Operator Manual For RC-12x Aircraft

CHAPTER 1 - INTRODUCTION
EXPLANATION OF CHANGE SYMBOLS.
CHAPTER 2 -AIRCRAFT AND SYSTEMS DESCRIPTION AND OPERATION
Figure 2-1. General Exterior Arrangement - Right Side
Figure 2-2. General Exterior Arrangement - Left Side
Figure 2-3. General Exterior Arrangement - Front
Figure 2-4. General Exterior Arrangement - Top
Figure 2-5. General Exterior Arrangement - Bottom (Sheet 1 of 2)
Figure 2-5. General Exterior Arrangement - Bottom (Sheet 2 of 2)
Figure 2-6. General Interior Arrangement
Figure 2-7. Principal Dimensions
Figure 2-8. Ground Turning Radius
Figure 2-9. Exhaust and Propeller Danger Areas
Figure 2-10. Instrument Panel with Master Warning Segment Panel
Figure 2-11. Pilot/Co-Pilot/Center Subpanel (Sheet 1 of 2)
Figure 2-11. Pilot/Co-Pilot/Center Subpanel (Sheet 2 of 2)
Figure 2-12. Overhead Circuit Breaker Panel
Figure 2-13. Overhead Control Panel
Figure 2-14. General Cockpit Arrangement
LANDING GEAR SYSTEM.
Landing Gear Warning Horn Test Switch
ENTRANCE AND EXIT PROVISIONS.
Figure 2-15. Cabin and Cargo Door
Cabin Door Annunciator
Figure 2-16. Pilot and Copilot Seats
SECTION II. EMERGENCY EQUIPMENT
SECTION III. ENGINES AND RELATED SYSTEMS
Figure 2-17. PT6A-67 Engine Left Side
Figure 2-18. PT6A-67 Engine Right Side
FRICTION LOCK KNOBS.
Figure 2-19. Control Pedestal and Pedestal Extension
Figure 2-20. Engine Fire Detection System
Table 2-1. - Engine Fire Extinguisher Gauge Pressure
Figure 2-21. Engine Fire Extinguisher System
ENGINE IGNITION SYSTEM.
ENGINE INSTRUMENTS.
Figure 2-22. Instrument Panel Left/Pilot Side
Figure 2-23. Instrument Panel Right/Co-Pilot Side
SECTION IV. FUEL SYSTEM
Figure 2-24. Fuel System Schematic
Figure 2-25. Fuel Management Panel
Figure 2-26. Auxiliary Fuel Tank Mechanical Fuel Gauge
Figure 2-27. Gravity Feed Fuel Flow
Figure 2-28. Crossfeed Fuel Flow
Table 2-3. - Fuel Sump Drain Locations
FUEL SYSTEM MANAGEMENT.
RUDDER SYSTEM.
Figure 2-29. Control Wheels
Figure 2-30. Control Locks
Wing Flap Control Switch
SECTION VI. HYDRAULIC AND PNEUMATIC SYSTEMS
Flow Control Unit
FEATHERING PROVISIONS.
LOW PITCH STOP.
PROPELLER REVERSING.
SECTION IX. UTILITY SYSTEMS
ANTENNA DEICE/ANTI-ICE SYSTEM.
PROPELLER ELECTRIC DEICE SYSTEM.
STALL WARNING HEAT SYSTEM.
FUEL SYSTEM ANTI-ICING.
Figure 2-31. Oxygen System Schematic
Table 2-4. - Oxygen Flow Planning Rates vs. Altitude (All Flows in LPM per Mask at NTPD)
Table 2-5. - Oxygen Duration in Minutes (140 Cubic Foot System)
Oxygen Duration Example Problem.
Figure 2-32. Cylinder Capacity vs. Pressure and Temperature
CIGARETTE LIGHTERS AND ASH TRAYS.
SECTION X. HEATING, VENTILATION, COOLING, AND ENVIRONMENTAL CONTROL SYSTEMS
Figure 2-33. Environmental System
Manual temperature control switch
Air conditioning cold operation bypass valve
UNPRESSURIZED VENTILATION.
