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STEMME S12 User Manual
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DO
CUMENT
NUMBER:
L500-912.820 ISSU
E JUL 20, 2016
AMENDMENT:
00
D
AT
E
: î
î
CHAPTERî
P
AGE Dî1
MAINTENANCE MANUAL STEMME
S12
ANNEX
D:
MAINTENANCE
AND INSPECTION F
ORMS
This section pro
vides pat
terns o
f maintenance and inspection f
orms,
r
elevant t
o maintenance
according t
o sections
î6î and î7î.
234
236
Table of Contents
Jul 20, 2016
2
List of Effective Pages
5
Table of Contents
11
General
21
Maintenance Instructions
21
Remarks on Maintenance
21
Chapter-Page
22
Chapter-Page
23
Conversion Table
23
Abbreviations
24
Chapter-Page
24
Chapter-Page
25
Safety Symbols
26
Chapter-Page
27
Description
27
Chapter-Page
28
Technical Data
28
Chapter-Page
29
Chapter-Page
30
Chapter-Page
31
Chapter-Page
32
Three View Drawing
33
Chapter-Page
34
Airframe, Primary and Secondary Structure
35
Chapter-Page
35
Description of Assemblies
35
Wing
35
Cockpit
36
Fuselage
36
General
36
Tail Unit
36
Control Elements and Instruments
37
Controls at the Instrument Panel
39
Instrument Panel
39
Chapter
41
Flight Control System
43
Lateral Control
43
Longitudinal Control
43
Longitudinal Trim
43
Wing Flap Control System
43
Control of Air Brakes
44
Directional Control
44
Engine
45
Power-Plant
45
Lubrication System
46
Cooling System
47
Air Induction System
48
Engine Exhaust Incl. Turbocharger and Attachment
48
Fuel System
49
Fuel System Related Controls and Indication System
49
Fuel System Design
50
Fuel System of the Fuselage
50
Electrical Layout and Operation of the Fuel Pumps
51
Engine Controls and Instrumentation
53
Engine Cowlings
53
Fire Protection
53
Propeller
54
Design of Variable Pitch Propeller
55
Propeller Blade Angle Control Mechanism
55
Propeller Blades
55
Propeller Weight Balance
58
Expansion Element and Control System
59
Forward Propeller Reduction Gearbox
60
Identification of Propeller System and Assembly
60
Power Transmission
60
Nose-Cone
61
Operation Mechanism of the Propeller Folding System
61
Propeller Positioning
61
Fluids
62
Fuel
62
Propeller Brake
62
Coolant Fluid
64
Lubricants
65
Landing Gear
67
Main Landing Gear
67
Tail Wheel
68
Flight Control Instruments, Pitot Static System
69
Electrical System
71
General System Architecture
71
DC Generation (ATA 24-30-00)
73
Main System DC Power Generation
73
Engine System DC Power Generation
74
DC Indication (ATA 24-37-00)
75
Description
75
Operation
75
Over Voltage Protection
75
Parts Specification
75
DC Power Distribution System (ATA 24-60-00)
76
Design of Electrical Connections
76
Wire Specifications
76
Protection Devices
77
Fuse and CB Specifications: Main System
78
Fuse Specifications: Engine System
79
Switching Devices
79
Electromechanical Relays
80
Manual Switches
80
Engine System Distribution Box
81
Main System Distribution Box
81
Semiconductor Switch Box
81
TCU Board
81
Instrument Panel Bus System
83
Description
84
Engine Starting System (ATA 80-00-00)
84
Operation
84
Parts Specification
84
Description
85
Engine Ignition System (ATA 74-00-00)
85
Independently from the Aircraft
85
Cylinder Head Temperature Indicating System (ATA 77-22-00)
86
Description
86
Engine RPM Indicating System (ATA 77-14-00)
86
Operation
86
Parts Specification
86
Description
87
Oil Pressure Indicating System (ATA 79-31-00)
87
Oil Temperature Indicating System (ATA 79-33-00)
87
Operation
87
Parts Specification
87
Description
88
Fuel Distribution System (ATA 28-20-00)
88
Operation
88
Parts Specification
88
Description
89
Fuel Quantity Indication (ATA 28-40-00)
89
Operation
89
Parts Specification
89
Transfer Pump Control and Tank Selection
89
Description
90
Fire Detection System (ATA 26-12-00)
90
Fuel Pressure Indicating (ATA 73-32-00)
90
Operation
90
Parts Specification
90
COM and NAV Equipment
91
Oxygen System
93
3.10 Wing Folding Device
95
General
98
Maintenance Limitations
98
Paint Finish
98
Component Replacement and Overhaul Limitations
99
Structural Limitations
101
Time Limits / Maintenance Checks
103
Overhaul and Replacement Schedule
104
Periodic Inspections
109
Pre-Flight Inspections
109
Rubber Hose and Clamp Integrity
109
Inspection Intervals
110
