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RV7 Mosaic eligibility

mr.sun

Well Known Member
Because my 20 year old RV7 stalls at 58 knots, will a light sport pilot be able to fly it under the new rules?
 
Because my 20 year old RV7 stalls at 58 knots, will a light sport pilot be able to fly it under the new rules?
Be sure to read carefully. New rule is for Vs1 (no flaps) and is in CAS (usually higher than IAS at low speeds).
 
I fly a 6A so I’m interested in MOSAIC. I went to the Vans website and it shows 55 MPH for the 6 And 58MPH for the 7. Well below 61KTS CAS in MOSAIC. What am I missing?
 
I fly a 6A so I’m interested in MOSAIC. I went to the Vans website and it shows 55 MPH for the 6 And 58MPH for the 7. Well below 61KTS CAS in MOSAIC. What am I missing?
You're missing the fact that 61 knots VS0 is the max stall speed for whether an airplane could be certified as an S-LSA/E-LSA. The max stall speed for whether a Sport Pilot can fly it is 59 knots VS1 (which, unfortunately, is quite a bit slower). Does Van's publish VS1 speeds for the -6 and -7?
 
You're missing the fact that 61 knots VS0 is the max stall speed for whether an airplane could be certified as an S-LSA/E-LSA. The max stall speed for whether a Sport Pilot can fly it is 59 knots VS1 (which, unfortunately, is quite a bit slower). Does Van's publish VS1 speeds for the -6 and -7?
You're missing the fact that 61 knots VS0 is the max stall speed for whether an airplane could be certified as an S-LSA/E-LSA. The max stall speed for whether a Sport Pilot can fly it is 59 knots VS1 (which, unfortunately, is quite a bit slower). Does Van's publish VS1 speeds for the -6 and -7?
OK, so it’s 66.6MPH for a light sport pilot. Vans shows different stall speeds for different weights (and based on my experience VSO). Who makes the determination of VS1?
Edit; After doing the deep dive into 717 pages and reading Vans comments and the FAA logic that hopefully the 6 and 7 should fall just within the limits. Anyone from Vans on the list care to comment?
Thanks
 
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Sean Duffy is United States secretary of transportation, he oversees the FAA and the FAA administrator.
Impressive that he did the announcement...
 
Final rule is max 59 KCAS S1 for sport pilots. The FAA comments explicitly address how you determine the CAS stall speed for your RV-7 and any other EAB cert aircraft.

Page 236: "FAA maintains published guidance with FAA-accepted methods for determining and documenting the VS1 CAS for an airplane in AC 90-89C, Amateur-Built Aircraft and Ultralight Flight Testing Handbook, including a method to determine CAS by conducting test flights."

What VAN's says is not necessarily your CAS or relevant - per the FAA, EAB must determine on a plane by plane basis per AC 90-89C accepted methods.
 
My -6 stalls at 52kts clean.
At what weight? Most likely the requirement is at your gross weight all though I have not seen that written anywhere. Those that have registered their -6 at 1800 lbs will have a higher Vs1 than those that use the Vans 1650 lbs.
Also is that IAS or CAS? Do you have an indicated to calibrated correction?
As stated by talon167 above on how YOUR Vs1 is to be determined, some people may need to go back and do some flight testing.
 
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At what weight? Most likely the requirement is at your gross weight all though I have not seen that written anywhere. Those that have registered their -6 at 1800 lbs will have a higher Vs1 than those that use the Vans 1650 lbs.
Also is that IAS or CAS? Do you have an indicated to calibrated correction?
As stated by talon167 above on how YOUR Vs1 is to be determined, some people may need to go back and do some flight testing.
Unless otherwise noted, all performance numbers are considered to be @ gross weight.
 
At what weight? Most likely the requirement is at your gross weight all though I have not seen that written anywhere. Those that have registered their -6 at 1800 lbs will have a higher Vs1 than those that use the Vans 1650 lbs.
Also is that IAS or CAS? Do you have an indicated to calibrated correction?
As stated by talon167 above on how YOUR Vs1 is to be determined, some people may need to go back and do some flight testing.
1650 gross. Pretty much all RV's minus maybe 10 and 14 will now fit into the new requirements. Also keep in mind, they state 59 CAS. IAS and CAS are not always the same thing. Food for thought
 
Anyone gone up yet to test your CAS per the guidelines and what it comes in at?

