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Maintenance Manual   LS8-s and LS8-sb 

Contents

 

Edition: June 2016   

Rev. 6  TN 8024 

 

 

 

  0-5 

 

 

0.2  List of Effective Pages

 (continued)

 

 

Chapter Page  Edition  Replaced Replaced 

Replaced 

4 4-10 

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2005

 

 

 

 

 4-11 

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2005

 

June 2016 

 

 

 4-12 

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 4-13 

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 4-14 

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 4-15 

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 4-16 

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 4-17 

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Dec. 2011 

 

 

 4-18 

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 4-19 

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 4-20 

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5 5-1 

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 5-2 

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 5-3 

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June 2016 

 

 

 5-4 

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June 2016 

 

 

 5-5 

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 5-6 

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June 2016 

 

 

 5-7 

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 5-8 

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 5-9 

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 5-10 

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 5-11 

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 5-12 

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 5-13 

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 5-14 

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6 6-1 

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June 2016 

 

 

 6-2 

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June 2016 

 

 

 6-3 

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 6-4 

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Dec. 2011 

 

 

 

 

 

 

 

 

7 7-1 

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2005

 

 

 

 

 

 

 

 

 

 

 

 

Summary of Contents for LS8-s

Page 1: ...8 3 TN8019 wheel brake actuated by airbrake handle Feb 2011 2 Title page 0 1 0 3 0 6 0 9 1 2 1 6 1 8 1 21 1 23 1 28a 4 1 4 17 6 4 11 11 9E4 M LS8 1 Miscellaneous improvements from ser No 8527 on Decem...

Page 2: ...og of revisions 0 7 April 2005 0 8 April 2005 0 9 April 2005 Dec 2011 0 10 April 2005 June 2016 0 11 April 2005 1 1 1 April 2005 Feb 2011 1 2 April 2005 Dec 2011 1 3 April 2005 1 4 April 2005 1 5 Apri...

Page 3: ...4 15 April 2005 4 16 April 2005 4 17 April 2005 Dec 2011 4 18 April 2005 4 19 April 2005 4 20 April 2005 5 5 1 April 2005 5 2 April 2005 5 3 April 2005 June 2016 5 4 April 2005 June 2016 5 5 April 200...

Page 4: ...2015 June 2016 8 2 April 2005 June 2016 8 3 April 2005 Feb 2011 9 9 1 April 2005 9 2 April 2005 10 10 1 April 2005 11 11 1 April 2005 11 2 April 2005 11 3 April 2005 11 4 April 2005 11 5 April 2005 11...

Page 5: ...instruction is required see also TN DG G 01 Approved repair methods according to EU Commission Regulation 1702 2003 part 21 subpart M 0 4 2 Airframe structural Life limit Maximum FRP structural life...

Page 6: ...hes local 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 t...

Page 7: ...hat non 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 spac...

Page 8: ...d installed 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...

Page 9: ...Load normally should be 110 kg 242 lbs as given in empty weight C G table It may be lower due to trim conditions excessive equipment or repairs Calculate Maximum Cockpit Load on weighing report see a...

Page 10: ...t No 1 1 Baggage comp No 0 0 Batteries installed Vert tail fin No 1 1 Date Inspector 18 08 2005 GS 18 08 2005 GS The discrepancy between Maximum Cockpit Load of 110 kg 242 lbs and Minimum Cockpit Load...

Page 11: ...o meet TSO C2 reading to 300 km h 160 Kt 180 mph may be used Maximum instrument error 2 Colour marking must be according to Flight Manual section 2 3 6 2 Altimeter Manufacturer Type TCDS No Winter 4 F...

Page 12: ...KJ 13A FD 19 77 Bohli 46 MFK 1 Not approved only as additional system 6 5 UHF Transmitter and Receiver Manufacturer Type TCDS No Dittel FSG 40 S 10 911 45 FSG 50 10 911 71 FSG 60 M 10 911 72 FSG 70 7...

Page 13: ...1157 Max Take off Mass 18 59 575 1267 including water ballast Aerobatic manoeuvres not approved Weight Limitations Maximum Cockpit Load max ______kg lbs Minimum Cockpit Load with tail battery tail tan...

Page 14: ...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...

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