Spencer S-12 Air Car / Republic RC-1 Thunderbolt / OA-15 Seabee / RC-3 Seabee

Percival H. Spencer left Spencer-Larsen in September 1940 and starts the work on his own S-12 Air Car amphibian design. The Spencer Air Car was his 12th design. On 1 March 1941, the first parts are cut for the amphibian Air Car. It was built of steel tube and fabric, featuring an angular cabin with a high wing, a slender low-mounted tail boom, and an engine mounted at the back of the wing / cabin, driving a two-bladed propeller in pusher configuration.

S-12 Air Car

The Spencer S-12 Amphibian Air Car, NX29098, took to the air for the first time on 8 August 1941, from sea on Belmore, Great South Bay, Long Island.

S-12 Air Car NX29098

After the USA is at war, from the Pearl Harbor attack on 7 December 1941, Spence put the Air Car in storage.

Spence accepts a job offer from The Mills Novelty Company, Chicago, IL, which was interested in the potential of the Air Car as a promotional gimmick for their company, in 1943. In April the Air Car was flown from Long Island to Chicago, Illinois. Using the wood-forming facilities at Mills, the Air Car forward cabin or reformed to a rounder ‘egg’-shape.

S-12 Air Car

The Mills Novelty Company was not likely to put the Air Car into production, so Spencer showed it off to his former employers at Republic. By that time, Republic officials were thinking of what the company should be doing when the war came to an end. Expecting private aviation to boom once the fighting stopped, the Air Car plans and manufacturing rights were sold to Republic Aviation Corporation, Farmingdale, New York, in December 1943. Redesign of the Air Car design started in January 1944, to develop an all metal production version. The first development prototype is named Model RC-1 Thunderbolt Amphibian.

Republic RC-1 Thunderbolt

The RC-1 prototype, NX41816, made her first flight from Republic Farmingdale Airport on Long Island, on 30 November 1944. Spence is at the controls.

Republic RC-1 Thunderbolt Amphibian (NX41816)

The Republic Amphibian was presented at the St. Louis Convention in December 1944. A ‘Seabee’ diorama was displayed at the RAC booth at Jefferson Hotel and tentative arrangements are made with the first distributors. Quota commitments made at the convention totals 1972 airplanes at a basic retail price of $3,500. The Republic Aviation Corporation’s Board of Directors approved the plans for RAC’s entry into the personal plane market. Also, in December 1944, NX41816 is demonstrated for the USAAF, US Navy and USCG from National Airport, Washington D.C.

The US Navy officially approved the commercial use of the name “Seabee” for the new Republic amphibian on 19 February 1945.

May 1947 saw Seabee NC6429K (s/n 674) built. It was delivered new by Republic’s pilots and demonstrated by Republic’s pilots for a total of two days to the USAAF as Model YOA-15. The Republic pilots then flew it back to the factory where it was used by the factory as a demonstrator on the east coast the rest of that year and the next.

NC6429K was never assigned a military number or painted any other color than a standard Seabee. Republic sold it to a John Philbrook, who used it in his air charter business, Adirondiacs Airways Maine. John had a second Seabee in the business and was killed in that one. Mr. Herman Mau bought it from the estate and based it at his Florida home, land locked (for a few years) because the water level in the lake it is on is too low to fly it out.

Republic RC-3 Seabee NC6429K (s/n 674)

On 17 April 1945, RAC President Alfred Marched ordered full steam ahead for engineering, tooling and manufacturing divisions, after initial contract is made with US Army for the order of OA-15 Seabees to be used for rescue work in the Far East. The projected military rescue amphibian was to be powered by a geared engine and have a cabin arrangement for 2 litters. The contract is later cancelled, when US Army after V-J Day cancelled orders with RAC for $242,000,000.

Republic RC-3 Seabee

In the wake of massive cutbacks following the end of the war in August 1945, the military orders for the Seabee were cut; it is unclear if the military ever got their hands on any. Work on the civilian Seabee continued, with the prototype of the production RC-3 Seabee, NX87451, rolled off the construction line at Republic Aviation Corporation on 22 November 1945. At 9:17 a.m, 1 December 1945, the first prototype Model RC-3 Seabee, NX87451, makes her first flight, taken to the air by designer and test pilot Percival H. Spencer from Republic Airport, Farmingdale.

