Mirage IV. Просмотр ZIP-архива
M4P/MIRAGE_IV_flight_procedures/MP4_check.htm
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<div class=Section1>
<p class=MsoTitle><span lang=EN-GB style='mso-ansi-language:EN-GB'>MIRAGE IV<o:p></o:p></span></p>
<p class=MsoNormal align=center style='text-align:center'><b><span lang=EN-GB
style='font-size:14.0pt;mso-bidi-font-size:12.0pt;mso-ansi-language:EN-GB'>FLIGHT
PROCEDURES<o:p></o:p></span></b></p>
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<p class=MsoNormal><b><u><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></u></b></p>
<p class=MsoNormal><b><u><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></u></b></p>
<p class=MsoNormal><b><u><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></u></b></p>
<p class=MsoNormal><b><u><span lang=EN-GB style='mso-ansi-language:EN-GB'>Preliminary
warning<o:p></o:p></span></u></b></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>These
simplified<span style="mso-spacerun: yes"> </span>flight procedures presented
below retain only what is <span style='color:black'>distinctly</span> essential
for Flight Simulator virtual flights. These procedures can serve as a guide for
cadet virtual pilots who are not familiar with the high performance military
delta jet. The data are as precise as Flight Simulator permit. Even the real
Mirage IVP pilots will have to read carefully<span style="mso-spacerun: yes">
</span>this document in order to fully enjoy the virtual model.<o:p></o:p></span></p>
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<p class=MsoNormal><b><u><span lang=EN-GB style='mso-ansi-language:EN-GB'>Main
airspeed and weight<span style="mso-spacerun: yes"> </span>limitations<o:p></o:p></span></u></b></p>
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<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>With DT*
maximal subsonic airspeed<span style='mso-tab-count:2'> </span>IAS
550 kt. Mach<1<span style="mso-spacerun: yes"> </span>FL 400<span
style="mso-spacerun: yes"> </span><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Maximal
airspeed with low altitude turbulence<span style='mso-tab-count:1'> </span>IAS
400 kt.<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Clean
supersonic maximal<span style="mso-spacerun: yes"> </span>airspeed <span
style='mso-tab-count:3'> </span>IAS 650 kt. Mach
2.0<span style="mso-spacerun: yes"> </span>FL 550<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Maximum
Landing Gear Operating/Extended :<span style='mso-tab-count:1'> </span>240
kt.<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Maximal
load factor clean or empty DT <span style='mso-tab-count:2'> </span>+5
g -1.5 g<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><span
style='mso-tab-count:3'> </span>with full DT<span
style='mso-tab-count:3'> </span>+4 g – 1.5 g<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Maximal<span
style="mso-spacerun: yes"> </span>pitch attitude angle<span style='mso-tab-count:
4'> </span>19° **<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=NL style='mso-ansi-language:NL'>Chute brake
opening maximal airspeed<span style='mso-tab-count:2'> </span>200
kt<o:p></o:p></span></p>
<p class=MsoNormal><span lang=NL style='mso-ansi-language:NL'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Maximal
crosswind dry runway<span style='mso-tab-count:3'> </span>25
kt. <o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Maximal
crosswind wet runway<span style='mso-tab-count:3'> </span>20
kt.<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Releasing
DT :maximal airspeed <span style='mso-tab-count:3'> </span>M
0.9<span style="mso-spacerun: yes"> </span>IAS 280 – 450 kt.<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>(Releasing
partly fill DT is forbidden unless emergency)<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Releasing
JATOS stand maximal airspeed<span style='mso-tab-count:2'> </span>
250 kt.<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Maximal
airspeed fuel dump<span style='mso-tab-count:4'> </span>400
kt.<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Maximum
Take Off Weight : <span style='mso-tab-count:3'> </span>33.8
tonnes <o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Maximum
Landing Weight :<span style="mso-spacerun: yes"> </span><span
style='mso-tab-count:3'> </span>26 tonnes <o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><u><span lang=EN-GB style='mso-ansi-language:EN-GB'>Notes<o:p></o:p></span></u></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>* DT = Drop
tanks<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>** Pitch
attitude angle greater than 19° will result in pitch instability. In other
words, the aircraft will increase the angle of attack without any pilot input
and will stall. The pilot should imperatively avoid to reach 19° pitch attitude
angle In such case the pilot may loose control of the aircraft. At low altitude
it will be practically impossible to recover before hitting the ground. The
mirage IVP is a strategic reconnaissance military delta jet bomber and not a
fighter. This instability phenomenon have been introduced in the flight dynamic
model. So be careful.<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>*** VIP =
Variomиtre а Indication de Poussйe / Vertical speed & Thrust
Indicator.<span style="mso-spacerun: yes"> </span>The VIP is located below the
altimeter at the right of ADI. The VIP give the vertical speed (needle) and the
total vertical speed (index). But only the vertical speed indicator is
operational.<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-CA>**** Not implemented</span></p>
<p class=MsoNormal><span lang=EN-CA><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-CA><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-CA><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><b><u><span lang=EN-GB style='mso-ansi-language:EN-GB'>Flight
preparation<o:p></o:p></span></u></b></p>
<p class=MsoNormal><b><u><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></u></b></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>You can use
either 2D panel or the virtual cockpit according to your personal choice. The
2D panel is more simple to work with. Virtual cockpit present the advantage to
be more immerse and more realistic. Moreover you can use the hardware system
which permit to modify the point of view in virtual cockpit when you turn your
head for example.<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Even
without this system, you can look around using the hat switch of the joystick.
It will be very useful to zoom or unzoom with appropriate keyboard commands.
Also useful, the keyboard commands for raise, lower and rotate the pilot's
seat. These keyboard commands will be a convenient way to increase and ease the
forward view. So, if not already done, you should assign keyboard commands tot
these functions. (see an example below)<o:p></o:p></span></p>
<p class=MsoNormal><b><u><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></u></b></p>
<p class=MsoNormal><!--[if gte vml 1]><v:line id="_x0000_s1026" style='position:absolute;
flip:y;z-index:1;mso-position-horizontal:absolute;
mso-position-horizontal-relative:text;mso-position-vertical:absolute;
mso-position-vertical-relative:text' from="9pt,131.4pt" to="36pt,140.4pt"
strokecolor="red" strokeweight=".71mm">
<v:stroke endarrow="block" color2="aqua" joinstyle="miter"/>
</v:line><![endif]--><![if !vml]><span style='mso-ignore:vglayout;position:
absolute;z-index:0;margin-left:0px;margin-top:162px;width:61px;height:38px'><img
width=61 height=38 src="./MIRAGE_IV_flight_procedures_fichiers/image003.gif"
v:shapes="_x0000_s1026"></span><![endif]><!--[if gte vml 1]><v:line id="_x0000_s1027"
style='position:absolute;z-index:2;mso-position-horizontal:absolute;
mso-position-horizontal-relative:text;mso-position-vertical:absolute;
mso-position-vertical-relative:text' from="9pt,140.4pt" to="27pt,176.4pt"
strokecolor="red" strokeweight=".71mm">
<v:stroke endarrow="block" color2="aqua" joinstyle="miter"/>
</v:line><![endif]--><![if !vml]><span style='mso-ignore:vglayout;position:
absolute;z-index:1;margin-left:0px;margin-top:175px;width:49px;height:74px'><img
width=49 height=74 src="./MIRAGE_IV_flight_procedures_fichiers/image004.gif"
v:shapes="_x0000_s1027"></span><![endif]><span lang=EN-CA><!--[if gte vml 1]><v:shape
id="_x0000_i1026" type="#_x0000_t75" style='width:423.75pt;height:221.25pt'
filled="t">
<v:fill color2="black"/>
<v:imagedata src="./MIRAGE_IV_flight_procedures_fichiers/image005.jpg"
o:title=""/>
<v:textbox inset="0,0,0,0"/>
</v:shape><![endif]--><![if !vml]><img width=565 height=295
src="./MIRAGE_IV_flight_procedures_fichiers/image006.jpg" v:shapes="_x0000_i1026"><![endif]></span></p>
<p class=MsoNormal><span lang=EN-CA><!--[if gte vml 1]><v:shape id="_x0000_i1027"
type="#_x0000_t75" style='width:414.75pt;height:283.5pt' filled="t">
<v:fill color2="black"/>
<v:imagedata src="./MIRAGE_IV_flight_procedures_fichiers/image007.jpg"
o:title=""/>
<v:textbox inset="0,0,0,0"/>
</v:shape><![endif]--><![if !vml]><img width=553 height=378
src="./MIRAGE_IV_flight_procedures_fichiers/image008.jpg" v:shapes="_x0000_i1027"><![endif]></span></p>
<p class=MsoNormal><span lang=EN-CA><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><b><u><span lang=EN-GB style='mso-ansi-language:EN-GB'>BEFORE
STARTING ENGINES<o:p></o:p></span></u></b></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Parking
brakes<span style='mso-tab-count:4'> </span>Set<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Battery<span
style='mso-tab-count:2'> </span> <span style='mso-tab-count:4'> </span>ON
<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Breakers<span
style='mso-tab-count:5'> </span>Engaged<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>VHF/UHF<i
style='mso-bidi-font-style:normal'> </i><span style='mso-tab-count:5'> </span>ON<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Intercom <span
style='mso-tab-count:5'> </span>TEST<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>ADI
(Horizon Flight Director) <span style='mso-tab-count:2'> </span>CHECK<span
style="mso-spacerun: yes"> </span>index set<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Standby
Horizon<span style='mso-tab-count:4'> </span>CHECK<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>COM2 <i
style='mso-bidi-font-style:normal'><span style='mso-tab-count:5'> </span></i>Test
with ATC<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>COM1 <span
style='mso-tab-count:5'> </span>Ask
clearance for starting engines<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><b><u><span lang=EN-GB style='mso-ansi-language:EN-GB'>Right
bank: <o:p></o:p></span></u></b></p>
<p class=MsoNormal><b><u><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></u></b></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Navigation
& Anti Collision<span style="mso-spacerun: yes"> </span>lights<span
style='mso-tab-count:2'> </span>OFF<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Cockpit
