DG Flugzeugbau LS8-st Скачать руководство пользователя страница 7

 

Maintenance Manual   LS8-st 

Systems

 

 

Edition: June 2016   

Rev. 6     TN 8024 

 

 

 

  1-10 

 

 

1.

 

S

YSTEM 

D

ESCRIPTION AND 

A

DJUSTMENT 

D

ATA

 

(continued) 

 

1.4 Elevator Control System 

(continued) 

 

1.4.2 Deflections and Tolerances 

 

Elevator: 

up 

28° - 30° 

 

down 

22° - 26° 

 

For easier checking, measured angles may be converted to mm / in 
deflection values, using the actual local radius of the defined measuring 
place. See also table below. 
 
Limit values for elevator deflections in Millimetres/Inches 

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 to 1.220 

33 to 36 

1.299 to 1.417 

70 

2.756 

27 to 31 

1.063 to  1.220

34 to 36 

1.339 to 1.417 

71 

2.795 

27 to 32 

1.063 to 1.260 

34 to 37 

1.339 to 1.457 

72 

2.835 

27 to 32 

1.063 to 1.260 

35 to 37 

1.378 to 1.457 

 

1.4.3 Stops 

 

Elevator stops at lower control stick end. Adjustment by use of two 
10

mm open end wrenches. 

 
 

1.4.4 Elevator Rear Edge Play 

 

Play should be measured with control stick fixed to neutral position. 

 

 

 

Elevator : 

maximum 2.5 mm <0.1 in> at inner edge 

 

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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