TM-1-1510-224-10 Army RC-12P Aircraft and Army RC-12Q Aircraft Manual

WARNINGS, CAUTIONS, AND NOTES.
SERIES AND EFFECTIVITY CODES.
CHAPTER 2 AIRCRAFT AND SYSTEMS DESCRIPTION AND OPERATION - TM-1-1510-224-10_8
Figure 2-1. General Exterior Arrangement - Right Side, (Sheet 1 of 6)
Figure 2-1. General Exterior Arrangement - Left Side, (Sheet 2 of 6)
Figure 2-1. General Exterior Arrangement - Front, (Sheet 3 of 6)
Figure 2-1. General Exterior Arrangement - Top, (Sheet 4 of 6)
Figure 2-1. General Exterior Arrangement - Bottom, (Sheet 5 of 6)
Figure 2-1. General Exterior Arrangement - Bottom, - Continued (Sheet 6 of 6)
Figure 2-2. General Exterior Arrangement - Right Side, (Sheet 1 of 6)
Figure 2-2. General Exterior Arrangement - Left Side, (Sheet 2 of 6)
Figure 2-2. General Exterior Arrangement - Front, (Sheet 3 of 6)
Figure 2-2. General Exterior Arrangement - Top, (Sheet 4 of 6)
Figure 2-2. General Exterior Arrangement - Bottom, (Sheet 5 of 6)
Figure 2-2. General Exterior Arrangement - Bottom, - Continued (Sheet 6 of 6)
Figure 2-3. General Interior Arrangement,
Figure 2-4. General Interior Arrangement,
Figure 2-5. Principal Dimensions
Figure 2-6. Ground Turning Radius
Figure 2-7. Exhaust and Propeller Danger Areas
Figure 2-8. Subpanels
Landing Gear Warning Indicator Light Test Switch
Figure 2-9. Overhead Circuit Breaker Panel
Landing Gear Alternate Extension
Figure 2-10.   Cockpit
ENTRANCE AND EXIT PROVISIONS - TM-1-1510-224-10_31
Figure 2-11. Cabin and Cargo Doors
WINDOWS
Figure 2-12. Pilot's and Copilot's Seats
Section II. EMERGENCY EQUIPMENT - TM-1-1510-224-10_35
Section III. ENGINES AND RELATED SYSTEMS - TM-1-1510-224-10_36
Figure 2-13. Engine (Sheet 1 of 2)
Figure 2-13. Engine (Sheet 2 of 2)
Figure 2-14. Control Pedestal and Pedestal Extension (Sheet 1 of 2)
Figure 2-14. Control Pedestal and Pedestal Extension (Sheet 2 of 2)
Figure 2-15. Overhead Control Panel
ENGINE FUEL CONTROL SYSTEM - TM-1-1510-224-10_42
Figure 2-16. Engine Fire Detection System
Table 2-1. Engine Fire Extinguisher Gage Pressure
Figure 2-17. Engine Fire Extinguisher System
ENGINE IGNITION SYSTEM
Figure 2-18. Instrument Panel (Sheet 1 of 2)
Figure 2-18. Instrument Panel (Sheet 2 of 2)
Section IV. FUEL SYSTEM - TM-1-1510-224-10_49
Figure 2-19. Fuel System Schematic
Figure 2-20. Fuel Management Panel.
Figure 2-21. Crossfeed Fuel Flow - TM-1-1510-224-10_52
Figure 2-22. Gravity Feed Fuel Flow
Fuel    Gaging    System.
Figure 2-23. Auxiliary Fuel Tank Fuel Gage
Table 2-3. Fuel Sump Drain Locations - TM-1-1510-224-10_56
Section V. FLIGHT CONTROLS - TM-1-1510-224-10_57
Figure 2-24. Control Wheels
Elevator Trim Tab Control.
WING FLAPS
PROPELLER GOVERNORS. - TM-1-1510-224-10_61
PROPELLER SYNCHROPHASER
Section VII. UTILITY SYSTEMS - TM-1-1510-224-10_63
ANTENNA DEICING SYSTEM
FORWARD   GUARDRAIL   DUAL   DATA   LINK ANTENNA RADOME ANTI-ICE
BRAKE DEICE SYSTEM
PRESSURIZATION SYSTEM - TM-1-1510-224-10_67
OXYGEN SYSTEM - TM-1-1510-224-10_68
Figure 2-26. Oxygen System
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 - TM-1-1510-224-10_71
Oxygen Duration Examples.
WINDSHIELD WIPERS.
Section VIII. HEATING, VENTILATION, COOLING, AND ENVIRONMENTAL CONTROL SYSTEM - TM-1-1510-224-10_74
Figure 2-28. Environmental System
AIR CONDITIONING SYSTEM.
