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MH370 Flying In The Clouds

Authors:

Abstract and Figures

Aircraft are well known to leave contrails at high altitude, or “holes” in thick billowing lower-level clouds from hot exhaust turbulence and cooling of air over the wings. These can last for several hours. The day MH370 disappeared was a very cloudy day, especially during its final descent phase. The ocean had to be surveyed (at least that is what I thought) before reaching the landing site, so it’s reasonable to assume that it punched through the clouds near the 7th arc; a point at which it was in a proven, controlled but steep descent for the landing phase. Is it possible to verify that it did punch through the clouds? As a precautionary study, I investigated the Terra/MODIS cloud data and found not just a hole, but very surprisingly, an apparent trail of cloud anomalies in the Corrected Reflectance (True Color) image. Despite 2 hours and 48 minutes elapsing since the 7th-arc descent, the cloud imprint was obvious and consistent with what I expected to find from MH370 flying within the clouds. In retrospect, it was an obvious tactic to avoid detection and to minimize time to the landing location. An overlay of the “Cloud Top Height” data showed a very remarkable, unmistakable, and isolated trail of very anomalous height-fluctuations from 4 km (general height) to over 10 km (very abnormal height), associated (in an unknown way) with the trail punching through the clouds intermittently and leaving imprints within the clouds and an apparent signature above. The distance from source (at the event time), directions, wind speed/direction, and length of anomaly-trail, are all very consistent and plausible with the trail being made from the 7th-arc. This trail ends precisely very near the final destination at the Penang Longitude Deep Hole. The observed average north-eastward cloud drift speed of about 104 km/hr also matches a theoretically predicted wind-profile drift speed of ~96 km/hr. Nearly 7 hours later, the trail was still obvious in 3 additional images from two satellites. This trail was apparent in both the Reflectance and Cloud Top Pressure data. I conclude that from the 7th arc, MH370 was flying within the clouds and punching through it occasionally and leaving a distinct trail along its final descent to its precise planned landing site. This observation, if correct, is a second direct confirmation of MH370’s path, added to the previous direct confirmation of a MODIS-satellite-observed debris trail from the landing site (another deceived algorithm).
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MH370 Flying In The Clouds
Vincent Lyne 1*
1 Retired Scientist
Hobart. Tasmania. Australia
* Correspondence: Vincent.lyne@utas.edu.au
Abstract
Aircraft are well known to leave contrails at high altitude, or “holes” in thick billowing lower-
level clouds from hot exhaust turbulence and cooling of air over the wings. These can last for
several hours. The day MH370 disappeared was a very cloudy day, especially during its final
descent phase. The ocean had to be surveyed (at least that is what I thought) before reaching
the landing site, so it’s reasonable to assume that it punched through the clouds near the 7th arc;
a point at which it was in a proven, controlled but steep descent for the landing phase. Is it
possible to verify that it did punch through the clouds? As a precautionary study, I investigated
the Terra/MODIS cloud data and found not just a hole, but very surprisingly, an apparent trail
of cloud anomalies in the Corrected Reflectance (True Color) image. Despite 2 hours and 48
minutes elapsing since the 7th-arc descent, the cloud imprint was obvious and consistent with
what I expected to find from MH370 flying within the clouds. In retrospect, it was an obvious
tactic to avoid detection and to minimize time to the landing location. An overlay of the “Cloud
Top Heightdata showed a very remarkable, unmistakable, and isolated trail of very anomalous
height-fluctuations from 4 km (general height) to over 10 km (very abnormal height),
associated (in an unknown way) with the trail punching through the clouds intermittently and
leaving imprints within the clouds and an apparent signature above. The distance from source
(at the event time), directions, wind speed/direction, and length of anomaly-trail, are all very
consistent and plausible with the trail being made from the 7th-arc. This trail ends precisely
very near the final destination at the Penang Longitude Deep Hole. The observed average north-
eastward cloud drift speed of about 104 km/hr also matches a theoretically predicted wind-
profile drift-speed of ~96 km/hr. Nearly 7 hours later, the trail was still obvious in 3 additional
images from two satellites. This trail was apparent in both the Reflectance and Cloud Top
Pressure data. I conclude that from the 7th arc, MH370 was flying within the clouds and
punching through it occasionally and leaving a distinct trail along its final descent to its precise
planned landing site. This observation, if correct, is a second direct confirmation of MH370’s
path, added to the previous direct confirmation of a MODIS-satellite-observed debris trail from
the landing site (another deceived algorithm).
