XtremeAIR XA41, Maintenance Manual, Page: 269 / 284

Mass and Balance XA42
POA Nr. : DE.21G.0227
Form FO P-05 XA42 Issue: Rev.0
Type:
XA42
Prod.-Nr.: Registration: Job-Nr.
Equipment List from: Reason for M&B:
Data according to Airplane Operating Handbook or Type Certificate:
Reference Plane (RP): Firewall
Levelling reference (LR): Firewall vertical
Remaining fuel, comments,
configuration
MTOM in category 999 kg Utility 850 kg Acrobatic
CG Limits for Flight X
front
550 mm X
aft
700 mm
MTOM Utility (kg): 999
Weighing and Empty CG position:
Support point Total (Kg) Tara(Kg) Mass Net (Kg) Moment Arm (m) Mass Moment (mkg)
Tailwheel / /
Mainwheel LH / /
Mainwheel RH / /
Fuel Acrotank
(0,72 kg/l)
(0,285)
Fuel Wingtank
(0,72 kg/l)
(0,340)
Empty mass EM =
Empty mass moment ME
Empty mass CG x
E
M1 * A + M2 * B
XE =
M1 + M2
Variable masses
1. Fuel Acrotank
(0,72 kg/l)
0,285
2. Fuel Wingtanks
(0,72 kg/l)
0,340
3. Front seat 0,780
4. Rear Seat 1,670
5. Baggage 2,225
6. Miscellaneous
Masses and moment arms are to be taken from aircraft documents:
Type certificate, AFM, Equipment List)
Determination of CG for flight {front (x
v
) and aft (x
h
) CG positions}
X
front
Empty mass EM
X
aft
Empty mass EM
Place and Date Stamp Signature CS