====== A-4 Specs ======

From book NAVAIR 01-40AVF-1 - "Supplement to NATOPS Flight Manual Navy Model A-4E/F International Model A-4G AIRCRAFT"

^Engine Thrust|9300 pounds sea-level static thrust|
^Engine Type|P&WA J52-P-8A (for A-4E/F)|
^Aircraft Weight|For Field landing, maximum 14,500 pounds|