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Military


P2V-5 (P-2) Neptune

Specifications
Propulsion Two Wright R-3350-30WA engines
Length 91 ft 2 in
Height 28 ft 1 in
Wing Area1,000 sq ft
Span104 ft
Tread25 ft 11 in
M.A.C.10 ft 6 in
Weight
   Empty
   Basic
   Design
   Combat
   Max T.O.
   Max Overload Landing
43,000
44,900
67,500
61,320
80,000
62,000
Ordnance
   Guns



   Fire Control

   Bombs and Rockets
2 x 20mm in the Nose with 800 rds.
2 x 20 mm in the Tail with 800 rds.
2 x .50 cal. on the deck with 800 rds.

Mk. 15 Mod. 6

16-Aero 14B-2 rocket launcher (max. cap. 500 lbs. each) on alternate outer wing slats.
Torpedoes, Mines and Bombs carried in the fuselage.
Max Load Capacity of 12,000 lbs
Electronics
   Interphone
   Radio Transm
   Comm. Rec
   Liaison Rec.
   UHF
   VHF
   Indicator
   Direct Finder
   Radio Altimeter
   Marker Beacon
   Loran
   IFF Equipment
   ECM
   Sonobuoy Rec.
   Grd. Pos. Ind
   M.A.D.
   D.M.E.
   Search Radar
   ECM-Dir. Find
   Omn. Dir. Find
   Radar Bomb
AN/AIC-5B
AN/ART-13
AN/ARC-5
AN/ARP-15A
AN/ARC-27
AN/ARC-1
AN/APA-81
AN/ARN-6
AN/APN-22
AN/APN-12
AN/APN-70
AN/APX-6, AN/APX-7
AN/APA-9B, AN/APA-11
AN/ARR-26
AN/APA-57B
AN/ASQ-8
AN/ARN-21
AN/APS-20B
AN/APA-69
AN/ARN-14A (P.S.I.), AN/APS/20C (P.S.I.), AN/APS-31
AN/APS-16
First FlightDecember 1951
Service UseSeptember 1951



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