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CHAPTER 1 INTRODUCTION - TM-1-1510-223-10_12
USE OF WORDS SHALL, SHOULD, AND MAY
CHAPTER 2 AIRCRAFT AND SYSTEMS DESCRIPTION AND OPERATION
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 1 (Sheet 5 of 6)
Figure 2-1. General Exterior Arrangement - Bottom 2 (Sheet 6 of 6)
Figure 2-2. General Interior Arrangement
Figure 2-3. Principal Dimensions
Figure 2-4. Ground Turning Radius
Figure 2-5. Exhaust and Propeller Danger Area
Figure 2-6. Subpanels
figure 2-7 Overhead Circuit Breaker Panel
Landing Gear Warning Indicator Light Test Switch.
Landing Gear Alternate Extension.
Figure 2-8. Cockpit
ENTRANCE AND EXIT PROVISIONS - TM-1-1510-223-10_30
Figure 2-9. Cabin and Cargo Doors
WINDOWS.
Section II. EMERGENCY EQUIPMENT
Section III. ENGINES AND RELATED SYSTEMS - TM-1-1510-223-10_34
Figure 2-11. Engine (Sheet 1 of 2)
Figure 2-11. Engine (Sheet 2 of 2)
Figure 2-12. Control Pedestal and Pedestal Extension (Sheet 1 of 2)
Figure 2-12. Control Pedestal and Pedestal Extension (Sheet 2 of 2)
figure 2-13 Overhead Control Panel
ENGINE FUEL CONTROL SYSTEM.
ENGINE FIRE EXTINGUISHER SYSTEM
Figure 2-14. Engine Fire Detection System
Figure 2-15. Engine Fire Extinguisher System
Figure 2-16. Instrument Panel (Sheet 1 of 2)
Figure 2-16. Instrument Panel (Sheet 2 of 2)
AUTO IGNITION SYSTEM. - TM-1-1510-223-10_46
ENGINE INSTRUMENTS.
Figure 2-17. Fuel System Schematic
Figure 2-18. Fuel Management Panel
Figure 2-19. Crossfeed Fuel Flow
Figure 2-20. Gravity Feed Fuel Flow
FLIGHT CONTROL LOCKS
WING FLAPS.
Section VI. PROPELLERS
PROPELLER GOVERNORS. - TM-1-1510-223-10_55
PROPELLER LEVERS.
Section VII. UTILITY SYSTEMS - TM-1-1510-223-10_57
ANTENNA DEICING SYSTEM.
STALL WARNING SYSTEM
WINDSHIELD ELECTROTHERMAL ANTI-ICE SYSTEM
Pressure Differential.
OXYGEN SYSTEM.
Figure 2-24. Oxygen System - TM-1-1510-223-10_63
Normal Operation.
Table 2-5. Oxygen Duration in Minutes 140 Cubic Foot System - TM-1-1510-223-10_65
WINDSHIELD WIPERS - TM-1-1510-223-10_66
Section VIII. HEATING, VENTILATION, COOLING, AND ENVIRONMENTAL CONTROL
Figure 2-26. Environmental System - TM-1-1510-223-10_68
AIR CONDITIONING SYSTEM
Normal Operation. - TM-1-1510-223-10_70
ENVIRONMENTAL CONTROLS.
Section IX. ELECTRICAL POWER SUPPLY AND DISTRIBUTION SYSTEM - TM-1-1510-223-10_72
DC POWER SUPPLY.
Figure 2-27. DC Electrical System (Sheet 1 of 3)
Figure 2-27. DC Electrical System (Sheet 2 of 3)
Figure 2-27. DC Electrical System (Sheet 3 of 3)
Figure 2-28. Single Phase AC Electrical System
Figure 2-29. Three Phase AC Electrical System
Figure 2-30. Mission Equipment DC Power System
Figure 2-31. Mission AfDC Power Cabinet
AC POWER SUPPLY
Section X. LIGHTING - TM-1-1510-223-10_82
Figure 2-32. Exterior Lighting - TM-1-1510-223-10_83
Cabin Lighting
Section XI. FLIGHT INSTRUMENTS
STANDBY ATTITUDE INDICATOR.
ACCELEROMETER.
Mission Annunciator Panel.
Table 2-6. Warning Annunciator Panel Legend - TM-1-1510-223-10_89
Figure 2-37. Caution/Advisory Annuciator Panel
Table 2-7. Caution/Advisory Annunciator Panel Legend - TM-1-1510-223-10_91
Zulu or Greenwich mean time mode (ZU)
Section XII. SERVICING, PARKING, AND MOORING - TM-1-1510-223-10_93
FILLING FUEL TANKS.
DRAINING MOISTURE FROM FUEL SYSTEM
USE OF FUELS.
Figure 2-39. Servicing Locations
SERVICING THE CHEMICAL TOILET.
SERVICING OXYGEN SYSTEM.
GROUND HANDLING - TM-1-1510-223-10_100
Figure 2-40. Oxygen System Serving Pressure
Figure 2-41. Parking, Covers, Ground Handling, and Towing Equipment
PARKING.
MOORING.
