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King Air B200/B200GT/250 Pro Line 21 Aircraft Systems Pilot Training Manual Vol. 2 - Rev 0.3 PDF
King Air B200/B200GT/250 Pro Line 21 Aircraft Systems Pilot Training Manual Vol. 2 - Rev 0.3 PDF - Image 2
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King Air B200/B200GT/250 Pro Line 21 Aircraft Systems Pilot Training Manual Vol. 2 – Rev 0.3 PDF

Original price was: $39.95.Current price is: $24.95.

A 490-page FlightSafety International Pilot Training Manual, Volume 2 – Aircraft Systems, for the King Air B200/B200GT/250 with Pro Line 21. Revision 0.3, May 2014, covers airframe and aircraft systems, PT6A-42/52 powerplants, Pro Line 21 avionics, maneuvers and procedures, weight and balance, crew resource management, walkaround material, terminology, and chapter review questions. This manual is intended for familiarization and training purposes.

SKU: HD-KA-B200-B200GT-250-PL21-V2-R03 Category: Tags: , , , Vendor: Lube Chart Manuals
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Description

King Air B200/B200GT/250 Pro Line 21 Aircraft Systems Pilot Training Manual Vol. 2 – Rev 0.3 PDF

This 490-page training reference is Volume 2, Aircraft Systems, of the FlightSafety International King Air B200/B200GT/250 with Pro Line 21 Pilot Training Manual. Revision 0.3 is dated May 2014. It brings together aircraft-system descriptions, cockpit controls and indications, operating principles, limitations, diagrams, training questions, flight profiles, weight-and-balance instruction, and crew resource management material in one substantial volume.

The King Air B200/B200GT/250 Pro Line 21 Aircraft Systems Pilot Training Manual Vol. 2 – Rev 0.3 PDF is designed for familiarization and training. The manual itself states that its material is based on information obtained from the aircraft manufacturer’s Airplane Flight Manual, Pilot Manual, and Maintenance Manuals, and that manufacturer or FAA publications take precedence if a conflict exists. That distinction is important for buyers: this is an in-depth pilot training manual, not a substitute for the approved aircraft flight manual or maintenance documentation.

File Details

  • Manual type: Pilot Training Manual, Volume 2 – Aircraft Systems
  • Models: King Air B200, B200GT and 250 with Pro Line 21
  • Engine coverage: PT6A-42 and PT6A-52
  • Revision: 0.3
  • Date: May 2014
  • Language: English
  • Page count: 490 pages
  • File format: PDF

Aircraft Systems and Training Scope

The manual begins by orienting the pilot to the aircraft, its structure and major systems. It then develops each system in dedicated chapters. Electrical coverage explains DC and AC power, the battery, starter-generators, distribution, controls, indications and generator limitations. Fuel-system material follows the main and auxiliary systems through pumps, filters, heating, transfer, crossfeed, fueling and operating limitations. Powerplant coverage goes much deeper, describing the PT6A-42/52 engine sections, lubrication, engine fuel control, ignition, propeller governing, feathering, autofeather and the engine indicating system.

System knowledge is reinforced with a large number of illustrations and schematics. Examples include electrical distribution, fuel routing, the PT6A engine cutaway, oil-system flow, ignition circuits, propeller governor operation, fire detection and extinguishing, pneumatic routing, landing-gear extension, brake hydraulics and cockpit layouts. The Pro Line 21 chapter is particularly extensive, covering flight instruments and displays, integrated avionics processing, air data and attitude/heading references, reversionary operation, flight guidance, the control display unit, flight management, GPS, communication/navigation equipment and additional installed or optional avionics functions.

Complete PDF Bookmark Tree

Complete Bookmarks

The complete bookmarks in the “King Air B200/B200GT/250 Pro Line 21 Aircraft Systems Pilot Training Manual Vol. 2 – Rev 0.3 PDF” are as follows:

