Limitations Placards - DG Flugzeugbau DG-1000 Flight Manual

2.21 Limitations placards

DG Flugzeugbau GmbH
Type: DG – 1000T Serial No.: 10-
Year of construction:
Maximum airspeeds
Winch launching
Aero-tow
Manoeuvring V
A
Rough air
Maximum speed V
NE
Powerplant extended
Powerplant extension-retraction
Approved aerobatic manoeuvres, only without
waterballast:
Pos. Loop, Chandelle, Spin, Stall turn
In addition Category A:
Only with 17,2 m or 18 m span without winglets, without
water ballast, engine retracted or removed:
Half loop and half roll, half roll and half loop, slow roll,
inverted flight, half positive flick roll from normal flight with
half loop, half negative flick roll from inverted flight
Maximum mass:
Category A
Category U
Category U without waterballast
Loading chart
Cockpit load front seat
maximum 110 kg
or maximum 105 kg
minimum kg
minimum kg
With lower pilot weight necessary ballast must be added.
Cockpit Check
1. Lead ballast (for under weight pilot)?
2. Parachute worn properly?
3. Safety harness buckled?
4. Front seat: pedals adjusted?
Rear seat: seating height adjusted?
5. All controls and knobs in reach?
6. Altimeter?
7. Dive brakes cycled and locked?
8. Positive control check ? (One person at the control
surfaces).
9. Fin ballast tank emptied or correct amount filled in?
10. Trim ballast box in the fin, correct amount filled in?
Locking device completely engaged?
11. Battery in the fin? Loading chart regarded?
12. Trim?
13. Fuel level?
14. Fuel cock open?
15. Both canopies locked?
16. Runway free?
limits for use of the waterballast tank
minimum °C
ground temperature
°F
maximum flight m
altitude above GND
ft.
Altitude in [m] 0-3000
V IAS km/h 270
NE
Altitude in [ft] 0-10000
V IAS kts. 146
NE
Issued: February 2016
Flight manual DG-1000T
T
km/h
150
185
185
185
270
185
100
630 kg 1389 lbs.
750 kg 1653 lbs.
kg
rear seat
242 lbs. 90 kg 198 lbs. included)
231 lbs. 105 kg 231 lbs.
lbs. / /
lbs. / /
13.5 17 24
56 63 75
1500 2000 3000
5000 6500 10000
4000 5000
256 243
13000 16000
138 131
TN1000/25
Other cockpit placards
see section 7
kts.
81
100
100
100
146
100
54
Main wheel
lbs.
(Parachute
without fin battery
With fin battery
box empty
At the control-light in the
front instrument panel
31 38
88 100
4000 5000
13000 16500
6000 7000 8000
230 217 205
20000 23000 26000
124 117 111
Gepäck max. 15 kg
baggage max. 33 lbs.
Sollbruchstelle 10000 N
rated load 2200 lbs.
Reifendruck
Tyre pressure 58 psi
Tail wheel
Reifendruck 2,5 bar
Tyre pressure 36 psi
Reifendruck 2,5 bar
Tyre pressure 36 psi
Nose wheel (if installed)
Ballast box in the fin
Min. load in the front seat
kg
box filled
Warning:
Rigging of the horizontal
tailplane is only permitted with
nose down trim-setting!
at the upper left hand
side of the fin
EASA app.
4 bar
kg
2.15