MAINTENANCE MANUAL
STEMME TSA-M
MAINTENANCE MANUAL
STEMME TSA-M
Page 06
05-20-00
Page 07
05-20-00
* ROTAX Maintenance Manual (ref. 00-00-00, 2.A), Cha./para.
** mt-propeller, E-118 (ref. 00-00-00, 2.A), /para.
(1) if more than 30% of operation with leaded fuel (AVGAS 100 LL)
* ROTAX Maintenance Manual (ref. 00-00-00, 2.A), Cha./para.
** mt-propeller, E-118 (ref. 00-00-00, 2.A), /para.
(1) if more than 30% of operation with leaded fuel (AVGAS 100 LL)
Nov 18/11
Nov 18/11
1. Check condition of supply, return and drain lines
outside the engine compartment, supply and
return lines inside the engine compartment.
2. Check condition, security and function of fuel
pumps.
3. Replace main fuel pump. (acc. to ROTAX)
4. Check fuel shut-off valve. Inspect firewall
feedthroughs of the fuel supply and return lines for
security and leakage.
5. Check condition of fire protective sleeves on fuel
supply and return lines in the engine compartment.
1. General visual inspection of engine and auxiliaries
for damage, abnormalities and leakage.
2. Check friction torque in free rotation of engine gear
box.
3. Inspect overload clutch.
4. Check of the engine gear box.
5. Check of fuel filters, renew if necessary.
6. Check idle speed.
7. Inspect float chamber assembly for contamination
and corrosion at minimum one time a year.
8. Check of carburetors with inspection of ventilation
of the float chambers and disassembling/assembling
for checking.
9. Check carburetor synchronization.
5.1.9 Engine and Engine Mounts
X
X
X
X
(X)
(X)
(X)
(X)
(X)
(X)
(X)
(X)
(X)
X
X
X
X
X
X
X
X
X
X
X
(1)
X
X
X
R* 05-20-00
28-20-00
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R* 05-20-00
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R* 05-20-00
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R* 05-20-00
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5.1.8 Fuel System Components in the Fuselage
Reference Initials
Motor 100h
Motor 25h
Airframe
100h
Motor 200h
Motor 600h
Motor 1000h
Annual
Type and Subject of Inspection
No.
4. Check condition and security of landing gear
attachment.
5. Check condition of entire control linkage in the
center fuselage.
6. Main battery: Check electrical terminals, condition
and security of mounting tray.
1. Visual inspect members of elevator control looking
into the forward and aft end of tail boom.
2. Visual inspect members of rudder control looking
into the forward and aft end of tail boom.
3. Check trim control system.
4. Check tail skid for security and wear.
5. Check attachment of ballast compartment for
cracks.
6. Check baggage compartment door for correct
closure.
7. Check attachment points in the baggage
compartment for security.
1. Check rudder system and fittings for condition and
security. Play allowed (hinges):
only axial: 0.4 ± 0.1 mm / 0.016 ± 0.004 in
2. Check backlash in fittings of horizontal stabilizer
when installed.
Maximum play allowed for front and aft fitting:
Axial: 0.15 mm / 0.006 in
Radial: 0.15 mm / 0.006 in
3. Check gap sealings and zigzag tape on the
empennage.
5.1.6 Tail Boom
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
Reference Initials
Motor 100h
Motor 25h
Airframe
100h
Motor 200h
Motor 600h
Motor 1000h
Annual
Type and Subject of Inspection
No.
5.1.7 Empennage
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