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Search: Posts Made By: Connedrod
Showing results 1 to 35 of 37
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Forum: The Pacific: General Aviation & Questions
30th Dec 2020, 06:04
Replies: 1,350
Views: 590,420
Posted By Connedrod

please tell me how the trim was extended during...

please tell me how the trim was extended during the accident ?

the rudder trim control surface was still attached to the Trim actulator.

trim required rotary motion to turn into linear....
Forum: The Pacific: General Aviation & Questions
24th Dec 2020, 21:31
Replies: 1,350
Views: 590,420
Posted By Connedrod

Does not matter at all how in the first place the...

Does not matter at all how in the first place the trim was placed in this position.
At the end of the day the PIC has to take full responsibility. The end.
The evidence clearly shows that the...
Forum: The Pacific: General Aviation & Questions
4th Oct 2018, 02:27
Replies: 1,350
Views: 590,420
Posted By Connedrod

Some on on here earlier said btw that the CVR...

Some on on here earlier said btw that the CVR power came from #1&2 bus. This is incorrect power for the CVR comes from the HOT bus directly the unit. If it came via 1or 2 bus it can be turned off....
Forum: The Pacific: General Aviation & Questions
3rd Oct 2018, 02:08
Replies: 1,350
Views: 590,420
Posted By Connedrod

well thats 30 years on type add another 10 on...

well thats 30 years on type add another 10 on that. So how many flying hours do you have ?
Forum: The Pacific: General Aviation & Questions
29th Sep 2018, 09:16
Replies: 1,350
Views: 590,420
Posted By Connedrod

mmm thanks for my edumagation yeah i only have...

mmm thanks for my edumagation yeah i only have ofver 30 years muti cat lic coverage on type what would i know.
the conclusion that the trim position is from the actual positioning of the rudder...
Forum: The Pacific: General Aviation & Questions
28th Sep 2018, 20:58
Replies: 1,350
Views: 590,420
Posted By Connedrod

incorrect thats why its called rudder boost. Its...

incorrect thats why its called rudder boost. Its is air activation and operation. If it didnt have the power it would not be in the aircraft as it is.
Forum: The Pacific: General Aviation & Questions
26th Sep 2018, 08:17
Replies: 1,350
Views: 590,420
Posted By Connedrod

So the trims all are there to relieve load on...

So the trims all are there to relieve load on flying the aircraft. One would think that if the load is so great he would have reach down and put in the opposite load on the ruddef trim. This would...
Forum: The Pacific: General Aviation & Questions
25th Sep 2018, 08:06
Replies: 1,350
Views: 590,420
Posted By Connedrod

incorrect even if the nylon drive fails the...

incorrect

even if the nylon drive fails the over speed gov will caputure and allow slighty over max prop rpm. Independent system.

so if the rudder trim was full set to one way to which it...
Forum: The Pacific: General Aviation & Questions
11th Sep 2018, 02:31
Replies: 1,350
Views: 590,420
Posted By Connedrod

It be easy to see if if the wife’s were making...

It be easy to see if if the wife’s were making pwr just by the b to c flange position. From what I have heard they were making pwr.
Forum: The Pacific: General Aviation & Questions
15th May 2018, 07:26
Replies: 1,350
Views: 590,420
Posted By Connedrod

so clearly nothing to do with Maintence with...

so clearly nothing to do with Maintence with respect to friction knobs.
J hook is controlled by the gear wow switch. Once wow is achieved the the J hook is moved out of position and the hook is...
Forum: The Pacific: General Aviation & Questions
15th May 2018, 03:02
Replies: 1,350
Views: 590,420
Posted By Connedrod

was this the first flight after maintenance? we...

was this the first flight after maintenance?
we use the friction controls during engine runs after maintenance
Forum: The Pacific: General Aviation & Questions
13th May 2018, 09:05
Replies: 1,350
Views: 590,420
Posted By Connedrod

Really dose it matter if the outcome is 12 months...