Automatic Mode Control
SECTION XI. ELECTRICAL POWER SUPPLY AND DISTRIBUTION SYSTEM
Figure 2-34. DC Electrical System (Sheet 1 of 2)
Figure 2-34. DC Electrical System (Sheet 2 of 2)
Figure 2-35. Single Phase AC Electrical System
Figure 2-36. Three Phase AC Electrical System
Figure 2-37. Mission Equipment DC Power System
Figure 2-38. Mission AC/DC Power Cabinet
Generator Out Warning Annunciators
Three phase AC OFF annunciator
SECTION XIII. LIGHTING
Figure 2-39. Exterior Lighting
Cockpit Lighting.
EMERGENCY LIGHTING.
Figure 2-40. Pitot and Static System
FREE AIR TEMPERATURE (FAT) GAUGE.
Figure 2-41. Warning Annunciator Panel
Figure 2-42. Caution/Advisory Panel
Table 2-7. - Caution/Advisory Annunciator Panel Legend
Table 2-8. Mission Control Panel Annunciator Legend
Table 2-8. - Mission Control Panel Annunciator Legend -- Continued
Figure 2-43. Chronometer
Table 2-9. - Approved Military Fuels, Oil, Fluids and Unit Capacities
DRAINING MOISTURE FROM FUEL SYSTEM.
Table 2-10. - Approved Fuels
Table 2-11. - Standard, Alternate, and Emergency Fuels
Figure 2-44. Servicing Locations
SERVICING THE HYDRAULIC SYSTEM.
Table 2-12. - Recommended Fluid Dilution Chart
SERVICING OXYGEN SYSTEM.
Figure 2-45. Oxygen System Servicing Pressure
GROUND HANDLING.
Moving Aircraft on Ground
Figure 2-46. Parking, Covers, Ground Handling and Towing Equipment
Figure 2-47. Towing, Turn Limits
INSTALLATION OF PROTECTIVE COVERS.
Mooring Procedures for High Winds
Figure 2-48. Mooring the Aircraft
CHAPTER 3 - AVIONICS
SECTION II. COMMUNICATIONS
Figure 3-1. Audio Control Panel
UHF TRANSCEIVER (AN/ARC-164, HAVE QUICK II).
VOICE SECURITY SYSTEM TSEC/KY-58 (COMPLETE PROVISIONS ONLY).
Figure 3-2. AN/ARC-210 Advanced Communications System Control Unit
Figure 3-3. Radio Control Unit (RCU)
Figure 3-4. Emergency Locator Transmitter
DIGITAL INTEGRATED FLIGHT CONTROL SYSTEM (SPZ-4500).
Figure 3-5. EFI-890R PFD/MFD and UNS-1F FMS Interface
Figure 3-6. Pedestal Extension
ATTITUDE AND HEADING REFERENCE SYSTEM (AHS-3000).
Figure 3-7. Electronic Standby Instrument System display (ESIS)
Table 3-1. - Digital Flight Control System Error Codes
Table 3-2. - Digital Flight Control System Limits
Table 3-2. - Digital Flight Control System Limits - Continued
Figure 3-8. Autopilot Controller
Figure 3-9. Flight Director Mode Selector/Annunciator
Vertical speed hold mode button-indicator
Heading select mode
TACAN navigation and approach mode
Back course mode
ILS approach mode
Vertical speed hold mode
SECTION IV. TRANSPONDER AND RADAR
Figure 3-10. Weather RADAR Mode Selector Control Panel
TGT (Target Alert).
Table 3-3. - Relectivity Chart
TURB (Turbulence Only).
Figure 3-11. Radar Relector size versus Beam Width
STB (Stabilization) Pushbutton
Fault Monitor
Figure 3-12. TWR-850 Weather RADAR Functional Block Diagram
TRANSPONDER (AN/APX-119).
