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Old 24th Aug 2008, 01:15
  #709 (permalink)  
fdr
 
Join Date: Jun 2001
Location: 3rd Rock, #29B
Posts: 2,956
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SLATS: 777fly, dash-27 et al

The configuration of the Slats (and flaps) will be a basic part of the initial investigation to verify. The system is well decribed in the MD-80 LAMM Section 27-85-00 page 101-103, including the auto slat behavior and warning systems.
  • The Slat position is recorded to DFDR/QAR via the DFDAU
  • The cables may have witness marks to indicate position when tensile loads may cause separation of the cable
  • The actuator will indicate the position of the Slat drive drum (27-81-1), as will the autoslat actuator MI 76/77 etc. As well, the Flap/Slat handle position will be identifiable
.

quote reports unquote of possible lateral instability will certainly ensure some investigation is conducted in this area by competent investigating authorities.

As to CAWS: the 28v DC -L CB would need to be tripped, B1-832, AND the 28V DC-R CB B1-851 would need to be tripped for the crew to NOT get a warning of the CAWS being degraded/failed. (LAMM 31-51-00)

CVR will be interesting.
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