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Cessna Grand Caravan 208B (675 SHP) Pilot’s Operating Handbook & FAA Approved Flight Manual – Revision 23

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Complete Cessna Grand Caravan 208B (675 SHP) Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual, Revision 23. Covers PT6A-114A engine, all systems, limitations, emergency and normal procedures, performance charts, weight and balance, and all Section 9 supplements S1 through S66.

SKU: CESSNA-208B-POH-REV23-HD Category: Tags: , , , Vendor: Equipment Repair Hub
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Description

Cessna Grand Caravan 208B (675 SHP) Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual

This is the complete Pilot’s Operating Handbook (POH) and FAA Approved Airplane Flight Manual for the Cessna Grand Caravan 208B equipped with the Pratt & Whitney Canada PT6A-114A engine flat-rated at 675 shaft horsepower. Issued as Revision 23 dated 4 May 2007 in the Training Edition format, this document gathers the full basic manual plus every Section 9 supplement into one reference covering Serial 208B0179, 208B0230 and On, and Serials 208B0001 through 208B0178 and 208B0180 through 208B0229 modified by SK208-80.

The Grand Caravan 208B is a single-engine, high-wing turboprop built for utility and commuter work, and this handbook reflects that mission with cargo-version and passenger-version data presented side by side where the two diverge. Everything an operator or technician needs to understand the aircraft β€” from preflight and engine start through cruise, descent, landing and securing β€” is laid out section by section using the standard GAMA-1 handbook format.

File Details

  • Manual type: Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual
  • Brand / Manufacturer: Cessna Aircraft Company
  • Model: 208B (675 SHP) Grand Caravan
  • Engine: Pratt & Whitney Canada PT6A-114A free-turbine turboprop, 675 SHP
  • Document part number: D1329-23-13PH
  • Original issue: 1 May 1990
  • Revision: Revision 23, 4 May 2007
  • Edition: Training Edition
  • Language: English
  • File format: PDF

Chapters Covered

The handbook is organized into nine sections. The basic manual carries the core operational content, and Section 9 gathers the supplements that adapt the aircraft for optional systems and special operations.

IMAGES PREVIEW

Cessna Grand Caravan 208B (675 SHP) Pilot's Operating Handbook & FAA Approved Flight Manual - Revision 23 β€” PDF page 3 preview
Cessna Grand Caravan 208B (675 SHP) Pilot's Operating Handbook & FAA Approved Flight Manual - Revision 23 β€” PDF page 434 preview
Cessna Grand Caravan 208B (675 SHP) Pilot's Operating Handbook & FAA Approved Flight Manual - Revision 23 β€” PDF page 459 preview

  • Section 1 β€” General: descriptive data, engine and propeller description, fuel and oil, maximum certificated weights, standard airplane weights, cabin and entry door dimensions, baggage/cargo compartment dimensions, specific loadings, symbols, abbreviations, terminology, warnings, cautions and notes
  • Section 2 β€” Limitations: airspeed limitations and indicator markings, power plant limitations, power plant instrument markings, miscellaneous instrument markings, preflight visual and tactile check, weight limits, center of gravity limits, maneuver limits, flight load factor limits, flight crew limits, kinds of operation limits, required equipment for day VFR, night VFR, IFR and flight into known icing, cold weather operations, fuel limitations, maximum operating altitude, outside air temperature limits, maximum passenger seating limits, flap limitations, Type II/III/IV anti-ice fluid takeoff limitations, flight in known icing visual cues, placards
  • Section 3 β€” Emergency Procedures: operational checklists and amplified procedures covering engine failures, airstarts (starter assist and no starter assist), emergency landing without engine power, precautionary landing with engine power, ditching, smoke and fire, icing, static source blockage, spins, engine malfunctions, fuel system malfunctions, flap system malfunctions, landing gear malfunctions, electrical power supply system malfunctions, emergency descent, inadvertent opening of doors in flight, emergency exits
  • Section 4 β€” Normal Procedures: speeds for normal operation, preflight inspection, before starting engine, starting engine (battery and auxiliary power), engine clearing, engine ignition, inertial separator procedures, taxiing, before takeoff, takeoff (normal, short field, Type II/III/IV anti-ice fluid), enroute climb, cruise climb, maximum performance climb, cruise, descent, before landing, landing (normal, short field, balked), after landing, shutdown and securing, overspeed governor check, autopilot checks, standby power check, known icing check, amplified procedures, cold weather operation, high altitude operation, engine compressor stalls, noise characteristics
  • Section 5 β€” Performance: use of performance charts, sample problem, airspeed calibration (normal and alternate static source), altimeter correction, pressure conversion, temperature conversion, ISA conversion and operating temperature limits, stall speeds, wind components, maximum engine torque for takeoff, maximum engine torque for climb, takeoff distance, rate of climb, climb gradient, maximum rate of climb, cruise climb, balked landing climb, time/fuel/distance to climb, cruise performance tables at altitudes from 2,000 through 24,000 feet, cruise maximum torque, fuel and time required, range profile, endurance profile, time/fuel/distance to descend, landing distance
  • Section 6 β€” Weight & Balance / Equipment List: airplane weighing form, sample weight and balance record, airplane weighing procedures, weight and balance, weight and balance plotter, loading manifest, crew/passenger loading, baggage/cargo loading, cabin area loading, cargo pod loading, maximum zone/compartment loadings, center of gravity precautions, cargo load restraint, transportation of hazardous materials, equipment list
  • Section 7 β€” Airplane & Systems Description: airframe, cargo pod, flight controls, trim systems, instrument panel, annunciator panel, ground control, wing flap system, landing gear, seats, cabin entry doors, cargo doors, windows, control locks, engine, engine controls, engine instruments, new engine break-in, lubrication, ignition, air induction, inertial separator, exhaust, fuel system, brake system, electrical system, lighting, cabin heating/ventilating/defrosting, oxygen, pitot-static system and instruments, vacuum system and instruments, stall warning, avionics support equipment, cabin features, miscellaneous equipment
  • Section 8 β€” Handling, Service & Maintenance: identification plate, Cessna Owner Advisories, publications, airplane file, inspection periods, FAA required inspections, Cessna Progressive Care, Cessna Customer Care Program, CESCOM, Engine Condition Trend Monitoring, pilot-conducted preventive maintenance, alterations or repairs, ground handling (towing, parking, tie-down, jacking, leveling), servicing (oil, fuel, landing gear, oxygen, ground deice/anti-ice operations), cleaning and care (windshield and windows, painted surfaces, stabilizer abrasion boots, deice/anti-ice boot care, propeller care, engine care, interior care), prolonged out-of-service care, bulb replacement during flight
  • Section 9 β€” Supplements: individual supplements covering known icing equipment, emergency locator transmitters, King and Bendix/King flight control and autopilot systems, digital ADF, high altitude takeoff and landing, parachute jumping installations, GPS navigation systems, Russian and China certification configurations, 30-amp power outlets, GPS/KLN 94, KLN 94 interfaced with KNI 582 RMI, hot weather operations, ARNAV MFD 5200 and Geolink, stand-alone VFR GPS, BFGoodrich SkyWatch SKY497 traffic advisory, BFGoodrich Stormscope WX-1000+/1000E and WX-500, Arctic Diesel fuel, 300-amp starter-generator, Shadin Mini-Flow fuel totalizer, King KY-196A digital comm, Bendix/King KN 53 nav receiver, light weight landing with cargo pod, oxygen systems in several configurations, seating options for international operations, Bendix/King KFC-225 flight control, dual HSI and FDI with KFC-225, Fairchild F1000 and FA2100 recorders, Bendix/King KRA-405 radar altimeter, five-place seating option for cargo version, Honeywell KMH 880 IHAS, Honeywell KTA 870 TAS, Garmin GMA 340 audio panel, Garmin GTX 327 and GTX 330 transponders, Spanish commercial night IMC operations, fuel totalizer system, British CAA kit configurations, Altair ADAS+ engine trend monitor, Bendix/King KI 825 EHSI, Bendix/King KT 73 transponder, US-configured aircraft on UK registration, 12 VDC power outlets, TKS ice protection for cargo pod equipped aircraft, Artex ME406 ELT, Honeywell KHF 1050 HF transceiver, Configuration Deviation List, and standby electrical system supplements for 75-amp and 81-amp alternator installations

Working through this handbook gives a technician or pilot the complete operational envelope of the Grand Caravan 208B: every limitation the FAA approved, every emergency checklist to commit to memory, every normal procedure from preflight through shutdown, all the performance charts needed to plan a flight, the weight and balance method for cargo and passenger loadings, a full systems description for troubleshooting, and the servicing and inspection guidance that keeps the aircraft airworthy. The Section 9 supplements extend that coverage to just about every avionics package, seating configuration, certification variant and optional system that has been installed on the type.

Complete PDF Bookmark Tree

Complete Bookmarks

The complete bookmarks in the β€œCessna Grand Caravan 208B (675 SHP) Pilot's Operating Handbook & FAA Approved Flight Manual – Revision 23” are as follows:

