STEMME S6

MAINTENANCE MANUAL
STEMME TSA-M
MAINTENANCE MANUAL
STEMME TSA-M
Page 04
05-20-00
Page 05
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)
Reference Initials
Motor 100h Motor 25h
Airframe
100h
Motor 200h Motor 600h Motor 1000h
Annual
Type and Subject of Inspection
No.
3. Check security and condition of drive gear
cowlings. Clearance allowed (all around):
1 +1.0, -0.5 mm / 0.04 + 0.04, -0.02 in
1. Inspect canopy for damage and check proper
function of locking mechanism, grease canopy
locks. Clearance allowed (all around):
2 ± 1.0 mm / 0.08 ± 0.04 in
2. Canopy emergency jettison: Check function.
3. Check function of lateral canopy gas springs
(canopy must remain in open position).
4. Check seat belts and their attachments.
5. Check controls in front fuselage for foreign objects,
condition and proper installation.
6. Check condition and security of all instruments,
switches, circuit breakers, fuses and wiring.
7. Check condition and integrity of ventilation hoses.
8. Check rudder pedals and control cables. Check
provisions for pedal adjustment.
Play allowed (at rudder, with pedals fixed,
measured in direction of movement):
max. 2.5 mm / 0.1 in
9. Check condition, security and adjustment
mechanism of the seats.
1. Check condition of center fuselage steel frame
(corrosion, deformation). Check paint for cracks.
2. Check condition of framework/tailboom
connection.
3. Check condition of upper and lower connection
framework / front fuselage.
5.1.5 Center Fuselage (except for fairings)
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
5.1.4 Cockpit
Reference Initials
Motor 100h Motor 25h
Airframe
100h
Motor 200h Motor 600h Motor 1000h
Annual
Type and Subject of Inspection
No.
5.1.3 Front Fuselage
3. Check vent line outlets at end ribs of central wing.
4. Check function and leak tightness of quick-release
couplings (supply lines) to and from fuselage.
5. Check all fuel filters and replace if required.
6. Check fuel filler cap for leakage and wing for any
signs of wing fuel tank leakage.
7. Check condition and backlash of wing fittings,
check safety device of wing attachment bolts.
Maximum play allowed for all wing bolts:
Axial: 0.4 mm / 0.016 in
Radial: 0.15 mm / 0.006 in
For front and aft shear force bolts (inner wing -
outer wing, outer wing - winglet) only radial play is
allowed.
8. Check condition, security and function of fuel
pumps (located under the spar).
9. Check condition of wing flaps and ailerons, check
clearance between components spanwise 3 ± 0.5
mm / 0.12 ± 0.02 in., check gap sealings and fairings
on flap/aileron links, check security of axial stops.
10. Check entire control linkage and bearings in the
center wing and in the wing attachment area,
verify the spring pin on each quick-connector is
attached securely.
11. Inspect bell-crank levers and adjacent components
of wing flap and aileron control system.
12. Check condition of airbrakes.
Clearance between cover strap and wing shell
(spanwise, overall): 4 ± 0.5 mm / 0.16 ± 0.02 in
1. Check condition and security of drive gear
attachment.
2. Verify the gap between Center wing and fuselage is
at least 2 ± 0.5 mm / 0.08 ± 0.02 in.
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
(X)
X
X
X
Nov 18/11
Nov 18/11