3-8
Date of Issue: 04/2008
Revision: 1.0
2.6 Weight
Empty weight (standard equipment) ................... 340 kg
NOTE
Actual empty weight is shown in SECTION 6
Max. take-off weight ............................................ 600 kg
Max landing weight ............................................. 600 kg
Max. weight of fuel .............................................. 98 kg
Max. baggage weight in rear fuselage ................ 15 kg
Max. baggage weight in each wing locker .......... 20 kg
2.7 Center of gravity
Operating C.G. range ..........................................
25 to 35 % of
MAC
2.8 Approved maneuvers
Airplane Category: LSA
The NG 4 ML is approved for normal and below listed maneuvers:
Steep turns not exceeding 60° bank
Lazy eights
Chandelles
Stalls (except whip stalls)
WARNING
Aerobatics and intentional spins are prohibited !
2.9 Maneuvering load factors
Maximum ultimate positive limit load factor ....... +6 g
Maximum ultimate negative limit load factor ...... - 4 g