Figure 3-13. Transponder Control Panel
Table 3-4. - Transponder Operating Controls and Indicators
Table 3-4. - Transponder Operating Controls and Indicators - Continued
Figure 3-14. Lightning Sensor System control panel
Figure 3-15. Lightning Sensor Display Icons
CHAPTER 4 - MISSION EQUIPMENT
Figure 4-2. Annunciator Control Panel
Table 4-1. - Annunciator Panel Controls and Indicators
Table 4-1. - Annunciator Panel Controls and Indicators - Continued
Figure 4-3. Mission Control Panel
Table 4-2. - Mission Control Panel Controls and Indicators
SECTION II. AIRCRAFT SURVIVABILITY EQUIPMENT
Table 4-3. - Common Missile Warning System Components
Figure 4-4. Electronic Control Unit
Figure 4-5. User Data Module Installation
Figure 4-6. Electro-Optic Missile Sensor
Figure 4-7. Coarse/Acquisition - Miniature Integrated GPS/INS Tactical System (C-MIGITS)
Figure 4-8. Sequencer
Figure 4-9. Improved Countermeasures Dispenser (ICMD) Components
Figure 4-10. Payload Module
Figure 4-11. Flare Zone Load Pattern
Figure 4-12. CMWS Control Indicator Panel
Figure 4-13. CMWS Safe/Arm Control Panel
Figure 4-14. ECU Service Panel
Figure 4-15. I/F Ampliier (Front, Back and Side views)
Figure 4-16. Wing Mounted Safety Switch
AAR-57 CMWS OPERATION.
CI Display Messages
Table 4-11. - CI Display Messages
Table 4-11. - CI Display Messages - Continued
Table 4-11. - CI Display Messages - Continued
RADAR SIGNAL DETECTING SET (AN/APR-39(V) 2 ).
CHAPTER 5 - OPERATING LIMITS AND RESTRICTIONS
STARTER LIMITATIONS
Figure 5-1. Instrument Markings (Sheet 1 of 5)
Figure 5-1. Instrument Markings (Sheet 2 of 5)
Figure 5-1. Instrument Markings (Sheet 3 of 5)
Figure 5-1. Instrument Markings (Sheet 4 of 5)
Figure 5-1. Instrument Markings (Sheet 5 of 5)
FUEL SYSTEM LIMITS.
Table 5-1. - Engine Operating Limitations
OVER TEMPERATURE AND OVERSPEED LIMITATIONS.
SECTION IV. LOADING LIMITS
SECTION V. MAXIMUM AND MINIMUM AIRSPEED LIMITS
Figure 5-2. Flight Envelope
SECTION VII. ENVIRONMENTAL RESTRICTIONS
SEVERE ICING LIMITATIONS.
SECTION VIII. OTHER LIMITATIONS
CHAPTER 6 - WEIGHT/BALANCE AND LOADING
Figure 6-1. Aircraft Compartments and Stations
Table 6-1. - Occupants Useful Loads, Weights, and Moments
Table 6-3. - Useful Load Weights and Moments/Usable Fuel, 6.4 to 6.7 LB/GAL
Table 6-4. - Useful Load Weights and Moments/Usable Fuel, 6.8 to 7.1 LB/GAL
Table 6-4. - Useful Load Weights and Moments/Usable Fuel, 6.8 to 7.1 LB/GAL - Continued
SECTION III. FUEL/OIL
Table 6-5. - Center of Gravity Limits (Landing Gear Down) Restricted Category
Figure 6-2. Density Variation of Aviation Fuel
SECTION VI. CARGO LOADING
Figure 6-3. Center of Gravity Loading Diagram
CHAPTER 7 - PERFORMANCE DATA
Airspeed Calibration - Normal System, I Takeoff Ground Roll.
Static Take-off Power at 1700 RPM, Ice Vanes Retracted or Extended.
Maximum Take-Off Weight as Limited by Tire Speed - Flaps Up.
Net Take-off Flight Path-Second Segment - Flaps Up.
Accelerate Go - Flaps Approach.
Horizontal Distance from Reference Zero to Third Segment Climb - Flaps Approach.
Service Ceiling-One Engine Inoperative.
Range Proile - Maximum Cruise Power at 1700 RPM.
Range Proile Maximum Range Power at 1500 RPM.
Endurance Proile - Full Main Tanks.
Landing Distance-One Engine Inoperative - Flaps Down.
