The modified Navions (the original ones only had two flap positions: full up and full down), suggest half flaps (about 17 degrees) for short fields.IIRC....the POH for both the Bonanza and the PA-32 call for +20 deg flaps for short field ops.
The modified Navions (the original ones only had two flap positions: full up and full down), suggest half flaps (about 17 degrees) for short fields.IIRC....the POH for both the Bonanza and the PA-32 call for +20 deg flaps for short field ops.
You can takeoff with full flaps in the Navion as well. The ground roll is extremely short but you won't climb worth crap, so unless you have a 200' runway with no obstacles for miles, it's not a particularly good technique (don't ask me how I know this).
Some Skyhawk manuals call for 10degrees on short fields and some call for zero. Analysis shows that while 10 degrees shortens the ground run, it doesn't really decrease the distance to clearing a 50' obstacle. If you have an older 172, you can get the best of both by starting your takeoff run with no flaps, pulling in ten as you rotate, and then getting them out once you get near Vx.
Seriously? The shorter the runway the more reasons to be using 40 degrees.
I teach 40 degrees (or whatever maximum flaps are for the airplane), all the time, regardless of the winds, touch and go, or full stop.
The only reason my students would use less than 40 degrees would be to show them why the hell they should be using 40 and to know how the airplane will handle if they had equipment failures.
The majority of flight instructors would most definitely not agree with what your instructor taught you.
2999 ft is by no means short for a 172...not even close...like double what you'd need in most cases.
None of those 172s have 40 degrees. There are a great many cases where 40 (or 30) will just make things more difficult, high OAT/high elevation/@ gross/windshears/etc, or any combination of them come to mind.
My 150B had manual 40, I loved that setup. I flew a lot of rides with some big passengers on hot windy days, I would come in high enough to drag 40 and make shallow S-turns at idle. Easy way to make your non-flying friends turn green.
You mean that Cessna called it 40deg, but it really wasn't 40deg?
Some folks like using full flaps and lot of power on final.
I lean more towards flying final closer to idle and using full flaps only when needed.
I was taught to do TNG's with 20deg, then when you do the go part, simultaneously push in the throttle with your hand and push in the carb heat with your thumb, then climb out and once you have some altitude and cleared the obstacles, flaps all the way to 0.
I think it's nuts to do a touch in go with 40 deg of flaps, especially at the 2999' rwy I practice at.
As mentioned you will get a difference of opinions on this, Apparently I am not one of the "majority of instructors", I personally prefer 20 degrees or less of flaps for TNG's and normal landings. Especially with new students. One reason is that it makes Go arounds much easier just because you don't have to immediately reset the flaps.
It has been a while but I did some figures that once showed the stopping difference between 20 and 40 degrees of flaps was less than 100 feet difference IIRC. Just look at the difference in stall speeds it is only a few kts.
It would be interesting to do some testing to see if a TNG approach with 40degrees or 20degrees results in a shorter distance to clear a 50ft obstacle. Probably to many variables to really give a definitive answer, things like what speed do you slow down to and when do you change flap settings.
I also find that many 172's with 2 people are near the forward CG limit and landing full flaps power off it is difficult to touch down on the main gear 1st.
Many pilots compensate for this by landing with power on, which kind of defeats the purpose of landing with full flaps, especially when landing with 20 degrees power off will likely get you stopped sooner and it is much easier to touch down on the main gear.
Brian
CFIIG/ASEL
please clap...yup....low energy is a bad thing.
That sounds about right, and a increase in pitch when you decrease flaps might be required.
Yup....and folks we'll be here all week....and don't forget to tip the wait staff.please clap...
Two of our 172s have 40 degrees...80725 & 73477 (M models). The N model, 734PG, does not. Regardless of if we're flying a M or N I teach to default to full flaps. I've landed them full flaps with the wind gusting over 50 knots more than once.None of those 172s have 40 degrees. There are a great many cases where 40 (or even 30) will just make things more difficult, high OAT/high elevation/@ gross/windshears/etc, or any combination of them come to mind.
Pretty much the same policy the FAA espouses. Full flaps, all the time.
Nonsense. It is substantially easier to land a 172 on the main gear first with full flaps than clean. If someone can't, they aren't flaring, and are probably combining that with a fast approach speed. In a 172 loaded to max, it's 61 knots. Not 65, and definitely not 70. That's not a problem with flaps, it's a problem with technique. Same thing with landing a 182 on the nosegear. They aren't "nose heavy," the pilots are lazy in the flare; there is plenty of elevator authority to do it, even at slow speeds with the power idle. And two big guys up front in a 172 puts you real close to the forward CG limit. I did almost all my instrument training that way.
You also misunderstand what landing with power means if you think it affects stopping distance. Once the gear is on the ground, the power goes to idle, every time. You can get quite short landing rolls that way, especially if you approach behind the power curve.
There are quite a few different models of 172's newer ones land full flaps on the mains better than older ones. Many older ones at forward CG, power off, full flap, will only touch down about 3 point with yoke against the stop. I have put 50lbs in the baggage compartment of some when practicing short field approachs, for this reason.
My view on flaps comes from flying everything from cubs and champs with no flaps to gliders with 90 degree flaps. As a CFI and glider pilot I practice simulated power failure approaches and actual off field landings probably more than most pilots. I view flaps as a tool that can be used, to control the approach, not just an on/off selection for minimum touch down speed.