Figure 2-43. Mooring the Aircraft
Disconnect battery
CHAPTER 3 AVIONICS Section I. GENERAL
Section II. COMMUNICATIONS - TM-1-1510-223-10_108
Figure 3-1. Audio Control Panel - TM-1-1510-223-10_109
Figure 3-2. VHF-FM IF/AM Alternate Communication Switch Panel
UHF TRANSCEIVER (AN/ARC-164, HAVE QUICK II).
Figure 3-3. UHF Transceiver - TM-1-1510-223-10_112
VHF COMMUNICATIONS TRANSCEIVERS (VHF-22B).
Figure 3-4. VHF Communications Transceiver Control Unit - TM-1-1510-223-10_114
Equipment turn-on
HF COMMUNICATIONS TRANSCEIVER (KHF-950).
Table 3-1. VHF Communications Transceiver Fault Codes
Frequency Selection.
Programming semi-duplex preset channels
Maritime Radiotelephone Network Channel
VHF-FM TRANSCEIVER (AN/ARC-201A(V), SINCGARS.
TUNING
FH (frequency hopping mode)
Top line - 2-FM SETUP.
EMERGENCY LOCATOR TRANSMITTER (ELT 110-4)
Section III. NAVIGATION
figgure 3-7 Integrated Flight Control System Block Diagram
ATTITUDE AND HEADING REFERENCE SYSTEM.
Weather pushbutton selector switch
INS/TACAN
ELECTRONIC ATTITUDE DIRECTOR INDICATOR (EADI). - TM-1-1510-223-10_131
Figure 3-9. Electronic Attitude Director Indicator (EADI) - TM-1-1510-223-10_132
Fast/slow pointer and scale
ELECTRONIC HORIZONTAL SITUATION INDICATOR (EHSI).
Figure 3-10. EADI Caution Annunciators (Amber)
Figure 3-11. EADI Failure Annunciations (Red)
Figure 3-12. EADI Input/Output Processer Failure Indications
Figure 3-13. Electronic Horizontal Situation Indicator (EHSI)
Weather radar mode annunciator.
Figure 3-14. Flight Director Remote Heading/Course Control Panel
Figure 3-15. EHSI Partial Compass Format Unique Indications
Figure 3-16. EISI Partial Compass VOR Map Mode
EHSI Weather Radar Displays.
EHSI Red failure annunciations (fig. 3-19)
DIGITAL FLIGHT CONTROL SYSTEM (DFZ450).
Autopilot Self-Disconnection Fault Messages.
Figure 3-20. EADI/EHSI Composite Display - TM-1-1510-223-10_147
Table 3-4. Digital Flight Control System Error Codes - TM-1-1510-223-10_148
Table 3-5. Digital Flight Control System Limits (Sheet 1 of 3) - TM-1-1510-223-10_149
Table 3-5. Digital Flight Control System Limits (Sheet 2 of 3) - TM-1-1510-223-10_150
Autopilot switch-indicator.
Figure 3-22. Flight Director Mode Selector - TM-1-1510-223-10_152
Table 3-6. Flight Director Modes Reset when EFIS Sources Change
Figure 3-23. Altitude Preselector - TM-1-1510-223-10_154
Elevator trim follow-up - Check
Digital Flight Control System Modes of Operation
VOR approach mode
Inertial navigation system (INS) steering mode
Back course mode
ILS approach mode.
Indicated airspeed hold mode.
VHF NAVIGATION RECEIVERS (VIR-32).
Figure 3-24. VHF Navigation Receiver Control Unit - TM-1-1510-223-10_163
Frequency selection
Marker beacon self-test. - TM-1-1510-223-10_165
ADF RECEIVER (ADF-60).
Table 3-7. VHF Navigation Receiver Fault Codes - TM-1-1510-223-10_167
Figure 3-25. ADF Control Unit - TM-1-1510-223-10_168
TACAN/DME SYSTEM (AN/ARN-154)
PAGE pushbutton selector switch
Figure 3-27. TACAN/DME Display Unit
INERTIAL NAVIGATION SYSTEM
Figure 3-28. INS Mode Selector
Alignment states 7 and 6.
Normal Operating Procedures - TM-1-1510-223-10_175
Table 3-9. INS Malfunction Codes - TM-1-1510-223-10_176
Table 3-10. INS Action Codes and Recommended Actions - TM-1-1510-223-10_177
Pattern steering mode
Table 3-11. Datum Cross Reference
INS operation.
GLOBAL POSITIONING SYSTEM (AN/ ASN-149 ((B)3))
GPS time data insertion
CHALS USE OF GPS AND INS
Section IV. RADAR AND TRANSPONDER
Figure 3-29. Weather Radar/Lightning Sensor System Control Panel
Figure 3-30. EFIS Weather Test Pattern (Typical, 120-Degree Scan)
Table 3-12. Video Integrated Processor VS, .Aircraft Radar Return Levels
Antenna tilt angle control.
Weather Radar Modes of Operation. - TM-1-1510-223-10_189
Lightning Sensor System Display
Figure 3-33. Lightning Rate of Occurrence Symbols
TRANSPONDER SET (APX-100)
Table 3-13. Lightning Sensor System Failure Codes
Figure 3-34. Transponder Control Panel
PILOT'S BAROMETRIC ALTIMETER INDICATOR (BA-141).
Controls, Indicators and Functions.