Republic RC-3 Seabee

The first standard production Model RC-3 Seabee rolled off production lines at Republic in March 1946. As the production RC-3 Seabee emerged, it was built mostly of metal, with an egg-shaped forward fuselage and a slender tailboom, both riding on a stepped boat hull. It had a high strut-braced wing with fixed floats mounted just outboard of mid-span. It was powered by Franklin 6A8-215-B8F or -B9F air-cooled flat-six piston engine providing 160 kW (215 HP), mounted in pusher configuration at the rear of the cabin, behind the wing. Images of surviving Seabees show them to have a three-bladed variable-pitch propeller, but apparently the RC-3 was originally built with a two-bladed fixed-pitch prop. The fuel tank was in the wing center section.

The Seabee had tailwheel landing gear, all gear with single wheels, the main gear retracting up and back to (not into) the fuselage, the tail wheel hinging up behind the rear of the boat hull. There was a water rudder behind the tail wheel. Flight controls were conventional — ailerons, elevators, rudder, and one-piece flaps. There were seats for four, including the pilot, access being through a front-hinged car-style door on each side of the fuselage.

P. H. Spencer, designer of Republic’s Seabee, smilingly painted the ‘NC’ on the tail of Seabee NC87457 (ex NX87457) to celebrate the CAA certification of the Seabee on 21 July 1946.

The first Seabee, N87463 (s/n 13) is officially delivered to a customer on 25 July, 1946, when handed over to president J. G. (Tex) Rankin, Rankin Aviation Industries, Tulare, California, at Republic.

In 1947 Republic RC-3 Seabee s/n 1019 (NC6731K) was sold from Republic Aviation to a businessman. Official RAC records list says that s/n 1019 was imported to Israel by Aerogypt High Speed Development Company, Palestine, Israel. This businessman donated the Seabee to the new Israel AF for utility flying. The Seabee was initially registered VQ-PAV, but was soon transferred to the Israel AF.

Republic RC-3 Seabee B-61 (s/n 1019) Israel 1948

During the 1980s a Republic Seabee was donated to the Israeli Air Force Museum, Beer Sheva, Israel, by an American businessman, Mr. Robert Hebron. The Seabee, s/n 864 (ex N6564K), was put on display painted as the original Israel AF Seabee.

Republic had hoped to sell 5,000 Seabees a year but the boom in private aviation didn’t really materialize. Republic had also raised the price, with a Seabee going for $6,000 USD in 1946. On the 4th of October 1947 Republic Aviation Corp. announced that the production of the RC-3 Seabee amphibian has been terminated. Last production RC-3 Seabee was N6770K (s/n 1060). The last Seabees were not sold until early 1948.

Republic RC-3 Seabee

The S-12-D Air Car first flew on 25 May 1970.

In 1984 P. H. Spencer planned to resume production of all the metal parts for his S12-E model four-place Amphibian Air Car. He had stopped production early in 1982. In addition to the metal parts, he was contemplating manufacture of hull and empennage parts should a market survey indicate a favorable response.

The Air Car is basically a wooden aircraft, skinned with fiberglass in molded sections for the hull, cabin, engine cowl, wing root fairings, wingtips, floats, etc. Its heart is a single steel tube weldment combining engine mount, wing spar carry-throughs, and lift strut attach points. This section carries all major flight and water loads. Wings are wooden with three-ply skin. Original powerplant was a 260-hp Lycoming, later replaced with the Teledyne Continental Tiara which came in two models, the 6-285-B, C (285 hp) and the 6-320 (320 hp). A Hartzell three-bladed, reversible propeller permits backing up during taxiing to dock.

The S12-E has a span of 37 feet and a length of 26 feet with an empty weight of 2150 pounds and a gross of 3200 pounds. Max speed is 155 mph, cruise 140 mph, landing 55 mph with a 300-hp Continental Tiara engine. Ten were flying in 1984 and 35 are under construction, including one each in Indonesia, New Zealand and Brazil.

All owners pronounce it a rugged, stable and forgiving airplane. It has been flown with six different engines, ranging from 180 to 300 hp.

