DG Flugzeugbau LS8-st Скачать руководство пользователя страница 14

 

Maintenance Manual   LS8-st 

Placards

 

 

Edition: June 2016   

Rev. 6  TN 8024 

 

 

 

  8-2 

 

 

8.  Markings and Placards 

(continued) 

 

 

     Soaring  at instrument panel  

 

FUEL:            

Two stroke

 

Mixture

 

1:40 

of 

Vario    ASI 

Static/pitot switches 

 

Unleaded Four Star/Premium min. 95 ROZ 

   powered 

(Option) 

 

or AVGAS 100 LL 

 

 

 

with 2-stroke oil Castrol Super TT/TTS 

 

 

at left side of main bulkhead near 

   refuelling 

pump

16 

Right- and left 

 

When using a battery in the 

15 

at main fuel tank front 

 

vertical tail fin. Minimum

 

 

14 

 

 

Cockpit Load must be 

 

13  

 

redetermined 

by 

weighing 

 

12 

 

 

Use vertical tail fin battery only 

11 

 

 

with main fuse at battery 

10 

 

 

at vertical tail fin battery cover

9  

 

8  

 

 

 

 

Canopy Emergency Release

: open left side normally, 

 

 

pull right side with approx.15 kg/33 lbs force to stop

 

 

 

at right canopy frame

 

Altitude related 
Never Exceed Speed 

 

km/h 

 

Altitude related Never 

Exceed Speed 

 

km/h 

 

Kt. 

 

mph 

Up to   2000 m MSL  280   

Up to   6500 ft MSL 

280 

151 

174 

Up to   3000 m MSL  266   

Up to   9800 ft MSL 

266 

144 

165 

Up to   4000 m MSL  253   

Up to 13100 ft MSL 

253 

136 

157 

Up to   6000 m MSL  227   

Up to 19700 ft MSL 

227 

122 

141 

Up to   8000 m MSL  202   

Up to 26200 ft MSL 

202 

109 

126 

Up to 10000 m MSL  179   

Up to 32800 ft MSL 

179 

  97 

111 

Up to 12000 m MSL  156   

Up to 39400 ft MSL 

156 

  84 

  97 

On panel near airspeed indicator, 

On panel near airspeed indicator

for countries operating with metric 

 

units only. 

 

 

DEI-NT Placarding 

 

 0-5500 
17 5500-6000 
0,3 L 

6000 RPM 

  

 

Above DEI-NT Display 

 

 

 

 

   

on 

Fuel pump

 

off 

 

on

Kraftstoffpumpe

 

 

Main 

Haupt- 

schalter

 

 

   

auto 

   

 

Below DEI-NT Switches 

 
 

Содержание LS8-st

Страница 1: ...airbrake handle Feb 2011 3 Title page 0 1 0 3 0 4 0 6 0 8 0 11 1 3 1 7 1 9 1 22 1 29 1 36 1 40 1 48a 4 1 4 21 4 27 6 4 10 2a 11 15 9E2 M LS8 1 Miscellaneous improvements Ser no 8474 and from ser No 8...

Страница 2: ...ions 0 8 See log of revisions 0 9 April 2005 0 10 April 2005 0 11 April 2005 Nov 2010 Dec 2011 0 12 April 2005 June 2016 0 13 April 2005 1 1 1 April 2005 Feb 2011 1 2 April 2005 1 3 April 2005 Dec 201...

Страница 3: ...05 4 8 April 2005 4 9 April 2005 4 10 April 2005 4 11 April 2005 June 2016 4 12 April 2005 Oct 2015 4 13 April 2005 Oct 2015 4 14 April 2005 4 15 April 2005 4 16 April 2005 Nov 2010 4 17 April 2005 4...

Страница 4: ...l 2005 5 7 April 2005 5 8 April 2005 5 9 April 2005 5 10 April 2005 5 11 April 2005 5 12 April 2005 5 13 April 2005 5 14 April 2005 5 15 April 2005 5 16 April 2005 5 17 April 2005 5 18 April 2005 6 6...

Страница 5: ...0 6 April 2005 10 7 April 2005 10 8 April 2005 Nov 2010 10 9 April 2005 Oct 2015 11 11 1 April 2005 11 2 April 2005 Nov 2010 11 3 April 2005 11 4 April 2005 11 5 April 2005 11 6 April 2005 11 7 April...

Страница 6: ...part M 0 4 2 Airframe structural Life limit Maximum FRP structural life limit of sailplanes and powered sailplanes is 12000 hours of flight To reach this limit special inspections according to chapter...

Страница 7: ...ocal radius 22 to 26 28 to 30 down up mm in mm in mm in 67 2 638 26 to 30 1 024 to 1 181 32 to 35 1 260 to 1 378 68 2 677 26 to 31 1 024 to 1 220 33 to 35 1 299 to 1 378 69 2 717 26 to 31 1 024 to 1 2...

Страница 8: ...on concentric position of bearing keeps relative position to direction of flight Bond bushing with for instance Loctite 72 b 672 5 connect rudder cables provisionally do not forget to insert spacing c...

Страница 9: ...talled in baggage compartment when required decreases by 10 kg 22 lbs Finally resulting 4 different cockpit loads should be entered in the following places a in weighing report of inspection b in Flig...

Страница 10: ...t C G table It may be lower due to trim conditions excessive equipment or repairs Calculate Maximum Cockpit Load on weighing report see also examples at end of this section Resulting Maximum Cockpit L...

Страница 11: ...o 2 Baggage comp No 0 Batteries installed Vert tail fin No 1 Engine INstalled REmoved IN Date Inspector 18 08 2005 GS The discrepancy between Maximum Cockpit Load of 110 kg 242 lbs and Minimum Cockpit...

Страница 12: ...1 KJ 13A FD 19 77 Bohli 46 MFK 1 Not approved only as additional system 6 5 VHF transceiver Manufacturer Type TCDS No Dittel FSG 40 S 10 911 45 FSG 50 10 911 71 FSG 60 M 10 911 72 FSG 70 71 M 10 911 8...

Страница 13: ...ock OPEN TCDS No 902 Right Cockpit side at fuel cock Serial Number 8xxx Reg Signs D xxxx OPEN Deco CLOSED Type placard at main bulkhead Left Cockpit side at Deco lever Refueling pump at instrument pan...

Страница 14: ...y Release open left side normally pull right side with approx 15 kg 33 lbs force to stop at right canopy frame Altitude related Never Exceed Speed km h Altitude related Never Exceed Speed km h Kt mph...

Страница 15: ...45002039 Gas strut 100N for propeller stopper 45002074 Propeller stopper rubber stop Shock mounts for engine installation 45002079 Upper engine shock mounts 2 units installed 45002080 Lower engine sho...

Страница 16: ...510815 limit switch 164 025 with roller and screw contacts for intermediate positions 45002075 Proximity switch for RPM measurement complete with three pin plug 60510484 manual extend retract switch 6...

Страница 17: ...Maintenance Manual LS8 st Diagrams Issued June 2016 Rev 6 TN 8024 10 2 Diagram 2 Fuel system up to serial no L8528 In Datei br 236...

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