Tecnam P92 Echo MKII - Weights

Page 2- 10
Section 2 - Limitations
WEIGHTS
1
st
Edition - Rev. 0
12. WEIGHTS
Condition
Weight
Maximum take-off weight
600 kg
Maximum landing weight
600 kg
Maximum zero wing fuel weight
600 kg
Maximum baggage weight
20 kg
13. CENTER OF GRAVITY RANGE
Datum
Propeller support flange without spacer
Levelling
Seat track supporting trusses
(ref. to sect.6 for the procedure)
Forward limit
1.841 m (23.0% MAC) aft of datum for all weights
Aft limit
1.939 m (30% MAC) aft of datum for all weights
WARNING
The pilot is responsible for ensuring that the airplane is
properly loaded. Refer to Section 6 for appropriate instruc-
tions.