Good evening, would you tell me what are the reasons of Aviation Securuty was formed? Thank you

hi everyone , now im getting training as an airline pilot, im turning of the ATPL exams term, i would like to help anyone and get something from you .. i would be useful for all..
it would be

On articles that cite the source as the book "Weather", is there a link to said book?

why does an aircraft's centre of pressure move forward when it goes from transonic to supersonic flight?

hi buddy
i need help to solve a question
it is about meteorological radar
who can help me?
tisdell
passenger moving, nose landing gear, fuel burning
it coul move the cg of an acft

hi guys!!! is right to take single engine taxi as event?

normally ATR aircraft yes

what the effect of that?

just to save fuel
normally the companies do it to sava money of fuel burning, there is not effect to the engines
it because is one day for cut off one engine, and other day for the other engine. So there is no negative consequence fot it.
did u understand?

yes, little bit, i have another question what about high speed on approach 90s to touch down,?

what is 90s?

90 second

I think it depends os the acft class
if it is a small plane is easy to reduce speed.
but on a jet plane is it impossible because you need to be on a touchdown zone at Vref
if you are faster than expected you will increase the ASDA
and LDR will be longer.
Did you undertand?

yes. it is jet engine but how to measure the speed by indicated airspeed with out landing flap setting and 90 sceonds before touch down ? is right to set this event ?

OK
Are you talking about clean configuration?
with out flap setting?
so
What you need to know is that you must be 23% above the speed stol when you are approaching
if you stol speed is about 100kt, you must be 123kt
it will be the lowest speed to mantain with out flap setting

OK. what about highest speed with out landing flap setting .

for approach?

yes?

So, in my opnion there isn´t
it is up to you
it is up your feeling
the minimum speed there is but the highest i believe there isnt

thank you , that why i am confused, when work detail analysis with out flap setting it come high speed on approach event
OK, one more what about GPWS warning that possible come with out other warning?

What are you planning to do?
high speed
with out GPWS

GPWS warning is another question ?
not related with high speed

I know
i´m saying about the contest
context

i want to known is is tha possible to come gpws warning with out other warning like pull up...during detail analysis?

so man
i dont about that
sorry.

ok

try to find it on ACE the technical pilot interview

no problem, i just to known it.
ok. i will

i´m not sure about this question, when you find it just tell us he
here*

you guys, you work anaysis?

i´m not

ok

i´m pilot just.
bye

the thing is , i want understand this things form analysis perspective , but i am not pilot
ok , bye thank you very much for your assistance.

no worries brow

once aligned, the inertia navigation computer's always referenced to:?

centre of pressure and centre of gravity explained
email me for notes

im going to the the exams on monday, im beeing studying with the books and atplonline question bank
im freaking out because u have been reading that the bank is crap and staf
any advice how to master the exams?

orda havalar nasil ? burasi bom bok

get bristol or avexam

not atplonline?

hi anyone from germany here ?

here

oh cool, did you finished your exam at the LBA ?

are you finished with all the exams?

i have my first 7 exams in 3 week
weeks

oh nice

rip me :P

are these all bank questions or similar? im doing my first this week starting with met tommorw

selamin aleyküm

aleykum salam

do you know if cat software is adequate for good preparation?

a.s

as

yes these are probably bank questions

ok thanks
which flight school?

Ceylan join the Pilots and students group on facebook, many ppl asking about CAT
big one in uk :)

wow

im not familiar with german LBA and exam stuff

is that not the same as the ease?
easa*

its all in german :) probably a bit different
am I right?

questions in english

really? oh didnt know that cool!

atpl is usually always english isnt it

teaching in EN as well?

no german

i dont know. I you go for AVEXAM questiobank you can choose between german exam and english so I tought there is a differnece
lol why do they teach in german but test you in english :D

its better to learn in english since LBA questions are also in english
ähh idk

haha
which school?

RWL
german flight academy
so you r muslim

no im not
i know RWL and some students there

haha ok, cause you replied aleykumselam :D
oh ok

hi
any one here
whom i can aask a question

hi
what ll be the formula for calculating TAS

QIn order to produce an alternating voltage of 400 Hz, the number of poles required in an AC generator running at 6000 rpm is:
?
my ansr is coming out to be 8 but anser given in JAR is 4

Has anyone sat instruments at the CAA recently?

@gabbar. They should have asked for pole pairs (4) instead of poles (8). Calculations on this page: http://www.theairlinepilots.com/forum/viewtopic.php?t=505
Not your fault
nu you'll be needing the whiz wheel for TAS

Hellow Pilots

Hello

hello i have some quries

Hi all.

can somebody explane to me what a fire detection card is?
they are talking about it in the engine fire detection system explenation but i don't understand what the fire detection card is? is it like a sensor or something?

Hi, can anyone explain the difference between autopilot control inner loop and outer loop?
in details if possible

sure
inner loop is only Stabilization of the aircraft.
outer loop is the guidance function
stabilization like wings level or pitch. guidance like ALT HLD or HDG HLD

do you mean inner loop = stability augmention?
or autopilot and stability augmentation is a different thing?

the autopilot is also a tool for the stabilization of the aircraft
so stabilization is one part of the AP

So Stability augmentation systems is included in autopilot system?

yes :)
thats the inner loop

which relate to yaw/pitch damper?

yaw damper is stabilization
same as pitch and wings leveler (roll)

i see.
but inner loop can only stabilize the aircraft

:)
yes i think so! for the rest you have the outer loop

how does it maintain a particular heading without outer loop?
cause outer loop provide external input.
cause i read from a notes that is say that inner loop does not have the capability to main a particular eading or course
maintain*
sorry for the long question

hm
if it has an outer loop it can maintain heading...Im not sure what you mean that it misses the outer loop?
in the first part of ur question you are mixing it up :)
maybe lol

erm
ok wait i misread your chat
lol
stabilization like wings level or pitch. guidance like ALT HLD or HDG HLD
so inner loop can only stabilize aircraft like a yaw damper
and outer loop is like using the external source to guide the aircraft automatically to desired course?

yes

i see
thank you
so both works in a control loop with feedback

yes but watch out bc for example the yap damper feedbeck is only on the little gauge

what do you mean on a little gauge?

there is no actual movement of the pedals but there is for the roll on the yoke (in a boeing at least)
https://goo.gl/images/zX0dQF
pic of a yaw damper gauge

hmm
do you mean that only roll and pitch will have movement on the pedals?
and yaw does not?

not on the pedals but the other controls yes

i see
cause i am currently writing a report mainly focusing on the autopilot system inner & outer loop control

good luck with that

thanks
am i on the right track if i focus inner loop on stability augmentation system
and outerloop on holding pitch mode, heading mode, landing mode etc
like how the control loop works like a PID control

yes that should be good
check it with some other page as well

is this link relevant?
'inner loop: http://aerostudents.com/files/automaticFlightControl/stabilityAugmentationSystems.pdf
but too much formulas lol

looks good
im a student pilot so we dont learn too deeply abt this

i see
nice

good night and good luck with the assignement!

ok man
morning over here
haha

bye

bye

hello, i have a question
does somebody know what AIMS stands for
it has to do something with the overheat detection system
i hope somebody knows what it means because i can't find it online
y

@ Robbert: In some aircraft, in addition to fire and overheat detection, the Kidde continuous-loop system can supply nacelle temperature data to the airplane condition monitoring function of the aircraft in-flight monitoring system (AIMS). Check this link for the details on fire protection system.
http://www.theairlinepilots.com/forum/viewtopic.php?t=1222

salam everyone
i need assistance regarding CD Bank aviation questions
there are questions which refer to figures which are no where to found and CAP graphs, if anyone has them please let me know
e.g.

Hi, I need help with this question. Analyse, individually, the consequence of accepting 1) a V1 20 knots below the correct figure and 2) accepting a VR 20 knots below the correct figure. Which mistake will most likely have more impact on the take off? Explain your answer.

Hello!Where in the forum can you ask our queries concerning atpl questions?

hello i need help
what you mean by gust load

hi
what is TOGW refer to in fmc

Hi
https://aerospace.honeywell.com/en/products/cockpit-systems/airplane-information-management-system
concerning AIMS
TOGW Takeoff Gross Weight
Gust loads are loads caused by gusts. So the contributring factor to the load factor caused by gusts.
V1 is equal or smaller than Vr
So the question is not relevant

Hello :D

Hello :D

Does anyone has ATPL EASA questions bank? I find on the internet but it's limit and must pay lots of money :((

lora lasoon

is there still spanwise flow from tip to root on upper surface/root to tip on upper surface on a SWEPTBACK wing? or only spanwise from root to tip due to pressure gradient?
so basically opposing eachother creating low energy boundary layer

Hi!

0

theres spanwise flow from root to wingtip from the underside to the upper side due to pressure differences

what ar e some aircraft electrical systems that use a capacitor and an indicator to control AC flow

Can anyone help with a low level cruise chart please ?

hi its me, is that possible make configuration any fleet with other service provider software?