Figure 3-35. Pilot's Barometric Altimeter Indicator
CHAPTER 4 MISSION EQUIPMENT Section I. MISSION AVIONICS
Radio altimeter switch
Figure 4-1. Mission Control Panel
Section II. AIRCRAFT SURVIVABILITY EQUIPMENT
SYSTEM DAILY PREFLIGHT/RE-ARM TEST.
DISPENSER COMP lamp
Chaff Dispenser (Right Nacelle) - Preliminary Procedure
MANUAL SYSTEM RESET
AMMUNITION.
RADAR SIGNAL DETECTING SET (AN/ APR-39(V)2).
Figure 4-2. Multifunction Display (MFD)
Figure 4-3. Keyboard Unit (KU)
CHAPTER 5 OPERATING LIMITS AND RESTRICTIONS - TM-1-1510-223-10_210
Figure 5-1. Instrument Markings (Sheet 1 of 4)
Figure 5-1. Instrument Markings (Sheet 2 of 4)
Figure 5-1. Instrument Markings (Sheet 3 of 4)
Figure 5-1. Instrument Markings (Sheet 4 of 4)
PITOT HEAT LIMITATIONS
Section III. POWER LIMITS
Table 5-1. Engine Operating Limitations - TM-1-1510-223-10_217
Section V. AIRSPEED LIMITS, MAXIMUM AND MINIMUM
Figure 5-2. Flight Envelope
Section VII. ENVIRONMENTAL RESTRICTIONS
ICING LIMITATIONS (SEVERE).
Section VIII. OTHER LIMITATIONS - TM-1-1510-223-10_222
Table 5-3. Required Equipment Listing
Table 5-3. Required Equipment Listing - Continued - TM-1-1510-223-10_224
Table 5-3. Required Equipment Listing - Continued - TM-1-1510-223-10_225
Table 5-3. Required Equipment Listing - Continued - TM-1-1510-223-10_226
CHAPTER 6 WEIGHT/BALANCE AND LOADING - TM-1-1510-223-10_227
Figure 6-1. Aircraft Compartments and Stations - TM-1-1510-223-10_228
Section III. FUEL/OIL
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 IV. CENTER OF GRAVITY
figure 6-2 Density Variation of Aviation Fuel
Figure 6-3. Center of Gravity Loading Diagram
Section VI. SURVIVABILITY EQUIPMENT - TM-1-1510-223-10_235
CHAPTER 7 PERFORMANCE - TM-1-1510-223-10_236
CHAPTER 7 PERFORMANCE - TM-1-1510-223-10_237
CHAPTER 7 PERFORMANCE - TM-1-1510-223-10_238
INTRODUCTION TO PERFORMANCE - TM-1-1510-223-10_239
Fahrenheit to Celsius Temperature Conversion
Accelerate-stop distance.
Figure 7-1. Takeoff Path Profile One Engine Inoperative
Flight Planning Example
Cruise speeds
Reserve fuel
Range and Endurance
Enroute Instrument Corrections
Figure 7-2. Airspeed Calibration - Normal System., Takeoff Ground Roll
Figure 7-3. Airspeed Calibration - Normal System - TM-1-1510-223-10_249
Figure 7-4. Altimeter Correction - Normal System - TM-1-1510-223-10_250
Figure 7-5. Airspeed Calibration - Alternate System - TM-1-1510-223-10_251
Figure 7-6. Altimeter Correction - Alternate System - TM-1-1510-223-10_252
Figure 7-7. Indicated Outside Air Temperature Correction - TM-1-1510-223-10_253
Figure 7-8. ISA Conversion - TM-1-1510-223-10_254
Figure 7-9. Fahrenheit to Celsius Temperature Conversion - TM-1-1510-223-10_255
Figure 7-10. Static Take-off Power at 1700 RPM, Ice Vanes Retracted to IR
Figure 7-11. Static Take-off Power at 1700 RPM, Ice Vanes Retracted CA
Figure 7-12. Static Take-off Power at 1700 RPM, Ice Vanes Extended IR
Figure 7-13. Static Take-off Power at 1700 RPM, Ice Vanes Extended CA
Figure 7-14. Wind Components
MAXIMUM TAKE-OFF WEIGHT PERMITTED BY ENROUTE CLIMB REQUIREMENTS
Figure 7-16. Maximum Take-off Weight to Achieve Positive One Engine Inoperative Climb at Liftoff- Flaps Up IR
Figure 7-17. Maximum Take-off Weight as Limited by Tire Speed - Flaps Up
Figure 7-18. Take-off Speeds (KIAS) - Flaps Up
Figure 7-19. Take-off Distance Over 50 Foot Obstacle - Flaps Up IR
Figure 7-20. Accelerate Stop - Flaps Up IR
Figure 7-21. Accelerate-Go Distance Over 50 Foot Obstacle - Flaps Up IR
