DG Flugzeugbau LS8-st Скачать руководство пользователя страница 8

 

Maintenance Manual   LS8-st 

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-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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