Air    conditioning    cold    operation    bypass valve
Cooling Mode - TM-1-1510-224-10_78
Section IX. ELECTRICAL POWER SUPPLY AND DISTRIBUTION SYSTEM - TM-1-1510-224-10_79
Figure 2-29. DC Electrical System
Figure 2-30. DC Electrical System
Figure 2-31. DC Electrical System Busses (Sheet 1 of 2)
Figure 2-31. DC Electrical System Busses (Sheet 2 of 2)
Figure 2-32. Single Phase AC Electrical System
Figure 2-33. Three Phase AC Electrical System
Figure 2-34. Mission Equipment DC Power System
Figure 2-35. Mission Equipment DC Power System
Figure 2-36. Mission AC/DC Power Cabinet
DC Load and Voltmeters.
Instrument AC annunciator.
Section X. LIGHTING - TM-1-1510-224-10_91
Figure 2-37. Exterior Lighting
Engine instrument lights
Section XI. FLIGHT INSTRUMENTS - TM-1-1510-224-10_94
COPILOT'S BAROMETRIC ALTIMETER
VERTICAL SPEED INDICATORS
STANDBY MAGNETIC COMPASS
Figure 2-42. Caution/Advisory Annunciator Panel
Table 2-7. Caution/Advisory Annunciator Panel Legend - TM-1-1510-224-10_99
Table 2-8. Mission Control Panel Annunciator Legend - TM-1-1510-224-10_100
Figure 2-43. Autopilot/EFIS/Rudder Boost Remote Annunciator Panel
Section XII. SERVICING, PARKING, AND MOORING - TM-1-1510-224-10_102
Table 2-10. Approved Fuels - TM-1-1510-224-10_103
Table 2-11. Standard, Alternate, and Emergency Fuels - TM-1-1510-224-10_104
Figure 2-44. Servicing Locations
FILLING FUEL TANKS
Fuel limitations.
INFLATING TIRES - TM-1-1510-224-10_108
APPLICATION OF EXTERNAL POWER
Figure 2-45. Oxygen System Servicing Pressure
General Ground Handling Procedure
Figure 2-46. Parking, Covers, Ground Handling, and Towing Equipment
Figure 2-47. Towing Turn Limits
control lock
CHAPTER 3 AVIONICS - TM-1-1510-224-10_115
Section II. COMMUNICATIONS - TM-1-1510-224-10_116
Figure 3-1. Audio Control Panel - TM-1-1510-224-10_117
Transmitter-intercom selector switch.
Normal Operation. - TM-1-1510-224-10_119
Figure 3-3. UHF Transceiver - TM-1-1510-224-10_120
Transceiver operating procedure
Figure 3-4. VHF Communications Transceiver Control Unit - TM-1-1510-224-10_122
Frequency   selection
Frequency   storage.
Over-temperature protection.
Figure 3-5. HF Communications Transceiver Control Unit
Programming simplex preset channels.
Programming semi-duplex preset channels.
Maritime Radiotelephone Network Channel Operation
COMM control page.
SC   (single   channel)   mode.
FH/M (frequency hopping
Figure 3-6. Emergency Locator Transmitter
Section III. NAVIGATION - TM-1-1510-224-10_134
Figure 3-7. Integrated Flight Control System Block Diagram
ATTITUDE     AND     HEADING     REFERENCE SYSTEM - TM-1-1510-224-10_136
DISPLAY CONTROLLER
Heading pushbutton selector switch
Attitude source annunciator.
Figure 3-9. Electronic Attitude Director Indicator (EADI) - TM-1-1510-224-10_140
Glideslope deviation pointer, annunciator
Table 3-2. Comparison Monitor Symbols and Miscompare Levels
Same    attitude    source.
Figure 3-12. EADI Input/Output Processer Failure Indications
Figure 3-13. Electronic Horizontal Situation Indicator (EHSI)
Single-needle     bearing     pointer.
Course     deviation     bar.
Weather   radar   tilt   angle   display.
Figure 3-15. EHSI Partial Compass Format Unique Indications
Figure 3-16. EHSI Partial Compass VOR Map Mode
Figure 3-17. EHSI Multiple Waypoint Map Mode (LRN)
Table 3-3. Weather Radar Return Levels
EADI AND EHSI COMPOSITE DISPLAY
Figure 3-19. EHSI Failure Annunciators (Red)
Figure 3-20. EADI/EHSI Composite Display - TM-1-1510-224-10_155
Table 3-4. Digital Flight Control System Error Codes - TM-1-1510-224-10_156
Table 3-5. Digital Flight Control System Limits (Sheet 1 of 3) - TM-1-1510-224-10_157
Table 3-5. Digital Flight Control System Limits (Sheet 2 of 3) - TM-1-1510-224-10_158
Autopilot Controller
Figure 3-21. Autopilot Controller
Figure 3-22. Flight Director Mode Selector - TM-1-1510-224-10_161
Figure 3-23. Altitude Preselector - TM-1-1510-224-10_162
Table 3-6. Flight Director Modes Reset when EFIS
Control wheel - Move to mid-travel.
