22 Nov 2025, 13:48 [ UTC - 5; DST ]
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Post subject: Re: Single engine pressurized above FL 250 Posted: 24 Jan 2016, 21:27 |
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Joined: 01/16/11 Posts: 11068 Post Likes: +7097 Location: Somewhere Over the Rainbow
Aircraft: PC12NG, G3Tat
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Username Protected wrote: Mike - I was referring to jets and certainly there is no large body of evidence or false perceptions here but anyway, others have already pointed it out,  Bruce, my bad, I was talking about Turboprops. I got zero jet experience, except for commercial.  ...and we gotta work on your [quote] tag handling 
_________________ ---Rusty Shoe Keeper---
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Post subject: Re: Single engine pressurized above FL 250 Posted: 24 Jan 2016, 22:26 |
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Joined: 07/21/08 Posts: 5836 Post Likes: +7285 Location: Decatur, TX (XA99)
Aircraft: 1979 Bonanza A36
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Username Protected wrote: Your statement about the unusually high loss of control accidents is not correct. I believe it is. Read through the 10 PC12 fatals and 12 TBM fatals since 1/1/2007. Loss of control recurs quite a lot. Here are the PC12s: 1/16/2013: "The pilot's failure to maintain airplane control due to spatial disorientation during the initial climb after takeoff in night instrument flight rules conditions." 6/7/2012: "The failure of the pilot to maintain control of the airplane while climbing to cruise altitude in instrument meteorological conditions (IMC) following disconnect of the autopilot. The reason for the autopilot disconnect could not be determined during postaccident testing. Contributing to the accident was the pilot's lack of experience in high-performance, turbo-propeller airplanes and in IMC." 7/5/2009: "The pilot's failure to maintain control of the airplane while in instrument meteorological conditions following a reported instrumentation failure for undetermined reasons." 3/22/2009: "(1) the pilot's failure to ensure that a fuel system icing inhibitor was added to the fuel before the flights on the day of the accident; (2) his failure to take appropriate remedial actions after a low fuel pressure state (resulting from icing within the fuel system) and a lateral fuel imbalance developed, including diverting to a suitable airport before the fuel imbalance became extreme; and (3) a loss of control while the pilot was maneuvering the left wing-heavy airplane near the approach end of the runway." 1/11/2009: "The pilot's loss of control due to snow/ice contamination on the airplane's lifting surfaces as a result of his decision not to deice the airplane before departure." 9/29/2008: "The pilot's incapacitation due to fatigue resulting in an in-flight collision with terrain." Of the 7 fatal PC12 accidents with a probable cause listed in the NTSB database since 1/1/2007, 6 of them are related to loss of control with no defect in the airplane. 3 are foreign, no cause listed. To me, that is an abnormally high rate of loss of control, representing the overwhelming majority of the fatal accidents. Or do you think that predominance of loss of control is "normal"? Mike C. Are you inferring that these accidents are somehow the product of the plane being a single TP? If so, what plane would have been a better choice for any of these pilots. Poor decisions are pretty non discriminatory when it comes to brand/type.
_________________ I'm just here for the free snacks
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Post subject: Re: Single engine pressurized above FL 250 Posted: 25 Jan 2016, 00:41 |
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Joined: 12/03/14 Posts: 20758 Post Likes: +26247 Company: Ciholas, Inc Location: KEHR
Aircraft: C560V
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Username Protected wrote: Are you inferring that these accidents are somehow the product of the plane being a single TP? This line of discussion started with the "pilots won't get an ME rating". As noted, it is an easy rating to get, yet it was suggested this was a barrier for some. So a possible theory is that pilots of lesser talent may be more common in single engine aircraft. A self selection process. The high number of loss of control accidents, which are pilot caused, suggests this may be a factor. Quote: If so, what plane would have been a better choice for any of these pilots. One of lesser performance so they aren't behind the airplane. A 10,000 lb, 1200 HP, ~300 knot airplane needs a pilot to match no matter how many engines it has. Quote: Poor decisions are pretty non discriminatory when it comes to brand/type. While that seems obviously true, it may not be. Certain types attract certain kinds of pilots. Loss of control in jets, for example, occurs very rarely (despite a recent example). Pilots have to get a type rating to fly a jet so any pilot who thinks they can't do that avoid a jet. So jet pilots are, on average, better. They've had more training, to higher standards, and passed a type rating check ride. If I was an aircraft manufacturer, the last thing I'd want to do is promote my aircraft as being so easy an idiot could fly them. That means idiots will, and they will determine the type's safety reputation. Mike C.
