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Search: Posts Made By: mirkoni
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20th Aug 2022, 18:42
Replies: 16
Views: 931
Posted By mirkoni

Two pilots + full tanks was calculated to be a...

Two pilots + full tanks was calculated to be a little overweight... airplane measured on scales previously, got BEW from the maintenance organisation...
20th Aug 2022, 06:24
Replies: 16
Views: 931
Posted By mirkoni

Thanks for the answer. The common practice is...

Thanks for the answer.
The common practice is to fill the tanks right up, but with two of us in the cockpit and full tanks Seneca IV goes overweight. So I need to find a way to fill it to an amount...
20th Aug 2022, 06:21
Replies: 16
Views: 931
Posted By mirkoni

Thanks for the answer. The common practice is...

Thanks for the answer.
The common practice is to fill the tanks right up, but with two of us in the cockpit and full tanks Seneca IV goes overweight. So I need to find a way to fill it to an amount...
18th Aug 2022, 20:36
Replies: 16
Views: 931
Posted By mirkoni

Precise Fuel Mass Measurement in GA

Dear fellow pilots,
How do you practically solve the problem of precise measurement of fuel quantity in your tanks, in order to calculate the fuel mass that you have in them, needed for mass and...
Replies: 30
Views: 17,354
Posted By mirkoni

...Talking about studying the new syllabus,...

...Talking about studying the new syllabus, anyone knows anything about new CBTs and Textbooks based on the new EASA syllabus? Tried to email some well known CBT producers a few times regarding that,...
Forum: Tech Log
24th Nov 2017, 07:17
Replies: 5
Views: 6,557
Posted By mirkoni

vapilot2004, Thank you very much for the...

vapilot2004,

Thank you very much for the answer, it all seems logical. In the meantime, I found something in the 737 FCOM and similar explanation in youtube video on hydraulic system for PMDG...
Forum: Tech Log
23rd Nov 2017, 09:38
Replies: 5
Views: 6,557
Posted By mirkoni

Can hydraulic EDP in B737 overheat?

Hello all,

On the hyraulic panel there is an OVERHEAT indication above electric motor driven pump. There is no such indication above mechanical EDP. In some textbooks there is a mention of case...
28th Jan 2017, 15:52
Replies: 1
Views: 1,914
Posted By mirkoni

Oxford PPL Books

Hello all,

Anyone has a link to PDF version of 7 Oxford PPL Books, please?
Much needed.

Thank you!
Forum: Tech Log
18th Aug 2016, 11:16
Replies: 10
Views: 4,566
Posted By mirkoni

Ground connection to the right manifold could be....

Ground connection to the right manifold could be.
Is it maybe about always starting first the engine no 1, which is connected to the left manifold? Do they necessarily always start No 1 first?
Forum: Tech Log
11th Aug 2016, 11:56
Replies: 10
Views: 4,566
Posted By mirkoni

737 - Why is APU bleed connected to left pneumatic manifold

I just can not remember - but there must be a simple reason - why is that APU bleed is connected to left pneumatic manifold in Boeing 737?...

For the APU fuel feed I know it is connected to the...
Forum: Tech Log
11th Aug 2016, 08:31
Replies: 0
Views: 724
Posted By mirkoni

Wisdom on Virtual Procedure Trainers

Hi everyone,

I just could not google any general information on Virtual Procedure Trainers - who are the manufacturers etc.

What are your experiences with it? Who are main manufacturers in...
Replies: 1,315
Views: 924,065
Posted By mirkoni

two thirds of cruise alt for average TAS

Hi ,

This is really bugging me. Please help. Why do we use 2/3 of the cruising altitude for calculating average TAS during climbing (and why we use 1/2 for descent). Why this value? Where is it...
Forum: Tech Log
14th Jul 2015, 10:10
Replies: 2
Views: 2,198
Posted By mirkoni

Why 2/3 of the cruising altitude for TAS

Hi chaps,

Just wandering if anyone knows why we use 2/3 of the cruising altitude for calculating average TAS during climbing (and why we use 1/2 for descent). Why this value? Where is it derived...
Forum: Tech Log
21st Jan 2015, 11:24
Replies: 14
Views: 8,590
Posted By mirkoni

If I understood you well: - Ice IS forming...

If I understood you well:

- Ice IS forming on LE of tailplanes and fin, but is not having large detrimental effect on aerodynamics ? How is this possible?

