Douglas A-4M - Page 38

Section XI
P3l'i 4
NAVAlR 01-40AVM -l
~ (B) Cruise altitude. 25,000 ft
(C) Drag index. . . . . . . . . . . . 100
(D) True Jlilach number .. .
0.615
I (E)
!
Al1I\)ient air temperatu re at
cru i se altitude (ICAO standar d
temperature + IOOC) ..... . -24. SoC
(F) True airspeed ..
380 kn
(G) T ailwind ...
50 kn
!I (II) Grou,d dj,"",ce ..... 200 NM J
w
(J) Time ..
28. a m:n
tl- SO
SAMPLE MAXIMUM RANGE
CRUISE -
TIME AND SPEED
,-,--- -
FA1-1S6
M aximum Rang e Cr uise - Na utical Miles per
Pound of Fu el
(For fi gure 11-2 8)
(K) A verage gr oss weight.
1 8.000 II>
(L) Cr uise altitude . . . . ..... 25.000 ft
(M ) Temperatur e deviation from
reAO stan da rd (Am'lient
temperature -24. 5°C).
(N) Drag ind c. \(. .
(P) Cruise altitude.
(Q) Ambient temperature ....
100
25.000 ft
. -24. 5°C
(R) N[ l\Iticalm il espc rp otind ofh lc l . . 0.152 NMJ lb
S AMPL E MAXIMUM RAN GE CRUISE -
NAUTICAL MIL
ES PER POU ND OF FUEl
,
,