Underground - Hard Rock

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R2900G
UNITS:
Metric
Imperial
Engine Model
Cat® C15
Cat® C15
 
Cat® C15
Cat® C15
 
Cat® 3306B DITA
Cat® 3306B DITA
Engine Power - Tier 3 Engine - ISO 14396:2002
299 kW
401 HP
 
299 kW
401 HP
 
-
Engine Power - VR Engine - ISO 14396:2002
299 kW
401 HP
 
299 kW
401 HP
 
-
Bore
137.2 mm
5.4 in
 
137.2 mm
5.4 in
 
120.7 mm
4.75 in
Stroke
171.5 mm
6.8 in
 
171.5 mm
6.8 in
 
152.4 mm
6 in
Displacement
15.2 l
927.9 in³
 
15.2 l
927.6 in³
 
10.5 l
640.75 in³
Note (1)
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 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 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.
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/TR 14396:2002, 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/TR 14396:2002, 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 (7.05-7.09 lb/gal @ 59° F) and fuel inlet temperature 40° C (104° F).
Note (3)
No engine derating required up to 591 m (1,938 ft) altitude.
No engine derating required up to 591 m (1,938 ft) altitude.
 
No engine derating required up to 3050 m (10,006 ft) altitude for equivalent Tier 3 engines, and 3506 m (11,502 ft) for VR engines.
No engine derating required up to 3050 m (10,006 ft) altitude for equivalent Tier 3 engines, and 3506 m (11,502 ft) for VR engines.
 
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).
Note (4)
Optional Ventilation Reduction Package available.
Optional Ventilation Reduction Package available.
 
Optional Ventilation Reduction package available.
Optional Ventilation Reduction package available.
 
-
Note (5)
Optional Tier 3 engine package emits equivalent to U.S. EPA Tier 3 and EU Stage IIIA.
Optional Tier 3 engine package emits equivalent to U.S. EPA Tier 3 and EU Stage IIIA.
 
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.
 
-
Engine Power - ISO 14396:2002
-
 
-
 
117 kW
157 HP
Nominal Payload Capacity
17200 kg
37920 lb
 
20000 kg
44092 lb
 
6800 kg
14991 lb
Gross Machine Mass
70350 kg
155095 lb
 
82000 kg
180779 lb
 
29702 kg
65482 lb
Static Tipping Load - Straight Ahead - Lift Arms Horizontal
39923 kg
88015 lb
 
47264 kg
104199 lb
 
20575 kg
45360 lb
Static Tipping Load - Full Turn - Lift Arms Horizontal
34069 kg
75109 lb
 
-
 
17870 kg
39397 lb
Breakout Force - SAE
27346 kg
60298 lb
 
28020 kg
61773 lb
 
12020 kg
26504 lb
Static Tipping Full Turn Ahead Lift Arms Horizontal
-
 
40003 kg
88191 lb
 
-
Operating Mass*
50209 kg
110692 lb
 
58263 kg
128448 lb
 
20725 kg
45691 lb
Operating Mass* - Front Axle
23057 kg
50832 lb
 
24747 kg
54558 lb
 
7625 kg
16810 lb
Operating Mass* - Rear Axle
27152 kg
59860 lb
 
33499 kg
73853 lb
 
13100 kg
28881 lb
Operating Mass + Rated Payload*
67409 kg
148611 lb
 
78263 kg
172540 lb
 
27525 kg
60682 lb
Operating Mass + Rated Payload* - Front Axle
50220 kg
110716 lb
 
56784 kg
125187 lb
 
18645 kg
41105 lb
Operating Mass + Rated Payload* - Rear Axle
17189 kg
37895 lb
 
21462 kg
47316 lb
 
8880 kg
19577 lb
Note
*Calculated Weight.
*Calculated Weight.
 
*Calculated weight.
*Calculated weight.
 