I found that my IAS is accurate to within +/-1 knot over the range from 80 to 140 KIAS. GAP 26 pitot and Cleaveland static ports.

However, I didn't test mine at high angles of attack such as you'd see at the stall - not clear how you do that accurately without an air data boom.
 
Unless otherwise noted, all performance numbers are considered to be @ gross weight.
AND most adverse CG location, typically the forward CG limit.

Theoretically, you could have a more complex edge case where you have a lower MGTOW at the forward CG limit, but I don’t think that is the case here.
 
What data will the FAA use in assessing whether or not your particular RV meets the new Vs1 requirement to be flown under Sport Pilot rules? Where will they get that information? Like…in the unlikely event of a ramp check?
 
What data will the FAA use in assessing whether or not your particular RV meets the new Vs1 requirement to be flown under Sport Pilot rules? Where will they get that information? Like…in the unlikely event of a ramp check?
I think the EAB, all the test information is logged in the airplane book. Just like the stall number a builder has to log and signed in the log to certify it was tested with a specific weight.
 
CAFE Foundation testing of RV 8 yielded a clean stall at 1788 lbs to be 52.4 kcas. Perhaps the same info exists for the RV 7
 
What data will the FAA use in assessing whether or not your particular RV meets the new Vs1 requirement to be flown under Sport Pilot rules? Where will they get that information? Like…in the unlikely event of a ramp check
This language is on page 236 of the "rule"

If the aircraft’s manual does not have a published VS1, FAA maintains published guidance with FAA-accepted methods for determining and documenting the VS1 CAS for an airplane in AC 90-89C, Amateur-Built Aircraft and Ultralight Flight Testing Handbook, including a method to determine CAS by conducting flight tests.

So, perhaps a log entry stating the stall speed as determined in accordance with the Advisory Circular?
 
This language is on page 236 of the "rule"

If the aircraft’s manual does not have a published VS1, FAA maintains published guidance with FAA-accepted methods for determining and documenting the VS1 CAS for an airplane in AC 90-89C, Amateur-Built Aircraft and Ultralight Flight Testing Handbook, including a method to determine CAS by conducting flight tests.

So, perhaps a log entry stating the stall speed as determined in accordance with the Advisory Circular?
Hmmm...OK. I guess if the time ever comes when I need to fly under Sport Pilot, and in the unlikely event anyone asks me for proof of Vs1, I'll just use what the original builder published in the POH. My suspicion is that that FAA Enforcement Agent will just see that it's an RV-9A and assume that it's fine. I am curious now though...I'll have to rummage around in the logbook and construction documents and see if he documented that stuff.
 
I would guess/hope, that once the rule is published in the federal register, a list of airplanes will be listed that fall under the new rule, either by the kit manufacturer or the FAA. I'm sure all the kit manufacturers were involved in the petitioning for that VS1 number to make sure their product is within the scope.
 
I would guess/hope, that once the rule is published in the federal register, a list of airplanes will be listed that fall under the new rule, either by the kit manufacturer or the FAA. I'm sure all the kit manufacturers were involved in the petitioning for that VS1 number to make sure their product is within the scope.
Rule was published well over a week ago -fyi
 
I would guess/hope, that once the rule is published in the federal register, a list of airplanes will be listed that fall under the new rule, either by the kit manufacturer or the FAA. I'm sure all the kit manufacturers were involved in the petitioning for that VS1 number to make sure their product is within the scope.
That, of courser, was the crux of my question. Not a hard question to answer for a type-certified airplane...they lend themselves to consistent cataloguing. E-AB's.....not so much.
 
Rule was published well over a week ago -fyi


Edit: The rule was published but does not go into effect for 90 days.

Key dates and effective timelines

EventDate
Final rule submitted to Federal RegisterJuly 18, 2025 (FAA signature date)In Flight USA+1
Final rule published in Federal RegisterJuly 24, 2025RedditGovInfo
Rule becomes effectiveOctober 22, 2025 (90 days after publication)GovInfo
Some amendatory provisions effective laterJuly 24, 2026 (365 days after publication)GovInfo
 
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That, of courser, was the crux of my question. Not a hard question to answer for a type-certified airplane...they lend themselves to consistent cataloguing. E-AB's.....not so much.
Wouldn't you think that the Van's brand would lend itself to grouping most under < 59kts VS1? How would the FAA ever police a ramp check?
 
