Underground - Hard Rock

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R1300G
R1300G
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  • R1700
  • R2900 XE (Diesel-Electric)
  • R2900G
  • R3000H
R1600H
  • R1300G
  • R1700
  • R2900 XE (Diesel-Electric)
  • R2900G
  • R3000H
R1700
  • R1300G
  • R1600H
  • R2900 XE (Diesel-Electric)
  • R2900G
  • R3000H
UNITS:
Metric
Imperial
Engine Model
Cat® 3306B DITA
Cat® 3306B DITA
 
Cat® C11
Cat® C11
 
Cat® C13
Cat® C13
Engine Power - ISO 14396:2002
117 kW
157 HP
 
-
 
-
Bore
120.7 mm
4.75 in
 
130 mm
5.1 in
 
-
Stroke
152.4 mm
6 in
 
140 mm
5.5 in
 
-
Displacement
10.5 l
640.75 in³
 
11.1 l
680.4 in³
 
-
Note (1)
Power ratings apply at a rated speed of 2,200 rpm when tested under the reference conditions for the specified standard.
Power ratings apply at a rated speed of 2,200 rpm when tested under the reference conditions for the specified standard.
 
Power ratings apply at a rated speed of 1,800 rpm when tested under the reference conditions for the specified standard.
Power ratings apply at a rated speed of 1,800 rpm when tested under the reference conditions for the specified standard.
 
Power ratings apply at a rated speed of 1,800 rpm for LRCs (VR and Tier 3/Stage IIIA) engines when tested under the reference conditions for the specified standard.
Power ratings apply at a rated speed of 1,800 rpm for LRCs (VR and Tier 3/Stage IIIA) engines when tested under the reference conditions for the specified standard.
Note (2)
All rating conditions are based on ISO/TR14396:2002, inlet air standard conditions with a total barometric pressure of 100 kPa (29.5 in Hg), with a vapor pressure of 1 kPa (0.295 in Hg), and 25° C (77° F). Performance measured using fuel to EPA specifications in 40 CFR Part 1065 and EU specifications in Directive 97/68/EC with a density of 0.845-0.850 kg/L @ 15° C (7.05-7.09 lb/gal @ 59° F) and fuel inlet temperature 40° C (104° F).
All rating conditions are based on ISO/TR14396:2002, inlet air standard conditions with a total barometric pressure of 100 kPa (29.5 in Hg), with a vapor pressure of 1 kPa (0.295 in Hg), and 25° C (77° F). Performance measured using fuel to EPA specifications in 40 CFR Part 1065 and EU specifications in Directive 97/68/EC with a density of 0.845-0.850 kg/L @ 15° C (7.05-7.09 lb/gal @ 59° F) and fuel inlet temperature 40° C (104° F).
 
All rating conditions are based on ISO/TR14396:2002, inlet air standard conditions with a total barometric pressure of 100 kPa (29.5 in Hg), with a vapor pressure of 1 kPa (0.295 in Hg), and 25° C (77° F). Performance measured using fuel to EPA specifications in 40 CFR Part 1065 and EU specifications in Directive 97/68/EC with a density of 0.845-0.850 kg/L @ 15° C (59° F) and fuel inlet temperature 40° C (104° F).
All rating conditions are based on ISO/TR14396:2002, inlet air standard conditions with a total barometric pressure of 100 kPa (29.5 in Hg), with a vapor pressure of 1 kPa (0.295 in Hg), and 25° C (77° F). Performance measured using fuel to EPA specifications in 40 CFR Part 1065 and EU specifications in Directive 97/68/EC with a density of 0.845-0.850 kg/L @ 15° C (59° F) and fuel inlet temperature 40° C (104° F).
 
Power ratings apply at a rated speed of 2,050 rpm for HRC (Stage V) engine when tested under the reference conditions for the specified standard.
Power ratings apply at a rated speed of 2,050 rpm for HRC (Stage V) engine when tested under the reference conditions for the specified standard.
Note (3)
Engine derate will commence at an altitude of 4500 m (14,763.7 ft).
Engine derate will commence at an altitude of 4500 m (14,763.7 ft).
 
No engine derating required up to 3048 m (10,000 ft) for Tier 3 Engine and 1828 m (6,000 ft) for VR Engine.
No engine derating required up to 3048 m (10,000 ft) for Tier 3 Engine and 1828 m (6,000 ft) for VR Engine.
 
