Lombardini Diesel Motor Catalog 9LD625 2
Lombardini Diesel Motor Catalog 9LD625 2
Lombardini Diesel Motor Catalog 9LD625 2
12.0-26.0 kW
Engines with 2 and 3 cylinders in model s
KD 330/2 - 25 LD 330/2, KD 425/2 - 25 LD 425/2,
KD 477/2 - 12 LD 477/2, kd 625/2 - 9 LD 625/2
and kd 626/3 - 11 ld 626/3 covering a power
r ange of 12.0 to 26.0 kW. These are the best
option in their market sector, offering
dur able performance, compactne ss and
low maintenance costs. Widely used for
applications such a s motor-cultivators,
sm a ll four-w heeled tr ac tor s, pump s
and compre ssor s.
AIR cooled
Diesel engines
12.0-26.0 kW
s ta n da r d e q u i p m e n t Acc e s s o r i e s o n d e m a n d
Electric starting with 12 V starter motor Different guards according to use
and alternator Range of alternative alternators and 24 V
Remote throttle Compression release
Oil pressure switch Flanges
Combined manifold and exhaust muffler Dry air filter
Engine feet External fuel filter
Fuel lift pump Clutches
Counter-clockwise rotation on power Hydraulic pump adapters
take-off side Range of fuel tanks of various sizes
Automatic extra fuel device Range of flywheels for various clutches
Use, maintenance and spare parts Mufflers and exhaust pipes
booklet Controls
Oil bath air filter Pulleys
Manual control accelerator Oil cooler (KD 625/2 - 9 LD 625/2; KD
Power take-off on flywheel (KD 625/2 - 9 330/2 - 25 LD 330/2; KD 425/2 - 25 LD
LD 625/2; KD 626/3 - 11 LD 626/3) 425/2; KD 626/3 - 11 LD 626/3)
Power take-off on crankshaft (KD 330/2 - Crank starter (KD 625/2 - 9 LD 625/2)
25 LD 330/2; KD 425/2 - 25 LD 425/2; KD Keyswitch panel
477/2 - 12 LD 477/2)
Fuel tank with filter
Guard for belt (KD 626/3 - 11 LD 626/3)
KD 330/2
25 ld 330/2
quick specifics
2
cylinder
307,5
339
485
*57
122
137
p e r fo r m a n c e c u r v e s ( I F N - I S O 3 0 4 6 a n d i s o 14 3 96 )
32.0
3.2
30.0 MB
3.0
2.8
28.0 kW HP
26.0 13.0
2.6 17.0
24.0 N 12.0 16.0
2.4
NB 15.0
11.0
NA 14.0
kgm Nm 10.0
13.0
9.0 12.0
8.0 11.0
10.0
7.0
9.0
6.0 8.0
7.0
5.0
6.0
g/HPh g/kWh 4.0
5.0
215 290
C
270
195
250
175 230
1200 1400 1600 1800 2000 2200 2400 2600 2800 3000 3200 3400 3600 3800
rpm
N - Power curve - 80/1269/CE E-ISO 1585 MB - Torque curve - (NB curve)
NB - Power curve - ISO 3046/1 -IFN C - Specific fuel consumption - (NB curve)
NA - Power curve - ISO 3046/1 - ICXN
Power ratings refer to engines equipe with air filter, standard muffler, after being run in and in ambient
conditions of 25°C and 1 bar. Power levels drop by 1% every 100m altitude and by 2% every 5°C above 25°C.
KD 425/2
25 ld 425/2
quick specifics
2
cylinder
122
p e r fo r m a n c e c u r v e s ( I F N - I S O 3 0 4 6 a n d i s o 14 3 96 )
40.0
4.0
38.0
3.8 kW HP
36.0
3.6
MB
34.0
3.4 N 19.0
32.0 14.0
3.2 18.0
NB 13.0
kgm Nm 17.0
NA 12.0 16.0
11.0 15.0
14.0
10.0
13.0
9.0 12.0
8.0 11.0
10.0
7.0
9.0
g/HPh g/kWh
6.0 8.0
230 7.0
290 5.0
210 270
250 C
190
230
170
210
1200 1400 1600 1800 2000 2200 2400 2600 2800 3000 3200 3400 3600 3800
rpm
N - Power curve - 80/1269/CE E-ISO 1585 MB - Torque curve - (NB curve)
NB - Power curve - ISO 3046/1 -IFN C - Specific fuel consumption - (NB curve)
NA - Power curve - ISO 3046/1 - ICXN
Power ratings refer to engines equipe with air filter, standard muffler, after being run in and in ambient
conditions of 25°C and 1 bar. Power levels drop by 1% every 100m altitude and by 2% every 5°C above 25°C.
