Bankstown RNP RWY 11 approach on Garmin G1000
When carrying out the Bankstown RNP RWY 11C approach from the RAKSO IAF with a Garmin G1000 equipped aircraft while coupled to the autopilot, strange things happen. Fly over RAKSO at 3,700 feet and the Garmin unit doesn’t start descending to the 2,500’ SBKWI IF until there is a 3˚ approach angle. This would put the aircraft into the 2,500’ step.
In fact, if you look at the approach plate, it shows the descent should start at RAKSO from 3,700’, then go at a constant angle to WI at 2,500’. Once again, that means that the aircraft will clip the 2,500’ 20 DME Sydney Class C step. In effect, it means that the expensive and safer autopilot coupled system can not be used in this case. Does anyone have an answer to this as to why the Garmin approach doesn't actually follow what is required in practice? |
Dick,
The approach coding for that procedure does not have any coded vertical guidance prior to SBKWI. Any vertical advisory provided before this point is Garmin system derived, and not from coded data. Therefore the only vertical advisory the system can generate is based on a known final altitude......the only coded 'known' final altitude is the 2500ft at SBKWI and so it generates a path to this point. In this particular instance, because there is a break in the descent, the vertical advisory provided will not ensure you reach 2500ft by 6.5nm to SBKWI. Its a case of the navigation systems 'smarts' being smarter than the approach. It happens. Alpha |
I am sure that the Collins Pro Line in my CJ3 flew the approach correctly.
So why the problem with Garmin? |
Sounds like that particular approach may be coded wrong for that particular units database, it happens.
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If it's any consolation Dick, a 'modern' 747-8 would have the same problem with its new 'Integrated Approach Navigation' mode. We won't arm this mode for RNP/RNP-AR descent until all altitude constraints are complied with and we're approaching the FAF.
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That's why you have a pilot as the "master monitor" of the aircraft. It's why you're there mate.
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Have not flown G1000 in 9 years and unfamiliar with the approach, I’m just looking at the plate:
https://www.airservicesaustralia.com..._24MAR2022.pdf I’m not understanding why a 3 degree from Rakso to SBKWI would encroach the 2500’ shelf. That’s 20.3 miles and it should start descending approximately 3.7 miles out. |
My FMS would do the same. For obvious reasons, it tries to stay as high as it can. Since there is no limiting step on the chart at 6.5WI, the FMS will stay up until in needs to descend to reach 2500ft at WI. In fact, my FMS would probably go through RAKSO around 5000ft (and WB at around 3000ft, for that matter). Airspace steps are not in my database and the box knows nothing of them.
If this particular airspace config doesn't change, then an "at or below" step at 6.5WI would be in order. Whether that is an allowed design feature for an IAF>IF leg is another issue. And don't be naughty and edit the approach to put in a step. :oh: Or, "request a clearance to leave and re-enter"... (note note 4).
Originally Posted by Dick
In fact, if you look at the approach plate, it shows the descent should start at RAKSO from 3,700’, then go at a constant angle to WI at 2,500’.
Originally Posted by B2N2
I’m not understanding why a 3 degree from Rakso to SBKWI would encroach the 2500’ shelf. That’s 20.3 miles and it should start descending approximately 3.7 miles out.
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Just another thought, the approach plate has a SYD CTR frequency, they’re the ones clearing you for the approach.
The hard altitude is 2500’ that one should be respected by the G1000. Should be 4 ways to do this :
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Originally Posted by Dick Smith
(Post 11201136)
When carrying out the Bankstown RNP RWY 11C approach from the RAKSO IAF with a Garmin G1000 equipped aircraft while coupled to the autopilot, strange things happen. Fly over RAKSO at 3,700 feet and the Garmin unit doesn’t start descending to the 2,500’ SBKWI IF until there is a 3˚ approach angle. This would put the aircraft into the 2,500’ step.
In fact, if you look at the approach plate, it shows the descent should start at RAKSO from 3,700’, then go at a constant angle to WI at 2,500’. Once again, that means that the aircraft will clip the 2,500’ 20 DME Sydney Class C step. In effect, it means that the expensive and safer autopilot coupled system can not be used in this case. Does anyone have an answer to this as to why the Garmin approach doesn't actually follow what is required in practice? The initial segment from RAKSO to WI is actually from the Westmead Hospital RNP 052 chart, that charts has crossing WI at 2700 (it’s steeper at 3.07 degree). To fly the BWU approach at near 3 degree all the way, cross RAKSO at 6700 ft (13.3 nmx318 ft/nm +2500), cross 6.5 WI at 4600 (6.5x318+2500), that is the 2500 ft SY step, cross WI at 2500. |
The chart is a LNAV chart, i.e. 2D, there is no descent angle coded in database. What annunciation did you have on the HSI, LNAV or LNAV+V ? https://cimg9.ibsrv.net/gimg/pprune....4dcf77a7ed.png So back to Dicks issue. Each navigation manufacturer can tweak the procedure coding to optimise performance for that particular navigation system. The final version of coding for each system will differ and its why the Collins Proline and Garmin system each fly the procedure differently. You will also notice that the 2500ft altitude at SBKWI is an AT altitude, so this altitude will be honoured. How the aircraft gets there is up to each individual manufacturers navigation logic. Alpha |
Alpha, why would each equipment manufacturer elect to code the descent differently?
