Douglas M-1 / M-2 / M-3 / M-4
1925
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Douglas M-1 / M-2 / M-3 / M-4

The US Post Office Department had been responsible for US internal air mail routes from 1918 onwards, and by 1925 the various types of DH-4 biplane which had been primary equipment since inception of the service were worn out. A decision was thus made to order a conversion of the Douglas O-2 observation biplane, which had been ordered into quantity production for the US Army.

The Douglas DAM-1 (Douglas Air Mail-One), quickly shortened to M-1, was test flown during the spring of 1925. It had twice the payload of the DH-4, but made use of the same tried and tested Liberty engine, of which large numbers were in store and readily available. The M-1 was a straightforward conversion of the O-2, with the forward cockpit covered in sheet aluminium to form a reinforced mail compartment with access through two deck hatches, the pilot being located in what was formerly the rear (observer's) cockpit in the O-2. During tests, extended exhaust piping was installed to keep fumes away from the pilot. The M-1 was adjudged successful, but no production order was received by Douglas.

With the introduction of Contract Air Mail (CAM) routes, however, the newly formed Western Air Express Company (later Western Airlines) ordered six Douglas mailplanes. Designated M-2, they differed from the M-1 mainly by replacement of the original tunnel radiator with a frontal type. Provision was also made for quick conversion of the freight section to permit carriage of a passenger in place of mail. A month before Western Air Express inaugurated its Los Angeles-Salt Lake City service in April 1926, the US Post Office ordered 50 of the M-3 version for its major routes. The M-3s differed only in detail from the M-2s, sporting an overall aluminium finish with US Air Mail emblazoned in black on the fuselage sides and on the undersurfaces of the lower wing. Western's machines had a red and silver paint scheme.

The Douglas Company's chief engineer, J. H. 'Dutch' Kindelberger, then redesigned the M-3 with the aim of doubling its payload. The main change in this new M-4 was an entirely new 'stretched' wing which spanned 1.47m more than the 12.09m of the earlier types, and lacked the cut-out in the trailing edge of the upper wing inherited from the US Army O-2s. The Post Office was sufficiently impressed to arrange for 40 of the 50-plane M-3 order to be delivered in M-4 configuration. A single M-4 bought by Western Air Express was designated M-4A by Douglas to differentiate it from the Post Office order. With the leasing of route CAM-3 (Chicago-Dallas) to National Air Transport (NAT) in October 1925, a need arose for more mailplanes. NAT at first used the Curtiss Carrier Pigeon and then, having acquired the important Chicago-New York route, bought at auction all 10 M-3s and eight M-4s from the Post Office when, during July 1926, that department relinquished all its routes to private operators.

The Douglas mailplanes were introduced by NAT on 1 September 1927, and were phased out during 1930 in favour of three-engined Ford tri-motors. In their three years' service they performed admirably in all weathers and in the most difficult flying conditions. NAT had bought other M-4s from a variety of sources and at one stage had as many as 24 Douglas mailplanes in operation. Among them was a privately owned aircraft which had been confiscated by the US Treasury while illegally smuggling . liquor from Cuba to Florida during Prohibition; it became known as the 'Booze Ship'. NAT M-3s were flown with new long-span wings from the spring of 1928 onwards; for economic reasons these had been designed and constructed by the company's own engineering department. One M-4 was converted by NAT to take a 391kW Pratt & Whitney Hornet radial engine.

A total of 57 Douglas mailplanes was built, but with the advent of the Ford and other three-engined types they were soon withdrawn from air mail services. A few were sold to private owners but the majority were scrapped.


Specification 
 MODELM-4
 ENGINE1 x Liberty 12 V-12 piston engine, 298kW
 WEIGHTS
    Take-off weight2223 kg4901 lb
    Loaded weight1544 kg3404 lb
 DIMENSIONS
    Wingspan13.56 m45 ft 6 in
    Length8.81 m29 ft 11 in
    Height3.07 m10 ft 1 in
    Wing area38.18 m2410.97 sq ft
 PERFORMANCE
    Max. speed225 km/h140 mph
    Cruise speed177 km/h110 mph
    Ceiling5030 m16500 ft
    Range1127 km700 miles

Comments
Don Harrington, 30.09.2010

Great site.Well suited for Scale model airplane builders for documented specs.
Also as an aero engineer I have a reference to a lot of airplanes rarely seen or heard about.
Thanks !!

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