MAINTENANCE MANUAL
STEMME TSA-M
MAINTENANCE MANUAL
STEMME TSA-M
Page 12
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)
Page 13
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)
1. Check condition of pressure system , renew
filters/water separators if required.
2. Check condition and function of flight instruments
(refer to equipment list).
1. Check wiring of the electric system.
2. Check condition of all electrical devices installed.
3. Check condition and function of all switches.
4. Check condition of all ground terminals.
5. Visually check electric distribution box.
1. Check NAV and COM equipment for proper
installation and security and compare to equipment
list.
2. Check condition, function and, if applicable, service
life limits of NAV and COM equipment (refer to
records of operating times).
3. Check all antennas installed.
X
X
X
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X
5.1.20 Electrical System (except for engine and TCU)
5.1.21 COM / NAV Equipment
5.1.19 Flight Instrumentation and Pressure Systems
Reference Initials
Motor 100h
Motor 25h
Airframe
100h
Motor 200h
Motor 600h
Motor 1000h
Annual
Type and Subject of Inspection
No.
1. Remove main gear fairings and inspect for
damages.
2. Verify the bearings of the wheel shoes are free
moveable.
3. Inspect the main gear legs and trailing arms for
deformation and possible cracks as a result of an
excessive load.
4. Check condition of main gear tires and creep
markings. Check tire pressure: 3.5 ± 0.1 bar / 51.0
± 1.5 p.s.i.
5. Check function of rocking arm spring damping
system.
6. Check wheel bearings for freedom of movement
and excessive play.
7. Check brake master cylinder and wheel brake
cylinders incl. hoses and lines.
8. Check brake discs and brake linings
(at least 1,5 mm / 0.06 in.).
9. Check quantity of brake fluid.
10. Renew brake fluid (DOT 4) if indicated.
1. Remove fairings and inspect for damages.
2. Check condition of nose gear tire and check tire
pressure: 3.5 ± 0.2 bar / 51.0 ± 3.0 p.s.i.
3. Visually inspect wheel fork for cracks or
deformations.
4. Check function of wheel fork damping system.
12-15-00
12-15-00
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(X)
X
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X
Reference Initials
Motor 100h
Motor 25h
Airframe
100h
Motor 200h
Motor 600h
Motor 1000h
Annual
Type and Subject of Inspection
No.
5.1.17 Main Landing Gear (Fix L/G)
5.1.18 Nose Landing Gear (Fix L/G)
Nov 18/11
Nov 18/11
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