Cessna Grand Caravan Airplane Flight Manual P/N D1329R23-13PHp. 1
Title Pagep. 3
Introductionp. 5
Congratulationsp. 6
Performance – Specifications Cargo Versionp. 7
Performance – Specifications Passenger Versionp. 9
Coveragep. 11
Original Issue and Revisionsp. 11
Revision Filing Instructionsp. 13
Regular Revisionsp. 13
Temporary Revisionsp. 14
Identifying Revised Materialp. 14
Warnings, Cautions and Notesp. 15
Temporary Revision TR02p. 12
Log of Temporary Revisionsp. 16
Log of Effective Pagesp. 20
Table of Contentsp. 26
Section 1 – Generalp. 27
Three Viewp. 28
Introductionp. 30
Descriptive Datap. 31
Enginep. 31
Propeller (Hartzell)p. 31
Propeller (McCauley)p. 31
Fuelp. 32
Oilp. 33
Maximum Certified Weightsp. 34
Standard Airplane Weightsp. 34
Cabin and Entry Door Dimensionsp. 35
Baggage/Cargo Compartment And Cargo Door Entry Dimensionsp. 35
Specific Loadingsp. 35
Symbols, Abbreviations, and Terminologyp. 36
General Airspeed Terminology and Symbolsp. 36
Meteorological Terminologyp. 37
Engine Power Terminologyp. 37
Airplane Performance and Flight Planning Terminologyp. 39
Weight And Balance Terminologyp. 39
Autopilot/Flight Director Terminologyp. 41
Warning, Cautions, And Notesp. 42
Ground Operations Stall Warning Disable Switchp. 42
Section 2 – Limitationsp. 43
Introductionp. 44
Airspeed Limitationsp. 45
Airspeed Indictor Markingsp. 46
Power Plant Limitationsp. 47
Temporary Revision TR13p. 48
Power Plant Instrument Markingsp. 53
Miscellaneous Instrument Markingsp. 54
Preflightp. 55
Visual and Tactile Checkp. 55
Weight Limitsp. 56
Center of Gravity Limitsp. 56
Maneuver Limitsp. 56
Flight Load Factor Limitsp. 57
Flight Crew Limitsp. 57
Kinds of Operations Limitsp. 57
Required Equipmentp. 58
Day VFRp. 58
Night VFRp. 59
IFRp. 59
Flight into Known Icingp. 59
Temporary Revision TR05p. 61
Fuel Limitationsp. 60
Maximum Operating Altitude Limitsp. 64
Outside Air Temperature Limitsp. 65
Temporary Revision TR04p. 65
Maximum Passenger Seating Limitsp. 65
Other Limitationsp. 65
Flap Limitationsp. 65
Type II, Type III or Type IV Anti-Ice Fluid Takeoff Limitationsp. 65
Flap Limitationsp. 65
Airspeed Limitationsp. 65
Temporary Revision TR06p. 67
Flight in Known Icing Visual Cuesp. 69
Placardsp. 70
Section 3 – Emergency Proceduresp. 82
Temporary Revision TR09p. 84
Introductionp. 87
Airspeeds for Emergency Operationp. 87
Operational Checklistsp. 88
Engine Failuresp. 88
Engine Failure During Takeoff Rollp. 88
Engine Failure Immediately After Takeoffp. 88
Engine Failure During Flightp. 88
Engine Flameout During Flightp. 89
Airstartp. 89
Starter Assist (Preferred Procedure)p. 89
No Starter Assistp. 90
Forced Landingsp. 92
Emergency Landing Without Engine Powerp. 92
Precautionary Landing With Engine Powerp. 92
Ditchingp. 93
Smoke and Firep. 93
Engine Fire In Flight (Red ENGINE FIRE Annunciator ON or OFF)p. 93
Electrical Fire In Flightp. 94
Cabin Firep. 95
Wing Firep. 96
Cabin Fire During Ground Operationsp. 96
Engine Fire During Start On Ground (Red ENGINE FIRE Annunciator On or OFF)p. 97
Icingp. 97
The Following Weather Conditions May Be Conducive To Severe In-Flight Icingp. 97
Procedures For Exiting the Severe Icing Environmentp. 98
Temporary Revision TR07p. 101
Inadvertent Icing Encounterp. 99
Static Source Blockage (Erroneous Instrument Reading Suspected)p. 100
Engine Malfunctionsp. 103
Loss of Oil Pressure (Red OIL PRESSURE LOW Annunciator On)p. 103
Fuel Control Unit Malfunction In the Pneumatic or Governor Sections (Engine Power Falls Back to Idle)p. 103
Gear Box Contamination (Amber Chip Detector Annunciator On)p. 103
Fuel System Malfunction/Inadvertent Fuel Flow Interruption Proceduresp. 104
Loss of Fuel Pressure (Amber FUEL PRESS LOW Annunciator On)p. 104
Fuel Flow Interruption To Fuel Reservoir (Red Reservoir Fuel Low Annunciator On)p. 104
Fuel Tank Selector Off During Engine Start (Red Fuel Select Off Annunciator On and Both Fuel Selector Warning Horns Activated)p. 104
Fuel Level Low With Single Tank Selected (Red Fuel Select Off and Amber Left or Right Fuel Low Annunciator On and Fuel Selector Warning Horn Activated)p. 105
Flap System Malfunction Proceduresp. 105
Asymmetric Flap Extension Or Sudden Flap Retraction On One Sidep. 105
Flaps Fail To Extend or Retractp. 105
Landing Gear Malfunction Proceduresp. 106
Landing With Flat Main Tirep. 106
Landing With Flat Nose Tirep. 107
Electrical Power Supply System Malfunctionsp. 107
Battery Temperature High (Amber Battery Hot Annunciator On)p. 107
Battery Overheated (Red Battery Overheat Annunciator On)p. 108
Temporary Revision TR08p. 108
Temporary Revision TR11p. 115
Generator Failure (Red Voltage Low And/Or Red Generator Off Annunciators On)p. 108
Inverter Failure (Amber Inverter Inop Annunciator On)p. 117
Starter Contactor Does Not Disengage After Engine Start (Amber Starter Energized Annunciator On)p. 117
Emergency Descent Proceduresp. 117
Rough Airp. 117
Smooth Airp. 118
Inadvertent Opening Of Airplane Door In Flightp. 118
Upper Half Of Cargo Door Or Upper Half of Passenger Airstair Door Open (Red Door Warning Annunciator On)p. 118
Lower Half of Passenger Airstair Door Openp. 118
Right or Left Crew Doors Openp. 118
Cargo Pod Door(s) Openp. 118
Amplified Proceduresp. 119
Engine Failurep. 119
Figure 3-1 Maximum Glidep. 120
Forced Landingsp. 123
Landing Without Elevator Controlp. 124
Smoke and Firep. 124
Emergency Operation In Clouds (Airplanes with KFC-150 or KFC-225 Autopilot)p. 126
Emergency Operation in Clouds (Airplanes with KFC-250 Autopilot)p. 126
Inadvertent Flight Into Icing Conditionsp. 126
Static Source Blockedp. 127
Spinsp. 127
Engine Malfunctionsp. 128
Loss of Oil Pressurep. 128
Fuel Control Unit Malfunction In The Pneumatic or Governor Sectionsp. 128
Gear Box Contaminationp. 129
Fuel System Malfunction/Inadvertent Fuel Flow Interruption Proceduresp. 130
Electrical Power Supply System Malfunctionsp. 131
Battery Malfunctions (Ni-Cad Battery Only)p. 131
Generator or Main Bus Malfunctionsp. 132
Loss of Electrical Powerp. 133
Partial Avionics Power Failurep. 133
Standby Electrical System Malfunctionsp. 134
Inadvertent Opening of Airplane Doors In Flightp. 135
Emergency Exitsp. 135
Figure 3-2 Emergency Exitsp. 136
Section 4 – Normal Proceduresp. 137
Introductionp. 139
Speeds For Normal Operationp. 139
Checklist Proceduresp. 140
Temporary Revision TR17p. 140
Preflight Inspection Warningsp. 161
Preflight Inspectionp. 162
Cabinp. 162
Left Sidep. 163
Left Wing, Leading Edgep. 164
Left Wing, Trailing Edgep. 165
Figure 4-2 Measures Fuel Depth vs Fuel Quantityp. 166
Empennagep. 167
Right Wing, Trailing Edgep. 167
Right Wing, Leading Edgep. 168
Nosep. 169
Before Starting Enginep. 171
Starting Engine (Battery Start)p. 172
Starting Engine (Auxiliary Power Start)p. 173
Taxiingp. 177
Temporary Revision TR18p. 175
Before Takeoffp. 177
Takeoffp. 179
Normal Takeoffp. 179
Short Field Takeoffp. 180
Type II, Type III, or Type IV Anti-Ice Fluid Takeoffp. 180
Enroute Climbp. 180
Cruise Climbp. 180
Maximum Performance Climbp. 181
Cruisep. 182
Descentp. 182
Before Landingp. 183
Landingp. 183
Normal Landingp. 183
Short Field Landingp. 184
Balked Landingp. 184
After Landingp. 184
Shutdown And Securing Airplanep. 185
System Checksp. 186
Overspeed Governor Checkp. 186
Autopilot Check (King KFC-150)p. 186
Before Takeoff Reliability Testsp. 186
Autopilot Check (King KAP-150)p. 187
Before Takeoff Reliability Testsp. 187
Autopilot Check (Bendix/King KFC-225)p. 189
Before Takeoff Reliability Testsp. 189
Autopilot Check (Bendix/King KFC-250 Category I)p. 190
Preflightp. 190
Autopilot Check (Bendix/King KFC-250 Category II)p. 193
Preflightp. 193
Standby Power Checkp. 196
Known Icing Checkp. 196
Preflight Inspectionp. 196
Before Takeoffp. 197
Amplified Proceduresp. 199