NET TAKE-OFF FLIGHT PATH - FIRST SEGMENT - FLAPS UP ONE ENGINE INOPERATIVE
NET TAKE-OFF FLIGHT PATH - SECOND SEGMENT - FLAPS UP ONE ENGINE INOPERATIVE
ASSOCIATED CONDITIONS
Figure 7-25. Maximum Take-off Weight to Achieve Positive One Engine Inoperative Climb at Liftoff - Flaps Approach
Figure 7-26. Maximum Take-off Weight as Limited by Tire Speed - Flaps Approach
TAKE-OFF SPEEDS (KIAS) - FLAPS UP - TM-1-1510-223-10_273
TAKE-OFF DISTANCE - FLAPS APPROACH
ACCELERATE-STOP - FLAPS APPROACH
ACCELERATE-GO - FLAPS APPROACH OVER 50-FOOT OBSTACLE
NET TAKE-OFF FLIGHT PATH - FIRST SEGMENT - FLAPS APPROACH ONE ENGINE INOPERATIVE
NET TAKE-OFF FLIGHT PATH - SECOND SEGMENT - FLAPS APPROACH ONE ENGINE INOPERATIVE
Figure 7-33. Horizontal Distance from Reference Zero to Third Segment Climb - Flaps Approach IR
CLOSE-IN TAKE-OFF FLIGHT PATH
DISTANT TAKE-OFF FLIGHT PATH - TM-1-1510-223-10_281
NET TAKE-OFF FLIGHT PATH - THIRD SEGMENT ONE ENGINE INOPERATIVE
Figure 7-37. Climb - Two Engines - Flaps Up
CLIMB - TWO ENGINES - FLAPS APPROACH
Figure 7-39. Climb - One Engine Inoperative
SERVICE CEILING - ONE ENGINE INOPERATIVE
TIME, FUEL, AND DISTANCE TO CRUISE CLIMB
Figure 7-42. Maximum Cruise Power at 1700 RPM - ISA -300C (Sheet 1 of 2) IR
MAXIMUM CRUISE POWER 1700 RPM ISA -30C - TM-1-1510-223-10_289
MAXIMUM CRUISE POWER 1700 RPM ISA -30C - TM-1-1510-223-10_290
MAXIMUM CRUISE POWER 1700 RPM ISA -30C - TM-1-1510-223-10_291
MAXIMUM CRUISE POWER 1700 RPM ISA -20C
Figure 7-44. Maximum Cruise Power at 1700 RPM - ISA -20C (Sheet 2 of 2) IR
Figure 7-45. Maximum Cruise Power at 1700 RPM - ISA -20 C (Sheet 1 of 2) CA
Figure 7-45. Maximum Cruise Power at 1700 RPM - ISA -20 C (Sheet 2 of 2) CA
Figure 7-46. Maximum Cruise Power at 1700 RPM - ISA -10 C (Sheet 1 of 2) IR
Figure 7-46. Maximum Cruise Power at 1700 RPM - ISA -10 C (Sheet 2 of 2) IR
Figure 747. Maximum Cruise Power at 1700 RPM - ISA -10 C (Sheet 1 of 2) CA
Figure 7-47. Maximum Cruise Power at 1700 RPM - ISA -10 C (Sheet 2 of 2) CA
Figure 7-48. Maximum Cruise Power at 1700 RPM - ISA (Sheet 1 of 2) IR
Figure 7-48. Maximum Cruise Power at 1700 RPM - ISA (Sheet 2 of 2) IR
Figure 7-49. Maximum Cruise Power at 1700 RPM - ISA (Sheet 1 of 2) CA
Figure 7-49. Maximum Cruise Power at 1700 RPM - ISA (Sheet 2 of 2) CA
Figure 7-50. Maximum Cruise Power at 1700 RPM - ISA +10 C (Sheet 1 of 2) IR
Figure 7-50. Maximum Cruise Power at 1700 RPM - ISA +10 C (Sheet 2 of 2) IR
Figure 7-51. Maximum Cruise Power at 1700 RPM - ISA +10 C (Sheet 1 of 2) CA
Figure 7-51. Maximum Cruise Power at 1700 RPM - ISA +10 C (Sheet 2 of 2) CA
Figure 7-52. Maximum Cruise Power at 1700 RPM - ISA +20 C (Sheet 1 of 2) IR
Figure 7-52. Maximum Cruise Power at 1700 RPM - ISA +20 C (Sheet 2 of 2) IR
Figure 7-53. Maximum Cruise Power at 1700 RPM - ISA +20 C (Sheet 1 of 2) CA
Figure 7-53. Maximum Cruise Power at 1700 RPM - ISA +20 C (Sleet 2 of 2) CA
Figure 7-54. Maximum Cruise Power at 1700 RPM - ISA +30 C (Sheet 1 of 2) IR
Figure 7-54. Maximum Cruise Power at 1700 RPM - ISA +30 C (Sheet 2 of 2) IR
Figure 7-55. Maximum Cruise Power at 1700 RPM - ISA +30 C (Sheet 1 of 2) CA
Figure 7-55. Maximum Cruise Power at 1700 RPM - ISA +30 C (Sheet 2 of 2) CA
Figure 7-56. Maximum Cruise Power at 1700 RPM - ISA +37 C (Sheet 1 of 2) IR
Figure 7-56. Maximum Cruise Power at 1700 RPM - ISA +37 C (Sheet 2 of 2) IR
Figure 7-57. Maximum Cruise Power at 1700 RPM - ISA +37 C (Sheet 1 of 2) CA
Figure 7-57. Maximum Cruise Power at 1700 RPM - ISA +37 C (Sheet 2 of 2) CA