Hello Guys, anyone know where i can find some ATG questions on helicopter?

hi

hello guys,
one question aobut yaw damper, is that device operates on all yaw frequencies, does anybody know?
or only on mid range frequencies?

hello
anyone here
what is own alternate mimima plz define in simple word

Hello Guys dose any one know how to prepare for CAE CASS aft. any software

Hi Lads,
New on this forum. Passed so far 9/14. Have you any feedback from february session in the UK ? Heard about a massive QB update

on a moderately cambered airfoil lift increases steadily atpl
?
hi have you got an answer about please?
hi Rom can you answer to me? please

Is it perf or pof ? I haven't sitted those two yet

POF question

No idea sorry. I did not started this subject yet

I answered : increases steadily from minus 4deg alpha to plus 12 deg
ok wish you a good studying ATPL training courses. Are you in ATPL School?

Yes in the UK
but in distance learning. I'm a modular student

yes me too in BGS with the software sent to me Ipad. I can help you sometimes if you want?
in France
which certificats are you studying ?

Remaining MB, FPL, PoF perf and GNAV

have a nice day, thanks good luck

u2

hi
who can answer those question ?
//rumbletalk-images-upload.s3.amazonaws.com/f1ea12db905325ba1971704b1d32da0c/1486678437-IMG_8878.JPG

does anyone have the figures for performance and planning
test bank. for JAA

Hi

hey

Hey guys! anyone know if more of the EASA question has been changed?

hi guys
are these questions from easa questionabnk?

can anyone define AVGWC with definition. Thanks in advance.

what is flex, derate thrust

@Danisg: In which context did you find AVGWC. It seems to be Average Wind Component
@Ganan: Flex or Derate http://www.theairlinepilots.com/forum/viewtopic.php?t=609

@ haroon thank you sir

Salam sir Haroon

Hi
Need help, " The inlet guide vanes are considered a stage of compression." I put false but not sure

hi
need a help with stereographic projection
??

@Fayyaz W.S
@JP: http://www.theairlinepilots.com/forum/viewtopic.php?t=477 and http://www.theairlinepilots.com/forum/viewtopic.php?t=498
@Cheema: http://www.theairlinepilots.com/forum/viewtopic.php?t=684 and http://www.theairlinepilots.com/forum/viewtopic.php?t=713

heey

anyone here?

yes

What ???

How do you find the height of the outer obstacle identification surface, given that its a single 1100m runway with a circuling non precision approach

anyone got the Jeppessen figures for flight planning exam?
:(

hi

Hi is anyone taking jp exam for flight dispatch

hi friends pilots, some of you remember the formula of 4%?
first of all , thanks
i am confused
I was locking in my notes and I can't find it

hello

Hello, I've a question an ATPL GNAV Grid Navigation question, anyone willing to help?
forget it, it was just a brain fart!

haha

hi
what's about the 4% rule ?

TEC?

hey guys

hi everyone
i have a question, could you guide me plz?
how can i compute speed when the dynamic hydroplaning to occur with considre of tire pressure?

@Behnam this may help you. http://www.theairlinepilots.com/forum/viewtopic.php?t=611

i got a confusion. the question said that the aircraft flies at its mimimum drag and assume to be at constant altitude
as the aircraft flies, its weight decreases as fuel is burnt
bcos of that, airspeed is also decreases right?
how can an aircraft flies at constant altitude, when its speed is decrease?
do i have to change the angle of attack?
can i change the angle of attack but still keeping the minimum drag condition

hi guys anyone can help me with this one ?
What causes the gradient wind to be less than the geostrophic wind around a low

Hello, does anyone know where I can get charts for the Met questions? The ones in my qb are nest to unreadable

@hh :vthere is no way to change the AOA (optimum) and still keeping the Minimum drag

hi guys, how does the reduction in tas affects the critical point?

hi guys! which of the following equipment does not use information from external sources in flight? 1- pressure altimeter B- INS/IRS C- Slaved Gyro Compass D- VOR

GN

lf DME is 16, is that the distance in nm?

NG Wei Hong the answer is B
RAZERZ the DME measures slant distance and is considered aproximatelly acurate when the distance from the DME is at least 3 x your height but if DME is showing 16 than your distnace is 16nm

ICAO recommends accuracy of less than the sum of 0.25 nmi plus 1.25% of the distance measured.

feet

Guys why is 3 degrees glide slope used?

hi
what is air ops

?

can anyone help me
air ops document
why do we have these

hi everybody i have a question
anybody knows the reason of N1 and N2 overspeed in a twin spool jet engine?

hey guys, quick one:
Static port blocks on a pressurized a/c at FL280.
inside pressure vessel
why would Altimeter read cabin pressure and ASI under read

The ASI has its own Static Vent.

jobs in commercial operations takeoff climb gradient and landing distance requirments must be met by adjusting the aircraft?
speed , weight , engine thrust or horsepower
can someone plz help me with this Q?

hi

Hey guys please can someone remind me the coversion for US gallons to kg with gravity involved....

US Gallons x 3.8 (gallons to litres) x sp gravity
now convert answer by dividing it with 3.8 and then new sp. gravity
i hope i made it clear

https://www.facebook.com/airlinepilotsforum/videos/744309322400064/

Hi
I had a doubt regarding QDM AND QDR
QDM is stated as track from the aircraft to the station but QDR is "bearing" from the station
whyyy?
I mean the difference between the track and the bearing
I'm just reading off definitions im nt sure if my doubt is legit or not

Hello all

assalam o alaikum
i want to sell my SPORTYS E6B. anyone interested
i want to sell my SPORTYS E6B. anyone interested. contact on my email: ahsonbaig@hotmail.com

Hello All

//rumbletalk-images-upload.s3.amazonaws.com/f1ea12db905325ba1971704b1d32da0c/1488789059-Capture.JPG

hi all
anyone got a PIA manual?

what will happen to the aircraft in the headwind condition if the headwind conditions exceeds limit...will the aircraft sink?

some structural intrinsic damage, and the ac will produce high lift

What is the minimum height an aircraft must be to receive signals from a VOR at 196 ft amsl at a range of 175 nm?

What is the minimum height an aircraft must be to receive signals from a VOR at 196 ft amsl at a range of 175 nm?

hi
An airplane flew at an altitude of 8,000 feet. The flight instruments indicated that the plane was 17,000 feet from a radar tower. What was the horizontal distance (x) from the plane to the radar tower?
:o.O

the function of the diffuser in a carburetor is to ?
can anyone answer this pls

hello

Hello every one

hello
Rime ice forms when liquid water droplets in the air freeze onto a surface, growing into combs, needles, or feathery forms. In the two photographs above, the rime grew over the course of many hours, as a freezing fog lingered for most of a night and all of the following morning.

hello

:)

@mustafa6tyui Slant range is 17000 ft and altitude is 8000ft, Draw a right traingle and we get height of triangle as 8000ft and hypotenuse as 17000 ft , We need to find the Base of the triangle or the horizontal distance from station. sin(angle) = opp side/ hypotenuse ie, sin(angle)= 8000/17000= 0.47 so the angle = sin inverse(0.47)= 28 degrees. We know that cos(angle)= adjacent side/hypotenuse so adjacent side = cos(angle) x Hypotenuse= cos(28) x 17000 = 15000 ft or approx 2.5 NM

one question. how does hard iron magnetism affect the compass reading of the aircraft?
a) heading change b) magnetic latitude
which one is a better ans?

hii

howdy

how far does an aerodome have to be isolated

You are ying at FL 100 in an air mass that is 15°C colder than ISA. Local QNH is 983 hPa. What would the true altitude be?
wat is the answer for this

8950 feet
8590 feet

hi
has anyone done gnav lately?

yo asda
aircraft has to be 2 hours aways from your destination airport in order to be considered as isolated aerodrome

thats correct bariss

with the final reserve fuel included

bariss are you doing your atop in Turkey?
ATPL

Gas turbine engine efficiency increases with: a- An increase in volumetric efficiency. b- An increase in ambient temperature. c- A decrease in ambient temperature. d- A decrease in ambient air pressure.

Hi guys , i did my VFR coms exam yesterday . it was a question that i ve not ever seen but i think its logical but i want to make sure. If the transponder is working properly on Mode C , which parameter can you omit when calling the ATC? "The time" , "the Altitude or Level" , "The position" --- and another one that i forgot now , but it was not the correct one for sure :-)
i put the altitude because of Mode C is working. You are supposed to be transmitting your flight level with that Mode , right?
thanks guys

HI
want to know how i can see fully VC FSX
can anybody help

HOW MANY TIMES CAN A CHANGE INDICATOR BE USED IN A TAF

any help
im looking for Delivery of flight performance

Hi guys any one can help me I have a question the I need an answer for on B777 please

The objectives of ICAO were defined by

What is the limitation on the drift between the GPS and ADIRU when you select the POS from EFIS .

i passed everything! HELL YEAH

Ahmed Mulla, whats the problem with your triple 7?