Gallery

Variation:
STOL Aircraft Twin Bee

S-12 Air Car NX29098
Engine: 110hp Franklin
Wingspan: 33’7″
Length: 23’3″
Useful load: 527 lb
Max speed: 95 mph
Cruise: 86 mph
Stall: 50 mph
Seats: 2
Undercarriage: amphibian

S-12-D Air Car
Engine: 260hp Lycoming O-540-E4B5
Wingspan: 37’4″
Length: 26’0″
Useful load: 1050 lb
Max speed: 147 mph
Cruise: 135 mph
Stall: 53 mph
Range: 600 mi
Seats: 4

S-12-E Air Car N111DA
1970
Engine: 285hp Teledyne Continental Tiara 6-285-B
Max speed: 155 mph
Cruise:135 mph
Stall: 53 mph
Range: 800 mi
Seats: 4

RC-3 Seabee
Engine: 1 x Franklin 6A-215-B8F, 160kW / 215 hp
Wingspan: 11.48 m / 38 ft 8 in
Length: 8.53 m / 28 ft 0 in
Height: 2.92 m / 10 ft 7 in
Wing area: 18.21 sq.m / 196.01 sq ft
Max take-off weight: 1429 kg / 3150 lb
Empty weight: 953 kg / 2101 lb
Max. speed: 193 km/h / 120 mph
Ceiling: 3660 m / 12000 ft
Range: 579 km / 360 miles
Crew: 1
Passengers: 3

Republic RC-3 Seabee
Wingspan: 11.5 m / 37 ft 8 in
Length: 8.5 m / 27 ft 10 in
Height: 3.1 m / 10 ft 1 in
Wing area: 17.8 sq.m / 192 sq.ft
Empty weight: 995 kg / 2,190 lb
MTOW: 1,430 kg / 3,150 lb
Max speed at altitude: 240 kph / 150 mph / 130 kt
Service ceiling: 3,650 m / 12,000 ft
Range: 840 km / 520 mi / 450 nmi

Super Seabee
Engine: Lycoming TIO-540
ROC: 900 fpm
Cruise: 93-100 kt

Spencer Air Car
Engine: Continental IO-520, 300 hp
Speed max: 155 mph
Cruise: 135 mph
Range: 750 sm
Stall: 43 mph
ROC: 1000 fpm
Take-off dist: 700 ft
Landing dist: 500 ft
Service ceiling: 15,000 ft
Fuel cap: 96 USG
Weight empty: 2150 lb
Gross: 3200 lb
Height: 11.8 ft
Length: 26.4 ft
Wing span: 37.3 ft
Wing area: 184 sq.ft
Seats: 4
Landing gear: retractable nose wheel

Spencer Air Car
Engine: 285-hp Continental
Gross Wt. 3200 lb
Empty Wt. 2190 lb
Fuel capacity: 94 USG
Wingspan 37’ 4”
Length 26’ 5”
Top speed147 mph
Cruise 135 mph
Stall 43 mph
Climb rate 1000 fpm
Takeoff time 16 sec
Range 700 sm

Republic RC-3

Spencer S-10 Monoplane

Described by its inventor in Jan 1984, then 87, as “… a little puddle-jumper I made just for fun at Brainerd Field, Hartford CT, in 1922… The fuselage was laid out on the floor with spruce longerons and corner gussets and was fabric covered. The cockpit opening was formed by the wood rim of a bicycle wheel… (The) engine quit and parts began falling (but made a) normal landing. There was a teenager in the assembled crowd and I gave the plane to him. I don’t know if he re-engined it or what became of the plane.”

The S-10 Monoplane was a single-place, open cockpit, low wing monoplane, powered by a 25hp Lawrance La-3, and using wings from a Curtiss Oriole.

Appeared in 1926 as a Spenser with a 35hp Lawrance—possibly the re-rated La-3.
Wing span: 32’0″
Length: 20’0″
Useful load: 220 lb
Max speed: 55 mph
Cruise: 50 mph
Stall: 28 mph

Spencer Curtiss-type

Percival Hopkins “Spence” Spencer convinced his father to invest in the wreckage of a Curtiss F. At age 17 he rebuilt and modified it as flying boat.

On 12 April 1911 he not only took his creation on its first flight but on his own solo flight. Unskilled in turning the plane, he flew for five miles, landed on a river, and pushed it around for the return flight.

Spencer was still actively flying in 1987 at age 90.

