight increase, larger windows, emergency exit, optional retractable wingtip floats. Most common mod; parts are still supported via the Super Widgeon community. Delta: +30 KTAS cruise, +1,000 fpm climb, +1,000 lb useful.
- Gannet / PACE conversion — Higher-HP GO-480 variant (295 hp) from Texas-based PACE; rare, but offers even stronger climb and single-engine performance.
- Magnum Widgeon (O-540) — Direct-drive Lycoming O-540 conversion retains the gross weight increase without the geared GO-480's overhaul expense. Smoother, cheaper to own long-term but slightly less cruise performance.
- Continental IO-470/IO-520 conversions — Primarily on SCAN 30 airframes in Europe; some U.S. examples exist via field approval.
- Retractable wingtip floats — Reduces cruise drag by ~8 knots; popular addon during avionics/paint refurbishments.
- Hull reinforcement kits — Stainless keel strakes and step doublers extend hull life in rocky-water operations.
Maintenance & Support
See Maintenance Ecosystem. The Widgeon is a specialist airplane. A general A&P can do routine work, but hull and step inspections, gear system maintenance, and engine mount/exhaust work benefit from shops with Grumman amphibian experience (Antilles Seaplanes, Dean Franklin Aviation heritage, and a few individual IA/DARs). Annual inspections typically run $8,000–$15,000 without discrepancies; a "real" annual that opens hull bays can easily exceed $25,000.
Parts availability is "fair" overall: airframe parts are scarce but the owner community (Grumman Widgeon Owners Group) maintains a parts pool and fabrication sources. GO-480 engine parts flow through standard Lycoming channels; Ranger L-440 parts are the single worst supply-chain issue in Widgeon ownership and push most owners eventually to convert. Expected expensive items include propeller overhauls ($8k–$12k each), gear system overhaul, hull bladder replacements, and eventually a corrosion repair project.
Annual cost estimate (insurance + hangar + annual + $10k reserves for engines/hull) for a typical mid-market Super Widgeon flown 80–100 hrs/year: $35,000–$45,000 before fuel. Fuel at 25 GPH × 100 hrs × $6.50/gal = $16,250. All-in direct operating cost roughly $55,000/year.
Valuation Factors
See Aircraft Valuation Methodology for the general framework. Widgeon-specific drivers:
- Engine conversion status drives 40% of value. A Ranger-powered unconverted G-44A in average condition lists $180k–$240k; a mid-time Super Widgeon lists $300k–$400k; a recently-restored Super Widgeon with modern glass lists $450k–$550k.
- Hull condition and corrosion history — A freshwater-only Widgeon commands a 25–40% premium over one with any saltwater time.
- G-44A vs G-44 — The deeper-hull G-44A adds 10–15% over an original G-44 with equivalent panels and engines.
- Time since last major hull inspection/refurbishment — Hull bay opens within last 5 years add significant comfort and value.
- Wingtip floats, retractable floats, paint, interior — Each adds incremental value but is secondary to engines and hull.
- Documentation of STCs — Field-approved mods without clean 337s are a valuation trap.
ADs & Common Problems
The Widgeon fleet has relatively few recurring ADs by FAA standards — the big-ticket items are structural and corrosion, not component-level. Key concerns:
- Hull corrosion — Especially at the keel, chines, step, and bilge frame stations. Saltwater operation without rigorous rinse-down is fatal to airframe value. A proper pre-buy must include hull bay inspection with rivets bucked and bilges pumped dry.
- Wing spar corrosion at the hull-to-wing centersection carry-through. Repairs can exceed $50k.
- Main gear trunnion wear and retraction linkage — unique Grumman mechanical gear is reliable but parts are bespoke.
- Ranger engine availability — OEM parts (cylinders, crankshafts, mag adapters) are essentially NOS or hand-made. Ranger Widgeon owners who want to keep the originals must cultivate relationships with the handful of specialty shops still supporting the L-440; overhaul cost and downtime exceed the Lycoming GO-480 in practice.
- GO-480 gearbox wear — Super Widgeon's geared Lycoming is an expensive engine to overhaul ($55k+ per side) and has a historic reputation for gearbox sensitivity if operated outside of the proper RPM/MP envelope.
- Fuel bladder leaks — Original rubber cells age out; replacement via Eagle or Floats Inc. bladders is a recurring refurbishment item.
- Water rudder and anchor gear — Small but expensive bits that are frequently missing or non-functional on neglected examples.
Insurance Profile
Widgeons fall into a specialist niche (vintage amphibious twin) that only a handful of underwriters will quote — see GA Insurance Underwriting. Typical hull-plus-liability premiums run $7,500–$12,500/year for an owner with 500+ hours TT, multi-engine sea rating, and Widgeon-specific transition training. New owners without sea-multi experience may be denied outright or required to train for 25+ dual hours. Smooth-water operations and inland base airports yield better rates than coastal/saltwater operations. Hull values above $500k push premiums to $14,000+.
Named-insured training requirement is effectively universal — insurance will require dual instruction with a Widgeon-qualified CFI (a short list of instructors nationwide).
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