Hi can someone explain me plz the relation between airspeed and the rate of descent? Cheers

@David: Hi, see page 8 of this document. Might help http://www.theairlinepilots.com/forumarchive/concepts-procedures/managing-descent-profile.pdf
//rumbletalk-images-upload.s3.amazonaws.com/f1ea12db905325ba1971704b1d32da0c/1490596268-777.jpg
@ Mulla:

hello can any body help me with this question. Which frequencie band is not uesed in aeronautical radiotelephony

holi

Hi
is anyone doing a distance learning course through CATS aviation?

can someone please explain why jet engines are much efficient at higher altitudes

Gas Turbine Engines: http://www.theairlinepilots.com/forum/viewtopic.php?t=476

what are the odds-we never mentioned INS/IRS in our flight school and just a few days before the final exam our teacher sends us a message that it might be interesting to look it up

can someone explain how to get grid track by using the W0E circle technique?

Grid Navigation: http://www.theairlinepilots.com/forum/viewtopic.php?t=688

Whats the best way of navigating in the arctic ocean where gps isnt available?

thank you Khwaja

Inertial Reference System: http://www.boeing.com/commercial/aeromagazine/aero_16/polar_nav_by_model.html

An aircraft leaves airfield X ( elevation 510 feet) with the QFE 999 hpa set on the altimeter, enroute to Y ( 510 nm from X ) where the QNH is 1025 hpa. A spot height (450 meters AMSL) 114 nm from X is cleared by 2000 feet. what was the altimeter reading over the spot height? Ans: 2906 feet .. please solve this
i am not getting the QNH value for spot height. can anyone?

Hey, anyone did RNAV exam recently?

hi guys can anyone explain how wing tip stalling occurs and preventions cheers??

Tip Stall: http://www.theairlinepilots.com/forum/viewtopic.php?t=387

jake i already did that

does anyone can explain the distance of ILS identifier code
when we are approaching the final course we set the ils frequency and set the gps with the ILS identifier code . there is a distnace on the gps what is the reference ?

guys need basic concept of lifting line theory, what is it? no need equations

Hi i am having problems with this landing distance graph question

hi there anyone knows how to register
I did but I didn't get a password
//rumbletalk-images-upload.s3.amazonaws.com/f1ea12db905325ba1971704b1d32da0c/1492088922-dcbus.jpg
and do any one know how this thing work
from ac bus 2 to connect dc ess bus?

hi Mr.E. 1) You have to register your self on the forum first to get a password. (2) regarding your query, Rectifier is converting AC to DC and then the Main DC bus is supplying its sub busses.

Doesn anyone use Nordian ATPL books,I need help about their question bank.How I can get it I need to pass couple their school exams in distance learning?

how to calculate ground speed
??
gs=tas
GS=TAS+-windcomponent
but i dont know how to calculate wind component
any one there
????

http://www.theairlinepilots.com/forum/viewtopic.php?t=355&sid=697a96cc4f2d719ddc7f6c6245583aad
or
https://www.google.fr/webhp?sourceid=chrome-instant&ion=1&espv=2&ie=UTF-8#q=wind+component+formula

If the airworthiness documents do not specify a correction for landing on a wet runway; the landing distance must be increased by:
??
Pressure altitude = 2 080 ft True temperature = +15º C What is the density altitude? ?

@law: Wet Runway http://www.theairlinepilots.com/forum/viewtopic.php?p=899 and http://www.theairlinepilots.com/forum/viewtopic.php?p=1488 and Density Altitude http://www.theairlinepilots.com/forum/viewtopic.php?p=972

thanks haroon
Still air gradient of climb: 5% TAS: 250 kts G/S: 200 kts The rate of climb is:?

climb gradient http://www.theairlinepilots.com/forum/viewtopic.php?p=869

Hello

Hi ! I need help with this question
An air driven DGI is corrected for apparent wander at 56\xb0N. If the aircraft is maintaining constant DGI readings,A. When flying N from 56\xb0N the true heading of the aircraft will decreaseB. when flying east from 56\xb0N the true heading Will decreaseC. When flying south from 56\xb0N the true heading will decreaseD. When flying west from 56N True heading will increase
In my book the answer ( according to the correction ) is C and i don't understand why ><
I would say A Because normally it seems that flight North from the 'corrected latitude' gives an increasing reading no ?
Thanks in advance
i've found by myself sorry ^^ I confused The DGI reading & True Heading so i unde
*rstand now why the answer is C

Hello everyone
I need help For B737 Procedures
I must learn F/O Item
Can you help me ?

hi ahmet
i really dont have, but if you found any document please share with me
aliemreb777@gmail.com

http://www.theairlinepilots.com/forumarchive/b737/b737proceduresanddoitems.php
is that what you looking at ?
i hope it will helpful
http://air.felisnox.com/view.php?name=737.pdf
page 367

who could be having manual for fokker 50?

Hi Can anyone explain the difference between Reduced Vis. and LVP?

Any recent feedback for PoF and Performance exam in the UK?

@Rom. I passed POF and PERF two weeks ago. My advice would be, study, restudy then study some more and finyll study on top of that. And I am being serious. All new questions and you can forgett the question banks for those two!!

Is it possible for a plane design with no hydraulic system, purely fly-by-wire?

@Neil I Think the control surface need a back up i case of a failure, so only electric engine wouldn't be allowed
@Neil FBW actually send messages to hydraulic system to move the control surface

what a generator cut out prevents?

Thanks Chris for your feedback; I ll focus on the course rather than question bank

for the purpose.of completing the mass and documentation the operating mass is considered to be dry operating mass plus what?

@Jinab: plus definitions http://www.theairlinepilots.com/forum/viewtopic.php?t=648

If cabin pressure altitude exceeds 12,000 feet a crewmember on flight deck duty is required to use oxygen only during that time in excess of 30 minutes at that altitude.

i want to ask 1 question?

what is it?

Anybody else here using CATS luton?

can anyone give me the cg envelope of b787?

http://www.boeing.com/assets/pdf/commercial/airports/acaps/787.pdf

this is not what i want. i need the loading diagram which shows the forward and aft CG limits as a function Mean Aerodynamic Chord (MAC).

Hello All
My Ambition pilot
Please tell me pilot
Study details :)

hello i need help
can anyone help me
let me know

question about the radio altimeter, aircraft is 2000 feet above ground and in a 30 degree bank, what will the radio altimeter read? anyone know how to work this one out?

what is a fixed distance marking?

Fixed Distance Marking: http://www.theairlinepilots.com/forum/viewtopic.php?t=1100

hi guys
does anyone explaine what to do if we have antiskid inop because i dint get it here
?

hi..guys
:)

Any pilot from Turkey around?

Mass and Balance, third attempt failed :( 74,2 %
any suggestions :)
Multiple new paper handout and graphics not in the ATPL banks in the CAA exams

hi guys.
i got question to ask
How do gyroscopes help the pilot navigate?

Gyroscope: http://www.theairlinepilots.com/forum/viewtopic.php?t=900

what is the approximate size of cellular location area in meters?

I really want to know, i need to calculate fuel friction for reserves fuel, the problem is, its given in time, not in %
how can i calculate it? using data for cruise? like speed etc

Exhaust gas temp taken from free turbine and exhaust gas generator ,what is exhaust gas generator

@Pragyashree: http://www.theairlinepilots.com/forum/viewtopic.php?t=476

Hello, u r doing a wonderful job. I m greatly helped by all ur posts , its wonderful fr aeronautical degree graduates as there z very less content on web . I want to ask if u have any questionaire related to standard atmosphere
I am preparing fr an exam related to aircraft insurance .. So there llb
1m question all functional related questions of aeronautical degree graduate level, can u suggest some ideas on which topics to cover
Hair nails skinI WANT TO S GAIN INFORMATION ABOUT HELICOPTER DYNAMICS CAN U HELP ME WD IT

These may be used for error detection in Auto pilot system except select one: Air Data Computer Inertial Reference Unit Gyroscopes Yaw Damper Coupler Before glideslope capture during approach, an aircraft is flying with attitude mode. When glideslope signal is captured Select one : the attitude hold mode is automatically disconnected the attitude hold mode need to be disengaged first the attitude hold mode is attenuated by the gain programming system
can anyone help?

BEAUTIFUL BLOG , AS IT CONTAINS GIST OF EVERY TOPIC IN VERY concise N PRECISE MANNER... N it clears many doubts related to theoretical n practical issues of aircraft basically bridging d gap. And its d best website fr aviation n moreover author replies to queries really fast... Good efforts keep it up.....

hi

how is this forum for the SCAA exams? are the questions accurate or same to the exam?

hi
what is flux valve in directional gyro?

