STEMME S10 Service Manual

Stemme AG – Flugplatzstrasse F2 Nr. 7 – D-15344 Strausberg
A4010021_B19.doc Doc.No.: A40-10-021
MAINTENANCE MANUAL
for the powered sailplane STEMME S 10
Document No. A40-10-021
Date of Issue: October 1, 1990
Translation and conversion of technical data have been done by best knowledge and judgement.
In any case the original version in the German language is authoritative
Model: STEMME S 10 Serial number: 10-
Type Certificate: EASA.A.054 (former LBA 846) Registration:
Non-standard equipment or systems with effect to the contents of this manual, if
installed, are entered in the table on page 1.
Druck-Info: Datei enthält 64 Seiten gesamt

STEMME S10 Specifications

General

Wingspan	23.0 m (75 ft 6 in)
Max Takeoff Weight	850 kg (1, 874 lb)
Manufacturer	Stemme AG
First Flight	1986
Crew	1
Capacity	1 passenger
Length	8.42 m
Engine	Rotax 914
Power Output	60 kW (80 hp)
Maximum Speed	270 km/h
Propellers	2-bladed
Service Ceiling	6, 096 m (20, 000 ft)
Category	Sailplane
Never Exceed Speed	270 km/h
Powerplant	Single piston engine
Number Built	More 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.