Really dose it matter if the outcome is 12 months or 24 months if there was no mechanical defect which caused this accident which could lead to other accidents within the same type of aircraft. ...
Forum: The Pacific: General Aviation & Questions
10th Apr 2017, 07:15
Replies: 1,350
Views: 590,420
Posted By Connedrod

I like everyone else wondered why this accident ...

I like everyone else wondered why this accident happened. I can clearly see why now with comments like this.

English is not a sign of how smart one is. I feel blessed to have poor English...
Forum: The Pacific: General Aviation & Questions
10th Apr 2017, 01:59
Replies: 1,350
Views: 590,420
Posted By Connedrod

Min airspeed for a restart is 140KNOTS THATS...

Min airspeed for a restart is 140KNOTS THATS ABSOLUTELY MIN AIRSPEED.
Not 108 knots as has been quoted
Forum: The Pacific: General Aviation & Questions
10th Apr 2017, 00:57
Replies: 1,350
Views: 590,420
Posted By Connedrod

Mick, the report doesn't say the engines were...

Mick, the report doesn't say the engines were "operative". It just says that the cores were rotating at impact but they don't indicate at what possible speeds. Ram airflow will spin the core of a...
Forum: The Pacific: General Aviation & Questions
9th Apr 2017, 09:20
Replies: 1,350
Views: 590,420
Posted By Connedrod

[QUOTE=FGD135;9733708]You cannot draw that...

[QUOTE=FGD135;9733708]You cannot draw that conclusion from that evidence.

We sure can.
Atsb have stated it.
Indication marks on the roof are port to starboard in a forward diection. Not fwd to...
Forum: The Pacific: General Aviation & Questions
9th Apr 2017, 09:10
Replies: 1,350
Views: 590,420
Posted By Connedrod

Correct thats why its fitted with auto freather...

Correct thats why its fitted with auto freather to prevent this.
Forum: The Pacific: General Aviation & Questions
8th Apr 2017, 23:21
Replies: 1,350
Views: 590,420
Posted By Connedrod

Eddie We know the engine was operational at...

Eddie
We know the engine was operational at the time of impact. This is because the prop was not in a freathered position. At least postion of the condition levers may have been in two possibly...
Forum: The Pacific: General Aviation & Questions
8th Apr 2017, 19:21
Replies: 1,350
Views: 590,420
Posted By Connedrod

You obviously cannot understand what is happening...

You obviously cannot understand what is happening with the power plant IN FLIGHT. All of your experience and knowledge of this power plant is when you are doing static run ups, stationary ON THE...
Forum: The Pacific: General Aviation & Questions
8th Apr 2017, 09:22
Replies: 1,350
Views: 590,420
Posted By Connedrod

Do you understand how the Tq is calculated. Do...

Do you understand how the Tq is calculated. Do you understand that the oil suply to the prop at 1600 RPM IS AT VERY BEST ONLY JUST in gov range. This means to gov the prop is unlikely to occur. ...
Forum: The Pacific: General Aviation & Questions
8th Apr 2017, 01:32
Replies: 1,350
Views: 590,420
Posted By Connedrod

Yes its called an air drive between the cold and...

Yes its called an air drive between the cold and the hot section lol.
Forum: The Pacific: General Aviation & Questions
8th Apr 2017, 01:14
Replies: 1,350
Views: 590,420
Posted By Connedrod

Finally you are correct. You have no idea at all...

Finally you are correct. You have no idea at all do you. Zero thrust is only in the Beta condition. All other positions are ever forward or reverse thurst. And what is the primary perpose of the...
Forum: The Pacific: General Aviation & Questions
7th Apr 2017, 07:49
Replies: 1,350
Views: 590,420
Posted By Connedrod

Really so the figures given between 2000 down to...

Really so the figures given between 2000 down to 1586 Np. Pt6-42 is a free turbine engine. And even at a Np of 1586 the engine would be driving the prop. If you understand the engine and how it...
Forum: The Pacific: General Aviation & Questions
6th Apr 2017, 20:48
Replies: 1,350
Views: 590,420
Posted By Connedrod

Negative Tq. Are you really sure. Are you saying...

