The V/STOL capability of the AV-8B Harrier is provided through a sophi
sticated combination of vectored thrust and aerodynamic technology. Th
e proper interaction of the nozzle thrust and flap system is of extrem
e importance. Specific combinations of nozzle angle and flap position
are employed to optimize both jet lift and aerodynamic lift. However,
if the proper flap-nozzle position schedule is violated, the resulting
thrust and flap impingement may cause a severe nose-down pitching mom
ent sufficient to override the pilot control. Depending upon ground pr
oximity, this condition creates a hazard which causes great potential
for loss of aircraft and/or pilot. Flap impingement hazard was identif
ied on the AV-8B aircraft as a potential catastrophic flight hazard. I
n response, a requirement was established to 1) study the severity of
the flap impingement hazard on the AV-8B, 2) devise flight operational
procedures which would minimize pilot exposure to the hazard potentia
l and the resulting pilot control problems during flight, and 3) devis
e a training capability to familiarize pilots with flap impingement ha
zard characteristics and recovery procedures. This paper comprises the
results of a study which utilized piloted flight simulation and fleet
simulation trainers to meet these requirements.