CHAPTER 1 INTRODUCTION - TM-55-1510-219-10_10
1-11. AIRCRAFT DESIGNATION SYSTEM
CHAPTER 2 AIRCRAFT AND SYSTEMS DESCRIPTION AND OPERATION - TM-55-1510-219-10_12
Figure 2-1. General Exterior Arrangement (Sheet 1 of 7)
Figure 2-1. General Exterior Arrangement (Sheet 2 of 7)
Figure 2-1. General Exterior Arrangement (Sheet 3 of 7)
Figure 2-1. General Exterior Arrangement (Sheet 4 of 7)
Figure 2-1. General Exterior Arrangement (Sheet 5 of 7)
Figure 2-1. General Exterior Arrangement (Sheet 6 of 7)
Figure 2-1. General Exterior Arrangement (Sheet 7 of 7)
Figure 2-2. General Interior Arrangement
Figure 2-3. Principal Dimensions - TM-55-1510-219-10_21
Figure 2-4. Ground Turning Radius - TM-55-1510-219-10_22
Figure 2-5. Exhaust and Propeller Danger Areas - TM-55-1510-219-10_23
b. Landing Gear Down Position Indicator Lights.
Figure 2-6. Subpanels - TM-55-1510-219-10_25
f. Landing Gear Warning Horn Test Switch.
2-9. ENTRANCE AND EXIT PROVISIONS.
Figure 2-7. Cabin and Cargo Doors
(1) Opening cargo door.
2-11. WINDOWS.
Figure 2-9. Cockpit
Figure 2-10. PT6A-41 Engine (Sheet 1 of 2)
Figure 2-10. PT6A-41 Engine (Sheet 2 of 2)
Section III. ENGINES AND RELATED SYSTEMS - TM-55-1510-219-10_34
Figure 2-11. Pedestal
2-20. ENGINE ICE PROTECTION SYSTEMS.
2-22. POWER LEVERS
2-27. OIL SUPPLY SYSTEM.
2-30. ENGINE IGNITION SYSTEM.
Section IV. FUEL SYSTEM - TM-55-1510-219-10_40
Table 2-2. Fuel Quantity Data - TM-55-1510-219-10_41
Figure 2-12. Fuel System Schematic
Figure 2-13. Fuel Management Panel and Auxiliary Tank Mechanical Gage
Figure 2-14. Gravity Feed Fuel Flow
Figure 2-15. Crossfeed Fuel Flow - TM-55-1510-219-10_45
Table 2-3. Fuel Sump Drain Locations - TM-55-1510-219-10_46
Section V. FLIGHT CONTROLS - TM-55-1510-219-10_47
Figure 2-16. Control Wheels
2-41. TRIM TABS.
Figure 2-17. Control Locks
Section VI. PROPELLERS - TM-55-1510-219-10_51
2-45. PROPELLER GOVERNORS.
Section VII. UTILITY SYSTEMS - TM-55-1510-219-10_53
2-52. SURFACE DEICER SYSTEM.
2-54. PROPELLER ELECTROTHERMAL ANTI-ICE SYSTEM
2-56. PITOT AND STATIC SYSTEM.
2-58. FUEL SYSTEM ANTI-ICING - TM-55-1510-219-10_57
Figure 2-78. Overhead Control Panel
2-61. OXYGEN SYSTEM. - TM-55-1510-219-10_59
Figure 2-19. Oxygen System Schematic
Table 2-4. Oxygen Flow Planning Rates vs Altitude
(4) Oxygen supply pressure gage
Table 2-5. Oxygen Duration in Minutes 128 Cubic Foot System
Figure 2-20. Cylinder Capacity vs Pressure and Temperature
Section VIII. HEATING, VENTILATION, COOLING, AND ENVIRONMENTAL CONTROL SYSTEM - TM-55-1510-219-10_65
Figure 2-21. Environmental Systems
2-68. AIR CONDITIONING SYSTEM.
2-69. UNPRESSURIZED VENTILATION.
a. Heating Mode
Section IX. ELECTRICAL POWER SUPPLY AND DISTRIBUTION SYSTEM - TM-55-1510-219-10_70
Figure 2-22. DC Electrical System (Sheet 1 of 3)
Figure 2-22. DC Electrical System (Sheet 2 of 3)
Figure 2-22. DC Electrical System (Sheet 3 of 3)
Figure 2-23. Single Phase AC Electrical System - TM-55-1510-219-10_74
Figure 2-23. Single Phase AC Electrical System - TM-55-1510-219-10_75
Figure 2-25. Mission Equipment Power System
Figure 2-26. Overhead Circuit Breaker Panel
2-73. AC POWER SUPPLY.
Section X. LIGHTING - TM-55-1510-219-10_79
Figure 2-27. Exterior Lighting
2-76. EMERGENCY LIGHTING.
Section XI. FLIGHT INSTRUMENTS - TM-55-1510-219-10_82
2-85. MISCELLANEOUS INSTRUMENTS.
Figure 2-28. Instrument Panel (Sheet 1 of 2)
Figure 2-28. Instrument Panel (Sheet 2 of 2)
Table 2-6. Annunicator Panels
Annunicator Panels (Continued)
Section XII. SERVICING, PARKING, AND MOORING.
