Malfunction Details - Continued
Table 7-16.
Indications presented
Corrective
Aircraft indications
Required
to instructor/operator
Ref
action
and related effects
and trainee
malfunction
number
*
Yaw-axis flight control
Noncorrectable
Instructor: AUTO BUCS PDLS
AUTO BUCS
linkage is severed.
PDLS
appears on CRT.
Yaw-axis BUCS is engaged.
Trainee: BUCS ON and MASTER
CAUTION lights illuminate.
SAS damping not available
(ASE switches engaged). CAS
not available, and force
trim operational. In inte-
grated mode. control of air-
craft is assigned to desig-
nated flyer (pilot or CPG).
In independent mode. pilot
controls PLT cockpit, and
CPG controls CPG cockpit.
*
Noncorrectable
Instructor: AUTO BUCS CYC
Lateral-axis flight control
AUTO BUCS
linkage is severed. BUCS
LAT appears on CRT.
CYC- LAT
is engaged.
Trainee: BUCS ON and MASTER
CAUTION lights illuminate,
SAS damping not available
(ASE switches engaged). CAS
not available, and force
trim operational. In inte-
grated mode, control of air-
craft is assigned to desig-
nated flyer (pilot CPG). In
independent mode, pilot con-
trols PLT cockpit, and CPG
controls CPG cockpit.