KD 477/2
12 ld 477/2
quick specifics
2
cylinder
380
329
565
305,5
*250
175
185
N° 4 holes
194 66 Ø 13 144 161
399 202
* gravity center of the engine
p e r fo r m a n c e c u r v e s ( I F N - I S O 3 0 4 6 a n d i s o 14 3 96 )
60.0
6.0
5.5 55.0
50.0
5.0 MB kW HP
4.5 45.0 17
23
N
4.0 40.0 16 22
NB 15 21
14 20
kgm Nm NA
19
13
18
12
17
11 16
10 15
g/HPh g/kWh
9 14
220 13
290 8
12
200 270 7
11
250 6
180 10
C
230
160 210
1200 1400 1600 1800 2000 2200 2400 2600 2800 3000 3200
rpm
N - Power curve - 80/1269/CE E-ISO 1585 MB - Torque curve - (NB curve)
NB - Power curve - ISO 3046/1 -IFN C - Specific fuel consumption - (NB curve)
NA - Power curve - ISO 3046/1 - ICXN
Power ratings refer to engines equipe with air filter, standard muffler, after being run in and in ambient
conditions of 25°C and 1 bar. Power levels drop by 1% every 100m altitude and by 2% every 5°C above 25°C.
KD 625/2
9 ld 625/2
quick specifics
2
cylinder
557 633
217 340 434
236 122 275 285
182
397
421
367
47
599
161
229
164
162
107
47
176,6
178
178
162
14 19
18
13
17
g/HPh g/kWh
12 16
220 15
290 11
14
200 270 10
C 13
250 9 12
180
230 8 11
160 210
1200 1400 1600 1800 2000 2200 2400 2600 2800 3000 3200
rpm
N - Power curve - 80/1269/CE E-ISO 1585 MB - Torque curve - (NB curve)
NB - Power curve - ISO 3046/1 -IFN C - Specific fuel consumption - (NB curve)
NA - Power curve - ISO 3046/1 - ICXN
Power ratings refer to engines equipe with air filter, standard muffler, after being run in and in ambient
conditions of 25°C and 1 bar. Power levels drop by 1% every 100m altitude and by 2% every 5°C above 25°C.
KD 626/3
11 ld 626/3
quick specifics
3
cylinder
R120 292
275
435
201,5
0° 30°
° 3
177
20
n.6M10x1,5
686
30 °
n.4M10x1,5
180
40°
30°
0°
30°
180
°3
30
25
214
° 30
30
° 30°
14
N.2Ø10
10 26
305 129,5 295 78,5 89 400
381 18
592
p e r fo r m a n c e c u r v e s ( I F N - I S O 3 0 4 6 a n d i s o 14 3 96 )
11.0 110
10.0 100
9.0 90
80 MB kW HP
8.0
7.0 70 28
36
NB 26
34
kgm Nm NA 24 32
22 30
28
20
26
18 24
16 22
g/HPh g/kWh 20
14
18
220
290 12 16
C
270 10 14
200
250 8
180
230
160 210
1000 1200 1400 1600 1800 2000 2200 2400 2600 2800 3000 3200
rpm
N - Power curve - 80/1269/CE E-ISO 1585 MB - Torque curve - (NB curve)
NB - Power curve - ISO 3046/1 -IFN C - Specific fuel consumption - (NB curve)
NA - Power curve - ISO 3046/1 - ICXN
Power ratings refer to engines equipe with air filter, standard muffler, after being run in and in ambient
conditions of 25°C and 1 bar. Power levels drop by 1% every 100m altitude and by 2% every 5°C above 25°C.