Preflight Inspectionp. 199
Before Starting Enginep. 201
Starting Enginep. 202
Engine Clearing Procedures (Dry Motoring Run)p. 206
Engine Ignition Proceduresp. 207
Engine Inertial Separator Proceduresp. 207
Taxiingp. 208
Figure 4-3 Taxing Diagramp. 211
Temporary Revision TR19p. 208
Before Takeoffp. 212
Takeoffp. 213
Power Settingp. 213
Wing Flap Settingsp. 213
Short Field Takeoffp. 213
Type II, Type III or Type IV Anti-Ice Fluid Takeoffp. 214
Crosswind Takeoffp. 214
Enroute Climbp. 215
Cruisep. 216
Figure 4-4 Sample Cruise Performance Tablep. 217
Stallsp. 219
Landingp. 220
Normal Landingp. 220
Short Field Landingp. 221
Crosswind Landingp. 221
Balked Landingp. 222
After Shutdownp. 222
Cold Weather Operationp. 222
High Altitude Operationp. 223
Engine Compressor Stallsp. 223
Noise Characteristicsp. 224
Section 5 – Performancep. 225
Introductionp. 228
Use of Performance Chartsp. 228
Sample Problemp. 229
Takeoffp. 230
Cruisep. 231
Fuel Requiredp. 231
Landingp. 234
Temporary Revision TR20p. 236
Figure 5-1 Airspeed Calibration – Normal Static Souce/Alternate Static Sourcep. 235
Temporary Revision TR21p. 240
Figure 5-2 Altimeter Correction – Alternate Static Sourcep. 240
Figure 5-3 Pressure Conversion – Inches of Mercury To Millibarsp. 244
Figure 5-4 Temperature Conversion Chartp. 245
Figure 5-5 ISA Conversion And Operating Temperature Limitsp. 246
Figure 5-6 Stall Speedsp. 247
Figure 5-7 Wind Compnentsp. 248
Figure 5-8 Maximum Engine Torque For Takeoffp. 249
Figure 5-8A Maximum Engine Torque For Climbp. 250
Airplanes With Cargo Pod Installedp. 251
Figure 5-9 Takeoff Distance, Short Field – 8750 lbs, 8300 lbs Figure Takeoff Distance, Short Field – 7800 lbs, 7300 lbsp. 251
Figure 5-9A Takeoff Distance, 0Β° Flaps – 8750 lbs Takeoff Distance, 0Β° Flaps – 8300, 7800, 7300 lbsp. 253
Figure 5-10 Rate of Climb – Takeoff Flap Settingp. 255
Figure 5-11 Climb Gradient – Takeoff Flap Settingp. 256
Figure 5-12 Maximum Rate Of Climb – Flaps Upp. 257
Figure 5-13 Takeoff Climb Gradient – Flaps Upp. 258
Figure 5-14 Cruise Climb – Flaps Up – 115 KIASp. 259
Figure 5-15 Rate of Climb – Balked Landingp. 260
Figure 5-16 Time, Fuel, And Distance To Climbp. 261
Figure 5-17 Cruise Performancep. 263
Figure 5-17A Cruise Maximum Torquep. 276
Figure 5-18 Fuel And Time Required – Maximum Cruise Powerp. 281
Figure 5-19 Fuel And Time Required – Maximum Range Powerp. 283
Figure 5-20 Range Profilep. 285
Figure 5-21 Endurance Profilep. 286
Figure 5-22 Time, Fuel, And Distance To Descendp. 287
Figure 5-23 Landing Distancep. 288
Airplanes Without Cargo Podp. 290
Figure 5-24 Takeoff Distance Shortfieldp. 290
Figure 5-24A Takeoff Distancep. 292
Figure 5-25 Rate Climb – Takeoff Flap Settingp. 294
Figure 5-26 Climb Gradient – Takeoff Flap Settingp. 295
Figure 5-27 Maximum Rate Of Climb – Flaps Upp. 296
Figure 5-28 Takeoff Climb Gradient – Flaps Upp. 297
Figure 5-29 Cruise Climb – Flaps Up – 115 KIASp. 298
Figure 5-30 Rate of Climb – Balked Landingp. 299
Figure 5-31 Time, Fuel, And Distance To Climbp. 300
Figure 5-32 Cruise Performancep. 302
Figure 5-32A Cruise Maximum Torquep. 315
Figure 5-33 Fuel And Time Required – Maximum Cruise Powerp. 320
Figure 5-34 Fuel and Time Required – Maximum Range Powerp. 322
Figure 5-35 Range Profilep. 324
Figure 5-36 Endurance Profilep. 325
Figure 5-37 Time, Fuel, And Distance To Descendp. 326
Figure 5-38 Landing Distancep. 327
Section 6 – Weight and Balance/Equipment Listp. 329
Introductionp. 330
Airplane Weighing Formp. 331
Sample Weight and Balance Recordp. 332
Temporary Revision TR01p. 333
Airplane Weighing Proceduresp. 334
Weight and Balancep. 336
Weight and Balance Plotterp. 339
Weight and Balance Record (Loading Manifest)p. 339
Crew/Passenger Loadingp. 344
Baggage/Cargo Loadingp. 345
Cabin Areap. 345
Cargo Podp. 350
Maximum Zone/Compartment Loadingsp. 350
Center of Gravity Precautionsp. 351
Cargo Load Restraintp. 352
Prevention Of Movmentp. 352
Loading Of Piercing Or Penetrating Itemsp. 353
Transportation of Hazardous Materialp. 354
Equipment Listp. 354
Section 7 – Airplane and System Descriptionp. 387
Introductionp. 392
Airframep. 392
Cargo Podp. 394
Flight Controlsp. 394
Trim Systemsp. 394
Instrument Panelp. 399
Right Flight Intrument Panelp. 400
Left Sidewall Switch and Circuit Breaker Panelp. 400
Annunciatorp. 413
Temporary Revision TR010p. 409
Ground Controlp. 414
Wing Flap Systemp. 414
Landing Gear Systemp. 416
Baggage/Cargo Compartmentp. 416
Seatsp. 417
Pilots And Front Passenger Seatsp. 417
Aft Passengers Seats (Commuter) (Passenger Version)p. 418
Aft Passengers Seats (Utility) (Passenger Version)p. 418
Headrestsp. 423
Seat Belts, and Shoulder Harnessp. 423
Seat Belts, Strap and Shoulder Harness (Pilot/Front Passenger Seats)p. 423
Seat Belts (Aft Seats in Passenger Version)p. 424
Shoulder Harnesses (Aft Seats in Passenger Version)p. 424
Cabin Entry Doorsp. 425
Crew Entry Doorsp. 425
Passenger Entry Doors (Passenger Version Only)p. 426
Cargo Doorsp. 429
Cabin Windowsp. 431
Control Locksp. 431
Enginep. 432
Engine Controlsp. 435
Power Leverp. 435
Emergency Power Leverp. 436
Propeller Control Leverp. 438
Fuel Condition Leverp. 438
Quadrant Friction Lockp. 439
Engine Instrumentsp. 439
Torque Indicatorp. 439
Propeller RPM Indicatorp. 440
ITT Indicatorp. 440
Ng RPM Indicatorp. 440
Fuel Flow Indicatorp. 440
Oil Pressure Gagep. 441
Oil Temperature Gagep. 441
New Engine Break-In and Operationp. 441
Engine Lubrication Systemp. 442
Ignition Systemp. 444
Air Induction Systemp. 445
Inertial Separator Systemp. 445
Exhaust Systemp. 447
Engine Fuel Systemp. 447
Cooling Systemp. 448
Starting Systemp. 449
Engine Accessoriesp. 449
Oil Pumpp. 450
Fuel Pumpp. 450
Ng Tachometer-Generatorp. 450
Propeller Tachometer-Generatorp. 451
Torquemeterp. 451
Starter/Generatorp. 451
Interturbine Temperature Sensing Systemp. 452
Propeller Governorp. 452
Propeller Overspeed Governorp. 453
Engine Mountp. 453
Engine Fire Detection Systemp. 453
Engine Gear Reduction Systemp. 454
Chip Detectors (Optional)p. 454
Oil Breather Drain Canp. 455
Propellerp. 455
Overspeed Governor Test Switchp. 456
Fuel Systemp. 457
Firewall Fuel Shutoff Valvep. 461
Fuel Tank Selectorsp. 461
Fuel Selectors Off Warning Systemp. 462
Auxiliary Boost Pump Switchp. 463
Fuel Flow Indicatorp. 463
Fuel Quantity Indicatorsp. 464
Wing Tank Fuel Low Warning Annunciatorsp. 464
Reservoir Fuel Low Warning Annunciatorp. 465
Fuel Pressure Low Warning Annunciatorp. 465
Auxiliary Fuel Pump On Annunciatorp. 465
Drain Valvesp. 466
Fuel Drain Canp. 467
Fuel Pump Drain Reserviorp. 467
Brake Systemp. 467
Electrical Systemp. 469
Generator Control Unitp. 469
Ground Power Monitorp. 469
Battery Switchp. 470
Starter Switchp. 470
Ignition Switchp. 470
Generator Switchp. 470
Avionics Power Switchp. 471
Avionics Bus Tie Switchp. 475
Inverter Selector Switch (Airplanes with KFC-250 Autopilot Only)p. 475
External Power Switchp. 476
Circuit Breakersp. 476
Volt/Ammeter And Selector Switchp. 477
Annunciator Lightsp. 477
Ground Service Plug Receptaclep. 477
Lighting Systemsp. 478
Exterior Lightingp. 478
Navigation Lightsp. 478
Landing Lightsp. 478
Taxi/Recognition Lightsp. 479
Strobe Lightsp. 479
Flashing Beacon Lightp. 479
Courtesy Lightsp. 480
Interior Lightingp. 480
Left Flight Panel/Left Flood Lighting Control Knobsp. 480
Right Flight Panel/Right Flood Lighting Control Knobsp. 481
Lower Panel, Pedestal, Overhead, Switch/Circuit Breaker Lighting Control Knobsp. 481
Engine Instruments/Radio Lighting Control Knobsp. 481
Control Wheel Maplightp. 482
Cabin Lightsp. 482
Passenger Reading Lights (Passenger Version Only)p. 482
No Smoking/Seat Belt Sign (Passenger Version Only)p. 483
Cabin Heating, Ventilating And Defrosting Systemp. 483
Temporary Revision TR24p. 484