Spencer-Stirling 1910 monoplane

A tractor monoplane built by C. G. Spencer and Sons and displayed at the 1910 Aero Show at Olympia. It was designed by Herbert Spencer and W. Stirling, powered by a four-cylinder 40 hp British Aeroplane Syndicate R.H. engine, which drove by chains two propellers of 6 ft. 6 ins. diameter mounted on the leading-edges of the wings. A reverse gear was incorporated in one propeller bracket for opposite rotation. The fuselage was of the “A”-frame type. The machine was tested at Brooklands, but it was not successful and it was soon abandoned.

Spencer Airship

Stanley Spencer, with his brothers, ran a balloon factory at Highbury in North London. In 1902 they built a small 20,000 cu.ft capacity airship constructed along the lines of the Santos-Dumont craft.

The first successful navigable flight in Great Britain of a manned, powered aircraft took place on 22 September 1902, when Stanley Spencer piloting his airship No.1 flew from Crystal Palace via St Pauls to Eastcote Middlesex, a distance of 28 miles, in 94 minutes. It was intended to fly from Crystal Palace, round to St Paul’s and return to the starting point but contrary winds caused the airship to be driven to the north-west.

A Spencer Airship ascending at Ranelagh, watched by a fashionable crowd, 1903

Spencer Airship No.1 1902
Capacity: 20,000 cu.ft
Gross lift: 0.580 ton
Disposable lift: 600 lb
Engine: 1 x JAP water cooled single cylinder, 3 hp
Speed: 20 mph
Crew: 1-2

Spectrum RX-550 Beaver / ASAP Beaver RX 550

RX-550

A rugged, deluxe 2-place trainer and cross country Beaver RX550 has a 10.7 m wingspan, Rotax 503 47 hp engine and weighs 150 kgs. Both aircraft feature fibre¬glass pilot fairing and windscreen as standard equipment.
In 1993, ASAP began providing parts and service for the existing Beaver RX550, RX28 and RX35 all aircraft manufactured by a company no longer operating. The demand to continue offering the Beaver aircraft as a kit was high and so in 1996 ASAP introduced the new Beaver RX 550 Plus with new wings, new tail, stronger shock system, better performance but still keeping with its famous docile easy flight of the original Beaver.
The prototype of the Beaver Plus first flew in 1995.

ASAP Beaver RX 550

The kit price in 1998 was Can$9000.

Beaver
Engine: Rotax 277, 28 hp
Propeller diameter and pitch 50 x 28 inch, 1.27 x 0.71 m
Reduction ratio 2.0/1
Max static thrust 190 lb, 86 kg
Length overall 15. 0 ft, 4.57 m
Height overall 5.8ft, 1.75m
Wing span 33.0ft, 10.06m
Contant chord 5.3ft, 1.63m
Dihedral 2 deg
Sweepback 5 deg
Tailplane span 8.0ft, 2.44m
Fin height 4.8ft, 1.45m
Total wing area 158 sq.ft, 14.7 sq.m
Wing aspect ratio 6.9/1
Wheel track 4.7ft, 1.42m
Nosewheel dia¬meter overall 11 inch, 27cm
Main wheels diameter overall 11 inch, 27cm
Optional floats, dimensions: 10.0 ft, 3.05 m long
Power per unit area 0.18hp/sq.ft, 1.9hp/sq.m
Fuel capacity 2.8 US gal, 2.3 Imp gal, 10.4 litre
Empty weight 232 lb, 105 kg
Max level speed 55 mph, 88 kph
Never exceed speed 62 mph, 100 kph
Max cruising speed 55 mph, 88 kph
Economic cruising speed 30 mph, 48 kph
Stalling speed 24 mph, 39 kph
Max climb rate at sea level 600ft/min, 3.0m/s
Min sink rate 300 ft/min at 30 mph, 1.5 m/s at 48 kph
Best glide ratio with power off 11/1 at 35mph, 56kph
Take off distance 100ft, 30m
Land¬ing distance 125ft, 38m
Service ceiling 13,000ft, 3960m
Range at average cruising speed 40 mile, 64km

