Well, did you ever.
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Mmmm with about 4000hrs in them (owning and instructing) I can tell you they are not "horrible little monsters" anyone with that attitude simply can't fly the twin comanche.
Hands up those who have had close calls during assymetric training,,,,,me included. You must be current, know that particular aircraft, know the students capabilities and most important know and understand your own limitations. Inattentiveness, tiredness lack of concentration all play a big part of your survival when the unexpected happens.
Hands up those who have had close calls during assymetric training,,,,,me included. You must be current, know that particular aircraft, know the students capabilities and most important know and understand your own limitations. Inattentiveness, tiredness lack of concentration all play a big part of your survival when the unexpected happens.
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I have used ICO in this scenario many times in the past, not recently when the overseas CAA's for whom I worked, banned use of the mixture for low level EF training. But even when it was allowed, the mixture remained at ICO only long enough for the student to retard the throttle. From that point on the mixture went to rich. Why do people think the mixture has to stay at ICO all the way to the ground? Doesn't the CAO use the term "simulated" failure, allowing for use of either throttle or mixture at PIC discretion? Genuine question from a foreigner btw.
Anyway, sometimes I needed power back in a hurry. I never had any trouble with it. Perhaps others did.
I rehearsed on the ground, and got my META trainee-instructors to rehearse, a quick pull of both mixtures to ICO following a low-speed excursion when asymmetric. This applied regardless of the means of simulating the engine failure. Then the instructor would have time to sort out the airspeed and engine mess while wings level. But it did take practise and recency.
Anyway, sometimes I needed power back in a hurry. I never had any trouble with it. Perhaps others did.
I rehearsed on the ground, and got my META trainee-instructors to rehearse, a quick pull of both mixtures to ICO following a low-speed excursion when asymmetric. This applied regardless of the means of simulating the engine failure. Then the instructor would have time to sort out the airspeed and engine mess while wings level. But it did take practise and recency.
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Not again - please.
The how's and why for's of simulating have been done to death, ad infinitum, ad tedium, ad nauseum.
This is about the bald insistence that 'simulation' is not good enough, the blind adherence to the 'letter' of the law, the piss poor, shallow analysis trotted out by the ATSB and the flat refusal to adapt to or adopt current world best training practice as recommended by ATSB, NTSB, CAA etc.
It's also about CASA being satisfied that, in a generic procedural trainer (simulator) that "you" can handle a specific aircraft type OEI. (Duchess or C421 same same ??).
Whether you throw a cat down the intake, remove the mixture lever or cut through a fuel line don't signify, provided you've got all the bets covered.
This is about the bald insistence that 'simulation' is not good enough, the blind adherence to the 'letter' of the law, the piss poor, shallow analysis trotted out by the ATSB and the flat refusal to adapt to or adopt current world best training practice as recommended by ATSB, NTSB, CAA etc.
It's also about CASA being satisfied that, in a generic procedural trainer (simulator) that "you" can handle a specific aircraft type OEI. (Duchess or C421 same same ??).
Whether you throw a cat down the intake, remove the mixture lever or cut through a fuel line don't signify, provided you've got all the bets covered.
Death is "real".
How many pilots have been killed or nearly scared themselves to death doing stuff like is mentioned here.
I did my 'Initial Twin' in good ole' DFH, (PA-30)mostly at Camden, and 'BARELY' missed the hill on a EFATO....
We all know that the approach or departure phases of flight are the most critical times to stall an aircraft BUT do we do stall training at theses times? No we don't. So why do some instructors insist on engine failure drills at times and places that put the aircraft and occupants at unnecessary risk. By all means do engine failures after take off but at a sensible altitude and place with respect to terrain etc.
Regarding this comment,
The Comanche is no aircraft I would like to be doing engine failures in below 5000ft.
CASA don't believe this to be a valid concern however.
CASA don't believe this to be a valid concern however.
With a VMCA of 80kts and only 160Hp each, it's a horrible little monster.
PA30B S/E Roc 260 fpm S/E ceiling 5800 feet
PA44 S/E RoC 212 fpm S/E ceiling 3800 feet
BE76 S/E RoC 235 fpm S/E ceiling 6170 feet
GA 7 S/E RoC 200 fpm S/E ceiling 4250 feet
PA31-310 S/E RoC 245 fpm S/E ceiling 15800 feet
C402B S/E RoC 225 fpm S/E ceiling 11320 feet
DA42 S/E Roc 170 fpm S/E ceiling 10000 feet
Of this group the PA30 has the best S/E RoC, and second only to the BE76 for S/E ceiling among the nromally aspirated aircraft on the list.