Figure 7-58. Maximum Cruise Speeds at 1700 RPM IR
Figure 7-59. Maximum Cruise Speeds at 1700 RPM CA
Figure 7-60. Maximum Cruise Power at 1700 RPM IR
Figure 7-61. Maximum Cruise Power at 1700 RPM CA
Figure 7-62. Fuel Flow at Maximum Cruise Power at 1700 RPM IR
Figure 7-63. Fuel Flow at Maximum Cruise Power at 1700 RPM CA
Figure 7-64. Range Profile - Maximum Cruise Power at 1700 RPM
Figure 7-65. Normal Cruise Power at 1500 RPM - ISA -30 C (Sheet 1 of 2) IR
Figure 7-65. Normal Cruise Power at 1500 RPM - ISA -30 C (Sheet 2 of 2) IR
Figure 7-66. Normal Cruise Power at 1500 RPM - ISA -30 C (Sheet 1 of 2) CA
Figure 7-66. Normal Cruise Power at 1500 RPM - ISA -30 C (Sheet 2 of 2) CA
Figure 7-67. Normal Cruise Power at 1500 RPM - ISA -20 C (Sheet 1 of 2) IR
Figure 7-67. Normal Cruise Power at 1500 RPM - ISA -20 C (Sheet 2 of 2) IR
Figure 7-68. Normal Cruise Power at 1500 RPM - ISA -20 C (Sheet 1 of 2) CA
Figure 7-68. Normal Cruise Power at 1500 RPM - ISA -20 C (Sheet 2 of 2) CA
Figure 7-69. Normal Cruise Power at 1500 RPM - ISA -10 C (Sheet 1 of 2) IR
Figure 7-69. Normal Cruise Power at 1500 RPM - ISA -10 C (Sheet 2 of 2) IR
Figure 7-70. Normal Cruise Power at 1500 RPM - ISA -10 C (Sheet 1 of 2) CA
Figure 7-70. Normal Cruise Power at 1500 RPM - ISA -10 C (Sheet 2 of 2) CA
Figure 7-71. Normal Cruise Power at 1500 RPM - ISA (Sheet 1 of 2) IR
Figure 7-71. Normal Cruise Power at 1500 RPM - ISA (Sheet 2 of 2) IR
Figure 7-72. Normal Cruise Power at 1500 RPM - ISA (Sheet 1 of 2) CA
Figure 7-72. Normal Cruise Power at 1500 RPM - ISA (Sheet 2 of 2) CA
Figure 7-73. Normal Cruise Power at 1500 RPM - ISA +10 C (Sheet 1 of 2) IR
Figure 7-73. Normal Cruise Power at 1500 RPM - ISA +10 C (Sheet 2 of 2) IR
Figure 7-74. Normal Cruise Power at 1500 RPM - ISA +10 C (Sheet 1 of 2) CA
Figure 7-74. Normal Cruise Power at 1500 RPM - ISA +10 C (Sheet 2 of 2) CA
Figure 7-75. Normal Cruise Power at 1500 RPM - ISA +20 C (Sheet 1 of 2) IR
Figure 7-75. Normal Cruise Power at 1500 RPM - ISA +20 C (Sheet 2 of 2) IR
Figure 7-76. Normal Cruise Power at 1500 RPM - ISA +20 C (Sheet 1 of 2) CA
Figure 7-76. Normal Cruise Power at 1500 RPM - ISA +20 C (Sheet 2 of 2) CA
Figure 7-77. Normal Cruise Power at 1500 RPM - ISA +30 C (Sheet 1 of 2) IR
Figure 7-77. Normal Cruise Power at 1500 RPM - ISA +30 C (Sheet 2 of 2) IR
Figure 7-78. Normal Cruise Power at 1500 RPM - ISA +30 C (Sheet 1 of 2) CA
Figure 7-78. Normal Cruise Power at 1500 RPM - ISA +30 C (Sheet 2 of 2) CA
Figure 7-79. Normal Cruise Power at 1500 RPM - ISA +37 C (Sheet 1 of 2) IR
Figure 7-79. Normal Cruise Power at 1500 RPM - ISA +37 C (Sheet 2 of 2)IR
Figure 7-80. Normal Cruise Power at 1500 RPM - ISA +37 C (Sheet 1 of 2) CA
Figure 7-80. Normal Cruise Power at 1500 RPM - ISA +37 C (Sheet 2 of 2) CA
Figure 7-81. Normal Cruise Speeds at 1500 RPM IR
Figure 7-82. Normal Cruise Speeds at 1500 RPM CA
Figure 7-83. Normal Cruise Power at 1500 RPM IR
Figure 7-84. Normal Cruise Power at 1500 RPM CA
Figure 7-85. Fuel Flow at Normal Cruise Power at 1500 RPM IR
Figure 7-86. Fuel Flow at Normal Cruise Power at 1500 RPM CA
Figure 7-87. Range Profile - Normal Cruise Power at 1500 RPM
Figure 7-88. Maximum Range Power at 1500 RPM - ISA -30C (Sheet 1 of 2) IR
Figure 7-88. Maximum Range Power at 1500 RPM - ISA -30C (Sheet 2 of 2) IR
Figure 7-89. Maximum Range Power at 1500 RPM - ISA -30C (Sheet 1 of 2)CA
Figure 7-89. Maximum Range Power at 1500 RPM - ISA -30C (Sheet 2 of 2)CA
Figure 7-90. Maximum Range Power at 1500 RPM - ISA -20C (Sheet 1 of 2) IR