Fahrenheit to Celsius Temperature Conversion
Table 7-1. - Route Segment Data
Minimum Static Takeoff Power (Ice Vanes Retracted)
Figure 7-1. Takeoff Path Proile - One Engine Inoperative
Takeoff Path Proile (Flaps Approach, One Engine Inoperative)
Flight Planning Example
Table 7-2. - Example Cruise True Airspeeds
Cruise speeds
Cruise power setting
Table 7-3. - Example Cruise Results
Table 7-4. - Example Time, Fuel, and Distance
Enroute Instrument Corrections
Table 7-5. - Example Fuel Flow (lbs/hr)
Figure 7-2. Airspeed Calibration - Normal System, Take-Off Ground Roll
Figure 7-3. Airspeed Calibration - Normal System
Figure 7-4. Altimeter Correction - Normal System
Figure 7-5. Airspeed Calibration - Alternate System
Figure 7-6. Altimeter Correction - Alternate System
Figure 7-7. Indicated Outside Air Temperature Correction
Figure 7-8. ISA Conversion
Figure 7-9. Fahrenheit to Celsius Temperature Conversion
Figure 7-10. Static Take-Off Power at 1700 RPM, Ice Vanes Retracted
Figure 7-11. Static Take-Off Power at 1700 RPM, Ice Vanes Extended
Figure 7-12. Wind Components
Figure 7-13. Maximum Take-Off Weight Permitted by Enroute Climb Requirements
Figure 7-14. Maximum Take-off Weight to Achieve Positive One Engine Inoperative Climb at Liftoff - Flaps Up
Figure 7-15. Maximum Take-off Weight as Limited by Tire Speed - Flaps Up
Figure 7-16. Take-Off Speeds (KIAS) - Flaps Up (Sheet 1 of 2)
Figure 7-16. Take-Off Speeds (KIAS) - Flaps Up (Sheet 2 of 2)
Figure 7-17. Take-off Distance Over 50 Foot Obstacle - Flaps Up
Figure 7-18. Accelerate Stop - Flaps Up
Figure 7-19. Accelerate-Go Distance Over 50 Foot Obstacle - Flaps Up
Figure 7-20. Net Take-off Flight Path - First Segment - Flaps Up
Figure 7-21. Net Take-off Flight Path - Second Segment - Flaps Up
Figure 7-22. Horizontal Distance from Reference Zero to Third Segment Climb - Flaps Up
Figure 7-23. Maximum Take-off Weight to Achieve Positive One Engine Inoperative Climb at Liftoff - Flaps Approach
Figure 7-24. Maximum Take-off Weight as Limited by Tire Speed - Flaps Approach
Figure 7-25. Take-Off Speeds (KIAS) - Flaps Approach (Sheet 1 of 2)
Figure 7-25. Take-Off Speeds (KIAS) - Flaps Approach (Sheet 2 of 2)
Figure 7-26. Take-off Distance Over 50 Foot Obstacle - Flaps Approach
Figure 7-27. Accelerate Stop - Flaps Approach
Figure 7-28. Accelerate-Go Distance Over 50 Foot Obstacle - Flaps Approach
Figure 7-29. Net Take-off Flight Path - First Segment - Flaps Approach
Figure 7-30. Net Take-off Flight Path - Second Segment - Flaps Approach
Figure 7-31. Horizontal Distance from Reference Zero to Third Segment Climb - Flaps Approach
Figure 7-32. Close-in Take-off Flight Path - Flaps Approach
Figure 7-33. Distant Take-off Flight Path - Flaps Approach
Figure 7-34. Net Take-off Flight Path - Third Segment
Figure 7-35. Climb - Two Engine - Flaps Up
Figure 7-36. Climb - Two Engine - Flaps Approach
Figure 7-37. Climb - One Engine Inoperative
Figure 7-38. Service Ceiling - One Engine Inoperative