Bleed Air Heat Switchp. 484
Temperature Selector Knobp. 484
Mixing Air Push-Pull Controlp. 489
AFT/Forward Cabin Push-Pull Controlp. 490
Defrost/Forward Cabin Push-Pull Controlp. 490
Cabin Heat Firewall Shutoff Knobp. 490
Vent Air Control Knobsp. 491
Instrument Panel Vent Knobsp. 491
Ventilating Outletsp. 491
Oxygen Systemp. 492
Pitot-Static System And Instrumentsp. 492
Right Flight Instrument Panel Pitot-Static Systemp. 493
Airspeed Indicatorsp. 494
Vertical Speed Indicatorsp. 494
Altimetersp. 494
Vacuum System And Intrumentsp. 495
Attitude Indicator (Right Flight Instrument Panel)p. 497
Directional Indicator (Right Flight Instrument Panel)p. 497
Suction Gagep. 497
Vacuum-Low Warning Annunciatorp. 498
Outside Air Temperature (OAT) Gagep. 498
Stall Warning Systemp. 498
Avionics Support Equipmentp. 499
Avionics Cooling Fanp. 499
Microphone/Speaker And Mic/Phone Jacksp. 500
Static Dischargesp. 500
Cabin Featuresp. 501
Cabin Fire Extinguisherp. 501
Sun Visorsp. 502
Map and Storage Compartmentsp. 502
Miscellaneous Equipmentp. 503
Engine Inlet Covers and Propeller Anchorp. 503
Crew Entry Step Assemblyp. 503
Cargo Barrier And Netsp. 503
Cargo Partitionsp. 504
Cargo Door Restraining Netp. 504
Cargo/Airplane Tie Down Equipmentp. 504
Hoisting Ringsp. 505
Relief Tubep. 505
Oil Quick-Drain Valvep. 505
Section 8 – Handling, Service, and Maintenancep. 506
Introductionp. 507
Identification Platep. 508
Cessna Owner Advisoriesp. 508
Publicationsp. 509
Airplane Filep. 510
Airplane Inspection Periodsp. 511
FAA Required Inspectionsp. 511
Cessna Progressive Carep. 511
Cessna Customer Care Programp. 512
CESCOM Systemp. 513
Engine Condition Trend Monitoringp. 513
Pilot Conducted Preventive Maintenancep. 514
Alterations Or Repairsp. 514
Ground Handlingp. 515
Towingp. 515
Parkingp. 516
Tie-Downp. 516
Jackingp. 517
Levelingp. 519
Servicingp. 520
Temporary Revision TR12p. 522
Oilp. 521
Temporary Revision TR13p. 525
Fuelp. 528
Landing Gearp. 534
Oxygenp. 534
Ground Deice/Anti-Ice Operationsp. 534
Temporary Revision TR22p. 543
Cleaning And Carep. 552
Windshield and Windowsp. 552
Painted Surfacesp. 556
Stabilizer Abrasion Boot Carep. 556
Deice/Anti-Ice Boot Carep. 557
Propeller Carep. 559
Engine Carep. 560
Interior Carep. 563
Prolonged Out-Of-Service Carep. 564
Bulb Replacement During Flightp. 565
Figure 8-6 Bulb Replacementp. 566
Section 9 – Supplementsp. 567
Log of Supplementsp. 567
SUPPLEMENT S1 – KNOWN ICING EQUIPMENTp. 576
GENERALp. 578
WING, WING STRUT, MAIN LANDING GEAR LEG, CARGO POD NOSECAP AND STABILIZER DEICE BOOTSp. 579
PROPELLER ANTI-ICE BOOTSp. 581
WINDSHIELD ANTI-ICE PANELp. 582
PITOT/STATIC HEAT SYSTEMSp. 583
STANDBY ELECTRICA L SYSTEMp. 584
WING INSPECTION LIGHTp. 585
WINDSHIELD ICE DETECTOR LIGHT (IF INSTALLED)p. 586
LOW AIRSPEED AWARENESS SYSTEMp. 586
AIRSPEED REMINDER BUG (IF INSTALLED)p. 586
ENGINE INERTIAL SEPARATOR AND HEATED STALLWARNING SYSTEMSp. 586
LIMITATIONSp. 587
REQUIRED TRAININGp. 587
PREFLIGHTp. 587
VISUAL/TACTILE CHECKp. 588
WEIGHT LIMITSp. 588
REQUIRED EQUIPMENTp. 589
MAXIMUM OPERATING ALTITUDE L IMITSp. 589
ENVIRONMENTAL CONDITIONSp. 590
AUTOPILOT OPERATION IN ICING CONDITIONSp. 591
MINIMUM SPEED IN ICING CONDITIONSp. 592
FLAP SETTING IN ICING CONDITIONSp. 592
PLACARDSp. 593
EMERGENCY PROCEDURESp. 595
INADVERTENT ICING ENCOUNTER AT WEIGHTS ABOVE 8550 POUNDS (CARGO POD INSTALLED)p. 595
INADVERTENT ICING ENCOUNTER AT ALTITUDES ABOVE 20,000 FEETp. 595
ENGINE INERTIAL SEPARATOR MALFUNCTIONp. 596
PROPELLER ANTI-ICE SYSTEM MALFUNCTIONp. 596
PNEUMATIC DEICE BOOT MALFUNCTIONSp. 598
LEADING EDGE DEICE BOOTS REMAIN INFLATED(GREEN DEICE PRESSURE ANNUNCIATORILLUMINATED)p. 600
WINDSHIELD ANTI-ICE PANEL MALFUNCTIONp. 601
HE ATED PITOT/STATIC TUBE MALFUNCTIONp. 602
GENERATOR MALFUNCTION {RED GENERATOR OFFAND/OR AMBER STBY ELECT PWR ON ANNUNCIATORSILLUMINATED)p. 603
HEATED STALL WARNING TRANSDUCER MALFUNCTIONp. 603
LOW AIRSPEED (AMBER BELOW ICING MIN SPDANNUNCIATOR ILLUMINATED FLASHING AND AURALWARNING)p. 604
INADVERTENT ENCOUNTER WITH FREEZING RAIN ORFREEZING DRIZZLE OR OTHER PERFORMANCECRITICAL ICING SITUATIONp. 604
NORMAL PROCEDURESp. 606
PREFLIGHT INSPECTIONp. 606
ABBREVIATED PILOT CHECKLISTp. 607
BEFORE STARTING ENGINEp. 607
BEFORE TAKEOFFp. 607
TAKEOFFp. 608
IN FLIGHT (CLIMB, CRUISE, AND DESCENT)p. 608
BEFORE LANDINGp. 610
LANDINGp. 610
BALKED LANDINGp. 610
AFTER LANDINGp. 610
AMPLIFIED PROCEDURESp. 611
BEFORE TAKEOFFp. 611
IN FLIGHTp. 613
BEFORE LANDINGp. 619
LANDINGp. 620
BALKED LANDINGp. 620
PERFORMANCEp. 621
STALL SPEEDSp. 621
RATE OF CLIMBp. 621
PREFLIGHT PLANNINGp. 622
ENROUTE TOOL FOR EXITING ICINGp. 623
CRUISE PERFORMANCEp. 626
LANDING PERFORMANCEp. 628
SUPPLEMENT S2 – EMERGENCY LOCATOR TRANSMITTER (ELT) (SOCATA ELT 90) For FRENCH CERTIFIED AIRPLANESp. 629
GENERALp. 631
LIMITATIONSp. 633
EMERGENCY PROCEDURESp. 634
NORMAL PROCEDURESp. 635
PERFORMANCEp. 636
SUPPLEMENT S3 – KING FLIGHT CONTROL SYSTEM WITH DUAL FLIGHT DIRECTORS (TYPE KFC-150)p. 637
GENERALp. 639
LIMITATIONSp. 642
EMERGENCY PROCEDURESp. 643
NORMAL PROCEDURESp. 644
PERFORMANCEp. 647
SUPPLEMENT S4 – TAKEOFF PROCEDURES FOR AIRPORTS WITH GERMAN NOISE LIMITATIONSp. 648
GENERALp. 650
LIMITATIONSp. 650
EMERGENCY PROCEDURESp. 650
NORMAL PROCEDURESp. 651
CHECKLIST PROCEDURESp. 651
AMPLIFIED PROCEDURESp. 652
PERFORMANCEp. 652
(CARGO POD INSTALLED) – RATE OF CLIMB – TAKEOFF FLAP SETTING FLAPS 20 Β°p. 653
(CARGO POD INSTALLED) – CLIMB GRADIENT – TAKEOFF FLAP SETTING 20 Β°p. 654
(WITHOUT CARGO POD) – RATE OF CLIMB -TAKEOFF FLAP SETTING FLAPS 20 Β°p. 655
(WITHOUT CARGO POD) – CLIMB GRADIENT – TAKEOFF FLAP SETTING FLAPS 20 Β°p. 656
SUPPLEMENT S5 – BENDIX/KING DIGITAL ADF (TYPE KR-87 with Kl 227-01 INDICATOR)p. 657
GENERALp. 659
LIMITATIONSp. 663
EMERGENCY PROCEDURESp. 663
NORMAL PROCEDURESp. 663
TO OPERATE AS AN AUTOMATIC DIRECTION FINDERp. 663
ADF TEST (PRE-FLIGHT or IN-FLIGHT)p. 663
TO OPERATE BFOp. 664
TO OPERATE FLIGHT TIMERp. 664
TO OPERATE AS A COMMUNICATIONS RECEIVER ONLYp. 664
TO OPERATE ELAPSED TIME TIMER-COUNT UP MODEp. 664
TO OPERATE ELAPSED TIME TIMER-COUNT DOWN MODEp. 665
ADF OPERAION NOTESp. 665
PERFORMANCEp. 666
SUPPLEMENT – S6 – BENDIX/KING DUAL DIGITAL ADF SYSTEM (TYPE KR-87 with Kl 228-01 INDICATOR)p. 667
GENERALp. 669
LIMITATIONSp. 673
EMERGENCY PROCEDURESp. 673
NORMAL PROCEDURESp. 673
TO OPERATE AS AN AUTOMATIC DIRECTION FINDERp. 673
ADF TEST (PRE-FLIGHT or IN-FLIGHT)p. 673
TO OPERATE BFOp. 674
TO OPERATE FLIGHT TIMERp. 674
TO OPERATE AS A COMMUNICATIONS RECEIVER ONLYp. 674
TO OPERATE ELAPSED TIME TIMER-COUNT UP MODEp. 674
TO OPERATE ELAPSED TIME TIMER-COUNT DOWN MODEp. 675
ADF OPERAION NOTESp. 675
PERFORMANCEp. 676
SUPPLEMENT S7 – HIGH ALTITUDE TAKEOFF AND LANDING PERFORMANCE (ABOVE 12,000 FEET PRESSURE ALTITUDE)p. 677
GENERALp. 679
LIMITATIONSp. 679
EMERGENCY PROCEDURESp. 679
NORMAL PROCEDURESp. 679
PERFORMANCEp. 679
ENGINE TORQUE FOR TAKEOFFp. 680
TAKEOFF DISTANCE – SHORT FIELD (CARGO POD INSTALLED)p. 681
(CARGO POD INSTALLED) TAKEOFF DISTANCE (DRY GRASS GROUND ROLL) FLAPS 20Β°p. 683
(CARGO POD INSTALLED) TAKEOFF DISTANCE(GROUND ROLL DISTANCE AND TOTAL DISTANCE TO CLEAR 50 FEET) FLAPS UPp. 684
(CARGO POD INSTALLED) TAKEOFF DISTANCE (DRY GRASS GROUND ROLL) FLAPS UPp. 685
(CARGO POD INSTALLED) RATE OF CLIMB – TAKEOFF FLAP SETTING FLAPS 20Β°p. 686
(CARGO POD INSTALLED) CLIMB GRADIENT – TAKEOFF FLAP SETTING FLAPS 20Β°p. 687
(CARGO POD INSTALLED) TAKEOFF CLIMB GRADIENT FLAPS UPp. 688
(CARGO POD INSTALLED) CRUISE CLIMB FLAPS UP – 115 KIASp. 689
(CARGO POD INSTALLED) RATE OF CLIMB – BALKED LANDING FLAPS 30Β°p. 690
(CARGO POD INSTALLED) TIME, FUEL, AND DISTANCE TO CLIMB CRUISE CLIMB – 115 KIASp. 691
(CARGO POD INSTALLED) LANDING DISTANCE – SHORT FIELD FLAPS 30Β°p. 692
(WITHOUT CARGO POD) TAKEOFF DISTANCE – SHORT FIELD FLAPS 20Β°p. 694
