Paulic T3B-1 / XT3-B

Paulic XT3-B NX21726

The four-seat Paulic XT3-B NX21726 was originally built in 1939 as a joint project of John W. Thorp and Rudy Paulic. A side-by-side trainer planned for Boeing School of Aeronautics in Oakland, where both Paulic and Thorp worked.

It was dismantled after several test flights and stored until July 1958, when it was redesigned and rebuilt by Paulic as four-place retractable-gear T-3B-1 with a 190hp Lycoming O-435 engine and re-registered NX6497C.

Paulic T-3B-1 NX6497C

XT3-B NX21726
Engine: 125hp Warner Scarab
Wingspan: 33’0″
Length: 23’6″
Useful load: 1060 lb
Max speed: 144 mph
Cruise: 122 mph
Stall: 58 mph
seats: 2

T-3B-1 NX6497C
Engine: 190 hp Lycoming O-435-A
Span: 32 ft 11 in
Length: 22 ft
Wing area: 132 sq.ft
AUW: 2500 lb
Useful load: 1100 lb
Max speed: 170 mph
Cruise: 155 mph
ROC: 1200 fpm
Range: 800 mi
Seats: 4

Paulat Hydro-Aero Monoplane

As Paulat did not succeed in obtaining the required second Hilz engine for his seaplane, he designed the light 1912 Hydro-Aero Monoplane – suited for one Hilz engine – and completed in June 1912 as a landplane. This machine crashed on June 6, 1912.

Paulat was called under arms during the Balkan War (1912-1913), but once returning, decided to end his aeronautical work due to his financial difficulties.

Paulhan-Tatin Aéro Torpille No 1

Powered by a 50 hp Gnôme; the “Torpedo” was designed by Victor Tatin with Luis Paulhan being a sponsor of its 1911 construction.

The Aero-Torpille sported arched wings, a streamlined monocoque fuselage with a Gnome rotary engine buried within, its power delivered to a tail-mounted pusher propeller by a lengthy shaft.

Tatin testing a model with Gustav Eiffel at the right
Testing a model of the Tatin-Paulhan ‘Aéro-Torpille’

Span: 28’3″
Length: 28’3″
Weight: 790 lb empty

Paton Monoswift

For Maurice Paton of Canterbury, New Zealand, his re¬quirements were to design an aircraft that was bigger than a Corby Starlet and about the same size as a Thorp T18, but to be a single seater and meet the micro¬light rules.

With all of these ideas in mind Maurice sat down at his computer and with the help of the C.A.D system he designed his Monoswift over a period of six months. The next step was to build a 3D surface model to prove the concept. Then followed the printing of detailed drawings of all the components at full size. This made the building easier and very accurate because each piece was built directly on top of the drawing.

Western Hemlock is the main type of ma¬terial used in the construction, with fibre¬glass being used for the wing tips and the belly fairings.

The engine option was the water-cooled 3.9-litre Rover V8 using a single, two-inch SU carburettor (instead of fuel injection) and a radiator belly scoop, which direct drives a ground adjustable, 68-inch, three-blade Warp drive propeller via a custom made adapter to the flywheel end of the crankshaft. Fuselage construction is basically a wood and ply box section, with formers for the shape and fibreglass for the non-structural cowlings, wing tips, etc.

The undercarriage is a tailwheel configuration with the main wheels attached to the main spar and folding into the lower fuselage. Engine cooling is via a radiator housed beneath the fuselage. The starting point for the drawings was a Thorp three-view, with a radiator belly scoop and a larger rudder, the undercarriage moved to the wings, a raised rear turtle deck and a reshaped engine cowl. The wing is a single piece and based on the Sirocco (that is, a box spar with no dihedral but given one degree of washout at the tips).

From start to finish the Monoswift took Maurice three years and two months to build.

The aircraft, sn MPS001, was first registered, to M J Paton, Rangiora, New Zealand, on 24 September 2003.