- Water is drained during flight...
Forum: Tech Log
21st Jan 2015, 09:56
Replies: 14
Views: 8,590
Posted By mirkoni

A320 No Tail Antiicing

Hello experts,

What is the explanation on lack of tail anti / de icing on A320. i presume that horizontal tail is not impacted directly by supercooled droplets due to wing downwash, but what about...
Forum: Tech Log
8th Aug 2014, 08:14
Replies: 5
Views: 3,815
Posted By mirkoni

Thanks Goldenrivet, for prompt and clear answer. ...

Thanks Goldenrivet, for prompt and clear answer.

Do you happen to know if the reverser stow/deploy process on Airbus or Boing operation can be interrupted during the motor operation, or reverser...
Forum: Tech Log
7th Aug 2014, 09:20
Replies: 5
Views: 3,815
Posted By mirkoni

Thrust Reverser Effects On Touchdown

Hi All,

I read in Park's notes for A320:

"Be careful not to let the nose ride up when reverse is selected. Select Full Reverse as you lower nose."

Why would this happen when the moment of...
Forum: Tech Log
24th Jun 2014, 11:39
Replies: 6
Views: 4,395
Posted By mirkoni

Thumbs up OK I think this is more clear now, let's...

OK I think this is more clear now, let's summarize

- While in critical flight phase (T/O or landing), center tank fuel pumps inhibited, "Tank-to-Engine" principle used (even if there is...
Forum: Tech Log
19th Jun 2014, 14:45
Replies: 6
Views: 4,395
Posted By mirkoni

Thank you for the propmpt answer. But then...

Thank you for the propmpt answer.

But then again, why is this rule - why is it forbidden to use only one tank during take off? And presumably, landing too? Safety reasons? In what way?

Maybe...
Forum: Tech Log
19th Jun 2014, 13:43
Replies: 6
Views: 4,395
Posted By mirkoni

Center tank booster pumps on A320 series

Hello All,

If I understood well from airbus cbt and Park airbus notes, center booster pumps on A320 not working when slats are down?
Anybody know what is the reason? AFAIK, 737 doesn't have this...
Forum: Tech Log
3rd Feb 2014, 07:27
Replies: 70
Views: 15,394
Posted By mirkoni

Thanks for the prompt answer. Regarding...

Thanks for the prompt answer.

Regarding radio-altimeter not working on cruise altitudes, I presume it is because of the time it needs for the beam to go and return back from earth to the airplane...
Forum: Tech Log
3rd Feb 2014, 06:39
Replies: 70
Views: 15,394
Posted By mirkoni

Why use only pitot-static system for altimeter/airspeed

Hello all,

Yesterday I was watching AF 447 documentary on natgeo. What crossed my mind:
Why there is no backup system if all pitot systems fail - i.e. radio altimeter or at least GPS. I know this...
Forum: Tech Log
12th Jun 2013, 11:09
Replies: 0
Views: 934
Posted By mirkoni

Aviation Technical Podcasts

Hello,
Does anybody know of any specialized aviation technical / maintenance podcast? E.g. talk about how the airplane systems work, case studies, but from technical viewpoint...?
I know of...
Forum: Tech Log
12th Apr 2013, 14:09
Replies: 0
Views: 1,188
Posted By mirkoni

Why two serial crossfeed valves on Fokker 100?

Can somebody give an explanation please - why are there two crossfeed valves in SERIES installed on Fokker 100?

In B777 for example, there are two valves in parallel, but that is logical - if one...
Replies: 1
Views: 3,431
Posted By mirkoni

I was just curious, where did you get that...

I was just curious, where did you get that information from? Your own experience or...?

I think they have a lot of experience (training for ATPL from 1972) so I think the quality of training is...
Forum: Tech Log
8th Jun 2010, 13:53
Replies: 0
Views: 697
Posted By mirkoni

Oxygen Mask Exhale CO2

Question about the diluter demand Oxygen Masks :

How is CO2 exhaled by pilot exhausted from inside the mask, when you use diluter-demand (cockpit) oxygen mask in "Emergency" position (likewise...
Forum: Tech Log
26th May 2010, 09:06
Replies: 3
Views: 1,170
Posted By mirkoni

OK let's take a concrete example. For OAT of...

OK let's take a concrete example.
For OAT of 140 F and pressure altitude of 2000 FT you have N1 = 88.9%

If I understand you well, you still have space to push thrust lever above this N1, and by...
Forum: Tech Log
26th May 2010, 08:17
Replies: 3
Views: 1,170
Posted By mirkoni

737-600 Thrust Setting Question

If you look at the table of N1 setting for B 737-600, you can see that in one column (for the fixed pressure altitude) , as the OAT temperature rises from the lowest values, the N1 setting for max...
Showing results 1 to 28 of 28


 
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