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Both systems would put the aircraft into the 2500' class C controlled airspace step if the pilot relies on the automation.
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I am sure that the Collins Pro Line in my CJ3 flew the approach correctly. |
Originally Posted by Dick Smith
(Post 11201682)
Both systems would put the aircraft into the 2500' class C controlled airspace step if the pilot relies on the automation.
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Originally Posted by alphacentauri
(Post 11201594)
There is actually SWH....see attached extract of procedure coding (my red circle is the vertical path angle for the final segment)..........this only goes back to the FAF. There is no coded vertical path prior to the FAF. (Note this is source coding....not final coding for a specific navigation system)
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I don't think its ever been automation's responsibility to keep an aircraft OCTA. Obviously, VNAV is capable of flying and meeting the level restrictions and forming/flying an approach path, but I believe it has always been the pilot's responsibility where if they haven't been cleared to enter and leave airspace ( or in this case via the RNP approach), to maintain separation from airspace.
I think in the case of this approach. Some aircraft ( potentially heavier, unfamiliar to the local environment aircraft such as private jets or potentially larger aircraft) it isn't efficient or safe to be descending early on that initial leg or the approach as whilst it does get you below the CTA step, it places you smack bang in the middle of the training area in particular with aircraft headed to the inbound reporting point TWRN. Therfore, it would be expected that in some scenarios, aircraft would be cleared to enter CTA via the RNP approach into BK and thus can fly the aircraft as depicted on the chart and negate CTA steps. If Garmin put an altitude restriction to get the aircraft OCTA by the step, aircraft that had been cleared to enter CTA would now descend OCTA if following that VNAV profile. I think at the end of the day, id imagine it wouldn't be feasible for there to be an option to select if the pilot had been cleared to enter CTA or remain OCTA, so therfore build the approach and code it as any other approach, and make the pilot responsible for remaining OCTA as they should . Practically, you would brief that you must descend from at or above 3700 to 2500 by 6.5nm WI. This essentially makes the RAKSO- WI leg 6.8nm ( as you need to be at 2500ft by 6.5nm WI) rather than the 13.3nm unrestricted leg. 6.8nm x 318ft ( 318ft per nm for a 3 degree descent path) = 2162ft. This means that to fly a 3 degree descent and be established at 2500ft by the step, you can cross RAKSO at 4662ft ( 2500ft+2162ft), rather than the published 3700ft. This enables you to stay higher longer and delay your initial top of descent from cruise by a few miles. If you indeed crossed RAKSO at 3700ft, you could level off and maintain 3700ft. 3700ft-2500ft= 1200ft to lose. 1200/318ft= 3.77nm. Therfore, your descent should begin at 10.27nm WI to fly a 3 degree descent from 3700ft to 2500ft and not clip the step at 6.5nm WI Obviously, you could also cross RAKSO at 3700ft and descent straight away to 2500ft. Whilst this is less complicated, you are flying longer at low altitude which is less efficient and also having more conflict with training area traffic. |
Tossbag, different manufacturers modify the coding in order for their specific navigation system to perform in a certain way for certain aircraft. For example its widely known that Boeing and Airbus navigation systems perform vertical path generation differently depending on the aircraft being flown. All whilst utilising the original coded data from Jeppesen. Even Garmin post process the Jeppesen data for different navigation systems.
SWH, that screenshot is from the Jeppesen database, granted its an older cycle so unless it have been taken off, which I am not aware it has been, then it is accurate. How are you viewing the coded data? The procedure doesn't have to be a VNAV procedure to have the vertical path angle in the coding, hence the lack of temperature limitations. Alpha |
Thankyou Alpha.
Boeing & Airbus "in order for their specific navigation system to perform in a certain way for certain aircraft" as in, due to the different aerodynamic properties of individual airframes? |
Tossbag, yes pretty much.
