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-   -   PT6 Failure (https://www.pprune.org/pacific-general-aviation-questions/400433-pt6-failure.html)

av8trflying 31st Dec 2009 00:18

PT6 Failure
 
A skydiving caravan in Cairns just had a total engine failure at 12,000ft.

Glided back to the field safely.

Well done that man.:ok:

Super Cecil 31st Dec 2009 00:24

Fuel systems failure?

av8trflying 31st Dec 2009 00:26

Pilot said he doesn't know. Tried a restart but nothing. All skydivers got out at 12

Howard Hughes 31st Dec 2009 00:36

Skydivers weren't responsible perchance? They have been known to take the occasional thing, like keys!:eek:

OK, OK, I know Caravans don't have keys...well not start them anyway!

toolowtoofast 31st Dec 2009 01:12

I've had the mixture pulled by the DZ/aircraft owner, but never the keys. If someone did pull my keys, they would be nursing a very sore jaw about 5 minutes later, and I would refuse to ever take them up again. The guys at my DZ know this, so we're all on the same page :)

Back to the subject - highly unusual for a pT6 to give out without some outside influence like overtemp or overtorque or underfuelling, however poor maintennance will of course lead to failure (more often though lead to reduced performance, which leads to high temps etc...)

lk978 31st Dec 2009 01:44

nice work... see its not true what they say about skydive drivers they can actually fly :D

harder then it sounds from that altitude it is almost too much altitude would have been a slower decent than normal

ps i doubt any skydiver would mess around with a Caravan, they do sit pretty close to the FC lever though

The Green Goblin 31st Dec 2009 02:52

Those pesky PT6s playing up again hey?

kam16 31st Dec 2009 04:11

Well done to the pilot did a super job from SW of aerodrome left downwind snaking down final and an absolute greaser of a landing vacating at A3 under own steam so to speak.
No idea the reason for the failure but congradulations Mr Pilot you sounded very cool under pressure and never in doubt from our view:D:D.

VH-XXX 31st Dec 2009 06:35


harder then it sounds from that altitude it is almost too much altitude would have been a slower decent than normal
Are you for real? What could you possibly mean by this? How on earth can you have too much altitude with an engine failure (unless you are ojn fire and even then it would be a good thing to help it burn out)? Anyone who couldn't pull off a perfect landing from 12,000ft should have their licence pulled off them, even if they are a GFPT !!!!! :ugh:

fasterblaster 31st Dec 2009 08:02

12,000 feet
Very close to a 3km runway
No pax

Can't get much luckier than that, compare that to the poor guy in png!

Super Cecil 31st Dec 2009 08:18

Will be interesting to see why it stopped. Recon a Caravan might go allright with an 1820 innut, you'd have to use avgas then.:}

Howard Hughes 31st Dec 2009 10:34


Recon a Caravan might go allright with an 1820 innut, you'd have to use avgas then.
And oil!;)

zac21 2nd Jan 2010 00:01

Does anyone know why it stopped yet ?????

Ref + 10 2nd Jan 2010 00:53


If I had an engine failure in anything I'd want it to be in a van
or maybe a twin :O

Well done to the guy. I'll bet the pax were happy they had those bags on their backs.

There seemed to be a bunch of vans having engine failures around the world. For a while a year or two ago they always seemed to be in the accident reports of Australian Aviation. I know of 3 PT6 failures in King Airs and Vans. No of them happened to me thankfully but one of them was particularly concerning as the casing didn't contain the blades as they parted company from the turbine wheel.

It's good to hear that everyone was fine.

Wally Mk2 2nd Jan 2010 00:56

There's a 'van' operating out of EN these days often (shifty business) & wonder what the ability of same would be if an eng failure occurred at say 300ft on a typical day say 10 kts H/W. Can these big lumbering ducklings turn & glide back to the rwy from that height? Some guru 'van' man (or gal) might be able to shed some light here.
As for why the '6' failed? Can only be fuel related. The other 2 things needed for an 'infernal' combustion engine to work will always be there once running unless hardware mech failure prevailed which still really means fuel not being supplied or the inability not to be able to turn.

