SZD-55-1 FLIGHT MANUAL Page 2c

Appendix No. B4 to Service Bulletin No. BE-012/55-1/2012

ISS. IV Rev. 3

0 . L I S T O F R E V I S I O N S

The place where the text has been revised has been marked with a vertical line on the right side of the text and an appropriate number of revision.

No of rev.

Page Revision Date Signature

1. Pages : 2, 10, 11, 38, 42, 43, have been replaced as appropriate with pages 2a, 10a, 11a, 38a, 42a, 43a

07.04.1994 T.Łabu ć

2. Pages : 2a, 10a, 11a, 12, 25, 39 have been replaced with pages 2b, 10b, 11b, 12a, 25a, 39a

25.05.1995 T.Łabu ć

3. Pages : 2b, 15, have been replaced with pages 2c, 15a

18.05.2012 Marian Kroczek

SZD-55-1 FLIGHT MANUAL Page 15a

Appendix No. B4 to Service Bulletin No. BE-012/55-1/2012

ISS. IV Rev. 3

Fig. 3 MASS DISTRIBUTION

The glider in attitude for weighing acc. to Technic al Service Manual, item 2.8. (page 20).

The distance in respect to the base (leading edge o f the root rib) in measured in cm {in}.

NOTE – ON THE DRAWING THE MASSES OF THE BATTERY IN THE FIN CONTAINER AND PERMANENT EXTRA BALLAST HAVE BEEN OMITTED. THESE MASSES ARE AN OBLIGATORY ITEMS OF TH E EQUIPMENT AND HAVE BEEN CALCULATED INTO GLIDER’S EMPTY WEIGHT mM

THE BATTERY MASS (OR SUBSTITUTIVE ONE) IS 2,2 kg (4,85 lb). BATTERY WEIGHT ARM IS 438.5 cm

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