light<span style='mso-tab-count:1'> </span> <span style='mso-tab-count:4'> </span>As
required<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>engines
switches<span style='mso-tab-count:4'> </span>OFF<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>LP Pumps <span
style='mso-tab-count:5'> </span>STOP<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Warning
lights<span style='mso-tab-count:4'> </span>TEST<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>VOR/ILS <span
style='mso-tab-count:5'> </span>Frequency
tuned<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>TACAN <span
style='mso-tab-count:5'> </span>Frequency
tuned<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Fuel Dump
System<span style='mso-tab-count:4'> </span>Protective
cap down<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Pitot heat<span
style='mso-tab-count:5'> </span>OFF<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>ALT1 – ALT2
<span style='mso-tab-count:4'> </span>ON<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Chronometer
<span style='mso-tab-count:5'> </span>Crank
& set<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Emergency
de-pressurisation seal ****<span style='mso-tab-count:1'> </span>Forward
position <o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><b><u><span lang=EN-GB style='mso-ansi-language:EN-GB'>Panel
board<o:p></o:p></span></u></b></p>
<p class=MsoNormal><b><u><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></u></b></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Test fuel
gauges <span style='mso-tab-count:4'> </span>FUS-NOUR
<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Flow rate
gauge<span style='mso-tab-count:4'> </span>NULL<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>PC
Injection lights<span style='mso-tab-count:4'> </span>TEST<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>VIP ***<span
style='mso-tab-count:5'> </span>Index
set<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Main
altimeter<span style='mso-tab-count:1'> </span> <span style='mso-tab-count:
3'> </span>Pressure set<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Accelerometer<span
style='mso-tab-count:5'> </span>NULL<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Radio-Altimeter<span
style='mso-tab-count:4'> </span>Index
set<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Mach-meter<span
style='mso-tab-count:1'> </span> <span style='mso-tab-count:4'> </span>NULL<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Standby
altimeter<span style='mso-tab-count:4'> </span>Pressure
set<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>ADN <span
style='mso-tab-count:1'> </span>(Navigation Direction Indicator) <span
style='mso-tab-count:1'> </span>Set<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Fuel
failure board lights<span style='mso-tab-count:3'> </span>Test
2 <o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Intercom
Fuel<span style='mso-tab-count:5'> </span>CLOSE<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>MAL lights<span
style='mso-tab-count:5'> </span>OFF<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Warning
lights & sounds<span style='mso-tab-count:3'> </span>TEST<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>TNS Lights
(Landing Gear not Extend) <span style='mso-tab-count:1'> </span>Green<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>IFF <span
style='mso-tab-count:6'> </span>STOP<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><b><u><span lang=EN-GB style='mso-ansi-language:EN-GB'>Left
bank<o:p></o:p></span></u></b></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Gear lever<span
style='mso-tab-count:5'> </span>DOWN<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Gear
indicator lights <span style='mso-tab-count:4'> </span>3
green<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Drag chute<span
style='mso-tab-count:1'> </span> <span style='mso-tab-count:4'> </span>Flight
position<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Pitch, yaw
& roll Trim lights<span style='mso-tab-count:3'> </span>TEST<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Throttle<span
style='mso-tab-count:5'> </span>STOP<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Automatic
approach system<span style='mso-tab-count:3'> </span>Forward
position<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Air Intake
Cone<span style='mso-tab-count:4'> </span>AUTO<o:p></o:p></span></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=Default><b><u><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>STARTING ENGINES <o:p></o:p></span></u></b></p>
<p class=Default><b><u><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></u></b></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>Parking brakes <span style='mso-tab-count:4'> </span>SET<o:p></o:p></span></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>Fuel Transfer– <span style='mso-tab-count:4'> </span>Transfer
<o:p></o:p></span></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>MAL Lights (fuel sub-panel)<span style='mso-tab-count:
3'> </span>OFF<o:p></o:p></span></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>Throttles<span style='mso-tab-count:5'> </span>IDLE<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-CA><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=Default><b><u><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>Right engine<o:p></o:p></span></u></b></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>Cut off switch<span style='mso-tab-count:5'> </span>OPEN<o:p></o:p></span></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>BP (max 15 sec. after opening cut off switch) <span
style='mso-tab-count:1'> </span>ON<o:p></o:p></span></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>Verify BP light, Right BP light<span style='mso-tab-count:
2'> </span>OFF<o:p></o:p></span></p>
<p class=Default><span style='font-family:"Times New Roman"'>BP Pressure<span
style='mso-tab-count:5'> </span>1,14
bars <o:p></o:p></span></p>
<p class=Default><span style='font-family:"Times New Roman"'>Ignition –
Ventilation <span style='mso-tab-count:3'> </span>Ignition
<o:p></o:p></span></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>Starter<span style='mso-tab-count:6'> </span>ENGAGED<o:p></o:p></span></p>
<p class=Default style='margin-left:212.25pt;text-indent:-212.25pt'><span
lang=EN-GB style='font-family:"Times New Roman";mso-ansi-language:EN-GB'>Top
chronometer <span style='mso-tab-count:1'> </span>600
RPM<span style="mso-spacerun: yes"> </span><o:p></o:p></span></p>
<p class=Default style='margin-left:212.25pt;text-indent:-212.25pt'><span
lang=EN-GB style='font-family:"Times New Roman";mso-ansi-language:EN-GB'><span
style="mso-spacerun: yes"> </span>(in less than<span style="mso-spacerun:
yes"> </span>20 sec.<span style="mso-spacerun: yes"> </span>Otherwise release
starter button) <o:p></o:p></span></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'><span style="mso-spacerun: yes"> </span>During
right engine start verify 2000 RPM in less than 25 sec <o:p></o:p></span></p>
<p class=Default><span style='font-family:"Times New Roman"'>T4 <span
style='mso-tab-count:6'> </span>850°
max. (excep. </span><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>900° <3"). <o:p></o:p></span></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>Throttle position<span style='mso-tab-count:4'> </span>2920
RPM<span style="mso-spacerun: yes"> </span>+/- 100 RPM <o:p></o:p></span></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>Right Oil Pressure light<span style='mso-tab-count:
3'> </span>OFF<o:p></o:p></span></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>Hydraulic 2 Light <span style='mso-tab-count:4'> </span>OFF<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Hydraulic 2
Pressure<span style='mso-tab-count:4'> </span>210
bars<o:p></o:p></span></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>Stick test. Push, Pull, Left, and Right<o:p></o:p></span></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>Rudder pedal test Left, Right<o:p></o:p></span></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>The mechanic announce the displacement of the control
surfaces. <o:p></o:p></span></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=Default><b><u><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>Left engine</span></u></b><span lang=EN-GB
style='font-family:"Times New Roman";mso-ansi-language:EN-GB'> <o:p></o:p></span></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>Same procedure as for the right engine<o:p></o:p></span></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>Left Oil Pressure light<span style='mso-tab-count:
3'> </span>OFF<o:p></o:p></span></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>Hydraulic 1 <span style='mso-tab-count:5'> </span>LIGHT
OFF<o:p></o:p></span></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>Hydraulic1 Pressure<span style='mso-tab-count:4'> </span>210
bars <o:p></o:p></span></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=Default><b><u><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>PPOST STARTING ENGINES<o:p></o:p></span></u></b></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>Adjust Idle to obtain <span style='mso-tab-count:4'> </span>3200
RPM<o:p></o:p></span></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>ALT warning light<span style='mso-tab-count:4'> </span>OFF<o:p></o:p></span></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>Anti Collision<span style="mso-spacerun: yes">
</span>lights<span style='mso-tab-count:4'> </span>As
required<o:p></o:p></span></p>
<p class=Default><span style='font-family:"Times New Roman"'>TACAN REC <span
style='mso-tab-count:5'> </span>ON<o:p></o:p></span></p>
<p class=Default><span style='font-family:"Times New Roman"'>VOR/ILS <span
style='mso-tab-count:5'> </span>ON<o:p></o:p></span></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>Pitot heat<span style='mso-tab-count:5'> </span>ON<o:p></o:p></span></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>VIP ***<span style='mso-tab-count:5'> </span>TEST<o:p></o:p></span></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>Radio Altimeter <span style='mso-tab-count:4'> </span>TEST<o:p></o:p></span></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>Pitch attitude angle<span style='mso-tab-count:4'> </span>TEST<o:p></o:p></span></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>ADI <span style='mso-tab-count:6'> </span>CHECK
FD – TAKE OFF POSITION<o:p></o:p></span></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>ADN <span style='mso-tab-count:6'> </span>TEST<o:p></o:p></span></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>IFF <span style='mso-tab-count:6'> </span>Standby
<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>All red
