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PostPosted: Sat Jul 20, 2013 11:09 pm 
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Would like to know how to identify which C-47 and C-47A's were equipped with Ham-Std 23E50-6477A-0 (blade angle 16min/88max) propellers? When were they first installed? From my reading of T.O. 00-25-29, the 6477A-0 blade was used on many aircraft including B-17 and B-24s but this blade angle (16/88) was unique to the C-47(A). Is this true?


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PostPosted: Sat Jul 20, 2013 11:21 pm 
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same prop on the postwar DC3C.


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PostPosted: Thu Jul 25, 2013 4:35 pm 
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Could you tell me which variant of the R4D derives from the C-47 and C-47A?


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PostPosted: Thu Jul 25, 2013 7:29 pm 
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Pete AK wrote:
Could you tell me which variant of the R4D derives from the C-47 and C-47A?


If I understand your question correctly...
C-47 = R4D-1
C-47A = R4D-5 (later C-47H)

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PostPosted: Fri Aug 02, 2013 1:18 pm 
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Yes JohbB, That's exactly what I was looking for...Thanks!

Looks like I struck out on my original request. What series of C-47/C-47A were equipped with the 6477A-0 Hamilton-Standard propeller blade?

Could someone suggest another source for this info? Maybe someone who is really into C-47-DC-3 power plant details?

Pete


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PostPosted: Fri Aug 02, 2013 7:23 pm 
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Here should be all the answers to your questions
C-47 Type certificate
http://rgl.faa.gov/Regulatory_and_Guida ... v%2032.pdf

R-1830 Type certificate
http://rgl.faa.gov/Regulatory_and_Guida ... L/5E-4.pdf

23E series prop
http://rgl.faa.gov/Regulatory_and_Guida ... /p-603.pdf

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PostPosted: Sun Aug 04, 2013 6:20 am 
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almost all had the Ham Stan 23E15 hydromatic ,full swivel prop,governing a range from 1200-2700 rpm.


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