Hoffman DIMONA H 36 Flight Manual page 42

Hoffmann
H 36 DIMONA
6.1 Empty Weight:
The DIMONA is weighed at the factory after the minimum equipment and extra accessories have been
installed. The weight and the empty weight CG is entered upon the weight report found in Par. 6.3.
Should, at some time the aircraft be repaired, or additional equipment added, the aircraft should be
reweighed to adjust the weight report accordingly. After removing or adding equipment a sample
weight & balance problem should always be performed to insure the CG limits have not been exceeded.
6.2 Reference Datum Line (RDL) and CG Limits:
The reference datum line (RDL) is the leading edge of the wing at the wing root rib. The aircraft
leveling point is the underside of the wing, mid chord.. The CG Limits are measured in mm from the
RDL aft.
Forward CG Limit:
Aft CG Limit
Between 740 and 770 kg linear run between
270 mm
— Up to 740 kg:
— At 770 kg:
385 mm
370 mm
385 and 370 mm.
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6
Weight & Balance
Equipment list
6—2
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