Keywords: Contrails; MH370; Cloud Trails; Cloud Anomalies
1. Introduction
Malaysian Airlines MH370, a Boeing 777-200ER went missing on the 8th of March 2014 with
239 people on board (ATSB, 2017). Officially, the aircraft was flying southerly with all
onboard hypoxic, including the pilots. The aircraft then supposedly ran out of fuel and
underwent a gravitationally-accelerated dive resulting in a catastrophic high-speed crash with
flaps and flaperon fluttering wildly and flying off. This unbelievable story has been soundly
falsified as physically impossible (Lyne, 2022a; Lyne, 2022b; Vance, 2018) on all fronts.
Further all analyses purporting to support the 7th-arc-dive theory contained errors of physics,
logic, and in some cases common sense, as I explain in the Appendix to Lyne (2024). Finally,
not one scrap of debris was found in the extended, intensive, and hugely expensive searches
across 120,000 km2. In contrast the catastrophic crash of Swissair Flight 111 disintegrated the
entire aircraft into very small pieces, estimated at over 2 million by Larry Vance, who was the
decorated Chief Air-crash Investigator; see Figure 5 in Larry’s book detailing his excellent
investigation of MH370 debris (Vance, 2018). Continual denial, and relentless official criticism
of the alternate “controlled ditching” theory, has extended the failure to find MH370 now to
nearly ten years, with grieving relatives still waiting.
Since the beginning of 2021, the Penang Longitude Theory exposed a mastermind secret plan
for MH370 to evade detection to a very deep secret hole with substantial (not “a little” as one
official testified to Senators), but just enough, extra fuel taken onboard at departure from Kuala
Lumpur. But the plan for a “no-debris controlled ditching” failed, with the right wing ploughing
through a Southern Ocean wave with a number of large external and some positively
identifiable internal parts being emitted—along with many common cabin personal-items (that
were discarded if found for not being positively attributable) (Lyne, 2023a). Recently I showed
that despite Captain Sully expertly landing US Airways Flight 1549 on the relatively placid
Hudson River, the left engine was sheared off, with flaperon and flaps fractured off from both
sides. The French Captio-group also provided an excellent realistic simulation of flaperon
trailing-edge damage from ditching (Kamoulakos, 2020). Damages to the wings appear to
precisely mimic what happened to MH370 (Lyne, 2024); apart from the fact that the US
Airways impact was not severe enough to breach the fuselage as per MH370 (Vance, 2018).
The evidence is overwhelming that MH370 undertook a “controlled ditching” and further the
exact very precisely planned flightpath has been unravelled from the resolved riddles in the
Pilot-In-Command simulator track (Lyne, 2023b; Lyne, 2023c). We now have a highly
accurate flight path, as shown in Figure 1, as well as the critical point at the 7th arc when MH370
was in a controlled aggressive descent.
Figure 1. Figure adapted from (Lyne, 2023c) comparing the respective northern and southern Pilot-In-Command
(PIC) simulated tracks (left-side purple labels) with the planned tracks (right-side green labels). The PL Hole is
near where the 33oS latitude intersects the longitude of Penang (thin brown vertical line) at a 6000 m deep hole.
The Decoy Tracks (to Southern Ocean and Perth Airport runway) were not executed but merely to cause confusion.
Track lengths are noted in the labelled track boxes. The Jindalee-Over-the-Horizon Radar Network (JORN) range
and southern boundary from Laverton are drawn in purple (note purple JORN curve below the southern boundary
is not valid but merely part of the circle from Laverton as Google Earth Pro does not allow drawing of a part
circle). The Decoy Track to Perth is inferred from the other in the Simulator Track. Note that the map is not in
equi-distance projection.
2. Cloud Investigation
Our original aim here was to investigate evidence from anomalies in the clouds to determine
whether or not MH370 punched through the clouds during its controlled but aggressive descent
at the 7th arc (Lyne, 2022a). The image of clouds at the time is show in Figure 2. Careful
inspection (over many hours!) shows that it contains a trail of cloud-anomalies in approximate
alignment with the flight path from the turn of the JORN corner to the landing location.
Figure 2 A regional NASA Worldview satellite image of clouds (Reflectance) on the 8th March 2014. The satellite
image band to the right (of interest to us) was taken at about 03:07 UTC. The band to the left was taken later at
about 04:44 UTC. Of interest to our study are anomalies of a possible trail (not apparent at this regional scale)
highlighted within the green oval. At the “JORN Turn” MH370 switched from a southerly track to a direct flight
path to the landing location near (33oS, 100oE). The alignment of the flight path and anomaly trail is reasonable
and depends on wind direction at the time which was from south-west to north-east (see:
https://www.ventusky.com/?p=-31.6;84.9;4&l=gust&t=20140307/1500).
