STEMME S12 Maintenance Manual

STEMME
Aircrafts
Table of Contents
  • JUL 20, 2016

    2
  • Maintenance Instructions

    21
  • CHAPTER-PAGE

    22
  • Safety symbols

    26
  • Three view drawing

    33
  • Fuselage

    36
  • Control Elements and Instruments

    37
  • Controls at the Instrument Panel

    39
  • CHAPTER

    41
  • Flight Control System

    43
  • Control of Air Brakes

    44
  • Power-Plant

    45
  • Lubrication System

    46
  • Cooling System

    47
  • Air Induction System

    48
  • Fuel System

    49
  • Fuel System Design

    50
  • Electrical Layout and Operation of the Fuel Pumps

    51
  • Engine Controls and Instrumentation

    53
  • Propeller

    54
  • Design of Variable Pitch Propeller

    55
  • Propeller Weight Balance

    58
  • Expansion Element and Control System

    59
  • Identification of Propeller System and Assembly

    60
  • Operation Mechanism of the Propeller Folding System

    61
  • Propeller Brake

    62
  • Coolant Fluid

    64
  • Lubricants

    65
  • Landing Gear

    67
  • Tail Wheel

    68
  • Flight Control Instruments, Pitot Static System

    69
  • Electrical System

    71
  • DC Generation (ATA 24-30-00)

    73
  • Engine System DC Power Generation

    74
  • Over Voltage Protection

    75
  • DC Power Distribution System (ATA 24-60-00)

    76
  • Protection Devices

    77
  • Fuse and CB Specifications: Main System

    78
  • Fuse Specifications: Engine System

    79
  • Manual Switches

    80
  • Semiconductor Switch Box

    81
  • Instrument Panel Bus System

    83
  • Engine Starting System (ATA 80-00-00)

    84
  • Independently from the Aircraft

    85
  • Engine RPM Indicating System (ATA 77-14-00)

    86
  • Oil Pressure Indicating System (ATA 79-31-00)

    87
  • Operation

    88
  • Transfer Pump Control and Tank Selection

    89
  • Fuel Pressure Indicating (ATA 73-32-00)

    90
  • COM and NAV Equipment

    91
  • Oxygen System

    93
  • Wing Folding Device

    95
  • General

    98
  • Component Replacement and Overhaul Limitations

    99
  • Structural Limitations

    101
  • Time Limits / Maintenance Checks

    103
  • Airworthiness Limitations Section

    104
  • Pre-Flight Inspections

    109
  • Inspection Intervals

    110
  • General Remarks on Periodic Inspections

    112
  • Unscheduled Maintenance

    113
  • Special Conditions and Cautionary Notice

    114
  • Inspection Groups and Maintenance Criteria

    116
  • Other Particulars of Maintenance

    119
  • Check List for Periodic Inspections

    121
  • Wings and Fuel System Components in the Wing Center Section

    122
  • Forward Fuselage

    123
  • Cockpit

    124
  • Center Fuselage (except for fairings)

    125
  • Tail Boom

    126
  • Fuel System Components in the Fuselage

    127
  • Engine and Engine Mountings

    128
  • Cooling System (Liquid Cooling, Ram Air Cooling)

    131
  • Center Fuselage Fairing, Engine Cowlings and Firewall

    132
  • Drive Shaft with Propeller Reduction Gear

    134
  • Main Landing Gear

    135
  • 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
  • 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
  • Center Fuselage

    162
  • Vertical Tail

    163
  • Horizontal Tail

    164
  • 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
  • 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
  • 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
  • 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
  • Flight Control Instruments and Pitot and Static Pressure System

    205
  • Calibration of Stall Warning System (Optional)

    206
  • 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
  • Contents

    220
  • 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
  • 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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