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Maintenance Manual   LS8-s and LS8-sb 

Instruments  and. Equipment

 

 

Edition: June 2016   

Rev. 6  TN 8024 

 

 

 

  6-1 

 

6. Instruments- and Equipment List (

Master Equipment List

 

 

Maximum mass of all Instrument Panel Installations  max. 6.7 kg <14.8 lbs>

 

6.1 Airspeed Indicator 

 

Manufacturer Type TCDS 

No. 

Winter 6FMS-4 (Diameter 80mm) 

  0-300 km/h  Art.No. 6421-499  
  0-160 kts     Art.No. 6423-499 
6FMS-5 in km/h 

TS 10.210/15 

Winter 7FMS-4 (Diameter 58mm) 

  0-300 km/h  Art.No. 7421-499  
  0-160 kts     Art.No. 7423-499 
7FMS-42 

TS 10.210/19 

Thommen 5A58() range 300 km/h 

 

PZL PR-400 

S-A in km/h 

 

 

or other Airspeed indicators approved according to TSO, JTSO or ETSO for 
use in aircraft or similar FAA approved airspeed indicators to 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 FGH 10 (Diameter 80mm) 
  1000-10000m Art.No. 4110  
  3000-30000ft  Art.No. 4330 

TS 10.220/46 

Winter 

4 FGH 20 (Diameter 58mm) 
  1000-10000m Art.No. 4220  

TS 10.220/47 

Winter 

4 FGH 20 (Diameter 58mm) 
  1000-20000ft  Art.No. 4550 

TS 10.220/48 

PZL 

W-12S in m 

 

 

or other Altimeters approved according to TSO, JTSO or ETSO for use in 
aircraft; one turn of dial max. 1000 m or 3000 ft. A similar FAA approved 
altimeter to meet TSO C10 with a range of approximately 33000 ft and a 
mercury or millibar or hektopascal subscale may be used. When an altimeter of 
up to 20000 ft only is being used, a placard must be near the altimeter stating: 
Maximum flying altitude 20000 ft. See also Flight Manual section 2.10.

 

 

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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