Guess what guys? If CASA needs to have concerns about the Comanche there's quite a few other aircraft they need to have in their sights as well and there's quite few other horrible little monsters out there.
Reading a few of the other posts it would seem that one of the real issues is how CASA, or perhaps more correctly some CASA staff interpret what is a failed engine. Sounds to me that some CASA personnel need to be taken aside and put straight on a few points. Requiring an engine to be completely shutdown for the complete exercise is raising the level of risk to unacceptable level in my book.
This accident highlights the critical importance of conducting the appropriate response actions following both an actual or simulated engine failure in a multi-engine aircraft; and the inherent risks of using the mixture control to simulate a failure at low altitude.
The reason for using the mixture to simulate a failure is so that the student must identify the failed engine correctly (i.e they always have control of the throttles, and can't see which mixture has been moved to ICO). The ONLY "inherent risk" in using the mixture is that the student will mis-identify the engine - but that is a risk inherent in any training scenario (i.e. it's not inherent in using the mixture) - that the student will from time to time, get it wrong.
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"horrible little monsters"
PA 39 - "horrible little monsters" anyone with that attitude simply can't fly the twin Comanche.
27/09 - We all know that the approach or departure phases of flight are the most critical times to stall an aircraft BUT do we do stall training at theses times? No we don't.
27/09 - Guess what guys? If CASA needs to have concerns about the Comanche there's quite a few other aircraft. etc.
27/09 - Sounds to me that some CASA personnel need to be taken aside and put straight on a few points.
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Regarding "putting straight" some examiners.
I would have thought that the public liability insurers would have had input by now.
CFI to examiner: "I'm sorry Bob, but our insurance company won't allow us to do 'x' any more, as it is not a legal requirement and they won't cover us for it."
I would have thought that the public liability insurers would have had input by now.
CFI to examiner: "I'm sorry Bob, but our insurance company won't allow us to do 'x' any more, as it is not a legal requirement and they won't cover us for it."
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Well spotted that man.
8/8 - I would have thought that the public liability insurers would have had input by now.
Could be voodoo or perhaps the sweet siren song of spin, spin spin lulls them into their current somnambulist state.
Quote of week that man 8/8.
I would have thought that the public liability insurers would have had input by now.
Insurers have their own risk assessment departments that weigh up the risks vs money to gain from a dodgy client. That's not to say they won't file away for a rainy day any info on dodgy ops carried out by a 'valued client'!
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From another PA30 appreciator
"With a level of officialdom mixed with stupidity, the FAA recommended that Vmc demonstrations in twins be done at low altitudes to ensure maximum power from the live engine. Even in the placid Apache, low-level Vmc demonstrations could be terminal.
For training schools the PA-30 was an ideal Apache replacement. Small, economical and with great handling, it was a popular choice as a primary multi-engine trainer.
The only problem is that its high performance wing does not cut the pilot much slack or tolerate abuse from pupils.
With the benefit of 20/20 hindsight we now know that no light twin, (except Cessna's 336/337) should be stalled with one engine dead.
The wide distribution of weight in the engines and fuel has an aggravating affect under asymmetric thrust.
Once the rudder has run out of effective control (below Vmc), a stall may quickly turn into an unrecoverable flat spin. At FAA recommended low altitudes, this was a great prescription for killing pilots in training and is exactly what happened.
It led to the Twin Comanche acquiring a totally undeserved reputation.
In belated recognition of demonstrating the dangers of Vmc, the FAA responded in 1969 by a simple stroke of the pen, to increasing the PA-30's Vmc from 71 to 77 kts. The implications of this can be seen when evaluating the aircraft."
From: Fliteguide / Imperial Aviation
Keep the PA-30s' flying and respect their ability.
For training schools the PA-30 was an ideal Apache replacement. Small, economical and with great handling, it was a popular choice as a primary multi-engine trainer.
The only problem is that its high performance wing does not cut the pilot much slack or tolerate abuse from pupils.
