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maximum allowable load factor of Figure 4-5, the maneuvering
limits of Figure 4-8, and the sideslip limits
only under the following conditions:
1 WARNING 1
With roll SAS on, departurer esistanceis reducedb
ecauseo f adversey aw generatedb y
roll SAS inputs. Subsonic maneuvering with
roll SAS on shall not be conducted above 15
units AOA with landing gear retracted.
1. Wing sweep - AUTO.
2. Clean or all air-to-air store loadings except those
that include wing-mounted AIM-54.
Under all other conditions, maneuvering is permitted
only to the AOA limits of Figure 4-7 or the maximum
allowable load factor of Figure 4-5, whichever occurs
4-5 ORIGINAL
NAVAIR 01-F14AAD-1
DATE : FEBRUAFIY IS.92
DATA BASIS : FLIGHT TEST
40
0
ORIGINAL 4-6
1.1’ I’ 1’1’ 1’1’1’ I’ I’ I
0.2 0.4 0.6 0.6 1.0 13 1.4 1.6 1.6 20 2.2
TRUE MACH NUMBER
...... ....
1 ..i..
.....I. .....i . . ..i.. . .I I.... . ..., ; 1 / 1 ~, /I / i , / , j , /I / , / , i 2 i
/ids
...r. /...f 1..
i..~,
....I.
.........
:.I..
I..... ....
j STORE CONRGURATIONS ,c, zc, 2c2, 2Q, wND 2c4 +;-- ~--~I--~~ -+i~-:~::-:
r
i..~ ....
....
....
i”“l”“““” ...T. .............. ...1. ’ ...................
+.j “4.
.. .... ..... ..(.- ......*.. . .. ...... .......*.
..............$..- .~.. 1”” .........
I..
t”” .... ....(.“ “i’- ” ..v +...~.-~ ..- .,_ .“;. [+L i “1:” .......~ 3.. ....
....y. ...I.. .. ...... ...............
/
....$ ... .. ....
I..
+. ..... ......
i
.......... ..... .......... ....
.I
....+. ... .“. ..j. . ... .. ...j.. - ..... .... ..... . ....
~fi_::
.I
.
..... I/
,-.+ j
.
02 6.4 0.6 0.8 1.0 1.2 1.4 1.6 1.6 210 2.2
TRUE MACH NUMBER
Figure 44. Maximum Allowable Airspeeds (Sheet 1 of 3)
NAVAIR 01-FlUAD-I
DATE : FESRUARV ,332
DATA BASIS : FLIGHT TEST
1 j : i ,i.!i,i,iiSlil , : 0’
~~-7
f / yj
STORE CONFIQURAVIONS 1B1, ?A, Zi‘l, 2i,Zi 283, Ah 264’ ’
I,/,/
i
,-!
j ‘( + .‘..... i ^... f + (....,...,.... y.‘.... i...+...,..2 ._..; . . . . . . . . i..+-;
I
. . . . . . . I.... 4 i-J I..-~..J.”
:I I
0 1:; I , I I , I I I , I , I I
0.2 0.4 0.6 0.3 1.0 1.2 1.4 1.0 1.8 2.0 2.2
TRUE MACH NUMBER
3::::J:t: :::;l::::.:t ::::i:::::i::::: 1j::: :::/I: ..t
o. .q ,.,.. j I....; . . . . . j J J i . . . . . J”...] I.,,.; J J ./ . i.-.c..i.llll..;il;~~.
40 I i i .,. / ii
30 .,,j. ...f. . . . . . J / I.....: / i .. . . / j..ll:[IlllilllJff:::
10
0.2 0.4 0.6 0.0 1.0 1.2 rn 1:s 1s i0 iz
TRUE MACH NUMBER
Figure 4-4. Maximum Allowable Airspeeds (Sheet 2 of 3)
4-7 ORIGINAL
NAVAIR Ol-Fl4AAD-1
DATE: FEBRUARY1 032
DATA BASIS : FLIGHT TEST
o ,‘i,:i)!,,ifi!,rfl,,/q ! I,,,, /. i x: .i/ i $8 ,i ./:
I I, I, I, I, I, I, I, I, I
0.2 0.4 0.0 0.0 1.0 ,.a 1.4 1.6 1.8 2.0 a.2
STO; RE~ ’ CO/N FI1G UR; AT;I ON’S ’ j ’X 1, ’ S’ C,,’ S: C?.
. . . . . * 8 i...& ~ . . . . ..i L / . . . . .. . . . . + . . . . . . . . ..i.... ~ /: .? . .C . . .? .. . ?Nf .e . . . . . .\ ..CI i? i . .“..’ ! ““’ l.“.‘.... .i..“.“.i”f.”. ..f .‘ .. .“ .‘ .r I
5o -J:j :::t:: ::j :::1: ::::/:: ::p: &j :::L: j ::::::/ : ::p: ::f i l&i I..,.
O
;: j!.
’ IV’ I..! I/
/‘/ / :ii
I I I I , I 1 I , I
0.2 0.4 0.6 0.8 1.0 12 1.4 I.0 1.8 2.0 2.2
TRUE MACH NUMBER
Figure 4-4. Maximum Allowable Airspeeds (Sheet 3 of 3)
ORIGINAL
NAVAIR Ql-WIAAD-I
DATE: JUNE ,992
OATA BASIS: PLlOHT TEST
GROSS WElOM - ,000 POUNDS
Figure 4-5. Variation of Maximum Allowable Normal Load Factor With Gross Weight
4-9 ORIGINAL
NAVAIR Ol-F14AAD-1
first, and the maneuvering limits of Figure 4-8 and the
sideslip limits of Figure 4-6.
Note
Refer to High Angle-of-Attack Flight Characteristics
and Engine Operating Characteristics
in Chapter 11.
4.4.2 Approach Configuration. Maximum allowable
AOA with landing gear and flaps extended is shown
in Figure 4-6.
4.5 MANEUVERING LIMITS
4.5.1 Approach Configuration. Withlandinggear
and/or landing flaps and slats extended,a brupt yaws are
prohibited. Refer to Figure 4-6 for approach cont&uration
　
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