_________________ Email mikec (at) ciholas.com
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Post subject: Re: Single engine pressurized above FL 250 Posted: 25 Jan 2016, 01:29 |
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Joined: 11/03/08 Posts: 16904 Post Likes: +28714 Location: Peachtree City GA / Stoke-On-Trent UK
Aircraft: A33
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Username Protected wrote: For piston twins, generally true you have to feather. not only pistons. The last time I had an engine failure I remember sitting there watching it happen, I'd brought up power on the other engine, I knew which one had failed, but I sat there like a bump on a log and watched it (with the airplane climbing) for what seemed like an eternity thinking "criminey this autofeather is slow. Didn't I check it at the last stage check? I can't remember. What stage was that anyway" Finally it dawned on this numbskull "duh I'm in the 90 not the 200, I have to move a lever"
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Post subject: Re: Single engine pressurized above FL 250 Posted: 25 Jan 2016, 05:45 |
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Joined: 09/05/13 Posts: 125 Post Likes: +7
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Username Protected wrote: thinking "criminey this autofeather is slow" That's funny.  KW
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Post subject: Re: Single engine pressurized above FL 250 Posted: 25 Jan 2016, 10:35 |
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Joined: 12/03/14 Posts: 20758 Post Likes: +26247 Company: Ciholas, Inc Location: KEHR
Aircraft: C560V
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Username Protected wrote: It is not the initial training that is a barrier, it is the annual training requirements and the constant comments from other pilots about maintaining currency. You are not flying a jet without recurrent training. Thus, ME rating recurrency is a moot point. You are doing it anyways. Buying a single engine jet didn't get you out of anything. You need a type rating, you need recurrency training. Mike C.
_________________ Email mikec (at) ciholas.com
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Post subject: Re: Single engine pressurized above FL 250 Posted: 25 Jan 2016, 11:03 |
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Joined: 11/06/10 Posts: 12191 Post Likes: +3075 Company: Looking Location: Outside Boston, or some hotel somewhere
Aircraft: None
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Username Protected wrote: It is not the initial training that is a barrier, it is the annual training requirements and the constant comments from other pilots about maintaining currency. You are not flying a jet without recurrent training. Thus, ME rating recurrency is a moot point. You are doing it anyways. Buying a single engine jet didn't get you out of anything. You need a type rating, you need recurrency training. Mike C.
I agree. I was just commenting on the perception issue.
But one possible thing to consider, with a single engine, the emergency training syllabus is likely a lot shorter. This could collapse the annual training by a day or two. e.g. You do not need to test for single engine gradients, balanced field and many other items.
Tim
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Post subject: Re: Single engine pressurized above FL 250 Posted: 25 Jan 2016, 11:41 |
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Joined: 12/03/14 Posts: 20758 Post Likes: +26247 Company: Ciholas, Inc Location: KEHR
Aircraft: C560V
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Username Protected wrote: But one possible thing to consider, with a single engine, the emergency training syllabus is likely a lot shorter. This could collapse the annual training by a day or two. e.g. You do not need to test for single engine gradients, balanced field and many other items. I think that day or two will be needed to get piston pilots to be able to fly a 300 knot, pitch sensitive, tail wagging, jet up to ATP standards. Going to be some bruised egos and broken dreams in that process. Considering all the electronic related emergency procedures a TAA aircraft has, I don't think the emergency procedures section will be that much shorter. The Eclipse has over 200 pages of emergency procedures and very little of that comes from being a twin. A lot of comes from avionics and system related failures. AHRS failure, ADC failure, FADEC failure, and so on. As for single engine climb gradients, they do need to study that! And they need to study zero engine glides, too. As for balanced field, that is an interesting question on how the AFM is put together. Will the FAA require accel stop? Obviously there is no accel go, but there is no technical reason accel stop couldn't be required in the takeoff charts. Mike C.
_________________ Email mikec (at) ciholas.com
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Post subject: Re: Single engine pressurized above FL 250 Posted: 25 Jan 2016, 12:53 |
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Joined: 11/06/10 Posts: 12191 Post Likes: +3075 Company: Looking Location: Outside Boston, or some hotel somewhere
Aircraft: None
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Username Protected wrote: And they need to study zero engine glides, too.