Figure 7-39. Time, Fuel, and Distance to Cruise Climb
Figure 7-40. Maximum Cruise Power at 1700 RPM - ISA -30C (Sheet 1 of 2)
Figure 7-40. Maximum Cruise Power at 1700 RPM - ISA -30C (Sheet 2 of 2)
Figure 7-41. Maximum Cruise Power at 1700 RPM - ISA -20C (Sheet 1 of 2)
Figure 7-41. Maximum Cruise Power at 1700 RPM - ISA -20C (Sheet 2 of 2)
Figure 7-42. Maximum Cruise Power at 1700 RPM - ISA -10C (Sheet 1 of 2)
Figure 7-42. Maximum Cruise Power at 1700 RPM - ISA -10C (Sheet 2 of 2)
Figure 7-43. Maximum Cruise Power at 1700 RPM - ISA (Sheet 1 of 2)
Figure 7-43. Maximum Cruise Power at 1700 RPM - ISA (Sheet 2 of 2)
Figure 7-44. Maximum Cruise Power at 1700 RPM - ISA +10C (Sheet 1 of 2)
Figure 7-44. Maximum Cruise Power at 1700 RPM - ISA +10C (Sheet 2 of 2)
Figure 7-45. Maximum Cruise Power at 1700 RPM - ISA +20C (Sheet 1 of 2)
Figure 7-45. Maximum Cruise Power at 1700 RPM - ISA +20C (Sheet 2 of 2)
Figure 7-46. Maximum Cruise Power at 1700 RPM - ISA +30C (Sheet 1 of 2)
Figure 7-46. Maximum Cruise Power at 1700 RPM - ISA +30C (Sheet 2 of 2)
Figure 7-47. Maximum Cruise Power at 1700 RPM - ISA +37C (Sheet 1 of 2)
Figure 7-47. Maximum Cruise Power at 1700 RPM - ISA +37C (Sheet 2 of 2)
Figure 7-48. Maximum Cruise Speeds at 1700 RPM
Figure 7-49. Maximum Cruise Power at 1700 RPM
Figure 7-50. Fuel Flow at Maximum Cruise Power at 1700 RPM
Figure 7-51. Range Proile - Maximum Cruise Power at 1700 RPM
Figure 7-52. Normal Cruise Power at 1500 RPM - ISA -30C (Sheet 1 of 2)
Figure 7-52. Normal Cruise Power at 1500 RPM - ISA -30C (Sheet 2 of 2)
Figure 7-53. Normal Cruise Power at 1500 RPM - ISA -20C (Sheet 1 of 2)
Figure 7-53. Normal Cruise Power at 1500 RPM - ISA -20C (Sheet 2 of 2)
Figure 7-54. Normal Cruise Power at 1500 RPM - ISA -10C (Sheet 1 of 2)
Figure 7-54. Normal Cruise Power at 1500 RPM - ISA -10C (Sheet 2 of 2)
Figure 7-55. Normal Cruise Power at 1500 RPM - ISA (Sheet 1 of 2)
Figure 7-55. Normal Cruise Power at 1500 RPM - ISA (Sheet 2 of 2)
Figure 7-56. Normal Cruise Power at 1500 RPM - ISA +10C (Sheet 1 of 2)
Figure 7-56. Normal Cruise Power at 1500 RPM - ISA +10C (Sheet 2 of 2)
Figure 7-57. Normal Cruise Power at 1500 RPM - ISA +20C (Sheet 1 of 2)
Figure 7-57. Normal Cruise Power at 1500 RPM - ISA +20C (Sheet 2 of 2)
Figure 7-58. Normal Cruise Power at 1500 RPM - ISA +30C (Sheet 1 of 2)
Figure 7-58. Normal Cruise Power at 1500 RPM - ISA +30C (Sheet 2 of 2)
Figure 7-59. Normal Cruise Power at 1500 RPM - ISA +37C (Sheet 1 of 2)
Figure 7-59. Normal Cruise Power at 1500 RPM - ISA +37C (Sheet 2 of 2)
Figure 7-60. Normal Cruise Speeds at 1500 RPM
Figure 7-61. Normal Cruise Power at 1500 RPM
Figure 7-62. Fuel Flow at Normal Cruise Power at 1500 RPM
Figure 7-63. Range Proile - Normal Cruise Power at 1500 RPM
Figure 7-64. Maximum Range Power at 1500 RPM - ISA -30C (Sheet 1 of 2)
Figure 7-64. Maximum Range Power at 1500 RPM - ISA -30C (Sheet 2 of 2)
Figure 7-65. Maximum Range Power at 1500 RPM - ISA - 20C (Sheet 1 of 2)