General Remarks on Periodic Inspections
112
Unscheduled Maintenance
113
General Remarks on Maintenance
114
Special Conditions and Cautionary Notice
114
Inspection Groups and Maintenance Criteria
116
Other Particulars of Maintenance
119
Check List for Periodic Inspections
121
General
121
Wings and Fuel System Components in the Wing Center Section
122
Forward Fuselage
123
Cockpit
124
Center Fuselage (Except for Fairings)
125
Empennage
126
Tail Boom
126
Fuel System Components in the Fuselage
127
Engine and Engine Mountings
128
Lubrication System
130
Air Induction System
131
Cooling System (Liquid Cooling, Ram Air Cooling)
131
Engine Controls & Monitoring
131
Center Fuselage Fairing, Engine Cowlings and Firewall
132
Propeller
133
Drive Shaft with Propeller Reduction Gear
134
Main Landing Gear
135
Tail Wheel
136
Electric System (Except for Engine and TCU)
137
Completion Tasks
138
Optional Equipment
139
Special Inspections
141
Inspection Following Exceptional Events with Wing Folding Device
142
Maintenance Instructions, Tolerances, Adjustment Data for the Aircraft
143
Determination of Empty Weight and Corresponding Center of Gravity; Weight Limits
145
Flight Control System
150
Friction in Control System
151
Weights and Moments of Control Surfaces
152
Lubrication
153
Lubrication Plan
154
Surface of Composite Structures
155
Drainage and Ventilation Holes
157
Data for Assemblies / Equipment
159
Flaps and Ailerons
160
Fuselage
161
Center Fuselage
162
Vertical Tail
163
Horizontal Tail
164
Cockpit
165
Re-Installation of the Canopy
166
Equipment and Systems
167
Controls
168
Controls in the Wing
169
Deflection of Control Surfaces, Control System Friction, Control Forces
170
Power-Plant
171
Removal and Installation of the Engine
172
Cleaning of the Engine
173
Check of Gearbox
174
Check of Engine Wiring
175
Test Run of Engine
176
Oil Level Check
177
Flushing of Cooling System
178
Ram Air Cooling
179
Exhaust Headers
180
Fuel System in the Wing
182
Fuel System in the Fuselage
183
Engine Controls / Monitoring
184
Fire Protection
186
Fire Protective Sleeves
187
Propeller
188
Adjustment and Inspection Results, Tolerances
189
Removal of the Propeller Unit
190
Installation of the Propeller Unit
191
Spring Tension of the Propeller Folding Mechanism
192
Checking of Pitch Control and Adjusting the Variable Pitch Propeller
193
General Aspects of the Electrical Circuit
194
Drive Shaft System
195
Propeller Gearbox, Mounting and Support
196
Propeller Operation
198
Main Landing Gear
199
Functional Test of the Retractable Landing Gear
200
Functional Check of Emergency Undercarriage Extension
202
Tires, Condition and Inflation Pressure
203
Replacement of Brake Lining
204
Tail Wheel
204
Flight Control Instruments and Pitot and Static Pressure System
205
Calibration of Stall Warning System (Optional)
206
Electrical System
207
Grounding
208
Communication and Navigation Equipment
209
List of Placards and Their Positions
211
Placards in the Cockpit, Rear
216
Placards on Fuselage
217
Equipment
219
Supplementary Equipment
221
Optional Systems
223
List of Special Tools
225
Annex B: Service Bulletins, Airworthiness Directives
231
Annex C: Documents (Inspection and Operation Reports)
233
Control Surface Deflections
241
Annex F: Technical Drawings
253
Jul 20, 2016
254
A) Flight Controls: Pitch Control and Trim
255
B) Flight Controls: Lateral Control (Wing, Flap, Aileron)
257
C) Flight Controls: Airbrake Control
259
D) Flight Controls: Rudder Control
261
E) Propulsion System
265
F) S12 Main System - DC Generation
267
G) S12 Main System - Landing Gear
269
H) S12 Main System - Electrical Trim
271
I) S12 Main System - Autopilot
273
J) S12 Main System - Fire Warning
275
K) S12 Main System - Lighting
277
L) Transponder and Traffic Display
279
M) S12 Main System - Communication Radio
281
N) S12 Engine System - DC Generation
283
O) S12 Engine System - Engine Monitoring and Control
285
P) S12 Engine System - Fuel Pumps and Indication
287
Q) S12 Engine System - Propeller Control
289
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STEMME S12 Specifications
General
Brand
STEMME
Model
S12
Category
Aircrafts
Language
English
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