RX-550
Engine: Rotax 503
Empty wt: 375 lb
Max wt: 800 lb
Wing span: 35ft
Wing area: 170 sq.ft.
Wing loading: 4.3 lbs/sq.ft
Power loading: 17.4 lbs/hp
Max speed: 80 mph
Cruise: 58 mph
Stall: 30 mph
Vne: 80 mph
Seats: 2

Engine: Rotax 582, 65 hp
Speed max: 80 mph
Cruise: 65 mph
Range: 120 sm
Stall: 38 mph
ROC: 800 fpm
Take-off dist: 400 ft
Landing dist: 450 ft
Service ceiling: 13,000 ft
HP range: 64-75
Fuel cap: 7 USG
Weight empty: 450 lb
Gross: 1100 lbs
Height: 7 ft
Length: 21 ft
Wing span: 35 ft
Wing area: 164 sq.ft
Seats: 2
Landing gear: nose wheel

Beaver Plus
An upgraded version of the RX-550.
Engine: Rotax 582, 65 hp
Engine range: 50-65 hp
Empty wt: 430 lbs
MTOW: 1050 lb
Wingspan: 32 ft
Length: 20.8 ft
Wing area: 154.5 sq.ft
Fuel cap: 10 USG
Cruise: 73 mph
Stall: 37 mph
Range: 230 sm
ROC: 230 fpm
Seats: 2 tandem

ASAP Beaver RX-550 Plus
Engine: Rotax 582, 65 hp
Engine range: 64-75 hp
Empty wt: 450 lb
MTOW: 1050 lb
Wingspan: 35 ft
Length: 21 ft
Wing area: 164 sq.ft
Height: 7 ft
Fuel cap: 9 USG
Max speed: 95 mph
Cruise: 75 mph
Stall: 38 mph
Range: 120 sm
ROC: 800 fpm
TO dist: 400 ft
Ldg dist: 450 ft
Service ceiling: 13,000 ft
Seats: 2 tandem

Engine: Rotax 503, 50 hp
Propeller: 2 or 3 blade Wooden or Composite
Diameter: 68″
Vne: 105 mph
Length: 20 ft 8 in
Height: 6 ft 8 in
Wing Span: 32 ft
Wing Area: 154.5 sqft
Seats: Tandem
Empty Weight: 430 lb
Gross Weight: 1050 lb
Fuel Capacity: 10 USG
Design Load Factors: +4/-2G
Top Level Speed: 75 mph
Cruise Speed: 65 mph
Power Off Stall Speed: 37 mph
Rate of Climb: 900 fpm
Take of Distance: 250 ft.
Service Ceiling: 15,000 ft.

Engine: Rotax 582, 65 hp
Propeller: 2 or 3 blade Wooden or Composite
Diameter: 68″
Length: 20 ft 8 in
Height: 6 ft 8 in
Wing Span: 32 ft
Wing Area: 154.5 sqft
Seats: Tandem
Empty Weight: 430 lb
Gross Weight: 1050 lb
Fuel Capacity: 10 USG
Design Load Factors: +4/-2G
Vne: 105 mph
Top Level Speed: 85 mph
Cruise Speed: 73 mph
Power Off Stall Speed: 37 mph
Rate of Climb: 1050 fpm
Take of Distance: 200 ft.
Service Ceiling: 15, 000 ft.

Spectrum RX-28 Beaver

Beaver SS

Single seat single engined high wing monoplane with conventional three axis control. Wing has swept back leading and trailing edges, and constant chord; conventional tail. Pitch control by elevator on tail; yaw control by fin mounted rudder; roll control by three-quarter span ailerons; control inputs through stick for pitch/roll and pedals for yaw. Wing braced from below by struts; wing profile double surface. Undercarriage has three wheels in tricycle formation; bungee suspension on all wheels. Push right go right nosewheel steering connected to yaw control. No brakes. Aluminium tube framework, with optional pod or full enclosure. Engine mounted at wing height driving pusher propeller.

Since a prototype, the aircraft has been changed considerably. It features almost full span ailerons of 10.0 ft (3.05 m) length, which should give very powerful roll control. Another change has been the inclusion of an optional pod, which can be extended as a further option to become a full cockpit enclosure, rather in the manner of a Birdman Chinook.

