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L-39 speeds reference?


francesco.fgmc

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AFAIK there are 3 'main' publications available for free on the internet.

 

Aero-L-39-Flight-Manual.pdf

http://www.anythingaboutaviation.com/pilot-operating-handbooks/

 

L-39ZA Pilot Manual 1990.pdf (Book 1, Part 2)

http://www.code1aviation.com/index.php/publications

 

l-39_rle.zip (Russian Pilot Manual)

http://www.airwar.ru/other/bibl/l-39_rle.html

 

The T.O. 1T-L39C-1, Aero-L-39-Flight-Manual, Part 6 - descent charts show

 

Maximum Range - Idle

Drag Index 0, 291km/h Descent Speed

Drag Index 30, 285km/h Descent Speed

Drag Index 60, 279km/h Descent Speed

 

For a windmilling engine or locked rotor

Max Time to descend at approx. 220 km/h EAS @ 4000m

Max Distance during descent at approx. 290 km/h EAS @ 4000m

 

For best climb rate there are similar charts but I prefer to use the method described in the L-39ZA Pilot Manual

 

 


  • Maximum Power - 106% (20 min max), then 103% Max sustained
  • 400km/h IAS until 500km/h TAS (thin airspeed needle)
  • then maintain 500km/h TAS (allowing IAS to fall)
  • Air speed is controlled by pitch/ascent rate

Note: Glide/drag ratios are covered in DCS_L-39_Flight_Manual_EN.pdf Emergency Procedures - Forced Landing, Page 278 which show a maximum glide ratio of 10 for a clean aircraft @ 300 km/h.


Edited by Ramsay
typos

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