a p p l i cat i o n s s p e c s
KD 3 3 0 /2 - 2 5 L D 3 3 0 / 2 ; KD 4 2 5 / 2 - 2 5 L D 4 25 / 2
D2 n (rpm) n (rpm)
L1 L2
F1 F2 Max intermittent axial load in both directions A - B = 300 kg
KD 4 7 7 /2 - 1 2 L D 4 7 7 / 2
N (kW) N (kW)
D 1 (mm) ≥ 220 [78 + L 1 (mm)] D 2 (mm) ≥ 196 [150 + L 2 (mm)]
n (rpm) n (rpm)
B A
D2
D1
L2 L1
KD 6 2 5 /2 - 9 L D 6 2 5 / 2
N (kW) N (kW)
D 1 (mm) ≥ 136 [162 + L 1 (mm)] D 2 (mm) ≥ 204 [260 + L 2 (mm)]
A B n (rpm) n (rpm)
D1
D2
KD 6 2 6 /3 - 1 1 L D 6 2 6 / 3
N (kW) N (kW)
A B D 1 (mm) ≥ 100 [185 + L 1 (mm)] D 2 (mm) ≥ 113 [169 + L 2 (mm)]
D1
D2
n (rpm) n (rpm)
L1 L2
Max intermittent axial load in both directions A - B = 300 kg
AVAI L A B L E f l a n g e s *
136 44
60 ° 16
Kd 330/2 - 25 ld 330/2
15 4
ENGINE AXIS
ENGINE AXIS
8 TA P E R 1: 5
M .8 N ° 6 H O L E S
Ø 135
Ø 105
Ø 105
18
M. 14 X 1,5
Ø 14,5
Ø 44,5
Ø 44,5
M.8 N° 4 HOLES
13
I =33
Ø 30
15 4
37
136 8
136 44
60° 16
15 4
KD 425/2 - 25 LD 425/2
ENGINE AXIS
ENGINE AXIS
8 TA P E R 1: 5
M .8 N ° 6 H O L E S
Ø 135
Ø 105
Ø 105
18
M.8 N° 4 HOLES
M. 14 X 1,5
Ø 14,5
Ø44,5
Ø 44,5
13
I=33
Ø 30
15 4
37 136 8
55 55 5 30
10
R 3
ENGINE AXIS
90 TAPER 1:5
KD 477/2 - 12 LD 477/2
95.26
- 0 ,0 5
53
0
Ø 125
53
50
40
110
+ 0,0 5
Ø 38
M 18X1,5
+ 0,1
Ø 20
20
53 53 139 M 10 N° 9 HOLES
90.5 90.5
+0,05
+0,376
Ø3 1 4+0,425
Ø2 1 5.9 +0,1
60°
Ø2 4 4
Ø200
Ø184
A
.37
7.5
33
flywheel axis
Ø 3
40 76.5
4
116.5
LES
HO
N°8 X 1.5
0
M1
AVAI L A B L E f l a n g e s *
7
324
47
Kd 625/2 - 9 LD 625/2
5
Ø3
11
25
R.
19
5
Ø60 -00.030
Ø305 0.127
47
324
Ø 32
Ø42
+0
Ø 160
Ø 190
Ø 291
Ø 300
n.8 holes M10x1.5 8,5
45°
A 15° 71.4
n.8 holes 17.5 12
5/16" 18 UNC 2B 30
°
Ø3
81
30°
Kd 625/2 - 9 LD 625/2
+0,127
Ø241.3 +0,127
Ø52 -00.03
0
0
Ø403.3
Ø206
30°
Ø361.95
5 45° °
.2 45
22
Ø2
°
177
12
40°
+0,040
+0,057
16
24
0
Ø150
Ø288
Ø140
Ø340
Ø 365 A
180
30° 30°
N.8 M.10x1,5
45° Ø 105 34
7
5
400± 0,20
12 0,32
N12 HOLES
3/8-16 UNC - 2B
0,12
SEEN FROM "A" SIDE
N8 HOLES
S/16"-18 UNC-2B 0,20
Kd 626/3 - 11 LD 626/3
°
30
87±1
Ø241,3 +00,0 46
5
Ø361,95
45°
0,12 30,2±1
R.12
1ST CYLINDER AXIS
66,7
R105 M12X1,75-6H
24
18 0,16
211
407
KD 330/2 KD 425/2
Model
25 LD 330/2 25 LD 425/2
4 stroke air cooled diesel engine • •
Direct injection • •
Mechanical fuel lift pump • •
Forced lubrication with oil pump • •
Full flow oil filtration • •
Torque regulator • •
Centrifugal speed governor • •
Crankcase in die-cast aluminum • •
Engine specs
Electric starting • •
Counter-clockwise rotation (from power take-off side) • •
Aluminum alloy independent heads • •
Indipendent cast iron cylinders • •
Automatic extra fuel starting device • •
Air cooled by fan • •
Power take-off on crankshaft • •
Power take off on Flywheel - -
Cylinder 2 2
Bore (mm) 80 85
Stroke (mm) 65 75
Technical features
Engine displ (cm3) 654 851
Injection system DI DI
Compression ratio 19:1 19:1
Emission compliance ECE R 24 ECE R 24
Rating (kW/HP)
12.0/16.3 14.0/19.0
N (80/1269/CEE)ISO 1585
11.2/15.2 13.0/17.7
Performance NB ISO 3046 IFN
10.3/14.0 12.0/16.3
NA ISO 3046 ICXN
Max torque (Nm@rpm) 32.0@2400 42.0@2200
