NATOPS prep Flashcards
which pitot tube provides info to ESIS
1 pitot
what info is on ESIS
attitude, slip/skid, altitude, airspeed, heading
flight control system type
rigid control rod
collective routing
collective to torque tube beneath cockpit seats then up left pillar and across to mixing unit. along path is lvdt
cyclic routing
cyclic to 2 torque tubes then up right pillar then SAS actuators to mixing unit
pedal routing
pedals combine under center console then rods and bellcranks to yaw sas actuator then t/r servo then link in tail boom to pitch change mechanism
3 functions of pitch change levers
blade flapping limiter stop
pass pitch change inputs from pitch change links to blades
act as mount for hyd dampers
purpose of chinese weights
provide zero pitch return moment to reduce pitch control loads
t/r pitch change names
pitch change links connect to crosshead to pitch change horns to blades
how many T/R driveshafts
2
DC sys numbers
28VDC
AC sys numbers
115/26 Vac 400 Hz single phase
how to secure main bus
turn off gen sw
CB symbology
single block: batt bus
double block: emer bus
nothing: main bus
Battery numbers
24V 27Ah NiCd batt
batt hot at 71+-3C
what does GCU control for
starter control, voltage reg, overvolt, short circuit protection, reverse current protection
AUX GCU job
voltage reg, overvolt, aux bus tie connector, short circuit protec, reverse current protect
EXT pwr voltage requirement
28V
what’s the AC sys for
VG and SAS actuators
ENG name
PT6B-37A
eng type
free turbine turboshaft
1 of axial compressors
3
how is eng mounted to main frame
parallel rod on AGB
tripod of right RGB
bipod on left RGB
when does bleed air valve close for normal ops
91%