Now I know why we have '2' of 'em, safety in numbers:}


Wmk2

rigpiggy 2nd Jan 2010 01:10

Narrative:
En route from Tofino to Vancouver, the pilot issued a mayday and wanted to divert to Port Alberni Airport, BC (YPB). The aircraft did not make it and crashed in the woods, some 10 km from the airport.

CONCLUSIONS
FINDINGS AS TO CAUSES AND CONTRIBUTING FACTORS:
1. The engine lost power when a compressor turbine blade failed as a result of the overstress extension of a fatigue-generated crack. The fracture initiated at a metallurgical anomaly in the parent blade material and progressed, eventually resulting in blade failure due to overstress rupture.

2. The combination of aircraft position at the time of the engine failure, the lack of equipment enabling the pilot to locate and identify high terrain, and the resultant manoeuvring required to avoid entering instrument flight conditions likely prevented the pilot from attempting to glide to the nearest airfield.

glekichi 2nd Jan 2010 03:10


There's a 'van' operating out of EN these days often (shifty business) & wonder what the ability of same would be if an eng failure occurred at say 300ft on a typical day say 10 kts H/W. Can these big lumbering ducklings turn & glide back to the rwy from that height?
I'm no van man, never flown one, but my guess is that at EN you would hit 300ft with half the runway remaining and have plenty of room to land.

I'd still rather a King Air!

tail wheel 2nd Jan 2010 04:22


"...casing didn't contain the blades as they parted company from the turbine wheel."
Compressor turbine?

Surprising the failure was not contained as the -114 has a containment ring around the CT wheel.

In respect to 'Van engine failures, I wonder how many of those had daily compressor washes, engine trend monitoring systems and regular boroscope inspections?

fencehopper 2nd Jan 2010 04:48

The pilot has now set a standard for those tight ass tandem operators. They will want him to dead stick after every drop to save engine time and fuel.

Wally Mk2 2nd Jan 2010 04:56

Reliability of any engine is all about maintenance or lack thereof.

I know we (as in our Co) have near 30 '6's' all operating high cycles & at times in less than fav conditions & no engine failures after a zillion hrs.(a few shut down at pilot discretion, bunch of sissies they are:}) All hangin' in there due I believe good maintenance with reg comp washes & engine tear downs at the slightest hint of sumfun' fishy. BUT that doesn't mean am gunna fly with just one '6' at a time!:}
Tnxs to the boys who keep us safe, the Engineers, we loves ya!:ok:


"glekichi" am not too sure about ldg straight ahead on what's left of the AD after an eng failure at say 300 ft. I've watched the ugly ducklings (the van) get to about that height & I'd hate to have to get it back on the deck with what's left still I guess a controlled crash on airport is better than off airport especially off Rwy 17 @ 17....yeeek!
Amazing A/C just the same, be nice to fly if it's typical Cessna.




Wmk2

Howard Hughes 2nd Jan 2010 05:13

I second Wally's comments, it's great to work somewhere where even the slightest abnormality is taken seriously!

Keep up the good work guys!:ok:

Super Cecil 2nd Jan 2010 05:28

There have been failures to things other than bad maintenance and throttle bashing, and to resonably low hour powerplants.

Howard Hughes 2nd Jan 2010 05:42

Occasionally things break without warning, but if you take care of the areas you can control, then you are minimising the risk.

Of the six people I know who have had engine failures in turbines, five were FCU failures! :eek:

VH-XXX 2nd Jan 2010 05:59


where even the slightest abnormality is taken seriously!
like when the second backup AH fails, bummer.

manymak 2nd Jan 2010 07:34


In respect to 'Van engine failures, I wonder how many of those had daily compressor washes, engine trend monitoring systems and regular boroscope inspections?
If van's (or any S/E turbine) are operating as part of a ASETPA (Approved Single Engine Turbine Powered Aircraft) approval it is a requirement they undertake daily comp washes and have trend monitor systems fitted to those aircraft.