Coverp. 1
Noticep. 2
List of Effective Pagesp. 4
Table of Contentsp. 6
Chapter 1 Aircraft Generalp. 7
Contentsp. 7
Introductionp. 10
Generalp. 10
Aircraft Systemsp. 11
Electrical Power Systemp. 11
Lightingp. 11
Master Warning Systemp. 12
Fuel Systemp. 12
Powerplantp. 12
Fire Detection and Protectionp. 13
Bleed-Air Systemp. 14
Ice and Rain Protectionp. 14
Air Conditioning and Heatingp. 15
Pressurizationp. 15
Landing Gear and Brakesp. 16
Flight Controlsp. 17
Oxygen Systemp. 18
Aircraft Structuresp. 18
Fuselagep. 21
Doorsp. 24
Emergency Exitp. 26
Cabin Windowsp. 27
Control Locksp. 27
Illustrationsp. 8
Figure 1-1. External Power Socketp. 11
Figure 1-2. Overhead Light Control Panelp. 11
Figure 1-3. Fuel Control Panelp. 13
Figure 1-4. Bleed-Air Valves Controlp. 14
Figure 1-5. Ice Protection Switches—Pilot Right Subpanelp. 14
Figure 1-6. Windshield Wipers Control Switchp. 15
Figure 1-7. Parking Brake Handlep. 16
Figure 1-8. Flight Control Surfacesp. 17
Figure 1-10. Flap Control Leverp. 18
Figure 1-9. Trim Tab Controls and Indicationsp. 18
Figure 1-11. Cockpit Oxygen Handlesp. 18
Figure 1-12. King Air B200/B200GT Aircraft Dimensionsp. 19
Figure 1-13. King Air 250/250C Aircraft Dimensionsp. 20
Figure 1-14. Fuselage Stations and Compartmentsp. 21
Figure 1-15. Cockpit Layout (Prior to BB-1988)p. 22
Figure 1-16. Cockpit Layout (BB-1988 and Subsequent, and BY-1 and Subsequent)p. 23
Figure 1-17. Cabin Doorp. 24
Figure 1-18. Door Handlesp. 24
Figure 1-19. Placard and Inspection Portp. 25
Figure 1-20. Latch Boltp. 25
Figure 1-21. Cargo and Airstair Doorsp. 26
Figure 1-22. Emergency Exit Release Handlesp. 26
Figure 1-23. Control Locksp. 27
Tablesp. 9
Table 1-1. Cabin Altitudesp. 15
Chapter 2 Electrical Power Systemsp. 28
Contentsp. 28
Introductionp. 31
DC Power Systemp. 31
Descriptionp. 31
Componentsp. 32
Controls and Indicationsp. 39
Operationp. 40
AC Power Systemp. 41
Descriptionp. 41
Controls and Indicationsp. 41
Operationp. 42
Limitationsp. 42
Generator Limitsp. 42
Startersp. 42
Circuit Breakersp. 42
Emergency/Abnormalp. 42
Questionsp. 50
Illustrationsp. 29
Figure 2-1. Electrical Component Locationp. 32
Figure 2-2. Hot Battery Busp. 33
Figure 2-3. Volt-Loadmeters-Battery Ammeterp. 33
Figure 2-4. Electrical Distributionp. 34
Figure 2-5. Circuit Breaker Panels—Pilotp. 35
Figure 2-6. Circuit Breaker Panels—Copilotp. 36
Figure 2-7. Starter-Generatorp. 37
Figure 2-8. Generator Control Circuitp. 37
Figure 2-9. External Power Socket (Receptacle)p. 38
Figure 2-10. Electrical Control Switchesp. 39
Figure 2-11. Starter Switchesp. 39
Figure 2-12. Avionics Power Distributionp. 40
Figure 2-13. Loadmetersp. 40
Figure 2-14. Annunciatorsp. 41
Figure 2-15. Inverterp. 41
Figure 2-16. Copilot Left Subpanelp. 41
Tablesp. 30
Table 2-1. Limitations—Ground Operationsp. 42
Table 2-2. Circuit Breakersp. 43
Chapter 3 Lightingp. 52
Contentsp. 52
Introductionp. 54
Generalp. 54
Interior Lightingp. 55
Cabinp. 55
Cockpitp. 56
Controls and Indicationsp. 58
Exterior Lightsp. 59
Landing Lightsp. 59
Taxi Lightp. 60
Wing Ice Lightsp. 60
Navigation Lightsp. 60
Recognition Lightsp. 60
Beacon Lightsp. 60
Tail Floodlightsp. 60
Strobe Lightsp. 60
Airstair Floodlightp. 61
Understep Lightingp. 61
Questionsp. 62
Illustrationsp. 53
Figure 3-1. Threshold Lightp. 55
Figure 3-2. Fluorescent Light Switchp. 55
Figure 3-3. Passenger Warning Signsp. 56
Figure 3-4. Reading Lightsp. 56
Figure 3-5. Overhead Lighting Controlsp. 57
Figure 3-6. Copilot Subpanelsp. 57
Figure 3-7. Pilot Subpanelp. 58
Figure 3-8. Instrument Indirect Lightsp. 58
Figure 3-9. FREE AIR TEMP Gaugep. 59
Figure 3-10. Landing and Taxi Lightsp. 59
Figure 3-11. Exterior Lightsp. 60
Figure 3-12. Airstair Floodlightp. 61
Figure 3-13. Understep Lightingp. 61
Chapter 4 Master Warning Systemp. 63
Contentsp. 63
Introductionp. 65
Generalp. 65
Componentsp. 68
Dim Modep. 68
Test Modep. 68
Glareshield Flashersp. 68
Warning Annunciator Panel (Red)p. 68
Caution/Advisory Annunciator Panel (Amber/Green)p. 70
Emergency/Abnormalp. 70
Questionsp. 72
Illustrationsp. 64
Figure 4-1. Component Locations (Sheet 1 of 2)p. 66
Figure 4-2. MASTER WARNING and MASTER CAUTION Flashersp. 68
Figure 4-3. Warning Annunciator Panelp. 69
Figure 4-4. Caution/Advisory Annunciator Panelp. 70
Tablesp. 64
Table 4-1. Warning Annuciatorsp. 69
Table 4-2. Caution/Advisory Annunciatorsp. 71
Chapter 5 Fuel Systemp. 73
Contentsp. 73
Introductionp. 76
Generalp. 76
Main and Auxiliary Fuel Systemsp. 77
Componentsp. 77
Firewall Shutoff Valvep. 77
Engine-Driven Boost Pumpp. 79
Standby Boost Pumpp. 80
Firewall Fuel Filterp. 80
Fuel Heaterp. 80
High-Pressure Engine Fuel Pumpp. 81
Fuel Manifold Clearingp. 81
Controls And Indicationsp. 82
Low Fuel Pressure Switchp. 82
Fuel Flow Transmitter and Indicationsp. 83
Operationp. 83
Routing to the Enginep. 83
Auxiliary Fuel Transfer Systemp. 83
Fuel Crossfeed Systemp. 85
Fuelingp. 86
Limitationsp. 86
Approved Fuel Grades and Operating Limitationsp. 86
Approved Fuel Additivesp. 87
Fueling Considerationsp. 88
Zero-Fuel Weightp. 88
Emergency/Abnormalp. 88
Questionsp. 89
Illustrationsp. 75
Figure 5-1. Fuel System Schematicp. 78
Figure 5-2. Fuel Pressure Warning Lightsp. 79
Figure 5-3. Fuel Control Panelp. 80
Figure 5-4. Fuel Purge Systemp. 81
Figure 5-5. Fuel Flow Indicationsp. 83
Figure 5-6. Auxiliary Fuel Transfer Systemp. 84
Figure 5-7. Fuel Crossfeed Systemp. 85
Figure 5-8. FUEL CROSSFEED Annunciatorp. 86