From my own experience it seems that Boeing aircraft systems seem to favour a 2.5-3 degree profile, whereas the Airbus logic is not quite as straight forward and in some cases goes towards a more dive and drive profile. This can vary based on weight, wind, and temperature. Its just the different logic used in the navigation systems. Garmin systems being more GA focused seem to also favour a 3 degree profile. The key thing to remember here is that the system is only as smart as the information it hold. In the Bankstown case for the RAKSO-SBKWI leg there are only 2 known points that being RAKSO or SBKWI (the 6.5nm fix and the airspace boundary are unknown to the system). So starting at 3700ft at RAKSO and wanting to be 2500ft at SBKWI presents some options.. a) I can give you a 3 degree descent from 3700ft @ RAKSO to 2500ft, or b) I can give you a 3 degree descent to 2500ft @ SBKWI from 3700ft, or c) I can plot a constant descent from 3700ft @ RAKSO to 2500ft SBKWI which would be 1.5deg (approx) These are pretty much the only coding options available......each nav system manufacturer may choose a different option....and each of them are valid for a specific system/aircraft. For example option a) may be suited Cessna 400 series piston aircraft allowing for deceleration. Option b) may be more suited to turboprop aircraft and option c) may be suited to jet aircraft. In all cases the start, end and minimum altitudes are honoured. I hope this helps explain it. Alpha |
"... and the airspace boundary are unknown to the system"
Wow. As usual, I've learned something new from you, Alpha. It's counterintuitive, as I've seen airspace boundaries on (TSO'd) GPS displays. Thanks. |
Tossbag, yes pretty much. From my own experience it seems that Boeing aircraft systems seem to favour a 2.5-3 degree profile, whereas the Airbus logic is not quite as straight forward and in some cases goes towards a more dive and drive profile. This can vary based on weight, wind, and temperature. Its just the different logic used in the navigation systems. Garmin systems being more GA focused seem to also favour a 3 degree profile. The key thing to remember here is that the system is only as smart as the information it hold. In the Bankstown case for the RAKSO-SBKWI leg there are only 2 known points that being RAKSO or SBKWI (the 6.5nm fix and the airspace boundary are unknown to the system). So starting at 3700ft at RAKSO and wanting to be 2500ft at SBKWI presents some options.. a) I can give you a 3 degree descent from 3700ft @ RAKSO to 2500ft, or b) I can give you a 3 degree descent to 2500ft @ SBKWI from 3700ft, or c) I can plot a constant descent from 3700ft @ RAKSO to 2500ft SBKWI which would be 1.5deg (approx) These are pretty much the only coding options available......each nav system manufacturer may choose a different option....and each of them are valid for a specific system/aircraft. For example option a) may be suited Cessna 400 series piston aircraft allowing for deceleration. Option b) may be more suited to turboprop aircraft and option c) may be suited to jet aircraft. In all cases the start, end and minimum altitudes are honoured. I hope this helps explain it. |
So if you are given the BK 11 LNAV approach by Sydney Terminal when you are OCTA approaching RAKSO does that allow you to enter and leave the class C airspace on descent to WI?
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Originally Posted by alphacentauri
(Post 11201705)
SWH, that screenshot is from the Jeppesen database, granted its an older cycle so unless it have been taken off, which I am not aware it has been, then it is accurate. How are you viewing the coded data? The procedure doesn't have to be a VNAV procedure to have the vertical path angle in the coding, hence the lack of temperature limitations.
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Originally Posted by Dick Smith
(Post 11201810)
So if you are given the BK 11 LNAV approach by Sydney Terminal when you are OCTA approaching RAKSO does that allow you to enter and leave the class C airspace on descent to WI?
I’m a little confused by this thread - I would never expect a G1000 or other system to keep me clear of controlled airspace - only to fly the approach appropriately (I.e to the manufacturers specs as alfacentauri explained). How can your FMC know what clearances you have or don’t have? UTR |
Only in Australia from my experience would an IFR aircraft on an IFR approach go in and out then in again of controlled airspace.
Once I flew the approach with a US trained pilot coming in from overhead Richmond. It was beyond comprehension to him that he was not cleared for the approach. I explained that we would actually be in uncontrolled airspace when the approach started and he was on his own. No descent clearance would be given. |
Only in Australia from my experience would an IFR aircraft on an IFR approach go in and out then in again to controlled airspace. So if you are given the BK 11 LNAV approach by Sydney Terminal when you are OCTA approaching RAKSO does that allow you to enter and leave the class C airspace on descent to WI? |
You can only ever have one IFR aircraft ( that hasnt reported visual) in the BK CTR at one time. My understanding is the APPCH permission from SY CEN is for sequencing into BK even though you are OCTA from SY airspace for the majority apart from the aformentioned segment of the IAF-IF leg, which without a clearance to enter ( different to approach permission), you must avoid.