Figure 7-90. Maximum Range Power at 1500 RPM - ISA -20C (Sheet 2 of 2) IR
Figure 7-91. Maximum Range Power at 1500 RPM - ISA -20C (Sheet 1 of 2) CA
Figure 7-91. Maximum Range Power at 1500 RPM - ISA -20C (Sheet 2 of 2) CA
Figure 7-92. Maximum Range Power at 1500 RPM - ISA -10C (Sheet 1 of 2) IR
Figure 7-92. Maximum Range Power at 1500 RPM - ISA -10C (Sheet 2 of 2) IR
Figure 7-93. Maximum Range Power at 1500 RPM - ISA -10C (Sheet 1 of 2) CA
Figure 7-93. Maximum Range Power at 1500 RPM - ISA -10C (Sheet 2 of 2) CA
Figure 7-94. Maximum Range Power at 1500 RPM - ISA (Sheet 1 of 2) IR
Figure 7-94. Maximum Range Power at 1500 RPM - ISA (Sheet 2 of 2) IR
Figure 7-95. Maximum Range Power at 1500 RPM - ISA (Sleet 1 of 2) CA
Figure 7-95. Maximum Range Power at 1500 RPM - ISA (Sheet 2 of 2) CA
Figure 7-96. Maximum Range Power at 1500 RPM - ISA +10 C (Sheet 1 of 2) IR
Figure 7-96. Maximum Range Power at 1500 RPM - ISA +10 C (Sheet 2 of 2) IR
Figure 7-97. Maximum Range Power at 1500 RPM - ISA +10 C (Sheet 1 of 2) CA
Figure 7-97. Maximum Range Power at 1500 RPM - ISA +10 C (Sheet 2 of 2) CA
Figure 7-98. Maximum Range Power at 1500 RPM - ISA +20 C (Sheet 1 of 2) IR
Figure 7-98. Maximum Range Power at 1500 RPM - ISA +20 C (Sheet 2 of 2) IR
Figure 7-99. Maximum Range Power at 1500 RPM - ISA +20 C (Sheet 1 of 2) CA
Figure 7-99. Maximum Range Power at 1500 RPM - ISA +20 C (Sheet 2 of 2) CA
Figure 7-100. Maximum Range Power at 1500 RPM - ISA +30 C (Sheet 1 of 2) IR
Figure 7-100. Maximum Range Power at 1500 RPM - ISA +30 C (Sheet 2 of 2) IR
Figure 7-101. Maximum Range Power at 1500 RPM - ISA +30 C (Sheet 1 of 2) CA
Figure 7-101. Maximum Range Power at 1500 RPM - ISA +30 C (Sheet 2 of 2) CA
Figure 7-102. Maximum Range Power at 1500 RPM - ISA +37 C (Sheet 1 of 2) IR
Figure 7-102. Maximum Range Power at 1500 RPM - ISA +37 C (Sheet 2 of 2) IR
Figure 7-103. Maximum Range Power at 1500 RPM - ISA +37 C (Sheet 1 of 2) CA
Figure 7-103. Maximum Range Power at 1500 RPM - ISA +37 C (Sheet 2 of 2) CA
Figure 7-104. Range Profile - Maximum Range Power at 1500 RPM
Figure 7-105. Loiter Power at 1700 RPM - ISA -30C (Sheet 1 of 2) IR
Figure 7-105. Loiter Power at 1700 RPM - ISA -30C (Sheet 2 of 2) IR
Figure 7-106. Loiter Power at 1700 RPM - ISA -30C (Sheet 1 of 2) IR
Figure 7-106. Loiter Power at 1700 RPM - ISA -30C (Sheet 2 of 2) CA
Figure 7-107. Loiter Power at 1700 RPM - ISA -20C (Sheet 1 of 2) IR
Figure 7-107. Loiter Power at 1700 RPM - ISA -20C (Sheet 2 of 2) IR
Figure 7-108. Loiter Power at 1700 RPM - ISA -20C (Sheet 1 of 2) CA
Figure 7-108. Loiter Power at 1700 RPM - ISA -20C (Sheet 2 of 2) CA
Figure 7-109. Loiter Power at 1700 RPM - ISA -10C (Sheet 1 of 2) IR
Figure 7-109. Loiter Power at 1700 RPM - ISA -10C (Sheet 2 of 2) IR
Figure 7-110. Loiter Power at 1700 RPM - ISA -10C (Sheet 1 of 2) CA
Figure 7-110. Loiter Power at 1700 RPM - ISA -10C (Sheet 2 of 2) CA
Figure 7-111. Loiter Power at 1700 RPM - ISA (Sheet 1 of 2) IR
Figure 7-111. Loiter Power at 1700 RPM - ISA (Sheet 2 of 2) IR
Figure 7-112. Loiter Power at 1700 RPM - ISA (Sheet 1 of 2) CA
Figure 7-112. Loiter Power at 1700 RPM - ISA (Sheet 2 of 2) CA
Figure 7-113. Loiter Power at 1700 RPM - ISA +10C (Sheet 1 of 2) IR
Figure 7-113. Loiter Power at 1700 RPM - ISA +10C (Sheet 2 of 2) IR
Figure 7-114. Loiter Power at 1700 RPM - ISA +10C (Sheet 1 of 2) CA
Figure 7-114. Loiter Power at 1700 RPM - ISA +10C (Sheet 2 of 2) CA
Figure 7-115. Loiter Power at 1700 RPM - ISA +20C (Sheet 1 of 2) IR