Figure 5-9. Fuel Temperature (OAT) Versus Minimum Oil Temperature Graphp. 87
Tablesp. 75
Table 5-1. Drain Locationsp. 82
Chapter 6 Auxiliary Power Systemp. 90
Chapter 7 Powerplantp. 91
Contentsp. 91
Introductionp. 95
Generalp. 95
Enginep. 96
Descriptionp. 96
Major Sectionsp. 96
Operationp. 99
Engine Lubrication Systemp. 100
Componentsp. 100
Controls and Indicationsp. 101
Operationp. 101
Engine Fuel Systemp. 103
Componentsp. 103
Controls and Indicationsp. 103
Operationp. 103
Engine Ignition Systemp. 106
Descriptionp. 106
Componentsp. 106
Controls And Indicationsp. 106
Operationp. 107
Propellerp. 108
Descriptionp. 108
Controls and Indicationsp. 109
Operationp. 111
Powerplantp. 113
Engine Indicating System (EIS)p. 116
Propeller Featheringp. 118
Limitationsp. 122
Approved Fuelsp. 122
Propellerp. 123
Powerplant Engine Indicating System Colorsp. 125
Emergency/Abnormalp. 127
Questionsp. 130
Illustrationsp. 93
Figure 7-1. King Air B200/B200GTp. 96
Figure 7-2. PT6A Enginep. 97
Figure 7-3. Engine Cutawayp. 97
Figure 7-4. Compressor Bleed Valve(s)p. 98
Figure 7-5. Engine Stationsp. 100
Figure 7-7. CHIP DETECT Annunciatorsp. 101
Figure 7-6. Oil Pressure/Temperature Indicationsp. 101
Figure 7-8. Oil System Schematicp. 102
Figure 7-9. Fuel Low Pressure Annunciatorsp. 103
Figure 7-10. Fuel Flow Indicatorsp. 103
Figure 7-11. Simplified Fuel Control Schematicp. 104
Figure 7-12. IGNITION AND ENGINE START Switchesp. 106
Figure 7-13. ENG AUTO IGN Switchesp. 107
Figure 7-14. Ignition System Schematicp. 107
Figure 7-15. Propellerp. 108
Figure 7-16. PROP GOV TEST Switchp. 110
Figure 7-17. Propeller Onspeed Schematicp. 111
Figure 7-18. Overspeed Governor Schematicp. 112
Figure 7-19. Propeller Overspeed Schematicp. 112
Figure 7-20. Propeller Underspeed Schematicp. 113
Figure 7-21. Powerplant Control Leversp. 114
Figure 7-22. Beta and Reverse Controlp. 115
Figure 7-23. Propeller Control Leverp. 115
Figure 7-24. Friction Control Knobsp. 116
Figure 7-25. Engine Indicating Systemp. 117
Figure 7-26. Propeller Synchroscopep. 118
Figure 7-27. Propeller Synchroscope and Switches (Type II)p. 118
Figure 7-28. Type II System Schematicp. 119
Figure 7-29. AUTOFEATHER Switchp. 119
Figure 7-30. AUTO FEATHER Annunciatorsp. 120
Figure 7-31. Autofeather System Schematic (Both Power Levers at Approximately90% N1; Right Engine Has Failed)p. 121
Figure 7-32. Autofeather Test Schematic (Left Power Lever Below 200 Foot-Pounds; Right Power Lever Above 400 Foot-Pounds)p. 122
Tablesp. 94
Table 7-1. Engine Operating Limits (PT6A-42 Engine)p. 124
Table 7-2. Power Plant Instrument Markings (PT6A-42 Engine)p. 126
Table 7-3. Engine Operating Limits (PT6A-52 Engine)p. 128
Chapter 8 Fire Protectionp. 131
Contentsp. 131
Introductionp. 133
Fire-Detectionp. 134
Componentsp. 134
Controls and Indicationsp. 134
Fire-Extinguishingp. 134
Controls and Indicationsp. 134
Operationp. 134
System Testingp. 137
Portable Fire Extinguishersp. 138
Limitationsp. 138
Emergency/Abnormalp. 138
Questionsp. 139
Illustrationsp. 132
Figure 8-1. Fire-Detection Systemp. 135
Figure 8-2. Fire-Extinguishing Systemp. 136
Figure 8-3. Gauge Locationp. 137
Figure 8-4. Portable Fire Extinguisherp. 138
Tablesp. 132
Table 8-1. Temperature Vs. Pressure Datap. 137
Chapter 9 Pneumaticsp. 140
Contentsp. 140
Introductionp. 142
Generalp. 142
Descriptionp. 144
Pneumatic and Vacuum Systemsp. 144
Bleed-Air Warning Systemp. 145
Door Seal Systemp. 146
Controls And Indicationsp. 147
Limitationsp. 147
Emergency/Abnormalp. 147
Questionsp. 148
Illustrationsp. 141
Figure 9-1. Pneumatic and Vacuum Systemsp. 143
Figure 9-2. Bleed-Air Ejectorp. 144
Figure 9-3. VACUUM and PNEUMATIC PRESSURE Gaugesp. 144
Figure 9-4. Bleed-Air Warning System Diagramp. 145
Figure 9-5. L and R BL AIR FAIL Warning Annunciatorsp. 145
Figure 9-6. BLEED AIR VALVE Switchesp. 146
Figure 9-7. Pneumatic Plastic Tubingp. 146
Figure 9-8. Cabin Door Air Sealp. 147
Figure 9-9. FLIGHT Hourmeterp. 147
Chapter 10 Ice and Rain Protectionp. 149
Contentsp. 149
Introductionp. 151
Generalp. 151
Ice Protection—Pneumatic Sourcep. 152
Wing and Horizontal Stabilizer Deice Systemp. 152
Brake Deice Systemp. 155
Ice Protection—Electrical Sourcep. 157
Windshield Heatp. 157
Controls and Indicationsp. 158
Propeller Heatp. 158
Pitot Heatp. 160
Stall Warning Vane Heatp. 161
Fuel Vent Heatp. 161
Fuel Control Unit Heat (Prior to BB–1988)p. 162
Miscellaneous Systemsp. 162
Powerplantp. 162
Controls and Indicationsp. 162
Raisbeck Ram Air Recovery Systemp. 164
Windshield Wipersp. 164
Wing Ice Lightsp. 165
Limitationsp. 165
Emergency/Abnormalp. 167
Questionsp. 168
Illustrationsp. 150
Figure 10-1. Weather-Protected Aircraft Surfacesp. 152
Figure 10-2. Ice and Rain Protection Controls and Indicationsp. 153
Figure 10-3. Wing and Horizontal Stabilizer Deice Boots System Controlsp. 154
Figure 10-4. Brake Deice Systemp. 156
Figure 10-5. Windshield Anti-Ice Systemp. 157
Figure 10-6. Propeller Electrical Deice Controls and Indicatorsp. 159
Figure 10-7. Pitot Tubes, Stall Warning Vane, and Heat Controlsp. 160
Figure 10-8. Heated Fuel Vent and Controlsp. 161
Figure 10-9. Powerplant Intake Ice Protectionp. 163
Figure 10-10. Engine Intake Inertial Vane Positions and Bypass Doorp. 164
Figure 10-11. WINDSHIELD WIPERS Knobp. 165
Figure 10-12. Wing Ice Inspection Light and Controlp. 165
Chapter 11 Air Conditioningp. 170
Contentsp. 170
Introductionp. 172
Generalp. 172
Prior To SN BB-1988p. 174
Componentsp. 174
