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Printed page xi. PDF page 14.
and intercepted the final approach course about 14 nautical miles (nm) from the threshold at an altitude slightly above the desired 3� glidepath. This set the flight crew up for a straight-in visual approach; however, after the flight crew acceptedOpen final report at PDF page 14NTSB AAR-14/01: Asiana Airlines 214
Printed page xii. PDF page 15.
FLCH SPD mode, what happens when the A/T is overridden and the throttles transition to HOLD in a FLCH SPD descent, and how the A/T automatic engagement feature operates. The PF's faulty mental model of the airplane's automation logic ledOpen final report at PDF page 15NTSB AAR-14/01: Asiana Airlines 214
Printed page xiii. PDF page 16.
of flight, a low airspeed alert may need to be designed so that its activation threshold takes airspeed (kinetic energy), altitude (potential energy), and engine response time into account. Research that examines the injury potential from significant lateral forces inOpen final report at PDF page 16NTSB AAR-14/01: Asiana Airlines 214
Printed page 4. PDF page 22.
landing configuration. It is the speed required on crossing the landing runway threshold at a 50-ft height to achieve calculated aircraft performance. 4Open final report at PDF page 22NTSB AAR-14/01: Asiana Airlines 214
Printed page 5. PDF page 23.
it was configured with the flaps and landing gear up; the autothrottle (A/T) was in hold (HOLD) mode; and the autopilot flight director system (AFDS) was in flight level change speed (FLCH SPD) pitch mode and heading select (HDG SEL)Open final report at PDF page 23NTSB AAR-14/01: Asiana Airlines 214
Printed page 7. PDF page 25.
At 1126:33, the thrust levers reached the idle position, and the A/T mode changed to HOLD. Immediately before the A/T mode change occurred, at 1126:32.5, the PM stated, "flight director," and immediately after the change, at 1126:34.0, the PF replied,Open final report at PDF page 25NTSB AAR-14/01: Asiana Airlines 214