Wouldn't you think that the Van's brand would lend itself to grouping most under < 59kts VS1? How would the FAA ever police a ramp check?
Heh...if I knew the answer to either question I wouldn't have asked. Will they just assume that Van's design specs are accurate and rigorously adhered to in the build, or will they have to address the vivid imagination and wide variability that happens in the home-built world.

(it's a rhetorical question. I don't expect that anyone knows the actual answer, although I posted it out of curiosity hoping someone would)
 
Wouldn't you think that the Van's brand would lend itself to grouping most under < 59kts VS1? How would the FAA ever police a ramp check?
I wondered about that too.
There's nothing in the ARROW docs that specifies an airplane is compliant with the <59 kts VS1 rule.

How would an FAA Inspector know the "Boogie Woogie 12345" is compliant?
Or a Vans RV7A?

Maybe I'm missing something.
Doesn't effect me now, but someday it may.
 
Heh...if I knew the answer to either question I wouldn't have asked. Will they just assume that Van's design specs are accurate and rigorously adhered to in the build, or will they have to address the vivid imagination and wide variability that happens in the home-built world.

(it's a rhetorical question. I don't expect that anyone knows the actual answer, although I posted it out of curiosity hoping someone would)
I suspect we will see further guidance on this from the faa, as there is no requirement for specifying Vs1 on eab. The builder must log the tested Vs0 speed in the logbook, along with Vx and Vy. Beyond that, there is no official speed. I can’t see how the faa can accept the kit makers numbers, as they are not the manufacturer of the plane and there is absolutely no guarantee that any given plane will match that speed, given the freedoms afforded to builders. The easy answer is for the faa to do a kit level approval, but really struggle to think they would do that.

I suspect that in order to be eligible to fly an eab under these new rules, the faa will require that a airframe log entry be made defining Vs1. They will likely also point to an faa doc, dictating how the test is to be performed. Pretty sure they have a procedure for determining cas stall speeds in a current eab testing guide.

As written, it is almost unenforceable as there is no real way for a sport pilot to determine Vs1 on any eab other than a poh or markings on the indicator, neither of which is required to exist and if they do the numbers are all but guaranteed to be in ias.

Just my speculation here.
 
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I suspect that in order to be eligible to fly an eab under these new rules, the faa will require that a airframe log entry be made defining Vs1. They will likely also point to an faa doc, dictating how the test is to be performed. Pretty sure they have a procedure for determining cas stall speeds in a current eab testing guide.
I hope not.

This is fundamentally not a new issue. The exact speed threshold is changing, but for the past 21 years, sport pilots have been able to fly E-ABs as long as they meet various requirements including some airspeeds in CAS (and other things). There's no existing requirement for a log entry in that case, and I don't see why we would need one now.
 
There's nothing in the ARROW docs that specifies an airplane is compliant with the <59 kts VS1 rule.

How would an FAA Inspector know the "Boogie Woogie 12345" is compliant?
Or a Vans RV7A?
I suspect that in order to be eligible to fly an eab under these new rules, the faa will require that a airframe log entry be made defining Vs1. []

As written, it is almost unenforceable as there is no real way for a sport pilot to determine Vs1 on any eab other than a poh or markings on the indicator, neither of which is required to exist and if they do the numbers are all but guaranteed to be in ias.
59 KCAS VS1 is a pilot limitation, not an aircraft limitation. The question is not, "is this aircraft legal to fly?", but rather, "can you legally fly this aircraft?" The FAA should not, and I hope would not, add a requirement for aircraft (log book entry for VS1) based on a pilot limitation. This is no different from a perfectly airworthy tailwheel airplane being approached by a pilot without a tailwheel endorsement: plane is legal, pilot can't fly it.

The O in ARROW, or AROW is short hand, not the full requirement; that's 91.9:1754568218601.png
So, what flight manual, operating limitations, manual material, markings, or placards do you have for this aircraft that show you, as a sport pilot or a private pilot without a medical/BasicMed, are legal to fly it? If there's nothing available that documents VS1<= 59 KCAS then you're in violation and shouldn't be flying the aircraft, regardless of how closely the FAA is watching; that's how we as a community get a bad reputation, heavier enforcement and, maybe, privileges revoked. Poor (speeds only in indicated) or non-existent documentation on the aircraft side isn't permission to ignore the rule.