Hey haroon i just registered myself to the wwbsit but i am not able to downlaod the app for flight log
It seems

can anyone send me soft copy for Ace The Technical Pilot Interview 2/E ( this is the 2md edition june 2012)

@Bhrigu: Flight Log is online only at the moment.
@Sattar.Abtahi: Flux Valve = http://www.theairlinepilots.com/forum/viewtopic.php?t=917

please i am kelechi
can anyone please help me with what is meant by syncronization of autopilot

what are rhumblines on lambets chart

CG depends on the loading of the aircraft. it defers from operation to operation, but you can calculate it by using a simple formula

If the IAS remains constant, what effect will an increase in power have on the angle and rate of climb?

Hi guys
Need a bit of help
How do i calculate Rate of Climb for a jet engine

Rate of Climb: http://www.theairlinepilots.com/forum/viewtopic.php?t=601

hi
can anybody tell me how to calculate distances for rhumb line and great circle track?

Rhumb Line: http://www.theairlinepilots.com/forum/viewtopic.php?t=700 and http://www.theairlinepilots.com/forum/viewtopic.php?t=675

CAT III B can land the aircraft or it brings the aircraft down to certain height
CAT III C is not authorized yet but I know it doesnt require any RVR or DH and lands the plane also taxiis it

everything beyond CAT2 requires an autoland. no manual flying allowed

Hello do you guys think is better to sit all your exams at once or give them in different months in groups? Thanks

monitoring principals in Instruments? what section is that under?

Can anyone send me soft copy for Ace The Technical Pilot Interview "SECOND EDITION"?

Anyone know how much you can mess up on RT oral before you fail it?

can any one help me out with a clear labeled picture of air craft engine fire extinguishing system please
i need it for my ppt
any one online???

https://www.metabunk.org/attachments/docslide-us_a-320-engine-pdf.16733/
check this it is a320 schematic manual
may be u find something useful

thank you very much appreciate you help...... :)
do we use flame detector in aircraft engines
any one online???

https://www.skybrary.aero/index.php/Aircraft_Fire_Detection_Systems

hi

got my last atpl exam today!

trying to find out the answer for this.. anyone have any answer. "Just focusing on the apparent drift at the North versus South Pole, will it affect the read-out of the gyroscopic indicator in the same way? Explain."

mass and balance!

hi
got a question
what happens to the balanced field length if stopway soesnt exist

What does holding short mean?
and what is the diference between holding short an holding point?
anyon online?
ups anyone?

hello

Helo people
Hello

hii

hi

h r u
wats up
(Refer to figure 010-17)The following signal, seen in an airfield signals square indicates:
where can i get the fig?

hi

hi

How r u

good
you?

not bad
where u from

I cannot able to understand Convergence and CA , from last 2-4 hours. I cannot able to play the points.
Is there notes that I can follow or some books ?
All I have with me is the General Nav. 1st edition.

hi guys, can you give me answer for this question.. ''a three-phase electrical tachometer utilises a generator feeding''
thanks )) i've already founded)
if you have some question about atpl tests, i have almost all question of it.

@Ageless: Signals: https://www.theairlinepilots.com/forumarchive/quickref/visualaids.pdf @Gupta Convergency: https://www.theairlinepilots.com/forum/viewtopic.php?t=674 https://www.theairlinepilots.com/forum/viewtopic.php?t=701 @John Tachometer: https://www.theairlinepilots.com/forum/viewtopic.php?t=927 https://www.theairlinepilots.com/forum/viewtopic.php?t=967

Could you someone explain me the recurrent checck
if I finished check on DEC2016, it valid to June2017. so I can do on April, May June, right?\

hi guys
how r u
The rhumb line track between position A (45°00’N, 010°00'W) and position ? (48°30’N, 015°00'W) is approximately:
could anyone help to solve this problem please

If the grid datum is 054oW, position 80oN 140oE and true heading of 330o, what is the grid heading?
any idea for such questions guys?

hey
guys

Hi

hey
what are the three stage of alerting service

Uncertainty phase, Alert phase and Distress phase

hello everybody. My name is richard. tomorrow . sorry today i need to take a new attestation exam. How many megafon we need on board?
1 year before we dont need to know this... but now we need. i know the Extinguishers. but i dont know the megafone. any idea?

1 mega phone

ayyyyyyy lmaoooo

hii guys.m looking fr tech basic material fr CPL exam.Anyone?

For each passenger deck with 61 to 99 seats, one megaphone is required. With 100 or more seats, two megaphones are required

Outline three types of AIS data that are provided to pilots, along with a description of how each type of information is made available. Anyone can help me with this question?

@Help!: AIS https://www.theairlinepilots.com/forum/viewtopic.php?t=1028

hi guys. If Mach numer is 0.6 and LSS is 500 whats the TAS?

heloo friends
can anyone tell me how to calculate thermal winds
@jack formula is mach no.= TAS/LSS(local speed of sound)

hi
could anyone help me gettin all the related topics for airline interview
i would be deeply thankful

go for Ace Technical book

@kunal can i find it online ?

hi guys.

yup
@gautam do you know what is thermal winds

yeah
change in the direction of geostrophic winds due to ground temp gradient

struggling with a question. "How is a long great circle track entered in an ordinary flight plan?"

@kunal not sure though
just remeber something like it

do you know how to calculate it @gautam

@kunal sorry bro i dont kniw
know**

ok no problem...
btw which airline interview

na just preparing
can u send me if u have a soft copy
the book which u spoke about
?
still here

@Eperjesi Richard ....for Mega phone from 61 to 99 pax seating capacity only 1 is required and 100 or more 2 megha phones are required
hy
ya let me chk
//rumbletalk-images-upload.s3.amazonaws.com/f1ea12db905325ba1971704b1d32da0c/1497631579-Ace%20the%20Technical%20Pilot%20Interview.pdf

Does anyone know how fuel tanks are pressurised>

@Oskar: Fuel System https://www.theairlinepilots.com/forum/viewtopic.php?t=461

Oskar Fuel ltanks is not pressurized as far as I know.
hydraulic tank is pressurized

@GAUTAM try this website and find wish airline u going for
http://www.latestpilotjobs.com/interviews/index.html

Adam Lagahier ,nice web thanks ;)

Can anyone explain why the centre of pressure moves forward briefly in transonic flow before moving rearward as the aircraft accelerates?

hello all
@Sam : My guess is, as the aircraft acclerated from transonic to supersonic, the high pressure created behind the shockwaves are responsible for the centre of pressure to move rearward.

hey guys does anyone has some file for diferences between atr42-300 and atr 42-500. Thank you in advance

@Apostolos: Does this help?
//rumbletalk-images-upload.s3.amazonaws.com/f1ea12db905325ba1971704b1d32da0c/1498312361-ATR-Family.pdf

hello

good day everybody, I have in a couple of weeks a exam for module 8 aerodynamics, do you guys have mayby some good tips and tricks to help me out a bit, aerodynamics is not the greatesd thing by me

hello

guys, If an aircraft in level flight loses engine power it will a) pitch nose up b) pitch nose down c) not change pitch without drag increasing
doesn't it dippend on what kind of aircraft it is ?

@Sjored: Principles of Flight https://www.theairlinepilots.com/forum/viewforum.php?f=26
@ mike: Pitch Down. http://apps.apstraining.com/wp-content/uploads/2013/10/pitching.png

What is the distance in kilometres from 49° S 180° E/W to 58° S 180º E/W?

11890KM

how??
show me the calculation

online, go to NHRC site and convert

give me the site
will do it asap

National hurricane Centere

r u a boy or girl?

??

just asking...
nothing serious.

its ok
did find NHRC site?

nah..

ok

found it but..

google Lat/long convertion from National Hurricane Center

do not know where to go for computation

on the page correctly enter the lat/long in the format
r u a pilot?

yes

if you are on the correct page - the page will have this header "Latitude/Longitude Distance Calculator"
I don't want to share url here

yes i did

does it work?

but wud want to know how to do it manually
not gonna have this website on exam..so..

can somebody tell me a couple of must know things about aviation legislation, I suck at that module, I can't remeber anything when I read it

@ Milanov: Try this https://www.theairlinepilots.com/forum/viewtopic.php?t=671
@ SUS: Why dont you share the URL
@ Dave: Air Law https://www.theairlinepilots.com/forum/viewforum.php?f=37

can someone explain pendulous acceleration pls?
pendulous accelerometer

Wondering @sus answer if the latitude change was of 9* (540nm)?

@ Felix: https://en.wikipedia.org/wiki/PIGA_accelerometer

@felix this may help https://www.youtube.com/watch?v=C0pZ-mVcbbI&t=2s

thank you very much

you're most welcome

Goodmorning! question guys. A synchroscope indicates qualitative/quantitative.. RPM or Hz?
2nd question: An A/C with 5 deg flaps has a much higher CLLTOM than FLLTOM. What can you do to increase FLLTOM?Incr/decr flap setting or incr/decr V2?

