STEMME S6 Maintenance Manual

MAINTENANCE MANUAL
STEMME TSA-M
MAINTENANCE MANUAL
STEMME TSA-M
05-10-00
Page 02
and/or service life is intended) and will be notified by a new revision of this chapter.
(2) The TBO expires in each case of:
(a) impact stop (possible ground touch of the propeller);
(b) Non-observance of the periodical inspections as they are fixed in the Maintenance
Manual;
(c) non-authorized replacement of essential parts.
Damaging by ground contact, bird strike, stone strike or similar which require a „large
repair“, the manufacturer decides which parts of the complete drive system are affected and
if a repair may be practicable or if an overhaul or replacement have to be performed.
(3) Refer to latest issue of ROTAX Aicraft Engines TBO Service Bulletin (SB) “Extension of the
Time Between Overhaul (TBO)”, and to ROTAX Aircraft Engines Maintenance Manual for
ROTAX Engine Type 914F Serie.
(4) Refer to latest issue of the mt-propeller Service Bulletin No. 1.-( ), and to the mt-propeller
E-118 Operation and Installation Manual.
(5) Replacement is required after a heavy overloading (e.g. due to an accident), refer also to the
operating instructions of the manufacturer.
(6) All rubber parts of the engine Rotax 914F must be renewed. Subjected are the carburetor
venting hoses (between airbox and carburetor float chambers, between fuel pressure control
and pressure sensor), the air hoses between Turbo Charger and Airbox, the connecting hoses
on the compensating tube, the V-belt, all rubber hoses of the cooling system, and the rubber
diaphragms and the rubber flange on both carburetors.
(7) The installed aerotow release clutch type E22 by Tost company has to be overhauled by the
manufacturer every 10.000 actuations or every 2000 launches of aerotow (based on
assumption of about 5 actuations per launch in normal aerotow flight operation).
In case of more or less than 5 actuations per flight the permitted number of launches has to be
reduced or increased correspondingly, which lies in the responsibility of the aircraft holder.
The manufacturer recommends a general overhaul after 4 years. Refer to Operating Manual
for Tost Release E22 and service information provided by manufacturer to get further
information.
05-20-00
Page 01
SCHEDULED MAINTENANCE CHECKS
1. General
A. The inspection time intervals chart contained in this chapter provides the recommended intervals
at which maintenance and maintenance checks are to be carried out on the aircraft.
B. Inspections, preventive maintenance work and repairs must be carried out by qualified personnel.
In any case, the specific national laws and regulations are obligatory.
NOTE: Read maintenance instructions in the appropriate sections of this manual before carrying
out any adjustments.
WARNING: PRIOR TO ANY MAINTENANCE WORK SWITCH OFF MASTER SWITCH AND
IGNITION!
2. Inspection Intervals
A. The intervals for general maintenance depend on operating conditions, climate, hangarage, etc.
The types and intervals of the minimum scheduled maintenance established for the S6 are
indicated in the table below.
3. Definition Periodic Inspections
A. Periodic inspections are those which must be performed every 100, 200, 600 and 1000 engine
operating hours. They have to be carried out in accordance with the following S6 Inspection Time
Interval Chart.
This means for example that every 100 hr of operation (100, 200, 300 hr ...) a 100 hr check and all
200 hr (200, 400, 600 hr ...) additional checks as per maintenance interval chart must be carried out.
The same must be applied for the additional 600 hr and 1000 hr inspections.
B. For 100 hr periodic inspections marked additionally as (X) for annual inspection an inspection is to
be carried out periodically after every 100 engine operating hours or every 12 months, whichever
applies first.
C. The airframe periodic inspections must be performed every 100 flight hours of a/c (flight hours
documented in the a/c logbook).
D. Additional engine periodic inspections must be performed every 50 engine operating hours,
containing the following check points:
- 5.1.9 - 1; 5.1.11 - 6 (recommended for the engine by ROTAX)
- 5.1.10 - 5 and 6 (obligatory, if more than 30% of operation with leaded fuel, e.g. AVGAS
100 LL)
4. Definition Special Hours Inspections
A. In order to demonstrate continued airworthiness, the aircraft / engine must be inspected
additionally once after the first 25 engine operating hours or 100 flight hours, whichever applies
first. This applies to newly delivered and to overhauled aircrafts / engines.
Nov 18/11
May 04/12

STEMME S6 Specifications

General

Brand	STEMME
Model	S6
Category	Aircrafts
Language	English