(WITHOUT CARGO POD) TAKEOFF DISTANCE (DRY GRASS GROUND ROLL) FLAPS 20Β°p. 696
(WITHOUT CARGO POD) TAKEOFF DISTANCE(GROUND ROLL DISTANCE AND TOTAL DISTANCE TO CLEAR 50 FEET) FLAPS UPp. 697
(WITHOUT CARGO POD) TAKEOFF DISTANCE (DRY GRASS GROUND ROLL) FLAPS UPp. 698
(WITHOUT CARGO POD) RATE OF CLIMB – TAKEOFF FLAP SETTING FLAPS 20Β°p. 699
(WITHOUT CARGO POD) CLIMB GRADIENT – TAKEOFF FLAP SETTING FLAPS 20Β°p. 700
(WITHOUT CARGO POD) TAKEOFF CLIMB GRADIENT FLAPS UPp. 701
(WITHOUT CARGO POD) CRUISE CLIMB FLAPS UP – 115 KIASp. 702
(WITHOUT CARGO POD) RATE OF CLIMB – BALKED LANDING FLAPS 30Β°p. 703
(WITHOUT CARGO POD) TIME, FUEL, AND DISTANCE TO CLIMB CRUISE CLIMB – 115 KIASp. 704
(WITHOUT CARGO POD) LANDING DISTANCE – SHORT FIELD FLAPS 30Β°p. 705
SUPPLEMENT S8 – PARACHUTE JUMPING INSTALLATIONp. 707
GENERALp. 709
LIMITATIONSp. 714
EMERGENCY PROCEDURESp. 714
NORMAL PROCEDURESp. 714
PERFORMANCEp. 714
SUPPLEMENT S9 – BENDIX/KING GPS NAVIGATION SYSTEMp. 715
GENERALp. 717
LIMITATIONSp. 722
EMERGENCY PROCEDURESp. 725
NORMAL PROCEDURESp. 725
PERFORMANCEp. 726
SUPPLEMENT S10 – AIRPLANES CERTIFIED TO RUSSIAN CONFIGURATIONp. 727
GENERALp. 729
LIMITATIONSp. 729
MINIMUM OIL TEMPERATUREp. 731
FUEL LIMITATIONSp. 731
MAXIMUM OPERATING ALTITUDE LIMITp. 733
OUTSIDE AIR TEMPERATURE LIMITSp. 733
TAKEOFF AND LANDING OPERATIONAL LIMITSp. 734
MAXIMUM CROSSWIND ON CONTAMINATED RUNWAYSp. 734
CABIN CARGO LIMITSp. 735
EMERGENCY PROCEDURESp. 735
NORMAL PROCEDURESp. 736
PERFORMANCEp. 737
OPERATION ON CONTAMINATED RUNWAYp. 737
CONVERSION FROM FEET TO METERSp. 738
METRIC ALTlMETER CORRECTION – ALTERNATE STATIC SOURCEp. 739
SUPPLEMENT S11 – 30AMP POWER OUTLET – FUSELAGE STATION 282p. 740
GENERALp. 742
LIM IT ATIONSp. 742
EMERGENCY PROCEDURESp. 742
NORMAL PROCEDURESp. 742
PERFORMANCEp. 742
SUPPLEMENT S12 – BENDIX/KING GPS NAVIGATION SYSTEM (TYPE KLN 898) INTERFACED WITH THE KNI 582 RMIp. 743
GENERALp. 745
LIMITATIONSp. 745
EMERGENCY PROCEDURESp. 745
NORMAL PROCEDURESp. 746
PERFORMANCEp. 746
SUPPLEMENT S13 – HOT WEATHER OPERATIONSp. 747
GENERALp. 750
OPERATING LIMITATIONSp. 751
EMERGENCY PROCEDURESp. 751
NORMAL PROCEDURESp. 751
PERFORMANCEp. 752
(WITHOUT CARGO POD) SHORT FIELD TAKEOFF DISTANCEp. 752
(WITHOUT CARGO POD) LANDING DISTANCE SHORT FIELD FLAPS 30p. 755
(CARGO POD INSTALLED) SHORT FIELD TAKEOFF DISTANCE FLAPS 20p. 758
(CARGO POD INSTALLED) LANDING DISTANCE – SHORT FIELDp. 761
SUPPLEMENT S14 – ARNAV SYSTEMS MFD 5200 MUL Tl-FUNCTIONAL DISPLAY (MFD) SYSTEM AND ARNAV SYSTEMS GEOLINK (ABDS) WITH GPS RECEIVERp. 762
GENERALp. 764
LIMITATIONSp. 764
EMERGENCY PROCEDURESp. 766
NORMAL PROCEDURESp. 766
OPERATIONSp. 766
SYSTEM SWITCHESp. 766
POWER SOURCEp. 766
PERFORMANCEp. 767
PLACARDSp. 767
SUPPLEMENT S15 – BENDIX/KING STAND-ALONE – VFR ONLY GPS NAVIGATION SYSTEMp. 768
GENERALp. 770
LIMITATIONSp. 771
EMERGENCY PROCEDURESp. 772
NORMAL PROCEDURESp. 772
PERFORMANCEp. 772
SUPPLEMENT S16 – BFGOODRICH SKYWATCH SKY497 TRAFFIC ADVISORY SYSTEMp. 773
GENERALp. 775
LIMITATIONSp. 777
EMERGENCY PROCEDURESp. 777
NORMAL PROCEDURESp. 777
STARTING ENGINEp. 778
BEFORE TAKEOFFp. 778
BEFORE LANDINGp. 778
PERFORMANCEp. 778
SUPPLEMENT S17 – BFGOODRICH STORMSCOPE WX-1000 + /1000E WEATHER MAPPING SYSTEMp. 779
GENERALp. 781
LIMITATIONSp. 782
EMERGENCY PROCEDURESp. 782
NORMAL PROCEDURESp. 783
PERFORMANCEp. 783
SUPPLEMENT S18 – ARCTIC DIESEL FUELp. 784
GENERALp. 786
LIMITATIONSp. 786
EMERGENCY PROCEDURESp. 787
NORMAL PROCEDURESp. 787
PERFORMANCEp. 787
SUPPLEMENT S19 – 300-AMP ST ARTER-GENERATOR INSTALLATIONp. 788
GENERALp. 790
LIMITATIONSp. 791
EMERGENCY PROCEDURESp. 791
NORMAL PROCEDURESp. 791
PERFORMANCEp. 791
SUPPLEMENT S21 – SHADIN MINI-FLOW FUEL TOTALIZER COUPLED WITH A BENDIX/KING(ALLIEDSIGNAL) KLN 89B GPS NAVIGATION SYSTEMp. 792
GENERALp. 794
LIMITATIONSp. 794
EMERGENCY PROCEDURESp. 795
NORMAL PROCEDURESp. 795
ROTARY SWITCHp. 795
USED/REM TOGGLEp. 796
WARNING MESSAGESp. 796
PERFORMANCEp. 796
SUPPLEMENT S22 – KING DIGITAL COMM (TYPE KY-196A)p. 797
GENERALp. 799
LIMITATIONSp. 802
EMERGENCY PROCEDURESp. 802
NORMAL PROCEDURESp. 803
OPERATING MODE SELECTIONp. 803
FREQUENCY MODE COMMUNICATION RECEIVER-TRANSMITTER OPERATIONp. 803
CHANNEL PROGRAMMING MODE OPERATIONp. 804
DIRECT-TUNING MODE OPERATIONp. 805
PERFORMANCEp. 805
SUPPLEMENT S23 – BENDIX/KING KN 53 NAVIGATION RECEIVERp. 806
GENERALp. 808
LIMITATIONSp. 809
EMERGENCY PROCEDURESp. 809
NORMAL PROCEDURESp. 809
PERFORMANCEp. 809
SUPPLEMENT S24 – LIGHT WEIGHT LANDING FOR – AIRPLANES WITH CARGO PODp. 810
GENERALp. 812
LIMITATIONSp. 812
EMERGENCY PROCEDURESp. 812
NORMAL PROCEDURESp. 812
PERFORMANCEp. 813
LANDING DISTANCE- FEET – SHORT FIELDp. 814
SUPPLEMENT S25 – OXYGEN SYSTEM WITH QUICK-DON MASKS (2-PORT)p. 815
GENERALp. 817
PACIFIC PRECISION PRODUCTS MASKSp. 818
SCOTT AVIATION MASKSp. 820
LIMITATIONSp. 822
EMERGENCY PROCEDURESp. 822
NORMAL PROCEDURESp. 822
PACIFIC PRECISION PRODUCTS MASKSp. 822
OXYGEN DURATION CHARTFOR PACIFIC PRODUCTS MASK(50.67 CUBIC FEET CAPACITY)p. 823
OXYGEN DURATION CHARTFOR SCOTT AVIATION MASK(50.67 CUBIC FEET CAPACITY)p. 824
SCOTT AVIATION MASKS:p. 825
PERFORMANCEp. 826
SUPPLEMENT S26 – SEATING OPTIONS (INTERNATIONAL OPERATIONS)p. 827
GENERALp. 829
SEATING OPTIONSp. 829
13-PLACE COMMUTERSEATING ARRANGEMENTp. 830
14-PLACE COMMUTERSEATING ARRANGEMENTp. 831
UTILITYSEATING ARRANGEMENTp. 832
UTILITY SEATINGARRANGEMENT WITHOPTIONAL AFT BENCHp. 833
SEATSp. 834
PILOT AND FRONT PASSENGER SEATSp. 834
INDIVIDUAL (ONE-PLACE) AFT PASSENGER SEATS (Commuter)p. 835
TWO-PLACE AFT PASSENGER SEATS (Commuter)p. 835
AFT CABIN BENCH SEATp. 835
INDIVIDUAL (ONE-PLACE) AFT PASSENGER SEATS (Utility)p. 835
HEADRESTSp. 836
SEAT BELTS AND SHOULDER HARNESSESp. 836
LIMITATIONSp. 837
EMERGENCY PROCEDURESp. 838
NORMAL PROCEDURESp. 838
PERFORMANCEp. 839
CREW AND PASSENGERS (13-PLACE COMMUTER)p. 840
CREW AND PASSENGERS (14-PLACE COMMUTER)p. 841
CREW AND PASSENGERS (UTILITY SEATING)p. 842
SAMPLELOADING PROBLEM(13-PLACE COMMUTER)p. 843
SAMPLELOADING PROBLEM(14-PLACE COMMUTER)p. 845
SAMPLE LOADING PROBLEM (UTILITY SEATING)p. 847
SUPPLEMENT S27BENDIX/KINGFLIGHT CONTROL SYSTEM(TYPE KFC-225)p. 849
SUPPLEMENT S27 – BENDIX/KING FLIGHT CONTROL SYSTEM (TYPE KFC-225)p. 849
GENERALp. 851
LIMITATIONSp. 852
EMERGENCY PROCEDURESp. 853
IN CASE OF AUTOPILOTNAW DAMPER MALFUNCTIONp. 853
IN CASE OF ELECTRIC TRIM MALFUNCTIONp. 854
MAXIMUM ALTITUDE LOSS DUE TO AUTOPILOT MALFUNCTIONp. 854
YAW DAMPER (OPTIONAL) DISENGAGEMENTp. 854
In case of "CHECK PITCH TRIM" aural messagep. 855
FLASHING PTp. 855
RED "P" or "R"p. 855
FLASHING MODEp. 856
NORMAL PROCEDURESp. 856
PERFORMANCEp. 858
SUPPLEMENT S28 – OXYGEN SYSTEM WITH TWO QUICK-DON MASKS AND TWELVE CONSTANT-FLOW MASKSp. 859
GENERALp. 861
LIMITATIONSp. 865
EMERGENCY PROCEDURESp. 865
NORMAL PROCEDURESp. 865
QUICK-DON MASKSp. 865
CONSTANT-FLOW MASKSp. 866
PERFORMANCEp. 867
OXYGEN DURATION CHART(116.95 CUBIC FEET CAPACITY)p. 868
SUPPLEMENT S29 – BENDIX/KING KLN 94 GPS NAVIGATION SYSTEMp. 869
GENERALp. 871
LIMITATIONSp. 876
EMERGENCY PROCEDURESp. 878
NORMAL PROCEDURESp. 878
PERFORMANCEp. 879
SUPPLEMENT – S30 AIRPLANES CERTIFIED TO CHINA AAD-CAAC CONFIGURATIONp. 880
GENERALp. 882
INTRODUCTIONp. 882
EMERGENCY EXITSp. 882
EMERGENCY EXIT LIGHTp. 882
EMERGENCY EXIT MARKINGSp. 883
LIMITATIONSp. 883
PLACARDSp. 883
EMERGENCY PROCEDURESp. 883
NORMAL PROCEDURESp. 885
PERFORMANCEp. 887
SUPPLEMENT S31 – ARTEX 406 THREE FREQUENCY EMERGENCY LOCATOR TRANSMITTER (ELT)p. 888
GENERALp. 890
LIMITATIONSp. 890
EMERGENCY PROCEDURESp. 891
NORMAL PROCEDURESp. 892
PERFORMANCEp. 892
SUPPLEMENT S32 – POINTER MODEL 3000-11/MODEL 4000-11 EMERGENCY LOCATOR TRANSMITTER {ELT)p. 893
GENERALp. 895
LIMITATIONSp. 897
EMERGENCY PROCEDURESp. 898
NORMAL PROCEDURESp. 899
PERFORMANCEp. 900
