background image

 

Maintenance Manual   LS8-s and LS8-sb 

Instruments  and. Equipment

 

 

Edition: June 2016   

Rev. 6  TN 8024 

 

 

 

  6-2 

 

6.3 Seat Belt Harness (with multiple point buckles) 

 

Manufacturer Type TCDS 

No. 

Schroth 

4-01-0.104 (Lap belt and 
shoulder strap) 

40.073/11 

Gadringer 

Lap belt 5202  

40.070/32 

 

Shoulder strap 2700  

40.071/05 

 
6.4 Compass 

 

Manufacturer Type TCDS 

No. 

Ludolph FK 

16, FK 5, FK 10 10.410/3 

Airpath 

C 2300, C 2400 

TS 10.220/47 

PZL 

BS1, 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 

10.911/45 

 FSG-50 

10.911/71 

 FSG-60 

10.911/72 

 FSG-70,71 

10.911/81 

 FSG-90 

10.911/98JTSO 

 FSG 

2T 

LBA.0.10.911/103JTSO 

Becker AR 

3201-(1) 

10.911/76 

 

AR 2008/25 (A) 

10.911/48 

 

AR 4201 

JTSO-2C37 D, ED-23A 

 AR 

6201 

EASA.210.1249 

Avionik Dittel ATR 720 A 

10.911/74 

 

ATR 720 C 

10.911/83 

 ATR 

600 

LBA.0.10.911/106JTSO 

 ATR 

500 

LBA.0.10.911/113JTSO 

 ATR 

833 

EASA.210.0193 

Dittel Avionik KRT2 

EASA.210.10038036 

 

or other radios approved according to TSO, JTSO or ETSO for use in aircraft. 

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...

Отзывы: