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› Flaps at high altitudes
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Flaps at high altitudes (Read 1003 times)
May 26
th
, 2004 at 9:30pm
rgenius
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Captain
Philippines
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Posts: 3
Hi there, im a newbie fs pilot; and i have this trouble flying 747's at high altitude. say im flying at 35,000 at .80M, my plane suddenly turns into a stall. im on autopilot.
i tried again but now i put on flaps at that height and it seems to stabilize the plane at 5 deg pitch-up. is this really what pilots do up there? wont it damage the flaps at that speed. or im just doing it wrong.
rgen
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Reply #1 -
May 26
th
, 2004 at 10:42pm
Nexus
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The greater of two evils...
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Posts: 3282
Yes flaps would NOT like that
Maximum flap extension altitude for the big Boeings is 20.000ft
The reason why you're stalling may be because you're just too heavy to fly M.80 at those altitudes. If an aircraft has to take off with full fuel loads it will use
step climbs
. It basically means that you fly to an intermediate flight level, then level off until you've burned enough fuel so you can continue the climb to a higher flight level and still maintain the same speed.
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Reply #2 -
May 27
th
, 2004 at 12:49am
rgenius
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Philippines
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Posts: 3
but still i can go up as high as 35k?
what is the suggested vertical climb/min for 747's? i may have done this wrong, because i placed it at 1k/min; that could have caused it to pitch so high.
other suggestions...
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Reply #3 -
May 27
th
, 2004 at 4:31am
Ivan
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Colonel
No, I'm NOT Russian, I
only like Russian aircraft
The netherlands
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Posts: 6058
vertical climb in the 747...
you need a step climb, start with leveling at 30000ft
VS rate at 2500fpm until at 25000ft while doing 280kts IAS
decrease VSI to around 1000 after passing 25000 and keep speed hold until you get to M.60 then switch to mach hold
when level go to M.82-.85
Dont go over 91%N1 RPM
Keep track of the N1 rpm and climb a few 100ft when it drops under 91%
maximum altitude you can get is around 45000 ft
Russian planes:
IL-76 (all standard length ones)
,
Tu-154 and Il-62
,
Tu-134
and
An-24RV
&&&&AI flightplans and repaints can be found
here
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Reply #4 -
May 27
th
, 2004 at 8:17am
Nexus
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The greater of two evils...
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Posts: 3282
Quote:
vertical climb in the 747...
you need a step climb, start with leveling at 30000ft
VS rate at 2500fpm until at 25000ft while doing 280kts IAS
decrease VSI to around 1000 after passing 25000 and keep speed hold until you get to M.60 then switch to mach hold
when level go to M.82-.85
Dont go over 91%N1 RPM
Keep track of the N1 rpm and climb a few 100ft when it drops under 91%
maximum altitude you can get is around 45000 ft
Why climb at m.60?
Just keep the 280-300kts or whatever unlil you reach mach-crossover altitude and then change to climb speed mach number. Should occure around FL260 - FL290.
Normal procedure.
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Reply #5 -
Jun 20
th
, 2004 at 4:59pm
jrpilot
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Isn't the plane in real life controlled by autopilot with the FMC (when autopilot is on)....wouldn't the Boeing climb itself to that height with LNAV and VNAV?
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Reply #6 -
Jun 20
th
, 2004 at 5:24pm
Craig.
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Birmingham
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VNAV, but yes the autopilot does it usually. side note the 777 and 767 have very strict flap speed limits an overspeed on them will require extensive maintanence on them, because of this many airlines have lowered the speeds by 5 to 10 knots to avoid any chance of damage, so high altitude wouldnt be a good idea:)
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Reply #7 -
Jun 20
th
, 2004 at 5:39pm
Nexus
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The greater of two evils...
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Posts: 3282
Quote:
VNAV, but yes the autopilot does it usually. side note the 777 and 767 have very strict flap speed limits an overspeed on them will require extensive maintanence on them, because of this many airlines have lowered the speeds by 5 to 10 knots to avoid any chance of damage, so high altitude wouldnt be a good idea:)
Same for the 737's, one some airlines they have decreases the flap 1 speed by 20kts (from 250 to 230) and flap 5 speed by 25kts(250-225)...cheap buggers
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Reply #8 -
Jun 20
th
, 2004 at 5:40pm
Craig.
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Birmingham
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LOL arnt they just:)
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