Formation of anomalous “holes” in clouds is well known to be related to aircraft, so these
anomalies could potentially be due to MH370. For example, Figure 3 shows an image from
NASA of “holes” and “trails” left by aircraft flying through clouds. Those examples appear to
be thinner upper-level clouds, whereas in our case, the clouds were thick enough to “hide” the
flight of MH370 except on occasions when it punched through the billows in the clouds. The
substantial size of holes and trails are due to a number of factors: First, the physical disturbance
caused by an aircraft flying through cloud at over 800 km/hr; second, cooling of airflow over
the wing (due to pressure drop) may precipitate out moisture; third, exhaust gases ejecting out
at over 2000 km/hr1 and temperatures of 300oC 800oC2. This exhaust gas comes from air
within the cloud being rammed into the jet engine and exhausted at extremely high velocity,
temperature, and turbulence. The superheated stream of exhaust gases must in some way rise
through the clouds into higher altitude where it will dilute, cool down, and possibly generate
an upper-atmosphere trail above the clouds. For example, look carefully again at Figure 3 and
notice that each of the large disturbances has both dark and light (white) elements. The dark
structure appear to be the holes and tears in the clouds and the lighter structures are within the
core of the dark structures and appear to be “new clouds” associated with the disturbance. In
the case of MH370, the plane is going through the clouds and will therefore be expected to
generate a corresponding trail of “new cloud” of much larger scale than the isolated structures
seen in Figure 3.
1 https://www.jet-x.org/a8.html
2 https://homework.study.com/explanation/how-hot-is-jet-engine-exhaust.html
Figure 3 Illustration from NASA of the formation of trails and “holes” from aircraft flying through clouds3. Image
credit: NASA image by Jeff Schmaltz, LANCE/EOSDIS Rapid Response. Note the various patterns of holes with
somewhat tear-drop shapes, trails, and combinations of holes and trails. Note also the scale of “50 km” (lower left
of image) and compare that scale with the scale of the anomalies. They are big!
A zoomed-in view of the anomalies in Figure 4 shows more clearly, but still indistinct, a series
of holes and discolored patches strung along a linear path. Flip back to Figure 3 to see
similarities and key differences from the thicker clouds here. Note, anomalies are near the
surface to begin with, but later are only apparent within the cloud structure. Also note the
endpoint is within a distinct hole. Hence, anomalies are not on the surface of the cloud but
within the cloud structure. A reasonable interpretation is that MH370 was attempting a
secret flight within the clouds.
Anomalies would be distorted by the 2 hours and 48 minutes (from the 7th arc, and ~26 minutes
less from the PL Hole) of cloud drift. Nonetheless, that track of anomalies is still quite clearly
distinguished from its surroundings.
3 https://earthobservatory.nasa.gov/images/84916/supercool-clouds
Figure 4 Zoomed in view of the trail of anomalies in the cloud show in Figure 2. The anomalies are apparent as a
series of “holes” and discolored (relative to surrounding) patches strung along a trail within the marked oval.
A second satellite source for the anomalies is visible in the Terra/MODIS “Cloud Top Height”
(a measure of the top of the cloud) shown in Figure 5. The anomalies are now much more
distinct from the surroundings and show an apparent mix of the expected height (~4 km) to
many anomalies with values near ~10 km (abnormal). How such anomalies are formed is a
question for others to answer, but as discussed before, superhot gases are being emitted within
the clouds. We note for now that it overlays (closely but not exactly) the anomalies seen in the
finer detailed reflectance cloud image. The nearest distance to the anomaly trail is about 200
km, so this is the least distance possible for the cloud to drift in 2 hours and 48 minutes.
At the time of the image, the sun-elevation angle was 48.2o at and azimuth of 57.6o (clockwise
from North) so any shadows would be 1.34 times the cloud-height difference and oriented
towards the southwest. Assuming a height anomaly between the lower and upper cloud of (10
4) = 6 km, potential shadows would be ~8 km. The misalignment between the upper and
lower cloud levels seen in Figure 6 cannot differentiate this scale or the direction which appears
more oriented towards the southeast. This leads us to suggest that the anomalies are actual
disturbances in the structure of the clouds and that perhaps the height-determination algorithm
was affected in some way by the rising exhaust gases.
Figure 5 Very distinct anomalies (within oval) of the Top of Cloud Height from the Terra/MODIS satellite. Darker
blues are high values (~10 km height), whilst the brown-yellow background is between 3.5 to 4 km height.
Approximate landing location is shown by the red location marker.
The geometry and distances of the anomaly trail from the track between the 7th-arc descent and
the landing location are shown in Figure 6. The length of the anomaly trail of about 330 km is
shorter than the track length of about 340 km, hence there is a shortfall which may be due to
the aircraft descending before it reaches the final destination in order to prepare for a level-
flight attempted controlled ditching. The cloud drift displacement till the satellite image, results
in a drift north-east of 260 km (west end) to 280 km (east end).
