I retired effective 31 Jan 2010 as the Deputy Director of the 735 Supply Chain Management Group, part of the new Air Force Logistics Support Center, an AFMC organization.
1968-1969, A-1 Skyraider (Sandy, Spad)
From Year 1968
To Year 1969
Personal Memories
Not Specified
Image
A-1 Skyraider (Sandy, Spad) Details
Aircraft/Missile Information
Model Douglas AD-1 Skyraider Length 39.37 ft | 12.00 m Width 50.00 ft | 15.24 m Height 15.75 ft | 4.80 m Engine(s) 1 x Wright R-3350-24W air-cooled radial engine generating 2,500hp. Empty Weight 10,470 lbs | 4,749 kg MTOW 18,029 lbs | 8,178 kg Max Speed 321 mph | 517 km/h | 279 kts Max Range 1,553 miles | 2,500 km Ceiling 26,001 ft | 7,925 m | 4.9 miles Climb Rate 2,300 ft/min (701.4 m/min) Hardpoints 14 Armament 4 x 20mm Cannons 12 x Rockets
7,000 pounds of external ordnance including bombs and gun pods. Accommodations 1
* AD-5 - Anti-Submarine Model of which 212 produced; two crew-seating in side-by-side configuration; widened fuselage. * AD-6 - Improved AD-4B versions; improved low-level bombing capability; 713 produced. * AD-7 - AD-6 version fitted with R-3350-26WB and reinforced substructure of which 73 were produced in total in this way. * A-1E - AD-5 Redesignated from 1962 standard onwards. * A-1H - AD-6 Redesignated from 1962 standard onwards. * A-1J - AD-7 Redesignated from 1962 standard onwards.
