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Curtiss C-46 Commando

The Curtiss C-46 Commando is a twin-engine transport aircraft derived from the Curtiss CW-20 pressurized high-altitude airliner design.

Early press reports used the name “Condor III”, but the Commando name was in use by early 1942 in company publicity. 

It was used as a military transport during World War II by the United States Army Air Forces and also the U.S. Navy/Marine Corps, which called it R5C.

The C-46 served in a similar role to its Douglas-built counterpart, the C-47 Skytrain, but it was not as extensively produced as the latter.

After World War II, a few surplus C-46 aircraft were briefly used in their original role as passenger airliners but the glut of surplus C-47s dominated the marketplace and the C-46 was soon relegated to cargo duty.

The type continued in U.S. Air Force service in a secondary role until 1968.

The C-46 continues in operation as a rugged cargo transport for arctic and remote locations with its service life extended into the 21st century.

Variants

CW-20

Original passenger airliner design.

CW-20T

The original passenger airliner prototype, fitted with a dihedralled tailplane and endplate fins, powered by two 1,700 hp (1,268 kW) Wright R-2600 Twin Cyclone radial piston engines.

CW-20A

Company designation of the C-55.

CW-20B

Company designation of the C-46A.

CW-20B-1

Company designation of the XC-46B.

CW-20B-2

Company designation of the C-46D.

CW-20B-3

Company designation of the C-46E.

CW-20B-4

Company designation of the C-46F.

CW-20B-5

Company designation of the C-46G.

CW-20E

Company designation of the AC-46K.

CW-20G

Company designation of the XC-46C.

CW-20H

Company designation of the XC-46L.

C-55

Modification to the original CW-20T prototype, tail redesigned with a large single tail fin and rudder and an elevator with no dihedral and other improvements, including a change to Pratt & Whitney R-2800-5 radials.

It was used as a C-46 military transport prototype aircraft, also designated XC-46. Later sold to BOAC

C-46 Commando

Twin engined military transport aircraft, powered by two 2,000 hp (1,500 kW) Pratt & Whitney R-2800-43 radial piston engines.

C-46A Commando

Twin-engined military transport aircraft, powered by two 2,000 hp (1,500 kW) Pratt & Whitney R-2800-51 radial piston engines, fitted with a large cargo door on the port side of the fuselage, equipped with strengthened cargo floor, a hydraulic winch and folding seats for up to 40 troops.

TC-46A

Three C-46As converted to crew trainers.

XC-46A

A C-46A used for development tests; converted back to C-46 after tests were completed.

XC-46B Commando

One C-46A was converted into a test aircraft to evaluate a stepped windscreen design, it was powered by two 2,100 hp (1,567 kW) R-2800-34W radial piston engines with water injection.

XC-46C Commando

Redesignated from C-46G, later redesignated XC-113.

C-46D Commando

Twin-engined personnel, paratrooper transport aircraft, fitted with an extra door on the port side; 1,610 built.

TC-46D

15 C-46Ds converted to crew trainers.

C-46E Commando

17 C-46Ds modified with a large single cargo door on the port side of the fuselage, fitted with a stepped windscreen and 2,000 hp R-2800-75 engines with 3-bladed Hamilton Standard propellers.

ZC-46E

Redesignation of C-46Es in 1946.

C-46F Commando

Twin-engined cargo transport aircraft, equipped with single cargo doors on both sides of the fuselage, fitted with square cut wingtips; 234 built.

C-46G Commando

This one-off aircraft was fitted with a stepped windscreen and square wingtips, one built.

C-46H

More powerful version of C-46F, equipped with twin tail wheels, 300 ordered but later cancelled.

One C-46A was modified to C-46H standard after WWII.

C-46J

Planned update for C-46E with stepped windscreen; never ordered.

AC-46K Commando

Unbuilt version, intended to be powered by two 2,500 hp (1865-kW) Wright R-3350-BD radial piston engines.

XC-46K

Conversion project for C-46F with two 2,500 hp Wright R-3350-BD engines.

XC-46L

In 1945 three C-46As were fitted with Wright R-3350 radial piston engines.

XC-113

Engine change: One C-46G, s/n 44-78945, was converted into an engine testbed; the aircraft was fitted with a General Electric T31 turboprop in place of right-hand side R-2800.

The aircraft handled so poorly on the ground that it was never flown.

R5C-1

Twin-engined military transport aircraft for the U.S. Marine Corps. Similar to the C-46A Commando; 160 built.

C-46R

Riddle Airlines, of USA, conversion, with modification kit (mid-1950s) which added 40mph (64kmh) to cruising speed and 2,204 Ib (1,000 kg) to the payload.

Riddle subsequently converted its own fleet of 32 to have 2,100 hp Pratt & Whitney engines.

This conversion was also referred to as the Super 46C.

Specifications

Crew

4 or 5

Capacity

40 troops 

Or

30 stretcher patients 

Or

15,000 lb (6,800 kg) cargo

Length

76 ft 4 in (23.27 m)

Wingspan

108 ft 0 in (32.92 m)

Height

21 ft 9 in (6.63 m)

Wing area

1,360 sq ft (126 m2)

Airfoil

Root

NACA 23017

Tip

NACA 4410.5

Empty weight

30,669 lb (13,911 kg) 

Gross weight

45,000 lb (20,412 kg) 

Powerplant

2 × Pratt & Whitney R-2800-51 Double Wasp 18-cylinder air-cooled radial piston engines,

2,000 hp (1,500 kW) each

Propellers

4-bladed Curtiss Electric constant-speed propellers

Performance

Maximum speed

270 mph (430 km/h, 230 kn) at 15,000 ft (4,600 m)

Cruise speed

173 mph (278 km/h, 150 kn)

Range

3,150 mi (5,070 km, 2,740 nmi) at 173 mph (150 kn; 278 km/h) 

1,000 mi (870 nmi; 1,600 km) at 237 mph (206 kn; 381 km/h)

Service ceiling

24,500 ft (7,500 m)

Time to altitude

10,000 ft (3,000 m) in 17 minutes 24 seconds

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