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Maintenance Manual   LS8-s and LS8-sb 

Instructions

 

 

Edition: June 2016   

Rev. 6  TN 8024 

 

 

 

  4-11 

 

 
4.5 Installation of Control Surfaces

 (continued) 

 

Disassembly of Rudder

 

(1) disconnect rudder cables. 
 

Attention:

 Don’t loose spacing casings. 

 

Attention:

 Rudder cables may be drilled. If this is changed 

unintentionally, neutral positions of rudder and pedals do no longer 
correspond and must be realigned as detailed below. 

(2) loosen nut at lower bearing (6mm thread, M6 LN 9348 or DIN 985-8zn, 

width over flats 10mm) using a socket wrench, remember sequence and 
position of washers. 

(3) lift rudder upward from bearings. 

 

Assembly of Rudder

 

(1) grease bearings according to lubrication schedule, see section 3.3. 
(2) If need be, install new V-type internal seal, see section 4.6. 
(3) lower rudder into bearings, do not use force ! 
(4) check radial play of upper bearing: maximum permissible radial play 0.5 

mm <0.02 in>. If necessary renew brass bushing. Make sure, that 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 spacing casings 

into thimbles. 

(6) check rudder pedal alignment: with pedals in neutral position check if 

rudder is neutral. 
If rudder is deflected to one side, twist 

opposite

 cable 

counter-clockwise

 

(

maximum 5 turns

) until properly aligned. 

Should more than 5 turns be necessary for alignment, exchange cables. 

Caution:

 Never  turn cables 

clockwise 

(7) place washers on cable connection bolts and tighten nuts M6 LN 9348 or 

DIN 985-8zn, width over flats 10 mm, with maximum torque 6.4 Nm 
(0.65 mkg, 4.623 ft lbs). 

(8) set up washers at lower bearing as found during disassembly (normally: 

recessed washer first, then large washer). Tighten nut (6 mm thread, LN 
9348 or DIN 985-8zn, width over flats 10 mm) with maximum torque 6.4 
Nm, (0.64 mkg, 4.623 ft lbs). After assembly the rudder should have 
audible axial play, maximum axial play 1 mm (0.04 in), see section 1.5. 

(9) if necessary, restore gap seals (convex plastic strip) on both sides, see 

section 4.6. 

 

Содержание LS8-s

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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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