Lockheed CP-140 Aurora vs Utva Lasta: Specs Compared

Lockheed CP-140 Aurora — licensed reference photograph

ATrainer aircraft

Lockheed CP-140 Aurora

Maritime patrol aircraft (CP-140) MPA trainer aircraft (CP-140A)

Credit

Ken Mist · CC BY-SA 2.0 · Resized · CC BY-SA 2.0 · Source ↗ · Modified

Utva Lasta — licensed reference photograph

BTrainer aircraft

Utva Lasta

Trainer aircraft

Credit

Srđan Popović · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified

First system

Second system

At a glance

Side by side

Length comparisonOne shared metre scale

Lockheed CP-140 AuroraCP-140 Aurora · Length

35.61 m

Length source ↗

Utva LastaLasta 95N · Length

7.965 m

Length source ↗

Lengths retain their source configuration and measurement scope.

Measured figures

Head to head

20 of 43 rows sourced on both sides

35.61mCP-140 Aurora · Length

7.97mLasta 95N · Length

LengthScopes differ

All recorded figures & sources

35.61 m

CP-140 Aurora · Length

Single source

35.61 m

CP-140 · Length

Single source

116 ft 10 in (35.61 m)^[source]

35.61 m^[source]CP-140 Aurora

7.965 m

Lasta 95N · Length

Single source

7.965 m (26 ft 2 in)^[source]

30.38mCP-140 · Wingspan

9.7mLasta 95N · Wingspan

WingspanScopes differ

All recorded figures & sources

30.37 m

CP-140 Aurora · Wingspan

Single source

30.38 m

CP-140 · Wingspan

Single source

99 ft 8 in (30.38 m)^[source]

30.37 m^[source]CP-140 Aurora

9.7 m

Lasta 95N · Wingspan

Single source

9.7 m (31 ft 10 in)^[source]

10.3mCP-140 Aurora · Height

2.84mLasta 95N · Height

HeightScopes differ

All recorded figures & sources

10.3 m

CP-140 Aurora · Height

Single source

10.274 m

CP-140 · Height

Single source

33 ft 8.5 in (10.274 m)^[source]

10.30 m^[source]CP-140 Aurora

2.84 m

Lasta 95N · Height

Single source

2.84 m (9 ft 4 in)^[source]

64.4t

1.2tMaximum take-off; Lasta 95N · unarmed

MassScopes differ

All recorded figures & sources

64,410 kg

Gross; CP-140 Aurora · Gross weight · Maximum gross weight

Single source

27,833 kg

Gross; CP-140 · Gross weight

Single source

61,362 lb (27,833 kg)^[source]

64,410 kg^[source]CP-140 Aurora · Maximum gross weight

888 kg

Empty; Lasta 95N · Empty weight

Single source

1,145 kg

Gross; Lasta 95N · Gross weight

Single source

Mission minimum 8, typically 12 to 15

2Lasta 95N · Crew

Crew

All recorded figures & sources

Mission minimum 8, typically 12 to 15^[source]

2 people

Lasta 95N · Crew

Single source

2^[source]

750km/h

345km/hMaximum; Lasta 95N · Maximum speed

SpeedScopes differ

All recorded figures & sources

750 km/h

Maximum; CP-140 Aurora · Maximum speed · Maximum speed

Single source

694 km/h

Maximum; CP-140 · below cruise ceiling

Single source

375 kn (432 mph, 694 km/h) below cruise ceiling^[source]

750 km/h^[source]CP-140 Aurora · Maximum speed

280 km/h

Cruise; Lasta 95N · Cruise speed

Single source

345 km/h

Maximum; Lasta 95N · Maximum speed

Single source

9,300kmCP-140 · Range

1,160kmFerry; Lasta 95N · Ferry range

RangeScopes differ

All recorded figures & sources

7,400 km

CP-140 Aurora · Range

Single source

9,300 km

CP-140 · Range

Single source

5,000 nmi (5,800 mi, 9,300 km)^[source]

7,400 km^[source]CP-140 Aurora

1,160 km

Ferry; Lasta 95N · Ferry range

Single source

1,160 km

Lasta 95N · Range

Single source

3,661kW

232kW

PowerScopes differ

All recorded figures & sources

3,661 kW

CP-140 · 4 × Allison T56-A-14-LFE turboprop engines each

Single source

4 × Allison T56-A-14-LFE turboprop engines, 4,909 hp (3,661 kW) each^[source]