Figure 6 Orientation and distances of the cloud anomalies (overlay of “Cloud Top Height” and “Reflectance”)
from the assumed descent point at the 7th Arc, and the approximate landing location. Insert shows the winds from
Ventusky at 02:00 on the 8th March 2014. There is slight divergence of winds from west to east as expected from
the slightly greater drift observed from west to east. Due to vertical shear and Earth’s rotation, winds near the
surface (Ventusky winds are at 10 m level) increase and rotate with altitude; the cloud anomalies are nominally at
about 4 km altitude along the track. Note straight distances from Worldview do not accord with those from Google
Earth Pro (earth’s curvature considered), so are mainly used here for reasonable comparative purposes.
Wind velocities at 10 m level (ocean surface winds) were approximately 40 km/hr according
to Ventusky (https://www.ventusky.com/?p=-31.6;84.9;4&l=gust&t=20140307/1500).
Typically, the wind profile follows a power-law relationship:
where u and ur are winds at two different heights, z and zr respectively, and α is approximately
0.1434. With this formulation, we can expect the velocity at 4 km to be 2.4 times that at 10 m
near the ocean surface—about 96 km/hr. This is a reasonable agreement with the observed
value from the average distance of 270 km drifted in 2 hours and 35 minutes (average time
between start and end of track) = 270 / 2.6 ~ 104 km/hr. The end of the cloud anomaly track
is therefore due to the aircraft descending down from within the clouds for the final landing.
Hence secrecy was paramount and maintained till the very end. There are way too many
coincidences for the cloud anomaly trail to not be due to MH370 attempting a secret flight
within the clouds to hide the final location.
3. The Second Trail!
The Terra/MODIS satellite data analysed previously was a Descending Day (Terra) pass that
imaged the trail at about 03:07 UTC. A few hours later at about 07:24 UTC, the Aqua/MODIS
Ascending Day (Aqua) pass also imaged the area. Surprisingly, inspection of that image
(Figure 7) shows an anomalous trail in the clouds as well! The western half contains a long
trail-channel which is more distinct than the earlier image; almost as if the top of the cloud
layer has been peeled off as we expect hot gases would do. However, the eastern half shows
wider and deeper disturbances.
4 https://en.wikipedia.org/wiki/Wind_profile_power_law
Figure 7 Cloud anomalies from the Aqua/MODIS Ascending Day (Aqua) Cloud Reflectance pass at
approximately 07:24 UTC. Trail of anomalies (of roughly 304 km total length) are shown in the area within the
brown oval.
Figure 8, shows that the Reflectance anomalies are also accompanied by Cloud Top Pressure
anomalies which also mimic the disturbances seen in the Reflectance data. The overall length
is slightly less than the trail of anomalies seen more than 4 hours earlier.
Figure 8 Second trail of anomalies overlaid with the Cloud Top Pressure (Day) from Aqua/MODIS Ascending
Day (Aqua) pass. The Pressure data indicates that the greater disturbances seen in the Reflectance data to the east
are also reflected in the greater pressure anomalies.
Another supporting data is from the Suomi NPP/VIIRS satellite which passed 5 minutes later
and showed a trail of visible Cirrus Reflectance anomalies aligned with the Cloud Reflectance
data as seen in Figure 9 (note apparent misalignment is due to timing delays of ~5 minutes
between the two images).
Figure 9 Second Reflectance anomaly trail overlaid with Cirrus Reflectance (Visible & NIR) from the Suomi
NPP/VIIRS satellite. Note that Cloud Reflectance data is at 07:24 UTC whilst the Suomi Cirrus data is slightly
later at 07:29 UTC. Hence, the displacement between the features is due primarily to this timing delay and not a
shadow effect which for that time would be towards the south east in any case (303o azimuth).
Distances and timings from the First anomaly trail to the Second indicates that the latter trail
was advected at a slightly lesser drift speed of ~87 km/hr, and in a more easterly direction as
seen in the summary shown in Figure 10.
Figure 10 Cloud reflectance image at 07:24 UTC overlaid with three tracks: 1) red-dotted track is the assumed
path taken by MH370 from 00:19 UTC at the 7th arc to its landing site at the PL Hole estimated at 00:45 UTC; 2)
the first anomaly trail at 03:07 UTC; and, 3) the second anomaly trail at 07:24 UTC.
To summarise, Table 1 shows details of the satellites and data for the 5 images used to show
the drift of MH370 cloud anomalies from the final track between 00:19 – 00:45 UTC to a first
set of anomalies at 03:07 UTC and a second set at 07:29. This represents over 7 hours since
00:45 UTC
MH370 commenced its descent at the 7th arc. The anomaly trails are shorter than the track taken
by MH370 but the trails were obvious especially from the Cloud Top images.
