Sennheiser SI 234 - ANNEXE 802 Operations Instructions download pdf (Page 57)

100

101

DA 42 NG AFM Operating Limitations

Doc. No. 7.01.16-E Rev. 3 01-Apr-2014

EASA

approved

Page 2 - 17

2.7 MASS (WEIGHT)

Value

Mass (Weight)

Minimum flight mass 1450 kg' 3197 lb'

Maximum take-off mass 1900 kg 4189 lb

Maximum take-off mass (if MÄM 42-678 is carried out)' 1999 kg' 4407 lb'

Maximum zero fuel mass 1765 kg 3891 lb

Maximum zero fuel mass (if MÄM 42-659 is carried out)' 1835 kg' 4045 lb'

Maximum landing mass 1805 kg 3979 lb

Maximum landing mass (if MÄM 42-659 is carried out)' 1999 kg' 4407 lb'

Max. load in nose baggage compartment

(in fuselage nose)

30 kg 66 lb

Max. load in cabin baggage compartment

(behind rear seats)

45 kg 100 lb

Max. load in baggage extension

(behind cabin baggage compartment)

18 kg 40 lb

Max. load, cabin baggage compartment and baggage

extension together

45 kg 100 lb

if OÄM 42-207 is carried out:

Max. load in standard baggage compartment

(between rear seats and baggage bulkhead)

30 kg 66 lb

Max. load in short baggage extension 15 kg 33 lb

WARNING

Exceeding the mass limits will lead to overstressing of the

airplane as well as to degradation of flight characteristics and

flight performance.

1 2 ... 52 53 54 55 56 57 58 59 60 61 62 ... 439 440

Comments to this Manuals

No comments

Sennheiser SI 234 - ANNEXE 802 Operations Instructions Page 57

Comments to this Manuals