proposition_id,proposition,factual_status,reliance,source_ids
V06-P001,00:19 SATCOM sequence records an SDU log-on following an interruption and restoration of electrical power.,ESTABLISHED,R1,V06-S002; V06-S003; V06-S004
V06-P002,Fuel exhaustion followed by APU-supplied electrical restoration is the best-supported explanation for the 00:19 SDU log-on.,STRONGLY SUPPORTED,R2,V06-S003; V06-S004
V06-P003,"Absence of the expected post-log-on IFE connection constrains the terminal sequence but does not uniquely identify impact, APU power loss, IFE isolation or loss of satellite line-of-sight.",ESTABLISHED LIMITATION,R1,V06-S003
V06-P004,"The final BFO measurements are strongly consistent with a substantial and rapidly changing descent component but do not independently establish exact descent rate, attitude or control state.","STRONGLY SUPPORTED, MODEL-DEPENDENT",R3,V06-S004; V06-S005; V06-S006
V06-P005,The official final-BFO framework accounts for aircraft horizontal motion and track-dependent Doppler effects; it is not accurately described as simply ignoring horizontal motion.,STRONGLY SUPPORTED,R2,V06-S004; V06-S006
V06-P006,Alternative combinations of horizontal trajectory and vertical motion can change the final-BFO solution; the last two BFO values do not uniquely determine one exact 3-D trajectory.,STRONGLY SUPPORTED,R2,V06-S004; V06-S006; V06-S007
V06-P007,The 2024 controlled-eastward-descent paper raises a material adversarial challenge but does not presently falsify the ATSB/DSTG rapid-descent interpretation.,SUPPORTED - specialist review required,R3,V06-S006; V06-S007
V06-P008,The 18:25 SDU log-on is strongly consistent with restoration of SDU power after a material interruption; the specific historical cause of that interruption remains indeterminate.,STRONGLY SUPPORTED / cause INDETERMINATE,R2/R4,V06-S001; V06-S003
V06-P009,"A routine loss of only the left engine generator or a normal brief AC-bus transfer is not, by itself, a sufficient explanation for the 18:25 SDU log-on.",STRONGLY SUPPORTED,R2,V06-S003
V06-P010,The public record does not establish that the 18:25 event was an aircraft-wide dual-AC-bus failure or deliberate cockpit action.,INDETERMINATE,R4,V06-S003
V06-P011,The right outboard flap was most likely retracted when it separated; this weakens a conventional flap-extended ditching scenario but does not establish control state at impact.,"STRONGLY SUPPORTED, SPECIALIST-DEPENDENT",R3,V06-S005
V06-P012,"The pilot home-simulator evidence is relevant circumstantial evidence, but the official forensic record did not establish one continuous rehearsal of MH370's later route.",ESTABLISHED LIMITATION,R2,V06-S001
V06-P013,"The lithium-ion battery mass was 221 kg within a 2,453 kg consignment; describing MH370 as carrying 2.4 tonnes of lithium batteries is materially misleading.",ESTABLISHED,R1,V06-S001
V06-P014,"The Malaysian military associated the primary-radar track with MH370; radar-based speed/height reconstructions contain acknowledged limitations, while the track behaviour supports active control during at least part of the diversion.",STRONGLY SUPPORTED,R2/R3,V06-S001
V06-P015,Historic underwater search data includes areas with >95% detection confidence and lower-confidence/gap areas; searched must not automatically be equated with uniform 100% exclusion.,ESTABLISHED / QUALIFIED,R2,V06-S004; V06-S009
V06-P016,"The 2026 Ocean Infinity agreement was extended to 30 June 2027 with 7,428.54 km2 of the current target area reported as remaining.",ESTABLISHED CURRENT STATUS,R1,V06-S010