Landing technique and autobrake

FSS’s example disconnects A/T at MA/DA, begins a slight flare at 50 ft and reduces thrust to idle at 30 ft. It applies reverse after nose-gear touchdown, reduces to reverse idle at 80 kt and stows the reversers at 60 kt ^[9].

With autobrake and reverse thrust, FSS says the system adjusts brake pressure to maintain the selected deceleration. Pedal braking, selecting OFF or advancing a thrust lever above idle disengages autobrake ^[123].

FSS prohibits a go-around after thrust-reverser deployment ^[10].

The supplied SOPM gives a different reverse schedule: reduce toward MIN REV at 60 kt, then select idle at 30 kt ^[L01]. These are different source procedures; the guide’s simulator sequence follows the FSS example (PDF p. 368).