SUPPLEMENT S33 – BENDIX/KING KX-165 NAV/COM WITH INTEGRAL GLIDE SLOPE (For use with Kl-525A HSI or Kl-206 CDI)p. 901
GENERALp. 903
LIMITATIONSp. 904
EMERGENCY PROCEDURESp. 904
NORMAL PROCEDURESp. 909
PERFORMANCEp. 910
SUPPLEMENT S34 – GARMIN GMA 340 AUDIO PANELp. 911
GENERALp. 913
LIMITATIONSp. 913
EMERGENCY PROCEDURESp. 913
NORMAL PROCEDURESp. 913
POWER ON/OFFp. 913
VHF COMMUNICATIONSp. 914
PA SYSTEM (If Installed)p. 914
INTERCOM SYSTEM (ICS)p. 914
MARKER BEACON RECEIVERp. 914
PERFORMANCEp. 915
SUPPLEMENT S35 – GARMIN GTX 327 TRANSPONDERp. 916
GENERALp. 918
LIMITATIONSp. 918
EMERGENCY PROCEDURESp. 918
NORMAL PROCEDURESp. 919
MODE SELECTIONp. 919
CODE SELECTIONp. 919
OTHER FUNCTIONSp. 919
ALTITUDE TREND INDICATORp. 920
AUTOMATIC AL T/STBY MODE SWITCHINGp. 920
PERFORMANCEp. 920
SUPPLEMENT S36 – BENDIX/KING KGP 560 GENERAL AVIATION ENHANCED GROUND PROXIMITY WARNING SYSTEM (GA-EGPWS)p. 921
GENERALp. 923
TERRAIN AWARENESS DISPLAYp. 924
"LOOK-AHEAD" ALERTING AND WARNINGp. 925
RUNWAY FIELD CLEARANCE FLOORp. 925
EXCESSIVE RATE OF DESCENTp. 926
LOSS OF ALTITUDE AFTER TAKEOFFp. 926
ALTITUDE MONITORINGp. 926
ALTITUDE CALLOUTp. 927
LIMITATIONSp. 927
EMERGENCY PROCEDURESp. 927
GA-EGPWS ALERTS AND WARNINGSp. 927
FORCED LANDINGSp. 928
EMERGENCY LANDING WITHOUT ENGINE POWERp. 928
PRECAUTIONARY LANDING WITH ENGINE POWERp. 929
DITCHINGp. 929
SUPPLEMENT S37GARMIN GNS 530 or GNS 430NAVIGATION/COMMUNICATIONSYSTEMp. 931
NORMAL PROCEDURESp. 930
BEFORE TAKEOFFp. 930
GA-EGPWS VOICE CALLOUTp. 930
PERFORMANCEp. 930
SUPPLEMENT S37GARMIN GNS 530 or GNS 430NAVIGATION/COMMUNICATIONSYSTEMp. 931
SUPPLEMENT S37 – GARMIN GNS 530 or GNS 430 NAVIGATION/COMMUNICATION SYSTEMp. 931
GENERALp. 933
LIMITATIONSp. 933
EMERGENCY PROCEDURESp. 935
NORMAL PROCEDURESp. 936
DETAILED OPERATING PROCEDURESp. 936
PILOT'S DISPLAYp. 936
AUTOPILOT/ FLIGHT DIRECTOR OPERATIONp. 937
CROSSFILL OPERATIONSp. 937
AUTOMATIC LOCALIZER COURSE CAPTUREp. 937
DISPLAY OF LIGHTNING STRIKE DATAp. 938
DISPLAY OF TRAFFIC ADVISORY DATAp. 938
PERFORMANCEp. 938
SUPPLEMENT S38 – BENDIX/KING KMD 850 MULTl-FUNCTION DISPLAYp. 939
GENERALp. 941
LIMITATIONSp. 942
EMERGENCY PROCEDURESp. 942
NORMAL PROCEDURESp. 942
PERFORMANCEp. 943
SUPPLEMENT S39 – BFGOODRICH STORMSCOPE WX-500 WEATHER MAPPING SYSTEMp. 944
GENERALp. 946
LIMITATIONSp. 946
EMERGENCY PROCEDURESp. 947
NORMAL PROCEDURESp. 947
MESSAGESp. 947
BENDIX/KING KMD 850p. 947
GARMIN GNS 430 OR GNS 530p. 948
BENDIX/KING Kl 825 EHSIp. 948
PERFORMANCEp. 949
SUPPLEMENT S40 – FAIRCHILD F1000 FLIGHT DATA RECORDERp. 950
GENERALp. 952
LIMITATIONSp. 952
EMERGENCY PROCEDURESp. 952
NORMAL PROCEDURESp. 952
PERFORMANCEp. 953
SUPPLEMENT S41 – DUAL HSI and FDI with BENDIX/KING KFC-225 AUTOPILOTp. 954
GENERALp. 956
LIMITATIONSp. 956
EMERGENCY PROCEDURESp. 956
NORMAL PROCEDURESp. 957
PERFORMANCEp. 958
SUPPLEMENT S42 – FAIRCHILD FA2100 COCKPIT VOICE RECORDERp. 959
GENERALp. 961
LIMITATIONSp. 961
EMERGENCY PROCEDURESp. 961
NORMAL PROCEDURESp. 962
PERFORMANCEp. 962
SUPPLEMENT S43 – BENDIX/KING KRA-405 and KRA-405B RADAR ALTIMETERp. 963
GENERALp. 965
LIMITATIONSp. 967
EMERGENCY PROCEDURESp. 967
NORMAL PROCEDURESp. 968
PREFLIGHT SELF-TESTp. 968
TAXIINGp. 968
INFLIGHT OPERATIONp. 968
NORMAL OPERATIONp. 969
PERFORMANCEp. 969
SUPPLEMENT S44 – FIVE-PLACE SEATING OPTION (Cargo Version)p. 970
GENERALp. 972
FIVE-PLACE UTILITY SEATINGp. 972
SEATSp. 972
PILOT AND FRONT PASSENGER SEATSp. 972
5-PLACE UTILITYSEATING ARRANGEMENTp. 973
INDIVIDUAL (ONE-PLACE) AFT PASSENGER SEATS (Utility)p. 974
SEAT BEL TS AND SHOULDER HARNESSESp. 974
SEAT BELTS, STRAP, AND SHOULDER HARNESSES (Pilot/Front Passenger Seats)p. 974
SEAT BELTS (Aft Seats)p. 975
SHOULDER HARNESSES {Aft Seats)p. 975
LIMITATIONSp. 976
EMERGENCY PROCEDURESp. 976
NORMAL PROCEDURESp. 976
PERFORMANCEp. 977
WEIGHT & BALANCE/EQUIPMENT LISTp. 977
CREW AND PASSENGERS (5-PLACE UTILITY, CARGO VERSION )p. 978
SAMPLELOADING PROBLEM(5-Place Utility, Cargo Version)p. 979
SUPPLEMENT S45 – HONEYWELL KMH 880 INTEGRATED HAZARD AWARENESS SYSTEM {IHAS)p. 981
GENERALp. 983
LIMITATIONSp. 983
EMERGENCY PROCEDURESp. 983
NORMAL PROCEDURESp. 984
PERFORMANCEp. 984
SUPPLEMENT S46 – HONEYWELL KTA 870 TRAFFIC ADVISORY SYSTEM (TAS}p. 985
GENERALp. 987
BENDIX/KING KMD 850p. 988
GARMIN GNS 430 OR GNS 530p. 989
LIMITATIONSp. 989
EMERGENCY PROCEDURESp. 989
NORMAL PROCEDURESp. 990
BEFORE TAKEOFFp. 990
TAKEOFFp. 990
CLIMBp. 990
CRUISEp. 990
DESCENTp. 990
LANDINGp. 990
PERFORMANCEp. 991
SUPPLEMENT S47 – OXYGEN SYSTEM (2-PORT)p. 992
GENERALp. 994
LIMITATIONSp. 995
EMERGENCY PROCEDURESp. 996
NORMAL PROCEDURESp. 996
OXYGEN DURATION CHART(50.67 CUBIC FEET CAPACITY)p. 997
OXYGEN DURATION CHART(116.95 CUBIC FEET CAPACITY)p. 998
PERFORMANCEp. 999
SUPPLEMENT S48 – INFLIGHT OPENABLE CARGO DOORp. 1000
GENERALp. 1002
LIMITATIONSp. 1003
AIRSPEED LIMITATIONSp. 1003
OTHER LIMITATIONSp. 1004
PLACARDSp. 1004
EMERGENCY PROCEDURESp. 1005
CARGO DOOR FAILS TO OPEN OR CLOSEp. 1005
PREFLIGHT INSPECTIONp. 1006
CARGO DOOR/JUMP LIGHT (IF INSTALLED) OPERATION IN FLIGHTp. 1007
FLIGHT CHARACTERISTICSp. 1007
PERFORMANCEp. 1008
SUPPLEMENT S49 – HONEYWELL KDR 510 FLIGHT INFORMATION SERVICES {FIS)p. 1009
GENERALp. 1011
LIMITATIONSp. 1011
EMERGENCY PROCEDURESp. 1012
NORMAL PROCEDURESp. 1012
PERFORMANCEp. 1012
SUPPLEMENT S50 – GARMIN GTX 330 TRANSPONDERp. 1013
GENERALp. 1015
LIMITATIONSp. 1015
EMERGENCY PROCEDURESp. 1016
NORMAL PROCEDURESp. 1016
MODE SELECTIONp. 1016
CODE SELECTIONp. 1017
OTHER FUNCTIONSp. 1017
AUTOMATIC AL T/STBY MODE SWITCHINGp. 1018
PERFORMANCEp. 1018
SUPPLEMENT S51 – SPANISH COMMERCIAL NIGHT INSTRUMENT METEOROLOGICAL CONDITIONS (IMC) OPERATIONSp. 1019
GENERALp. 1021
LIMITATIONSp. 1022
EMERGENCY PROCEDURESp. 1022
NORMAL PROCEDURESp. 1022
PERFORMANCEp. 1022
SUPPLEMENT S52 – FUEL TOTALIZER SYSTEMp. 1023
GENERALp. 1025
LIMITATIONSp. 1026
EMERGENCY PROCEDURESp. 1026
NORMAL PROCEDURESp. 1026
PERFORMANCEp. 1026
SUPPLEMENT S53 – U.S. REGISTERED AIRPLANES WITH REQUIREMENTS FOR BRITISH (CAA) CERTIFICATIONp. 1027
GENERALp. 1029
LIMITATIONSp. 1029
EMERGENCY PROCEDURESp. 1029
NORMAL PROCEDURESp. 1030
PERFORMANCEp. 1030
WEIGHT AND BALANCEp. 1030
AIRPLANE AND SYSTEM DESCRIPTIONp. 1030
WING FLAP SYSTEMp. 1030
STARTER GENERATORp. 1031
PROPELLERp. 1031
ELECTRICAL SYSTEMp. 1031
SUPPLEMENT S54 – ALTAIR AVIONICS CORPORATION ADAS+ ENGINE TREND MONITORp. 1032
GENERALp. 1034
LIMITATIONSp. 1035
EMERGENCY PROCEDURESp. 1035
NORMAL PROCEDURESp. 1036
PERFORMANCEp. 1036
SUPPLEMENT S55 – BENDIX/KING Kl 825 ELECTRONIC HORIZONTAL SITUATION INDICATORp. 1037
GENERALp. 1039
LIMITATIONSp. 1040
EMERGENCY PROCEDURESp. 1040
DARK HSI DISPLAY (Airplanes 208B0001 thru 208B1082, except208B1071 and those equipped with SK208-162)p. 1040
HDG FLAG (white letters on a red background)p. 1041
NORMAL PROCEDURESp. 1041
PERFORMANCEp. 1043
SUPPLEMENT S56 – BENDIX/KING KT 73 TRANSPONDERp. 1044
GENERALp. 1046
LIMITATIONSp. 1046
EMERGENCY PROCEDURESp. 1046
NORMAL PROCEDURESp. 1047
PERFORMANCEp. 1048
SUPPLEMENT S57 – MODEL 2088 (675 SHP) AIRPLANES WITH U.S. CONFIGURATION AND U.K. REGISTRATIONp. 1049
GENERALp. 1051
LIMITATIONSp. 1052
EMERGENCY PROCEDURESp. 1053
NORMAL PROCEDURESp. 1053
TAKEOFF PROCEDURESp. 1053
NOISE CHARACTERISTICSp. 1053
PERFORMANCEp. 1054
INTRODUCTIONp. 1054
GENERAL PERFORMANCEp. 1054
CONVERSIONSp. 1054
POWER-OFF STALL SPEEDSp. 1054
TAKEOFF SPEEDSp. 1055
NET TAKEOFF FLIGHT PATHp. 1055
CLIMB SPEEDSp. 1056
ENROUTE PERFORMANCE CEILING AND GROSS RATE OF CLIMBp. 1056
NET GLIDE GRADIENT AFTER ENGINE FAILUREp. 1057
LANDING SPEEDSp. 1057
CONVERSION FROM FEET TO METERSp. 1059
POWER-OFF STALL SPEEDSp. 1060
TAKEOFF DISTANCE REQUIRED (WITHOUT CARGO POD) Flaps 20Β°p. 1061
ENROUTE GROSS RATE OF CLIMB (WITHOUT CARGO POD)p. 1062
LANDING DISTANCE REQUIRED (WITHOUT CARGO POD) Flaps 30Β°p. 1063