The aircraft was flown by Maurice from his home strip “Barraca” to the Rangiora airfield on 26-10-2003.
Maurice reports it just flies like any other plane with no real surprises. After eight hours he found it to cruise at 130 kts, stalls at 38 kts and uses 25 litres/hr. The manually operated system for the retractable undercarriage works well al¬though there is noticeable drag on the air¬craft when the wheels are going down. He approaches at 55 60 kts over the fence with good forward visibility and finds the air¬craft easy to control on the ground.
The empty weight has come out at 9001bs which allows for 300 Ibs. for fuel and pilot etc. Maurice is using a 3 blade, direct drive, ground adjustable propeller but has found that he is running out of pitch adjustment in flight. So he has purchased a new warp drive in flight adjustable propel¬ler which should see the cruise speed in¬crease to 145 150 kts. The only other mod he is considering is to add a trim tab on the elevator to unload the stick forces when the flaps are fully extended for approach and landing.

Engine: 1 x 3.9-litre Rover V8

Patchen Explorer/Observer

Patchen Explorer N1EX

Only one Patchen Explorer was ever built, in the 1960s, registered N1EX.

By 1982 the prototype was shipped to the Republic of South Africa and evaluated by the SAAF’s test flight and development centre for use as a light recon forward air control aircraft, but was not quite what was required. As a result it languished in a hangar for many years before being donated to the SAAF Museum.

National Dynamics (Pty) Ltd, South Africa, was formed 1975 after acquiring the prototype and all production rights of the Patchen Explorer/Observer four-seat cabin lightplane conceived originally by Thurston Aviation Corporation in the U.S.A., as a landplane development of the Teal amphibian.

Engine: Lycoming, 200hp
Max speed: 130 mph
Cruise speed: 115 mph
Seat: 2

The aircraft is still alive and well, operated by the South African Air Force Museum. Why only one prototype was ever built I do not know, as it is a great little aircraft with a fantastic helicopter-type view from the cockpit. I will admit that it does not have the greatest control harmony (sensitive rudder and elevator, heavy ailerons), but it goes well with a 200hp Lycoming and variable-pitch prop. I served with the SAAF Museum during 1999 as a display pilot and flew the Patchen at many airshows. It looks so weird that it attracts far more interest at airshows than many of the vintage aircraft! (James R Feuilherade 11/15/00)

Pasped Skylark W-1

Based at Glendale, California, Fred Pastorius and Stanley Pederson designed the W-1 Skylark two-seat light cabin monoplane in 1935.

NX14919

A prototype was built (ATC 2-546) NX/NC14919 c/n 1, powered with a 125 hp Warner Scarab engine. The W-1 was equipped with full-panted gear and side-by-side cockpit with optional enclosure. It was later approved for 145-165hp Warners, but only the one was built at a price of $4,485.

NC14919

The prototype survived and was restored to flight circa 2002.

Pasped W-1 NC14919 Restoration at 2002 AirVenture

Engine: Warner Scarab, 125 hp
Wing span: 35’11”
Wing area: 187 sq.ft
Length: 25’0″
Height: 7 ft 11 in
Empty weight: 1288 lb
Loaded weight: 1775 lb
Useful load: 597 lb
Max speed: 139 mph
Cruise sped: 125 mph
Stall: 35 mph
ROC: 850 fpm
Service ceiling: 16.000 ft
Range: 475 mi
Seats: 2

Pasotti F.6 Airone

Designed by Stelio Frati and built by Legnami Passoti, the F.6 Airone is a four-seat low wing twin engine monoplane with dual controls.

A cabin monoplane with two Lycoming engines.

First flown on 13 July 1954, the prototype was powered by two 90 hp Continental C90-12Fs.

Engines: two 90 hp Continental C90-12F
Wingspan: 34 ft 9 in
Wing area: 163.6 sq.ft
Length: 23 ft 9.5 in
Empty weight: 1984 lb
Loaded weight: 3196 lb
Max speed: 198 mph
Cruise: 168 mph
Service ceiling: 21,325 ft
Range: 714 mi