All rating conditions are based on ISO/TR14396, inlet air standard conditions with a total barometric pressure of 100 kPa (29.5 in Hg), with a vapor pressure of 1 kPa (0.295 in Hg), and 25° C (77° F). Performance measured using fuel to EPA specifications in 40 CFR Part 1065 and EU specifications in Directive 97/68/EC with a density of 0.845-0.850 kg/L @ 15° C (59° F) and fuel inlet temperature 40° C (104° F).
All rating conditions are based on ISO/TR14396, inlet air standard conditions with a total barometric pressure of 100 kPa (29.5 in Hg), with a vapor pressure of 1 kPa (0.295 in Hg), and 25° C (77° F). Performance measured using fuel to EPA specifications in 40 CFR Part 1065 and EU specifications in Directive 97/68/EC with a density of 0.845-0.850 kg/L @ 15° C (59° F) and fuel inlet temperature 40° C (104° F).
Engine Power - Tier 3 Engine - ISO 14396:2002
-
 
202 kW
271 HP
 
269 kW
361 HP
Engine Power - VR Engine - ISO 14396:2002
-
 
202 kW
271 HP
 
269 kW
361 HP
Note (4)
-
 
Optional Ventilation Reduction package available.
Optional Ventilation Reduction package available.
 
No engine derating required up to 2895 m (9,500 ft) altitude for Stage V engines, 3505 m (11,500 ft) altitude for Tier 3/Stage IIIA engines, and 3200 m (10,500 ft) for Tier 2/Stage II VR engines.
No engine derating required up to 2895 m (9,500 ft) altitude for Stage V engines, 3505 m (11,500 ft) altitude for Tier 3/Stage IIIA engines, and 3200 m (10,500 ft) for Tier 2/Stage II VR engines.
Note (5)
-
 
Optional engine with emissions equivalent to U.S. EPA Tier 3 and EU Stage IIIA is also available.
Optional engine with emissions equivalent to U.S. EPA Tier 3 and EU Stage IIIA is also available.
 
Optional Ventilation Reduction package available.
Optional Ventilation Reduction package available.
Engine Power - Stage V Engine - ISO 14396:2002
-
 
-
 
257 kW
345 HP
Note (6)
-
 
-
 
Optional engine with emissions equivalent to Tier 3 and Stage IIIA is also available.
Optional engine with emissions equivalent to Tier 3 and Stage IIIA is also available.
Note (7)
-
 
-
 
Optional engine meeting the U.S. EPA Tier 4 Final and EU Stage V emission standards is also available.
Optional engine meeting the U.S. EPA Tier 4 Final and EU Stage V emission standards is also available.
Nominal Payload Capacity
6800 kg
14991 lb
 
10200 kg
22487 lb
 
15000 kg
33069 lb
Gross Machine Mass
29702 kg
65482 lb
 
44204 kg
97453 lb
 
-
Static Tipping Load - Straight Ahead - Lift Arms Horizontal
20575 kg
45360 lb
 
25905 kg
57110 lb
 
37747 kg
83218 lb
Static Tipping Load - Full Turn - Lift Arms Horizontal
17870 kg
39397 lb
 
21803 kg
46067 lb
 
31586 kg
69635 lb
Breakout Force - SAE
12020 kg
26504 lb
 
-
 
-
Breakout Force - Tilt (ISO)
-
 
17928 kg
39524 lb
 
-
Breakout Force - Lift (ISO)
-
 
19202 kg
42333 lb
 
-
Gross Machine Mass - Loaded
-
 
-
 
62739 kg
138316 lb
Breakout Force - Lift and Tilt
-
 
-
 
24190 kg
53330 lb
Operating Mass*
20725 kg
45691 lb
 
30150 kg
66469 lb
 
43177 kg
95189 lb
Operating Mass* - Front Axle
7625 kg
16810 lb
 
12884 kg
28404 lb
 
17399 kg
38358 lb
Operating Mass* - Rear Axle
13100 kg
28881 lb
 
17266 kg
38065 lb
 
25778 kg
56831 lb
Operating Mass + Rated Payload*
27525 kg
60682 lb
 
40350 kg
88956 lb
 
58177 kg
128258 lb
Operating Mass + Rated Payload* - Front Axle
18645 kg
41105 lb
 
28128 kg
62011 lb
 
41464 kg
91412 lb
Operating Mass + Rated Payload* - Rear Axle
8880 kg
19577 lb
 
12222 kg
26944 lb
 
16713 kg
36846 lb
Note
*Calculated weights.
*Calculated weights.
 
*Calculated weights.
*Calculated weights.
 