TAKEOFF DISTANCE REQUIRED (CARGO POD INSTALLED) Flaps 20Β°p. 1064
ENROUTE GROSS RATE OF CLIMB (CARGO POD INSTALLED)p. 1065
LANDING DISTANCE REQUIRED (CARGO POD INSTALLED) Flaps 30Β°p. 1066
FLIGHT TEST "GROSS" PERFORMANCE DATAp. 1067
TAKEOFF RATE OF CLIMB – FLAPS 20 DEGREESp. 1067
TAKEOFF RATE OF CLIMB – FLAPS 20Β° (WITHOUT CARGO POD)p. 1068
TAKEOFF RATE OF CLIMB- FLAPS 20Β° (CARGO POD INSTALLED)p. 1069
SUPPLEMENT S60 12-VOLT DIRECT CURRENT (12VDC) POWER OUTLETSp. 1070
GENERALp. 1072
OPERATING LIMITATIONSp. 1072
EMERGENCY PROCEDURESp. 1072
NORMAL PROCEDURESp. 1073
PERFORMANCEp. 1073
SUPPLEMENT S61 – TKS ICE PROTECTION SYSTEM FOR CARGO POD EQUIPPED AIRPLANESp. 1074
GENERALp. 1077
LIMITATIONSp. 1078
REQUIRED TRAININGp. 1078
PREFLIGHTp. 1079
VISUAL AND TACTILE CHECKp. 1080
WEIGHT LIMITSp. 1081
MINIMUM DISPATCH FLUIDp. 1081
APPROVED ICE PROTECTION FLUIDp. 1082
POROUS PANEL CLEANINGp. 1082
MINIMUM SPEEDS IN ICING CONDITIONSp. 1083
FLAP SETTING IN ICING CONDITIONSp. 1083
REQUIRED EQUIPMENTp. 1084
WINDSHIELD PUMPp. 1084
INERTIAL SEPARATORp. 1085
PROPELLER SPINNERp. 1085
ENVIRONMENTAL CONDITIONSp. 1085
AUTOPILOT OPERATION IN ICING CONDITIONSp. 1087
MAXIMUM OPERATING ALTITUDESp. 1087
PLACARDSp. 1088
EMERGENCY PROCEDURESp. 1093
RED WARN ANNUNCIATOR COMES ON INTERMITTENTLY WITH PRIMARY SWITCH SELECTED TO NORMp. 1093
RED WARN ANNUNCIATOR COMES ON WITH PRIMARYSWITCH SELECTED TO HIGH OR MAX FLOW SWITCHSELECTED TO AIRFRAMEp. 1093
AMBER CAUT ANNUNCIATOR COMES ONp. 1094
FAILURE OF ICE PROTECTION SYSTEM OR EXCESSIVEICE ACCUMULATION (OBSERVED OR SUSPECTED) ONPROTECTED AIRPLANE SURFACESp. 1094
INADVERTENT ICING ENCOUNTER AT ALTITUDESABOVE 20,000 FEETp. 1097
INERTIAL SEPARATOR MALFUNCTIONp. 1098
PROPELLER ANTI-ICE SYSTEM MALFUNCTIONp. 1098
WINDSHIELD ANTI-ICE SYSTEM MALFUNCTIONp. 1099
HEATED PITOT/STATIC TUBE MALFUNCTIONp. 1100
RED GENERATOR OFF AND/OR AMBER STBY ELECTPWR ON ANNUNCIATORS COME ONp. 1101
HEATED STALL WARNING TRANSDUCER FAILUREp. 1101
INADVERTENT ENCOUNTER WITH FREEZING RAIN,FREEZING DRIZZLE, OR OTHER PERFORMANCECRITICAL ICING SITUATIONp. 1102
AMBER BELOW ICING MIN SPD ANNUNCIATORFLASHING AND AURAL WARNING HORN SOUNDSp. 1104
NORMAL PROCEDURESp. 1105
PREFLIGHT INSPECTIONp. 1107
BEFORE STARTING ENGINEp. 1113
BEFORE TAKEOFF CHECKp. 1114
ALL FLIGHT CONDITIONS/PHASESp. 1116
TAKEOFFp. 1117
INFLIGHT (CLIMB, CRUISE, AND DESCENT)p. 1118
APPROACHp. 1120
BEFORE LANDINGp. 1121
LANDINGp. 1121
BALKED LANDINGp. 1122
AFTER LANDINGp. 1122
SHUTDOWN AND SECURING AIRPLANEp. 1122
PERFORMANCEp. 1123
NORMAL AND BALKED LANDING RATE OF CLIMBp. 1123
STALL SPEEDp. 1124
PREFLIGHT PLANNINGp. 1124
ENROUTE TOOL FOR EXITING ICINGp. 1125
LANDINGp. 1128
WEIGHT AND BALANCEp. 1129
CARGO POD LOADING ARRANGEMENTSTKS TANK INSTALLEDp. 1129
WEIGHT AND MOMENT TABLE – TKS ICE PROTECTION FLUIDp. 1130
WEIGHING PROCEDURESp. 1131
SAMPLE LOADING PROBLEMp. 1132
AIRPLANE SYSTEMS AND DESCRIPTIONSp. 1134
SYSTEM DESCRIPTIONp. 1134
TKS ICE PROTECTION SYSTEM INSTALLATIONp. 1135
TKS ICE PROTECTION SYSTEM FLUID SCHEMATICp. 1136
TKS ICE PROTECTION SYSTEM OPERATION, INDICATION AND ANNUNCIATIONp. 1138
SYSTEMS ENDURANCE CHARACTERISTICSp. 1142
SYSTEM FLUID GAGEp. 1143
FLUID TANK SIGHT GAGEp. 1144
TKS SYSTEM ANNUNCIATORp. 1145
PITOT/STATIC HEAT SYSTEMSp. 1147
LAA ANNUNCIATORp. 1148
ICE DETECTION AND WING INSPECTION LIGHTSp. 1150
STANDBY ELECTRICAL SYSTEMp. 1150
ENGINE INERTIAL SEPARATOR AND HEATED STALLWARNING SYSTEMSp. 1151
PROLONGED OUT OF SERVICE CAREp. 1152
DURING FLYABLE STORAGEp. 1152
SERVICINGp. 1152
ICE PROTECTION FLUID TANKp. 1152
ICE PROTECTION FLUID STRAINERp. 1152
ICE PROTECTION FLUID FILTER(S)p. 1152
POROUS LEADING EDGE PANEL CLEANINGp. 1153
SUPPLEMENT S62 – ARTEX ME406 EMERGENCY LOCATOR TRANSMITTER (ELT)p. 1154
GENERALp. 1157
ARTEX ME406 ELT CONTROL PANELp. 1158
OPERATING LIMITATIONSp. 1159
EMERGENCY PROCEDURESp. 1160
NORMAL PROCEDURESp. 1161
NORMAL OPERATIONp. 1161
PERFORMANCEp. 1161
SUPPLEMENT S63 – HONEYWELL KHF 1050 HF TRA NSCEIVER WITH PS440 CONTROL DISPLAY UNITp. 1162
INTRODUCTIONp. 1164
OPERATING LIMITATIONSp. 1164
OPERATING PROCEDURESp. 1164
EMERGENCY PROCEDURESp. 1164
ABNORMAL PROCEDURESp. 1164
NORMAL PROCEDURESp. 1164
PERFORMANCEp. 1164
DESCRIPTIONp. 1165
SUPPLEMENT S64 – CONFIGURATION DEVIATION LIST {CDL}p. 1166
GENERALp. 1168
LIMITATIONSp. 1168
CONFIGURATION DEVIATION LISTp. 1169
EMERGENCY PROCEDURESp. 1170
NORMAL PROCEDURESp. 1170
PERFORMANCEp. 1170
WEIGHT AND BALANCEp. 1170
AIRPLANE SYSTEMS AND DESCRIPTIONS CAS MESSAGESp. 1170
HANDLING, SERVICING, AND MAINTENANCEp. 1170
SUPPLEMENT S65 – STANDBY ELECTRICAL SYSTEM EQUIPPED WITH 75-AMP STANDBY ALTERNATOR FOR AIRPLANES NOT EQUIPPED WITH FACTORY INSTALLED KNOWN ICING EQUIPMENT CARRYING PASSENGERS AS A COMMERCIAL OPERATOR OR FOR COMPENSATION OR HIREp. 1171
GENERALp. 1174
STANDBY ELECTRICAL SYSTEMp. 1175
OPERATING LIMITATIONSp. 1176
STANDBY ALTERNATOR OUTPUTp. 1176
EMERGENCY PROCEDURESp. 1177
GENERATOR FAILURE – GENERATOR OFF ANNUNCIATOR ILLUMINATEDp. 1177
NORMAL PROCEDURESp. 1183
AFTER ENGINE STARTp. 1183
BEFORE TAKEOFFp. 1183
ENGINE SHUTDOWNp. 1184
PERFORMANCEp. 1184
SUPPLEMENT S66 – STANDBY ELECTRICAL SYSTEM EQUIPPED WITH 81-AMP STANDBY ALTERNATOR (P/N 9910592-2) FOR AIRPLANES EQUIPPED WITH FACTORY INSTALLED KNOWN ICING EQUIPMENT CARRYING PASSENGERS AS A COMMERCIAL OPERATOR OR FOR COMPENSATION OR HIREp. 1185
GENERALp. 1188
STANDBY ELECTRICAL SYSTEMp. 1189
OPERATING LIMITATIONSp. 1190
STANDBY ALTERNATOR OUTPUTp. 1190
EMERGENCY PROCEDURESp. 1191
GENERATOR FAILURE – GENERATOR OFFANNUNCIATOR ILLUMINATEDp. 1191
STANDBY POWER FAILURE – STBY ELECT PWR INOPANNUNCIATOR ILLUMINATEDp. 1198
NORMAL PROCEDURESp. 1199
AFTER ENGINE STARTp. 1199
BEFORE TAKEOFFp. 1199
ENGINE SHUTDOWNp. 1200
PERFORMANCEp. 1200
General Supplementsp. 1201
Air Conditioning Systemp. 1201
Cargo Doors Removed Kitp. 1208
Oxygen System (14-Port)p. 1210
Oxygen System (2-Port)p. 1215
Oxygen System (13-Port)p. 1220
Rudder Gust Lock (Aero Twin)p. 1225
Standby Electrical Systemp. 1230
Ventilation Fan Systemp. 1235
Avionics Supplementsp. 1239
Emergency Locator Transmitter (Dorne and Margolin)p. 1239
Emergency Locator Transmitter (Pointer Model 3000-1)p. 1244
ELT Remote Switches And Monitor Lightp. 1250
Weather Radarp. 1256
ARVAV LORAN-C IFRp. 1265
Trimble GPS Navigatorp. 1274
Trimble GPS/Loran Navigatorp. 1280
Bendix/King GPS Navigation Systemp. 1286
King Area Navigation Systemp. 1294
King LORAN-C IFRp. 1304
King Audio Control System (Type KMA-24)p. 1311
King Audio Control System (Type KMA-24) with Marker Beacon Recieverp. 1316
King Flight Control System (Type KFC-150)p. 1321
King Audio Control System (Type KMA-24H-70)and Optional PA (Passenger Address) Systemp. 1342
King Autopilot System (Type KAP-150)p. 1349
King Flight Control System (Type KFC-250-Category I)p. 1368
King Flight Control System (Type KFC-250-Category II)p. 1393
King Digital ADF (Type KR-87)with Kl-227 Indicator or Kl-229 Optional RMIp. 1419
King Digital ADF (Type KR-87) with KNl-582 RMIp. 1427
King HF Tranceiver (Type KHF-950)p. 1435
King DME (Type KN-63)p. 1443
King Marker Beacon (Type KR-21)(Used with KMA-24H-70 Audio Control Panel)p. 1446
King Nav/Comm (Type KX-165) with Optional Integral Glidep. 1450
King Nav/Comm (Type KX-165) With Integral GlideSlope (for use With King KFC-250, Category I and IIOnly)p. 1457
King Radar Altimeter (Type KRA-1 0A)p. 1465
King Radio Magnet Indicator (Type Kl-229)p. 1469
King Radio Magnetic Indicator (Type KNl-582)p. 1473
King Transponder (Type KT-79) and EncodingAltimeter (Type KEA-130 or type 5035P-P45)p. 1478
King Mode S Transponder (Type KT-70 and KT-71)and Encoding Altimeter (Type KEA-130 orType 5035P-P45)p. 1485
Narco Weather Radar (Type KWX-56)p. 1492
Bendix/King Digital Weather Radar System(Type RDR 2000)p. 1501

