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STEMME S10 Service Manual

STEMME S10
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Maintenance Manual STEMME S10
Date of Issue: Oct. 01, 1990 page: 37
Amendment No.: - Date: -
A4010021_B19.doc
Doc.No.: A40-10-021
7.3.6 Controls/Instruments
The bowden cables for power and choke setting can be adjusted on the carburettors and/or at the
attachments to the power and choke control levers in the cockpit.
The power plant instruments do not require maintenance. Summary: see Equipment List.
Zero calibration of the cylinder head temperature indicator is based on 20°C (temperature of the refer ence
point, i.e. the soldered joints connecting the lines from the instrument to the thermocouples inside the
fuselage).
7.3.7 Fire Protection
Retouching of damaged coating: Remove damaged area down to the laminate, apply three layers of fire
protection paint and cover with clear varnish.
7.3.8 Engine Cowlings
Sealings on air ducts must be in close contact with the engine and oil cooler respectively. Replace them in
case of embrittlement.
7.3.9 Propeller
Tolerances:
Track of propeller joints (blade suspension) with reference to the position "upper left transmission gear
mounting": maximum difference of 0.012 in. (0.3 mm) between both joints.
Track of propeller blade tips: maximum difference of 0.12 in. (3 mm) between the blades.
Play of blade tips in flight direction: maximum of 0.16 in. (4 mm) total.
Unbalance: Basic Balancing by the manufacturer. Precission balancing by a knowledgeable person by
adjusting the compensation masses at the blade root by a maximum of 1.13 dr. (2 g).
Removal of the propeller:
Removal of the propeller dome: lift off left and right leg room covering in the cockpit. Loosen clamping
screw on the stay tube of the propeller dome, pull out locking screw, remove static pressure hoses,
withdraw propeller dome to the front.
Loosen fastening screws, remove propeller.
Installation of the propeller:
Clean and degrease the propeller and the transmission gear flange with an appropriate solvent. The
torque is transmitted by friction fit, therefore, the surfaces must be even, clean and free from grease.
Inspect threaded bushes in the transmission gear flange for visible damage.
Tighten the fastening screws by means of a torque wrench in two steps:
1st step: tightening torque: 74 lbft. (10 Nm);
2nd step: tightening torque: 220 lbft. (30 Nm).
Afterwards, lock 3 screws at a time with a safety wire.
Check the tolerances.

Table of Contents

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STEMME S10 Specifications

General IconGeneral
Wingspan23.0 m (75 ft 6 in)
Max Takeoff Weight850 kg (1, 874 lb)
ManufacturerStemme AG
First Flight1986
Crew1
Capacity1 passenger
Length8.42 m
EngineRotax 914
Power Output60 kW (80 hp)
Maximum Speed270 km/h
Propellers2-bladed
Service Ceiling6, 096 m (20, 000 ft)
CategorySailplane
Never Exceed Speed270 km/h
PowerplantSingle piston engine
Number BuiltMore than 250

Summary

1. General Remarks on Maintenance

2. Brief Description and Technical Data

Wing

Technical specifications and construction details of the aircraft wing.

Air Brakes

Description and dimensions of the Schempp-Hirth air brakes.

Wing Flaps

Details on the wing flaps, including span, area, and positions.

3. Description of Assemblies

3.1 Cell, Primary and Secondary Structures

Describes the primary and secondary structural components of the airframe.

3.2 Control System

Details the aircraft's control systems, including longitudinal, lateral, and directional.

3.3 Power Plant

Information on the engine, fuel system, oil system, cooling, induction, and exhaust.

3.4 Landing Gear

Description and operational details of the main and tail landing gear.

4. Airworthiness Limitations Section

5. Time Limits / Maintenance Checks

5.1 Life-Limited Components

Refers to airworthiness limitations for parts with prescribed service life limits.

5.2 Pre- Flight Checks

Instructions for conducting pre-flight checks as per the Flight Manual.

5.3 Periodical Checks, Inspection Lists

Outlines intervals and types of periodical checks for aircraft maintenance.

6. Maintenance Instructions, Tolerances, Adjustment Data for the Aircraft

6.2 Ground Towing, Supporting Points, and Lifting of Aircraft

Procedures for ground handling, supporting, and lifting the aircraft safely.

6.3 Determination of the Empty Mass and Corresponding Center of Gravity

Methods for determining aircraft empty mass and center of gravity.

7. Maintenance Instructions, Tolerances, Adjustment Data for Assemblies / Equipment

7.1 Airframe

Maintenance instructions for the airframe, including wing and fuselage.

7.3 Power Plant

Maintenance procedures for the engine, fuel, oil, and other powerplant systems.

7.4 Landing Gear

Maintenance procedures for the main and tail landing gear systems.

9. Equipment

9.1 Minimum Equipment List

Lists the minimum required equipment for aircraft operation.

9.3 Additional Equipment and Systems

Information on optional and supplementary equipment that can be installed.

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