39
Provincial Road n.78 Km 12.150
33050 Mortegliano (UD) – Italy
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Maintenance Manual
FLY SYNTHESIS TEXAN
TOP CLASS 580 ISR
(For Rotax 912 ULS
versions)
Identification: MM_TC_580_Rev.2
Page: 39 of 77
Date: 15/02/11
Issued: C. Cosatto
Verified: C. Cosatto
Approved: C. Cosatto
Revision Description:
Placard update
TYPE
TASKS TO BE PERFORMED
25
50
100
200
PROPELLER
Remove spinner
X
X X
Inspect the prop blade for cracks, stone damage and
other defects. For small defects, smooth with fine glass
paper and apply lacquer or epoxy as required.
X X X X
Check propeller bolt tightness, see propeller manual for
Torque value, check safe tying if required.
X
X X
Install spinner
X
X X
FUSELAGE
Inspect fuselage for condition and other sign of defect.
Check skin for delamination, inner structure bulkheads
seen to be to be glued to skin with no cracks or
separation between them.
O O O O
Exterior check main landing gear frame (steel tube spar)
for condition, no cracks. Check four points of connection
to fuselage structure, no delamination or skin separation,
check retaining bolts and nuts tightness
(this check can be made with special video equipment)
X
X
Internal check main landing gear frame (steel tube spar)
to fuselage for condition, no cracks. Check four points of
connection to fuselage structure, no delamination or skin
separation, bolts and nuts tightness (
floor below the
seat must be removed, part TB0200, unless suitable
special video equipment is used for inspection
).
X
X
Internal check main landing gear frame (steel tube spar)
to fuselage for condition, no cracks. Check four points of
connection to fuselage structure, no delamination or skin
separation, bolts and nuts tightness (
floor below the
seat must be removed, part TB0200
)
X
Check antenna attachment, check for cracks, loose Bolt,
connecting cable condition and security and antenna
condition.
O O O O
Check wing main spar connection in centre fuselage for
bolts tightness, no cracks (
floor below the seat must
be removed, part TB0200, unless suitable special
video equipment is used for inspection
).
X
X
Check wing main spar connection in centre fuselage for
bolts tightness, no cracks (
floor below the seat must
be removed, part TB0200
).
X
Check four wing fuselage connections for bolts tightness,
condition of fuselage spars
X
X X
Front windshield, clean and check condition, check
attachment to the structure
O O O O
Canopy, clean & check condition check connection to the frame,
check locks operation, lubricate lightly locks mechanism
O O O O