Heading hold mode (wings level).
VOR   (NAV)   mode.
Inertial navigation system (INS) steering mode
ILS approach mode. - TM-1-1510-224-10_168
ILS approach mode. - TM-1-1510-224-10_169
Altitude hold mode
VHF NAVIGATION RECEIVERS (VIR-32)
Figure 3-24. VHF Navigation Receiver Control Unit - TM-1-1510-224-10_172
Operating Procedures. - TM-1-1510-224-10_173
ILS (Localizer and Glide Slope)
Table 3-7. VHF Navigation Receiver Fault Codes - TM-1-1510-224-10_175
Figure 3-25. ADF Control Unit - TM-1-1510-224-10_176
Operating Procedures. - TM-1-1510-224-10_177
Table 3-8. ADF Receiver Fault Codes
Figure 3-26. TACAN/DME Control Unit
Figure 3-27. TACAN/DME Display Unit
INERTIAL NAVIGATION SYSTEM
Figure 3-28. INS Mode Selector
Alignment mode.
Normal Operating Procedures.
Table 3-9. INS Malfunction Codes - TM-1-1510-224-10_185
Table 3-10. INS Action Codes and Recommended Actions - TM-1-1510-224-10_186
Navigation Information.
Table 3-11. Datum Cross Reference
Desired    track.
Stored heading shut down
GPS position data insertion
CHALS USE OF GPS AND INS.
Section IV. RADAR AND TRANSPONDER - TM-1-1510-224-10_193
Figure 3-30. EFIS Weather Test Pattern (Typical, 120-Degree Scan)
Figure 3-31. Maximum Permissible Exposure Level
Table 3-12. Video Integrated Processor VS Aircraft Radar Return Levels
Radar receiver gain control.
Weather Radar Modes of Operation. - TM-1-1510-224-10_198
Figure 3-32. Lightning Strokes Required per Symbol vs. Range to Storm
Figure 3-33. Lightning Rate of Occurrence Symbols
Table 3-13. Lightning Sensor System Failure Codes
Figure 3-34. Transponder Control Panel
Transponder Normal Operation.
Shutdown procedure - TM-1-1510-224-10_204
Figure 3-35. Pilot's Barometric Altimeter Indicator
CHAPTER 4 MISSION EQUIPMENT - TM-1-1510-224-10_206
Weight-on-wheels    override    switch.
Figure 4-1. Mission Control Panel - TM-1-1510-224-10_208
Section II. AIRCRAFT SURVIVABILITY EQUIPMENT
SYSTEM DAILY PREFLIGHT/RE-ARM TEST
Flare Dispenser System Test Procedure.
Chaff   Dispenser   (Right   Nacelle)   System   Test Procedure - TM-1-1510-224-10_212
Chaff   Dispenser   (Right   Nacelle)   System   Test Procedure - TM-1-1510-224-10_213
AMMUNITION
Ammunition Unloading Procedure
AIRCRAFT SURVIVABILITY EQUIPMENT/ AVIONICS CONTROL SYSTEM (ASE/ACS)
CHAPTER 5 OPERATING LIMITS AND RESTRICTIONS - TM-1-1510-224-10_217
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
Section III. POWER LIMITS - TM-1-1510-224-10_224
OVERTEMPERATURE AND OVERSPEED LIMITATIONS
Section V. AIRSPEED LIMITS, MAXIMUM AND MINIMUM - TM-1-1510-224-10_226
Figure 5-2. Flight Envelope - TM-1-1510-224-10_227
Section VII. ENVIRONMENTAL RESTRICTIONS - TM-1-1510-224-10_228
OXYGEN REQUIREMENTS.