Figure 7-115. Loiter Power at 1700 RPM - ISA +20C (Sheet 2 of 2) IR
Figure 7-116. Loiter Power at 1700 RPM - ISA +20C (Sheet 1 of 2) CA
Figure 7-116. Loiter Power at 1700 RPM - ISA +20C (Sheet 2 of 2) CA
Figure 7-117. Loiter Power at 1700 RPM - ISA +30C (Sheet 1 of 2) IR
Figure 7-117. Loiter Power at 1700 RPM - ISA +30C (Sheet 2 of 2) IR
Figure 7-118. Loiter Power at 1700 RPM - ISA +30C (Sheet 1 of 2) CA
Figure 7-118. Loiter Power at 1700 RPM - ISA +30C (Sheet 2 of 2) CA
Figure 7-119. Loiter Power at 1700 RPM - ISA +37C (Sheet 1 of 2) IR
Figure 7-119. Loiter Power at 1700 RPM - ISA +37C (Sheet 2 of 2) IR
Figure 7-120. Loiter Power at 1700 RPM - ISA +37C (Sheet 1 of 2) CA
Figure 7-120. Loiter Power at 1700 RPM - ISA +37C (Sheet 2 of 2) CA
Figure 7-121. Endurance Profile - Loiter Power IR
Figure 7-122. Range Profile - Full Main Tanks
Figure 7-123. Endurance Profile - Full Main Tanks IR
Figure 7-124. Range Profile - Full Main and Aux Tanks
ENDURANCE PROFILE - FULL MAIN & AUX TANKS STANDARD DAY (ISA)
ONE-ENGINE-INOPERATIVE MAXIMUM CRUISE POWER 1700 RPM ISA -30C
Figure 7-126. One Engine Inoperative Max Cruise Power at 1700 RPM - ISA-30 C (Sheet 2 of 2) IR
ONE-ENGINE INOPERATIVE MAXIMUM CRUISE POWER 1700 RPM ISA -30C
Figure 7-127. One Engine Inoperative Max Cruise Power at 1700 RPM - ISA -30 C (Sheet 2 of 2) CA
Figure 7-128. One Engine Inoperative Max Cruise Power at 1700 RPM - ISA -20 C (Sheet 1 of 2) IR
Figure 7-128. One Engine Inoperative Max Cruise Power at 1700 RPM - ISA -20 C (Sheet 2 of 2) IR
Figure 7-129. One Engine Inoperative Max Cruise Power at 1700 RPM - ISA -20 C (Sheet 1 of 2) CA
Figure 7-129. One Engine Inoperative Max Cruise Power at 1700 RPM - ISA -20 C (Sheet 2 of 2) CA
Figure 7-130. One Engine Inoperative Max Cruise Power at 1700 RPM - ISA -10 C (Sheet 1 of 2) IR
Figure 7-130. One Engine Inoperative Max Cruise Power at 1700 RPM - ISA -10 C (Sheet 2 of 2) IR
Figure 7-131. One Engine Inoperative Max Cruise Power at 1700 RPM - ISA -10 C (Sheet 1 of 2) CA
Figure 7-131. One Engine Inoperative Max Cruise Power at 1700 RPM - ISA -10 C (Sheet 2 of 2) CA
Figure 7-132. One Engine Inoperative Max Cruise Power at 1700 RPM - ISA (Sheer 1 of 2) IR
Figure 7-132. One Engine Inoperative Max Cruise Power at 1700 RPM - ISA (Sheet 2 of 2) IR
Figure 7-133. One Engine Inoperative Max Cruise Power at 1700 RPM - ISA (Sheet 1 of 2) CA
Figure 7-133. One Engine Inoperative Max Cruise Power at 1700 RPM - ISA (Sheet 2 of 2) CA
Figure 7-134. One Engine Inoperative Max Cruise Power at 1700 RPM - ISA +10 C (Sheet 1 of 2) IR
Figure 7-134. One Engine Inoperative Max Cruise Power at 1700 RPM - ISA +10 C (Sheet 2 of 2) IR
Figure 7-135. One Engine Inoperative Max Cruise Power at 1700 RPM - ISA +10 C (Sheet 1 of 2) CA
Figure 7-135. One Engine Inoperative Max Cruise Power at 1700 RPM - ISA +10 C (Sheet 2 of 2) CA
Figure 7-136. One Engine Inoperative Max Cruise Power at 1700 RPM - ISA +20 C (Sheet 1 of 2) IR
Figure 7-136. One Engine Inoperative Max Cruise Power at 1700 RPM - ISA +20 C (Sheet 2 of 2) IR
Figure 7-137. One Engine Inoperative Max Cruise Power at 1700 RPM - ISA +20 C (Sheet 1 of 2) CA
Figure 7-137. One Engine Inoperative Max Cruise Power at 1700 RPM - ISA +20 C (Sheet 2 of 2) CA
Figure 7-138. One Engine Inoperative Max Cruise Power at 1700 RPM - ISA +30 C (Sheet 1 of 2) IR
Figure 7-138. One Engine Inoperative Max Cruise Power at 1700 RPM - ISA +30 C (Sheet 2 of 2) IR