Less flaps means better climb gradient after getting airborne due to less drag so there is an increase in Climb Limit Weight. However less flaps increases the ground roll due to less lift, so there is a decrease in the Field Length Limit Weight. If CLTOM is higher than FLLTOM then I think increase flap setting seems to be the answer. Increasing V2 will improve CLTOM at the cost of eating up the field length.
//rumbletalk-images-upload.s3.amazonaws.com/f1ea12db905325ba1971704b1d32da0c/1498561607-mtomflap.jpg

thanks.!
How about the first Q A synchroscope indicates qualitative/quantitative.. RPM or Hz?
I know that you can set engines to same speed... but is it a qualitative or quantitative reading of RPM or Hz?

Welcome.
Quantitative Display: In which quantity (being measured) is presented in terms of a numerical value by the position of a pointer etc. Qualitative Display: In which info is presented in symbolic or pictorial form. Synchroscope is used in conjuction with rpm indicating system to show state of synchronization between two rotating things (e.g. rotating to show speed difference between two engines) by symbolizing the propellers so its "Qualitative".

many thanks! Super!
another Q.. Since i am studying. How does it work regarding Vx and Vy with more wind/less wind fly faster/slower. When does what hange? I don't understand ROC vs gradient and so on... Sorry

read this https://www.theairlinepilots.com/forum/viewtopic.php?t=601

Hi guys, Been Studying for my CAAUK Performance exam. My peers who have written the exam say there is many new graphs which aren't in the CAP698 that we have. Is the most recent version of the CAP - "CAP698 third edition July 2006"

thats a very good question

For this contact http://www.atpforum.eu/ these guys should be updated on this development

Hi can any one tell me the mechanism behind this question
In a microburst downdrafts in the order of 3000 to 4000 ft/min can produce vector changes in horizontal wind of: 30 to 40 kts 10 to 20 kts 60 to 80 kts 100 to 140 kts
Answer 60-80

@Amir: https://www.theairlinepilots.com/forum/viewtopic.php?t=1223

can anyone tell how inoperative antiskid wil increase V1?

With inoperative anti skid Weight and V1 is reduced because you need more room for stopping. Think about the stopping scenario in case of abort with anti skid inop.

Yes got it. why the minimum value of V2 must exceed VMCS by 10% ?
VMCA*

safety margin

Thanks Khwaja Haroon !

Hi. What makes the nose of an aircraft heavy when speed is reduced?

http://apps.apstraining.com/wp-content/uploads/2013/10/pitching.png

Hi to everyone. Can someone help me with a subject....When do i have to put an enroute alternate in my flight plan specified in the section #18. Thanks!

Hi for alternate aerodromes see this: https://www.theairlinepilots.com/forum/viewtopic.php?p=1461

hi guy can you help me out
what instrument measures compressor low rpm
?????
hello

Hi, @Henry, this might help: http://pe.org.pl/articles/2013/3a/27.pdf

Thanks Khwaja. Is the diagram saying the Total pitching moment is a constant value and a reduction in several moments e.g. Thrust,Wing lift and tail lift will cause a corresponding increase in the Wing body moment?

Welcome Barry: The diagram shows various factors that contribute to pitching moments. As along as the moments are balanced the aircraft will be in equilibrium. When there is an imbalance then ofcourse the pitch changes accordingly e.g. increasing the thrust vector will create an imbalance and if you look at the diagram you'll figure out that the aircraft will pitch up. Wing contributes to moments about the CG of the aircraft, essentially through moment about aerodynamic center and lift acting through moment arm. The fuselage i.e. aircraft body at an angle of attack to an airstream experiences moments too about its aerodynamic center, along with some lift and drag around it. So when the wing is attached to the body its a wing-body combination. The airflow around this combination, beacuse of airflow interference, is different as compared to airflow around wing and body separately. Due to this interference the moment due to wing-body combination is different as compared to moment due to wing and body separately and is not merely the sum of the two (i.e. wing and body). Same is the case for lift and drag around it. So wing-body is one among other factors contributing to total pitching moments.

HI @Khwaja This Qustion. I faced in Interview Can Taxiway be used as a runway. I said no not sure is my answer is correct or not.

Sumit, if I was taking your interview I would accept your answer.

ok

Thanks for you reply

Hi
Magnetic compass working?
Ok

hello, can i find some how explain to me clearly the effect of thrust on speed and distance
?
also if u have doc it's okay :)

hi guys
got an exam on 17th nav
need some important questions or topic
help if you have any

17th nav?

navigation on 17th of this month

and what do u need exactly?
//rumbletalk-images-upload.s3.amazonaws.com/f1ea12db905325ba1971704b1d32da0c/1499456316-Cours%20de%20navigation%20a%C3%A9rienne-3LMD-2013.pdf

Unable to open file

what do you wany to open ?

the above pdf file sent by Ms.Fatima

hi
i want to become pilot
what is scope

hahaha
toh ann jaa bhai :p
bann*

hm

hehe sorry bro
kidding
ask anything you want

aha
navigation teach me?

where are you from ?

andhrapradesh

okay
anyone from mumbai here ?

im

hehe
now only you said Andrapradesh
and now saying im
yes

but staying in mumbai for pilot coaching
k

pilot coaching okay
where ?
in mumbai ?

skylne aviation borivali west
wt abt u?

i stay at kharghar
navi mumbai

k

giving nav on 17th ?

good
all the best

im asking you buddy
you giving nav on 17th ?

no
no

okay
then tech ?.

no

you have something to study on navigation ?
//rumbletalk-images-upload.s3.amazonaws.com/f1ea12db905325ba1971704b1d32da0c/1499522908-Basic%20Navigation.pdf

hi

hi
anyone online?
struggling with vor interception and moreover for the uk ppl rt practical the D/F procedure. any help would be greatly appreciated!
peace

What Exactly are you struggling with
Second find out where you are in relation to or from the VOR. To do that, Centre the CDI ( Course Deviation Indicator with a TO flag indicated. Then decide where you want to be. Select the Desired RADIAL (Look at the Bottom). Look at where the needle is deflected to. Now Pick a heading to intercept the radial and use the 30 degree rule, or use the heading that is double the difference between the actual radial and the desired radial. Simply fly that heading. If the needle is deflected to the right then fly right and vice versa. As the Radial Approaches, the CDI will move towards the centre of the instrument. At around one dot deflection turn back onto the radial to intercept the radial with the Needle centered
Intercepting is easy. Its divided into a few step obviously first TUNE IDENTIFY and TEST. Usually the tests should be performed on the ground to ensure the correct fuction of the equipment.

Hello Guys... Does anyone have a list of mnemonic for ATPL

Does anyone have information on the E2b in more depth? cheers Sam

pozdrav svima

I thought I had this down pact but I am having troubles with several questions. mainly wheter to add or subtract the height change based on pressure. For example Given: Aircraft at FL 150 overhead an airport Elevation of airport 720 FT. QNH is 1003 hPa. OAT at FL150 -5? C. What is the true altitude of the aircraft? (Assume 1 hPa = 27 FT) A) 15 840 FT B) 14 160 FT C) 15 280 FT D) 14 720 FT
need help with ^
Given: Aircraft at FL 150 overhead an airport Elevation of airport 720 FT. QNH is 1003 hPa. OAT at FL150 -5? C. What is the true altitude of the aircraft? (Assume 1 hPa = 27 FT) A) 15 840 FT B) 14 160 FT C) 15 280 FT D) 14 720 FT
:(

Hey Alpha, these questions can be quite tricky because sometimes they give QNH or QFE etc. However most of the time the give you QNH and a FL.
....
If they give you a flight level, then usually it is an easier question. Given a FL it means you are given a pressure altitude which is at 1013. Anyway, try not to think about it too much. But the trick i use if given a flight level is to always put 1013 on the right hand side of the equation, and then put the QNH on the left side, if you get a positive number then you add it to FL to get indicated altitude, if you get a negative answer you subtract it. If you alwas follow this rule, you wont have to think too hard.
But remember, it only works if your given a QNH and a FL. If given QFE its a bit different. So in your example it would be..
1003 - 1013 ... <<<< Here I put 1013 on the right and QNH on the left. 1003-1013 is -10. X27 = -270. So your indicated altitude is 15000 - 270.. 14730.. then use this alt and apply the TEC to it.
basically always subtract 1013 from your QNH, if its a positve number add it to flight level, if its a negative subtract it..

need help
descent from FL 250 to 5000 with average TAS 300 kts temperature is +15 find cas

@Stéfan Moosh Fouche thanks for your answer, it really has helped me understand better.
This is where it gets a little tricky for me, how can i obtain d/f assistance in flight? for example if my flight path is between a vor and an aerodrome with a "homer" callsign e.g. Dunsfold Homer?

