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17/2004

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25

31

36-37-38a

36-37-38a

36-37-38b

36-37-38b

36-37-38c

36-37-38c

32

33

34+34A

I-wire 0,5 mm

II-wire 0,5 mm

III-wire 0,5 mm

35

29

27

26

28

x2

x2

x1

A

B

C

D

E

F

G

1

2

2a

3

4

5

6

7

8

9

a

b

c

d

10

11

12

13

14+14a

15

15A

15B

15C

15D

15E

20

20A

8c

22

22

21b

21a

19

39 39c-wire

24

30b

WIRE

36-37-38a

36-37-38b

36-37-38c

34+34A

22

19

21a

21b

20

30a

19

23

23a

18

23+23a

19A

19B

19C

19D

19E

17

17a

17A

17B

16

17

19

To insert to centre

Belt of paper

1959, powered by a Bristol Siddeley Viper turbojet engine. The second prototype, first flown in July 1960, was powered by the Czech-

designed M701 engine, which was to become the standard installation.

In 1961, the L-29 was entered in a competitive design evaluation to find a new Warsaw pact basic/advanced jet trainer to replace the 

piston-engine trainer fleet. The other competitors were the Russian Yakovlev Yak-30 and the Polish TS-11 Iskra. The L-29 won and 
subsequently became the standard trainer in all Eastern-bloc counties except Poland.

The first production Delfin rolled off the assembly line in April 1963, and production continued for more than 11 years, a huge statement 

of its success. More than 2,000 were eventually supplied to the Soviet air force, and 400 more to the Czech air force. Others were supplied to 
Bulgaria, East Germany, Hungary and Romania.

Straightforward, rugged and easy to fly, the L-29 was ideal as both a primary jet trainer and as an advanced combat/weapons trainer. The 

Delfin was later exported to several other nations including Egypt and Indonesia. A small number of a single-seat version, the L-29A Delfin 
Akrobat, was produced, but it never caught on.

In recent years, the L-29 has become popular on the jet warbird market, mostly in the USA, but also in England, Italy and South Africa.

Nicknames: Maya (NATO Code name)
Number Built: Approximately 3,500

Specifications:
     Engine: One 1,960-lb thrust Motorlet M701 VC-150 or S-50 turbojet
     Weight: Empty 5,027 lbs., Max Takeoff 7,231lbs.
     Wing Span: 33ft. 9in.
     Length: 35ft. 5.5in.
     Height: 10ft. 3in.
     Performance:
          Maximum Speed at 16,000 ft: 407 mph
          Ceiling: 36,100 ft.
          Range: 397 miles with internal fuel
     Armament: None

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1

2

2a

3

4

4

5

6

7

8

a

b

8c

9

a

b

c

d

10

11

12

13

14

14a

15

16

17

17a

17

L

R

18

19

19

P

R

R

R

L

L

L

L

L

L

P

R

20

20

21a

21a

21b

21b

20A

22

23

23

23a

24

39

a

b

c

30

a

b

36

36

a

b

c

a

b

c

38

38

a

b

c

a

b

c

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37

a

a

b

b

c

c

29

26

27

28

a

b

c

32

33

34

35

25

31

G

A

B

B

C

C

D

D

E

E

F

15B

15C 15D

15A

15B

15C

15D

15E

15E

19B

19C

19B

19C

F

19D

19E

19D

19E

19A

19B

19B

19C

19C

19D

19D

19E

19E

17A

17B

29A

29B

29B

34A

34A

34A

34A

34A

34A

34A

34A


Document Outline