Negative Tq. Are you really sure. Are you saying the prop is in beta range or feather. Therefore the slash marks on the roof arnt slash marks which now marks what of the 2000 to 1586 rpm that has...
Forum: The Pacific: General Aviation & Questions
5th Apr 2017, 20:47
Replies: 1,350
Views: 590,420
Posted By Connedrod

No not at all. I was amazed that you could...

No not at all. I was amazed that you could detrime that the prop was at 2000 rpm from what little evidence was aviable at the time. You said simple maths was your answer. Well clearly not at you then...
Forum: The Pacific: General Aviation & Questions
3rd Apr 2017, 21:11
Replies: 1,350
Views: 590,420
Posted By Connedrod

Cherry picking? No... you revised that only after...

Cherry picking? No... you revised that only after i challenged you on that that, your reply was simple maths, down to 1586 rpm. How many goes do you wish to have. So no not cherry picking at all. ...
Forum: The Pacific: General Aviation & Questions
3rd Apr 2017, 11:23
Replies: 1,350
Views: 590,420
Posted By Connedrod

At 2050 rpm ish the O/S gov will take ovér prop...

At 2050 rpm ish the O/S gov will take ovér prop pitch. Any over tq will dump fuel from the fcu via py from the tq limiter.
Forum: The Pacific: General Aviation & Questions
3rd Apr 2017, 10:15
Replies: 1,350
Views: 590,420
Posted By Connedrod

Also if these estimates are correct for higher...

Also if these estimates are correct for higher rpm you can forget about the power lever roll back.
Forum: The Pacific: General Aviation & Questions
3rd Apr 2017, 09:53
Replies: 1,350
Views: 590,420
Posted By Connedrod

If the estimated prop speed is correct then it...

If the estimated prop speed is correct then it will be above the min auto Tq range, hence no auto feather.
Forum: The Pacific: General Aviation & Questions
3rd Apr 2017, 09:40
Replies: 1,350
Views: 590,420
Posted By Connedrod

Ummm 2000 rpm WAS given 1st then revised to 1586....

Ummm 2000 rpm WAS given 1st then revised to 1586. It WAS not given as an estimate as it WAS ginen as 2000rpm. Funny thing is you cant even agree on the size of the corrugations in the roof sheeting....
Forum: The Pacific: General Aviation & Questions
2nd Apr 2017, 02:56
Replies: 1,350
Views: 590,420
Posted By Connedrod

P3 / px pre fcu Py post fcu ie py to gov and tq...

P3 / px pre fcu Py post fcu ie py to gov and tq limiter on th -41/42
Forum: The Pacific: General Aviation & Questions
2nd Apr 2017, 02:48
Replies: 1,350
Views: 590,420
Posted By Connedrod

2000 rpm to 1586 rpm big difference. Please...

2000 rpm to 1586 rpm big difference. Please explain as you said it hit at 2000 rpm simple math you said. Difference is one being governed and one not. Nearly 25% not worried about a any ones...
Forum: The Pacific: General Aviation & Questions
1st Apr 2017, 08:18
Replies: 1,350
Views: 590,420
Posted By Connedrod

So what prop speed is it 2000rpm 1586 1833. So...

So what prop speed is it 2000rpm 1586 1833. So megans difference is nearly 25% ish. Thats a large difference is it not. Why is that important. Because one is in prop gov range and the other is...
Forum: The Pacific: General Aviation & Questions
31st Mar 2017, 10:37
Replies: 1,350
Views: 590,420
Posted By Connedrod

So over 24 hours has passed and you still not...

So over 24 hours has passed and you still not answered the question of fwd airspeed.
It is impossible to make the statment that the prop was at 2000 rpm with out knowing the airspeed to make the...
Forum: The Pacific: General Aviation & Questions
29th Mar 2017, 22:15
Replies: 1,350
Views: 590,420
Posted By Connedrod

Fwd airspeed at impact was ?

Fwd airspeed at impact was ?
Showing results 1 to 35 of 37
 
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