Manoeuvring Load Factors; Flight Crew; Issued: October - DG Flugzeugbau DG-1000 Flight Manual

2.10 Manoeuvring load factors

The following load factors must not be exceeded:
Category
at manoeuvring speed
at max. speed
with airbrakes extended

2.11 Flight crew

a) single seated, only permissible in the front seat
max. load in the front seat
min. load in the front seat
b) two seated
Either the front seat or the rear seat may designated as seat of the pilot in
command.
If the rear seat is to be designated it must be assured that all necessary
operating items and instruments are installed and that the pilot in command
has sufficient training in flying safely from the rear seat.
Max. load in both seats combined: 210 kg (462 lbs.)
Max. load in the front seat: 105 kg (231 lbs.)
Exception: The load in the front seat may be max. 110 kg (242 lbs.) with the
load in the rear seat not exceeding 90 kg (198 lbs.)
Max. load in the rear seat: 110 kg (242 lbs.)
Min. cockpit load in the front seat is the min. cockpit load see a) minus 40%
of the load in the rear seat. This means that 10 kg (22 lbs.) in the rear seat
replaces 4 kg (8.8 lbs.) missing cockpit load in the front seat.
With these loads, the C.G. range given under 6.8 will be kept in the limits if
the empty weight C.G. is in its limits. See loading chart in sect. 6.8.
Caution:
With lower pilot weights lead ballast must be added to the seat.
Ballast put on the seat (lead ballast cushion) must be fastened at the safety belt
anchor point.
Option: Provision for removable trim-ballast in the front cockpit see sect 7.17.1.
Note: For Australia the lower limit for the min. load in the cockpit should not
exceed 66 kg (146 lbs.). A provision for removable ballast see sect. 7.17.1 is
mandatory.

Issued: October 2014

Flight manual DG-1000T
V
A
V
NE
V
NE
110 kg (242 lbs.)
see placard in cockpit and weighing
report page 6.7
TN1000/24
Utility Aerobatic
+5,3 -2,65 +7,0 -5,0
+4,0 -1,5 +7,0 -5,0
+3,5 0 +3,5 0
EASA app.
2.9