Wing failures
Heinrich Gontermann's crashed
Dr.I (serial 115/17)
On 29 October 1917,
Leutnant der Reserve Heinrich Gontermann,
Staffelführer of
Jasta 15, was performing aerobatics when his triplane broke up.
[20] Gontermann was fatally injured in the ensuing crash landing.
Leutnant der Reserve Günther Pastor of
Jasta 11 was killed two days later when his triplane broke up in level flight.
[20] Inspection of the wrecked aircraft showed that the wings had been poorly constructed. Examination of other high-time triplanes confirmed these findings. On 2 November,
Idflieg grounded all remaining triplanes pending an inquiry.
Idflieg convened a
Sturzkommission (crash commission) which concluded that poor construction and lack of waterproofing had allowed moisture to damage the wing structure.
[21] This caused the
wing ribs to disintegrate and the ailerons to break away in flight.
[21]
In response to the crash investigation, Fokker improved quality control on the production line, particularly varnishing of the
wing spars and ribs, to combat moisture. Fokker also strengthened the rib structures and the attachment of the auxiliary spars to the ribs.
[22] Existing triplanes were repaired and modified at Fokker's expense.
[23] After testing a modified wing at Adlershof,
Idflieg authorized the triplane's return to service on 28 November 1917.
[24] Production resumed in early December. By January 1918,
Jastas 6 and 11 were fully equipped with the triplane. Only 14 squadrons used the Dr.I as their primary equipment. Most of these units were part of
Jagdgeschwadern I, II, or III.
[25] Frontline inventory peaked in late April 1918, with 171 aircraft in service on the Western Front.
[11]
Despite corrective measures, the Dr.I continued to suffer from wing failures. On 3 February 1918,
Leutnant Hans Joachim Wolff of
Jasta 11 successfully landed after suffering a failure of the upper wing leading edge and ribs.
[26] On 18 March 1918,
Lothar von Richthofen,
Staffelführer of
Jasta 11, suffered a failure of the upper wing leading edge during combat with
Sopwith Camels of No. 73 Squadron and
Bristol F.2Bs of No. 62 Squadron.
[27] Richthofen was seriously injured in the ensuing crash landing.
Postwar research revealed that poor workmanship was not the only cause of the triplane's structural failures. In 1929,
National Advisory Committee for Aeronautics (NACA) investigations found that the upper wing carried a higher lift coefficient than the lower wing — at high speeds it could be 2.55 times as much.
The triplane's chronic structural problems destroyed any prospect of large-scale orders.
[28] Production eventually ended in May 1918, by which time only 320 had been manufactured.
[29] The Dr.I was withdrawn from frontline service as the
Fokker D.VII entered widespread service in June and July.
Jasta 19 was the last squadron to be fully equipped with the Dr.I.
[30]
Surviving triplanes were distributed to training and home defense units. Several training aircraft were reengined with the 75 kW (100 hp) Goebel Goe.II.
[31] At the time of the
Armistice, many remaining triplanes were assigned to fighter training schools at
Nivelles, Belgium, and
Valenciennes, France.
[32] Allied pilots tested several of these triplanes and found their handling qualities to be impressive.
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