They will likely also point to an faa doc, dictating how the test is to be performed. Pretty sure they have a procedure for determining cas stall speeds in a current eab testing guide.
AC 23-8C, Flight Test Guide for Certification of Part 23 Airplanes, is quite descriptive on testing stall speeds, see the sections on 23.49 and 23.201. The EAB testing AC 90-89C is much less descriptive.
 
59 KCAS VS1 is a pilot limitation, not an aircraft limitation. The question is not, "is this aircraft legal to fly?", but rather, "can you legally fly this aircraft?" The FAA should not, and I hope would not, add a requirement for aircraft (log book entry for VS1) based on a pilot limitation. This is no different from a perfectly airworthy tailwheel airplane being approached by a pilot without a tailwheel endorsement: plane is legal, pilot can't fly it.

The O in ARROW, or AROW is short hand, not the full requirement; that's 91.9:View attachment 94386
So, what flight manual, operating limitations, manual material, markings, or placards do you have for this aircraft that show you, as a sport pilot or a private pilot without a medical/BasicMed, are legal to fly it? If there's nothing available that documents VS1<= 59 KCAS then you're in violation and shouldn't be flying the aircraft, regardless of how closely the FAA is watching; that's how we as a community get a bad reputation, heavier enforcement and, maybe, privileges revoked. Poor (speeds only in indicated) or non-existent documentation on the aircraft side isn't permission to ignore the rule.


AC 23-8C, Flight Test Guide for Certification of Part 23 Airplanes, is quite descriptive on testing stall speeds, see the sections on 23.49 and 23.201. The EAB testing AC 90-89C is much less descriptive.
The mosaic rules open things up for sport pilots allowing more EAB class planes.

Under these new rules, sport pilots will need to understand the Vs1stall speed of the EAB class airplanes that they were not previously allowed to fly in order to legally fly them. The rule seems clear that the aircrafts stall speed is a limitation for excersing priveleges.

Plane has tailwheel, cannot fly. Plane stalls over 59, cannot fly. Difference is that the tailwheel is obvious and the stall speed is not.

It remains unclear how they're going to be able to do that given that these speeds are typically not documented in EAB airplanes. The O in ARROW refers to operating handbooks, however EAB aircraft are not required to have these.

I certainly do not have the answers and did not mean to imply that I do. I was just providing some speculation in response to a question that seems relevant - "How does a sport pilot know the Vs1 of an EAB class aircraft he wants to fly, such that it is legal?" The answer cannot be to look in the POH, as these are often not available.
 
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I hope not.

This is fundamentally not a new issue. The exact speed threshold is changing, but for the past 21 years, sport pilots have been able to fly E-ABs as long as they meet various requirements including some airspeeds in CAS (and other things). There's no existing requirement for a log entry in that case, and I don't see why we would need one now.
I suppose if it has been done this way for a long time, it may not be an issue. But it does raise the question as to the legality if speeds are not well documented. It seems to me that this rule leaves a lot of room for interpretation given that most EABs have no requirements for specifying Vs1. Without knowing how the FAA will interpret this leaves a risk for sport pilots IMHO. I was just speculating on how the FAA might respond to this ambiguity. The new rule opens things up pretty wide now, so expect flying EABs under this rule will greatly increase. At some point, one of these folks is going to get ramp checked.
 
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Plane has tailwheel, cannot fly. Plane stalls over 59, cannot fly. Difference is that the tailwheel is obvious and the stall speed is not.
Something less obvious then: flying a 210 HP aircraft without a high performance endorsement. A lot of EABs don't fully document their engine model, much less how much power it makes and you can't tell from the outside what that RV-7's got under the cowl.
But it does raise the question as to the legality if speeds are not well documented. It seems to me that this rule leaves a lot of room for interpretation given that most EABs have no requirements for specifying Vs1.
I think the legality is very clear. If the answer to the question "What's the VS1, in KCAS, of this aircraft?" is "dunno" rather than a number less than or equal to 59, then it can't be flown by a sport pilot; VS1=? is no different than VS1=60 KCAS. Not only that, but because the rule is "since it's original certification", the documentation needs to exist since birth that the aircraft didn't have a non-compliant stall speed and then was subsequently modified to lower it, or vice-versa.

At the end of the day, if a pilot's answer to the question "How do you know you can legally operate this aircraft?" is, effectively, "I didn't know that I couldn't" then they're probably not going to have a good time if/when the FAA decides to start asking questions.
 
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