# Hamilton H-47

The Hamilton H-45 and H-47 were six-passenger-seat, all-metal, high-wing monoplanes powered by single Pratt & Whitney radial engines. They were built for passenger and mail-carrying work in the US in the late 1920s.

## Design and development

The Hamilton Metalplane Company, which merged with Boeing in 1926, built some of the earliest all-metal US aircraft. The H-45 and the H-47, which differed chiefly in having a more powerful engine, were part of that series.
Both types were corrugated-aluminium-skinned in the Junkers style. The high wings were semi-cantilevers, unsupported apart from pairs of parallel struts from the fuselage bottom edge to the wing close to the fuselage. The main legs of the fixed, tailwheel undercarriage were attached at the same wing points as the struts and joined laterally by inverted V bracing. The fuselage was flat-sided, with wide windows to the passenger cabin under the wing. This was accessed via a portside door, aft of which was a smaller door into a baggage compartment. The two crew members sat in a cabin in front of the wings, accessed by a rooftop hatch. The tail was conventional, with a braced tailplane.
Both the H-45 and the H-47 were powered by a single, uncowled, Pratt & Whitney 9-cylinder radial: the H-45 had a 450 hp (335 kW) Wasp and the H-47 a 525 hp (390 kW) Hornet. The Hornet gave a 10 mph (16 km/h) increase in cruising speed and a slight (3%) increase in useful load to 2300 lb (1043 kg).
Both types first flew in 1928. Both could be mounted on floats. In all, about 25 H-45s and 21 H-47s were built.

## Operational history

The H-45 and H-47 were used from 1928 to operate passenger and mail services within the US. Northwest Airways flew at least nine aircraft, introducing them on their Chicago-Minneapolis/St Paul route CAM 9 from September 1928. Other U.S. airlines to use the type for both passengers and cargo were Coastal Air Freight and Condor Air Lines. Wien Airways of Alaska used at least one H-45 on a route from Fairbanks to the western coast and on to Point Barrow.
During 1930, Isthmian Airways used Hamilton floatplanes for their service linking the Atlantic to the Pacific between respectively Cristóbal, Colón and Balboa in the Panama Canal Zone. The airline impudently claimed the 30-minute flight as the "fastest transcontinental service in North America".
One H-47 (originally built as an H-45) was impressed by the United States Army as a UC-89 in 1942. It was found unsuitable for Army work and was struck off charge in August 1943.
It was a featured aircraft in Howard Hawk's 1939 "Only Angels Have Wings" flying mail for "Barranca". The flying scenes were fake; however, the aircraft was used in ground scenes. The movie prop model (or one of them) survives.

## Variants

H-45 Wasp powered, ~25 built.
H-47 Hornet powered, 20 built.
H-47 Special 525 hp (390 kW) Wright Cyclone powered, span extended to 60 ft 5 in (18.4 m). One built.
UC-89 Single impressed aircraft.

## Surviving aircraft

One H-47 remains flyable. N879H was auctioned after restoration in January 2010 and flew at the Oshkosh meeting in the Summer of 2010.
It is now held in active flight condition for viewing, at the Historic Flight Foundation in Spokane, WA.

## Operators
### United States

* Condor Air Lines
* Alaskan Airways
* Coastal Air Freight
* Isthmian Airways
* Northwest Airways
* Wien Alaska Airways

### Peru

* Peruvian Air Force: operated during Colombia-Peru War

## Specifications (H-47)

Data from American Landplane Specifications aerofiles
General characteristics
* Crew: two
* Capacity: six passengers
* Length: 34 ft 2 in (10.41 m)
* Wingspan: 54 ft 5 in (16.59 m)
* Height: 9 ft 4 in (2.84 m)
* Wing area: 390 sq ft (36 m$^2$)
* Empty weight: 3,699 lb (1,678 kg)
* Gross weight: 5,750 lb (2,608 kg)
* Fuel capacity: 140 US gal (120 imp gal; 530 L)
* Powerplant: 1 × Pratt and Whitney R-1690 Hornet 9-cylinder air cooled radial, 525 hp (391 kW)
Performance
* Maximum speed: 145 mph (233 km/h, 126 kn)
* Cruise speed: 125 mph (201 km/h, 109 kn)
* Stall speed: 55 mph (89 km/h, 48 kn)
* Range: 600 mi (970 km, 520 nmi)
* Service ceiling: 15,000 ft (4,600 m)
* Rate of climb: 900 ft/min (4.6 m/s)