Min idling speed (rpm) 1000 1000
EN 590 • •
No 1 Diesel (US) - ASTM D 975-09 B - Grade 1-D S 15 • •
No 1 Diesel (US) - ASTM D 975-09 B - Grade 1-D S 500 • •
No 2 Diesel (US) - ASTM D 975-09 B - Grade 2-D S 15 • •
No 2 Diesel (US) - ASTM D 975-09 B - Grade 2-D S 500 • •
Fuel compatibility ARCTIC EN 590/ASTM D 975-09 B • •
High Sulfur Fuel < 5000 ppm (< 0.5%) • •
High Sulfur Fuel > 5000 ppm ( > 0.5%) • •
Military NATO Fuels F34 - F35 - F44 - F63 - F64 - F65 * • •
Military US Fuels JP5 - JP8 (AVTUR) * • •
Civil Jet Fuels Jet A/ A1* • •
Fuel tank capacity (l) 4 4
Oil sump capacity (l) 1.5 1.7
Oil consumption (kg/h) 0.007 0.0085
Service features
Oil change interval std/synthetic (hr) 250 ** 250 **
Oil filter change interval std/synthetic (hr) 250 ** 250 **
Valve adjustement 500 500
H × L × W (fan excluded) (mm) 485×485×438 503.5×485×464
Dry weight (kg) 60 63
Daily service points - positions 1 side service 1 side service
Physical Ambient operating temps (°C) -5° +45° *** -5° +45° ***
characteristics Gradeability-all round (intermittent-30 min) (deg) 25° 25°
Gradeability-all round (peak value-1min) (deg) 35° 35°
Cap. of air required for correct combustion @3600 (l/min) 1050/875 1330/1110
Cap. of air required for correct cooling @3600 (l/min) 11700/9750 14200/11835
SAE 15 W-40 API CF4/SG ACEA SAE 15 W-40 API CF4/SG ACEA
Lubrication Oil type
B2/E2 B2/E2
Physical Ambient operating temps (°C) -10° +45° *** -10° +45° *** -10° +45° ***
characteristics Gradeability-all round (intermittent-30 min) (deg) 25° 25° 25°
Gradeability-all round (peak value-1min) (deg) 35° 35° 35°
Cap. of air required for correct combustion @3600 (l/min) 1500/1220 1600 (@3000) 2400 (@3000)
Cap. of air required for correct cooling @3600 (l/min) 15800/13200 26300 (@3000) 38000 (@3000)
SAE 15 W-40 API CF4/SG SAE 10 W-40 API CF4/SG SAE 15 W-40 API CF4/SG
Lubrication Oil type
ACEA B2/E2 ACEA B2/E2 ACEA B2/E2
Europe uk france
Lombardini Srl Lombardini U.K. Ltd Lombardini France S.a.s.
Via Cav. del lavoro 1, Rochester Barn - Eynsham Road 47 Allée de Riottier,
Lombardini s.r.l. is a part of Kohler Group. A. Lombardini n° 2 OX2 9NH 69400 Limas, FRANCE
Lombardini has manufacturing facilities in Italy, Slovakia 42124 Reggio Emilia, ITALY Oxford, UK T. +33-(0)474-626500
and India and sales subsidiaries in France, Germany, UK, T. +39-(0)522-389-1 T. +44-(0)1865-863858 F. +33-(0)474-623945
Spain and Singapore. infodiesel@kohler.com F. +44-(0)1865-861754
Kohler/Lombardini reserves the right to make
modifications without prior notice.
deutschland e s pa Ñ a r o a pa c
For the latest version please visit our website:
Lombardini Motoren GmbH Lombardini ESPAÑA, S.L. Kohler Singapore Pte Ltd
www.lombardini.it Fritz-Klatte-Str. 6, Bürogebäude 2 P.I. Cova Solera 1-9 (Kohler Power Systems)
65933 Frankfurt am Main, 08191 - Rubí (Barcelona) 7 Jurong Pier Road
DEUTSCHLAND ESPAÑA SINGAPORE 619159
T. +49-(0)69-9508160 T. +34-(0)9358-62111 T. +65-63020701
F. +49-(0)69-95081630 F. +34-(0)9369-71613 Sgsalesall@kohler.com