Lasiorhinus 2nd Jan 2010 07:42

Wasn't VH-DVS, was it? If so, it's the second engine failure in 18 months- and the first one had absolutey nothing to do with fuel.

manymak 2nd Jan 2010 07:48


Wasn't VH-DVS, was it? If so, it's the second engine failure in 18 months- and the first one had absolutey nothing to do with fuel.
Didn't the ARO find turbine power blades on the rwy? :eek:

werbil 2nd Jan 2010 08:45

Caravan Pilots • View topic - Caravan Accident contains some interesting comments regarding an engine failure in a C208.

Arnold E 2nd Jan 2010 08:46

XXX
 
If the second A/H fails, please explain to me how you handle that?:confused:
To be honest, I am interested in how you know the second A/H HAS failed.

werbil 2nd Jan 2010 09:28

Arnold E:

Secondary instruments (which is the ONLY way you can tell a single AH has failed or determine which AH has failed if you have 2):

Turn cordinator & dg (compass in worst case) for lateral.
Power plus performance for pitch.

Big beef with my training was did a bit of limited panel work, but there was no training on how to diagnose a suspect insturment.

One AH failure I had was obvious - the thing was showing a roll rate of about 1400 degrees per second. You could even feel the vibration through the airframe.

werbil

PS - the most insidious instrument failure I've had was a partial blockage of a pitot tube - airspeed indicator was undereading by about 20 knots. At least with a blocked static system the constant altitude indication gives you a very good hint to treat the airspeed indication with extreme caution.

VH-XXX 2nd Jan 2010 10:18

Arnold, there was sarcasm in my post. I said second backup, as in AH #3.

Have a mate that flies and he was telling me how he comes to work for the day, checks everything, finds the tiniest of issue (eg failed second backup), declares ac us, collects his $500 and goes home again. It would be good to think that all operators were like that. (sorry thread drift)?

Arnold E 2nd Jan 2010 10:25

the thing was showing a roll rate of about 1400 degrees per second.
An A/H showing a roll rate of 1400 degrees /sec?? please explain??:confused:

Do you mean it had toppled?
Just for information, an A/H is not a rate gyro.

werbil 2nd Jan 2010 11:07

The AH was indicating that the aircraft was rolling completely around the longitudinal axis about 4 times each second - hence the calculated roll rate.

It had failed - I'm pretty sure it ended up just lolling about when it stopped spinning - I can't remember for sure - it did happen about 15 years ago. It's funny the bits you remember - I could show you on a map where it occured within a radius of a about half a mile - I was climbing at the time - possibly in a shallow right hand turn.

Arnold E 2nd Jan 2010 11:16

Hmmm, ok gymbal lock.

YMEN 2nd Jan 2010 14:56

It was VH-UMV, not VH-DVS!

YMEN 3rd Jan 2010 01:13

Ah you jumped with SAM! Top Bloke!

BackdoorBandit 3rd Jan 2010 03:17

Al's dodgy vans are everywhere. It is no surprise that the last two letters of the rego are "MV".

littlehurcules 3rd Jan 2010 06:27

Stay well clear of any plane ending with "MV"

Like the man - the planes are dodgy as well

beaver_rotate 3rd Jan 2010 11:14

Big Al has his own McRnav's into Tully he's making the kids fly.

I mean it's not like QLD's HIGHEST LSALT is nearby or anything.

CASA know and have been watching, many a trip to Tully one of the CS FOI's told me.

So boys, if you have these approaches loaded into your Vans, I would delete them quick smart (if you get my drift) ;)

j3pipercub 3rd Jan 2010 12:44

So it was U hey? Hmm interesting. All of the MV's were on a system of maintenance, I believe to try and extend the life of the donk, last I heard M was past 6k on its donk. Thought with the exception of O, U had the lowest time engine.

Something to do with the cool starts and the short-circuiting of the over-voltage protection (32 volt battery cart if memory serves). Just don't touch the avionics masters with the cart plugged in, lest the magic blue smoke start to pour out of the radion stack, or so I've heard.


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