Figure 7-65. Maximum Range Power at 1500 RPM - ISA - 20C (Sheet 2 of 2)
Figure 7-66. Maximum Range Power at 1500 RPM - ISA - 10C (Sheet 1 of 2)
Figure 7-66. Maximum Range Power at 1500 RPM - ISA - 10C (Sheet 2 of 2)
Figure 7-67. Maximum Range Power at 1500 RPM - ISA (Sheet 1 of 2)
Figure 7-67. Maximum Range Power at 1500 RPM - ISA (Sheet 2 of 2)
Figure 7-68. Maximum Range Power at 1500 RPM - ISA +10C (Sheet 1 of 2)
Figure 7-68. Maximum Range Power at 1500 RPM - ISA +10C (Sheet 2 of 2)
Figure 7-69. Maximum Range Power at 1500 RPM - ISA +20C (Sheet 1 of 2)
Figure 7-69. Maximum Range Power at 1500 RPM - ISA +20C (Sheet 2 of 2)
Figure 7-70. Maximum Range Power at 1500 RPM - ISA +30C (Sheet 1 of 2)
Figure 7-70. Maximum Range Power at 1500 RPM - ISA +30C (Sheet 2 of 2)
Figure 7-71. Maximum Range Power at 1500 RPM - ISA +37C (Sheet 1 of 2)
Figure 7-71. Maximum Range Power at 1500 RPM - ISA +37C (Sheet 2 of 2)
Figure 7-72. Range Proile - Maximum Range Power at 1500 RPM
Figure 7-73. Loiter Power at 1700 RPM - ISA -30C (Sheet 1 of 2)
Figure 7-73. Loiter Power at 1700 RPM - ISA -30C (Sheet 2 of 2)
Figure 7-74. Loiter Power at 1700 RPM - ISA -20C (Sheet 1 of 2)
Figure 7-74. Loiter Power at 1700 RPM - ISA -20C (Sheet 2 of 2)
Figure 7-75. Loiter Power at 1700 RPM - ISA -10C (Sheet 1 of 2)
Figure 7-75. Loiter Power at 1700 RPM - ISA -10C (Sheet 2 of 2)
Figure 7-76. Loiter Power at 1700 RPM - ISA (Sheet 1 of 2)
Figure 7-76. Loiter Power at 1700 RPM - ISA (Sheet 2 of 2)
Figure 7-77. Loiter Power at 1700 RPM - ISA +10C (Sheet 1 of 2)
Figure 7-77. Loiter Power at 1700 RPM - ISA +10C (Sheet 2 of 2)
Figure 7-78. Loiter Power at 1700 RPM - ISA +20C (Sheet 1 of 2)
Figure 7-78. Loiter Power at 1700 RPM - ISA +20C (Sheet 2 of 2)
Figure 7-79. Loiter Power at 1700 RPM - ISA +30C (Sheet 1 of 2)
Figure 7-79. Loiter Power at 1700 RPM - ISA +30C (Sheet 2 of 2)
Figure 7-80. Loiter Power at 1700 RPM - ISA +37C (Sheet 1 of 2)
Figure 7-80. Loiter Power at 1700 RPM - ISA +37C (Sheet 2 of 2)
Figure 7-81. Endurance Proile - Loiter Power at 1700 RPM
Figure 7-82. Range Proile - Full Main Tanks
Figure 7-83. Endurance Proile - Full Main Tanks
Figure 7-84. Range Proile - Full Main and Aux Tanks
Figure 7-85. Endurance Proile - Full Main and Aux Tanks
Figure 7-86. One Engine Inoperative Max Cruise Power at 1700 RPM (Ice Vanes Retracted) - ISA -30C (Sheet 1 of 2)
Figure 7-86. One Engine Inoperative Max Cruise Power at 1700 RPM (Ice Vanes Retracted) - ISA -30C (Sheet 2 of 2)
Figure 7-87. One Engine Inoperative Max Cruise Power at 1700 RPM (Ice Vanes Retracted) - ISA -20C (Sheet 1 of 2)
Figure 7-87. One Engine Inoperative Max Cruise Power at 1700 RPM (Ice Vanes Retracted) - ISA -20C (Sheet 2 of 2)
Figure 7-88. One Engine Inoperative Max Cruise Power at 1700 RPM (Ice Vanes Retracted) - ISA -10C (Sheet 1 of 2)
Figure 7-88. One Engine Inoperative Max Cruise Power at 1700 RPM (Ice Vanes Retracted) - ISA -10C (Sheet 2 of 2)
Figure 7-89. One Engine Inoperative Max Cruise Power at 1700 RPM (Ice Vanes Retracted) - ISA (Sheet 1 of 2)
