background image

 

Maintenance Manual   LS8-s and LS8-sb 

Systems

 

 

Edition: June 2016   

Rev. 6  TN 8024 

 

 

 

  1-9 

 

 

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 

 

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...

Reviews: