★ TRUSTED BY 321,897+ PROFESSIONALS WORLDWIDE
🏢
Trusted Business
Verified & Licensed
🛡️
Virus Free Files
100% Safe Downloads
🔒
Secure Payment
SSL Protected
⚡
Instant Delivery
Available Immediately
Sale!
King Air C90A C90B C90GT Pilot Training Manual - FlightSafety Complete Systems Course
King Air C90A C90B C90GT Pilot Training Manual - FlightSafety Complete Systems Course - Image 2
King Air C90A C90B C90GT Pilot Training Manual - FlightSafety Complete Systems Course - Image 3

King Air C90A C90B C90GT Pilot Training Manual – FlightSafety Complete Systems Course

Original price was: $42.95.Current price is: $25.95.

Complete FlightSafety International pilot training manual for the Beechcraft King Air C90A, C90B, and C90GT. Covers all major aircraft systems across 17 chapters plus a dedicated C90GT powerplant section. 409 pages, PDF.

SKU: FSI-KA-C90ABGT-PTM-HD Category: Tags: , , , Vendor: Mower Service Manuals
⚡
Instant PDF Download
Available immediately
💾
Save to Your Device
Download & keep forever
🛡️
Antivirus Scanned
100% virus-free
🌍
Trusted Worldwide
175,000+ customers

Description

This King Air C90A/B/GT Pilot Training Manual is the complete FlightSafety International training course document for the Beechcraft King Air C90A, C90B, and C90GT turboprop aircraft. It is the same structured training manual used in FlightSafety learning centers, covering every major aircraft system in detail, from the Pratt & Whitney PT6A powerplant and propeller system through electrical distribution, pressurization, avionics, ice protection, and landing gear.

At 409 pages across 17 chapters plus a dedicated C90GT powerplant chapter, this is one of the most thorough single-source references available for King Air C90-series pilots, type-rating candidates, and training departments.

File Details

  • Manual Type: Pilot Training Manual
  • Publisher: FlightSafety International
  • Aircraft Covered: Beechcraft King Air C90A, C90B, C90GT
  • Engines: Pratt & Whitney PT6A-21 (C90A/B), PT6A-135A (C90GT)
  • Language: English
  • File Format: PDF
  • Page Count: 409
  • Revision: Revision 1.3, May 2015

Chapters Covered

  • Aircraft General – external familiarization, cabin entry and exits, cockpit layout, three-view diagrams, specifications tables, servicing data, preflight inspection
  • Electrical Power Systems – battery and generators, bus tie system, bus isolation, load shedding, starter/generators, AC inverters, external power, avionics master power
  • Lighting – cockpit lighting, cabin lighting, exterior lighting, threshold lights, circuit breakers
  • Master Warning System – annunciator panel, warning/caution/advisory lights, fault warning flasher, dimming, testing and lamp replacement
  • Fuel System – fuel cells, boost pumps, transfer pumps, crossfeed operation, firewall shutoff valves, fuel drains, approved fuels and handling
  • Powerplant – PT6A free-turbine design, engine stations, compressor bleed valve, lubrication, fuel control unit, ITT and torque limits, starter limits, trend monitoring
  • Propellers – blade angle, primary governor, low pitch stop, Beta and reverse range, overspeed governor, autofeather system, synchrophaser
  • C90GT Powerplant – PT6A-135A engine specifics, Hartzell four-blade propellers, revised operating limits and procedures
  • Fire Protection – fire detection system, fire extinguishing system, testing procedures
  • Pneumatics – bleed air system, vacuum source, cabin door seal, surface deice system
  • Ice and Rain Protection – pitot heat, stall warning vane, fuel system anti-ice, windshield wipers, windshield anti-ice, engine inlet lip heat, inertial separators, propeller deice, wing ice lights
  • Air Conditioning – environmental system, bleed-air heating, electric heat, cooling system, automatic and manual mode controls
  • Pressurization – cabin pressure control, flow control unit, outflow and safety valves, preflight check, in-flight management, descent procedures
  • Landing Gear and Brakes – hydraulic system, extension and retraction, manual extension, steering, tires, shock struts, series brake system, parking brake
  • Flight Controls – flap system operation, flap airspeed limits, rudder boost system
  • Avionics – Collins Pro Line II, Collins EFIS-84, APS-65H flight director and autopilot, Garmin GPS 400, Bendix/King KLN-90B, King Silver Crown II, slaved compass systems, pitot-static system
  • Miscellaneous Systems – oxygen system, diluter-demand masks, oxygen duration computation, physiological training

What This Training Manual Delivers

The King Air C90A/B/GT Pilot Training Manual is built around the systems knowledge required for safe, confident operation of the aircraft. Each chapter pairs clear system descriptions with diagrams, schematics, and operational limitations, so a pilot or trainee can understand not just what a system does, but how to manage it correctly during normal and emergency operations.

