Stelly, Floyd J., Flight Engineer
Person
Biographical
Pan Am Flight Engineer from circa mid-1970 to mid-1990s. AEHS Member and donor.
Found in 37 Collections and/or Records:
"Methods Used in Preparing Engine Specifications" by E.F. Pierce, Wright Aeronautical Corporation, 1939-06-20, 2024-07-03
Item — Box TB.S3.001, Folder: TB.S3.A.001
Identifier: 20060316.07
Scope and Contents
Document Type: Report (Technical).Purpose: Authoritative reference.Authority: Company (Manufacturer).Scope: Commercially printed document prepared by E. F. Pierce (Specification Engineer) for internal use in Wright Aeronautical Corp, as well as for external use by Wright Aeronautical aircraft engine customers.Content: "The engine specification inherently is a compromise as it represents two distinct...
Dates:
Copyright: 1939-06-20; Digitized: 2024-07-03
"Power Control and It's Effect Upon Economy" [by Robert E. Johnson, Chief Field Engineer, Wright Aeronautical Corporation], 1941
Item — Box TB.S6.003, Folder: TF S6.B.035
Identifier: 20141107
Scope and Contents
Document Type: Report (Technical).Purpose: Technical Reference.Authority: Author's Expertise and Company (Manufacturer).Scope: Paper discusses improvements in both procedure and equipment as related to the cruise phase of flight.Content:
From page 1: "During the past few years considerable attention has been given to the study of engine operation, particularly in regard to methods of power control in...
Dates:
Copyright: 1941
"Power Control and Scheduled Performance in Transport Operation" (Wight Aeronautical Service Station Bulletin No. 254 for all Wright Cyclone R-1820-F engines), 1935-07-19
Item — Box TB.S6.003, Folder: TF S6.B.026
Identifier: 20060316.37
Scope and Contents
Document Type: Bulletin (Technical Service).Purpose: Authoritative Reference.Authority: Company (Manufacturer).Document #: Service Station Bulletin No. 254 (Service Division, Wright Aeronautical Corp).Scope: Service Station Bulletiin for the Wright Cyclone R-1820-F (all versions) titled "Power Control and Scheduled Performance in Transport Operation."Contents: From the introduction:...
Dates:
Issued: 1935-07-19
"The Apparent Effect of Pilot Technique and Atmospheic Disturbances upon the Measured Rate of Climb of an Airplane" (CAA Flight Engineering Report No. 17), 1945-05-01, 1945-06-07
Item — Box MC-019-002, Folder: 001.A.043
Identifier: 20060316.05
Dates:
Publication: 1945-05-01; Issued: 1945-06-07
"The Effect of Air Temperature Upon the Rate of Climb of an Airplane Equipped With a Constant Speed Propeller" (CAA Flight Engineering Report No. 12), 1943-12-01, 1943-11-02
Item — Box MC-019-002, Folder: 001.A.043
Identifier: 20060316.03
Dates:
Publication: 1943-12-01; Issued: 1943-11-02
"The Effect of Airplane Weight Upon the Rate of Climb" (CAA Flight Engineering Report No. 10), 1943-09-15, 1943-09-15
Item — Box MC-019-002, Folder: 001.A.043
Identifier: 20060316.02
Dates:
Publication: 1943-09-15; Issued: 1943-09-15
Wright Aircraft Engine Performance Chart (Models 739C18BA1 & 739C18BA2), 1945-11-30, 2024-07-03
Item — Box TB.S3.001, Folder: TB.S3.A.001
Identifier: 20060316.1
Scope and Contents
Document Type: Technical Data (Charts and Tables).Purpose: Authoritative reference.Authority: Company (Manufacturer).Scope: Chart shows engine performance for Wright Model 739C18BA1 and 739C18BA2 aircraft engines at various altitudes.Content: Using these engine charts and known factors, trained flight engineers and pilots can determine true airspeed, aircraft performance, etc. Possibly intended for aircrew of...
Dates:
Issued: 1945-11-30; Digitized: 2024-07-03