warning lights <span style='mso-tab-count:3'> </span>OFF<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>TRIM Roll & Yaw<span style='mso-tab-count:4'> </span>NULL<o:p></o:p></span></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>TRIM Pitch<o:p></o:p></span></p>
<p class=Default style='margin-left:35.4pt;text-indent:35.4pt'><span
lang=EN-GB style='font-family:"Times New Roman";mso-ansi-language:EN-GB'>With
DT<span style='mso-tab-count:3'> </span>0.5° <o:p></o:p></span></p>
<p class=Default style='margin-left:35.4pt;text-indent:35.4pt'><span
lang=EN-GB style='font-family:"Times New Roman";mso-ansi-language:EN-GB'>Clean <span
style='mso-tab-count:4'> </span>0.5° <o:p></o:p></span></p>
<p class=Default style='margin-left:35.4pt;text-indent:35.4pt'><span
lang=EN-GB style='font-family:"Times New Roman";mso-ansi-language:EN-GB'>Empty
wing fuel cells<span style='mso-tab-count:2'> </span>1.0° <o:p></o:p></span></p>
<p class=Default style='margin-left:35.4pt;text-indent:35.4pt'><b><u><span
lang=EN-GB style='font-family:"Times New Roman";mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></u></b></p>
<p class=Default><b><u><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>TAXI<o:p></o:p></span></u></b></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>Parking brakes<span style='mso-tab-count:4'> </span>Released<o:p></o:p></span></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>Adjust Throttle for 7000 RPM with parking brakes set<o:p></o:p></span></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>Brakes test 4 <o:p></o:p></span></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>Reduce Throttle completely before turning<o:p></o:p></span></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>Taxi,<span style="mso-spacerun: yes">
</span>avoid<span style="mso-spacerun: yes"> </span>4000 RPM < N < 5500
RPM<o:p></o:p></span></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'><span style="mso-spacerun: yes"> </span>N > 2800
RPM<o:p></o:p></span></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>Anti Collision Lights<span style='mso-tab-count:4'> </span>ON<o:p></o:p></span></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>ADN NAV <o:p></o:p></span></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>FF, TACAN, VOR, ILS <span style='mso-tab-count:3'> </span>TEST<o:p></o:p></span></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>COM1 Radio on take off frequency <span
style='mso-tab-count:2'> </span>CHECK<o:p></o:p></span></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>COM2 Radio on ground frequency <span style='mso-tab-count:
2'> </span>CHECK<o:p></o:p></span></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>VIP ***<span style='mso-tab-count:5'> </span>TEST<o:p></o:p></span></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>Radio Altimeter Test<span style='mso-tab-count:4'> </span>index
set at<span style="mso-spacerun: yes"> </span>500 ft<o:p></o:p></span></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=Default><b><u><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>MANEUVRING POINT<o:p></o:p></span></u></b></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>Altimeters Test, take note of possible errors<o:p></o:p></span></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=Default><b><u><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>LINE UP & TAKE OFF<o:p></o:p></span></u></b></p>
<p class=Default><b><u><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></u></b></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>Emergency release protection cap<span
style='mso-tab-count:2'> </span>OPEN<o:p></o:p></span></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>Verify ADI concordance with ADN <o:p></o:p></span></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>N <span style='mso-tab-count:6'> </span>8200
RPM<o:p></o:p></span></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>All red warning lights OFF except Radio altimeter<o:p></o:p></span></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>T4 > 720°, IF Weight>48400 lb <span
style='mso-tab-count:2'> </span>PC mini <o:p></o:p></span></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>Verify<span style="mso-spacerun: yes"> </span>pumping
7800 < N < 8900 <o:p></o:p></span></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>Peak<span style="mso-spacerun: yes"> </span>T4 <
720° <o:p></o:p></span></p>
<p class=Default><span lang=EN-GB style='font-family:"Times New Roman";
mso-ansi-language:EN-GB'>PC Injection light<span style='mso-tab-count:4'> </span>OFF
before 10 sec.<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>If
Weight< <span style='color:black'>48400 lb </span><span style="mso-spacerun:
yes"> </span><span style='mso-tab-count:4'> </span>PC
mini after brakes released<o:p></o:p></span></p>
<p class=MsoNormal><b><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></b></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>You are now
ready for take off<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>It is
important to synchronize the FD pitch bar. Look in the control assignments menu
to find the keyboard command or the joystick button assigned to « Flight
Director sync pitch » to activate this function.<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><a name="_1263803857"></a><span lang=EN-CA><!--[if gte vml 1]><v:shape
id="_x0000_i1028" type="#_x0000_t75" style='width:405.75pt;height:253.5pt'
o:ole="" filled="t">
<v:fill color2="black"/>
<v:imagedata src="./MIRAGE_IV_flight_procedures_fichiers/image009.wmz"
o:title=""/>
<v:textbox inset="0,0,0,0"/>
</v:shape><![endif]--><![if !vml]><img width=541 height=338
src="./MIRAGE_IV_flight_procedures_fichiers/image010.gif" v:shapes="_x0000_i1028"><![endif]><!--[if gte mso 9]><xml>
<o:OLEObject Type="Embed" ProgID="Word.Picture.8" ShapeID="_x0000_i1028"
DrawAspect="Content" ObjectID="_1266608843">
</o:OLEObject>
</xml><![endif]--></span></p>
<p class=MsoNormal><span lang=EN-CA><!--[if gte vml 1]><v:shape id="_x0000_i1029"
type="#_x0000_t75" style='width:405.75pt;height:234pt' filled="t">
<v:fill color2="black"/>
<v:imagedata src="./MIRAGE_IV_flight_procedures_fichiers/image011.jpg"
o:title=""/>
<v:textbox inset="0,0,0,0"/>
</v:shape><![endif]--><![if !vml]><img width=541 height=312
src="./MIRAGE_IV_flight_procedures_fichiers/image012.jpg" v:shapes="_x0000_i1029"><![endif]></span></p>
<p class=MsoNormal><span lang=EN-CA><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-CA><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Assign a
keyboard command or a joystick button to the following functions:<o:p></o:p></span></p>
<p class=MsoNormal style='text-indent:35.4pt'><span lang=EN-GB
style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal style='text-indent:35.4pt'><span lang=EN-GB
style='mso-ansi-language:EN-GB'>- AUTOPILOT PITCH REF INCREASE DOWN<o:p></o:p></span></p>
<p class=MsoNormal style='text-indent:35.4pt'><span lang=EN-GB
style='mso-ansi-language:EN-GB'>- AUTOPILOT PITCH REF INCREASE UP <o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>The use of
these two functions will ease the handling or your FS aircraft.<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>The pitch
reference<span style="mso-spacerun: yes"> </span>in FD may be adjust using the
pitch knob on the autopilot board.<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Before synchronized<span
style="mso-spacerun: yes"> </span>FD synchronized<span
style='mso-tab-count:1'> </span><span style="mso-spacerun: yes">
</span>Take off reference Pitch<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-CA><!--[if gte vml 1]><v:shape id="_x0000_i1030"
type="#_x0000_t75" style='width:453.75pt;height:158.25pt' filled="t">
<v:fill color2="black"/>
<v:imagedata src="./MIRAGE_IV_flight_procedures_fichiers/image013.jpg"
o:title=""/>
<v:textbox inset="0,0,0,0"/>
</v:shape><![endif]--><![if !vml]><img width=605 height=211
src="./MIRAGE_IV_flight_procedures_fichiers/image014.jpg" v:shapes="_x0000_i1030"><![endif]></span></p>
<p class=MsoNormal><span lang=EN-CA><span style='mso-tab-count:1'> </span></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Display the
exact QFU heading. </span><span lang=EN-CA>Engage HDG mode on autopilot,</span></p>
<p class=MsoNormal><span lang=EN-CA><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Set
friction knob<span style="mso-spacerun: yes"> </span>at maximum dry power.
This is done by pushing the throttles until you<span style="mso-spacerun:
yes"> </span>reach 8450 RPM. But verify that the PC warning lights are OFF.
The maximal dry power correspond to 90% of the throttles course. In these
conditions each engines reach 11000 pound of thrust. Verify the engine
parameters. If all parameters are OK, Top chronometer. Release the parking
brakes. Then push throttles to full PC.<span style="mso-spacerun: yes">
</span>PC load gauge will indicate 10. The engine run at 8500 RPM. <o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoBodyText><span lang=EN-GB style='mso-ansi-language:EN-GB'>One can
imagine an hardware stop on our joystick throttle set to 90 % of the maximal
throttle travel. This position will give the maximal dry power. Beyond that
point we will have PC working. One can dream..<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>The
aircraft is heavy and relatively under powered. The acceleration is positive
but not violent,,,<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>At 170 kt.,
rotate and maintain a 10 degree <span style='color:black'>pitch up attitude</span>
initially. Once with a positive vertical speed pull the stick to obtain a 15
degree <span style='color:black'>pitch up attitude</span>. Raise the landing
gear.<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>At maximal
weight, the Mirage IV is not a genuine two engines aircraft at take off.
Between 170 kt. to 220 kt., in case of an engine failure,<span
style="mso-spacerun: yes"> </span>you has to react rapidly: Raise the landing
gear,<span style="mso-spacerun: yes"> </span>and release the DT. If the
aircraft does not accelerate and does not climb..EJECT. Pull the handle at the
bottom of the seat...<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><b><span lang=EN-GB style='mso-ansi-language:EN-GB'>IMPORTANT </span></b><span
lang=EN-GB style='mso-ansi-language:EN-GB'>: Wait<span style="mso-spacerun:
yes"> </span>until you<span style="mso-spacerun: yes"> </span>reach 300 kt.
before turning<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>At 350 kt.
reduce power to PC mini (6 on PC load gauge.)<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>At 400kt
reduce power to max dry level. PC lights goes off at 8450 RPM<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Now you can
breathe...<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Do the <span
style='color:black'>after</span> take off check-list. You can synchronize the
FD using the « pitch synch » button. Then engage the autopilot to
keep constant heading.<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>During
acceleration you may notice that the rudder become less and less effective.
This behaviour was added<span style="mso-spacerun: yes"> </span>to the flight
dynamic model to reproduce the reality. From Mach 0,45 the yaw damper function
of the autopilot is activated automatically. This will reduce the risk of yaw –
roll oscillations (Dutch roll) <span style='color:black'>which might</span>
appear at high speed and high altitude.<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<h3 style='margin-left:0cm;text-indent:0cm;tab-stops:0cm'><span lang=EN-GB
style='mso-ansi-language:EN-GB'>Take off with<span style="mso-spacerun: yes">
</span>JATOS, maximum weight<o:p></o:p></span></h3>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>The JATO
(Jet Assisted Take Off) rockets are used to ease take off at maximum weight,
high temperature, high altitude<span style="mso-spacerun: yes"> </span>or
reduced length runway. The twelve rockets pack give a supplementary thrust of
12000 pounds. The rockets will give the thrust for 25 seconds and thus provide
a better acceleration. Eventually the rockets may help in case of an engine
failure during take off.<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>The rocket
supplementary thrust are included in the aircraft flight dynamic model. To
activate the JATO rocket, first fire PC. Then activate the button for firing
the JATO rockets.<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Extinction
of JATO rockets will occur at around IAS 220 kt. without a pilot's action.
After the take off, release the JATO racks before reaching IAS 250 kt.<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><span
style="mso-spacerun: yes"> </span><o:p></o:p></span></p>
<p class=MsoNormal><b><u><span lang=EN-GB style='mso-ansi-language:EN-GB'>Subsonic
climb<o:p></o:p></span></u></b></p>
<p class=MsoNormal><b><u><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></u></b></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>For best
operation of the aircraft at high altitude, the use of autopilot is strongly
recommended. The flight at high altitude and high speed required a very precise
aircraft control. For example a variation of the pitch attitude angle at Mach 2
will result in a 2000ft/minute vertical speed variation.<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>For a 420
kt. / Mach 0,9 climb, at full dry power, adjust pitch attitude angle as
required using the appropriate mode of the autopilot.<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><b><u><span lang=EN-GB style='mso-ansi-language:EN-GB'>Subsonic
cruise<o:p></o:p></span></u></b></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>At Mach
0.9, fly initially at FL300. Then continue to climb according to the remaining
fuel load. At the end of subsonic airspeed range, it is possible to reach FL400
which is the maximum authorized flight level for this configuration. Once DT
empty, you can release them to improve performance during the remaining flight
duration.<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><b><u><span lang=EN-GB style='mso-ansi-language:EN-GB'>Climb
– supersonic cruise<o:p></o:p></span></u></b></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Supersonic
flights are forbidden with drop tanks. The correct procedure is to climb and
cruise at subsonic speed. Then, once the fuel in DT is burned, release the DT.
This will reduce the drag. So the aircraft will be able to reach Mach 1 without
any problem,<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Transonic
acceleration below FL300. The transonic acceleration is possible in flight
level. Above FL300 the transonic acceleration will be possible only in descent.<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Put PGPC,
the acceleration between Mach 0,96 and Mach 1,10 is slow. This is normal<span
style="mso-spacerun: yes"> </span>because the drag is maximal. In this part of
the flight we must fly straight ahead. When we reach Mach 1,2 the aircraft
enter in the supersonic domain. The drag decrease and acceleration increase. So
you can resume climbing toward required flight level. Maximum flight level is
FL550, taking care to maintain<span style="mso-spacerun: yes"> </span>IAS 600
kt.<span style="mso-spacerun: yes"> </span>then Mach 1.85<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><u><span lang=EN-GB style='mso-ansi-language:EN-GB'>Note</span></u><span
lang=EN-GB style='mso-ansi-language:EN-GB'>: <o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>A strict
observance of the climb procedure, give to the Mirage IV the maximal
performances available. If you try to climb at Vi or at too low Mach number,
the result will be a decrease of performances. This may result, in propulsion's
instability at high altitude.<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>The maximal
Mach number is 2,2, but the optimal cruise airspeed is between Mach 1,85 and
Mach 2,0. Mach 2,20 is the operational limit<span style="mso-spacerun: yes">
</span>due to the risk of<span style="mso-spacerun: yes"> </span>overheating
the skin and thus life reduction<span style="mso-spacerun: yes"> </span>of the
structure. This overheating may made the canopy blind which is annoying during
approach. LOL<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Avoid to
let the airspeed drop below Mach 1,8 in cruise situation. Otherwise you risk
an<span style="mso-spacerun: yes"> </span>a propulsion's instability at high
altitude.<o:p></o:p></span></p>
<p class=MsoNormal><b><u><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></u></b></p>
<p class=MsoNormal><b><u><span lang=EN-GB style='mso-ansi-language:EN-GB'>Slow
down – supersonic descent</span></u></b><span lang=EN-GB style='mso-ansi-language:
EN-GB'>:<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Before<span
style="mso-spacerun: yes"> </span>starting the descent <o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Above 50
000ft<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><span
style='mso-tab-count:1'> </span>PC cut, full dry power<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><span
style='mso-tab-count:1'> </span>Let the plane slow down to 300
kt.<span style="mso-spacerun: yes"> </span>in flight level <o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Below 50
000 ft<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><span
style='mso-tab-count:1'> </span>reduce power to obtain 8000 RPM<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><span
style='mso-tab-count:1'> </span>Maintain 300 kt. then Mach 0,9<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><span
style='mso-tab-count:1'> </span>Reduce power to 7500 RPM<span
style="mso-spacerun: yes"> </span>when reaching Mach 1<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><b><u><span lang=EN-GB style='mso-ansi-language:EN-GB'>Subsonic
descent<o:p></o:p></span></u></b></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Throttle to
idle, maintain IAS 300 kt. (the maximum lift to drag ratio airspeed) This give
a gradient of 1000 feet per nautical miles. For example, you want to descent
from FL350 to FL50. So you have to loose 30000 feet, and you will take 30
nautical miles before reaching the FL50.<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<h4 style='margin-left:0cm;text-indent:0cm;tab-stops:0cm'><span lang=EN-GB
style='mso-ansi-language:EN-GB'>LOW LEVEL CRUUISE<o:p></o:p></span></h4>
<p class=MsoNormal><b><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></b></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Fly at<span
style="mso-spacerun: yes"> </span>IAS 420-480 kt., if there is turbulence
maintain IAS 400 kt.<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><b><u><span lang=EN-GB style='mso-ansi-language:EN-GB'>Break<o:p></o:p></span></u></b></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>The break
is done with a 60° bank at IAS 400 kt. at the runway axis. Then make a 60
degrees turn. Air brake extended. In the rear wind leg reduce speed to 200 kt.
At the end of the rear wind leg, lower the gear and activate the automatic
approach power controller. Then turn to the final approach leg.<o:p></o:p></span></p>
<p class=MsoNormal><b><u><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></u></b></p>
<p class=MsoNormal><b><u><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></u></b></p>
<p class=MsoNormal><b><u><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></u></b></p>
<p class=MsoNormal><b><u><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></u></b></p>
<p class=MsoNormal><b><u><span lang=EN-GB style='mso-ansi-language:EN-GB'>ILS
Approach<o:p></o:p></span></u></b></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>In the real
world the pilot use Ground Control Approach (GCA). In the virtual world we use
ILS approach. The ILS mode of the autopilot follow quite well the LOC path. But
the glide slope interception create problems. The angle of attack is high
during approach. So the autopilot give an pitch down command too strong. After,
the AP must restore the correct path and thus over react. For these reasons it
is preferable to activate the AP at quite long distance from the runway and at
3000 ft.<span style="mso-spacerun: yes"> </span>An other way to simulate a GCA
approach you may use NAV mode of the AP for the LOC interception, following the
glide slope manually using FD.<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><b><u><span lang=EN-GB style='mso-ansi-language:EN-GB'>Final
approach<o:p></o:p></span></u></b></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>Final
approach is a critical part of the flight for two reasons:<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>1-<span
style="mso-spacerun: yes"> </span>Angle of attack is around 10-12°, So the
forward vision is quite limited. If you use the VC, you must raise the seat and
shift the view to right or left so the central frame will not reduce forward
vision. Use keyboard command that you have assigned to this purpose in the
flight preparation section.<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal style='tab-stops:7.0pt'><span lang=EN-GB style='mso-ansi-language:
EN-GB'>Default VC forward view...one see almost noting... </span><span
lang=EN-CA><!--[if gte vml 1]><v:shape id="_x0000_i1031" type="#_x0000_t75"
style='width:396.75pt;height:292.5pt' filled="t">
<v:fill color2="black"/>
<v:imagedata src="./MIRAGE_IV_flight_procedures_fichiers/image015.jpg"
o:title=""/>
<v:textbox inset="0,0,0,0"/>
</v:shape><![endif]--><![if !vml]><img width=529 height=390
src="./MIRAGE_IV_flight_procedures_fichiers/image016.jpg" v:shapes="_x0000_i1031"><![endif]></span><span
lang=EN-GB style='mso-ansi-language:EN-GB'><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>If you
raise the seat and shift the the view to left,<span style="mso-spacerun: yes">
</span>you could see the runway now.....<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-CA><!--[if gte vml 1]><v:shape id="_x0000_i1032"
type="#_x0000_t75" style='width:396.75pt;height:261.75pt' filled="t">
<v:fill color2="black"/>
<v:imagedata src="./MIRAGE_IV_flight_procedures_fichiers/image017.jpg"
o:title=""/>
<v:textbox inset="0,0,0,0"/>
</v:shape><![endif]--><![if !vml]><img width=529 height=349
src="./MIRAGE_IV_flight_procedures_fichiers/image018.jpg" v:shapes="_x0000_i1032"><![endif]></span></p>
<p class=MsoNormal><span lang=EN-CA><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal style='margin-left:18.0pt;text-indent:0cm;mso-list:l1 level1 lfo2;
tab-stops:list 0cm left 18.0pt 36.0pt'><![if !supportLists]><span lang=EN-GB
style='mso-ansi-language:EN-GB'>2-<span style='font:7.0pt "Times New Roman"'>
</span></span><![endif]><span lang=EN-GB style='mso-ansi-language:EN-GB'>Delta
wing produce higher lift at high pitch attitude angle values, but generate also
high drag. In order to maintain<span style="mso-spacerun: yes"> </span>proper
airspeed you<span style="mso-spacerun: yes"> </span>should increase the engines
power (around 7500 to 7800 rpm). If for some reasons (e.g. wind gust) the
airspeed decrease, one must react promptly to avoid pitch<span
style="mso-spacerun: yes"> </span>instability. Dassault Aircraft have included<span
style="mso-spacerun: yes"> </span>an automatic airspeed regulator for final
approach. To activate this system use the lever at left of the throttle levers.