Table 1 Details of the final PIC Track and the two anomaly trails together with the satellite passes.
Track Time
(UTC)
Satellite Data Track Length
(km)
00:19 ~ 00:45
PIC Track 344
03:07 Terra/MODIS
(Descending)
Cloud Reflectance
Cloud Top Height
337
07:24 Aqua/MODIS
(Ascending)
Cloud Reflectance
Cloud Top Pressure
304
07:29 Suomi
(Ascending)
Cirrus Reflectance 304
To summarise, we have demonstrated that there were very clear trails of cloud anomalies in
both the Reflectance and especially the Cloud Top Height/Pressure satellite images, which
aligned and matched. The length of the trails were of the length expected from the steep descent
at the 7th arc to the final landing at the Penang Longitude Hole where the longitude of Penang
intersects the PIC Track (approximately at 33oS), 1500 km west of Perth. The cloud-drift
velocity and direction match what we expect from the classic Power-Law profile. Even some
7 hours later, the internal path within the clouds taken by MH370 was continuing to evolve and
indeed the western half showed a distinct channel as the top of the clouds was presumably
evaporated away by the heated exhaust and induced circulation.
The results suggest that even the final approach to the landing location was done in secret
within the clouds rather than below. A flight below cloud level would allow more time for
surveying the landing location. But it seems the priority was one of secrecy, but without the
realization that this would leave an obvious trail in satellite images that would last a long time.
There is a shortfall between the first anomaly trail length of 330 km and flight path distance of
340 km, which suggests there was ample allowance for an attempted near level-flight
controlled ditching.
As an aside, there is another fainter trail to the north east, barely visible in Figure 5. What that
might be due to is unclear as it involves a faster cloud drift speed and is rotated to the right, all
classic signs of a wind profile affected by vertical shear. These latter observations suggests it
may be due to a higher-altitude path. It may perhaps be associated with hot exhaust gases, but
that interpretation would require both sets of clouds aligned during formation and then
separated out after 2.8 hours. Either that or there is another interpretation, which may have
implications for our analysis. Both sets of anomaly trail images suggest instead that the Cloud
Top anomalies are right above the anomalies visible in the reflectance data. Solar inclination
and azimuth calculations do not support anomalies being due to shadows. We leave resolution
of the fainter second trail as an open question for further discussion and analysis by others. For
now, the anomaly trail matches precise predictions by the Penang Longitude Theory very well,
so we must go with that interpretation as a precautionary measure.
4. Conclusions
MH370’s-controlled descent at the 7th arc was to prepare for a secret flight path to the landing
location, within the clouds, in order to avoid detection. Distinct remnant anomalies in both
reflectance and cloud height/pressure revealed the “secret” flight path very clearly even after 7
hours.
Funding: This research received no external funding.
Acknowledgments: Thank you to Bill Tracy for past discussions about clouds and MH370. A sincere thank you to the un-
known voices for providing the insights. Rest in peace.
Conflicts of Interest: The author declares no conflict of interest.
5. References
ATSB (2017) The Operational Search for MH370, Canberra. Australia.AE-2014-054). Available at:
https://www.atsb.gov.au/media/5773565/operational-search-for-mh370_final_3oct2017.pdf.
Kamoulakos, A. 'Aspects of analysis and simulation of a flaperon ditching scenario', Aiaa Aviation 2020 Forum.
Lyne, V. (2022a) 'Final Communications from MH370 Supports Controlled Eastward Descent Scenario', Journal of
Navigation, (Under Review).
Lyne, V. (2022b) 'Flawed Vertical Dive Conclusion from MH370 Doppler-Shifts', Researchgate, pp. 44.
Lyne, V. (2023a) “Drift” Versus “Sail” of MH370 Flaperon to Réunion Island, Hobart, Australia.
Lyne, V. (2023b) MH370 Flight Hidden in Simulated Triple-Twist Riddle [Technical Report], Hobart. Tasmania.
Australia: Researchgate. Available at: http://dx.doi.org/10.13140/RG.2.2.12350.15685.
Lyne, V. (2023c) MH370 Malacca Track Riddle [Technical Report], Hobart. Tasmania. Australia: Researchgate.
Available at: http://dx.doi.org/10.13140/RG.2.2.26851.63528/1.
Lyne, V. (2024) Was MH370 Debris Adrift in the Leeuwin Current? , Hobart. Tasmania. Australia: University of
Tasmania. Available at:
https://www.researchgate.net/publication/377782958_Was_MH370_Debris_Adrift_in_the_Leeuwin_Current.