Complete PDF Bookmark Tree

Complete Bookmarks

The complete bookmarks in the “King Air C90A C90B C90GT Pilot Training Manual – FlightSafety Complete Systems Course” are as follows:

Chapter 1 Aircraft Generalp. 6
Contentsp. 6
Introductionp. 9
Generalp. 9
Airplane Systemsp. 10
Generalp. 10
Chaptersp. 10
Changes Distinguishing Model C90B From Model C90Ap. 12
Beechcraft King Air C90A And C90B Descriptionp. 14
King Air C90A And C90B Configurationp. 19
C90A Operating Speedsp. 22
C90B Operating Speedsp. 23
Cabin Entry And Exitsp. 24
Emergency Exitp. 26
Nose Baggage Door (Optional)p. 26
Cabin Compartmentsp. 26
Flight Deckp. 28
C90A Instrument Panel/Avionicsp. 37
Control Surfacesp. 38
Tiedown And Securingp. 39
Taxiingp. 40
Servicing Datap. 40
Product Supportp. 42
Preflight Inspectionp. 42
Illustrationsp. 7
Figure 1-1. Beechcraft King Air C90Ap. 14
Figure 1-2. General Arrangement—C90Ap. 15
Figure 1-3. Three-View Diagram—C90Ap. 16
Figure 1-4. General Arrangement—C90Bp. 17
Figure 1-5. Three-View Diagram—C90Bp. 18
Figure 1-6. Engine Air Inletp. 19
Figure 1-7. Optional Cabin Seating Arrangementp. 19
Figure 1-8. King Air C90A Front Three-Quarter View (Engines Primary)p. 22
Figure 1-9. King Air C90B in Flightp. 23
Figure 1-10. Entrance and Exit Provisionsp. 24
Figure 1-11. Dual Door Cablesp. 25
Figure 1-12. Nose Compartment Door (Baggage Compartment Not Shown)p. 26
Figure 1-13. Cabin Areasp. 27
Figure 1-14. Cabin Seating Layout (Typical)p. 27
Figure 1-15. Flight Deck Layoutp. 28
Figure 1-16. Control Wheels and Fuel Control Panelp. 29
Figure 1-17. Instrument Panelsp. 30
Figure 1-18. Instrumentationp. 31
Figure 1-19. Engine Instruments—Prior to LJ-1361p. 32
Figure 1-20. Engine Instruments—LJ-1361, LJ-1363, and Afterp. 33
Figure 1-21. Pedestal and Right Side Panelp. 34
Figure 1-22. Pilot’s and Copilot’s Subpanelsp. 35
Figure 1-23. Annunciatorsp. 36
Figure 1-25. Avionics Installation (C90A)p. 37
Figure 1-24. Overhead Light Control Panelp. 37
Figure 1-26. Flight Control Surfacesp. 38
Figure 1-27. Flight Control Locksp. 38
Figure 1-28. Tiedownsp. 39
Figure 1-29. Propeller Bootsp. 39
Figure 1-30. Turning Radiusp. 40
Figure 1-31. Danger Areasp. 40
Figure 1-32. Servicing Datap. 41
Figure 1-33. Exterior Inspectionp. 42
Tablesp. 8
Table 1-1. Specifications—C90Ap. 20
Table 1-2. Specifications—C90Bp. 21
Chapter 2 Electrical Power Systemsp. 43
Contentsp. 43
Introductionp. 46
Generalp. 46
Battery and Generatorp. 48
Bus Tie Systemp. 53
Bus Isolationp. 56
Load Sheddingp. 56
Batteryp. 57
Starter/Generatorsp. 57
AC Power Distributionp. 60
External Powerp. 61
Avionics Master Powerp. 64
Circuit Breakersp. 64
Questionsp. 81
Illustrationsp. 44
Figure 2-1. Electrical System Component Locationsp. 47
Figure 2-2. Basic Electrical Symbolsp. 48
Figure 2-3. Pilot and Copilot Subpanelsp. 49
Figure 2-4. Overhead Meter Panelp. 50
Figure 2-5. Right Side and Fuel Management Circuit Breaker Panels (LJ-1063 Thru LJ-1360, LJ-1362p. 54
Figure 2-6. Right Side and Fuel Management Circuit Breaker Panels (LJ-1361, LJ-1363 and After)p. 55
Figure 2-7. Battery Installationp. 57
Figure 2-8. Starter/Generator Installationp. 58
Figure 2-9. Simplified Inverter Schematicp. 61
Figure 2-10. Inverter Schematic—Condition 1p. 62
Figure 2-11. Inverter Schematic—Condition 2p. 62
Figure 2-12. Inverter Schematic—Condition 3p. 63
Figure 2-13. Avionics Master Power Schematicp. 64
Figure 2-14. Power Distribution Schematicp. 66
Figure 2-15. Power Distribution—Battery OFFp. 67
Figure 2-16. Power Distribution—Battery ONp. 68
Figure 2-17. Power Distribution—Battery ON (Generator Ties Manually Closed)p. 69
Figure 2-18. Power Distribution—Right Engine Start (Generator Ties Normal)p. 70
Figure 2-19. Power Distribution—Right Generator ONp. 71
Figure 2-20. Power Distribution—Left Engine Cross-Start (Right Engine Running)p. 72
Figure 2-21. Power Distribution—Both Generators ONp. 73
Figure 2-22. Power Distribution—Both Generators ON (Generator Ties Open)p. 74
Figure 2-23. Bus Sense Test—Both Generators ONp. 75
Figure 2-24. Both Generators Failed—Load Sheddingp. 76
Figure 2-25. Right Generator Bus Short—Bus Isolationp. 77
Figure 2-26. Center Bus Short—Bus Isolationp. 78
Figure 2-27. Triple-Fed Bus Short—Bus Isolationp. 79
Figure 2-28. Power Distribution—External Power (External Power and Battery Switches ON)p. 80
Tablesp. 45
Table 2-1. Electrical System Buses and Feedersp. 51
Chapter 3 Lightingp. 83
Contentsp. 83
Introductionp. 85
Descriptionp. 85
Cockpit Lightingp. 86
Cabin Lightingp. 86
Exterior Lightingp. 87
Circuit Breakersp. 87
Questionsp. 89
Illustrationsp. 84
Figure 3-1. Overhead Lighting Control Panelp. 86