Figure 7-89. One Engine Inoperative Max Cruise Power at 1700 RPM (Ice Vanes Retracted) - ISA (Sheet 2 of 2)
Figure 7-90. One Engine Inoperative Max Cruise Power at 1700 RPM (Ice Vanes Retracted) - ISA +10C (Sheet 1 of 2)
Figure 7-90. One Engine Inoperative Max Cruise Power at 1700 RPM (Ice Vanes Retracted) - ISA +10C (Sheet 2 of 2)
Figure 7-91. One Engine Inoperative Max Cruise Power at 1700 RPM (Ice Vanes Retracted) - ISA +20C (Sheet 1 of 2)
Figure 7-91. One Engine Inoperative Max Cruise Power at 1700 RPM (Ice Vanes Retracted) - ISA +20C (Sheet 2 of 2)
Figure 7-92. One Engine Inoperative Max Cruise Power at 1700 RPM (Ice Vanes Retracted) - ISA +30C (Sheet 1 of 2)
Figure 7-92. One Engine Inoperative Max Cruise Power at 1700 RPM (Ice Vanes Retracted) - ISA +30C (Sheet 2 of 2)
Figure 7-93. One-Engine-Inoperative Maximum Cruise Power 1700 RPM ISA +37C (Sheet 1 of 2)
Figure 7-93. One-Engine-Inoperative Maximum Cruise Power 1700 RPM ISA +37C (Sheet 2 of 2)
Figure 7-94. Time, Fuel, and Distance to Descend
Figure 7-95. Climb - Balked Landing
Figure 7-96. Normal Landing Distance - Flaps Down
Figure 7-97. Normal Landing Distance - Flaps Up
LANDING DISTANCE - ONE ENGINE INOPERATIVE FLAPS DOWN
CHAPTER 8 - NORMAL PROCEDURES
BEFORE EXTERIOR CHECK.
BEFORE EXTERIOR CHECK. - Continued
BEFORE EXTERIOR CHECK. - Continued
BEFORE EXTERIOR CHECK. - Continued
BEFORE EXTERIOR CHECK. - Continued
BEFORE EXTERIOR CHECK. - Continued
FUEL SAMPLE AND OIL CHECK.
Figure 8-1. Exterior Inspection.
Table 8-1. - Engine Fire Extinguisher Gauge Pressure
EXTERIOR CHECK.
EXTERIOR CHECK. - Continued
Fuselage Right Side
INTERIOR CHECK.
Overhead panel
FIRST ENGINE START (BATTERY START).
SECOND ENGINE START (BATTERY START).
FIRST ENGINE START (GPU START).
BEFORE TAXIING.
ENGINE RUNUP.
Primary governors
BEFORE TAKEOFF.
ENGINE ANTI-ICE
AFTER TAKEOFF.
Table 8-2. - Cruise Climb Schedule.
DESCENT-ARRIVAL.
TOUCH AND GO/STOP AND GO LANDING.
ENGINE SHUTDOWN.
BEFORE LEAVING AIRCRAFT.
SECTION IV. FLIGHT CHARACTERISTICS
SECTION IV. FLIGHT CHARACTERISTICS - Continued
Figure 8-2. Stall Speeds Power Idle.
SECTION V. ADVERSE ENVIRONMENTAL CONDITIONS
Warm-Up and Ground Test
Before Leaving Aircraft
ICE AND RAIN (TYPICAL).
SEVERE ICING.
CHAPTER 9 - EMERGENCY PROCEDURES
ENGINE MALFUNCTION.
MAXIMUM GLIDE.
Figure 9-1. Maximum Glide Distance Standard Day (ISA)
Figure 9-2. Emergency Exits and Equipment
ENGINE RESTART DURING FLIGHT (NO STARTER ASSIST).
ENGINE RESTART DURING FLIGHT (USING STARTER).
SINGLE-ENGINE DESCENT/ARRIVAL.
SINGLE-ENGINE GO-AROUND.
ENGINE BLEED AIR SYSTEM MALFUNCTION.
DUCT OVER TEMP CAUTION ANNUNCIATOR ILLUMINATED.
EMERGENCY DESCENT.
FUEL SYSTEM.
ELECTRICAL SYSTEM EMERGENCIES.
PROPELLER DE-ICE (AUTO SYSTEM).
FLIGHT CONTROL MALFUNCTIONS.
nding Gear Emergency Extension.
FLIGHT MANAGEMENT SYSTEM MALFUNCTIONS.
SECTION II. MISSION EQUIPMENT
Figure 9-4. Wind Swell Ditch Heading Evaluation
APPENDIX A - REFERENCES

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