Vance, L. (2018) MH370 Mystery Solved. Group of Three Publishing.
... For secrecy the aircraft needed to descend as low as possible to just below, or within, the clouds. In a very recent update, I report the discovery of a 300 km trail of cloud anomalies that align well with the expected final PIC track of MH370 (Lyne, 2024a). These anomalies were visible in five satellite images from three satellite passes. ...
Article
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Official interpretations of Doppler shifts from the final satellite communications of missing Malaysian Airlines MH370 were based on a motion-decoupled 'Up-Down model'. That model predicted an uncontrolled high-speed gravitationally accelerated dive following fuel starvation. Here, I challenge that model using a more-realistic motion-coupled 'Declination model'. Aerial, satellite and underwater searches failed to find the predicted official violent crash-site near the 7th arc. Meticulous re-examination of debris damage by air-crash investigator Larry Vance concluded that the aircraft glide-landed under power with extended wing-flaps. The trailing-edges were then damaged, broke off their mountings, flailing about and retracted along the guides to cause the observed wing-flap damage. Larry's conclusions complement interpretations from the 'Declination model' which we demonstrate here with three example flight tracks. Our revised Doppler-shift analyses support the hypothesis of a controlled eastward descent. We conclude that the official theory of fuel starvation and a high-speed dive are fundamentally flawed.
... For secrecy the aircraft needed to descend as low as possible to just below, or within, the clouds. In a very recent update, I report the discovery of a 300 km trail of cloud anomalies that align well with the expected final PIC track of MH370 (Lyne, 2024a). These anomalies were visible in five satellite images from three satellite passes. ...
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Update: 11 June 2024. The paper was Accepted by the Journal of Navigation and is now In Production. Official interpretations of Doppler Shifts from the final satellite communications of missing Malaysian Airlines MH370 were based on a motion-decoupled “Up-Down Model”. That model predicted an uncontrolled high-speed gravitationally accelerated dive following fuel starvation. Here, I challenge that model using a more-realistic motion-coupled “Declination Model”. Aerial, satellite, and underwater searches failed to find the predicted official violent crash-site near the 7th arc. Meticulous re-examination of debris damage by air-crash investigator Larry Vance concluded that the aircraft glide-landed under power with extended wing-flaps. The trailing-edges was then damaged, broke off their mountings, flailing about, and retracted along the guides to cause the observed wing-flap damage. Larry’s conclusions complement interpretations from the “Declination Model” which we demonstrate here with three example flight tracks. Our revised Doppler-Shift analyses support the hypothesis of a controlled eastward descent. We conclude that the official theory of fuel starvation and a high-speed dive are fundamentally flawed.
Technical Report
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Against cautionary advice from colleagues, I sought to provide much-needed support to veteran skipper Kit Olver for his claim in September-October 2014 that he had snagged in his trawl net what may have been a “wing” from a commercial jet airline off Robe, South Australia. Oceanographically the only way for that “wing” or other large debris from MH370 to reach that location was via the swift Leeuwin Current. I developed a novel guided-drift algorithm (named MH370 Drift Algorithm) to concord with our best understanding of how drifters behave in the open ocean and within swift currents like the Leeuwin Current. Simulations with the algorithm provided sound confirmation that the drift was indeed possible all the way from the only location which reconciles all MH370 evidence: the Penang Longitude Deep Hole. This is a very surprising and remarkable finding! Analyses of past drifters suggests that during early winter, the western and eastern segments of the Leeuwin Current which are nominally segregated, were joined temporarily to enable drift from west to east. NOAA Drifter 55600502 provided the observational support for such a drift. Another Drifter 55600557 was fortuitously located near the landing site on the 8th March 2014 but its sensors were failing and it eventually terminated in May 2014, but its drift provided confirmation of the simulated drift pattern after landing. Taking all these findings into consideration, I conclude that there is more than sufficient evidence for a precautionary investigation to be conducted of Kit Olver’s find. Further information is required of the find. But the debris item is likely to be still near where Kit left it (easy search), or at the bottom of the continental slope of a nearby canyon (much much more difficult search).
