Operating Limitations
DA 42 AFM
Page 2 - 18
Rev. 8
15-Dec-2017
EASA
approved
Doc. No. 7.01.05-E
2.8
CENTER OF GRAVITY
Datum Plane
The Datum Plane (DP) is a plane which is normal to the airplane’s longitudinal axis and
in front of the airplane as seen from the direction of flight. The airplane
*
s longitudinal axis
is parallel with the floor of the nose baggage compartment. When the floor of the nose
baggage compartment is aligned horizontally, the Datum Plane is vertical. The Datum
Plane is located 2.196 meters (86.46 in) forward of the most forward point of the root rib
on the stub wing (refer to figure in Section 6.2).
Center of Gravity Limitations
The center of gravity (CG position) for flight conditions must be between the following
limits:
Most forward flight CG:
2.35 m (92.52 in) aft of Datum Plane at 1250 kg (2756 lb)
2.35 m (92.52 in) aft of Datum Plane at 1468 kg (3236 lb)
2.40 m (94.49 in) aft of Datum Plane at max. take-off mass (see Section 2.7)
linear variation in between
Most rearward flight CG:
2.42 m (95.28 in) aft of Datum Plane at 1250 kg (2756 lb)
2.49 m (98.03 in) aft of Datum Plane at 1600 kg (3527 lb)
2.49 m (98.03 in) aft of Datum Plane at max. take-off mass (see Section 2.7)
linear variation in between
Refer to Section 6.4.4 for a graphical illustration of the CG limitations.
WARNING
Exceeding the center of gravity limitations reduces the
controllability and stability of the airplane.
Summary of Contents for DA 42
Page 1: ......
Page 20: ...Introduction DA 42 AFM Page 0 18 Rev 8 15 Dec 2017 Doc No 7 01 05 E Intentionally left blank ...
Page 46: ...General DA 42 AFM Page 1 26 Rev 8 15 Dec 2017 Doc No 7 01 05 E Intentionally left blank ...
Page 236: ...Performance DA 42 AFM Page 5 4 Rev 8 15 Dec 2017 Doc No 7 01 05 E ...
Page 237: ...DA 42 AFM Performance Doc No 7 01 05 E Rev 8 15 Dec 2017 Page 5 5 ...
Page 247: ...DA 42 AFM Performance Doc No 7 01 05 E Rev 8 15 Dec 2017 Page 5 15 ...
Page 251: ...DA 42 AFM Performance Doc No 7 01 05 E Rev 8 15 Dec 2017 Page 5 19 ...
Page 257: ...DA 42 AFM Performance Doc No 7 01 05 E Rev 8 15 Dec 2017 Page 5 25 ...
Page 268: ...Performance DA 42 AFM Page 5 36 Rev 8 15 Dec 2017 Doc No 7 01 05 E Intentionally left blank ...
Page 277: ...DA 42 AFM Mass and Balance Doc No 7 01 05 E Rev 8 15 Dec 2017 Page 6 9 6 4 2 LOADING DIAGRAM ...
Page 390: ...Handling Care Maintenance DA 42 AFM Page 8 12 Rev 8 15 Dec 2017 Doc No 7 01 05 E ...