Figure 3-2. Cabin Lighting Controlsp. 86
Figure 3-3. Threshold Light Switchp. 87
Figure 3-4. Exterior Light Controlsp. 87
Figure 3-5. Light System Circuit Breakersp. 88
Chapter 4 Master Warning Systemp. 90
Contentsp. 90
Introductionp. 92
Generalp. 92
Annunciator Systemp. 94
Fault Warning Flasherp. 94
Dimmingp. 94
Testing and Lamp Replacementp. 95
Annunciator Panel Descriptionp. 96
Questionsp. 99
Illustrationsp. 91
Figure 4-1. Annunciator Systemp. 93
Figure 4-2. Master Caution and Fault Warning Flashersp. 94
Figure 4-3. Lamp Replacep. 95
Tablesp. 91
Table 4-1. Warning Annunciatorsp. 96
Table 4-2. Caution Annunciatorsp. 97
Table 4-3. Advisory Annunciatorsp. 98
Chapter 5 Fuel Systemp. 100
Contentsp. 100
Introductionp. 102
Descriptionp. 102
Fuel Systemp. 103
Fuel Tank Systemp. 103
Boost Pumpsp. 103
Fuel Transfer Pumpsp. 106
Fuel Capacityp. 107
Fuel Tank Ventsp. 107
Fuel System Operationp. 108
Firewall Shutoff Valvesp. 110
Crossfeed Operationp. 111
Fuel Drain Purge Systemp. 113
Fuel Gaging Systemp. 113
Components and Operationp. 115
Fuel Drainsp. 115
Fuel Handling Practicesp. 117
Fuel Grades and Additivesp. 119
Filling the Tanksp. 119
Draining the Fuel Systemp. 120
Questionsp. 121
Illustrationsp. 101
Figure 5-1. Fuel System Schematic Diagramp. 104
Figure 5-2. Fuel Tank Systemp. 105
Figure 5-3. Fuel Transfer Pump Switchp. 106
Figure 5-4. Fuel Control Panelp. 107
Figure 5-5. Fuel Vent Systemp. 108
Figure 5-6. Fuel Flow Diagramp. 109
Figure 5-7. Firewall Shutoff Valvep. 111
Figure 5-8. Firewall Shutoff Valve Switchesp. 111
Figure 5-9. Crossfeed Schematicp. 112
Figure 5-10. Fuel Drain Purge System Schematicp. 113
Figure 5-11. Fuel Quantity Indication Systemp. 114
Figure 5-12. Fuel Probep. 115
Figure 5-13. Fuel Drainsp. 116
Figure 5-14. Fuel Temperature Graphp. 118
Tablesp. 101
Table 5-1. Fuel Drain Loacationsp. 116
Chapter 7 Powerplantp. 123
Contentsp. 123
Introductionp. 127
Generalp. 127
Enginesp. 128
Generalp. 128
Turboprop Engine Ratingsp. 128
Engine Termsp. 130
Free-Turbine Reverse-flow Principlep. 130
Engine Airflowp. 131
Engine Stationsp. 133
Engine Modular Conceptp. 133
Compressor Bleed Valvep. 134
Ignitersp. 135
Accessory Sectionp. 135
Lubrication Systemp. 137
Engine Fuel Systemp. 140
Engine Power Controlp. 143
ITT and Torquemetersp. 144
ITT Gagep. 144
Torquemeterp. 144
Gas Generator Tachometer (N1)p. 145
Control Pedestalp. 145
Engine Limitationsp. 146
Starter Operating Time Limitsp. 150
Data Collection Formp. 150
Propellersp. 151
Generalp. 151
Propeller Systemp. 151
McCauley and Hartzell Four-Blade Propellersp. 152
Blade Anglep. 152
Primary Governorp. 153
Primary Governor Operationp. 155
Low Pitch Stopp. 156
Beta and Reverse Controlp. 158
Overspeed Governorp. 160
Overspeed Governor Operationp. 160
Fuel Topping Governorp. 160
Power Leversp. 161
Autofeather Systemp. 162
Propeller Synchrophaser Systemp. 164
Questionsp. 167
Illustrationsp. 125
Figure 7-1. Powerplant Installationp. 128
Figure 7-2. Engine Installationp. 129
Figure 7-3. Free Turbinep. 130
Figure 7-4. Engine Cutawayp. 130
Figure 7-5. Engine Stationsp. 131
Figure 7-6. Engine Orientationp. 131
Figure 7-7. Engine Gas Flowp. 132
Figure 7-8. Power and Compressor Sectionsp. 132
Figure 7-9. Engine Constructionp. 132
Figure 7-10. Typical Engine Modular Constructionp. 133
Figure 7-11. Compressor Bleed Valvep. 134
Figure 7-12. Engine Start and Ignition Switchesp. 135
Figure 7-13. Typical PT6A Enginep. 136
Figure 7-14. Engine Lubrications Diagramp. 137
Figure 7-15. Engine Oil Dipstickp. 138
Figure 7-16. Magnetic Chip Detectorp. 139
Figure 7-17. Simplified Fuel System Diagramp. 140
Figure 7-18. Simplified Fuel Control Systemp. 141
Figure 7-19. Fuel Pressure Annunciatorsp. 142
Figure 7-20. Fuel Flow Indicatorp. 143
Figure 7-21. Control Leversp. 143
Figure 7-22. Engine Instrument Markingsp. 144
Figure 7-23. Control Pedestalp. 145
Figure 7-24. Overtorque Limits Chartp. 148
Figure 7-25. Overtemperature Limits (Starting)p. 148
Figure 7-26. Overtemperature Limits (Except Starting)p. 149
Figure 7-27. View through Exhaust Ductp. 149
Figure 7-28. In-Flight Engine Data Logp. 150
Figure 7-29. Propellersp. 151
Figure 7-30. Propeller Tiedown Boot Installedp. 151
Figure 7-31. Blade Angle Diagramp. 152
Figure 7-32. Primary Governor Diagramp. 153
Figure 7-33. Propeller Onspeed Diagramp. 154
Figure 7-34. Propeller Overspeed Diagramp. 154
Figure 7-35. Propeller Underspeed Diagramp. 155
Figure 7-36. Low Pitch Stop Diagramp. 157
Figure 7-37. Beta Range and Reverse Diagramp. 159
Figure 7-38. Overspeed Governor Diagramp. 161
Figure 7-39. Power Leversp. 162
Figure 7-40. Propeller Control Leversp. 162
Figure 7-41. Autofeather System Diagram—Left Engine Failed and Featheringp. 163
Figure 7-42. Autofeather System Diagram—Armedp. 163
Figure 7-43. Autofeather Test Diagramp. 164
Figure 7-44. Propeller Synchrophaserp. 165
Tablesp. 126
Table 7-1. PT6A-21 Specificationsp. 129
Table 7-2. Engine Limits Chartp. 147
Chapter 7 Powerplant (C90GT)p. 169
Contentsp. 169
Introductionp. 173
Generalp. 173
Enginesp. 174
Turboprop Engine Ratingsp. 175
Engine Termsp. 175
Free-Turbine Reverse-flow Principlep. 176
Engine Airflowp. 177
Engine Stationsp. 179
Engine Modular Conceptp. 179
Compressor Bleed Valvep. 180
Ignitersp. 181
Accessory Sectionp. 182
Lubrication Systemp. 182
Engine Fuel Systemp. 185
Fuel Control Unitp. 186
Fuel Pressure Indicatorsp. 188
Fuel Flow Indicatorsp. 188
Anti-icing Fuel Additivep. 189
Engine Power Controlp. 189
ITT and Torquemetersp. 190
ITT Gaugep. 190
Torquemeterp. 190
Gas Generator Tachometer (N1)p. 191
Control Pedestalp. 191
Engine Limitationsp. 192
Starter Operating Time Limitsp. 193
Data Collection Formp. 194
Propellersp. 195
Generalp. 195
Propeller Systemp. 195
Hartzell Four-Blade Propellersp. 196
Blade Anglep. 196
Primary Governorp. 197
Low Pitch Stopp. 200
Ground fine and Reverse Controlp. 202
Overspeed Governorp. 204
Fuel Topping Governorp. 205
Power Leversp. 205
Autofeather Systemp. 206
Propeller Synchrophaser Systemp. 208
Propeller Synchroscopep. 210
Questionsp. 211
Illustrationsp. 171
Figure 7 GT-1. Powerplant Installationp. 174
Figure 7 GT-2. Engine Installationp. 175
Figure 7 GT-3. Free Turbinep. 176
Figure 7 GT-4. Engine Cutawayp. 176
Figure 7 GT-6. Engine Stationsp. 177
Figure 7 GT-5. Engine Orientationp. 177
Figure 7 GT-7. Engine Gas Flowp. 178
Figure 7 GT-8. Power and Compressor Sectionsp. 178
Figure 7 GT-9. Typical Engine Modular Constructionp. 179
Figure 7 GT-10. Compressor Bleed Valvep. 180
Figure 7 GT-11. Engine Start and Ignition Switchesp. 181
Figure 7 GT-12. Typical PT6A Enginep. 182
Figure 7 GT-13. Engine Lubrications Diagramp. 183
Figure 7 GT-14. Engine Oil Dipstickp. 184
Figure 7 GT-15. Magnetic Chip Detectorp. 185
Figure 7 GT-16. Simplified Fuel System Diagramp. 186
Figure 7 GT-17. Simplified Fuel Control Systemp. 187
Figure 7 GT-18. Fuel Pressure Annunciatorsp. 188
Figure 7 GT-19. Fuel Flow Indicatorp. 189
Figure 7 GT-20. Control Leversp. 189
Figure 7 GT-21. Engine Indicating Systemp. 190
Figure 7 GT-22. Control Pedestalp. 191
Figure 7 GT-23. Engine Limits Chartp. 193
Figure 7 GT-24. In-Flight Engine Data Logp. 194
Figure 7 GT-25. Propellersp. 195
Figure 7 GT-26. Propeller Tiedown Boot Installedp. 196
Figure 7 GT-27. Blade Angle Diagramp. 196
Figure 7 GT-28. Primary Governor Diagramp. 197
Figure 7 GT-29. Propeller Onspeed Diagramp. 199
Figure 7 GT-30. Propeller Overspeed Diagramp. 199
Figure 7 GT-31. Propeller Underspeed Diagramp. 200
Figure 7 GT-32. Low Pitch Stop Diagramp. 201
Figure 7 GT-33. Beta Range and Reverse Diagramp. 203
Figure 7 GT-34. Overspeed Governor Diagramp. 204
Figure 7 GT-35. Power Leversp. 205
Figure 7 GT-36. Propeller Control Leversp. 206
Figure 7 GT-37. Autofeather System Diagram—Left Engine Failed and Featheringp. 207
Figure 7 GT-38. Autofeather System Diagram—Armedp. 207
Figure 7 GT-39. Autofeather Test Diagramp. 208
Figure 7 GT-40. Propeller Synchrophaserp. 209
Figure 7 GT-41. Propeller Synchroscopep. 210
Chapter 8 Fire Protectionp. 212
Contentsp. 212
Introductionp. 214
Generalp. 214
Fire Detection Systemp. 215
Fire Extinguishing Systemp. 215
Questionsp. 219
Illustrationsp. 213
Figure 8-1. Fire Detection Systemp. 215
Figure 8-2. Fire Extinguishing Systemp. 216
Figure 8-3. Fire Extinguisher Cylinder Pressure Gagep. 218
Chapter 9 Pneumaticsp. 220
Contentsp. 220
Introductionp. 222
Descriptionp. 222
Engine Bleed Air Pneumatic Systemp. 223
Pneumatic Air Sourcep. 224
Vacuum Air Sourcep. 224
Cabin Door Sealp. 225
Surface Deice Systemp. 225
Questionsp. 228
Illustrationsp. 221
Figure 9-1. Pneumatic System Diagramp. 223
Figure 9-2. Pneumatic Pressure Gagep. 224
Figure 9-3. Gyro Suction Gagep. 224
Figure 9-4. Surface Deice Boot Installationp. 225
Figure 9-5. Surface Deice System Diagramp. 226
Figure 9-6. Surface Deice Controlsp. 227
Chapter 10 Ice and Rain Protectionp. 229
Contentsp. 229
Introductionp. 231
Generalp. 231
Ice Protection Systemsp. 234
Description and Operationp. 234
Pitot Heatp. 234
Stall Warning Vanep. 235
Fuel System Anti-Icep. 235
Windshield Wipersp. 236
Windshield Anti-Icep. 237
Engine Air Inlet Lip Heatp. 239
Engine Inertial Separatorsp. 240
Ice Vane Controlsp. 241
Engine Autoignition Systemp. 242
Propeller Electric Deice Systemp. 242
