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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: 42 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
Check the fluid level in the nose landing gear hydraulic
shock strut. Remove the upper screw located in the strut.
Fluid level must be up to the threaded hole.
X X
Replace the fluid in the nose gear hydraulic shock strut.
X
Check the nose gear hydraulic shock strut function, by
pressing the nose down and release.
O O O O
Check the shock strut piston for abnormal play, both
Transversal and longitudinal. Should be 2
– 3 mm Max.
Check for no free play between pedals and Nose wheel.
X
Check nose wheel and tire condition. Inflation pressure
32 psi (2.2 bar).
O
O O
Support the aircraft. Remove the main landing gear
wheels and check the brake linings for wear. Replace
lining if necessary.
X X
Remove the main landing gear RH and LH struts. Clean
the strut housings in the tubular framework. Clean the
axle assemblies. Lubricate strut housings for corrosion
prevention. Check struts for alignment.
X
Reinstall the main landing gear struts and check the nuts
for tightness, both to wheel axle and to frame.
X
Check main landing gear RH and LH struts installation
on fuselage for tightness and safety.
X
Check the brake hydraulic line from the master cylinder
to the brake piston for condition and support attachment.
Replace if necessary.
O
O O
Drain the brake hydraulic fluid. Refill with fresh fluid
X
Check self-locking nuts for tightness
X X
Check brake disc condition, replace if necessary. Check
brake self-locking nuts for tightness.
X X
Check main wheel and tire condition. Inflation pressure
18 psi or ( 1.8 bar).
O
O O
Reinstall the wheels. Check nut for tightness and safety
X X
Ensure that wheel bearings are not noisy and turn freely
and smoothly without play.
X X
Check main wheel alignment.
X
X X
Install strut and wheel fairing
X X
ENGINE
All Engine maintenance is to be performed according to
ROTAX Maintenance manual 899 372, Section. 05-20-
00. This maintenance schedule assumes use of lead free
fuel only in Rotax.
This maintenance schedule covers only the airframe
manufacturer installation of the Rotax in the engine
compartment.
X X X X