Sennheiser SI 234 - ANNEXE 802 Operations Instructions download pdf (Page 331)

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101

DA 42 NG AFM Mass and Balance

Doc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 6 - 17

The flight CG position must be within the following limits:

Most forward flight CG:

2.350 m (92.52 in) aft of datum plane at 1450 kg (3197 lb)'

2.350 m (92.52 in) aft of datum plane at 1468 kg (3236 lb)'

2.418 m (95.20 in) aft of datum plane at max. take-off mass 1900 kg (4189 lb)'

If MÄM 42-678 is carried out:'

2.434 m (95.83 in) aft of datum plane at max. take-off mass 1999 kg (4407 lb)'

linear variation in between

Most rearward flight CG:

2.454 m (96.61 in) aft of datum plane at 1450 kg (3197 lb)

2.480 m (97.64 in) aft of datum plane at 1700 kg (3748 lb)

2.480 m (97.64 in) aft of datum plane at max. take-off mass (see Section 2.7)

linear variation in between

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Sennheiser SI 234 - ANNEXE 802 Operations Instructions Page 331

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