San Antonio TX.
USA
Built the Phillips Alouette, or “The Fly”, in 1924 with members of the Air Service at Kelly Field TX.
Author: Terry
Phillips-Fleet 7
The 1942 Phillips-Fleet (ATC 2-562) were Fleet 7 with 120hp Phillips-Martin 333 engines. Two were converted; NC64VA and NC637M.
Phillips CT-2 Skylark
The 1941 Phillips CT-2 Skylark featured an optional sliding cockpit canopy and was priced at $2,500.
Probably only two were built, N19989 c/n 101 and NC19995 s/n 102.
Engine: 120hp Phillips-Martin D-333
Wingspan: 28’3″
Length: 23’3″
Useful load: 570 lb
Max speed: 124 mph
Cruise: 115 mph
Stall: 45 mph
Range: 315 mi
Seats: 2
Phillips CT-1
In 1940 Phillips Aviation Co built the CT-1 two-seat biplane (ATC 731) designed by Ivan Driggs. A continuation of the Driggs Skylark, offered with a 95hp Menasco B-4 engine or optional 125hp C-4 and sliding cockpit canopy.
Two or three were built, the prototype being NX18989 c/n 100, and one went to Peru.
CT-1 Skylark
Engine 95hp Menasco B-4
Wingspan: 28’3″
Length: 23’2″
Useful load: 586 lb
Max speed: 114 mph
Cruise: 100 mph
Stall: 45 mph
Range: 340 mi
Seats: 2
Phillips 1-B Aeroneer / XPT
Phillips Aviation Co was founded at end of 1930s in Los Angeles, California, to continue development of light two-seat monoplane, the 1936 Phillips I-B (ATC 693), designed originally by Aero Engineering Corporation.
The one built, NC16075, was rebuilt in 1939 with a 145hp Ranger 6 engine as XPT (Experimental Primary Trainer) in an attempt to get an USAAC contract.
This failed, then MGM Studios reportedly bought it, as it has appeared in several films.
In 2005 it was stored in a hangar in Arizona. FAA says registered owner is, or was, in Oklahoma City but “sale reported” (2007).
1-B Aeroneer
Engine: 125hp Menasco C-4
Wingspan: 32’6″
Length: 24’0″
Useful load: 695 lb
Max speed: 140 mph
Cruise: 130 mph
Stall: 49 mph
Range: 600 mi
Seats: 2
XPT
Engine: 145hp Ranger 6
Wingspan: 32’6″
Length: 23’6″
Useful load: 810 lb
Max speed: 150 mph
Cruise: 130 mph
Stall: 46
Range: 500 mi
Seats: 2
Phillips Aviation Co.
1936: (James A) Phillips Aviation Co
South Pasadena & Van Nuys CA.
USA
Phillips Aviation Co was founded from Western Airmotive Corp in 1940 in Los Angeles, California, to continue development of light two-seat monoplane, the Phillips I-B, designed originally by Aero Engineering Corporation.
1940: Acquired rights from Aero Engineering Corp and Driggs (Western Airmotive), Long Beach CA.
Also built CT-1 two-seat biplane.
1941: Rights to Skylark and D-333 motor sold to Ayers Aviation Corp, Reno NV.
Phillips ST-1 Speedtwin
A fully aerobatic light twin, first flown in 1991. Partial and or prefabricated parts were available.
Mk.I
Engine: 2 x Continental O-200, 100 hp
Mk.II
Speed max: 220 mph
Cruise: 200 mph
Range: 1300 sm
Stall: 60 mph
ROC: 3500 fpm
Take-off dist: 600 ft
Landing dist: 600 ft
Service ceiling: 25,000 ft
Engines: 2 x Lycoming IO-320, 160 hp
Fuel cap: 96 USG
Weight empty: 1500 lb
Gross: 2250 lb
Height: 6.83 ft
Length: 22.83 ft
Wing span: 26 ft
Wing area: 120 sq.ft
Seats: 2
Landing gear: tail wheel
Philippine Aircraft Company Inc
Constructed a version of Denny Kitfox as Skyfox for marketing in Western Pacific region.
Philippine Air Force XT-001 Marko 1
The PAF XT-001 Marko 1 was a basic trainer aircraft developed by the Philippine Air Force Self-Reliance Development Wing (PAFSRDW). It was designed and built by the Self-Reliance Development Wing of the Philippine Air Force in 1975 from locally designed jigs and fixtures.
It closely resembles the SIAI-Marchetti SF.260MP trainer, but with modified wingtips and cockpit. The prototype was initially thought to be a modified SF.260MP. Comparison of data with those for the SF.260MP indicates a slight increase in wingspan (though not in gross wing area), a lower empty weight, and (despite a similar powerplant and identical maximum takeoff weight) a slightly reduced performance.
The first test flight was on May 21, 1975.
XT-001 Marko
Engine: 1 × Lycoming O-540-E4A5, 194 kW (260 hp)
Propeller: 2-bladed
Wingspan: 8.4 m (27 ft 7 in)
Height: 2.4 m (7 ft 10 in)
Wing area: 10.10 m2 (108.7 sq ft)
Length: 7.1 m (23 ft 4 in)
Empty weight: 720 kg (1,587 lb)
Max takeoff weight: 1,200 kg (2,646 lb)
Maximum speed: 260 km/h (160 mph, 140 kn)
Stall speed: 120 km/h (75 mph, 65 kn)
Seats: 3
Philippine Air Force
Self Reliance Development Wing built prototype of Lycoming powered three-seat primary trainer, the XT-001. Very similar to the Italian SIAI SF.260, of which 32 were bought for the PAR The SRDW also acquired the prototype of American Jet Industries’ Super Pinto COIN aircraft.