Wing Ice Lightsp. 243
Precautions During Icing Conditionsp. 244
Questionsp. 246
Illustrationsp. 230
Figure 10-1. Ice and Rain Protection Required Equipmentp. 232
Figure 10-2. Ice and Rain Proctection Controlsp. 233
Figure 10-3. Pitot Mast and Heat Controlsp. 234
Figure 10-4. Stall Warning Vane and Heat Controlp. 235
Figure 10-5. Fuel System Anti-icep. 236
Figure 10-6. Windshield Wipersp. 237
Figure 10-7. Windshield Installationp. 237
Figure 10-8. Windshield Anti-ice Diagramp. 238
Figure 10-9. Windshield Anti-ice Switchesp. 238
Figure 10-10. Windshield Anti-ice Diagram—Normal Heatp. 238
Figure 10-11. Windshield Anti-ice Diagram—High Heatp. 239
Figure 10-12. Engine Air Inlet Lip Heatp. 239
Figure 10-13. Inertial Separator in Retract Positionp. 240
Figure 10-14. Inertial Separator in Extend Positionp. 241
Figure 10-15. Ice Vane Controlsp. 241
Figure 10-16. Caution and Advisory Annunciatorsp. 242
Figure 10-17. Engine Autoignition Switchesp. 242
Figure 10-18. Propeller Electric Deice Systemp. 243
Figure 10-19. Wing Anti-ice Lightsp. 243
Chapter 11 Air Conditioningp. 248
Contentsp. 248
Introductionp. 250
Descriptionp. 250
Environmental Systemp. 252
Unpressurized Ventilationp. 254
Bleed-Air Heating Systemp. 255
Electric Heatp. 258
Cooling Systemp. 259
Environmental Controlsp. 260
Automatic Mode Controlp. 260
Manual Mode Controlp. 261
Bleed-Air Controlp. 262
Vent Blower Controlp. 262
Questionsp. 263
Illustrationsp. 249
Figure 11-1. Environmental System Schematicp. 251
Figure 11-2. Environmental Group Switches and Knobsp. 252
Figure 11-3. Air Control Knobs—Pilot Airp. 253
Figure 11-4. Air Control Knobs—Defrost Airp. 253
Figure 11-5. Air Control Knobs—Cabin Airp. 253
Figure 11-6. Air Control Knobs—Copilot Airp. 253
Figure 11-7. Ram-Air Scoopp. 254
Figure 11-8. Glareshield “Eyeball” Outletsp. 254
Figure 11-9. Cabin Floor Outletsp. 254
Figure 11-10. Fresh Air Source (Unpressurized Mode)p. 255
Figure 11-11. Cabin “Eyeball” Outletsp. 255
Figure 11-12. Cockpit “Eyeball” Outletsp. 255
Figure 11-13. Ambient and Bleed Air Flow Forward of Firewallsp. 256
Figure 11-14. Air Conditioning System Control Diagramp. 257
Figure 11-15. Mixing Plenump. 258
Figure 11-16. Electric Heaterp. 258
Figure 11-17. Grid Heating Elementsp. 259
Figure 11-18. Elec Heat Switchp. 259
Figure 11-19. Cooling System Components in Nosep. 259
Figure 11-20. Receiver-Dryer Sight Gagep. 260
Figure 11-21. Cabin Temp Mode Selector Switchp. 261
Figure 11-22. Cabin Temp Level Controlp. 261
Figure 11-23. Manual Temp Switchp. 261
Figure 11-24. Bleed Air Valve Switchesp. 262
Figure 11-25. Vent Blower Switchp. 262
Chapter 12 Pressurizationp. 264
Contentsp. 264
Introductionp. 266
Descriptionp. 266
Pressurization Systemp. 268
Air Delivery Systemp. 269
Cabin Pressure Controlp. 272
Preflight Checkp. 273
In Flightp. 274
Descentp. 274
Flow Control Unitp. 274
Questionsp. 276
Illustrationsp. 265
Figure 12-1. Pressurization and Air Conditioning Distribution Systemp. 267
Figure 12-2. Cabin Altitude for Various Airplane Altitudes Graphp. 268
Figure 12-3. Bleed Air Valves Switchesp. 269
Figure 12-4. Cabin Air Outflow Valvep. 270
Figure 12-6. Pressurization Controls Schematicp. 270
Figure 12-5. Cabin Air Safety Valvep. 270
Figure 12-7. Bleed Air Control (Pressurization and Pneumatics)p. 271
Figure 12-8. Pressurization Controllerp. 272
Figure 12-9. Cabin Altimeterp. 272
Figure 12-10. Cabin Climb Indicatorp. 272
Figure 12-11. Cabin Pressure Switchp. 273
Figure 12-12. Environmental System Circuit Breakersp. 273
Figure 12-13. Flow Control Unitp. 275
Tablesp. 265
Table 12-1. Pressurization Controller Setting for Landingp. 274
Chapter 14 Landing Gear and Brakesp. 278
Contentsp. 278
Introductionp. 281
Generalp. 281
Landing Gear Systemp. 282
Landing Gear Assembliesp. 282
Wheel Well Door Mechanismsp. 283
Steeringp. 283
Hydraulic Landing Gearp. 284
Landing Gear Extension and Retractionp. 285
Hydraulic Fluid Level Indication Systemp. 288
Landing Gear Warning Systemp. 291
Manual Landing Gear Extensionp. 291
Hydraulic Schematicsp. 292
Tiresp. 295
Shock Strutsp. 298
Landing Gear Operating Limitsp. 298
King Air Wheel Brakesp. 298
Series Brake Systemp. 298
Parking Brakep. 298
Brake Servicep. 301
Brake Wear Limitsp. 302
Cold Weather Operationp. 302
Questionsp. 303
Illustrationsp. 279
Figure 14-1. Main Gear Assemblyp. 282
Figure 14-2. Nose Gear Assemblyp. 282
Figure 14-3. Main Gear Door Mechanismp. 283
Figure 14-4. Landing Gear Electrical Schematicp. 284
Figure 14-5. Hydraulic Landing Gear Plumbing Schematicp. 285
Figure 14-6. Hydraulic Landing Gear Diagramp. 286
Figure 14-7. Hydraulic Landing Gear Power Packp. 287
Figure 14-8. Landing Gear Control Switch Handlep. 288
Figure 14-9. Hydraulic Fluid Indicatorp. 288
Figure 14-10. Safety Switchp. 289
Figure 14-11. Gear Position Indicatorp. 289
Figure 14-12. Gear Position Indicator—No Illuminationp. 289
Figure 14-14. Handle Light Testp. 290
Figure 14-13. Landing Gear Control Switch Handle—Red In-Transit Indicatorsp. 290
Figure 14-15. Landing Gear Alternate Extension Placardp. 292
Figure 14-16. Landing Gear Relay Circuit Breakerp. 292
Figure 14-17. Landing Gear Retraction Schematicp. 293
Figure 14-18. Landing Gear Extension Schematicp. 294
Figure 14-19. Hand Pump Emergency Extension Schematicp. 296
Figure 14-20. Landing Gear Maintenance Retraction Schematicp. 297
Figure 14-21. Brake System Schematicp. 299
Figure 14-22. Parking Brake Schematicp. 300
Figure 14-23. Brake Fluid Reservoirp. 301
Figure 14-24. Brake Wear Diagramp. 302
Tablesp. 280
Table 14-1. Landing Gear Warning Horn Operationp. 291
Table 14-2. Landing Gear Operating Limitsp. 298
Chapter 15 Flight Controlsp. 304
Contentsp. 304
Introductionp. 306
Descriptionp. 306
Flaps Systemp. 307
C90A Flap Operationp. 309
C90B Flap Operationp. 309
Landing Gear Warning Systemp. 309
Flap Airspeed Limitsp. 309
Rudder Boost Systemp. 310
Questionsp. 312
Illustrationsp. 305
Figure 15-1. Flap Control Systemp. 307
Figure 15-2. Flap Control Leverp. 308
Figure 15-3. Flap Position Indicatorp. 308
Figure 15-4. Flap System Circuit Breakerp. 308
Figure 15-5. Airspeed Indicatorp. 309
Figure 15-6. Rudder Boost System Diagramp. 310
Figure 15-7. Rudder Boost Switchp. 311
Chapter 16 Avionicsp. 313
Contentsp. 313
Introductionp. 320
Descriptionp. 320
Avionics Power Distributionp. 322
Collins EFIS-84p. 323
Electronic Flight Instrument Systemp. 323
Componentsp. 323
EFIS AUX Power Systemp. 325
Display Select Panel Operationp. 328
EHSI Displayp. 331
EHSI Warning Flagsp. 334
Limitationsp. 335
Collins APS-65Hp. 336
Flight Director and Autopilotp. 336
Modes of Operationp. 336
Flight Director Operationp. 338
Limitationsp. 346
Garmin GPS 400 Global Positioning Systemp. 346
General Informationp. 346
Operationp. 347
Groups and Pagesp. 348
NAV (Navigation)p. 348
WPT (Waypoint)p. 349
AUX (Auxiliary)p. 349
NRST (Nearest)p. 349
Direct-To Navigationp. 349
Flight Plansp. 349
OBS and Auto Modesp. 351
GPS Approachesp. 351
Loading the Approachp. 351
Understanding the Displayp. 353
Flying the Missed Approachp. 353
MAP Pagep. 354
Bendix/King KLN-90B Global Positioning Systemp. 355
General Informationp. 355
Operationp. 357
Waypoint Chapters and Pagesp. 358
Direct-To Navigationp. 358
Flight Plansp. 358
Nearest Waypointsp. 359
Obs and Leg Modesp. 359
GPS Approachesp. 360
Loading the Approachp. 360
Understanding the Displayp. 361
Flying the Missed Approachp. 362
Changing or Deleting an Approachp. 362
Super NAV 5 Pagep. 362
Collins Pro Line II Equipmentp. 363
NAV Systemp. 363
DME Systemp. 364
COMM Systemp. 365
ADF Systemp. 366
Transponder Systemp. 366
Audio Systemp. 366
Componentsp. 366
Audio System Operationp. 368
Slaved Compass Systemsp. 369
MCS-65, KCS-55A, MCS-103, AND C-14A-43 Systemsp. 369
Collins PN-101 Systemp. 371
Pitot-Static Systemp. 371
Descriptionp. 371
Pitot and Static Systemp. 371
King Silver Crown II Equipmentp. 375
Audio Control Systemp. 375
Communications Transceiver Systemp. 376
VOR/LOC/GS Receiver Systemp. 377
DME Systemp. 377
RNAV Systemp. 377
ADF Systemp. 377
Questionsp. 379
Illustrationsp. 316
Figure 16-1. NAV/COM Control Panelp. 321
Figure 16-2. Avionics Master Switch OFFp. 322
Figure 16-3. Avionics Master Switch ONp. 322
Figure 16-4. Alternate Avionics Bus Powerp. 322
Figure 16-5. Avionics Busesp. 323
Figure 16-6. Inverter Power Supplyp. 323
Figure 16-7. EFIS Block Diagramp. 324
Figure 16-8. EADI/EHSI DIM Control Knobp. 324
Figure 16-9. Electronic Attitude Director Indicatorp. 324
Figure 16-10. Electronic Horizontal Situation Indicatorp. 324
Figure 16-11. Display Select Panelp. 325
Figure 16-12. EFIS AUX Power Panel Controlsp. 325
Figure 16-13. EADI Displaysp. 326
Figure 16-14. Excessive Attitude Displayp. 326
Figure 16-15. EADI Warning Flagsp. 327
Figure 16-16. Range (RNG) Knob and Format Switchp. 328
Figure 16-17. HSIp. 328
Figure 16-18. ARCp. 328
Figure 16-19. MAPp. 329
Figure 16-20. ARC Weatherp. 329
Figure 16-21. MAP Weatherp. 329
Figure 16-22. Bearing Pointersp. 330
Figure 16-23. EHSI Displaysp. 332
Figure 16-27. EHSI Warning Flagsp. 335
Figure 16-28. APS-65H Flight Director and Autopilot Systemp. 336
Figure 16-29. Flight Director Annunciators and Command Barsp. 336
Figure 16-30. Heading Modep. 338
Figure 16-31. Altitude Hold Modep. 339