*Calculated weights.
*Calculated weights.
Forward - 1
4.5 km/h
2.8 mile/h
 
4.5 km/h
2.8 mile/h
 
4.9 km/h
3 mile/h
Forward - 2
7.8 km/h
4.8 mile/h
 
9 km/h
5.6 mile/h
 
9.2 km/h
5.7 mile/h
Forward - 3
15 km/h
9.3 mile/h
 
16.8 km/h
10.4 mile/h
 
16.4 km/h
10.2 mile/h
Forward - 4
26.3 km/h
16.3 mile/h
 
27.5 km/h
17.1 mile/h
 
28.8 km/h
17.9 mile/h
Reverse - 1
4.5 km/h
2.8 mile/h
 
5 km/h
3.1 mile/h
 
5.9 km/h
3.7 mile/h
Reverse - 2
7.8 km/h
4.8 mile/h
 
11 km/h
6.8 mile/h
 
10.5 km/h
6.5 mile/h
Reverse - 3
14.8 km/h
9.2 mile/h
 
19 km/h
11.8 mile/h
 
18.7 km/h
11.6 mile/h
Reverse - 4
23 km/h
14.3 mile/h
 
29.3 km/h
18.2 mile/h
 
32.5 km/h
20.2 mile/h
Raise
5 s
5 s
 
7.6 s
7.6 s
 
6.8 s
6.8 s
Dump
2 s
2 s
 
1.6 s
1.6 s
 
3.3 s
3.3 s
Lower, Empty, Float Down
2.3 s
2.3 s
 
2 s
2 s
 
2.9 s
2.9 s
Total Cycle Time
9.3 s
9.3 s
 
11.2 s
11.2 s
 
13.2 s
13.2 s
Dump Bucket - 1
2.5 m³
3.2 yd³
 
4.2 m³
5.5 yd³
 
-
Dump Bucket - 2
2.8 m³
3.7 yd³
 
-
 
6.1 m³
8 yd³
Dump Bucket - 3 - Standard Bucket
3.1 m³
4.1 yd³
 
-
 
-
Dump Bucket - 4
3.4 m³
4.4 yd³
 
5.9 m³
7.7 yd³
 
7.2 m³
9.4 yd³
Ejector Bucket
2.4 m³
3.1 yd³
 
4.8 m³
6.3 yd³
 
5.8 m³
7.6 yd³
Bucket Capacities
-
 
4.2-5.9 m³ (5.5-7.7 yd³)
4.2-5.9 m³ (5.5-7.7 yd³)
 
5.7-8.6 m³ (7.5-11.2 yd³)
5.7-8.6 m³ (7.5-11.2 yd³)
Dump Bucket - 2 - Standard Bucket
-
 
4.8 m³
6.3 yd³
 
-
Dump Bucket - 3
-
 
5.6 m³
7.3 yd³
 
6.6 m³
8.6 yd³
Bolt Together Bucket
-
 
5.3 m³
6.9 yd³
 
-
Dump Bucket - 1 - Standard Bucket
-
 
-
 
5.7 m³
7.5 yd³
Dump Bucket - 5
-
 
-
 
7.5 m³
9.8 yd³
Dump Bucket - 6
-
 
-
 
8 m³
10.5 yd³
Light Material Bucket
-
 
-
 
8.6 m³
11.2 yd³
Bolt Together Bucket (1)
-
 
-
 
6.8 m³
8.9 yd³
Bolt Together Bucket (2)
-
 
-
 
7.5 m³
9.8 yd³
Outside Clearance Radius
5717 mm
225.1 in
 
-
 
6909 mm
272 in
Inner Clearance Radius
2825 mm
111.2 in
 
-
 
3139 mm
123.5 in
Axle Oscillation
10°
10°
 
10°
10°
 
8°
8°
Articulation Angle
42.5°
42.5°
 
42.5°
42.5°
 
44°
44°
Outside Clearance Radius*
-
 
6638 mm
261.3 in
 
-
Inner Clearance Radius*
-
 
3291 mm
129.6 in
 
-
Note
-
 
*Clearance dimensions are for reference only.
*Clearance dimensions are for reference only.
 
-
Tire Size
17.5 × R25
17.5 × R25
 
18 × R25
18 × R25
 
26.5R25
26.5R25
Engine Crankcase - With Filter
25 l
6.6 gal (US)
 
34 l
8.98 gal (US)
 
-
Transmission
45 l
11.9 gal (US)
 
47 l
12.4 gal (US)
 
-
Hydraulic Tank
88 l
23.2 gal (US)
 
125 l
33 gal (US)
 
135 l
35.7 gal (US)
Cooling System
67 l
17.7 gal (US)
 
61 l
16.1 gal (US)
 
75 l
19.8 gal (US)
Front Differential and Final Drives
38 l
10 gal (US)
 
80 l
21.1 gal (US)
 
-
Rear Differential and Final Drives
42 l
11.1 gal (US)
 
80 l
21.1 gal (US)
 
-
Fuel Tank
295 l
77.9 gal (US)
 
400 l
105.7 gal (US)
 
-
Secondary Fuel Tank - If Equipped
-
 
330 l
87.2 gal (US)
 
-
Engine Crankcase
-
 
-
 
37 l
9.8 gal (US)
Standards
ROPS/FOPS Certified Cab
ROPS/FOPS Certified Cab
 
ROPS/FOPS Certified Cab
ROPS/FOPS Certified Cab
Fuel System
486 l
128.4 gal (US)
DEF Tank
27 l
7.1 gal (US)
Front Differential and Final Drive
148 l
39 gal (US)
Rear Differential and Final Drive
141 l
37.2 gal (US)
Transmission
54 l
14.2 gal (US)
X
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