Why This Manual Matters

Operating a turboprop like the Grand Caravan 208B is a matter of limits. Torque, ITT, Ng, propeller RPM, oil pressure and temperature, fuel imbalance, center of gravity β€” all of them are specified in Section 2, and every one of them exists to protect the engine and the airframe. This handbook gives the exact numbers as published by Cessna and approved by the FAA, including the PT6A-114A engine operating limits chart, the airspeed limitation and indicator marking charts, the weight and CG envelopes, and the cargo zone load limits for both the cabin and the cargo pod.

The emergency procedures in Section 3 are written as operational checklists with amplified procedures that explain the reasoning behind each step. Engine failure after takeoff, airstart with and without starter assist, loss of oil pressure, fuel control unit malfunction, inadvertent icing encounter, electrical system failures, flap system malfunctions, landing with a flat tire β€” every one of them is covered. Having the correct sequence and the supporting explanation is what turns a bad day into a manageable one.

For maintenance and engineering work, the systems description in Section 7 combined with the handling and service information in Section 8 covers ground handling, jacking and leveling, fluid capacities and specifications, deice and anti-ice operations, cleaning and care, and the inspection schedule. Section 6 handles the paperwork side β€” weighing procedures, loading manifests, cargo restraint requirements, and the equipment list reference.

What You Get

This is a digital PDF download delivered instantly after purchase. No shipping, no waiting. The file can be opened on any device that reads PDFs β€” computer, tablet, or phone β€” and individual pages or sections can be printed for use in the cockpit, hangar or classroom. The Training Edition format makes it a useful teaching aid for transition training, recurrent training, or self-study on the Grand Caravan 208B.

Because the manual covers Serial 208B0179, 208B0230 and On, and the earlier serials modified by SK208-80, it applies to a broad slice of the 208B fleet, including aircraft equipped with the numerous optional systems documented in Section 9. If you operate, maintain or train on a Grand Caravan 208B with the 675 SHP PT6A-114A, this handbook is the reference the aircraft was delivered with.

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