Controls And Indicationsp. 176
BLEED AIR VALVES Switchesp. 177
CABIN TEMP MODE Knobp. 177
AIR COND N1 LOW Annunciatorp. 178
BL AIR OFF L–R Annunciatorsp. 178
Operationp. 179
SN BB-1988 and Subsequent, SN BY-1 and Subsequentp. 181
Componentsp. 181
Controls and Indicationsp. 183
BLEED AIR VALVES Switchesp. 183
COCKPIT and CABIN TEMP Control Knobsp. 186
Operationp. 188
Limitationsp. 190
Emergency/Abnormalp. 190
Questionsp. 191
Illustrationsp. 171
Figure 11-1. Air Conditioning System (Prior to BB-1988)p. 173
Figure 11-2. Condenser and Receiver-Dryer Sight Gaugep. 174
Figure 11-3. Air Conditioner Condenser Intakep. 174
Figure 11-4. Floor and Ceiling Outletsp. 175
Figure 11-5. Cockpit Eyeball Outletsp. 175
Figure 11-6. Air Conditioning System Control Diagramp. 176
Figure 11-7. ENVIRONMENTAL Panelp. 177
Figure 11-8. CABIN TEMP MODE Control Knobp. 177
Figure 11-9. MANUAL TEMP INCR-DECR Switch/ELECT HEAT–OFF Switchp. 178
Figure 11-10. Annunciator Panelp. 178
Figure 11-11. Condenser and Receiver-Dryer Sight Gaugep. 181
Figure 11-12. Cockpit Heating Air Outletsp. 182
Figure 11-13. Floor and Ceiling Outletsp. 182
Figure 11-14. Cockpit Eyeball Outletsp. 182
Figure 11-15. Air Conditioning System Control Diagramp. 184
Figure 11-16. Air Conditioning System (BB-1988 and Subsequent and BY-1 and Subsequent)p. 185
Figure 11-17. ENVIRONMENTAL Panelp. 186
Figure 11-18. Environmental Control System Knobp. 186
Figure 11-19. COCKPIT and CABIN BLOWER Control Knobsp. 186
Figure 11-20. Annunciator Panelp. 188
Chapter 12 Pressurizationp. 192
Contentsp. 192
Introductionp. 194
Generalp. 194
Componentsp. 196
Flow Control Unit (FCU)p. 196
Controls and Indicationsp. 198
BLEED AIR VALVES Switchesp. 198
ENVIR BLEED AIR Switch (BB-1988 and Subsequent, BY-1 and Subsequent)p. 198
Pressurization Controllerp. 198
CABIN ALT Gaugep. 199
CABIN CLIMB Gaugep. 199
CABIN PRESS DUMP Switchp. 199
L–R BL Air Off Annunciatorp. 199
ALT WARN Annunciatorp. 200
Operationp. 200
Preflight Operationp. 200
In-Flight Operationp. 200
Descent and Landing Operationp. 200
Limitationsp. 201
Questionsp. 202
Illustrationsp. 193
Figure 12-1. Pressurization Controlsp. 195
Figure 12-2. Electronic Flow Control Unitp. 196
Figure 12-3. Outflow Valvep. 197
Figure 12-4. Safety Valvep. 198
Figure 12-5. Pressurization Controllerp. 199
Figure 12-6. CABIN ALT Gaugep. 199
Figure 12-7. CABIN CLIMB Gaugep. 199
Figure 12-8. CABIN PRESS DUMP Switchp. 200
Figure 12-9. ALT WARN Annunciatorp. 200
Tablesp. 193
Table 12-1. Pressurization Controller Setting—Landingp. 201
Chapter 13 Hydraulic Power Systemp. 203
Chapter 14 Landing Gear And Brakesp. 204
Contentsp. 204
Introductionp. 206
Generalp. 206
Landing Gearp. 207
Descriptionp. 207
Componentsp. 207
Controls and Indicationsp. 210
Operationp. 213
Normal Retractionp. 213
Nosewheel Steeringp. 215
Descriptionp. 215
Operationp. 215
Brake Systemp. 218
Operationp. 218
Care And Handling In Cold Weatherp. 219
Preflightp. 219
Taxiingp. 219
Limitationsp. 219
Airspeed Limitationsp. 219
Emergency/Abnormalp. 219
Questionsp. 220
Illustrationsp. 205
Figure 14-1. Hydraulic Power Packp. 207
Figure 14-2. Components Locationsp. 208
Figure 14-3. Hydraulic Landing Gear Systemp. 208
Figure 14-4. Nose Gear Assemblyp. 209
Figure 14-5. Internal Nose Gear Lockp. 209
Figure 14-6. Main Gear Assemblyp. 210
Figure 14-7. Main Gear Door Mechanism (Standard Gear)p. 211
Figure 14-8. Main Gear Do or Mechanism (High-Flotation Gear)p. 211
Figure 14-9. Landing Gear Control Handle and Indicator Lightsp. 212
Figure 14-10. Normal Indications Gear Downp. 212
Figure 14-11. Normal Indications, Gear Upp. 212
Figure 14-13. Normal Indications, Gear Upp. 213
Figure 14-12. Normal Indications Gear Downp. 213
Figure 14-14. Normal Retractionp. 214
Figure 14-15. Normal Extensionp. 216
Figure 14-16. Alternate Extensionp. 217
Figure 14-17. Brake System Schematicp. 218
Chapter 15 Flight Controlsp. 222
Contentsp. 222
Introductionp. 224
Generalp. 224
Flight Controlsp. 225
Componentsp. 225
Rudder Boost Systemp. 226
Controls and Indicationsp. 226
Operationp. 227
Yaw Damping Systemp. 227
Trim Systemp. 228
Elevator Electric Trimp. 228
Descriptionp. 229
Controls and Indicationsp. 230
Limitationsp. 232
Maneuver Limitsp. 233
Maximum Operating Pressure-Altitude Limitsp. 233
Flight Load Factor Limits at 12,500 Poundsp. 233
Emergency/Abnormalp. 233
Questionsp. 234
Illustrationsp. 223
Figure 15-1. Flight Controls and Trim Tabsp. 225
Figure 15-2. Flight Control Locksp. 225
Figure 15-3. Rudder Boost Diagramp. 226
Figure 15-4. RUDDER BOOST Switchp. 227
Figure 15-5. Autopilot and Yaw Damp Switchesp. 227
Figure 15-6. Trim System Controlp. 228
Figure 15-7. E and A Indicatorsp. 228
Figure 15-8. Split Flap Protectionp. 229
Figure 15-9. Flap Control and Indicationp. 230
Figure 15-10. Flap Control and Indicationp. 231
Chapter 16 Avionicsp. 235
Contentsp. 235
Introductionp. 245
Flight Instrumentsp. 245
Primary Flight Display (PFD)p. 246
Multifunction Display (MFD)p. 257
Display Control Panels (DCP)p. 260
Integrated Avionics Processor System (IAPS)p. 267
Air Data Computers (ADC)p. 268
Attitude And Heading Reference System (AHRS)p. 268
Reversionary Operationsp. 269
Pitot and Static Systemp. 273
Outside Air Temperaturep. 274
Stall Warning Systemp. 275
Flight Guidance System (FGS)p. 276
Flight Guidance Computers (FGC)p. 277
Flight Guidance Panel (FGP)p. 277
Control Wheel Switchesp. 283
Control Display Unit (CDU)p. 285
Flight Management System (FMS)p. 290