Everyone does, so no change there. Look at something simple Cirrus did on the SR20 and SR22 which reduces pilot workload and for the vast majority of pilots does not have a material affect on the performance of the plane. They removed the prop control; it is determined by the throttle position. Now I am sure some of the best pilots can get a tiny margin more performance out of the plane at non-standard configurations, but that is the exception, not the rule. By removing this lever, Cirrus shortened training. Five minutes here, five minutes there... it all adds up. Tim
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Post subject: Re: Single engine pressurized above FL 250 Posted: 25 Jan 2016, 13:38 |
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Joined: 12/10/07 Posts: 8226 Post Likes: +7958 Location: New York, NY
Aircraft: Debonair C33A
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Username Protected wrote: Really? It seems lackluster to me. Looking at the longer flights (which presumably are nearer gross weight): http://flightaware.com/live/flight/N252 ... A/tracklogTook 21 minutes from 3,400 ft to FL270. Average rate 1123 FPM. http://flightaware.com/live/flight/N252 ... L/tracklogTook 19 minutes from 5,400 ft to FL250. Average rate 1031 FPM. http://flightaware.com/live/flight/N252 ... V/tracklogTook 16 minutes from 8,000 ft to FL280. Average rate 1250 FPM. http://flightaware.com/live/flight/N252 ... F/tracklogTook 28 minutes from 10,300 ft to FL280. Average rate 632 FPM. http://flightaware.com/live/flight/N252 ... H/tracklogTook 14 minutes from 11,000 ft to FL280. Average rate 1214 FPM. http://flightaware.com/live/flight/N252 ... H/tracklogTook 16 minutes from 12,500 ft to FL280. Average rate 969 FPM. Those were long flights with a reasonably unabated climb. The starting points were often well above the ground on the FA tracks, which pessimizes it a bit, and they are doing various tests. We don't know if these test were at gross weight, either. But still, you'd expect at least ONE flight with a good climb rate in the past 7 months, no? The published profile says: 20 minutes from 0 to FL280. Average rate 1400 FPM. Doesn't seem like they have demonstrated that with this particular example, and the profile is not particularly exciting, either. Best initial climb rate I saw was 1900 FPM and that was one of the shorter flights, so perhaps not at gross. Most were 1500-1800 FPM. For comparison, an Eclipse, which is the same weight, but with 100 pounds less total thrust, climbs at 3,424 FPM all engines (and nearly 1000 FPM one one!). If you normalize for thrust, the Eclipse climbs twice as fast. I knew the SEJ aerodynamics were bad, but I didn't think it was THAT bad. Mike C. Beautiful. It's SR-22 on steroids. Exactly what market needs. 
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Post subject: Re: Single engine pressurized above FL 250 Posted: 25 Jan 2016, 14:35 |
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Joined: 12/03/14 Posts: 20758 Post Likes: +26247 Company: Ciholas, Inc Location: KEHR
Aircraft: C560V
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Username Protected wrote: It's SR-22 on steroids. Those drugs don't seem very effective. Your pusher is watering them down. Mike C.
_________________ Email mikec (at) ciholas.com
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Post subject: Re: Single engine pressurized above FL 250 Posted: 25 Jan 2016, 14:46 |
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Joined: 12/03/14 Posts: 20758 Post Likes: +26247 Company: Ciholas, Inc Location: KEHR
Aircraft: C560V
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Username Protected wrote: CJ2/CJ3/CJ4 have rudder bias system that uses bleed air to keep rudder centered and when bleed air is lost from an engine it pushed the rudder automatically. Are there failure modes where the bleed air fails, but the engine runs? Like a valve closes, or a bleed air line comes off. Could be interesting if that happens. Pilot would get sudden yaw, but no engine discrepancy, so may end up confused as to what is going on. Mike C.
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Post subject: Re: Single engine pressurized above FL 250 Posted: 25 Jan 2016, 15:37 |
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Joined: 08/08/12 Posts: 1445 Post Likes: +940
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It probably has some sort of logic that knows if the loss of bleed air is from the engine or a valve failure. Then a check valve between the L&R would allow the bleed air to pass to both sides. I don't know for sure with the rudder bias, but typically, jets have a valve between the L&R systems in case of one source.
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Post subject: Re: Single engine pressurized above FL 250 Posted: 25 Jan 2016, 15:53 |
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Joined: 01/31/09 Posts: 5193 Post Likes: +3038 Location: Northern NJ
Aircraft: SR22;CJ2+;C510
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Username Protected wrote: CJ2/CJ3/CJ4 have rudder bias system that uses bleed air to keep rudder centered and when bleed air is lost from an engine it pushed the rudder automatically. Are there failure modes where the bleed air fails, but the engine runs? Like a valve closes, or a bleed air line comes off. Could be interesting if that happens. Pilot would get sudden yaw, but no engine discrepancy, so may end up confused as to what is going on. Mike C.
Not at all a big deal. You do a check of the rudder bias on the ground before every flight. Advance one throttle, feel the peddle move, back to idle, advance other throttle, feel peddle move, back to idle. So if the check is done the pilot should be familiar with how the rudder bias moves the rudder.
If you get uncommanded rudder movement then step on the peddle to maintain directional control, pull RUDDER BIAS CB to disable system.
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