Section IX. REQUIRED EQUIPMENT FOR VARIOUS CONDITIONS OF FLIGHT - TM-1-1510-224-10_230
Table 5-3. Required Equipment Listing - TM-1-1510-224-10_231
Table 5-3. Required Equipment Listing - (Cont'd) - TM-1-1510-224-10_232
Table 5-3. Required Equipment Listing - (Cont'd) - TM-1-1510-224-10_233
Table 5-3. Required Equipment Listing - (Cont'd) - TM-1-1510-224-10_234
EXTENT OF COVERAGE
Figure 6-1. Aircraft Compartments and Stations - TM-1-1510-224-10_236
Figure 6-2. 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 6.8 LB/GAL
Table 6-4. Useful Load Weights and Moments Usable Fuel 6.9 to 7.1 LB/GAL
Section III. FUEUOIL
Figure 6-3. Density Variation of Aviation Fuel - TM-1-1510-224-10_242
Section IV. CENTER OF GRAVITY
Figure 6-4. Center of Gravity Loading Diagram
INTRODUCTION TO PERFORMANCE.
Altimeter Correction Normal System.
Accelerate-Stop Flaps Up.
Net   Take-off   Flight   Path   First   Segment   Flaps Up
Accelerate Stop Flaps Approach
Climb One Engine Inoperative. - TM-1-1510-224-10_250
Fuel   Flow   at   Maximum   Cruise   Power
Maximum Range Power.
Purpose.
Table 7-1. Route Segment Data2
Minimum    Static    Takeoff    Power    (Ice    Vanes Retracted)
Takeoff Path One Engine Inoperative
Tak eoff    Path    Profile    (Flaps    Approach,    One Engine Inoperative).
Flight Planning Example
Cruise    power    setting.
Total    fuel    requirement.
Normal     landing     distance     flaps     down.
Figure 7-2. Airspeed Calibration - Normal System, Takeoff Ground Roll
Figure 7-3. Airspeed Calibration - Normal System - TM-1-1510-224-10_263
Figure 7-4. Altimeter Correction - Normal System - TM-1-1510-224-10_264
Figure 7-5. Airspeed Calibration - Alternate System - TM-1-1510-224-10_265
Figure 7-6. Altimeter Correction - Alternate System - TM-1-1510-224-10_266
Figure 7-7. Indicated Outside Air Temperature Correction - TM-1-1510-224-10_267
Figure 7-8. ISA Conversion - TM-1-1510-224-10_268
Figure 7-9. Fahrenheit to Celsius Temperature Conversion - TM-1-1510-224-10_269
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 - TM-1-1510-224-10_272
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
TAKE-OFF SPEEDS (KIAS) - FLAPS UP - TM-1-1510-224-10_276
TAKE-OFF SPEEDS (KIAS) - FLAPS UP (Contd)
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) - TM-1-1510-224-10_287
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 -200C (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 Profile - 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 Profile - 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 +37 C (Sheet 2 of 2)
Figure 7-72. Range Profile - 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 -300C (Sheet 2 of 2)
Figure 7-74. Loiter Power at 1700 RPM - ISA -200C (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 Profile - Loiter Power at 1700 RPM
Figure 7-82. Range Profile - Full Main Tanks
Figure 7-83. Endurance Profile - Full Main Tanks
Figure 7-84. Range Profile - Full Main and Aux Tanks
Figure 7-85. Endurance Profile - Full Main and Aux Tanks
Figure 7-86. One Engine Inoperative Max Cruise Power at 1700 RPM (Engine Anti-Ice Off) - ISA -300C (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 +300C (Sheet 2 of 2)
Figure 7-93, One Engine Inoperative Max Cruise Power at 1700 RPM (Ice Vanes Retracted) - ISA +37C (Sheet 1 of 2)
Figure 7-93. One Engine Inoperative Max Cruise Power at 1700 RPM (Ice Vanes Retracted) - 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
Figure 7-98. Landing Distance - One Engine Inoperative - Flaps Down
INTRODUCTION TO PERFORMANCE - TM-1-1510-224-10_401
Altimeter Correction - Normal System
Purpose - TM-1-1510-224-10_403
Net   Take-off   Flight   Path   -   Second   Segment- Flaps Up
Accelerate Stop - Flaps Approach
Net Take-off Flight Path - Third Segment.
Maximum Cruise Power At 1700 RPM.
Maximum Range Power at 1500 RPM.
Endurance Profile Full Main and Aux Tanks.
Table 7A-1. Route Segment Data2
Minimum    Static    Takeoff    Power    (Ice    Vanes Retracted).
Takeoff Path - One Engine Inoperative.