Hi , a question... what can be danger when extending flap and pitch moment is changing ?
trailing edge flaps

Extending flap will reduce Critical A O A ,decrease stall speed,Increase Camber,Co. of lift & drag, I may say pitching up can reduce margin for stall before airplane had stabilised in new configuration, correct me if wrong.

correct

Who all giving dgca exam?

(y)

Hi guys has anyone got a downloadable version of "the pilot's r/t handbook" by chris Leech??

Flight time from departure to destination = 2:15. Flight time destination to alternate = 1:06. Average fuel consumption: 10 gall/hr @ SG 0.72 (Avgas). Flight plan status: IFR. Aircraft: Reciprocating, multi-engine. The minimum fuel to be carried? can anyone help me with this question please

AUW = 60000lbs C of G 2 feet forward of datum. Calculate how much weight can be added to hold arm 5 feet aft of the datm?
a) 40000lbs b) 4000lbs c) 21000lbs

given: TAS=205 HDG(T)=180 W/V=240/25. calculate drift angle and gs? can anybody explain what i have to do?

CX2 calculation unknown wind your GS is windspeed and tcrs is wind direction: results in a GS of 193,7kts and a track of 173,6°. hdg to track is drift which gives you 6,4° left drift

thanks maybe you got the formulas too?

no formula, either with cx2 calculator or with the wizzwheel or by drawing and pythagoras

ok thanks

easiest is CX2 if you use it
CX2: flight - act leg - unknown wind. enter datas, but your gs is given windspeed, tcrs is given wind direction. results in an wdir which is your required track and wsped which is your required gs
and drift is always from your thdg to your ttrack

thanks a lot for explaining
Given: MT 210 MH 215 VAR 15E TAS 360 Aircraft flies 64NM in 12 min
W/V?
could anybody help me?

Thanks Sumit!
Climb gradient 3,3% , maintaining TAS is 180 kt and a tailwind is 25 kt. minimun climb gradient corresponds to a rate of climb of approx? need help with this question. I know that it 3,3 x 180 without tailwind but what should i do with tailwind?

spitzi. out of distance and time you can calc. your GS. with your GS and the other given values CX2 unknown wind, enter datas
cnr you got a tas and a tailwind, which gives you a GS. in your case 180+25=205kts GS
ROC=gradient x GS

AUW = 60000lbs C of G 2 feet forward of datum. Calculate how much weight can be added to hold arm 5 feet aft of the datm? a) 40000lbs b) 4000lbs c) 21000lbs
any ideas guys?
?

Thank you Rusty , it was so helpfull

what is the lat and long of the SHA VOR (5243N 00853W) 239M/36nm radial/range ? how can I do it ?

how the tail wind thrust setting vary with ROD GS and Pitch for ILS approach.
?

what is the feedback in fly-by wire system?

Hello everyone. Does anyone know a typical value of inductance and resistance in DC system in aircraft?

how the tail wind thrust setting vary with ROD GS and Pitch for ILS approach. ?

Dose any one know what exactly CSTPL-AA exam is, which is conducted by CAE as a Crew resource consultant .

hi sumit...is your question(CSTPL-AA) in regards to the latest vacancy of air asia?

Yes SIERRA ROMEO I know CAE CASS but what exactly is CSTPL-AA exam

hii
hlw
anyone there?

Hello everyone

A BALANCED FIELD LENGTH is said to exist where: "The accelerate stop distance is equal to the take off distance available" . Saw his question here what I understand is that BFL is ASDA = take of run required . As take of distance available may include clearway

whr is the oxygen maslk locate for cabin crew
mask

@Zeeshan: Balanced Field https://www.theairlinepilots.com/forum/viewtopic.php?t=350
@Amanda: At their stations. If at the time of oxygen requirement they are not at their stations then they can use cabin masks which are at least 10% more than passenger seats.

ASDA = TODR , but the question say take of distance available so the question is wrong as take of distance available has clear way in it too :)
BFL (TODR = ASDA) and not TODA

Hi, hope someone will illuminate me. It's a simple mass & balance excercise: <For the medium range transport aeroplane, from the loading manual, determine the maximum total volume of fuel which can be loaded into the main wing tanks. (Fuel density value 0.78kg/l)>
From the annex the total of both main wing tanks is: 2998gal or 9084kg
If I convert gal to liters (1gal = 3.785lts) you get the correct answer (11347 aprox)
If I convert kg to liters with the density given in the question you get 11646lts which is listed in the options but it is not correct
I think both ways should be correct but obviously i'm mistaken
And I don't know why

Is it US Gal or IMP Gal?
???????????????????????

@diego: the question is: what the max. total volume is and not the total mass. :)

hi

hi @majid

Hello.. can someone please answer this?
a constant speed propeller is switched off in HIGH PITCH or FINE PITCH? and why?

Hi
Any summary for Radio Nav ?

anyone knows where i can find the new questions being uploaded to the exams for vfr communications

HI

GUYS WHAT DOES IT MEAN WHITE DUMBELL

Aerodrome marking to tell the pilots looking at it how the runway is
//rumbletalk-images-upload.s3.amazonaws.com/f1ea12db905325ba1971704b1d32da0c/1501231494-SmartSelectImage_2017-07-28-13-38-58

@fdfdf If you wanna find the questions for VFR comms i suggest you to buy a subscription of the VFR Communications in www.aviationexam.com>

Given: TAS = 465 kt,HDG T = 124,W/V = 170/80kt.Calculate the drift and GS?

Tas 408 kts drift 7* left so add 7 for correction from my E6B
GS*

help me
im struggling with my proposed airport

Distance 3600nm, PET = 1360nm, TAS 400 knots. If the headwind going out was 40 knots stronger than expected what is the new PET

acceleration, artificial horizon shows pitch up and (left or right) turn?

wasuo

anyone know the question ID of Tuck under may occur :...... from principle of flight in AE?

help me out please i have a question giving me a problem
when about to fly into a prohibited airspace, do you get a solid or flashing light beam?answer options that are given is flashing red,flashing white beam or solid red beam,explain why you choice of answer.

Humphrey i haven't come accros this questions but i know that Red means no, and Flashing it means Get off / get out of , so flashing red would be the best answer

help im writing ATG cpl any help ?

Hi! I have a question. Why is wind not a variable in the Landing/Approach Climb Limit Weight Chart

What i believe is that , Pilot needs to have known winds before using the graphs that is to be either head or tail, most graphs have in them compensation for 50% head and 150% tail wind calculations

Please specify how Non RVSM, RVSM , sami circular and qudrental rules apply to chose FL,

@sumit check this out https://www.theairlinepilots.com/forum/viewtopic.php?t=1007

hola
good page for pilots

HI
please help me to find ISA deviation
we have only TAS 356, FL25000, GS 407
hello
HI PONNY'

Igors it should be CAS 407 not GS 407 for this question to be logical

Kingjac26@gmail.com
What is the fire drill skill in human factor
Slip also

hi all
i think slip is Slips can be thought of as actions not carried out as intended or planned, e.g. “finger trouble” when dialling in a frequency or “Freudian slips” when saying something.

guys good afternoon ,
there is a question in IR exam that ask what are the disadvantages of EFIS system , the answers were crazy and i searched all the books and couldnt find any of disadvantages of any

Good afternoon

hello

hi there , need help with this question
500 feet before the break-release end of the runway there is an obstacle 60 feet high.How much is the runway displaced for calculation of landing distance avalible?

Hi, I got questions about RTOW/ RLW charts. When an airline wants to operate at a newly built aerodrome, they need to have RTOW and RLW charts for their aircraft. What data will they require to produce RTOW /RLW charts? Where would the required data come from? Who would provide the data? How would the data be used to produce RTOW/ RLW charts? Many thanks

hello
I have a question can anyone help
is there any one

Hi there, maybe I can help!

HI

hey there
how do you do pallets exercises?

hello
anyone here?

@Jess Hi, your answer: https://www.theairlinepilots.com/forum/viewtopic.php?p=1871

hey

hiiiiiiiiiii

is anyone here
what does wing lift vector 12" aft of the aircraft cg mean?

In this diagram http://apps.apstraining.com/wp-content/uploads/2013/10/pitching.png wing lift vector is aft of cg

.

hello
An aircraft is following a true course (TC) of 040° at a constant true airspeed (TAS) of 180 kt. The wind vector is 350°/30 kt. The wind correction angle (WCA) equals...
Can anyone help me in this

uhm
do u have crp-5 or a different navcomputer?
its very straight forward
WCA will be the opposite of the drift if that makes sense. so 8degrees left if im not mistaken.

Thanks man
I don't have CRP now. there is any mathematical calculation ?

hi guys
anymore question to do?

9 An aircraft is flying at a pressure altitude of 7000 feet with an outside air temperature of +10° C. The QNH altitude is 6500 ft. The true altitude equals...