To reduce the workload of the virtual pilot we have develop an auto-throttle
that compute the proper approach airspeed with respect to weight of the
aircraft.<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<h3 style='margin-left:0cm;text-indent:0cm;tab-stops:0cm'><span lang=EN-GB
style='mso-ansi-language:EN-GB'>Landing<o:p></o:p></span></h3>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'>The ground
effect is important with this aircraft and help to round out the path. You
should land with constant angle of attack and cut engine power only after the
touch down. Otherwise a big bang may be hear meaning that the tires are not
happy with the landing. LOL !.<span style="mso-spacerun: yes"> </span>After
touch down maintain the angle of attack for an aerodynamic slow down. Then
activate air brake and drag chute. The drag chute is activated using the
folding wing keyboard command. The drag chute reduce airspeed. During the
activation of the drag chute the engines rotation speed<span
style="mso-spacerun: yes"> </span>increase. This is a secondary effect due to
FS limitation.<o:p></o:p></span></p>
<p class=MsoNormal><span lang=EN-GB style='mso-ansi-language:EN-GB'><![if !supportEmptyParas]> <![endif]><o:p></o:p></span></p>
<p class=MsoNormal><b><i><u><span lang=EN-GB style='mso-ansi-language:EN-GB'>Conclusion:
Mirage IV is a demanding aircraft to fly. So take the time to read attentively
this document<o:p></o:p></span></u></i></b></p>
<p class=MsoNormal style='margin-left:141.6pt;text-indent:35.4pt'><span
lang=EN-GB style='mso-ansi-language:EN-GB'>Bee Gee<span style="mso-spacerun:
yes"> </span>February 2008<o:p></o:p></span></p>
<p class=MsoNormal style='margin-left:141.6pt;text-indent:35.4pt'><span
lang=EN-GB style='mso-ansi-language:EN-GB'>English translation<span
style="mso-spacerun: yes"> </span>Benoit M. Dubй <o:p></o:p></span></p>
<p class=MsoNormal style='margin-left:141.6pt;text-indent:35.4pt'><span
lang=EN-GB style='mso-ansi-language:EN-GB'>Many thanks<span
style="mso-spacerun: yes"> </span>Benoit…..<o:p></o:p></span></p>
</div>
</body>
</html>
26364-M4P.ZIP
| Имя файла | Дата | Размер |
|---|---|---|
| M4P/ | 08.01.2010 13:48 | |
| M4P/Aircraft.cfg | 19.04.2008 03:04 | 20 KB |
| M4P/effects/ | 08.01.2010 13:47 | |
| M4P/effects/fx_mirage_BURN_ONE.fx | 22.10.2003 20:42 | 19 KB |
| M4P/effects/fx_mirage_BURN_TWO.fx | 22.10.2003 20:42 | 23 KB |
| M4P/effects/fx_mirage_GLITTER.fx | 22.10.2003 19:49 | 4 KB |
| M4P/effects/fx_mirage_TORCH_FLAM.fx | 21.10.2007 23:32 | 22 KB |
| M4P/effects/texture/ | 08.01.2010 13:47 | |
| M4P/effects/texture/fx_2.bmp | 19.06.2001 01:14 | 171 KB |
| M4P/effects/texture/Thumbs.db | 18.11.2007 22:36 | 6 KB |
| M4P/Mirage IV_panel_manual.pdf | 10.03.2008 04:17 | 7 MB |
| M4P/MirageIV-bg19.air | 21.02.2008 13:37 | 10 KB |
| M4P/MirageIV-bg19J.air | 21.02.2008 14:57 | 10 KB |
| M4P/MIRAGE_IV_flight_procedures/ | 08.01.2010 13:47 | |
| M4P/MIRAGE_IV_flight_procedures/English_language.txt | 10.03.2008 03:19 | 279 B |
| M4P/MIRAGE_IV_flight_procedures/MIRAGE_IV_flight_procedures_fichiers/ | 08.01.2010 13:47 | |
| M4P/MIRAGE_IV_flight_procedures/MIRAGE_IV_flight_procedures_fichiers/filelist.xml | 10.03.2008 03:01 | 760 B |
| M4P/MIRAGE_IV_flight_procedures/MIRAGE_IV_flight_procedures_fichiers/image001.jpg | 10.03.2008 03:01 | 136 KB |
| M4P/MIRAGE_IV_flight_procedures/MIRAGE_IV_flight_procedures_fichiers/image002.jpg | 10.03.2008 03:01 | 35 KB |
| M4P/MIRAGE_IV_flight_procedures/MIRAGE_IV_flight_procedures_fichiers/image003.gif | 10.03.2008 03:01 | 121 B |
| M4P/MIRAGE_IV_flight_procedures/MIRAGE_IV_flight_procedures_fichiers/image004.gif | 10.03.2008 03:01 | 172 B |
| M4P/MIRAGE_IV_flight_procedures/MIRAGE_IV_flight_procedures_fichiers/image005.jpg | 10.03.2008 03:01 | 60 KB |
| M4P/MIRAGE_IV_flight_procedures/MIRAGE_IV_flight_procedures_fichiers/image006.jpg | 10.03.2008 03:01 | 30 KB |
| M4P/MIRAGE_IV_flight_procedures/MIRAGE_IV_flight_procedures_fichiers/image007.jpg | 10.03.2008 03:01 | 180 KB |
| M4P/MIRAGE_IV_flight_procedures/MIRAGE_IV_flight_procedures_fichiers/image008.jpg | 10.03.2008 03:01 | 32 KB |
| M4P/MIRAGE_IV_flight_procedures/MIRAGE_IV_flight_procedures_fichiers/image009.wmz | 10.03.2008 03:01 | 43 KB |
| M4P/MIRAGE_IV_flight_procedures/MIRAGE_IV_flight_procedures_fichiers/image010.gif | 10.03.2008 03:01 | 46 KB |
| M4P/MIRAGE_IV_flight_procedures/MIRAGE_IV_flight_procedures_fichiers/image011.jpg | 10.03.2008 03:01 | 80 KB |
| M4P/MIRAGE_IV_flight_procedures/MIRAGE_IV_flight_procedures_fichiers/image012.jpg | 10.03.2008 03:01 | 31 KB |
| M4P/MIRAGE_IV_flight_procedures/MIRAGE_IV_flight_procedures_fichiers/image013.jpg | 10.03.2008 03:01 | 72 KB |
| M4P/MIRAGE_IV_flight_procedures/MIRAGE_IV_flight_procedures_fichiers/image014.jpg | 10.03.2008 03:01 | 34 KB |
| M4P/MIRAGE_IV_flight_procedures/MIRAGE_IV_flight_procedures_fichiers/image015.jpg | 10.03.2008 03:01 | 184 KB |
| M4P/MIRAGE_IV_flight_procedures/MIRAGE_IV_flight_procedures_fichiers/image016.jpg | 10.03.2008 03:01 | 34 KB |
| M4P/MIRAGE_IV_flight_procedures/MIRAGE_IV_flight_procedures_fichiers/image017.jpg | 10.03.2008 03:01 | 156 KB |
| M4P/MIRAGE_IV_flight_procedures/MIRAGE_IV_flight_procedures_fichiers/image018.jpg | 10.03.2008 03:01 | 27 KB |
| M4P/MIRAGE_IV_flight_procedures/MIRAGE_IV_flight_procedures_fichiers/oledata.mso | 10.03.2008 03:01 | 76 KB |
| M4P/MIRAGE_IV_flight_procedures/MIRAGE_IV_flight_procedures_fichiers/Thumbs.db | 10.03.2008 03:14 | 33 KB |
| M4P/MIRAGE_IV_flight_procedures/MP4_check.htm | 10.03.2008 03:01 | 88 KB |
