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Douglas A-4M - Default Chapter; Table of Contents

Douglas A-4M
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I
NAV
AlR 01-40AVM-1
Section
XI
SECTION
XI
PERFORMANCE
OAT
A
T
ABLE
OF
CONTENTS
P a
rt
Intr
od
uction
GENERAL
..
Performance
Data
Basis
Abbreviations
, Symbo
ls
, and
Definitions
...........
.
Drag
Count Index
System
. . .
A
irspe
ed
Corrections
..
Al
timeter
Corr
ections
.....
2
TAKEOFF
.....
Takeo
ff
Charts
..
Oper
a
tional
Take
off
Distance
..
Maximum
Takeoff W
eig
ht - With
and
Without
JA
TO
..........
.
JATO
Firing
Delay
, Minimum
Takeoff
Distance
- Two
MK
7
MOD
2,
5KS-4500
JATO
Bottles
..
Refusal
Speed
...
.
Stopping
Distance
.....
.
3 CLIMB
.....
.
Climb
.....
Combat
Ceiling
and
Optimum
Cruise
Attitude
.........
...
....
. . . .
4 RANGE
.......
.....
. . . .
•..
Range
Factor
Chart
F
ouled
Deck Ra
nge.
Long
Range
Cruise.
Ma.,<imum Range
Cruise
Nautical
Miles
per
Pound
of
Fuel
INTRODUCTION
P
age
11
- 1
11
-3
11
-3
11
-3
11
-4
1l-7
11
-7
11
-7
11
-7
11
-7
11
-8
11-19
11-20
11-20
11
-3
1
11
-31
11
-3
1
11
-39
11-39
11
-39
11
-39
11
-46
11
-5
1
The
ope
rating
data
charts
contai
ned in
this
sedio
n
provide
the
pilot
with
informa
tion
enabling
him
to
realize
the
ma.'<imum
performance
capabilities
of
the
aircraft.
Use of
the
c
hart
material
for
preflight
planning
and
application
of the
prescribed
operating
procedures
will
result
in
op
timum
effectiveness
of
the
aircraft.
P
art
5 ENDURANCE.
Fou
l
ed
Deck
Enduran
ce
..
M
aximum
Enduran
ce
...
6
Am
RE FUELI
NG
...
Air
Refueling
Chart
s
Tanker
Speed Envelope
...
Tanker
Fuel
Available
for
Trans
f
er
...........
.
Tanker
Fuel
Transf
er
Time
..
F
uel
Consumption
oC
Tank
er
D
uring
Air
Refuelin
g
.....
.
7 DESCENT
•..........
Maximum
Range
Descent
8 LANDING . . .
Landing
....
9 COMBAT P ERF
OR
MANCE
Comba
t P
erformance
T
urning
Rad
i
us
...
.
Maneuverabilit
y
..
.
M
aximum
Ma
ch
Number
.
10 MI
SS
I
ON
PLANNlNG
.....•••....
f..1ission
Planning
.......
....•..
P
age
11-63
11
-63
11-63
11-71
11-71
11-71
11-73
11
-73
11
-76
11-79
11-79
11-
83
11-83
11-93
11
-93
11
-93
11·93
11-98
11·101
~
1l
· 101 I
Section XI
is
divided into
10
parts
to
present
per
f
ormance
data
in
proper
se
qu
ence
for
prefli
ght
planning
.
Sample
problems
and
char
ts
are
pro·
vided
to
present
the
sequence
of
steps
required
to
find the
proper
values
and
solution
of
a
given
problem.
Performan
ce
data
are
presented
in
g
raphical
type
charts
for
ICAO
standard
day
conditions.
In
some
instances,
temperature
co
rrections
for
non-standard
atmosphere
have
been
included.
11
-1
/(
11
·2
blank)
A-4M
NATOPS
Nov 1971