69
VIRUS
www.pipistrel.si
REV. 0
daily
st 5
hours
50
hours
100
hours
250
hours
500
hours
1.000
hours
10.000
hours
FUSELAGE
SC O
surface and structure condition
C SC
elevator control tube bearing
C SC
undercarriage stuts attaching points
C C SC
doors, hinges
C C SC LO
rudder control wires and hinges
C C SC
CABIN
SC O
control levers, instr. panel, seats
C SC
control levers’ free play
C C SC
intstruments and pitot-static
C SC test
glass surfaces: clean, attached
C C SC
rivet condition
C SC
safety harnesses and attach. points
C SC
parachute rescue sys. activation handle
C SC
wing connectors: fuel, electrical
C C SC
bolts and spar pins
C C SC
wing main bushings, control connectors
SC
UNDERCARRIAGE
O
tires
C C R
main strut, nose wh. fork condition
C C SC
wheel axis and wheels
C
brake wires
C SC R
brake drums
C C R
wheel bearings
C SC R
tail wheel main bolt
C R
wheel fairings
C C C
CONTROLS
R
general free play
C C SC
control stick
C LO SC
rudder pedals (damage, centered, paral.)
C C C LO
rudder wire rope
C SC
bolts, visible bearings (tail, fuselage)
SC LO
dicult-to-reach bearings (wings, under cabin oor)
LO
aileron, elevator and rudder hinges
SC LO
equal spoiler extension, undisrupted m.
C SC LO
spoiler plate spring stiness
C
ap handle
C SC LO
elevator trim
C LO
springs: aps, rudder, el. trim, stablizer main fastening bolt
LO C R
airbrakes internal connector rod (if own or stored where possibilty for
corrosion is increased (oceanside, wet regions ..)
change every 2 years
spoilers’ (airbrakes’) drive ne adjustment
see page 67 for detailed description
Handling and maintenance