This Military Service Page was created/owned by
SSgt Robert Bruce McClelland, Jr.
to remember
O'Neill, Eugene Walter, Jr., Col USAF(Ret).
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Contact Info
Home Town Jersey City, NJ; Cincinnati, OH; Long Island, NY
Last Address Miami, Florida
Date of Passing Aug 30, 1998
Location of Interment Arlington National Cemetery (VLM) - Arlington, Virginia
The President of the United States of America, authorized by Act of Congress July 9, 1918, takes pleasure in presenting the Silver Star to Captain (Air Corps) Eugene W. O'Neill, Jr. (ASN: 0-432203), United States Army Air Forces, for gallantry in action while serving as a Pilot of the 62d Fighter Squadron, 56th Fighter Group, EIGHTH Air Force, while leading a Flight of P-47 fighter aircraft furnishing support for bombers withdrawing from a mission over Germany, 26 November 1943. As rendezvous was made with the bombers, a large force of rocket-carrying aircraft were observed preparing to attack the formation. In a furious aerial battle which ensued, Captain O'Neill engaged and destroyed one of the enemy planes, pressing his attack so close that pieces of the disintegrating plane damaged his own aircraft, knocking off a portion of the wing tip and damaging the tail assembly. In spite of this, Captain O'Neill, thinking only of the safety of the bombers, attacked and destroyed another enemy fighter that was vigorously attacking a straggling bomber. The gallantry, aggressive fighting spirit and exceptional skill displayed by Captain O'Neill contributed in a large measure to the successful withdrawal of the bomber formation.
General Orders: Headquarters, 8th Air Force, General Orders No. 263 (April 10, 1944)
Aircraft/Missile Information
Model Curtiss P-40N / Kittyhawk IV Length 33.46 ft | 10.20 m Width 37.47 ft | 11.42 m Height 12.37 ft | 3.77 m Engine(s) 1 x Allison V-1710--81 inline piston engine generating 1,360hp. Empty Weight 6,005 lbs | 2,724 kg MTOW 8,858 lbs | 4,018 kg Max Speed 378 mph | 609 km/h | 329 kts Max Range 240 miles | 386 km Ceiling 38,156 ft | 11,630 m | 7.2 miles Climb Rate 2,142.86 ft/min (653 m/min) Hardpoints 1 Armament 6 x 12.7mm machine guns 1 x 500lb bomb under fuselage Accommodations 1
Major Variants
* Model 75I - Prototype Base Model derived from XP-37A airframe fitted with Allison 1,150hp V-1710-11 inline engine. * P-40 - United States Army Air Corps production version fitted with V-1710-33 powerplant. * Hawk 81-A1 - Export model for French use. * P-40B - Improved model featuring improved armor and armament with seal-sealing fuel tanks. * P-40C - Additional 2 x 12.7mm machine guns added to wings; improved seal-sealing fuel tanks. * P-40D - Fitted with V-1710-39 generating 1,150hp; increase performance at high altitude; improved supercharger. * P-40E - Only 4 x 12.7mm machine guns in wings. * P-40F - Improved supercharger. * P-40L - Similar to the P-40F with improved supercharger and 1,300hp Packard V-1650-1 (license-built 1,300hp Rolls-Royce Merlin) powerplant. * P-40K - Based on the P-40E model with V-1710-33 powerplant. * P-40M - Fitted with V-1710-71 powerplant. * P-40N - Fitted with V-1710-81 OR V1710-99 OR V1710-115 powerplants; improved performance capabilities; decreased overall weight.