*Calculated weights.
*Calculated weights.
Forward - 1
5.4 km/h
3.4 mile/h
 
4.9 km/h
3 mile/h
 
4.5 km/h
2.8 mile/h
Forward - 2
9.7 km/h
6 mile/h
 
9.1 km/h
5.7 mile/h
 
7.8 km/h
4.8 mile/h
Forward - 3
17.3 km/h
10.7 mile/h
 
16.4 km/h
10.2 mile/h
 
15 km/h
9.3 mile/h
Forward - 4
29.8 km/h
18.5 mile/h
 
28.2 km/h
17.5 mile/h
 
26.3 km/h
16.3 mile/h
Reverse - 1
6.6 km/h
4.1 mile/h
 
6.6 km/h
4.1 mile/h
 
4.5 km/h
2.8 mile/h
Reverse - 2
11.8 km/h
7.3 mile/h
 
11.5 km/h
7.1 mile/h
 
7.8 km/h
4.8 mile/h
Reverse - 3
21 km/h
13 mile/h
 
20.5 km/h
12.7 mile/h
 
14.8 km/h
9.2 mile/h
Reverse - 4
35.5 km/h
22 mile/h
 
31.3 km/h
19.4 mile/h
 
23 km/h
14.3 mile/h
Raise
9.2 s
9.2 s
 
8.8 s
8.8 s
 
5 s
5 s
Dump
3.4 s
3.4 s
 
1.85 s
1.85 s
 
2 s
2 s
Lower, Empty, Float Down
3.1 s
3.1 s
 
3.54 s
3.54 s
 
2.3 s
2.3 s
Total Cycle Time
15.7 s
15.7 s
 
14.2 s
14.2 s
 
9.3 s
9.3 s
Bucket Capacity
6.3-8.9 m³ (8.2-11.6 yd³)
6.3-8.9 m³ (8.2-11.6 yd³)
 
-
 
-
Dump Bucket - 1
6.3 m³
8.2 yd³
 
-
 
2.5 m³
3.2 yd³
Dump Bucket - 2
7.2 m³
9.4 yd³
 
9.5 m³
12.4 yd³
 
2.8 m³
3.7 yd³
Dump Bucket - 3
8.3 m³
10.9 yd³
 
10.5 m³
13.7 yd³
 
-
Dump Bucket - 4
8.9 m³
11.6 yd³
 
-
 
3.4 m³
4.4 yd³
Bucket Capacities
-
 
8.9-11.6 m³ (11.6-15.2 yd³)
8.9-11.6 m³ (11.6-15.2 yd³)
 
-
Dump Bucket - 1 - Standard Bucket
-
 
8.9 m³
11.6 yd³
 
-
Light Material Bucket
-
 
11.6 m³
15.2 yd³
 
-
Dump Bucket - 3 - Standard Bucket
-
 
-
 
3.1 m³
4.1 yd³
Ejector Bucket
-
 
-
 
2.4 m³
3.1 yd³
Outside Clearance Radius
7323 mm
288.3 in
 
-
 
5717 mm
225.1 in
Inner Clearance Radius
3383 mm
133.2 in
 
-
 
2825 mm
111.2 in
Axle Oscillation
 
8 °
8 °
 
10°
10°
Articulation Angle
42.5°
42.5°
 
42.5 °
42.5 °
 
42.5°
42.5°
Outside Clearance Radius**
-
 
7536 mm
296.7 in
 
-
Inner Clearance Radius**
-
 
3247 mm
127.8 in
 
-
Note
-
 
**Clearance dimensions are for reference only.
**Clearance dimensions are for reference only.
 
-
Tire Size
29.5 × 29
29.5 × 29
 
35/65 R33
35/65 R33
 
17.5 × R25
17.5 × R25
Engine Crankcase
34 l
9 gal (US)
 
34 l
9 gal (US)
 
-
Transmission
62 l
16.4 gal (US)
 
62 l
16.4 gal (US)
 
45 l
11.9 gal (US)
Hydraulic Tank
140 l
37 gal (US)
 
140 l
37 gal (US)
 
88 l
23.2 gal (US)
Cooling System
75 l
19.8 gal (US)
 
75 l
19.8 gal (US)
 
67 l
17.7 gal (US)
Front Differential and Final Drives
119 l
31.4 gal (US)
 
119 l
31.4 gal (US)
 
38 l
10 gal (US)
Rear Differential and Final Drives
127 l
33.5 gal (US)
 
127 l
33.5 gal (US)
 
42 l
11.1 gal (US)
Front Differential and Final Drives - With Axle Oil Cooling System
159 l
42 gal (US)
 
159 l
42 gal (US)
 
-
Rear Differential and Final Drives - With Axle Oil Cooling System
167 l
44.1 gal (US)
 
167 l
44.1 gal (US)
 
-
Fuel Tank - Dual
1425 l
376.4 gal (US)
 
-
 
-
Fuel Tank
-
 
1539 l
406.5 gal (US)
 
295 l
77.9 gal (US)
Engine Crankcase - With Filter
-
 
-
 
25 l
6.6 gal (US)
Brakes
ISO 3450, AS2958.1, CAN-CSA424.30-M90
ISO 3450, AS2958.1, CAN-CSA424.30-M90
 
-
 
-
Cab - FOPS
ISO 3449, SAE J231, AS2294.3, EN13627
ISO 3449, SAE J231, AS2294.3, EN13627
 
-
 
-
Cab - ROPS
ISO 3471, SAE J1040, AS2294.2, EN13510
ISO 3471, SAE J1040, AS2294.2, EN13510
 
-
 
-
Standards
-
 
Rollover Protective Structure (ROPS)/Falling Object Protective Structure (FOPS) Certified Cab
Rollover Protective Structure (ROPS)/Falling Object Protective Structure (FOPS) Certified Cab
 
ROPS/FOPS Certified Cab
ROPS/FOPS Certified Cab
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