MODEL

STAGGER

GAP

INCIDENCE

DIHEDRAL

 

 

 

Degrees

Degrees

 

 

 

Lower

Upper

Lower

Upper

WACO GXE

10-1/2”

62-1/4”

0

0

0

0

 

 

 

 

 

 

 

WACO ASO

10-1/2”

62-1/4”

0

0

0

0

 

 

 

 

 

 

 

WACO RNF

28-1/2”

54”

0

0

2

2

 

 

 

 

 

 

 

WACO INF

28-1/2”

54”

0

0

2

2

 

 

 

 

 

 

 

WACO QDC

33-5/16”

55-1/2”

0

0

1-3/4

1-3/4

 

 

 

 

 

 

 

WACO QCF

33-1/4”

55-1/2”

0

0

2

2

 

 

 

 

 

 

 

WACO UEC

31-5/16”

5-1/2”

0

0

2-1/2

2-1/2

 

 

 

 

 

 

 

WACO UIC

33-1/2”

53-1/8”

0

0

2-1/2

2-1/2

 

 

 

 

 

 

 

WACO UKC, VKC, VKS

31-5/16”

53-1/16”

0

0

2-1/2

2-1/2

 

 

 

 

 

 

 

WACO YKC, YKS. ZKS

31-5/16”

53-1/16”

0

0

2-1/2

2-1/2

 

 

 

 

 

 

 

WACO YOC***

38-3/8”

49” RS

0

0

2-1/2

2-1/2

 

 

 

 

 

 

 

            Note: RS = Root Section *** ( WACO YOC ) Wing sweepback in degrees, upper and lower = 2-1/2

 

 

 

 

 

 

 

   

Signed by John F. Warlick for E. S. Henley, Acting Director, Office of Aviation Safety

Thanks to member John Barker for submitting this item!

index016002.jpg
Back
index016001.jpg
TOP
RESTORATION TIPS

Many people who restore antique airplanes are faced with one major obstacle when putting their airplane back together... "How is it supposed to be rigged?"  Well friends, here is the suggested answer for at least 15 models of Wacos!  This document is the Aviation Safety Release No. 317 Dated April 7, 1949 as distributed by the CAA.  The subject is:  Rigging Data on Older Type Biplanes and states the following:

 

"Because of the numerous requests for rigging data on the older type biplanes, the following table is presented to assist field personnel in this matter. Only those aircraft of which  there are numerous models still flying are listed. The values given  were taken from manufacturer’s data on file with the CAA. Due to service changes alone in these older aircraft, it is not practical  to assume that all aircraft of a given model can be rigged in accordance with predetermined values and maintain satisfactory flight characteristics. The values shown are therefore presented only as a guide and it may be necessary to vary these values to obtain satisfactory flight characteristics."

 

The dimensions and angles given in the following table are measured from vertical or horizontal lines determined with the airplane in level attitude. Gap is measured between basic chord lines.