Climb One Engine Inoperative. - TM-1-1510-224-10_413
Table 7A-2. Example Cruise True Airspeeds
Table 7A-3. Example Cruise Results
Table 7A-4. Example Time, Fuel, and Distance
Table 7A-5. Example Fuel Flow (Ibs/hr)
Figure 7A-2. Airspeed Calibration - Normal System, Takeoff Ground Roll
Figure 7A-3. Airspeed Calibration - Normal System
Figure 7A-4. Altimeter Correction - Normal System
Figure 7A-5. Airspeed Calibration - Alternate System
Figure 7A-6. Altimeter Correction - Alternate System
Figure 7A-7. Indicated Outside Air Temperature Correction
Figure 7A-8. ISA Conversion
Figure 7A-9. Fahrenheit to Celsius Temperature Conversion
Figure 7A-10. Static Take-off Power at 1700 RPM, Ice Vanes Retracted
Figure 7A-11. Static Take-off Power at 1700 RPM, Ice Vanes Extended
Figure 7A-12. Wind Components
Figure 7A-13. Maximum Take-off Weight Permitted by Enroute Climb Requirements
Figure 7A-14. Maximum Take-off Weight to Achieve Positive One Engine Inoperative Climb at Liftoff - Flaps Up
Figure 7A-15. Maximum Take-off Weight as Limited by Tire Speed - Flaps Up
Figure 7A-16. Take-off Speeds (KIAS) - Flaps up (Sheet 1 of 2)
Figure 7A-16. Take-off Speeds (KIAS) - Flaps up (Sheet 2 of 2)
Figure 7A-17. Take-off Distance Over 50 Foot Obstacle - Flaps Up
Figure 7A-18. Accelerate Stop - Flaps Up
Figure 7A-19. Accelerate-Go Distance Over 50 Foot Obstacle - Flaps Up
Figure 7A-20. Net Take-off Flight Path - First Segment - Flaps Up
Figure 7A-21. Net Take-off Flight Path - Second Segment - Flaps Up
Figure 7A-22. Horizontal Distance from Reference Zero to Third Segment Climb - Flaps Up
Figure 7A-23. Maximum Take-off Weight to Achieve Positive One Engine Inoperative Climb at Liftoff - Flaps Approach
Figure 7A-24. Maximum Take-off Weight as Limited by Tire Speed - Flaps Approach
Figure 7A-25. Take-off Speeds (KIAS) - Flaps Approach (Sheet 1 of 2)
Figure 7-25. Take-off Speeds (KIAS) - Flaps Approach (Sheet 2 of 2) - TM-1-1510-224-10_443
Figure 7A-26. Take-off Distance Over 50 Foot Obstacle - Flaps Approach
Figure 7A-27. Accelerate Stop - Flaps Approach
Figure 7A-28. Accelerate-Go Distance Over 50 Foot Obstacle - Flaps Approach
Figure 7A-29. Net Take-off Flight Path - First Segment - Flaps Approach
Figure 7A-30. Net Take-off Flight Path - Second Segment - Flaps Approach
Figure 7A-31. Horizontal Distance from Reference Zero to Third Segment Climb - Flaps Approach
Figure 7A-32. Close-in Take-off Flight Path - Flaps Approach
Figure 7A-33. Distant Take-off Flight Path - Flaps Approach
Figure 7A-34. Net Take-off Flight Path - Third Segment
Figure 7A-35. Climb - Two Engines - Flaps Up
Figure 7A-36. Climb - Two Engines - Flaps Approach
Figure 7A-37. Climb - One Engine Inoperative
Figure 7A-38. Service Ceiling - One Engine Inoperative
Figure 7A-39. Time, Fuel, and Distance to Cruise Climb
Figure 7A-40. Maximum Cruise Power at 1700 RPM - ISA -30C (Sheet 1 of 2)
Figure 7A-40. Maximum Cruise Power at 1700 RPM - ISA -30C (Sheet 2 of 2)
Figure 7A-41. Maximum Cruise Power at 1700 RPM - ISA -20C (Sheet 1 of 2)
Figure 7A-41. Maximum Cruise Power at 1700 RPM - ISA -20C (Sheet 2 of 2)
Figure 7A-42. Maximum Cruise Power at 1700 RPM - ISA -10C (Sheet 1 of 2)
Figure 7A-42. Maximum Cruise Power at 1700 RPM - ISA -10C (Sheet 2 of 2)
Figure 7A-43. Maximum Cruise Power at 1700 RPM - ISA (Sheet 1 of 2)
Figure 7A-43. Maximum Cruise Power at 1700 RPM - ISA (Sheet 2 of 2)
Figure 7A-44. Maximum Cruise Power at 1700 RPM - ISA +10C (Sheet 1 of 2)
Figure 7A-44. Maximum Cruise Power at 1700 RPM - ISA +10C (Sheet 2 of 2)