Spectrum says that the Beaver takes 30 hr to assemble from kit. Construction is of double surface, strut braced, high wing with aluminium spars and ribs. Stressed to + 7.5 G’s and – 3 G’s. Mylar reinforced leading edge for smooth air flow. Conventional 3-axis controls, centre mounted joy stick, rudder pedals, tricycle undercarriage (with castering nosewheel) and tail skid. Independent shock absorbers give excellent rough field capabilities.

In 1993, ASAP began providing parts and service for the existing Beaver RX550, RX28 and RX35 all aircraft manufactured by a company no longer operating. The demand to continue offering the Beaver aircraft as a kit was high and so in 1996 ASAP introduced the new Beaver RX 550 Plus with new wings, new tail, stronger shock system, better performance but still keeping with its famous docile easy flight of the original Beaver.
The ASAP Single seat Beaver SS standard kit includes: Beaver SS Airframe, Rotax 447 Engine – 40 hp pull-start, Engine accessories, Basic Instrument Package (EGT, CHT, RPM, Airspeed), GSC – 2 blade, 60″ TECH2 prop (ground adjustable, wooden blades w/composite leading edge, Single colour primer and paint package (Endura, 2 part catalyzed polyurethane), Ceconite covering material and edge tape, 3M Latex adhesive, Azusa Tires, nose wheel brakes.

The Beaver SS offers a high useful load with a maximum gross take-off weight of 650 pounds and a typical empty weight of 340 pounds, the Beaver offers more than 300 pounds of useful load. The Beaver SS has a newly designed and cleaner wing, and full span ailerons. Pre-cut, pre-drilled components combined with a modern Assembly Manual (light on cad drawings, heavy on photos) makes for easy assembly even for first time builders.

Cenconite fabric is attached to the structure using a 3M, water-based latex glue before being “shrunk to fit” with a simple home iron. The standard kit includes an educational video to show how. The Beaver kit even includes a high end, catylized polyurethane primer and paint package by Endura incorporating UV protection, flex agent, and instructions. The Standard Beaver SS kit includes everything needed to assemble the aircraft. Everything is jig drilled at the factory with all of the difficult work done.

Complete kit includes airframe, engine, engine accessories, 3 Bld GA prop, paint package, front brake, standard wheels, upright engine mount, instruments steerable nosewheel, ceconite fabric, adapts to floats and skis. Price 2009: US$13150

The Beaver SS first flew in 2000. In 2007 10 were built.

ASAP marketed in kit form the Beaver RX-550 tandem two-seat microlight (as a variant of Spectrum Beaver RX-550), the Beaver RX-28 two-seat training model, and the Chinook Plus 2 tandem two-seat microlight.

Engine: Rotax 277 (268cc) 28 hp
Static thrust: 210 lb
Prop: 127cm x 71 cm pitch
Empty wt: 252 lb
Max wt: 524 lb
Wing span: 31ft
Wing area: 148 sq.ft
Height: 5’8”
Length: 17’8”
Fuel cap: 5 USG
Construction: Aluminium: Dacron
Wing loading: 3.54 lbs/sq.ft
Power loading: 18.71 lbs/hp
Max speed: 72 mph
Cruise: 50 mph
Stall: 24 mph
Vne: 75 mph
Climb rate: 800 fpm @ 50 mph
Design limits: +7.5, -3g
Glide ratio: 8-1
Seats: 1

Beaver SS
Engine: Rotax 447, 40 hp
Engine range: 40-50 hp
Empty wt: 340 lbs
MTOW: 650 lb
Wingspan: 31 ft
Length: 17.6 ft
Wing area: 138 sq.ft
Fuel cap: 5 USG
Cruise: 67 mph
Stall: 30 mph
ROC: 800 fpm
Seats: 1
To dist: 90 ft
Ldg dist: 65 ft
Cockpit width: 39 inch

Aircraft Sales and Parts Ltd (ASAP)
Beaver SS-single place
Stall: 26 kt / 30 mph / 48 kmh
Cruise: 58 kt / 67 mph / 108 kmh
VNE: 78 kt / 90 mph / 145 kmh
Empty Weight: 154 kg / 340 lbs
MTOW Weight: 295 kg / 650 lbs
Climb Ratio: 850 ft/min / 4 m/s
Glide Ratio: 7:1
Take-off distance (50ft obstacle): 90 ft / 27 m
Landing distance (50ft obstacle): 75 ft / 23 m