Douglas A-4M - Page 19

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Sectio n XI
Part 2
MAXIMUM TAKEOFF WEIGHT
HALF FLAPS
WITH AND WITHOUT JATO
MODEL: A-4M DATA AS OF: 1 DECEMBER 1970
ENGINE; J52-P-408 DATA BASIS : FLIGHT TEST (NAVY)
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t • TAKEOFF WEIGHT lI 'f IT = 24 , SOO t pdU~DS :If itt~ t-tf:t:1
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WHEN USING C-l1 / e-ll _1
CATAPULT , MAXIMU,.,.
GROSS TAKEOfF WEIGHT
IS 23.500 POUNDS.
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TEMPERATURE - DEGREES CENTIGRADE
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30 40 50 60 70 80
TEMPERATURE - uEGREES FAHRENHEIT
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Figure 11-9. Maximum Takeoff Weight
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