232 kW

Lasta 95N · 1 × Lycoming AEIO-580-B1A 6-cyl. air-cooled horizontally-opposed piston engine

Single source

1 × Lycoming AEIO-580-B1A 6-cyl. air-cooled horizontally-opposed piston engine, 232 kW (311 hp)^[source]

120m²CP-140 · Wing area

12.9m²Lasta 95N · Wing area

Wing areaScopes differ

All recorded figures & sources

120 m²

CP-140 · Wing area

Single source

1,300 sq ft (120 m 2 )^[source]

12.9 m²

Lasta 95N · Wing area

Single source

12.9 m 2 (139 sq ft)^[source]

8.2h

—

Endurance

All recorded figures & sources

8.2 h

CP-140 · on station at 1,000 nmi (1,151 mi; 1,852 km) radius

Single source

8 hours 12 minutes on station at 1,000 nmi (1,151 mi; 1,852 km) radius^[source]

10,700mCP-140 · Service ceiling

6,000mLasta 95N · Service ceiling

Service ceilingScopes differ

All recorded figures & sources

10,700 m

CP-140 · Service ceiling

Single source

35,100 ft (10,700 m)^[source]

6,000 m

Lasta 95N · Service ceiling

Single source

6,000 m (20,000 ft)^[source]

2.2t

—

Payload

All recorded figures & sources

277–1,111 kg

CP-140 · Hardpoints: 8 in weapons bay; 10 under-wing from capacity with a capacity of

Single source

2,177 kg

CP-140 · total in weapons bay, with provisions to carry combinations of

Single source

Hardpoints: 8 in weapons bay; 10 under-wing from 611 to 2,450 lb (277 to 1,111 kg) capacity with a capacity of 4,800 lb (2,177 kg) total in weapons bay, with provisions to carry combinations of:^[source]

—

8.5m/sLasta 95N · 1,670 ft/min

Rate of climb

All recorded figures & sources

8.5 m/s

Lasta 95N · 1,670 ft/min

Single source

8.5 m/s (1,670 ft/min)^[source]

Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.

Configuration

Details

Lockheed CP-140 Aurora and Utva Lasta configuration
Specification	Lockheed CP-140 Aurora	Utva Lasta
Type	Maritime patrol aircraft (CP-140) MPA trainer aircraft (CP-140A)^[source]	Trainer aircraft^[source]
Manufacturer	Lockheed Corporation^[source]	Utva Aviation Industry^[source]
Status	Active (CP-140M only)^[source]	In service^[source]
Primary user	Royal Canadian Air Force^[source]	—
Number built	21 (18 CP-140M + 3 CP-140A)^[source]	37^[source]
Introduction date	1980^[source]	2010^[source]
First flight	22 March 1979 (CP-140)^[source]	Lasta 1 prototype: 2 September 1985 Lasta 95: 26 February 2009^[source]
Retired	2011 (CP-140A only)^[source]	—
Developed from	Lockheed P-3 Orion^[source]	—
Fuel capacity	7,661 imp gal (9,200 US gal; 34,828 L) usable fuel in one fuselage tank and four wing integral tanks^[source]	—
Hardpoints	8 in weapons bay; 10 under-wing from 611 to 2,450 lb (277 to 1,111 kg) capacity with a capacity of 4,800 lb (2,177 kg) total in weapons bay, with provisions to carry combinations of: Other: signal chargers, smoke markers , illumination flares^[source]	2 with a capacity of 100 kg (220 lb) bombs, 7.62 mm (0.300 in) or 12.7 mm (0.500 in) calibre machine-gun pods or 57 mm (2.244 in) rocket pods (7 rockets each)^[source]
Aspect ratio	7.5^[source]	6.3^[source]
Airfoil	root: NACA 0014 (modified) ; tip: NACA 0012 (modified)^[source]	—
Propellers	4-bladed Hamilton Standard 54H60, 13 ft 6 in (4.11 m) diameter constant-speed fully-feathering reversible-pitch propellers^[source]	2-bladed HARTZELL HC-C2YR-4CF/FC 8475-8 constant speed propeller, 1.98 m (6 ft 6 in) diameter^[source]
Maximum transit speed	395 kn (455 mph; 732 km/h) at optimum altitude^[source]	—
FAR balanced field length	7,900 ft (2,408 m)^[source]	—
Take-off distance to 50 ft (15 m)	6,000 ft (1,829 m)^[source]	—
Landing distance from 50 ft (15 m)	3,200 ft (975 m) at 114,000 lb (51,710 kg) landing weight^[source]	—
Other	signal chargers, smoke markers , illumination flares^[source]	—
Rockets	air-to-surface rockets can be fitted after a minor retrofit.^[source]	—
Bombs	Mk 46 Mod V torpedoes, conventional bombs^[source]	—
Country of origin	United States^[source] United States^[source]	Serbia^[source]
Designer	—	Military Technical Institute^[source]
Primary users	—	Serbian Air Force Iraqi Air Force^[source]
Stall speed	—	95 km/h (59 mph, 51 kn)^[source]
Never exceed speed	—	425 km/h (264 mph, 229 kn)^[source]
g limits	—	+6 -3 g^[source]
Reported operators	—	Reported operator · Iraq Reported operator · Serbia