With the benefit of 20/20 hindsight we now know that no light twin, (except Cessna's 336/337) should be stalled with one engine dead.
The wide distribution of weight in the engines and fuel has an aggravating affect under asymmetric thrust.
Once the rudder has run out of effective control (below Vmc), a stall may quickly turn into an unrecoverable flat spin. At FAA recommended low altitudes, this was a great prescription for killing pilots in training and is exactly what happened.
It led to the Twin Comanche acquiring a totally undeserved reputation.
In belated recognition of demonstrating the dangers of Vmc, the FAA responded in 1969 by a simple stroke of the pen, to increasing the PA-30's Vmc from 71 to 77 kts. The implications of this can be seen when evaluating the aircraft."
From: Fliteguide / Imperial Aviation
Keep the PA-30s' flying and respect their ability.
Last edited by Up-into-the-air; 30th Jan 2012 at 13:36.
Splitty
What a lot of unmitigated Cr*p. Where ever did you get this idea from?
Isn't there a lot of uninformed clap trap about some aircraft?
Up-into-the-air
Vmc went from 71 KIAS to 77 KIAS at the stroke of the FAA's pen not the 81 to 91 as quoted in your reference. 91 kts is Vy. Otherwise a good brief summary.
Pull the Mixture .... Pull the Death Cord ...........Cutting the Mixture was banned in NZ many years ago in the PA 30's after many fatals in the USA.
Isn't there a lot of uninformed clap trap about some aircraft?
Up-into-the-air
Vmc went from 71 KIAS to 77 KIAS at the stroke of the FAA's pen not the 81 to 91 as quoted in your reference. 91 kts is Vy. Otherwise a good brief summary.
As Vmc is a performance number, and is determined by the engine power/rudder authority, how can a "stroke of the pen" possibly change it?
It was a knee jerk reaction to a string off accidents which were largely caused by the FAA stupid Vmc demonstration requirements.
Interestingly Vmc for the the PA 39 is still 71 knots which was the original figure for the PA30. Perhaps there was some more flight testing done on the PA 30 and it was determined with the critical engine inoperative the Vmc was 77, but so far as I am aware it was just a "stroke of the pen". Perhaps someone with a good knowledge on such things may be able to tell us if 6 knots difference in Vmc between the critical and non critical engines is the sort of difference to expect.
As a learner, one of the most exquisite issues for me is the relationship between the edges of the actual flight envelope and the published flight envelope.
Without a detailed understanding of how the published edges of the envelope were promulgated, one is asking for trouble.
This from a mug that has only once neared the edge (as far as he knows) - stall warning on a hurried base to final turn in a C172.
Without a detailed understanding of how the published edges of the envelope were promulgated, one is asking for trouble.
This from a mug that has only once neared the edge (as far as he knows) - stall warning on a hurried base to final turn in a C172.
Hi 27/09,
Yep! We 'barely' missed that bloody hill. And, guess what? ITS STILL THERE!
And so are 'we'.
It was quite apparent that we were going to go 'close' but, close and clear.
(Unless the 'good one' coughed), then the plan - yes, there was always a plan - bring up the other one from 'zero thrust' and keep on going, to the clear ground beyond.
I reckoned it was better to maintain the 'ole girl' in S&L, trying to climb, rather than make a turn 'away' from the hill which we were going to clear anyway, and invite 'trouble'.....
Even in the AC-50 as described earlier, there was certainly a 'plan'...
I guess that its when we don't consider much beyond the 'now' that we are likely to get into problemos....
And if you think this is all 'in hindsight', then I have been 'lucky' and have had good instructors and colleagues who think this way, and it 'rubbed off'.
Fortunately. I'm now 'old enuf' to enjoy the 'mistakes'.......
Cheers
Yep! We 'barely' missed that bloody hill. And, guess what? ITS STILL THERE!
And so are 'we'.
It was quite apparent that we were going to go 'close' but, close and clear.
(Unless the 'good one' coughed), then the plan - yes, there was always a plan - bring up the other one from 'zero thrust' and keep on going, to the clear ground beyond.
I reckoned it was better to maintain the 'ole girl' in S&L, trying to climb, rather than make a turn 'away' from the hill which we were going to clear anyway, and invite 'trouble'.....
Even in the AC-50 as described earlier, there was certainly a 'plan'...