| M4P/MIRAGE_IV_flight_procedures.pdf | 05.03.2008 19:24 | 5 MB |
| M4P/model/ | 08.01.2010 13:47 | |
| M4P/model/mirage 4.mdl | 12.03.2008 14:08 | 4 MB |
| M4P/model/Model.cfg | 25.12.2003 18:12 | 25 B |
| M4P/model.JATO/ | 08.01.2010 13:47 | |
| M4P/model.JATO/mirage 4.mdl | 12.03.2008 00:39 | 4 MB |
| M4P/model.JATO/Model.cfg | 25.12.2003 18:12 | 25 B |
| M4P/MP4_check.htm | 05.03.2008 21:42 | 56 KB |
| M4P/MP4_check_fichiers/ | 08.01.2010 13:47 | |
| M4P/MP4_check_fichiers/filelist.xml | 05.03.2008 21:42 | 742 B |
| M4P/MP4_check_fichiers/image001.jpg | 05.03.2008 21:42 | 135 KB |
| M4P/MP4_check_fichiers/image002.jpg | 05.03.2008 21:42 | 35 KB |
| M4P/MP4_check_fichiers/image003.gif | 05.03.2008 21:42 | 172 B |
| M4P/MP4_check_fichiers/image004.gif | 05.03.2008 21:42 | 121 B |
| M4P/MP4_check_fichiers/image005.jpg | 05.03.2008 21:42 | 59 KB |
| M4P/MP4_check_fichiers/image006.jpg | 05.03.2008 21:42 | 30 KB |
| M4P/MP4_check_fichiers/image007.jpg | 05.03.2008 21:42 | 179 KB |
| M4P/MP4_check_fichiers/image008.jpg | 05.03.2008 21:42 | 32 KB |
| M4P/MP4_check_fichiers/image009.wmz | 05.03.2008 21:42 | 43 KB |
| M4P/MP4_check_fichiers/image010.gif | 05.03.2008 21:42 | 46 KB |
| M4P/MP4_check_fichiers/image011.jpg | 05.03.2008 21:42 | 78 KB |
| M4P/MP4_check_fichiers/image012.jpg | 05.03.2008 21:42 | 31 KB |
| M4P/MP4_check_fichiers/image013.jpg | 05.03.2008 21:42 | 70 KB |
| M4P/MP4_check_fichiers/image014.jpg | 05.03.2008 21:42 | 34 KB |
| M4P/MP4_check_fichiers/image015.jpg | 05.03.2008 21:42 | 182 KB |
| M4P/MP4_check_fichiers/image016.jpg | 05.03.2008 21:42 | 35 KB |
| M4P/MP4_check_fichiers/image017.jpg | 05.03.2008 21:42 | 156 KB |
| M4P/MP4_check_fichiers/image018.jpg | 05.03.2008 21:42 | 32 KB |
| M4P/MP4_check_fichiers/oledata.mso | 05.03.2008 21:42 | 76 KB |
| M4P/MP4_check_fichiers/Thumbs.db | 10.03.2008 02:47 | 57 KB |
| M4P/panel/ | 08.01.2010 13:47 | |
| M4P/panel/$cvM4p.bmp | 19.02.2008 23:59 | 3 MB |
| M4P/panel/$cvM4pBK.bmp | 10.02.2008 19:55 | 768 KB |
| M4P/panel/Mirage4_Empty.bmp | 07.04.2003 04:50 | 768 KB |
| M4P/panel/Mirage4_Fuel.bmp | 08.10.2007 21:27 | 521 KB |
| M4P/panel/Mirage4_IFR.bmp | 23.08.2007 23:09 | 2 MB |
| M4P/panel/Mirage4_Instr.gau | 29.02.2008 16:04 | 9 MB |
| M4P/panel/Mirage4_Landing.bmp | 09.08.2007 18:12 | 2 MB |
| M4P/panel/Mirage4_Left_Bank.bmp | 22.10.2007 18:26 | 579 KB |
| M4P/panel/Mirage4_Right_Bank.bmp | 21.08.2007 19:58 | 642 KB |
| M4P/panel/Mirage4_Timer.bmp | 10.08.2007 18:06 | 32 KB |
| M4P/panel/Mirage4_VFR.bmp | 25.07.2007 14:57 | 2 MB |
| M4P/panel/Panel.cfg | 02.03.2008 22:58 | 24 KB |
| M4P/panel/Thumbs.db | 25.04.2008 03:42 | 23 KB |
| M4P/ReadmeM4P.txt | 25.04.2008 15:21 | 1 KB |
| M4P/ReadmeMirage4English.pdf | 13.03.2008 03:03 | 37 MB |
| M4P/soonMp4fsXsp2/ | 08.01.2010 13:47 | |
| M4P/soonMp4fsXsp2/AAfsx1.jpg | 04.04.2008 16:18 | 104 KB |
| M4P/soonMp4fsXsp2/AAfsx10.jpg | 04.04.2008 16:25 | 23 KB |
| M4P/soonMp4fsXsp2/AAfsx11.jpg | 04.04.2008 16:25 | 24 KB |
| M4P/soonMp4fsXsp2/AAfsx2.jpg | 04.04.2008 16:18 | 97 KB |
| M4P/soonMp4fsXsp2/AAfsx3.jpg | 04.04.2008 16:19 | 37 KB |
| M4P/soonMp4fsXsp2/AAfsx4.jpg | 04.04.2008 16:19 | 38 KB |
| M4P/soonMp4fsXsp2/AAfsx5.jpg | 04.04.2008 16:20 | 38 KB |
| M4P/soonMp4fsXsp2/AAfsx6.jpg | 04.04.2008 16:20 | 37 KB |
| M4P/soonMp4fsXsp2/AAfsx7.jpg | 04.04.2008 16:21 | 46 KB |
| M4P/soonMp4fsXsp2/AAfsx8.jpg | 04.04.2008 16:21 | 30 KB |
| M4P/soonMp4fsXsp2/AAfsx9.jpg | 04.04.2008 16:24 | 22 KB |
| M4P/soonMp4fsXsp2/aaNewJ1.jpg | 08.04.2008 04:26 | 45 KB |
| M4P/soonMp4fsXsp2/aaNewJ10.jpg | 08.04.2008 04:26 | 23 KB |
| M4P/soonMp4fsXsp2/aaNewJ11.jpg | 08.04.2008 04:26 | 34 KB |
| M4P/soonMp4fsXsp2/aaNewJ12.jpg | 08.04.2008 04:26 | 43 KB |
| M4P/soonMp4fsXsp2/aaNewJ13.jpg | 08.04.2008 04:26 | 27 KB |
| M4P/soonMp4fsXsp2/aaNewJ14.jpg | 08.04.2008 04:26 | 36 KB |
| M4P/soonMp4fsXsp2/aaNewJ15.jpg | 08.04.2008 04:26 | 36 KB |
| M4P/soonMp4fsXsp2/aaNewJ16.jpg | 08.04.2008 04:26 | 69 KB |
| M4P/soonMp4fsXsp2/aaNewJ17.jpg | 08.04.2008 04:26 | 63 KB |
| M4P/soonMp4fsXsp2/aaNewJ18.jpg | 08.04.2008 04:26 | 25 KB |
| M4P/soonMp4fsXsp2/aaNewJ2.jpg | 08.04.2008 04:26 | 65 KB |
| M4P/soonMp4fsXsp2/aaNewJ3.jpg | 08.04.2008 04:26 | 40 KB |
| M4P/soonMp4fsXsp2/aaNewJ4.jpg | 08.04.2008 04:26 | 46 KB |
| M4P/soonMp4fsXsp2/aaNewJ5.jpg | 08.04.2008 04:26 | 46 KB |
| M4P/soonMp4fsXsp2/aaNewJ6.jpg | 08.04.2008 04:26 | 63 KB |
| M4P/soonMp4fsXsp2/aaNewJ7.jpg | 08.04.2008 04:26 | 43 KB |
| M4P/soonMp4fsXsp2/aaNewJ8.jpg | 08.04.2008 04:26 | 51 KB |
| M4P/soonMp4fsXsp2/aaNewJ9.jpg | 08.04.2008 04:26 | 22 KB |
| M4P/soonMp4fsXsp2/Thumbs.db | 25.04.2008 03:52 | 79 KB |
| M4P/sound/ | 08.01.2010 13:50 | |
| M4P/sound/BAN1STRT.WAV | 01.05.2003 07:00 | 279 KB |
| M4P/sound/BAN2STRT.WAV | 01.05.2003 07:00 | 45 KB |
| M4P/sound/door_close.wav | 25.06.2004 03:38 | 157 KB |
| M4P/sound/door_open.wav | 25.06.2004 03:38 | 157 KB |
| M4P/sound/jet2.wav | 25.06.2004 22:21 | 70 KB |
| M4P/sound/jet3comb.wav | 15.09.2005 16:43 | 399 KB |
| M4P/sound/jet4.wav | 14.01.2005 14:19 | 395 KB |
| M4P/sound/jet4comb.wav | 15.09.2005 16:46 | 299 KB |
| M4P/sound/jeta.wav | 22.06.2004 20:52 | 27 KB |
| M4P/sound/jetb.wav | 22.06.2004 20:53 | 22 KB |
| M4P/sound/jetc.wav | 22.06.2004 20:52 | 22 KB |
| M4P/sound/jetflaps.wav | 15.09.2005 17:11 | 55 KB |
| M4P/sound/jetgear.wav | 20.09.2005 23:58 | 333 KB |
| M4P/sound/jetovsp.wav | 21.06.2004 08:46 | 4 KB |
| M4P/sound/jetroll.wav | 22.06.2004 20:52 | 371 KB |
| M4P/sound/jetroll2.wav | 22.06.2004 20:51 | 353 KB |
| M4P/sound/jetstall.wav | 21.06.2004 08:45 | 10 KB |
| M4P/sound/jetwind.wav | 14.01.2005 14:37 | 395 KB |
