Boyle, Clarence Edward, Jr., 1st Lt

Fallen
 
 Service Photo   Service Details
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Last Rank
First Lieutenant
Last Primary AFSC/MOS
AAF MOS 1051-Pilot - Two-Engine
Last AFSC Group
Pilot (Officer)
Primary Unit
1951-Present, Status - POW/MIA
Service Years
1944 - 1951
Officer srcset=
First Lieutenant

 Last Photo   Personal Details 

37 kb


Home State
California
California
Year of Birth
1922
 
This Military Service Page was created/owned by Sgt Duane Kimbrow (Skip) to remember Boyle, Clarence Edward, Jr., 1st Lt.

If you knew or served with this Airman and have additional information or photos to support this Page, please leave a message for the Page Administrator(s) HERE.
 
Casualty Info
Home Town
Westwood Village/Santa Monica, CA
Last Address
Pusan-East AB, South Korea



Casualty Date
Jul 01, 1951
 
Cause
MIA-Finding of Death
Reason
Air Loss, Crash - Sea
Location
Korea, North
Conflict
Korean War
Location of Interment
Arlington National Cemetery (VLM) - Arlington, Virginia

 Official Badges 




 Unofficial Badges 




 Military Associations and Other Affiliations
National Cemetery Administration (NCA)Korean War Fallen
  1951, National Cemetery Administration (NCA)
  1951, Korean War Fallen


 1948-1949, P-61 Black Widow
From Year
1948
To Year
1949
   
Personal Memories
Not Specified
   
Image
 P-61 Black Widow Details
 


Aircraft/Missile Information
General characteristics

* Crew: 2-3 (pilot, radar operator, optional gunner)
* Length: 49 ft 7 in (15.11 m)
* Wingspan: 66 ft 0 in (20.12 m)
* Height: 14 ft 8 in (4.47 m)
* Wing area: 662.36 ft² (61.53 m²)
* Empty weight: 23,450 lb (10,637 kg)
* Loaded weight: 29,700 lb (13,471 kg)
* Max takeoff weight: 36,200 lb (16,420 kg)
* Powerplant: 2× Pratt & Whitney R-2800-65W Double Wasp radial engines, 2,250 hp (1,680 kW) each
* Propellers: four-bladed Curtiss Electric propeller, 1 per engine
o Propeller diameter: 146 in (3.72 m)
*

* Main wheel track: 17 ft 2 in (5.24 m)
* Fuel capacity:
o Internal: 640 US gal (2,423 L) of AN-F-48 100/130-octane rating gasoline
o External: Up to four 165 US gal (625 L) or 310 US gal (1,173 L) tanks under the wings
* Oil capacity: 22 US gal (83.3 L) of AN-0-8 oil per engine

Performance

* Maximum speed: 318 knots (366 mph, 589 km/h) at 20,000 ft (6,095 m)
* Combat range: 530 nm (610 mi, 982 km)
* Ferry range: 1,650 nm (1,900 mi, 3,060 km) with four external fuel tanks
* Service ceiling 33,100 ft (10,600 m)
* Rate of climb: 2,540 ft/min (12.9 m/s)
* Wing loading: 45 lb/ft² (219 kg/m²)
* Power/mass: 0.15 hp/lb (25 W/kg)
* Time to altitude: 12 min to 20,000 ft (6,100 m) (1,667fpm)

Armament

* Guns:
o 4× 20 mm Hispano M2 cannon in ventral fuselage, 200 rounds per gun
o 4× 0.50 cal (12.7 mm) Browning M2 machine guns in upper turret, 560 rounds per gun
* Bombs: for ground attack, four bombs of up to 1,600 lb (726 kg) each or six 5 inch (127 mm) HVAR unguided rockets could be carried under the wings. Some aircraft could also carry one 1,000 lb (454 kg) bomb under the fuselage.

Avionics

* SCR-720 (AI Mk.X) search radar
* SCR-695 tail warning radar




   
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Last Updated: Feb 6, 2012
   
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  9 Also There at This Aircraft:
 
  • Lucero, Verne, Sgt, (1947-1950)
  • Piraino, Francis, TSgt, (1948-1956)
  • Rima, Merton, MSgt, (1947-1977)
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