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ElaKiri Talk!
Why the Turkish 737 went down???
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<blockquote data-quote="rochel1977" data-source="post: 4099685" data-attributes="member: 371"><p><strong>Dutch Safety Safety Board: Safety Alert to Boeing: </strong></p><p></p><p>Recommend to review Fligth Manual B737: if radio altimeters are inop, autothrottles and autopilot must not be engaged;</p><p></p><p><img src="http://cdn-www.airliners.net/aviation-photos/photos/6/0/6/1489606.jpg" alt="" class="fr-fic fr-dii fr-draggable " style="" /></p><p></p><p></p><p>* 9 casualties;</p><p>* 80 wounded, 28 still in hospital;</p><p>* TK 1951 ETA 10.40</p><p>* No problems until last moment;</p><p>* 3 qualified pilots in cockpit;</p><p>* 1st officer flying the aircraft;</p><p>* TK1951 received landing clearance, no delay in approach, direct approach;</p><p>* Autopliot engaged during approach;</p><p>* DFDR and CVR in good condition;</p><p>* at 1950 ft, LH radio altimeter step change read out from 1950 ft to -8ft;</p><p>* this faulty altitude was also reported to autothrottle;</p><p></p><p>* CVR: crew saw altimeter discrepancy;</p><p>* Crew did not see this discrepancy as problem, and lowered gear as gear warning was activated due to -8 ft radio alt;</p><p>* As a result, autothrottle went into retard mode at 1950 ft rather than 50 ft due to faulty radio altimeter read out;</p><p>* Aircraft slowed to stall speed;</p><p>* Aircraft flight controls [autothrottles] thought airplane was above runway and went into "flare mode";</p><p></p><p>* At 450 ft stall warning /stick shaher activated;</p><p>* power was increased immediately [!] [TOGA?], but power increase was too late to continue flight;</p><p></p><p></p><p>* identical problem with LH radio altimeter happened twice before on this airplane in last eight flights;</p><p>* that data was still on DFDR, as it had 25 hrs upto crach of recorded information;</p><p></p><p>* Landing gear and engines broke off at impact as designed;</p><p>* due to high power setting engines flew forward by 250m at impact separation;</p><p></p><p>* investigation will now focus on radio altimeter, and relation/logic with autothrottle system;</p><p>* runway was not [very well] visable to crew;</p><p></p><p>* Dutch Safety Board will lead investigation;</p><p>* Several other parties will support investigation [NTSB, Boeing, CFM internaional, Turkish authorities, ;</p><p></p><p>* Good words for justice department, especially in isolating area around airplane;</p><p>* Safety Board and Jutice Department back on same frequency;</p><p>* Main objective of investigation is fact finding and improve safety;</p><p>* Justice department will limited access to data, to protect "whistleblowers";</p><p></p><p>* radio altimeter fault is only technical fault found so far;</p><p></p><p>* No indications of ATC faults;</p><p>* No indications of [wake-]turbulence;</p><p>* Too early to tell if crew made mistakes;</p><p>* All members of invetsigation team are on same line of thinking</p><p>* Not yet known where the 2 previous occurances of LH radio Alt happened</p><p>* LH radio Alt not considered flight critical component, as function can be taken over manually by crew;</p><p>* No conclusions on TK maintenance activities and procedures;</p><p></p><p>* Aircraft will be recovered this week;</p><p></p><p><img src="/styles/default/xenforo/smilies/default/dull.gif" class="smilie" loading="lazy" alt=":dull:" title="Dull :dull:" data-shortname=":dull:" /> <img src="/styles/default/xenforo/smilies/default/dull.gif" class="smilie" loading="lazy" alt=":dull:" title="Dull :dull:" data-shortname=":dull:" /> <img src="/styles/default/xenforo/smilies/default/dull.gif" class="smilie" loading="lazy" alt=":dull:" title="Dull :dull:" data-shortname=":dull:" /></p></blockquote><p></p>
[QUOTE="rochel1977, post: 4099685, member: 371"] [B]Dutch Safety Safety Board: Safety Alert to Boeing: [/B] Recommend to review Fligth Manual B737: if radio altimeters are inop, autothrottles and autopilot must not be engaged; [IMG]http://cdn-www.airliners.net/aviation-photos/photos/6/0/6/1489606.jpg[/IMG] * 9 casualties; * 80 wounded, 28 still in hospital; * TK 1951 ETA 10.40 * No problems until last moment; * 3 qualified pilots in cockpit; * 1st officer flying the aircraft; * TK1951 received landing clearance, no delay in approach, direct approach; * Autopliot engaged during approach; * DFDR and CVR in good condition; * at 1950 ft, LH radio altimeter step change read out from 1950 ft to -8ft; * this faulty altitude was also reported to autothrottle; * CVR: crew saw altimeter discrepancy; * Crew did not see this discrepancy as problem, and lowered gear as gear warning was activated due to -8 ft radio alt; * As a result, autothrottle went into retard mode at 1950 ft rather than 50 ft due to faulty radio altimeter read out; * Aircraft slowed to stall speed; * Aircraft flight controls [autothrottles] thought airplane was above runway and went into "flare mode"; * At 450 ft stall warning /stick shaher activated; * power was increased immediately [!] [TOGA?], but power increase was too late to continue flight; * identical problem with LH radio altimeter happened twice before on this airplane in last eight flights; * that data was still on DFDR, as it had 25 hrs upto crach of recorded information; * Landing gear and engines broke off at impact as designed; * due to high power setting engines flew forward by 250m at impact separation; * investigation will now focus on radio altimeter, and relation/logic with autothrottle system; * runway was not [very well] visable to crew; * Dutch Safety Board will lead investigation; * Several other parties will support investigation [NTSB, Boeing, CFM internaional, Turkish authorities, ; * Good words for justice department, especially in isolating area around airplane; * Safety Board and Jutice Department back on same frequency; * Main objective of investigation is fact finding and improve safety; * Justice department will limited access to data, to protect "whistleblowers"; * radio altimeter fault is only technical fault found so far; * No indications of ATC faults; * No indications of [wake-]turbulence; * Too early to tell if crew made mistakes; * All members of invetsigation team are on same line of thinking * Not yet known where the 2 previous occurances of LH radio Alt happened * LH radio Alt not considered flight critical component, as function can be taken over manually by crew; * No conclusions on TK maintenance activities and procedures; * Aircraft will be recovered this week; :dull: :dull: :dull: [/QUOTE]
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