FMS Initializationp. 291
Vertical Navigationp. 291
Global Positioning System (GPS)p. 293
Integrated Flight Information System (IFIS)p. 294
Cursor Control Panel (CCP)p. 298
Electronic Charts (E-CHARTS) [Optional]p. 301
Graphical Weather (GWX) [Optional]p. 304
Communication/Navigation Systemsp. 309
Audio Systemp. 312
Radio Tuning Unit (RTU)p. 315
HF Operation (Optional)p. 318
TCAS II Operation (Optional)p. 318
CDU Tuningp. 319
Electronic Standby Instrument System (ESIS)p. 323
Weather Radar Systemp. 326
Cockpit Voice Recorder (CVR)p. 330
Emergency Locator Transmitter (ELT)p. 330
Enhanced Ground Proximity Warning System (EGPWS)p. 331
Basic Ground Proximity Warning System (GPWS)p. 331
Enhanced Ground Proximity Warning System (EGPWS)p. 333
Terrain Awareness and Warning System (TAWS+)p. 335
Basic Ground Proximity Warnings (Reactive)p. 335
Enhanced Ground Proximity Warnings (Predictive)p. 336
Traffic Collision and Avoidance System (TCAS I)p. 339
Traffic Collision and Avoidance System (TCAS II) (OPTIONAL)p. 342
Appendix A—Avionics Equipment Locationsp. 347
Appendix B—Flight Guidance Modesp. 349
Appendix C—Avionics Acronymsp. 351
Questionsp. 353
Illustrationsp. 237
Figure 16-1. Adaptive Flight Displays (AFD)p. 246
Figure 16-2. Primary Flight Displayp. 247
Figure 16-3. Attitude Displayp. 248
Figure 16-4. Airspeed Displayp. 248
Figure 16-5. Trend Vectorp. 248
Figure 16-6. Low Speed Cuep. 249
Figure 16-7. High Speed Cuep. 249
Figure 16-8. Airspeed Bugp. 249
Figure 16-9. Acceleration Displayp. 250
Figure 16-10. Altimeter Displayp. 250
Figure 16-11. Altitude Negativep. 250
Figure 16-12. Baro Switchp. 251
Figure 16-13. Vertical Speed Indicator (VSI)p. 251
Figure 16-14. Altitude Preselect Bugsp. 251
Figure 16-15. Metric Altitudep. 252
Figure 16-16. BARO ALT Switchp. 252
Figure 16-17. Heading and Navigation Displayp. 252
Figure 16-18. DME Holdp. 253
Figure 16-20. PFD Arc Formatp. 254
Figure 16-19. PFD Compass Rose Formatp. 254
Figure 16-21. PFD Map Formatp. 254
Figure 16-22. Terrain and Radar Overlay Sectionp. 255
Figure 16-23. PFD TCAS Message Area (Non-IFIS)p. 255
Figure 16-24. PFD Lower Display Informationp. 255
Figure 16-25. Pilot's MFD Displayp. 256
Figure 16-26. Non-IFIS MFD Checklistp. 258
Figure 16-27. MFD Upper Format (IFIS)p. 258
Figure 16-28. MFD Plan Formatp. 259
Figure 16-29. MFD TCAS Onlyp. 260
Figure 16-30. MFD Lower Display Informationp. 260
Figure 16-31. Display Control Panelsp. 261
Figure 16-32. Display Control Panel (DCP)p. 261
Figure 16-33. Barometric Setting With Yellow Underlinep. 261
Figure 16-34. IN/hPa Switchp. 262
Figure 16-35. Barometric Setting with STDp. 262
Figure 16-36. PFD REFS Menu Page 1 of 2p. 262
Figure 16-37. PFD V-Speedsp. 263
Figure 16-38. Radio Altitude Minimump. 264
Figure 16-39. Barometric Minimump. 264
Figure 16-40. Minimums Annunciatorp. 264
Figure 16-41. PFD REFS Menu Page 2 of 2p. 265
Figure 16-42. Metric Altitudep. 265
Figure 16-43. Flight Director Formatsp. 265
Figure 16-44. PFD NAV BRG Menup. 266
Figure 16-45. Bearing Pointer Informationp. 267
Figure 16-46. IAPSp. 267
Figure 16-47. ADCp. 268
Figure 16-48. AHRSp. 268
Figure 16-49. Heading Slave and Slewp. 269
Figure 16-50. AFD Reversionsp. 269
Figure 16-51. Reversionary Modesp. 270
Figure 16-52. ADC1 Failurep. 271
Figure 16-53. ADC Miscomparep. 271
Figure 16-54. ADC Switch—ADC2 Selectedp. 271
Figure 16-55. AHRS1 Failurep. 272
Figure 16-56. AHRS Miscomparep. 272
Figure 16-57. AHRS Switch—AHRS2 Selectedp. 272
Figure 16-58. Pitot Tubesp. 273
Figure 16-59. Static Portsp. 273
Figure 16-60. Alternate Static Source Selectionp. 273
Figure 16-61. System Integrationp. 274
Figure 16-62. OAT Gaugep. 275
Figure 16-63. Rosemont Probep. 275
Figure 16-64. Transducer Vanep. 275
Figure 16-65. STALL WARN TEST Switchp. 275
Figure 16-66. Stall Warning Heatp. 276
Figure 16-67. Flight Guidance Panel (FGP)p. 276
Figure 16-68. Flight Guidance System Displayp. 277
Figure 16-69. Flight Guidance Couple Arrowp. 277
Figure 16-70. Indepandant Flight Director Operationp. 278
Figure 16-71. YD/AP Disconnect Barp. 278
Figure 16-72. Heading Vector Linep. 279
Figure 16-73. Half Bank Modep. 279
Figure 16-74. APPR Mode Selectionp. 280
Figure 16-75. Localizer Nav-to-Nav Capturep. 281
Figure 16-76. VNAV Glidepath (GP) Modep. 281
Figure 16-77. APPR Mode Selectionp. 282
Figure 16-78. Flight Level Change (FLC) Modep. 282
Figure 16-79. Left Yokep. 284
Figure 16-80. Pilot's PFD with SYNCp. 284
Figure 16-81. GO AROUND Buttonp. 284
Figure 16-82. PFD Go-Around (GA) Modep. 285
Figure 16-83. Control Display Unit (CDU)p. 285
Figure 16-84. Active Flight Plan Pagep. 287
Figure 16-85. Active Legs Pagep. 287
Figure 16-86. Direct to Pagesp. 287
Figure 16-87. Hold FLPN Modep. 288
Figure 16-88. MFD Menu Key (CDU)p. 289
Figure 16-89. MFD Advance Key (CDU)p. 289
Figure 16-90. MFD Text Pagep. 289
Figure 16-91. Database Unitsp. 290
Figure 16-92. Active Legs Page with VNAV Altitudesp. 291
Figure 16-93. VNAV Top of Descentp. 292
Figure 16-94. VNAV Modesp. 293
Figure 16-95. GPS CONTROL Pagep. 294
Figure 16-96. PROGRESS Pagep. 294
Figure 16-97. IFS Block Diagramp. 295
Figure 16-98. Ethernet Database Unitp. 296
Figure 16-99. USB Database Unit (DBU-5000)p. 296
Figure 16-100. MCDU Menup. 296
Figure 16-101. IFS Dataload Block Diagramp. 297
Figure 16-102. CCPp. 298
Figure 16-103. MFD Store Completep. 298
Figure 16-104. Geo-Political Overlayp. 299
Figure 16-105. Airspace Overlayp. 299
