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Douglas TA-4B 'Skyhawk'

Description
Notes: Small, SINGLE-SEAT, delta wing, CARRIER-BASED, attack aircraft with tricycle landing gear and inflight refueling capability.
  Manufacturer:Douglas
  Base model:A-4
  Designation:TA-4
  Version:B
  Nickname:Skyhawk
  Designation System:U.S. Tri-Service
  Designation Period:1962-Present
  Basic role:Attack
  Modified Mission:Trainer
  First Flew:1954/06/22
  See Also:

Specifications
  Length: 39' 4" 11.9 m
  Height:15' 4.5 m
  Wingspan: 27' 6" 8.3 m
  Wingarea: 260.0 sq ft 24.1 sq m
  Empty Weight: 9,853 lb 4,468 kg

Propulsion
  No. of Engines: 1
  Powerplant: Wright J65-W-16A
  Thrust (each): 7,800 lb 3,537 kg

Performance
  Range: 700 miles 1,127 km
  Max Speed: 675 mph 1,086 km/h 587 kt
  Ceiling: 47,900 ft 14,599 m


 

Recent comments by our visitors
 James Frederick
 Chicago, IL
As a ADJ-2, during the mid-60's, I was assigned as petty officer in charge of the flight test office at NARF Jacksonville, FL. We were the first group of Navy airmen to receive air crew wings in the TA-4's, flying back seat during test flights out of rework. Our test pilots were returning Viet Nam combat pilots, so things were a little "loose" to say the least. We all got plenty of stick time and I was even allowed to get in some touch and goes. Our group also flew back seat in RA5C's, no flight controls in the rear seat but one hell of a ride.

I would very much like to hear from anyone assigned to NARF Jacksonville during the 60's. I know you are out there - jimf@loebequipment.com
03/24/2009 @ 11:45 [ref: 24006]