Technical Report
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You Ain't From Around These Parts Are Ya?"-David Chaltas (2021). ------------Simulated drift of MH370's flaperon, discovered at Réunion Island, from the unsuccessfully-searched 7 th-arc location, and the unsearched Penang-Longitude (PL) location, are both deemed feasible using CSIRO's model with different drift formulations. Locations are 700 km apart, and 1800 km added drift is required from the heavily-handicapped 7 th arc. CSIRO's 7 th-arc model used a "10 cm/s plus 1.2% windage" formula, but PL drift was a standard 1.2% windage (drift speed as a percent of wind speed). Did one of these break the rules in the "Drift to Réunion Island"? Over 508 days, CSIRO's flaperon "drifted" nearly 4400 km extra to reach Réunion Island on time, but little speed up was required from PL. Flaperon (real-Boeing plus replicas) field trials by CSIRO were under light-moderate winds in a shallow semi-enclosed embayment, and another with just wood/steel replica flaperons, offshore under high-winds. But embayment light-wind perpetual-motion 10 cm/s speedup for the real flaperon, above offshore model-calibrated 1.2% windage for general drift, was statistically well supported! Data exploration of embayment field trials suggested that drift was affected by Wind speed and observed Windage (drift speed/wind speed) itself! In the embayment trials, Wind (standard % formula) dominated above 9 m/s when Windage gremlins are asleep, with sleepless exceptions that identify mischief makers. Windage gremlins awaken, with the asymmetric flaperon flipping into a fast-slow "break-dance", between 9 to 5 m/s Wind to transition, below 5 m/s, tail-up, hooning mischievously left-of-wind along the fast-lane, low-wind, low-roughness, uplifted, "10 cm/s plus 1.2% windage" formula of good statistical fit! The referee in the form of a new innovative "windage" diagnostic modelling algorithm confirms "windage stratification" (where gremlins hide) also affected non-flaperon drifters but only from exposed surface drag and strong current shear in the top meter-expected from past research on lakes/embayments and density-stratified environments. Significant flaperon performance boost was from wind-sailing pressure forces wedged under the tail-up "sail canopy", uplift from trailing-edge wind separation, direct wind pressure uplift, and hydroplane lift-the reverse effects of a "duck-tail spoiler" used by race car "drifters" for extra downward drag pressure. In effect the flaperon flies with lift in air but sails with lift upside-down in water (on calm seas that is!). The new statistical diagnostic algorithm (over 99% deviance explained) suggests these performance-enhancing stable-condition tail-up postures, and wind shear effects in the top meter, are not perpetually viable in unstable deep turbulent conditions, such as the wild Southern Indian Ocean-just as no ballerina can perform the same on a wobbly boat, let alone a small surfboard-stage, heaving on the wild Southern Indian Ocean. Disappointingly, after accounting for justifiable object-related open-ocean drift enhancement, the 7 th-arc embayment-formula flaperon simulation was deemed to have sailed at least 3000 km more than justified by open-ocean drift rules. As before, MH370 still lies waiting patiently at the Penang Longitude location; a location supported by new direct satellite evidence of debris trail from the location and reconciled-evidence rejected by the sleepless-gremlin-infested 7 th-arc theory. No 7 th-arc analysis past the 5 th arc has withstood the test of time. All that is doable there is Done! The misleading 7 th-arc theory is Done! Let's not be blindly misled to that disappointing place again, which has been more than desperately searched in confused science and sea. Give it a rest and give us all a break! In memory of MH370, the new diagnostic algorithm is named "MH370 Open-Ocean Drift Algorithm", or MOODA. Rest in peace, it won't be much longer now.
Technical Report
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Previously I unraveled the southerly track of the “Pilot-in-Command“ (PIC) flight simulator to show that it was composed of three parts where the final location of MH370 at the Penang Longitude (PL) deep hole (PL Hole) was a pivot point (Part 1) that separated out a northern track (Part 2), and a southern track (Part 3). The Part 2 northern track length of under ~5000 km optimally fitted the PL theory predicted MH370 track length with a tight turn near the southwest corner of the Jindalee Over-the-Horizon Radar Network (JORN) range. Part 3 was an unexecuted decoy track (~1480 km) of precisely the same distance as the PL location to Perth Airport. Given the obsessive precise planning that went into this track, here I ask whether the northern straight PIC-simulated Malacca Strait track from Kuala Lumpur International Airport (KLIA) to waypoint (DOTEN) well northwest of Sumatra also held a riddle? I found that the PIC-simulated Malacca Strait track length of ~1563 km precisely fitted the planned MH370 track starting from KLIA proceeding northeast to just past waypoint (IGARI) at the boundary between Malaysian and Vietnamese ATC (Air Traffic Control space), followed by a sharp southwest turn to just south of Penang airport (PEN), before heading along the Malacca Strait to a turnoff just west of Sumatra for the start of the southward track, described previously. There is remarkable precise agreement between the respective track lengths of ~1563 km, and as before the turnoff to the southward track was at a simple latitude/longitude waypoint. The MH370 track overshot IGARI, possibly to allow for the turn from northeast to southwest and agreed closely with the ATSB track. I conclude that the simulation was to enable an accurate calculation of the fuel load required to reach the PL Hole and that the simulation with a Boeing 777-200LR, not part of Malaysia Airlines’ fleet, was to cause confusion. This adds yet another confirmation of the PL theory and suggests an obsession with precise track planning and execution. In the end, this obsession with precision was a critical element in unravelling all evidence and finding new evidence in support of the PL theory. There can be very little doubt now that MH370 lies waiting at the PL location as all discarded evidence are now reconciled, plus new insights and evidence complete a coherent integrated interpretation of MH370’s entire flight, landing and location.