Figure 7A-45. Maximum Cruise Power at 1700 RPM - ISA +20C (Sheet 1 of 2)
Figure 7A-45. Maximum Cruise Power at 1700 RPM - ISA +20C (Sheet 2 of 2)
Figure 7A-46. Maximum Cruise Power at 1700 RPM - ISA +30C (Sheet 1 of 2)
Figure 7A-46. Maximum Cruise Power at 1700 RPM - ISA +30C (Sheet 2 of 2)
Figure 7A-47. Maximum Cruise Power at 1700 RPM - ISA +37C (Sheet 1 of 2)
Figure 7A-47. Maximum Cruise Power at 1700 RPM - ISA +37C (Sheet 2 of 2)
Figure 7A-48. Maximum Cruise Speeds at 1700 RPM
Figure 7A-49. Maximum Cruise Power at 1700 RPM
Figure 7A-50. Fuel Flow at Maximum Cruise Power at 1700 RPM
Figure 7A-51. Range Profile - Maximum Cruise Power at 1700 RPM
Figure 7A-52. Normal Cruise Power at 1500 RPM - ISA -30C (Sheet 1 of 2)
Figure 7A-52. Normal Cruise Power at 1500 RPM - ISA -30C (Sheet 2 of 2)
Figure 7A-53. Normal Cruise Power at 1500 RPM - ISA -20C (Sheet 1 of 2)
Figure 7A-53. Normal Cruise Power at 1500 RPM - ISA -200C (Sheet 2 of 2)
Figure 7A-54. Normal Cruise Power at 1500 RPM - ISA -10C (Sheet 1 of 2)
Figure 7A-54. Normal Cruise Power at 1500 RPM - ISA -10C (Sheet 2 of 2)
Figure 7A-55. Normal Cruise Power at 1500 RPM - ISA (Sheet 1 of 2)
Figure 7A-55. Normal Cruise Power at 1500 RPM - ISA (Sheet 2 of 2)
Figure 7A-56. Normal Cruise Power at 1500 RPM - ISA +10C (Sheet 1 of 2)
Figure 7A-56. Normal Cruise Power at 1500 RPM - ISA +10C (Sheet 2 of 2)
Figure 7A-57. Normal Cruise Power at 1500 RPM - ISA +20C (Sheet 1 of 2)
Figure 7A-57. Normal Cruise Power at 1500 RPM - ISA +20C (Sheet 2 of 2)
Figure 7A-58. Normal Cruise Power at 1500 RPM - ISA +300C (Sheet I of 2)
Figure 7A-58. Normal Cruise Power at 1500 RPM - ISA +30C (Sheet 2 of 2)
Figure 7A-59. Normal Cruise Power at 1500 RPM - ISA +370C (Sheet 1 of 2)
Figure 7A-59. Normal Cruise Power at 1500 RPM - ISA +370C (Sheet 2 of 2)
Figure 7A-60. Normal Cruise Speeds at 1500 RPM
Figure 7A-61. Normal Cruise Power at 1500 RPM
Figure 7A-62. Fuel Flow at Normal Cruise Power at 1500 RPM
Figure 7A-63. Range Profile - Normal Cruise Power at 1500 RPM
Figure 7A-64. Maximum Range Power at 1500 RPM - ISA -30C (Sheet 1 of 2)
Figure 7A-64. Maximum Range Power at 1500 RPM - ISA -300C (Sheet 2 of 2)
Figure 7A-65. Maximum Range Power at 1500 RPM - ISA -20C (Sheet 1 of 2)
Figure 7A-65. Maximum Range Power at 1500 RPM - ISA -20C (Sheet 2 of 2)
Figure 7A-66. Maximum Range Power at 1500 RPM - ISA -10C (Sheet 1 of 2)
Figure 7A-66. Maximum Range Power at 1500 RPM - ISA -10C (Sheet 2 of 2)
Figure 7A-67. Maximum Range Power at 1500 RPM - ISA (Sheet 1 of 2)
Figure 7A-67. Maximum Range Power at 1500 RPM - ISA (Sheet 2 of 2)
Figure 7A-68. Maximum Range Power at 1500 RPM - ISA +10C (Sheet 1 of 2)
Figure 7A-68. Maximum Range Power at 1500 RPM - ISA +10C (Sheet 2 of 2)
Figure 7A-69. Maximum Range Power at 1500 RPM - ISA +20C (Sheet 1 of 2)
Figure 7A-69. Maximum Range Power at 1500 RPM - ISA +20C (Sheet 2 of 2)
Figure 7A-70. Maximum Range Power at 1500 RPM - ISA +30C (Sheet 1 of 2)
Figure 7A-70. Maximum Range Power at 1500 RPM - ISA +30C (Sheet 2 of 2)
Figure 7A-71. Maximum Range Power at 1500 RPM - ISA +37C (Sheet 1 of 2)
Figure 7A-71. Maximum Range Power at 1500 RPM - ISA +37C (Sheet 2 of 2)
Figure 7A-72. Range Profile - Maximum Range Power at 1500 RPM
Figure 7A-73. Loiter Power at 1700 RPM - ISA -30C (Sheet 1 of 2)
Figure 7A-73. Loiter Power at 1700 RPM - ISA -30C (Sheet 2 of 2)
Figure 7A-74. Loiter Power at 1700 RPM - ISA -20C (Sheet 1 of 2)
Figure 7A-74. Loiter Power at 1700 RPM - ISA -20C (Sheet 2 of 2)