Figure 16-32. Altitude Select Modep. 339
Figure 16-33. Climb Modep. 340
Figure 16-34. Descend Modep. 340
Figure 16-35. Vertical Speed Modep. 340
Figure 16-36. Indicated Airspeed Modep. 341
Figure 16-37. Navigation Modep. 341
Figure 16-38. VOR Approach Modep. 342
Figure 16-39. Localizer Approach Modep. 343
Figure 16-40. Localizer Back Course Approach Modep. 344
Figure 16-41. ILS Approach Modep. 345
Figure 16-42. Go-Around Modep. 346
Figure 16-43. Garmin GPS 400p. 346
Figure 16-44. Garmin GPS 400 Initialization—Welcome Pagep. 347
Figure 16-45. Garmin GPS 400 Initialization—Data Land Pagep. 347
Figure 16-46. Garmin GPS 400 Initialization—Database Confirmation Pagep. 348
Figure 16-47. Garmin GPS 400 Initialization—Satellite Status Pagep. 348
Figure 16-48. GPS 400 Default NAV Pagep. 348
Figure 16-49. GPS 400 MAP Pagep. 348
Figure 16-50. GPS 400 Nearest Airportp. 350
Figure 16-51. GPS 400 Active Flight Planp. 350
Figure 16-52. GPS 400 Flight Plan Catalogp. 350
Figure 16-53. GPS 400 Approach Scalingp. 352
Figure 16-54. GPS 400 Approach Loadingp. 352
Figure 16-58. GPS 400 Approach Displayp. 353
Figure 16-59. GPS 400 Change or Delete Approachp. 354
Figure 16-60. GPS 400 MAP Pagep. 354
Figure 16-61. GPS 400 MAP Page—Dual Data Fieldsp. 354
Figure 16-62. KLN-90B Displays—Standard Formatp. 355
Figure 16-63. KLN-90B Displays—Split Screen Formatsp. 355
Figure 16-64. KLN-90B Displays—Super Pagesp. 356
Figure 16-65. KLN-90B Initialization—Powerup Pagep. 357
Figure 16-66. KLN-90B Initialization—Data Outputs Pagep. 357
Figure 16-67. KLN-90B Initialization—Database Verification Pagep. 357
Figure 16-68. KLN-90B Initialization—Process Completed Pagep. 357
Figure 16-69. KLN-90B Flight Plan Pagep. 358
Figure 16-70. KLN-90B Nearest Airport Pagep. 359
Figure 16-71. KLN-90B Approach Scalingp. 360
Figure 16-72. KLN-90B Approach Loadingp. 360
Figure 16-75. Approach Flight Planp. 361
Figure 16-76. KLN-90B Change Approachp. 362
Figure 16-77. KLN-90B Delete Approachp. 362
Figure 16-78. KLN-90B Super Nav 5 Displayp. 362
Figure 16-79. Pro Line II NAV Controlp. 364
Figure 16-80. Pro Line II DME Controlp. 364
Figure 16-81. Pro Line II Single DME Installationp. 365
Figure 16-82. Pro Line II Dual DME Installationp. 365
Figure 16-83. Pro Line II COM Controlp. 365
Figure 16-84. Pro Line II ADF Controlp. 366
Figure 16-85. Pro Line II Transponder Controlp. 366
Figure 16-86. Pro Line II Audio Panel Controlsp. 367
Figure 16-87. Slaved Compass System Block Diagramp. 369
Figure 16-88. Compass System Connectionsp. 370
Figure 16-89. Compass Compensation Unitp. 370
Figure 16-90. Pitot and Static System Schematicp. 372
Figure 16-91. Pitot-Static Normal Alternate Air Source Valvep. 372
Figure 16-92. Schematic Diagram of Pitot and Static Systemp. 373
Figure 16-93. Ice Protection Switchesp. 374
Figure 16-94. King Audio Control Systemp. 375
Figure 16-95. King Communications Transceiverp. 376
Figure 16-96. King VOR/LOC/GS Receiverp. 376
Figure 16-97. King DME Systemp. 377
Figure 16-98. King ADF Systemp. 378
Tablesp. 319
Table 16-1. Momentary Actuation Adjustmentsp. 338
Table 16-2. Pro Line II Audio Panel Controlsp. 367
Chapter 17 Miscellaneous Systemsp. 381
Contentsp. 381
Introductionp. 384
Descriptionp. 384
Oxygen Systemp. 385
Manual Plug-In Systemp. 386
Diluter-Demand Crew Oxygen Masksp. 387
Plug-In Masksp. 388
Oxygen Supply Cylinderp. 388
Oxygen System Controlsp. 388
Oxygen Durationp. 388
Oxygen Duration Computationp. 389
Time of Useful Consciousnessp. 390
Physiological Trainingp. 390
What Is It?p. 390
Who Needs It?p. 390
Where Can You Get It?p. 390
How Long is the Course?p. 390
What Is Contained in the Course?p. 390
What Are the Prerequisites for Training?p. 391
How Do You Apply For Training?p. 391
How Can You Get Further Information?p. 391
Servicing the Oxygen Systemp. 391
Filling the Oxygen Systemp. 392
King Air C90A and C90B Capacityp. 392
Oxygen Cylinder Retestingp. 392
Questionsp. 393
Illustrationsp. 383
Figure 17-1. Oxygen System Schematic—Typical C90Ap. 385
Figure 17-2. Plug-in Type Oxygen Maskp. 386
Figure 17-3. Oxygen Mask Donnedp. 386
Figure 17-4. Crew Oxygen Maskp. 386
Figure 17-5. Oxygen Cylinder Installationp. 387
Figure 17-6. Oxygen System Control Handlep. 387
Figure 17-7. Oxygen Pressure Gagep. 387
Figure 17-8. Oxygen Pressure Gagep. 388
Figure 17-9. Percent of Usable Oxygen Capacityp. 389
Figure 17-10. FAA Altitude Chamberp. 391
Appendix A Symbols, Abbreviations, and Terminologyp. 394
Contentsp. 394
Airspeedp. 395
Meteorologicalp. 396
Powerp. 396
Control and Instrumentp. 397
Graph and Tabularp. 397
Weight and Balancep. 398
Avionicsp. 399