Figure 16-106. Airsways Overlayp. 300
Figure 16-107. Database Effectivity (STAT Key)p. 300
Figure 16-108. STAT Menup. 301
Figure 16-109. Chart Subscription (STAT Key)p. 301
Figure 16-110. MFD Chart Displayp. 301
Figure 16-111. MFD Chart Menup. 302
Figure 16-112. MFD Chart Approach Indexp. 302
Figure 16-113. MFD Chart Zoom Chartp. 303
Figure 16-114. MFD Chart Geo-Reference Symbolsp. 303
Figure 16-115. MFD PLAN Map Weather Overlayp. 304
Figure 16-116. MFD Dedicated Graphical Weather Format (XM Weather)p. 305
Figure 16-117. MFD XM Weather Menup. 305
Figure 16-118. MFD Metar Displayp. 305
Figure 16-119. Graphical Weather Overlay Selections (IFIS v 6.0)p. 306
Figure 16-120. Overlay Legendsp. 306
Figure 16-121. MFD Graphical Weather Time Stampsp. 306
Figure 16-122. MCDU Datalink Pages (Universal Weather)p. 307
Figure 16-123. Datalink Weather Selections (Universal Weather)p. 308
Figure 16-125. MFD Dedicated Graphical Weather Format (Universal Weather)p. 308
Figure 16-124. MFD Plan Map Weather Overlayp. 308
Figure 16-126. Universal Weather Menup. 309
Figure 16-127. RTU / CDU TUNE switchp. 309
Figure 16-129. Antennasp. 310
Figure 16-128. Emergency Frequency Buttonp. 310
Figure 16-130. RMT Tune Switchp. 311
Figure 16-131. PFD DME Displaysp. 311
Figure 16-132. DME Hold Selection and Imagesp. 311
Figure 16-133. ATC Transponder Switchp. 312
Figure 16-134. Flight ID Selectionp. 312
Figure 16-135. Audio panelsp. 312
Figure 16-136. Audio System Componentsp. 313
Figure 16-137. Control Wheel (PTT) Switchesp. 314
Figure 16-138. Radio Tuning Unit (RTU)p. 315
Figure 16-139. RTU in Preset Tuning Modep. 315
Figure 16-140. RTU COMM Pagesp. 316
Figure 16-141. RTU NAV Pagesp. 316
Figure 16-142. RTU ADF Pagesp. 317
Figure 16-143. RTU ATC Pagep. 317
Figure 16-144. RTU HF Pagesp. 318
Figure 16-145. RTU TCAS II Pagesp. 318
Figure 16-146. CDU Tune with TCAS Ip. 319
Figure 16-147. CDU Frequency Datap. 319
Figure 16-148. CDU COMM Pagep. 320
Figure 16-149. CDU NAV Pagep. 320
Figure 16-150. CDU ATC Pagep. 320
Figure 16-151. CDU ADF Pagep. 321
Figure 16-152. CDU TUNE With TCAS IIp. 321
Figure 16-153. MFD TCAS Displayp. 321
Figure 16-154. CDU TCAS II Controlp. 322
Figure 16-155. CDU HF Controlp. 322
Figure 16-156. Radio Tuning Unit (RTU)p. 323
Figure 16-157. Static Wicksp. 323
Figure 16-158. ESIS Displayp. 323
Figure 16-159. ESIS Power Switchp. 324
Figure 16-160. ESIS Menup. 325
Figure 16-161. PFD Radar Menup. 326
Figure 16-162. Test Modep. 326
Figure 16-163. Radar Ground Map Modep. 327
Figure 16-164. Radar Display with Path Attenuation Barp. 327
Figure 16-165. Radar Display Turbulence Modep. 327
Figure 16-166. Turbulence Only Displayp. 328
Figure 16-167. Radar Gain Displayp. 328
Figure 16-168. Pilot's PFD with TGTp. 328
Figure 16-170. Radar Tilt Displayp. 329
Figure 16-169. Radar Ground Clutter Supressionp. 329
Figure 16-171. CVR Controllersp. 330
Figure 16-172. ELT Manual Switchp. 330
Figure 16-174. GPWS Failure Annunciatorsp. 331
Figure 16-173. PFD GND PROX and PULL UP Annunciatorsp. 331
Figure 16-175. EGPWS Buttonsp. 333
Figure 16-176. EGPWS Terrain Displayp. 334
Figure 16-177. EGPWS Terrain Fail and TERR Annunciatorsp. 334
Figure 16-179. TAWS Failure Annunciatorsp. 335
Figure 16-178. PFD GND PROX and PULL UP Annunciatorsp. 335
Figure 16-180. TAWS Buttonsp. 337
Figure 16-181. TAWS Terrain Displayp. 337
Figure 16-182. Terrain Advisory Line (TAL)p. 338
Figure 16-183. Avoid Terrain Warningp. 338
Figure 16-184. Terrain Fail and TERR Annunciationsp. 339
Figure 16-185. TCAS I TESTp. 340
Figure 16-186. Operating Mode Buttonp. 340
Figure 16-187. TCAS II Testp. 342
Figure 16-188. Overview of Avionics Unitsp. 347
Tablesp. 244
Table 16-1. GPWS Cautions and Warningsp. 332
Table 16-2. EGPWS Buttonsp. 333
Table 16-3. EGPWS Cautions and Warningsp. 334
Table 16-4. Basic Cautions and Warningsp. 336
Table 16-5. TAWS Buttonsp. 337
Table 16-6. TAWS+ Cautions and Warningsp. 338
Table 16-7. TCAS Messagesp. 343
Table 16-8. TCAS II Annunciatorsp. 343
Table 16-9. TCAS II Traffic Advisoryp. 344
Table 16-10. TCAS II Resolution Advisoriesp. 344
Chapter 16A Wide Area Augmentation System (WAAS)p. 355
Contentsp. 355
Introductionp. 358
Generalp. 358
Operationp. 360
Integrityp. 360
Departuresp. 360
Enroutep. 360
Arrivalsp. 361
Approachesp. 361
Degraded SBAS Integrity During LPV Approachp. 365
Missed Approachp. 366
Lateral Guidancep. 366
FMS Quick Referencep. 368
Select SBAS Providerp. 368
Load LPV Approachp. 368
Failure of SBAS During LPV Approachp. 369
Failure of SBAS During LNAV/VNAV Approachp. 371
Load LNAV/VNAV Approach with WAAS (RARE)p. 372
Load Non-GPS Approachp. 372
Navigation Integrityp. 373
Raim Predictionp. 373
Rockwell Collins FMS Differencesp. 374
Questionsp. 375
Tablesp. 357
Table 16A-1. Loss of Integrityp. 360
Table 16A-2. Non-WAAS/WAAS Differencesp. 374
Illustrationsp. 356
Figure 16A-1. Worldwide SBAS Providersp. 359
Figure 16A-2. SBAS Service Providersp. 361
Figure 16A-3. Check SBAS Providerp. 361
Figure 16A-4. Approach Loadingp. 362
Figure 16A-5. Approach Selectionp. 362
Figure 16A-6. Arrival Datap. 363
Figure 16A-7. NON-WGS-84 Airportp. 363
Figure 16A-8. WAAS Channel Numberp. 363
Figure 16A-9. PFD Annunciations LPV Approachp. 364
Figure 16A-10. Course To Final Approach Messagep. 364
Figure 16A-11. SBAS Failure Messagesp. 365
Figure 16A-12. VNAV Flagp. 365
Figure 16A-13. Changing VNAV Guidancep. 366
Figure 16A-14. PFD Annunciations LPV Approachp. 366
