354 documents - page 5 of 18
Report 386 Mean Aerodynamic Calculations, Model 66-70, and Model 66-87 VPJ, January 7, 1940
Report 387 Performance Calculations, Including Justification, Model 66-87 VPJ, Patrol Utility Airplane, January 3, 1940
Report 388 Engine Mount, Stress Analysis, Model 14-9L, December 29, 1939
Report 389 Bonding of Wood With Plastics Bonding Formulae 944-6 and 945-6, November 6, 1939
Report 390 Process Specification For the Use and Application of Plastics Bonding Formulae 944-6, and 945-6, January 4, 1940 [Three Copies]
Report 391 Preliminary Investigation of Wing Beam Construction Using Plastics Bonding Formula Number 944-6, April 30, 1940
Report 392 Flight Test Program, Bellanca Model YO-50, Liaison Observation Airplane, June 18, 1940
Report 394 Seaplane Stress Analysis, Bellanca Model F, Serial Number 805, July 6, 1940
Report 395 Analysis of Flap Control System Components [Model 14-12] July, 18, 1940 [Two Copies]
Report 396 Actual Weight and Balance of Model 14-9L Airplane, Serial Number 1011, August 13, 1940
Report 397 Basic Data, Model T 14-14, August 24, 1940 [Two Copies]
Report 398 Fuselage Analysis, Model T 14-14, October 1, 1940 [Two Copies]
Report 399 Fin, Preliminary Stress Analysis, Martin Model 187 [A-30 Baltimore], August 26, 1940
Report 399-A Stress Analysis of Fin, [Martin] Model 187-B1 [A-30 Baltimore], December 16, 1940 [Martin Report Number 1252 Appendix B]
Report 400 Wing Analysis, Model T 14-14, October 3, 1940
Report 401 Investigation of Overload of 14-9L Model, September 27, 1940 [Two Copies]
Report 402 Landing Gear Stress Analysis, Model T 14-14, October 29, 1940
Report 403 Proposed Static Tests, Model T 14-14, March 10, 1941 This Report is Not Complete
Report 404 Actual Weight and Balance of Model 14-9L Airplane, Serial Number 1011, for 1750 Pound Gross Weight. October 15, 1940 [Two Copies]
Report 405 Actual Weight & Balance, Model 14-9 Airplane (With Flaps) Serial Number 1038, October 26, 1940