Maintenance Manual STEMME S10-VT
Date of Issue: Jan. 01, 1998
Page vi
Amendment No. 23
Date: Jan. 29, 2015
A4011121_B23.doc
Doc. No. A40-11-121
0.3 Contents
0.1
Record of Amendments
ii
0.2
List of Effective Pages
iv
0.3
Contents
vi
1.
General Remarks on Maintenance
1-1
1.1
Conversion table
1-2
1.2
Abbreviations
1-2
2.
Brief Description and Technical Data
2-1
3.
Description of Assemblies
3-1
3.1
Airframe, Primary and Secondary Structure
3-1
3.1.1
Wing
3-1
3.1.2
Fuselage
3-1
3.1.3
Tail Unit
3-2
3.2
Cockpit 3-2
3.2.1
General
3-2
3.2.2
Control Elements and Instruments
3-3
3.3
Flight Control System
3-8
3.4
Power Plant (Fig. 3.4.a)
3-17
3.4.1
Engine
3-17
3.4.2
Lubrication System
3-19
3.4.3
Cooling System
3-19
3.4.4
Air Induction System
3-20
3.4.5
Engine Exhaust incl. Turbocharger and Attachment
3-20
3.4.6
Fuel System (Fig. 3.4.6)
3-21
3.4.7
Engine Controls and Instrumentation
3-23
3.4.8
Fire Protection
3-23
3.4.9
Engine Cowlings
3-23
3.4.10
Propeller (Fig. 3.4.10.a/b/c)
3-24
3.4.11
Power Transmission
3-27
3.4.12
Front gear
3-27
3.4.13
Operation Mechanism of the Propeller Folding System
3-28
3.4.14
Operating Media
3-29
3.5
Landing Gear
3-31
3.5.1
Main Landing Gear (Fig. 3.5.1)
3-31
3.5.2
Tail Wheel
3-31
3.6
Flight Control Instruments, Pitot Static System (Fig. 3.6.a,b)
3-33
3.7
Electrical System
3-35
3.7.1
General
3-35
3.7.2
Wiring
3-35
3.7.3
Bus-Structure of the Electrical System
3-35
3.7.4
Structure of Grounding
3-36
3.7.5
Generation of Electric Energy
3-36
3.7.6
Engine Electric
3-37
3.7.7
Engine Monitoring
3-37
3.7.8
Instruments on the Instrument Panel
3-38
3.7.9
Warning, Caution and Status Lights on the Instrument Panel:
3-38
3.7.10
Fuses and Circuit Breakers (CB´s):
3-39
3.7.11
Switches on the Instrument Panel:
3-39
3.7.12
Variable Pitch Propeller
3-41
3.7.13
Main Landing Gear
3-41
3.7.14
Landing Gear Warning System
3-41
3.7.15
Avionics
3-41
3.8
COM and NAV Equipment
3-55
3.9
Oxygen System
3-55