Figure 16A-15. Loss of Nonprecision Approach RAIMp. 366
Figure 16A-16. Rockwell Collins WAAS FMS (Version 4.0)p. 367
Figure 16A-17. Select SBAS Providerp. 368
Figure 16A-18. LPV Approachp. 368
Figure 16A-19. Failure of SBAS During LPV Approachp. 369
Figure 16A-20. Load LNAV/VNAV or LNAV Approachp. 371
Figure 16A-21. RAIM Failure after SBAS Failurep. 371
Figure 16A-22. LNAV/VNAV Approach with WAASp. 372
Figure 16A-23. Load Non-GPS Approachp. 373
Figure 16A-24. Navigation Integrityp. 373
Figure 16A-25. RAIM Predictionp. 374
Chapter 17 Oxygen Systemp. 376
Contentsp. 376
Introductionp. 378
Generalp. 378
Crew Oxygenp. 380
Controls and Indicationsp. 380
First Aid Oxygenp. 380
Controls and Indicationsp. 380
Passenger Oxygenp. 381
Controls And Indicationsp. 382
Limitationsp. 383
Emergency/Abnormalp. 383
Questionsp. 384
Illustrationsp. 377
Figure 17-1. Oxygen Systemp. 379
Figure 17-2. Oxygen Mask Stowedp. 380
Figure 17-3. Oxygen Mask Selectorp. 380
Figure 17-4. First Aid Mask Access Panelp. 381
Figure 17-5. Oxygen System Push-Pull Handlesp. 381
Figure 17-6. Oxygen Bottle and Shutoff Valvep. 381
Figure 17-7. Passenger Oxygen Mask Deployedp. 382
Figure 17-8. Oxygen System Annunciatorsp. 382
Figure 17-9. Oxygen Available with Partially Full Bottlep. 383
Chapter 18 Water and Wastep. 385
Contentsp. 385
Introductionp. 387
Toiletp. 388
Relief Tubesp. 388
Emergency/Abnormalp. 388
Questionsp. 389
Illustrationsp. 386
Figure 18-1. Toiletp. 388
Figure 18-2. Relief Tubep. 388
Chapter 19 Maneuvers and Proceduresp. 390
Contentsp. 390
Introductionp. 393
Flight Maneuversp. 394
Takeoffp. 394
Landingp. 394
WindShearp. 395
Microburstsp. 395
Flight Profilesp. 395
King Air 200 / B200p. 396
King Air B200GT / 250p. 410
General Profilesp. 424
Illustrationsp. 391
Figure 19-1. 200/B200 Normal Takeoff and Departurep. 396
Figure 19-2. 200/B200 Engine Loss at or Above V1p. 397
Figure 19-3. 200/B200 Rejected Takeoffp. 398
Figure 19-4. 200/B200 Steep Turnsp. 399
Figure 19-5. 200/B200 Approach to Stall—Takeoff Configuration (Simulator Only)p. 400
Figure 19-6. 200/B200 Approach to Stall—Enroute Configuration (Simulator Only)p. 401
Figure 19-7. 200/B200 Approach to Stall—Approach Configuration (Simulator Only)p. 402
Figure 19-8. 200/B200 Approach to Stall—Landing Configuration (Simulator Only)p. 403
Figure 19-9. 200/B200 Visual Approach and Landingp. 404
Figure 19-10. 200/B200 One Engine Inoperative—Visual Approach and Landingp. 405
Figure 19-11. 200/B200 Flap Malfunction—Visual Approach and Landingp. 406
Figure 19-12. 200/B200 ILS Approach—Landing in Sequence from an ILSp. 407
Figure 19-13. 200/B200 Nonprecision Approach—Procedure Turnp. 408
Figure 19-14. 2200/B200 Circling Approach and Landingp. 409
Figure 19-15. B200GT/250 Normal Takeoff and Departurep. 410
Figure 19-16. B200GT/250 Engine Loss at or Above V1p. 411
Figure 19-17. B200GT/250 Rejected Takeoffp. 412
Figure 19-18. B200GT/250 Steep Turnsp. 413
Figure 19-19. B200GT/250 Approach to Stall—Takeoff Configuration (Simulator Only)p. 414
Figure 19-20. B200GT/250 Approach to Stall—Enroute Configuration (Simulator Only)p. 415
Figure 19-21. B200GT/250 Approach to Stall—Approach Configuration (Simulator Only)p. 416
Figure 19-22. B200GT/250 Approach to Stall—Landing Configuration (Simulator Only)p. 417
Figure 19-23. B200GT/250 Visual Approach and Landingp. 418
Figure 19-24. B200GT/250 One Engine Inoperative—Visual Approach and Landingp. 419
Figure 19-25. B200GT/250 Flap Malfunction—Visual Approach and Landingp. 420
Figure 19-26. B200GT/250 ILS Approach—Landing in Sequence from an ILSp. 421
Figure 19-27. B200GT/250 Nonprecision Approach—Procedure Turnp. 422
Figure 19-28. B200GT/250 Circling Approach and Landingp. 423
Figure 19-29. Emergency Descentp. 424
Figure 19-30. Standard Holding Pattern—Direct Entryp. 425
Figure 19-31. Standard Holding Pattern—Teardrop Entryp. 426
Figure 19-32. Standard Holding Pattern—Parallel Entryp. 427
Chapter 20 Weight and Balancep. 428
Contentsp. 428
Introductionp. 430
Weight And Balancep. 431
Weight and Balance Computationp. 431
Questionsp. 442
Illustrationsp. 429
Figure 20-1. Basic Empty Weight and Balance Formp. 432
Figure 20-2. Weight and Balance Loading Formp. 433
Figure 20-3. Loading Data (Passenger)p. 434
Figure 20-4. Cabin Loadingp. 435
Figure 20-5. Loading Data Cargo Configurationp. 436
Figure 20-6. Density Variation of Aviation Fuelp. 437
Figure 20-7. Useful Load Weights and Moments Usable Fuelp. 438
Figure 20-8. Moment Limits vs. Weightp. 439
Figure 20-9. Moment Limits vs. Weight with CGp. 440
Chapter 21 Flight Planning and Performancep. 443
Chapter 22 Crew Resource Management (CRM)p. 444
Contentsp. 444
Introductionp. 446
Crew Concept Briefing Guidep. 448
Descriptionp. 448
Common Termsp. 448
Pretakeoff Briefing (IFR/VFR)p. 448
Crew Coordination Approach Sequencep. 448
Illustrationsp. 445
Figure 22-1. Situational Awareness in the Cockpitp. 447
Figure 22-2. Command and Leadershipp. 447
Figure 22-3. Communication Processp. 449
Figure 22-4. Decision-Making Processp. 449
Figure 22-5. Error Management Processp. 449
Figure 22-6. Crew Performance Standardsp. 451
Tablesp. 445
Table 22-1. Altitude Callouts—Enroutep. 453
Table 22-2. Altitude Callouts—Approach (Precision)p. 453
Table 22-3. Altitude Callouts—Approach (Nonprecision)p. 453
Table 22-4. Altitude Callouts—Callouts Of Significant Deviationp. 453
Appendix A Terminologyp. 484
Appendix B Answers to Questionsp. 489
Annunciatorsp. 490