But I also teach to practice all kinds of approaches and decided for yourself what kind of approach and configuration you and the specific airplane you are flying works best for your normal landings. If full flap power on approaches work best for you then great. I just prefer partial flap power off approaches (kind of a requirement in my glider(no spoilers)). This is a middle of the envelope approach. But when I get in a new airplane I will practice different approaches to find out what I like for that airplane. I can't say I blanket teach any specific configuration because it changes from airplane to airplane.
I just looked and the C172N 2300GW 40 degree flaps, landing distance is shown as 520ft Ground Roll, 1250ft over 50ft obstacle
The C172P 2400GW 30 degree flaps, landing distance shown as 540ft Ground Roll, 1280ft over 50 ft obstacle.
So per the Cessna manuals, add a 100lbs and reducing the flaps from 40 to 30, increased the ground roll 20ft and the 50ft obstacle landing 30 feet.
Brian
CFIIG/ASEL
Same thing with landing a 182 on the nosegear. They aren't "nose heavy," the pilots are lazy
It is substantially easier to land a 172 on the main gear first with full flaps than clean.
You have not flown many 182s. Some will still want to touch nose first with the elevator against the upstop.
I've flown N, P, Q, R and T models. Is that enough?
You have not flown many 182s. Some will still want to touch nose first with the elevator against the upstop.
If you stall an airplane in level flight with full flaps versus zero flaps, will the nose be higher, lower, or the same?
Is the nose higher or lower on a full-flap approach versus a zero-flap approach? Which one requires more pitch change during the flare?
And add 1, because the first 172 was just a 172 (with no model letter). The 172A was the second mode.How many letters are in the alphabet between A and N?
You're certainly free to have a different opinion - and free to teach it however you'd like once you get your CFI. I've said my perspective and what I teach when I have full control over a pilot's training from day one. It's based on four digit hours worth of sitting in the right seat and preventing new pilots and old pilots from crashing their airplanes when they land them. I have pairs of shoes that have more landings in Cessna's than most any private pilot will accomplish in their entire life, and I say that not because that means anything in itself. It's just a fact and evidence that I'm not just pulling this advice out of my ass. It works.It great how accident investigators can lump all accidents into one group and determine without a doubt that one thing would have prevented it lol, "if only they had less energy prior to crashing!"
https://www.faa.gov/news/safety_briefing/2010/media/MarApr2010-FlyingByTheNumbers.pdf
This says pretty much use whatever gets the job done, which seems reasonable to me in a small airplane. I don't want max drag in nasty conditions, I want to be able to initiate a go-around without max drag, hopefully escaping whatever sinking air / tail shear I might have flown into on final. It probably sounds like I've scared the crap out of myself once and you WOULD BE RIGHT! Max flaps with a heavy load on a hot day and flown into sinking air and full power doesn't arrest the decent, that's NOT COOL.
Arguing that touching down slower is gonna exponentially increase safety seems like a stretch when the stall speed with & without flaps a whopping 7 knots different. If you're way over on energy that causes an accident using full flaps probably wouldn't have changed it.
Arguing that touching down slower is gonna exponentially increase safety seems like a stretch when the stall speed with & without flaps a whopping 7 knots different. If you're way over on energy that causes an accident using full flaps probably wouldn't have changed it.
The drag effect of the flaps doesn't stop after the touchdown and the accident doesn't usually happen at touchdown, but later. 7 knots difference in stall speed but a large difference in drag AFTER touchdown. The real problem is arguing stall speed and not overall deceleration.
Stall speed is almost a meaningless number once the wheels are on the ground other than as a reference as to what speed one SHOULD have touched down at. It's too late at that point. Now the question is, will you get it stopped before it's in the ditch? You've already transitioned from a flying machine to a very poor efficiency go kart.
Jeez, this is full of misdirection.
To land mains first, you need the nose above the horizon with the stall warning sounding. And that's it. You lift it higher, and you still land on the mains first, just with the tail a bit closer to the ground.
Many older ones at forward CG, power off, full flap, will only touch down about 3 point with yoke against the stop.
Brian
CFIIG/ASEL
Overall, as an instructor, you pick and choose your battles. If I have control over a pilot from day one (zero hour to private) they're going to be using full flaps all the time by default. We certainly do landings with different flap settings.
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Now we should discuss if braking works better with full flaps or no flaps and does braking decelerate the airplane faster than flaps
Quite easily.It's not misdirection.
Point 1. Full flaps lead to a lower pitch attitude during approach (you acknowledged this in your "can't see the runway without flaps" comment). This means more pitch change is required to flare.
Point 2. You can raise the nose more without stalling without flaps.
I conclude it is easier to land nose-high (on the mains) without flaps. Explain how you have drawn the opposite conclusion.
Nonsense, and I've taught in those old 172s. Never had that problem.
those limits aren't checked every year?.....during the annual inspection?Those old 172s, like most older airplanes, are often way out of rig. Too much control surface travel, too little, rudder rigged off-center, ailerons out of sync, and so on. A lot of pilots get strong impressions from the airplanes they fly, and if the elevator's up-stop was set for three or four degrees too little up-travel, he'd think that these old 172s don't have enough elevator authority.