DG Flugzeugbau LS8-st Panduan Pemeliharaan - Halaman 13
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Halaman Cetak8. Markings and Placards
LS8-st Checklist
This powered sailplane must be operated in
compliance with operating limitations stated in
the form of markings, placards and Flight
Manual.
1. Main pins secured ?
2. Horizontal tail secured ?
3. Winglets secured ?
4. Test controls ?
5. Tail fin valve operating checked ?
6. When water ballast, then always
in wings and tail tank !
7. Check loading conditions
8. Check tail dolly removed
9. Fasten seat belt harness
10. Connect parachute static line
11. Lock air brakes
12. Check trim position
13. Check release system
14. Lock canopy
15. Propulsion system ready for use ?
16. Sufficient amount of fuel ?
17. Propulsion system retracted?
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-t
TCDS- No.
902
Serial Number 8xxx
Reg. Signs
D-xxxx
Type placard at main bulkhead
Refueling pump at instrument panel
Edition: June 2016
Maintenance Manual LS8-st
.
.
.
.
Rev. 6 TN 8024
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. ________
Under instrument panel cover
DG Flugzeugbau GmbH
Type: LS8-t
Serial No.:_______
Data Placard
Airspeed Limits:
Winch launch/Auto tow
Aero tow
In rough air
Never exceed (VNE)
Extend/retract engine
Engine extended
Max. Take-off Mass *) 15 42
with 4"-wheel: 18 59
with 5"-wheel: 18 59
*) including water ballast
Aerobatic manoeuvres not approved
Take-off under own power not approved
Weight Limitations
Maximum Cockpit Load
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.______kg/lbs
Lighter pilots must compensate lack of weight as
suggested in Flight Manual
Ball of bearing
at forward horizontal tail
must be fixed
attachment on vertical tail fin
CLOSED ◄ Fuel Cock ► OPEN
Right Cockpit side at fuel cock
OPEN ◄ Deco ► CLOSED
Left Cockpit side at Deco-lever
Placards
kg / lbs
min. ________
min. ________
min. ________
km/h
Kt MPH.
140
76
87
195
105 121
195
105 121
280
151 174
110
59
68
160
99
86
m
ft
kg
lbs
525 1157
525 1157
575 1267
max. ______kg/lbs
min. ______kg/lbs
min. ______kg/lbs
min. ______kg/lbs
At right cockpit wall
8-1