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Lead Balloon,
To clarify, the airspace data and approach data are in separate parts of the database. They are unknown to each other, and so there are no smarts to compare approach path and airspace data….. Thats kind of the point of the prediction arc in large fms systems. It allows the pilot to know if an altitude is going to be reached by a certain point and adjust if required. |
You can only ever have one IFR aircraft ( that hasnt reported visual) in the BK CTR at one time. My understanding is the APPCH permission from SY CEN is for sequencing into BK even though you are OCTA from SY airspace for the majority apart from the aformentioned segment of the IAF-IF leg, which without a clearance to enter ( different to approach permission), you must avoid. |
Originally Posted by tossbag
(Post 11202161)
Just out of interest, is this 'procedure' published anywhere? ERSA, DAP's/Jepps?
I believe it is to do with ATC are required to seperate IFR from IFR in Class D. Under normal circumstances, most IFR aircraft when VMC prevails operate inbound via the VFR reporting points, and report visual with their inbound call, which enables ATC to employ visual separation to IFR aircraft as they are visual, which obviously cant be done in conditions less than VMC with aircraft on IAP's. Radar/ ADSB is only available for situational awareness to controllers in BK tower to my knowledge. The only quote that somewhat references it is in the ERSA " IFR Operations in VMC", " Pilots electing to terminate an IFR flight under the VFR should communicate itention to ensure their arrival is processed efficently " |
So what it looks like is a 'local procedure.' Unpublished, but IFR pilots are expected to understand and comply. Contributing to confusion and misunderstanding (as in Dick's question).
Great airspace system (sarcasm). |
tossbag, it's pretty simple really. You're IFR operating in Class D airspace so subject to a clearance to conduct the approach in D, and as you're required to be separated from other IFR aircraft in D you have exclusive use of the airspace until you've either landed or conducted a missed approach.
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Tossbag, Dick's question had nothing to do with your "local procedure". He asked about why his FMS didn't stop him clipping a CTA step in when in full auto. He was given the answer.
I see nothing "local" about being cleared for an approach. The fact that you start out OCTA and, because of the way you operate your aeroplane/FMS, you then clip a CTA step, sound like a personal problem. There is much nashing of teeth about hypotheses here. To go anywhere with this, we need to know exactly what ATC says. Obviously they won't "give" you the approach (your post #27). As for Just out of interest, is this 'procedure' published anywhere? ERSA, DAP's/Jepps? Perhaps a more-specific caution on the chart re the Sydney step might be in order. AVSEF it. |
I'm just wondering if a note is missing from the RNP chart, there is a star next to the @2500 limit at WI, which resembles the same star on the NDB RWY 11C chart which states you have to be 2500 by 17 DME SY. Although this procedure is horribly non aligned with rules concerning CTA as some of them seem to pass in and out of CTA steps. The marked descent line seems to infer all is ok as long as you are 2500 at WI. It would be interesting what a controller familiar with the area would expect an aircraft to do, ie remain clear of the 20 DME step or as long as you are 2500 by 17 DME SY no probs...
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tossbag, it's pretty simple really. You're IFR operating in Class D airspace so subject to a clearance to conduct the approach in D, and as you're required to be separated from other IFR aircraft in D you have exclusive use of the airspace until you've either landed or conducted a missed approach. |
Captain Bloggs, you'll note in my previous posts I was asking questions to understand what is being said by ATC. You obviously have someone sitting beside you to help clear up any confusion, sit in the cockpit by yourself in IMC and manage the workload of this procedure and see how you go. Personal problem? No, Dick is confused by whether he has a clearance to clip, the last thing you need when SP-IFRing in IMC is to be chipped by ATC for busting CTA.
I think you need to calm down a little, look at the broader implications of what is being discussed. |
I say again:
To go anywhere with this, we need to know exactly what ATC says. |
Garmin navigators will provide vertical guidance on almost every approach in the database. On LNAV approaches it will give you LNAV+V where the the +V refers to a pseudo glide path that is a mathematically derived 3 deg slope. This is very handy but care must be taken because it will not account for any mandatory crossing altitudes.
One gotcha with GARMIN systems is that the system switches from terminal mode to approach mode (ie LPV, LNAV/VNAV or LNAV) when the active leg is the leg to the FAF. If there is a fix between the IAF and the FAF it will not sequence to approach mode until after that waypoint which means there will be no glide path until after you pass the waypoint at which point you will be above the glide path. The work around is to activate vectors to final after you pass the IAF which will cause the FAF to be the active to waypoint. |
The work around is to activate vectors to final after you pass the IAF which will cause the FAF to be the active to waypoint. |
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