Technical Report
Full-text available
Update: Northern track riddle is solved in "Malacca Track Riddle" manuscript. A "Pilot-in-Command" (PIC) flight simulator for a "Long-Range" Boeing 777-200LR recovered by FBI and official MH370 investigators shows a track from Kuala Lumpur up the Strait of Malacca, followed by a sharp southward left turn well northwest of the northern turn estimated from satellite and phone communications (just west of Sumatra), and ending deep in the Southern Ocean, well past the fuel load aboard the shorter "Extended Range" MH370 Boeing 777-200ER. Whilst resembling the official track along the Malacca Strait, after the turnoff, the PIC track heads towards the southeast compared to the official southerly track. No significant official interpretation was therefore attached to this track, other than a fleeting suggestion, that was dismissed in the search for MH370 (based on a questionable retracted-flap theory, logically challenged, and rectified by Larry Vance), that it may reflect a "very unlikely" intention for "controlled ditching" in the Southern Ocean. In 2021, I showed that this track crossed over, or passed very near, the location predicted by the Penang Longitude theory (the PL location). Here, I reflect, as part of the "scenario backlash" process, on the PIC track assuming that it may be a riddle with hidden planning details such that the start of the southward track (at the northern left turn) and end point obfuscate simulation of flight path intentions. A three-part riddle was identified where the PL location, as the pivot point (Part 1), separated out a northern track (Part 2), and a southern track (Part 3). With Part 1 solved, the Part 2 northern track length of ~5000 km optimally fits the PL theory predicted track length, if the southeast turn to the PL location occurs tightly near the southwest corner of the Jindalee Over-the-Horizon Radar Network (JORN) range (a critical core feature of the PL theory). The Part 3 decoy southern track length (~1480 km) is precisely the same distance as the PL location to Perth Airport. I conclude that Part 1 and 2 were related to the intended flight path, and that Part 3 was a diversion; simply because a PIC track with just Part 1 and 2 may have been enough to solve the riddle. If this is indeed the resolution of the riddle, it is yet another confirmation added to the list of all valid evidence reconciled by the PL theory. The remaining unsolved riddles are whether the PL location is indeed the very precise final resting place of MH370; and why search investigators still insist on searching at or near the extensive mathematically flawed and failed 7 th-arc searches; or the very least why an international science review hasn't been instigated?
Conference Paper
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In the wake of the disappearance of the MH370 Boeing 777 and the recovery of the right wing flaperon debris, a ditching scenario has been envisaged by the investigating authorities. In this respect, this paper attempts to assess the forces exerted by fluid-structure interaction upon a guided-ditching flaperon both through analytical and numerical means and compare the results with the evidence. The author presents a modified version of the Karman wedge water impact theory, suitably adapted for a single flat panel ditching case, which leads to a simple analytical relation for the total hydrodynamic force as a function of the flaperon horizontal and vertical speeds and its angle of impact. Validation of the analytically obtained force to that obtained by Smoothed Particle Hydrodynamics (SPH) water simulations is presented. An extension of the analytical relation is made for the flaperon section failure stresses as a function of velocity vector and angle of impact with the perspective towards areas containing fastened parts. A basic Finite Element Model (FEM) of the flaperon is then conceived from available geometric and material data and subjected to a typical ditching impact. The type and place of failure of the flaperon (notably its trailing edge) appears in accordance with the analytically obtained upper bounds and with the state of the recovered flaperon.
The Operational Search for MH370, Canberra. Australia.AE-2014-054)
ATSB (2017) The Operational Search for MH370, Canberra. Australia.AE-2014-054). Available at: https://www.atsb.gov.au/media/5773565/operational-search-for-mh370_final_3oct2017.pdf.
Final Communications from MH370 Supports Controlled Eastward Descent Scenario
  • V Lyne
Lyne, V. (2022a) 'Final Communications from MH370 Supports Controlled Eastward Descent Scenario', Journal of Navigation, (Under Review).
Flawed Vertical Dive Conclusion from MH370 Doppler-Shifts', Researchgate
  • V Lyne
Lyne, V. (2022b) 'Flawed Vertical Dive Conclusion from MH370 Doppler-Shifts', Researchgate, pp. 44.