Storage; Flyabie Storage 7 To; Days; Preparation For Service - Raytheon BEECH BARON 58P Maintenance Manual

BEECHCRAFT
BARON 58P AND BARON 58TC
MAINTENANCE MANUAL
STORAGE
d.
Flight Control Surfaces. Lock
flight control surfaces
with internal and external locks.
The
storage procedures
are
intended to
protect
the airplane
e.
Grounding. Static
ground airplane securely and
from deterioration while it is not in
use.
The primary objectives effectively.
of these
measures are
to prevent corrosion and
damage
from f. Pitot Tubes. Install
pitot tube
covers
exposure
to the
elements. The three
types
of
storage
are:
g.
Windshield
and Windows.
a.
Flyable
storage
7 to 30 days
1. Close all windows.
b.
Temporary Storage
31 to 90 days
2.
It is recommended that
covers
be installed
c.
Indefinite Storage 91 days
to
over
the windshield and windows.
FL YABLE STORAGE
7
TO 30 DA YS
PREPARA
TION FOR SERVICE
a.
Mooring.
a.
Remove all
covers,
tape and control locks, clean
the airplane and give it
a
thorough
inspection, particularly
i.
Place the airplane in
a
hangar. wheel wells, flaps and control openings.
2. If the airplane cannot be placed in
a
hangar, b. If the engines have
a
total time of
more
than 25
tie, down securely
at
the three tie down points provided
on
the hours,
the
MIL-C-6529 oil (3, Chart
207, 91-00-00) shall be
airplane. Do
not
use
hemp
or
manila rope. It is recommended
drained after
a
ground warm-up. Fill with engine oil (2, Chart
a
tail
support be used to compress the
nose
strut
which will 207, 91-00-00) before flight.
It should be noted that
reduce the
wing angle of attack. Attach
a
line
to
the
nose gear.
MIL-C-6529 TYPE
II oil (3,
Chart
207, 91-00-00) is the TCM
(Teledyne Continental Motors) recommended break-in oil for
b. Engine.
the first 25 hours of flight.
c.
Prefiight
the airplane.
1.
Operate
the engine until the oil temperature
reaches the normal range. Drain the oil
supply
from the sump
TEMPORARY STORAGE
31 TO 90 DA YS
as
completely
as
possible and replace the drain plug.
2. Fill the
sump
to
the full mark
on
the oil
dipstick
a.
Mooring.
with
MIL-C-6529 TYPE
II oil (3,
Chart
207.91 -00-00). This will
mix with normal
oil,
is suitable
as a
lubricant and will
provide
1.
Place
airplane in hanger.
protection against
corrosion. 2. If the airplane
cannot
be placed in
a
hangar.
3. Run the engine
at
least five minutes
at
a
tie down securely
at
the three tiedown
points provided
on
the
speed between 1000 and 1200 rpm with the oil
temperature airplane.
Do not
use
hemp
or
manilla rope. It is recommended
and cylinder head
temperature
in the normal
operating
range.
a
tail
support
be used
to compress the
nose
strut which will
reduce the wing angle of attach. Attach
a
line
to
the
nose gear.
WARNING
b. Engine.
Before rotating the propeller blades, make certain
1.
Operate the
engine
until the oil
temperature
magneto start
switches
are
OFF, throttles
are
in
reaches the normal
range.
Drain the oil
supply
from the sump
the CLOSED position, and mixture controls
are
in
as
completely
as
possible and replace the drain plug.
the idle cut-off position. Always
stand clear
2.
Fill the sump
to
the full mark
on
the oil
dipstick
while turning the propellers,
with MIL-C-6529 TYPE II oil (3, Chart 207, 91-00-00). This will
mix with normal
oil,
is suitable
as a
lubricant and will
provide
4. Each
seven
days during flyable
storage,
the
protection against corrosion.
propellers
shall be rotated by hand without running the engine.
3.
Run the
engine
at
least five minutes
at
a
After rotating the engine six revolutions,
stop the
propeller 45"
speed between 1000 and 1200 rpm with the oil
temperature
to 90" from it's previous position,
and cylinder head
temperature
in the normal
operating
range.
5.
If
at
the end of
thirty days the airplane will not
4. Remove
top
and bottom spark plugs and
be removed from
storage,
the engine shall be started and
run,
atomize
spray
preservative
oil
(54,
Chart
207, 91-00-00)
The
preferred method will be to fly the airplane for
thirty through
upper
spark plug hole of each cylinder
with the
piston
minutes. If flying
the
airplane is
impractical,
a
ground
run
shall
in the down position. Rotate crankshaft
as
each pair of cylin-
be made of
thirty
minutes duration, and up to, but
not
exceed- ders is sprayed. Stop
crankshaft with
no
piston
at top
position.
ing normal oil and cylinder
temperatures.
5.
Re-spray each cylinder
without rotating
crankshaft. To thoroughly
cover
all surfaces of the
cylinder
c.
Fuel Cells. Fill fuel cells to capacity
to minimize fuel interior,
move
the nozzle of the
spray gun from the
top to
the
vapor and
protect
cell inner liners,
bottom of the cylinder.
10-10-00
Page 201
Nov 30/76