7200??

its 6750
But, I don't know what are the steps
this is model answer

i dont get 6750 but close
Isa+9 almost 4%
10 is 4% 9 is 3.6%
7000*3.6 / 100 = 252ft
7000-252= 6748
close enough

Thankk youu
I will try it now

no rpob
i dont know why u get the qnh altitude...
But alot of times the questions give 2 much info
ALOT of times...nightmare i hate this

6500 + 252 = 6752

but why would u use 6500 when they ask for true alt

4 feet per each thousand feet per deg of ISA dev
4 * 7 = 28
28 * 9 = 252

we will add as temp is higher so the True altitude will be higher than indicated

true is higher than indicated in case of warm air mass

I think temperature correction will be added to pressure altitude to give true altitude

yeah this is true

good to see all of you here helping each other
keep it up, byr

I dont know why they give Pressure altitude tho

bye

if you see a flight computer they tell you to set air temperature over pressure altitude
and read the true altitude over calibrated scale

in crp5 u can do this..?

if you are flying in a warm air you will be flying higher than indicated , so your true altitude will be higher than the ressure altitude as pressure surfaces bend upwards in a warm airmass
https://www.youtube.com/watch?v=IaYcHBrxIcM

Altimeter https://www.theairlinepilots.com/forum/viewtopic.php?t=1359

4 feet per each thousand feet per deg of ISA dev 4 * 7 = 28 28 * 9 = 252
what does 9 represent?

isa deviation

how did you calculate it ?

7000ft
7x2 = 14
15-14 = 1
and u said OAT was 10degrees
deviation = 9
I hope u figure it out. I have to mute the chat, exam tomorrow. good luck with everything

Thanks alott

no prob

if you have time
how to determine degrees of QDN QTE QDR QUJ

give an example question please, this is too broad..

okay
A pilot receives a QDR of 135° from the VDF ground station. Where is the aircraft located in relation to the ground station?

So QDR is radial
and you areo n radial 135
so you are east/ south/east
or what are the answers..?

southeast
but how can I determine that

you draw a vor
and set north up south down east right west left
then you know where 135degrees is. on this line somewhere, your plane is..

A route leg track angle is 250°. Declination is 3° East. Wind is from 190°,, calculations show that it diverts the aeroplane with 4°. Deviation is 2° West What is your compass heading?
Can you help me in this gus
guys

Your compas heading is 241

What is the TAS....do you mean Drift is 4deg ...if yes left or right?
250 +4(if left) +2=256(C)...else if 4(right) then 250 -4(if right) +2= 248(C)
Sorry didnot notice the wind direction give. Since wind direction is left of your track hence drift is right, Therefore WCA is left therefore magnetic heading will be 250-4=246...Compass heading "devn west compass best" so 246 +2=248(c) :-Z

Goodday all bosses
//rumbletalk-images-upload.s3.amazonaws.com/f1ea12db905325ba1971704b1d32da0c/1504243945-b737flyingtips.pdf
My apology. Pls disregard

ladies and gents
the pressure altitude gives an allowance for real pressure at sealevel to be: 1-the same as standard atmospheric pressure 2-to be different than the standard atmospheric pressure 3-to find density altitude
please help i did not understand this question

1.Same as standard atmosphere , since Pressure altitude refers to a setting of 1013Hpa or QNE on the altimeter subscale which is the pressure under ISA condns at Sea-Level......the question is an example of how questions are set to test ignorance rather than knowledge of the candidates and shows poor english comprehension of the exam setter rather than the examinee. :-(

Good afternoon Can Any Give Help about issue time of significant weather at 1200z

time on sig wx charts means that data will be valid at that time i.e. 1200z and not up till 1200z

SWC is a forcast for the Time given on the Chart

thank you so much Arindam , i was shocked in the exam of how basic is the information but we call this ( the impossible easy) did you see this question somewhere because i tried looking for it on the whole internet and i counldny find it

Why is directional stability the strongest out of the 3 stabilities?

Hy guyes
guys*
Who 's studying for instrumentation ATPL exam?
May someone help me about the INS and IRS pleeeeease
??

@JR: checkout INS/IRS info here https://www.theairlinepilots.com/forum/viewforum.php?f=35

hey, i have to make a raport for school and i want to do it about the landing gear, but witch plane has steering main landing gears? is that a boeing 777 or also to boeing 747?

hi, b777 has it. dont know about 747

by the t7 have all the main landing gears the option to steer right?
i looked around a bit and i saw that the b747 only can steer with the body gear, but i'm not complety sure tho

one side has 3 pairs (6 pairs), the last pair moves

yea

try searching for 747-800
thats the new one
correction (6 wheels), not pairs
http://www.boeing.com/assets/pdf/commercial/airports/acaps/747_8.pdf

where did you find that if i may ask ?

what

the pdf file, i have to make more rapports about different ATA's

boeing.com

o ok, thx :)

welcome

thx for the help man c:

;)

Hi, I have a question. What’s the critical engine on a 4-engine jet plane? Thanks for the help.
And one more, within how many degrees can you do a reversal entry?

The most outboard engine facing the wind I think!
For a jet
Not too sure on the second question.... have only just started my ATPL Theory!

Hi, i want to know about purpose Gyromagnetic Heading in Planes

@Ahtisham: for a steady and accurate heading reference system

Hey guys.
is there anyone who can help me with this question?
An aircraft is flying at FL45 in ISA conditions, with a Radio Altimeter reading of 1860 ft. If the elevation of the terrain beneath the aeroplane is 3090 feet, what is local QNH? a) 1030 hPa b) 996 hPa c) 1042 hPa d) 1013 hPa

hello

Altitudet overreads 450feet (see1860+3090=4950feet) which is (450/27) about 17hpa. QNH will be 17 higher than standard so 1013 + 17 = 1030.

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https://www.theairlinepilots.com/forumarchive/a320/vprep/vprep.htm

HELLO

If the gliding range changes between headwind and tailwind, will the rate of decent change as well?

Hi Jim. Rate of descent and ascent are independent of wind components.

Altimeter Errors: https://www.theairlinepilots.com/forum/viewtopic.php?t=256

Thanks alot

Hello there
Anyone online?

yigitelma - Thanks. just wanted to confirm :)

Mode 5 of GPRS is superseded by which modes

gonna go for my atpl paper later in the day
wish me lluck

best of luck :D

Hi guys Passed my instrument paper :)
would like to ask about a qns
for slush, will it increase friction or decrease friction while during t/o or landing
like does it increase friction due to resistance or decrease friction

Congrats (y)
Slush: https://www.tc.gc.ca/eng/civilaviation/publications/tp185-4-03-464-3879.htm

An airplane has an airspeed of 275 km/h, and flies on a bearing of 295. The wind is blowing at a speed of 225 km/h from West to East. What is the head wind and what is the cross wind? can anyone help me in solving this..

"Visual Flight Rules Except when a clearance is obtained from an ATC unit, flights under VFR shall not take off from an aerodrome within a Control Zone or enter a Control Zone when the"
Please help me for answer

VFR: https://www.theairlinepilots.com/forum/viewtopic.php?p=1536
see if this helps

Thank you Khwaja

welcome

You know adres in internet experimental test ?
conversation where it is?

what :o.O

het guys! anyone good at GNAV here?

I wish I was good at GNAV, still learning it.

GNAV: https://www.theairlinepilots.com/forum/viewforum.php?f=31

On a Lambert conformal chart the distance between two parallels of latitude having a difference of latitude=2?, is measured to be 112mm. The distance between 2 meridians, spaced 2? longitude, is, according to the chart 70NM. The parallel of origin runs trough the middle of the described square. What is the convergence for a dlong of 15? on this.
got it ,thanks anyway
distance=chlongxcoslat con:chlongxsinlat

Hi everybody
can someone help to solving this Dist. A - B = 1200Nm PSR is 84% of AB PET is 60% of AB Endurance = 8h24mins What is the Groundspeed from PSR to A?
B-)

PSR: https://www.theairlinepilots.com/forum/viewtopic.php?t=337

easy theory on performance
any links

try this https://www.theairlinepilots.com/forum/viewforum.php?f=29

thanks

hey whatsup

anyone there

hellp
hello

Hi
I need some help

hi

Morning

morning
any one have questioon

hi there

Hy there

hello guys?
anyone on?
am i the only 1 here right now?
i guess so ...
hi?

hello
how r u?
do you know if there is many new questions in easa exams for systems?
i use eatpl rightnow

adel chetori ?

Hi all :)

hi

Can someone tell me how many questions we have in the Air Law exam? I found 44 or 75 on internet , so I don't know :s

in witch country ?

