STEMME S10 Service Manual

Maintenance Manual STEMME S10 Date of Issue: Oct. 01, 1990 page: 29
Amendment No.: 18 Date: Oct. 15, 2012
A4010021_B19.doc Doc.No.: A40-10-021
Inspection Type
Type and Subject of Inspection
Type 1a
Type 1b
Type 2 Type 3
5.3.13 Electrical System
1.
Inspect wiring and conduits for improper routing, insecure mounting and
obvious defects, electrical components for tightness of fit and poor condition.
X
2.
Inspect the main battery
for poor condition (check drop in voltage during starter
operation). For battery maintenance refer to manufacturer instructions.
X
5.3.14 Radio and Navigation Equipment
1.
Inspect radio and navigation equipment (refer to the Equipment List) for poor
condition, improper operation and, if applicable, service life limits.
X
2.
Check each antenna installed X
5.3.15 Oxygen System
1.
Inspect oxygen system, if installed, including mounting. Observe Maintenance
Instructions of the Manufacturer (Annex A).
X
5.3.16 Completition works
1.
After end of maintenance on the drive train system – Engine check run X X X X

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.