William Davis

Document ID: FAA-2008-0750-0002
Document Type: Public Submission
Agency: Federal Aviation Administration
Received Date: October 28 2008, at 07:50 PM Eastern Daylight Time
Date Posted: October 31 2008, at 12:00 AM Eastern Standard Time
Comment Start Date: August 29 2008, at 12:00 AM Eastern Standard Time
Comment Due Date: October 28 2008, at 11:59 PM Eastern Standard Time
Tracking Number: 807820ac
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Regarding the Applicability statement, there were no Dowty Rotol propellers installed on the Convair Model 240, 340 or 440 aircraft. Per TCDS A-793 for the Convair Model 240 - 2 Curtiss-Wright C632S-B/740-6C2-0 or C632S-B/740-9C2-0 propellers or 2 Hamilton Standard 23260/2H17K3-48R, 23260/2H17U3-48R, 23260/2H17AC3-48R or 2H17AA3-48R or 43E60/6895-12 propellers. Per TCDS 6A6 for the Convair Model 340 - 2 Hamilton Standard 43E60-9/6895A-8, 43E60-301/6895B-8, 43E60-325/6895B-8, 43E60-333/6895B-8, 43E60-319/6895D- 8, 43E60-325/6895E-8, 43E60-385/6895E-8, 43E60-333/6895G-8 or 43E60- 387/6895G-8 propellers. Per TCDS 6A6 for the Convair Model 440 - 2 Hamilton Standard 43E60-377/6895E- 8, 43E60-435/6895E-8 or 43E60-469/6895E-8 propellers. Per TCDS 6A6 for the Convair Model 340/440 Military versions - 2 Hamilton Standard 43E60-341/6895B-8, 43E60-501/6895B-8, 43E60-523/6895B-8, 43E60- 539/6895M-8, 43E60-565/6895N-8 propellers. In 1964, the Convair Division of General Dynamics started a turbo prop conversion program for all of the Convair Liner series aircraft - the 240, 340 and 440 - using the Rolls Royce Dart Rda 10 Mark 542 engine with a Dowty Rotol propeller. Originally designated 240D for the Model 240 and 340D and 440D, for the Model 340 and 440 respectively, the designation was later changed to Model 600 (240) or 640 (340/440). Per SA1054WE - 2 Dowty Rotol R.245/4-40-4.5/13 propellers - Model 600 (240). Per SA1096WE - 2 Dowty Rotol R245/4-40-4.5/13 or R259/4-40-4.5/17 propellers - Model 640 (340/440). The Applicability paragraph should be corrected to denote Convair 600 (240 modified per STC SA1054WE) Convair 640 (340/440 modified per STC SA1096WE).

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Total: 1
William Davis
Public Submission    Posted: 10/31/2008     ID: FAA-2008-0750-0002

Oct 28,2008 11:59 PM ET