| M4P/sound/jetx1.wav | 14.01.2005 15:04 | 250 KB |
| M4P/sound/jetx2.WAV | 14.01.2005 15:01 | 78 KB |
| M4P/sound/jetx2comb.wav | 12.01.2005 14:15 | 221 KB |
| M4P/sound/jetx3.wav | 14.01.2005 14:40 | 418 KB |
| M4P/sound/jetx3comb.wav | 05.09.2005 09:00 | 948 KB |
| M4P/sound/jetx4.wav | 18.02.2005 13:55 | 97 KB |
| M4P/sound/jetx4comb.wav | 14.01.2005 15:57 | 441 KB |
| M4P/sound/sound.cfg | 21.06.2004 08:54 | 7 KB |
| M4P/sound/Xban1shut.WAV | 05.09.2005 09:16 | 483 KB |
| M4P/sound/Xban1strt.WAV | 05.09.2005 09:19 | 1 MB |
| M4P/sound/XBAN2STRT.WAV | 05.09.2005 09:17 | 516 KB |
| M4P/texture/ | 08.01.2010 13:47 | |
| M4P/texture/amp4cab.bmp | 16.01.2008 21:26 | 1 MB |
| M4P/texture/ATTERRISSEURS.bmp | 06.12.2007 22:45 | 1 MB |
| M4P/texture/cab2.bmp | 12.01.2008 05:24 | 1 MB |
| M4P/texture/cabine_T.bmp | 05.01.2008 20:11 | 1 MB |
| M4P/texture/canopM4_T.bmp | 28.01.2008 04:40 | 64 KB |
| M4P/texture/casquemoteur.bmp | 05.03.2007 20:15 | 1 MB |
| M4P/texture/cvM4p.bmp | 10.03.2008 18:13 | 1 MB |
| M4P/texture/cvM4pbank.bmp | 17.02.2008 19:16 | 1 MB |
| M4P/texture/deltaDR_T.bmp | 06.12.2007 23:11 | 1 MB |
| M4P/texture/deltaG_T.bmp | 06.12.2007 23:12 | 1 MB |
| M4P/texture/dorsal_T.bmp | 04.02.2008 18:59 | 1 MB |
| M4P/texture/grey2_L.bmp | 19.02.2008 16:07 | 1 MB |
| M4P/texture/grey3_L.bmp | 13.02.2008 14:50 | 256 KB |
| M4P/texture/grey4_L.bmp | 13.02.2008 14:45 | 1 MB |
| M4P/texture/grey5_L.bmp | 13.02.2008 14:38 | 1 MB |
| M4P/texture/grey6_L.bmp | 13.02.2008 05:43 | 64 KB |
| M4P/texture/grey_L.bmp | 19.02.2008 23:46 | 1 MB |
| M4P/texture/LIGHT_LAND.bmp | 03.12.2003 18:05 | 21 KB |
| M4P/texture/MP4_LM.bmp | 05.10.2007 22:39 | 16 KB |
| M4P/texture/pilotesiege.bmp | 09.01.2008 16:36 | 1 MB |
| M4P/texture/radarDR_T.bmp | 06.12.2007 23:06 | 1 MB |
| M4P/texture/radar_T.bmp | 05.02.2008 19:27 | 1 MB |
| M4P/texture/vetvol.bmp | 09.09.2007 20:45 | 1 MB |
| M4P/texture/voilureDR_T.bmp | 06.12.2007 23:07 | 1 MB |
| M4P/texture/voilureG_T.bmp | 06.12.2007 23:07 | 1 MB |
| M4P/texture.Alu/ | 08.01.2010 13:47 | |
| M4P/texture.Alu/amp4cab.bmp | 16.01.2008 21:26 | 1 MB |
| M4P/texture.Alu/ATTERRISSEURS.bmp | 06.12.2007 22:45 | 1 MB |
| M4P/texture.Alu/cab2.bmp | 12.01.2008 05:24 | 1 MB |
| M4P/texture.Alu/cabine_T.bmp | 05.01.2008 20:11 | 1 MB |
| M4P/texture.Alu/canopM4_T.bmp | 28.01.2008 04:40 | 64 KB |
| M4P/texture.Alu/casquemoteur.bmp | 05.03.2007 20:15 | 1 MB |
| M4P/texture.Alu/cvM4p.bmp | 10.03.2008 18:13 | 1 MB |
| M4P/texture.Alu/cvM4pbank.bmp | 17.02.2008 19:16 | 1 MB |
| M4P/texture.Alu/deltaDR_T.bmp | 07.12.2007 20:35 | 1 MB |
| M4P/texture.Alu/deltaG_T.bmp | 07.12.2007 19:00 | 1 MB |
| M4P/texture.Alu/dorsal_T.bmp | 12.01.2008 05:33 | 1 MB |
| M4P/texture.Alu/grey2_L.bmp | 19.02.2008 16:07 | 1 MB |
| M4P/texture.Alu/grey3_L.bmp | 13.02.2008 14:50 | 256 KB |
| M4P/texture.Alu/grey4_L.bmp | 13.02.2008 14:45 | 1 MB |
| M4P/texture.Alu/grey5_L.bmp | 13.02.2008 14:38 | 1 MB |
| M4P/texture.Alu/grey6_L.bmp | 13.02.2008 05:43 | 64 KB |
| M4P/texture.Alu/grey_L.bmp | 19.02.2008 23:46 | 1 MB |
| M4P/texture.Alu/LIGHT_LAND.bmp | 03.12.2003 18:05 | 21 KB |
| M4P/texture.Alu/MP4_LM.bmp | 05.10.2007 22:39 | 16 KB |
| M4P/texture.Alu/pilotesiege.bmp | 09.01.2008 16:36 | 1 MB |
| M4P/texture.Alu/radarDR_T.bmp | 23.02.2008 03:54 | 1 MB |
| M4P/texture.Alu/radar_T.bmp | 21.12.2007 23:19 | 1 MB |
| M4P/texture.Alu/vetvol.bmp | 09.09.2007 20:45 | 1 MB |
| M4P/texture.Alu/voilureDR_T.bmp | 24.12.2007 00:14 | 1 MB |
| M4P/texture.Alu/voilureG_T.bmp | 08.01.2008 06:29 | 1 MB |
| M4P/texture.AX/ | 08.01.2010 13:47 | |
| M4P/texture.AX/amp4cab.bmp | 16.01.2008 21:26 | 1 MB |
| M4P/texture.AX/ATTERRISSEURS.bmp | 06.12.2007 22:45 | 1 MB |
| M4P/texture.AX/cab2.bmp | 12.01.2008 05:24 | 1 MB |
| M4P/texture.AX/cabine_T.bmp | 05.01.2008 20:11 | 1 MB |
| M4P/texture.AX/canopM4_T.bmp | 28.01.2008 04:40 | 64 KB |
| M4P/texture.AX/casquemoteur.bmp | 05.03.2007 20:15 | 1 MB |
| M4P/texture.AX/cvM4p.bmp | 10.03.2008 18:13 | 1 MB |
| M4P/texture.AX/cvM4pbank.bmp | 17.02.2008 19:16 | 1 MB |
| M4P/texture.AX/deltaDR_T.bmp | 06.12.2007 23:25 | 1 MB |
| M4P/texture.AX/deltaG_T.bmp | 06.12.2007 23:25 | 1 MB |
| M4P/texture.AX/dorsal_T.bmp | 04.02.2008 19:18 | 1 MB |
| M4P/texture.AX/grey2_L.bmp | 19.02.2008 16:07 | 1 MB |
| M4P/texture.AX/grey3_L.bmp | 13.02.2008 14:50 | 256 KB |
| M4P/texture.AX/grey4_L.bmp | 13.02.2008 14:45 | 1 MB |
| M4P/texture.AX/grey5_L.bmp | 13.02.2008 14:38 | 1 MB |
| M4P/texture.AX/grey6_L.bmp | 13.02.2008 05:43 | 64 KB |
| M4P/texture.AX/grey_L.bmp | 19.02.2008 23:46 | 1 MB |
| M4P/texture.AX/LIGHT_LAND.bmp | 03.12.2003 18:05 | 21 KB |
| M4P/texture.AX/MP4_LM.bmp | 05.10.2007 22:39 | 16 KB |
| M4P/texture.AX/pilotesiege.bmp | 09.01.2008 16:36 | 1 MB |
| M4P/texture.AX/radarDR_T.bmp | 06.12.2007 23:24 | 1 MB |
| M4P/texture.AX/radar_T.bmp | 05.02.2008 19:40 | 1 MB |
| M4P/texture.AX/Thumbs.db | 10.10.2007 16:09 | 8 KB |
| M4P/texture.AX/vetvol.bmp | 09.09.2007 20:45 | 1 MB |
| M4P/texture.AX/voilureDR_T.bmp | 06.12.2007 23:21 | 1 MB |
| M4P/texture.AX/voilureG_T.bmp | 06.12.2007 23:22 | 1 MB |
| M4P/texture.Blanc/ | 08.01.2010 13:47 | |
| M4P/texture.Blanc/amp4cab.bmp | 16.01.2008 21:26 | 1 MB |
| M4P/texture.Blanc/ATTERRISSEURS.bmp | 06.12.2007 22:45 | 1 MB |
| M4P/texture.Blanc/cab2.bmp | 12.01.2008 05:24 | 1 MB |
| M4P/texture.Blanc/cabine_T.bmp | 05.01.2008 20:11 | 1 MB |
| M4P/texture.Blanc/canopM4_T.bmp | 28.01.2008 04:40 | 64 KB |
| M4P/texture.Blanc/casquemoteur.bmp | 05.03.2007 20:15 | 1 MB |
| M4P/texture.Blanc/cvM4p.bmp | 10.03.2008 18:13 | 1 MB |