Figure 7A-75. Loiter Power at 1700 RPM - ISA -10C (Sheet 1 of 2)
Figure 7A-75. Loiter Power at 1700 RPM - ISA -10C (Sheet 2 of 2)
Figure 7A-76. Loiter Power at 1700 RPM - ISA (Sheet 1 of 2)
Figure 7A-76. Loiter Power at 1700 RPM - ISA (Sheet 2 of 2)
Figure 7A-77. Loiter Power at 1700 RPM - ISA +10C (Sheet 1 of 2)
Figure 7A-77. Loiter Power at 1700 RPM - ISA +10C (Sheet 2 of 2)
Figure 7A-78. Loiter Power at 1700 RPM - ISA +20C (Sheet 1 of 2)
Figure 7A-78. Loiter Power at 1700 RPM - ISA +20C (Sheet 2 of 2)
Figure 7A-79. Loiter Power at 1700 RPM - ISA +30C (Sheet 1 of 2)
Figure 7A-79. Loiter Power at 1700 RPM - ISA +30C (Sheet 2 of 2)
Figure 7A-80. Loiter Power at 1700 RPM - ISA +37C (Sheet 1 of 2)
Figure 7A-80. Loiter Power at 1700 RPM - ISA +37C (Sheet 2 of 2)
Figure 7A-81. Endurance Profile - Loiter Power at 1700 RPM
Figure 7A-82. Range Profile - Full Main Tanks
Figure 7A-83. Endurance Profile - Full Main Tanks
Figure 7A-84. Range Profile - Full Main and Aux Tanks
Figure 7A-85. Endurance Profile - Full Main and Aux Tanks
Figure 7A-86. One Engine Inoperative Max Cruise Power at 1700 RPM (Engine Anti-Ice Off) - ISA -30C (Sheet 1 of 2)
Figure 7A-86. One Engine Inoperative Max Cruise Power at 1700 RPM (Ice Vanes Retracted) - ISA -30C (Sheet 2 of 2)
Figure 7A-87. One Engine Inoperative Max Cruise Power at 1700 RPM (Ice Vanes Retracted) - ISA -20C (Sheet 1 of 2)
Figure 7A-87. One Engine Inoperative Max Cruise Power at 1700 RPM (Ice Vanes Retracted) - ISA -20C (Sheet 2 of 2)
Figure 7A-88. One Engine Inoperative Max Cruise Power at 1700 RPM (Ice Vanes Retracted) - ISA -10C (Sheet 1 of 2)
Figure 7A-88. One Engine Inoperative Max Cruise Power at 1700 RPM (Ice Vanes Retracted) - ISA -10C (Sheet 2 of 2)
Figure 7A-89. One Engine Inoperative Max Cruise Power at 1700 RPM (Ice Vanes Retracted) - ISA (Sheet 1 of 2)
Figure 7A-89. One Engine Inoperative Max Cruise Power at 1700 RPM (Ice Vanes Retracted) - ISA (Sheet 2 of 2)
Figure 7A-90. One Engine Inoperative Max Cruise Power at 1700 RPM (Ice Vanes Retracted) - ISA +10C (Sheet 1 of 2)
Figure 7A-90. One Engine Inoperative Max Cruise Power at 1700 RPM (Ice Vanes Retracted) - ISA +10C (Sheet 2 of 2)
Figure 7A-91. One Engine Inoperative Max Cruise Power at 1700 RPM (Ice Vanes Retracted) - ISA +20C (Sheet 1 of 2)
Figure 7A-91. One Engine Inoperative Max Cruise Power at 1700 RPM (Ice Vanes Retracted) - ISA +20C (Sheet 2 of 2)
Figure 7A-92. One Engine Inoperative Max Cruise Power at 1700 RPM (Ice Vanes Retracted) - ISA +30C (Sheet 1 of 2)
Figure 7A-92. One Engine Inoperative Max Cruise Power at 1700 RPM (Ice Vanes Retracted) - ISA +30C (Sheet 2 of 2)
Figure 7A-93. One Engine Inoperative Max Cruise Power at 1700 RPM (Ice Vanes Retracted) - ISA +37C (Sheet 1 of 2)
Figure 7A-93. One Engine Inoperative Max Cruise Power at 1700 RPM (Ice Vanes Retracted) - ISA +37C (Sheet 2 of 2)
Figure 7A-94. Time, Fuel, and Distance to Descend
Figure 7A-95. Climb - Balked Landing
Figure 7A-96. Normal Landing Distance - Flaps Down
Figure 7A-97. Normal Landing Distance - Flaps Up
Figure 7A-98. Landing Distance - One Engine Inoperative - Flaps Down
Section II. OPERATING PROCEDURES AND MANEUVERS - TM-1-1510-224-10_557
BEFORE EXTERIOR CHECK - TM-1-1510-224-10_558
HYD   FLUID   SENSOR   TEST
HYD FLUID SENSOR TEST
AP & YD/TRIM DISC
ASE/ACS Perform BIT checks
ASE/ACS Program
Avionics Check
FUEL SAMPLE AND OIL CHECK - TM-1-1510-224-10_565
Figure 8-1. Exterior Inspection - TM-1-1510-224-10_566
Left wing center section Check
Right Wing Area.