The later portions broaden the training beyond individual systems. Maneuvers and procedures include flight profiles for the 200/B200 and B200GT/250, while weight and balance works through loading data and computation. Crew resource management addresses situational awareness, command and leadership, communication, decision making, error management and crew performance. A dedicated walkaround section, terminology appendix, answers to chapter questions and an annunciator-panel reference round out the volume.

Chapters Covered

  • Chapter 1 – Aircraft General: aircraft systems; aircraft structures; fuselage; doors; emergency exit; cabin windows; control locks
  • Chapter 2 – Electrical Power Systems: DC power system; AC power system; controls and indications; operation; generator and starter limitations; circuit breakers; emergency/abnormal; questions
  • Chapter 3 – Lighting: interior lighting; cabin and cockpit lighting; controls and indications; landing, taxi, wing ice, navigation, recognition, beacon, tail flood, strobe, airstair and understep lighting; questions
  • Chapter 4 – Master Warning System: components; dim and test modes; glareshield flashers; red warning annunciators; amber/green caution and advisory annunciators; emergency/abnormal; questions
  • Chapter 5 – Fuel System: main and auxiliary fuel systems; pumps, filters and fuel heater; fuel manifold clearing; controls and indications; auxiliary transfer; crossfeed; fueling; approved fuels and additives; limitations; questions
  • Chapter 6 – Auxiliary Power System: chapter identifies this system as not applicable to this particular aircraft
  • Chapter 7 – Powerplant: PT6A engine; lubrication; engine fuel system; ignition; propeller; controls and indications; engine indicating system; feathering and autofeather; operating limitations; questions
  • Chapter 8 – Fire Protection: fire detection; fire extinguishing; controls and indications; operation; system testing; portable extinguishers; limitations; emergency/abnormal; questions
  • Chapter 9 – Pneumatics: pneumatic and vacuum systems; bleed-air warning system; door seal system; controls and indications; limitations; emergency/abnormal; questions
  • Chapter 10 – Ice and Rain Protection: pneumatic and electrical ice-protection functions, including surface deice, engine anti-ice, windshield, fuel vent, propeller, pitot and stall-warning heat, plus rain protection
  • Chapter 11 – Air Conditioning: cooling, heating and unpressurized ventilation; environmental-system components; automatic and manual temperature control; bleed-air controls; cockpit and cabin temperature controls; operation; limitations; emergency/abnormal; questions
  • Chapter 12 – Pressurization: flow control unit; bleed-air valves; pressurization controller; cabin altitude and climb indications; cabin pressure dump; annunciators; preflight, in-flight, descent and landing operation; limitations; questions
  • Chapter 13 – Hydraulic Power System
  • Chapter 14 – Landing Gear and Brakes: landing-gear description and operation; controls and indications; normal retraction and extension; alternate extension; nosewheel steering; brake system; cold-weather care and handling; limitations; emergency/abnormal; questions
  • Chapter 15 – Flight Controls: primary flight controls; control locks; ailerons, elevators and rudder; rudder boost; trim systems; flaps and split-flap protection; stall warning
  • Chapter 16 – Avionics: PFD and MFD; display control panels; IAPS; air data computers; AHRS; reversionary operations; pitot/static and outside-air-temperature functions; stall warning; flight guidance; CDU; FMS; GPS; IFIS; communications/navigation; audio; ESIS; weather radar; CVR; ELT; EGPWS
  • Chapter 16A – Wide Area Augmentation System (WAAS)
  • Chapter 17 – Oxygen System: crew oxygen; controls and indications; first-aid oxygen; passenger oxygen system
  • Chapter 18 – Water and Waste: toilet; relief tubes; emergency/abnormal; questions
  • Chapter 19 – Maneuvers and Procedures: takeoff; landing; windshear; microbursts; flight profiles for King Air 200/B200 and B200GT/250; general profiles
  • Chapter 20 – Weight and Balance: weight-and-balance computation; loading forms and data; passenger and cargo loading; fuel density; useful-load moments; moment and CG limits; questions
  • Chapter 21 – Flight Planning and Performance: directs the reader to the OEM manual applicable to the particular aircraft
  • Chapter 22 – Crew Resource Management: crew concept briefing guide; common terms; pretakeoff briefing; crew coordination; situational awareness; command and leadership; communication; decision making; error management; crew performance standards
  • Walkaround
  • Appendix A – Terminology
  • Appendix B – Answers to Questions
  • Annunciator Panel

Taken as a whole, the chapter sequence moves from basic aircraft orientation through the systems a pilot must understand to interpret cockpit indications and system behavior, then into operating profiles, loading calculations and crew coordination. The many system diagrams, panel illustrations, operating-limit tables and question sets make the manual useful for structured study, recurrent familiarization and cockpit-systems review.

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King Air B200/B200GT/250 Pro Line 21 Aircraft Systems Pilot Training Manual Vol. 2 - Rev 0.3 PDF — PDF page 1 preview
King Air B200/B200GT/250 Pro Line 21 Aircraft Systems Pilot Training Manual Vol. 2 - Rev 0.3 PDF — PDF page 23 preview
King Air B200/B200GT/250 Pro Line 21 Aircraft Systems Pilot Training Manual Vol. 2 - Rev 0.3 PDF — PDF page 97 preview

Powerplant, Pro Line 21 and System Detail

Powerplant training is a major part of this volume. The manual identifies the engines as PT6A-42/52 and describes the PT6A as a free-turbine, reverse-flow turboprop. It explains major engine sections, compressor and turbine operation, lubrication, fuel metering, ignition, engine indications, propeller governing and protection functions. The propeller section covers four-blade propellers, constant-speed operation, feathering, reversing, ground fine control, overspeed protection and autofeather. Operating-limit tables are provided separately for PT6A-42 and PT6A-52 engines.

The avionics chapter gives the King Air B200/B200GT/250 Pro Line 21 training manual a strong cockpit-systems focus. It covers the primary flight displays, multifunction display, display control panels, integrated avionics processor system, air-data computers, attitude and heading reference system, flight guidance, flight management system and GPS. It also addresses reversionary operations and supporting communication, navigation, audio, standby-instrument, weather-radar and warning-system equipment. This depth is valuable when studying how system information is presented to the crew rather than simply memorizing component names.

For Familiarization and Training

This is specifically a training publication. It is well suited to pilots, students and instructors who need a detailed systems reference for the King Air B200/B200GT/250 with Pro Line 21, including the relationship between aircraft hardware, cockpit controls, indications and operating principles. It can support ground-school preparation, recurrent training, systems review, procedural familiarization, annunciator study, weight-and-balance practice and review of normal training profiles. Where the manual points to the approved AFM, POH, checklists, maintenance material or OEM performance data, those controlling publications remain the source for aircraft-specific operational decisions.

Get the Complete Aircraft Systems Training Volume

The King Air B200/B200GT/250 Pro Line 21 Aircraft Systems Pilot Training Manual Vol. 2 – Rev 0.3 PDF gives you one extensive reference for studying the electrical, fuel, powerplant, fire protection, pneumatic, environmental, pressurization, landing gear, flight-control, oxygen and Pro Line 21 avionics systems, together with maneuvers, loading instruction and crew resource management. The diagrams, controls-and-indications explanations, system operation descriptions and limitations help you understand not just where a component is located, but how the systems interact and what cockpit indications mean during training.

After payment, the manual is delivered instantly as a PDF with no shipping delay. Open it on a compatible computer, tablet or phone, keep it available for study on your preferred device, or print the pages you want for training and reference.

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