FORCETALLY

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Lockheed CP-140 Aurora

Utva Lasta

Type

Maritime patrol aircraft (CP-140) MPA trainer aircraft (CP-140A)^[source]

Trainer aircraft^[source]

Manufacturer

Lockheed Corporation^[source]

Utva Aviation Industry^[source]

Status

Active (CP-140M only)^[source]

In service^[source]

Primary user

Royal Canadian Air Force^[source]

—

Number built

21 (18 CP-140M + 3 CP-140A)^[source]

37^[source]

Introduction date

1980^[source]

2010^[source]

First flight

22 March 1979 (CP-140)^[source]

Lasta 1 prototype: 2 September 1985 Lasta 95: 26 February 2009^[source]

Retired

2011 (CP-140A only)^[source]

—

Developed from

Lockheed P-3 Orion^[source]

—

Fuel capacity

7,661 imp gal (9,200 US gal; 34,828 L) usable fuel in one fuselage tank and four wing integral tanks^[source]

—

Hardpoints

8 in weapons bay; 10 under-wing from 611 to 2,450 lb (277 to 1,111 kg) capacity with a capacity of 4,800 lb (2,177 kg) total in weapons bay, with provisions to carry combinations of: Other: signal chargers, smoke markers , illumination flares^[source]

2 with a capacity of 100 kg (220 lb) bombs, 7.62 mm (0.300 in) or 12.7 mm (0.500 in) calibre machine-gun pods or 57 mm (2.244 in) rocket pods (7 rockets each)^[source]

Aspect ratio

7.5^[source]

6.3^[source]

Airfoil

root: NACA 0014 (modified) ; tip: NACA 0012 (modified)^[source]

—

Propellers

4-bladed Hamilton Standard 54H60, 13 ft 6 in (4.11 m) diameter constant-speed fully-feathering reversible-pitch propellers^[source]

2-bladed HARTZELL HC-C2YR-4CF/FC 8475-8 constant speed propeller, 1.98 m (6 ft 6 in) diameter^[source]

Maximum transit speed

395 kn (455 mph; 732 km/h) at optimum altitude^[source]

—

FAR balanced field length

7,900 ft (2,408 m)^[source]

—

Take-off distance to 50 ft (15 m)

6,000 ft (1,829 m)^[source]

—

Landing distance from 50 ft (15 m)

3,200 ft (975 m) at 114,000 lb (51,710 kg) landing weight^[source]

—

Other

signal chargers, smoke markers , illumination flares^[source]

—

Rockets

air-to-surface rockets can be fitted after a minor retrofit.^[source]

—

Bombs

Mk 46 Mod V torpedoes, conventional bombs^[source]

—

Country of origin

United States^[source]

Serbia^[source]

Designer

—

Military Technical Institute^[source]

Primary users

—

Serbian Air Force Iraqi Air Force^[source]

Stall speed

—

95 km/h (59 mph, 51 kn)^[source]

Never exceed speed

—

425 km/h (264 mph, 229 kn)^[source]

g limits

—

+6 -3 g^[source]

Reported operators

—

Reported operator · Iraq
Reported operator · Serbia