I guess that its when we don't consider much beyond the 'now' that we are likely to get into problemos....
And if you think this is all 'in hindsight', then I have been 'lucky' and have had good instructors and colleagues who think this way, and it 'rubbed off'.
Fortunately. I'm now 'old enuf' to enjoy the 'mistakes'.......
Cheers
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Tall tales- but true.
And all good yarns, no doubt. But off the point lads, away off. Finally hunted down a 1996 AFM, page 3-7 presents a small paragraph referring to 'Simulated Single Engine Operations'. The manufacturer holds (held) the type certification data and, produces the AFM against that data and as correctly pointed out, meets the pertinent FAR 23 requirements.
The AFM paragraph mentions a couple of small items which the ATSB have managed not to mention such as. "Simulated engine failure should be performed at an altitude that will allow enough room for a safe recovery (5000 ft min, terrain clearance is recommended) should control of the airplane be lost".
Left engine throttle - - Retard.
**Note**. "While Vsse is the accepted airspeed below which an engine should never be intentionally failed, it is recommended that the airspeed should never be allowed to fall below the blue line (105 mph) when operating single engine".
It is of interest to us that these are from the Emergency Procedures section of the AFM.
The proposed changes to the Operations Manual (refer ATSB report) do not comply with the manufacturer procedures, are accepted by CASA and the ATSB fails to mention the fact.
Questions: you bet, lots of. But first, lets see what the esteemed members make of the 'Bible' version of how it is recommended that single engine operations be conducted in an aircraft which is not certified for low. slow. dead cut failure and climb out. Not the practical stuff, but as it would be heard in a Coroners Court.
"well M'lud, seems they operating contrary to etc. etc".
The AFM paragraph mentions a couple of small items which the ATSB have managed not to mention such as. "Simulated engine failure should be performed at an altitude that will allow enough room for a safe recovery (5000 ft min, terrain clearance is recommended) should control of the airplane be lost".
Left engine throttle - - Retard.
**Note**. "While Vsse is the accepted airspeed below which an engine should never be intentionally failed, it is recommended that the airspeed should never be allowed to fall below the blue line (105 mph) when operating single engine".
It is of interest to us that these are from the Emergency Procedures section of the AFM.
The proposed changes to the Operations Manual (refer ATSB report) do not comply with the manufacturer procedures, are accepted by CASA and the ATSB fails to mention the fact.
Questions: you bet, lots of. But first, lets see what the esteemed members make of the 'Bible' version of how it is recommended that single engine operations be conducted in an aircraft which is not certified for low. slow. dead cut failure and climb out. Not the practical stuff, but as it would be heard in a Coroners Court.
"well M'lud, seems they operating contrary to etc. etc".
Sounds to me that some CASA personnel need to be taken aside and put straight on a few points. Requiring an engine to be completely shutdown for the complete exercise is raising the level of risk to unacceptable level in my book.
Actually, they need to betaken out and shot, so they can't pass their dominant stupid gene on to another generation.
Much of Polar Air's troubles started with a argument about how EFATO training would be conducted, with the owner of Polar flatly refusing to "fail" and engine as required by "CASA" ----- then followed the "special audits" etc. There is a thread here somewhere with all the details ---- this case is going to the High Court of Australia.
I am not short of other examples on the easy coast.
Tootle pip!!
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Quite a slience.
Sunfish - This from a mug that has only once neared the edge (as far as he knows) - stall warning on a hurried base to final turn in a C172.
Had a beer with a wise man last evening, clever fellah. Suggested I read between the lines of the ATSB report on this and see what could be gleaned from the oh so subtle, tongue in cheek way it penned. Suddenly the light came on – 'lighty training incident, no broken bones' – Alt/F/Del.
Except there are matters outstanding on this account, in primus the conflict between the eye witnesses (which are pretty hard to find alive), the 'candidate pilot' and his erstwhile instructor. Secundus the method employed to train the hapless victim, the reason for the training being conducted as it was and to finish; why has there not been a deep and meaningful recommendation made to the puzzled plebs.
ATSB are probably sick to death of passing along recommendations which are blithely ignored, all those lovely shiny brochures, carefully written sage advice and bright hopes dashed. Got some very interesting numbers (NFP) related to 'ignored' recommendations.
Bring back Russ Evans, before we all end up crispy critters. Steam off.