Width/Span
100.0 ft
(30.48 m)
Empty Wgt
41,548 lb
(18,846 kg)
MTOW
79,999 lb
(36,287 kg)
Wgt Diff
+38,451 lb
(+17,441 kg)
(Showcased structural values pertain to the Lockheed P2V-4 Neptune production variant)
Installed:
2 x Wright R-3350-30W superchargered piston engines developing 3,250 horsepower each.
Max Speed
314 mph
(505 kph | 273 kts)
Ceiling
24,698 ft
(7,528 m | 5 mi)
Range
2,807 mi
(4,518 km | 8,367 nm)
Rate-of-Climb
1,100 ft/min
(335 m/min)
♦ MACH Regime (Sonic)
Sub
Trans
Super
Hyper
HiHyper
ReEntry
RANGES (MPH) Subsonic: <614mph | Transonic: 614-921 | Supersonic: 921-3836 | Hypersonic: 3836-7673 | Hi-Hypersonic: 7673-19180 | Reentry: >19030
(Showcased performance specifications pertain to the Lockheed P2V-4 Neptune production variant. Performance specifications showcased above are subject to environmental factors as well as aircraft configuration. Estimates are made when Real Data not available. Compare this aircraft entry against any other in our database or View aircraft by powerplant type)
STANDARD:
6 x 20mm M-24 cannons in nose
2 x 12.7mm machine guns (on deck)
2 x 20mm M-24 cannons in tail
OPTIONAL:
Mission-Specific Armament can include the following (all ordnance held in internal bay unless noted). Maximum bombload capacity of 4,800 lbs:
6 x 100lb bombs
6 x 500lb bombs
4 x 1,000lb bombs
2 x 2,000lb mines
2 x 1,600lb bombs
4 x Mk 24 mines
4 x Mk 34 mines
4 x 1,200lb torpedoes
2 x A.R. 11.75 inch
16 x HVAR 5 inch rockets (underwing)
(Not all ordnance types may be represented in the showcase above)
Hardpoint Mountings: 16 (for underwing rockets)
Ribbon graphics not necessarily indicative of actual historical campaign ribbons. Ribbons are clickable to their respective aerial campaigns / operations / aviation periods.