In UK with CAA

in fact i dont know about uk
but in iran we have about 100 question

Ok thanks for your help ;) What time is it in Iran now?

your wlc
2
2
2:30 am
:(

wooo go to sleep ! lol

i want to but i cant , i have to study
:( :S- :o.O
lol

oh! good luck! are you studying the atpl too ?

no i have cpl final exam 2 mounts later
you have atpl exam ?

ok , enjoy, soon you'll be on a cockpit ! Yes, I'm studying atpl and my first sitting will be in December for mod1

hey hello

oooh good luck captain

u still up studiing :)
good to see im not the only one :)

i have to go
bye

bye

good night, maybe see you :)

if you have instagram account follow me to be in touch together
nima
nima_nabizade

hello guys, I have to make a report about the landing gear of the boeing 747.
i want to know a couple of things about the tires, like how big are they, how much pressure are in them (PSI), what kind of tires are normaly used on them
I can't find that kind of inforation very easy, mayby you guys can help me a bit with it :)

nose wheel 180 psi

Hello mate!

hi

what do you up to?

study :(

same here and its getting boring :(

where are you from ?

turkey
you?

iran

which school?

we are neighbor
arta kish

yeah man ^_^
let me check it
atpl?

yes

im new im getting ready for ppl :P

how much hours do you fly until now

0 so far

not bad

hahaha :D

;)

i ll have my first flight in 10 days
and the ppl exam in 11-12

then you ill have solo flight about one mounts later

10 days later from my first flight
i ll have the first solo

yes

i got my schedule
how it feels?!

wich school ?

flycoop
in budapest / hungary
i ll just do ppl there
for the rest im thinking of poland
greece maybe for time building

do you have insagram ?

Freable
feel free to add me mate :)
alpicuno
sorry.

i will follow you now

that was my previous acc
i ll be waiting
any advises by the way as an experienced student?

just study hard to save people lives :D

hahahaha :D thats why im here as a ppl student
trying to learn every detail

thats good bro

i ll take an online test now take care mate! good luck with your studies :) was nice talking to you

hi guys
any one know how to reaarnge mach formula to make LSS sound the subject?
mach= tas/lss
lss=tas divide mach?
is that correct
fuck brain freeze

hi

hi
does anyone here know if there's alot of difference between the calculations on jepessen flight computer and pooley's crp 5?

no idea mate

yeah that is right. But you must also know that LSS=38.95* (square root of the OAT in Kelvin)

thanks man
yeah i know that lss=38.94 sqaure root
then plus 273 to get into celcius
arc to time shit is annoying as well

hie guys :)

gidday mate

how are you

Hello everyone, I hope you are all doing fine. I have a question concerning boundary layer movement on swept wings, with tip stall and CP movement
Could anyone help on that topic?
I understand why there is tip stalling. What I don't quite get is how the pool of stagnant air at the tip grows and why the ram's horn vortex moves inward with increasing AOA. Why does the CP move inward and forward with increasing AOA?

Hakan Hocam gecenin bu saatinde su site bana ilaç gibi oldu. içimden geldi yazdim :)

hi

Hi

what is the difference between CANPA and CDFA ??
what are the problems in the Airbus a320 neo enhines
engine**

hi
any of you went to ryanair assessment?

An aircraft is flying at FL 75 over point A where the QNH is 1013mb, en-route to B where the QNH is 979mb. Assuming that 1mb = 30ft and that the elevation of B is 823 metres, the terrain clearance over B is:

hi
is anyone here?

HI ASHLEY
im here
HI

Distance from departure to destination: 165 NM ¿ True track: 055 ¿ W/V: 360/20 ¿ TAS: 105 kt What is the distance of the PET from the departure point?
Find me this question
Solve this question please

ETP https://www.theairlinepilots.com/forum/viewtopic.php?t=723

Hi, What happened, when the altitude increase and IAS is cste, about lateral stability static and dynamic

Hello Friends how are you
I Friends i am preparing for my finall viva for FOO(Flight Dispatcher) if you know about any question which is important for flight planing please send me on this email muhammadzeeshan767@gmail.com i will be thankfull
Friends please send me questions for oral viva for FOO Licence i will be thankfull muhammadzeeshan767@gmail.com
or inbox me https://www.facebook.com/zeeshan.rehmani.50
When NOTAM becomes permanent
how to identify domestic and international NOTAM?

guys what is the maximum rudder force required to move the aircraft on ground ?

finally got my atpl, 92% average no fail
thanks for this website
especially for you Haroon

The design and operation of the inserting device?

Congrats Romain! (y) If you have found this resource to be a useful service, you may express your gratitude here https://www.theairlinepilots.com/membership-subscription.php Thankyou. Safe flying!

hello guys... any idia what should i expect for a written test exam for an airline first officer position... thx

@ijij: http://www.latestpilotjobs.com/index.php

Hi ...
How are you all please tell me where s genral knowledge section ....inform me plz i am unable to find here

Hi, @ Abdul Qudus https://www.theairlinepilots.com/forum/viewforum.php?f=27

hey i am finding the section for distance calculation along a meridian and along a parallel in general navigation but cant find it

@Anushka: are you looking for this https://www.theairlinepilots.com/forum/viewtopic.php?t=673
See also: https://www.theairlinepilots.com/forum/viewtopic.php?t=672 and https://www.theairlinepilots.com/forum/viewtopic.php?t=671

Hi, I have a question. When i climb with constant Power (i.e. 50 % MCP) with an injection system. Do i have to change my mixture setting with increasing altitude ?

Hi just one question, Are these topics updated to the current learning objectives or is some of the old stuff in here irrelevant now?

@Gianluca: Hi, The ATPL topics have not been updated after the date they were posted on this forum
@highegt: air density decreases with altitude so mixture has to changed
just a general rule, not talking about a specific question or an aircraft

Consider an aerofoil with a certain camber and a positive angle of attack. At which location will the highest flow velocities occur?

Hello Adnan
the highest velocity occurs at the point of maximum thickness

hello everyone, do anyone know what is middle wing of a plane

The force which causes the air to flow parallel to the curved isobars is called

@Marlon: See if this helps https://www.theairlinepilots.com/forum/viewtopic.php?p=502
@ Wai Kin: Hi
//rumbletalk-images-upload.s3.amazonaws.com/f1ea12db905325ba1971704b1d32da0c/1512708914-Untitled.png

Hi guys

When the weight of the aircraft is reduced to half during flight, what is the new airspeed in order to maintain level flight? 0.25,
0.5
0.71 of priginal height
original speed*

@me: In straight and level flight when IAS is doubled, the change in lift coefficient will be 0.25
hi, need help?

Hi guys, can somebody explain me why? "at a constant tas the dynamic pressure - willbe greater at sea level than at high altitudes"
or any links to understant

because of air density

so what is the difference between "constant tas" and "constant TAS through an inversion"
or they are the same?

Dynamic Pressure = 1/2 x density x Square of Speed
more density at sea level
in inversion the temperature increases with height
high temperature means lower density
that means low dynamic pressure
unless TAS is increased to compemsate

thanks you very much, but everything what you said i knew them, i dont know why im still doing stupid mistakes in aviation exam

Welcome. Mind becomes saturated in exams, its normal and happens with everyone ;)

Good day Everybody! can somebody explain why? - During a flight when the trailing edge flaps are lowered to the fully extended position ---> the wing CP moves aft( i got this part) , but How L/D ratio decreases?

Hi, Apart from increasing lift, flaps also increase drag. The increase in drag is more so ratio decreases e.g. 20/10 = 2.00, 23/20 = 1.15, 26/30 = 0.86 Both lift and drag are increasing but drag is increasing more so ratio value is decreasing.

what happens to thrust when I double flight speed while simultaneously double the rotational rate of a propeller

Propeller thrust depends on the blade angle of attack. At low airspeeds the angle of attacK will be large and thrust will more and vice versa. Coarsening the blade angle (on a variable pitch propeller) at higher speeds can help offsetting this effect to some extent. On a fixed pitch propeller the angle of attack can be increased by increasing power and reducing TAS. I don't know about the exact ratios in reference to your question as that might involve propeller efficiency mathematics. Following links might give you some clue: http://www.epi-eng.com/propeller_technology/selecting_a_propeller.htm or http://aerotrash.over-blog.com/2015/02/2-blade-vs-3-blade-and-4-blade-propellers.html

Hi All, I searched some websites but I couldn’t find anything about my questions, I would appreciate if someone can help with the following questions, 1) I read that starting from UK CAA and at some of the EASA countries the ATPL questions have changed but what about Bulgaria did the question also changed or BQ are just fine ? 2) Which QB would you suggest for ATPL exams in Bulgaria BGS or Aviation exam ?

Hi CFK: Are you in Bulgaria and what do the training academies over there say? You can try this one and see if they can guide http://flytraining.aero/become-a-pilot/atpla-distance-theory/

Would I need a degree in geography to become a pilot?

hi, no

ok thanks
wait
nvm
u said it to someone else lol

kbye

Hi, I'm a beginner airplane pilot. I look for tips and help to pass on job interview.

Hi, try this: http://www.latestpilotjobs.com/interviews/index.html

An aeroplane is tracking towards NDB maintaining track 120 degrees with 15 degree starboard drift. RBI should indicate bearing of ??

hu
hi
any body here?

hii

hi