Fuselage Right Side. - TM-1-1510-224-10_569
INTERIOR CHECK - TM-1-1510-224-10_570
Magnetic     compass
FIRST ENGINE START (BATTERY START) - TM-1-1510-224-10_572
ABORT START PROCEDURE - TM-1-1510-224-10_573
SECOND ENGINE START (GPU START) - TM-1-1510-224-10_574
ENGINE RUNUP - TM-1-1510-224-10_575
PNEUMATIC PRESSURE - TM-1-1510-224-10_576
BEFORE TAKEOFF - TM-1-1510-224-10_577
TAKEOFF.
DESCENT-ARRIVAL - TM-1-1510-224-10_579
TOUCH AND GO/STOP AND GO LANDING - TM-1-1510-224-10_580
ENGINE SHUTDOWN - TM-1-1510-224-10_581
Section III. INSTRUMENT FLIGHT - TM-1-1510-224-10_582
Figure 8-2. Stall Speeds - Power Idle - TM-1-1510-224-10_583
Section V. ADVERSE ENVIRONMENTAL CONDITIONS - TM-1-1510-224-10_584
During Flight. - TM-1-1510-224-10_585
DESERT   OPERATION   AND   HOT   WEATHER OPERATION.
ICE AND RAIN (TYPICAL)
SEVERE ICING
ARRIVAL BRIEFING - TM-1-1510-224-10_589
Section I. AIRCRAFT SYSTEMS
Figure 9-1. Emergency Exits and Equipment - TM-1-1510-224-10_591
ENGINE SHUTDOWN IN FLIGHT - TM-1-1510-224-10_592
ENGINE    RESTART    DURING    FLIGHT    (NO STARTER ASSIST)
SINGLE-ENGINE DESCENT/ARRIVAL - TM-1-1510-224-10_594
Figure 9-2. Maximum Glide Distance
Figure 9-3. Maximum Glide Distance
SINGLE-ENGINE LANDING CHECK
ENGINE ANTI-ICE FAILURE - TM-1-1510-224-10_598
Fuselage Fire - TM-1-1510-224-10_599
FUEL SYSTEM. - TM-1-1510-224-10_600
ELECTRICAL SYSTEM EMERGENCIES - TM-1-1510-224-10_601
EMERGENCY DESCENT - TM-1-1510-224-10_602
LANDING EMERGENCIES.
DITCHING - TM-1-1510-224-10_604
Figure 9-4. Ferry Chair Occupant Emergency Body Position
Figure 9-5. Wind Swell Ditch Heading Evaluation
APPENDIX A REFERENCES - TM-1-1510-224-10_607
APPENDIX B ABBREVIATIONS AND TERMS - TM-1-1510-224-10_608
METEOROLOGICAL TERMINOLOGY - TM-1-1510-224-10_609
CONTROL AND INSTRUMENT the shortest possible horizontal TERMINOLOGY
WEIGHT AND BALANCE TERMINOLOGY. - TM-1-1510-224-10_611
MISCELLANEOUS ABBREVIATIONS - TM-1-1510-224-10_612
MISCELLANEOUS ABBREVIATIONS (cont) - TM-1-1510-224-10_613
MISCELLANEOUS ABBREVIATIONS (cont)
MISCELLANEOUS ABBREVIATIONS (cont) - TM-1-1510-224-10_615
MISCELLANEOUS ABBREVIATIONS (cont) - TM-1-1510-224-10_616
MISCELLANEOUS ABBREVIATIONS (cont) - TM-1-1510-224-10_617

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