Figure 7-139. One Engine Inoperative Max Cruise Power at 1700 RPM - ISA +30 C (Sheet 1 of 2) CA
Figure 7-139. One Engine Inoperative Max Cruise Power at 1700 RPM - ISA +30 C (Sheet 2 of 2) CA
Figure 7-140. One Engine Inoperative Max Cruise Power at 1700 RPM - ISA +37 C (Sheet 1 of 2) IR
Figure 7-140. One Engine Inoperative Max Cruise Power at 1700 RPM - ISA +37 C (Sheet 2 of 2) IR
Figure 7-141. One Engine Inoperative Max Cruise Power at 1700 RPM - ISA +37 C (Sheet 1 of 2) CA
Figure 7-141. One Engine Inoperative Max Cruise Power at 1700 RPM - ISA +37 C (Sheet 2 of 2) CA
Figure 7-142. Time, Fuel, and Distance to Descend
Figure 7-143. Climb - Balked Landing IR
Figure 7-144. Normal Landing Distance - Flaps Down
LANDING DISTANCE - FLAPS UP
Figure 7-146. Landing Distance - One Engine Inoperative - Flaps Down
CHAPTER 8 NORMAL PROCEDURES Section I. MISSION PLANNING
Section II. OPERATING PROCEDURES AND MANEUVERS
Lighting and anti-ice/deice systems
INS Alignment Align as required
Flight director - TM-1-1510-223-10_477
RUDDER BOOST/YAW CONTROL TEST - TM-1-1510-223-10_478
ASE/ACS Programming
Flight plan
TACAN/DME indicator system
FUEL SAMPLE AND OIL CHECK. - TM-1-1510-223-10_482
Figure 8-1. Exterior Inspection - TM-1-1510-223-10_483
Left wing center section
Right wing center section - TM-1-1510-223-10_485
Fuselage Right Side. - TM-1-1510-223-10_486
Fuselage Left Side.
Copilots instrument panel
FIRST ENGINE START (BATTERY START).
ENGINE CLEARING PROCEDURE - TM-1-1510-223-10_490
SECOND ENGINE START (GPU START). - TM-1-1510-223-10_491
ENGINE RUNUP - TM-1-1510-223-10_492
Engine anti-ice - TM-1-1510-223-10_493
Pneumatics/vacuum/pressurization
CABIN CONTROLLER - TM-1-1510-223-10_495
AFTER TAKEOFF - TM-1-1510-223-10_496
CRUISE - TM-1-1510-223-10_497
LANDING. - TM-1-1510-223-10_498
BEFORE LEAVING AIRCRAFT - TM-1-1510-223-10_499
Section IV. FLIGHT CHARACTERISTICS
FLIGHT CONTROLS. - TM-1-1510-223-10_501
Figure 8-2. Stall Speeds - Power Idle - TM-1-1510-223-10_502
Section V. ADVERSE ENVIRONMENTAL CONDITIONS - TM-1-1510-223-10_503
DESERT OPERATION AND HOT WEATHER OPERATION.
ICE AND RAIN (TYPICAL). - TM-1-1510-223-10_505
ICING (SEVERE)
ICING (SEVERE)-cont.
Section V. CREW DUTIES
ARRIVAL BRIEFING.-cont.
CHAPTER 9 EMERGENCY PROCEDURES Section I. AIRCRAFT SYSTEMS
Figure 9-1. Emergency Exits and Equipment - TM-1-1510-223-10_511
ENGINE SHUTDOWN IN FLIGHT - TM-1-1510-223-10_512
ENGINE RESTART DURING FLIGHT (USING STARTER) - TM-1-1510-223-10_513
MAXIMUM GUIDE.
Figure 9-2. Maximum Glide Distance - TM-1-1510-223-10_515
TWO ENGINES INOPERATIVE/OFF AIRFIELD LANDING
PROPELLER FAILURE (OVER 1802 RPM) - TM-1-1510-223-10_517
FUEL SYSTEM - TM-1-1510-223-10_518
ELECTRICAL SYSTEM EMERGENCIES - TM-1-1510-223-10_519
FLIGHT CONTROL MALFUNCTIONS
LANDING EMERGENCIES - TM-1-1510-223-10_521
BAILOUT.
Figure 9-4. Wild Swell Ditch Heading Evaluation
Table 9-1. Ditching - TM-1-1510-223-10_524
APPENDIX A REFERENCES - TM-1-1510-223-10_525
APPENDIX A REFERENCES-cont.
APPENDIX B ABBREVIATIONS AND TERMS - TM-1-1510-223-10_527
METEOROLOGICAL TERMINOLOGY - TM-1-1510-223-10_528
GRAPH AND TABULAR TERMINOLOGY.
WEIGHT AND BALANCE TERMINOLOGY. - TM-1-1510-223-10_530
MISCELLANEOUS ABBREVIATIONS-cont. - TM-1-1510-223-10_531
MISCELLANEOUS ABBREVIATIONS-cont. - TM-1-1510-223-10_532
MISCELLANEOUS ABBREVIATIONS-cont. - TM-1-1510-223-10_533
MISCELLANEOUS ABBREVIATIONS-cont. - TM-1-1510-223-10_534
MISCELLANEOUS ABBREVIATIONS-cont. - TM-1-1510-223-10_535
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