| M4P/texture.Blanc/cvM4pbank.bmp | 17.02.2008 19:16 | 1 MB |
| M4P/texture.Blanc/deltaDR_T.bmp | 11.12.2007 16:14 | 1 MB |
| M4P/texture.Blanc/deltaG_T.bmp | 11.12.2007 15:32 | 1 MB |
| M4P/texture.Blanc/dorsal_T.bmp | 04.02.2008 19:36 | 1 MB |
| M4P/texture.Blanc/grey2_L.bmp | 19.02.2008 16:07 | 1 MB |
| M4P/texture.Blanc/grey3_L.bmp | 13.02.2008 14:50 | 256 KB |
| M4P/texture.Blanc/grey4_L.bmp | 13.02.2008 14:45 | 1 MB |
| M4P/texture.Blanc/grey5_L.bmp | 13.02.2008 14:38 | 1 MB |
| M4P/texture.Blanc/grey6_L.bmp | 13.02.2008 05:43 | 64 KB |
| M4P/texture.Blanc/grey_L.bmp | 19.02.2008 23:46 | 1 MB |
| M4P/texture.Blanc/LIGHT_LAND.bmp | 03.12.2003 18:05 | 21 KB |
| M4P/texture.Blanc/MP4_LM.bmp | 05.10.2007 22:39 | 16 KB |
| M4P/texture.Blanc/pilotesiege.bmp | 09.01.2008 16:36 | 1 MB |
| M4P/texture.Blanc/radarDR_T.bmp | 11.12.2007 19:36 | 1 MB |
| M4P/texture.Blanc/radar_T.bmp | 11.12.2007 19:32 | 1 MB |
| M4P/texture.Blanc/vetvol.bmp | 09.09.2007 20:45 | 1 MB |
| M4P/texture.Blanc/voilureDR_T.bmp | 10.12.2007 22:26 | 1 MB |
| M4P/texture.Blanc/voilureG_T.bmp | 10.12.2007 22:25 | 1 MB |
| M4P/texture.celebration/ | 08.01.2010 13:47 | |
| M4P/texture.celebration/amp4cab.bmp | 16.01.2008 21:26 | 1 MB |
| M4P/texture.celebration/ATTERRISSEURS.bmp | 06.12.2007 22:45 | 1 MB |
| M4P/texture.celebration/cab2.bmp | 12.01.2008 05:24 | 1 MB |
| M4P/texture.celebration/cabine_T.bmp | 05.01.2008 20:11 | 1 MB |
| M4P/texture.celebration/canopM4_T.bmp | 28.01.2008 04:40 | 64 KB |
| M4P/texture.celebration/casquemoteur.bmp | 05.03.2007 20:15 | 1 MB |
| M4P/texture.celebration/cvM4p.bmp | 10.03.2008 18:13 | 1 MB |
| M4P/texture.celebration/cvM4pbank.bmp | 17.02.2008 19:16 | 1 MB |
| M4P/texture.celebration/deltaDR_T.bmp | 06.12.2007 16:15 | 1 MB |
| M4P/texture.celebration/deltaG_T.bmp | 06.12.2007 16:07 | 1 MB |
| M4P/texture.celebration/dorsal_T.bmp | 04.02.2008 19:44 | 1 MB |
| M4P/texture.celebration/grey2_L.bmp | 19.02.2008 16:07 | 1 MB |
| M4P/texture.celebration/grey3_L.bmp | 13.02.2008 14:50 | 256 KB |
| M4P/texture.celebration/grey4_L.bmp | 13.02.2008 14:45 | 1 MB |
| M4P/texture.celebration/grey5_L.bmp | 13.02.2008 14:38 | 1 MB |
| M4P/texture.celebration/grey6_L.bmp | 13.02.2008 05:43 | 64 KB |
| M4P/texture.celebration/grey_L.bmp | 19.02.2008 23:46 | 1 MB |
| M4P/texture.celebration/LIGHT_LAND.bmp | 03.12.2003 18:05 | 21 KB |
| M4P/texture.celebration/MP4_LM.bmp | 05.10.2007 22:39 | 16 KB |
| M4P/texture.celebration/pilotesiege.bmp | 09.01.2008 16:36 | 1 MB |
| M4P/texture.celebration/radarDR_T.bmp | 06.12.2007 15:47 | 1 MB |
| M4P/texture.celebration/radar_T.bmp | 05.02.2008 19:19 | 1 MB |
| M4P/texture.celebration/vetvol.bmp | 09.09.2007 20:45 | 1 MB |
| M4P/texture.celebration/voilureDR_T.bmp | 06.12.2007 15:55 | 1 MB |
| M4P/texture.celebration/voilureG_T.bmp | 06.12.2007 16:02 | 1 MB |
| M4P/texture.UN/ | 08.01.2010 13:47 | |
| M4P/texture.UN/amp4cab.bmp | 16.01.2008 21:26 | 1 MB |
| M4P/texture.UN/ATTERRISSEURS.bmp | 06.12.2007 22:45 | 1 MB |
| M4P/texture.UN/cab2.bmp | 12.01.2008 05:24 | 1 MB |
| M4P/texture.UN/cabine_T.bmp | 05.01.2008 20:11 | 1 MB |
| M4P/texture.UN/canopM4_T.bmp | 28.01.2008 04:40 | 64 KB |
| M4P/texture.UN/casquemoteur.bmp | 05.03.2007 20:15 | 1 MB |
| M4P/texture.UN/cvM4p.bmp | 10.03.2008 18:13 | 1 MB |
| M4P/texture.UN/cvM4pbank.bmp | 17.02.2008 19:16 | 1 MB |
| M4P/texture.UN/deltaDR_T.bmp | 06.12.2007 23:11 | 1 MB |
| M4P/texture.UN/deltaG_T.bmp | 06.12.2007 23:12 | 1 MB |
| M4P/texture.UN/dorsal_T.bmp | 04.02.2008 19:25 | 1 MB |
| M4P/texture.UN/grey2_L.bmp | 19.02.2008 16:07 | 1 MB |
| M4P/texture.UN/grey3_L.bmp | 13.02.2008 14:50 | 256 KB |
| M4P/texture.UN/grey4_L.bmp | 13.02.2008 14:45 | 1 MB |
| M4P/texture.UN/grey5_L.bmp | 13.02.2008 14:38 | 1 MB |
| M4P/texture.UN/grey6_L.bmp | 13.02.2008 05:43 | 64 KB |
| M4P/texture.UN/grey_L.bmp | 19.02.2008 23:46 | 1 MB |
| M4P/texture.UN/LIGHT_LAND.bmp | 03.12.2003 18:05 | 21 KB |
| M4P/texture.UN/MP4_LM.bmp | 05.10.2007 22:39 | 16 KB |
| M4P/texture.UN/pilotesiege.bmp | 09.01.2008 16:36 | 1 MB |
| M4P/texture.UN/radarDR_T.bmp | 06.12.2007 23:06 | 1 MB |
| M4P/texture.UN/radar_T.bmp | 05.02.2008 19:27 | 1 MB |
| M4P/texture.UN/vetvol.bmp | 09.09.2007 20:45 | 1 MB |
| M4P/texture.UN/voilureDR_T.bmp | 06.12.2007 23:07 | 1 MB |
| M4P/texture.UN/voilureG_T.bmp | 06.12.2007 23:07 | 1 MB |
| avsim_su.diz | 08.01.2010 18:52 | 406 B |
| Итого: | 214 MB | |
Mirage IV.
| Rating: 5!
Developer: Dassault Country: France First flight: 1959 Type: Strategic bomber modification Mirage IV Wingspan, m 11.85 Length, m 23.49 Height, 5.40 m Wing area, m2 Weight 78.00 kg empty plane 14500 maximum take-off 33475 Fuel, l, the internal 19000 PTB 2 x 2500 Type 2 Engine Turbojet SNECMA Atar 9K-50 (9K14) Thrust, kN neforsirovannaya 49.03 forced 70.61 Maximum speed km / h at an altitude of 11000 m 2340 (M = 2.20) at sea level, 1349 (M = 1.27) Cruising speed, km / h 1913 (M = 1.80) Range, 4000 miles Combat range, km Maximum rate of climb 1240 m / min Service ceiling 2588 m 18500 Takeoff, Mileage 1700 m, 700 m Landing speed, km / h 260 being developed as a carrier of nuclear weapons (including). Because it uses the sounds of credit default Boeing 737, they are replaced by the sounds of another Mirage. Six textures. Realistic dynamics. Without Forsazh very hard climb. Good development. A detailed manual on the panel and flight procedures.
→ Size:
103 MB
→ Date:
16 years ago (08.01.2010 18:35)
→ Author:
Roland Laborie.
→ Approved by moderator:
Lenya69
→ License:
Freeware - Free version, Unlimited Distribution
→ Downloaded:
3843 time(s)