Hamilton H-47 - Misplaced Pages

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H-45 and H-47

The sole surviving Hamilton H-47 in Northwest Airways markings exhibited at EAA Oshkosh Wisconsin in 2010
Role	Civil passenger and mail carrierType of aircraft
National origin	United States
Manufacturer	Hamilton Metalplane Company
Designer	James McDonnell
First flight	1928
Number built	46

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

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)
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)

References

Joe Christy, LeRoy Cook. American Aviation. p. 110.
^ H-45 & H-47 in aerofiles
Davies, 1998, p.127
Davies, 1998, p.126.
"H-47 Metalplane". Historic Flight. Retrieved 25 April 2020.
Wien Alaska Airways H-45
Davies, 1998, p. 151
Fahey, James C.,US Army Aircraft 1908-1946, 1946. Ships and Aircraft. New York. p.27
UC-89
H-47 at Oshkosh 2010
Aviation March 1931, pp. 180, 183.

Bibliography

"Courrier des Lecteurs" [Readers' Letters]. Avions: Toute l'Aéronautique et son histoire (in French) (103): 5. October 2001. ISSN 1243-8650.
Davies, R.E.G., Airlines of the United States since 1914, reprinted 1998. Smithsonian Institution Press, Washington DC, ISBN 1-888962-08-9.
"Table 2: American Landplane Specifications: Single-Engined Planes With Seats For More Than Three Persons". Aviation. Vol. 30, no. 3. March 1931. pp. 180, 183.

v t e United States military transport aircraft designations, Army/Air Force and Tri-Service systems
Army/Air Force sequence (1925–1962)	C-1 C-2 C-3 C-4 C-5 C-6 C-7 C-8 C-9 C-10 C-11 C-12 C-13 C-14 C-15 C-16 C-17 C-18 C-19 C-20 C-21 C-22 C-23 C-24 C-25 C-26 C-27 C-28 C-29 C-30 C-31 C-32 C-33 C-34 C-35 C-36 C-37 C-38 C-39 C-40 C-41 C-41A C-42 C-43 C-44 C-45 C-46 C-47 C-47F C-47T AC-47 C-48 C-49 C-50 C-51 C-52 C-53 C-54 C-55 C-56 C-57 C-58 C-59 C-60 C-61 C-62 C-63 C-64 C-65 C-66 C-67 C-68 C-69 C-70 C-70B C-71 C-72 C-73 C-74 C-75 C-76 C-77 C-77B–D C-78 C-79 C-80 C-81 C-82 C-83 C-83A C-83B C-84 C-85 C-86 C-87 C-88 C-89 C-90 C-91 C-92 C-93 C-94 C-95 C-96 C-97 KC-97 C-98 C-99 C-100 C-101 C-102 C-103 C-104 C-105 C-106 C-107 C-108 C-109 C-110 C-111 C-112 C-113 C-114 C-115 C-116 C-117 C-117D C-118 C-119 AC-119 C-120 C-121 C-121F EC-121 C-122 C-123 C-123A C-124 C-125 C-126 C-127 C-127 (I) C-127 (II) C-128 C-129 C-130 C-130J AC-130 DC-130 EC-130/H HC-130 KC-130 LC-130 MC-130 WC-130 C-131 NC-131H C-132 C-133 C-134 C-135 KC-135 C-136 C-137 YC-137 (I) YC-137 (II) C-137 C-138 C-139 C-140 C-141 C-142
Tri-service sequence (1962–present)	C-1 C-2 C-3 C-4 C-5 C-6 C-7 C-7 RC-7 C-8 C-9 C-10 C-10 KC-10 C-11 C-12 RC-12 C-13 C-14 C-15 C-16 C-17 C-18 C-19 C-20 C-20A–D C-20F–J C-21 C-22 C-23 C-24 C-25 C-26 C-27 C-27J C-28 C-29 C-30 C-31 C-32 C-33 C-34 C-35 C-36 C-37 C-37B C-38 C-39 C-40 C-41 C-42 C-43 C-44 C-45 C-46
Revived original sequence (2005–present)	C-143 C-144 C-145 C-146 C-147
Non-sequential designations	C-767 C-880
Related designations	CT-39 CT-43 CV-2 CV-7
Not assigned • Assigned to multiple types • Unconfirmed

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