Coverage spans the full range of C90-series systems, including the Pratt & Whitney PT6A-21 and PT6A-135A engines, propeller governing and reversing, electrical distribution and bus isolation, fuel transfer and crossfeed, pressurization and environmental control, hydraulic landing gear, and the complete avionics suite. Dedicated chapters on the master warning system and annunciator panel help pilots interpret and respond to system warnings correctly.

Who This Manual Is For

This manual suits pilots studying for a King Air C90 type rating, current C90 pilots refreshing system knowledge, training departments building internal course material, and owners who want a deeper understanding of how their aircraft’s systems work. The document covers the C90A, C90B, and C90GT in a single volume, with model-specific differences identified throughout.

Get the Complete FlightSafety King Air C90A/B/GT Training Course

Whether you are preparing for simulator training, studying for an oral exam, or simply want a complete systems reference for the King Air C90A, C90B, or C90GT, this training manual gives you the depth you need in one PDF.

The manual supports detailed study of every major aircraft system: engine operation and limits, propeller control, electrical distribution, fuel management, pressurization, avionics, ice protection, landing gear, and emergency procedures. Having the correct system descriptions and operating limitations in one place helps you prepare properly, avoid misdiagnosis, and operate the aircraft within its approved envelope.

Instant PDF delivery after purchase. No shipping, no waiting. Read on any device and print the chapters you need for study or the flight bag.

IMAGES PREVIEW

King Air C90A C90B C90GT Pilot Training Manual - FlightSafety Complete Systems Course — PDF page 14 preview
King Air C90A C90B C90GT Pilot Training Manual - FlightSafety Complete Systems Course — PDF page 15 preview
King Air C90A C90B C90GT Pilot Training Manual - FlightSafety Complete Systems Course — PDF page 129 preview

Reviews

There are no reviews yet.

Be the first to review “King Air C90A C90B C90GT Pilot Training Manual – FlightSafety Complete Systems Course”

What Our Customers Say

★★★★★ Live reviews from customers
Loading customer reviews...

🌟 Related Products

Discover more professional manuals for your equipment

-37% OFF
Cabin Crew Training Manual - Flight Attendant Course Training Guide
-33% OFF
Cessna Citation CJ2+ Pilot Training Manual - Revision 1.1 July 2014 PDF
-43% OFF
Diamond DA40 Series Austro Engine Maintenance Type Training B1.2 C May 2010
-37% OFF
Basic Aircraft Maintenance Training Handbook Module 21 - Maintenance Management PDF
0
    0
    Your Cart
    Your cart is emptyReturn to Shop
    Start Downloading your Manual immediately by proceeding to checkout page
    Continue Shopping
    🛒
    Recently Purchased
    🕒 verified order