DG Flugzeugbau LS8-s Посібник з технічного обслуговування - Сторінка 13
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Також для DG Flugzeugbau LS8-s: Керівництво з польотів (8 сторінок)
Друкувати сторінкуMaintenance Manual LS8-s and LS8-sb
8. Markings and Placards
LS8-s and -sb Checklist
This sailplane must be operated in
compliance with operating limitations
stated in the form of markings,
placards and EASA approved Flight
Manual.
1.
Main pins secured?
2.
Elevator secured?
3.
Winglets secured?
4.
Check controls
5.
Tail fin valve operation checked?
6.
When using water ballast, then
always in wing and tail!
7.
Check loading conditions
8.
Check tail dolly removed?
9.
Fasten seat belt harness
10. Fasten parachute and connect
parachute static line
11. Lock air brakes
12. Check trim position
13. Check release system
14. Lock canopy
At underside of instrument panel
Tyre pressure
3.5 bar
on right
(51 psi)
landing gear door
Tyre pressure
above tail wheel,
2.5 - 3.5 bar
when fitted
(36 to 51 psi)
Tyre Pressure
above tailwheel
6,2 bar/90 psi
small tailwheel according to TN 8021, if installed
at Baggage Compartment
Maximum Baggage weight 5 kg (11 lbs)
(For soft items only)
DG-Flugzeugbau GmbH
TYPE
LS8-s
TCDS- No.
A.047
Serial Number 8xxx
Reg. Signs
D-xxxx
DG-Flugzeugbau GmbH
TYPE
LS8-sb
TCDS- No.
A.047
Serial Number 8xxx
Reg. Signs
D-xxxx
Type placard at main bulkhead
Edition: June 2016
MINIMUM COCKPIT LOAD:
with tail battery, tail tank full
with tail battery, tail tank empty
without tail battery, tail tank full
without tail battery, tail tank empty min. ________
DG Flugzeugbau GmbH
Type: LS8-xx
Airspeed Limits:
Aerobatic manoeuvres not approved
Maximum Cockpit Load ....max.______kg/lbs
Minimum Cockpit Load
with tail battery, tail tank full min.
with tail battery, tail tank empty min. ______kg/lbs
without tail battery, tail tank full min
without tail battery, tail tank empty min._____kg/lbs
Lighter pilots must compensate lack of weight as
suggested in Flight Manual
.
.
.
.
.
.
.
.
Rev. 4 TN 8024
Under instrument panel cover
Serial No.:_______
Data Placard
Winch launch/Auto tow
Aero tow
In rough air
Never exceed (VNE)
Max. Take-off Mass *) 15 42
Max. Take-off Mass *): 18 59
*) including water ballast
Weight Limitations
xx= variant –s or –sb
Ball of bearing
at forward horizontal tail
must be fixed
attachment on vertical tail fin
Placards
kg / lbs
min. ________
min. ________
min. ________
km/h
Kt MPH.
140
76
87
195
105 121
195
105 121
280
151 174
m
ft
kg
lbs
525 1157
575 1267
______kg/lbs
_____kg/lbs
At right cockpit wall
8-1