2-88. FILLING FUEL TANKS
Figure 2-29. Servicing Locations
Table 2-7. Fuel, Lubricants, Specifications and Capacities
Table 2-8. Approved Fuels (Continued)
2-95. SERVICING THE ELECTRIC TOILET.
2-96. ANTI-ICING, DEICING AND DEFROSTING PROTECTION.
Table 2-10. Recommended Fluid Dilution Chart
2-99. GROUND HANDLING
Figure 2-30. Oxygen System Servicing Pressure
Figure 2-31. Parking, Covers, Ground Handling, & Towing Equipment
2-100. INSTALLATION OF PROTECTIVE COVERS.
Figure 2-32. Mooring the Aircraft
2-102. PARKING
b. The control lock
CHAPTER 3 AVIONICS - TM-55-1510-219-10_103
Section II. COMMUNICATIONS - TM-55-1510-219-10_104
(3) Transmitter select switch
Figure 3-1. Audio Control Panel (C-499) (Typical pilot, copilot) - TM-55-1510-219-10_106
Figure 3-2. Radio Control Panel
Figure 3-3. UHF Control panel (AN/ARC- 164)
(5) Volume - Adjust.
3-10. VHF-AM COMMUNICATIONS (VHF-20B).
Figure 3-4. VHF-AM Control Panel (VHF-20B)
Figure 3-5. VHF AM/FM Control Panel (AN/ARC- 186)
c. Normal Operation
3-12. VOICE SECURITY SYSTEM TSEC/KY-28 (PROVISIONS ONLY)
Figure 3-6. Voice Security Control Indicator (C-8157/ARC) (KY-28)
b. Controls and Indicators.
Figure 3-7.HF Control Panel (718 U-5)
3-15. EMERGENCY LOCATOR TRANSMITTER (ELT)
Figure 3-8. Emergency Locator Transmitter (ELT-10)
Section III. NAVIGATION - TM-55-1510-219-10_120
3-18. HORIZONTAL SITUATION INDICATORS
b. Controls and Indicators - Pilot's HSI.
Figure 3-11. Copilot's Horizontal Situation Indicator (331A-6P)
3-19. HORIZON REFERENCE INDICATOR
Figure 3-12. Horizon Reference Indicator (329B-9A)
Figure 3-13. Pilot's Turn and Slip Indicator (329T- 1)
Figure 3-14. Copilot's Gyro Horizon Indicator (GH-14)
3-23. VOR/LOC NAVIGATION SYSTEM
Figure 3-15. Dual NAV 1 - NAV 2 Control Panel (VIR-30AGM, VIR-30AG)
c. Operation
3-24. MARKER BEACON
Figure 3-16. ADF Control Panel (DF-203)
3-26. TACAN SYSTEMS.
Figure 3-17. TACAN Control Panel and Range Indicator (ID-2218)
3-27. AUTOMATIC FLIGHT CONTROL SYSTEM.
b. Controls and Indicators.
Figure 3-18. Autopilot Mode Selector Panel (614E-42A)
Figure 3-20. Autopilot/Flight Director Annunciator Panel
(3) Pedestal extension.
(c) Navigation mode.
e. Autopilot Operation.
f. Takeoff and Climb Out.
h. Automatic Approach Front Course.
3-28. INERTIAL NAVIGATION SYSTEM.
Figure 3-22. Mode Selector Unit (C-IV-E)
Figure 3-23. INS Control Display Unit (C-IV-E)
The INS can provide test signals - TM-55-1510-219-10_147
c. INS - Normal Operating Procedures.
Passenger or cargo loading
2) (CDU) AUTO/MAN/TEST switch Press and hold
Table 3-1. Various Values for UTM Grid Coefficients - TM-55-1510-219-10_151
The INS can provide test signals - TM-55-1510-219-10_152
Extra precision values
(8) To insert magnetic variation. (Only if compass is not operational)
(b) Insertion of geographic waypoint coordinates - TM-55-1510-219-10_155
(a) Insertion of UTM TACAN station data
UTM data
(b) Insertion of geographic TACAN station data - TM-55-1510-219-10_158
Altitude inputs - TM-55-1510-219-10_159
(12) Designating fly-to-destinations or TACAN
(15) Switching from aided to unaided inertial. operation.
(n) Geographic present inertial position display
(r) Distance to any TACAN station
(t) TACAN station data
(17) INS updating.
(c) Extra precision geographic present position check and update
(d) UTM present position check and update
(18) Flight course changes.
(20) Transient stops.
Table 3-2. Malfunction Code Check - TM-55-1510-219-10_170
Table 3-3. Malfunction Indications and Procedures (Continued)
(e) To determine corrective action
Table 3-5. Malfunction Codes
3-29. WEATHER RADAR SET (AN/APN-215).
c. Normal Operation. - TM-55-1510-219-10_175
(3) Test procedure.
Figure 3-25. Transponder Control Panel (AN/APX - 100)
c. Transponder - Normal Operation - TM-55-1510-219-10_178
3-31. PILOT'S ENCODING ALTIMETER
Figure 3-26. Pilot's Encoding Altimeter
CHAPTER 4 MISSION EQUIPMENT - TM-55-1510-219-10_181
Figure 4-1. Mission Control Panel - TM-55-1510-219-10_182
Table 4-2. Mission Control Switches
Figure 4-2. Chaff/Flare Dispenser Control Panel
(8) Ammunition for dispenser.
4-4. SYSTEM DAILY PREFLIGHT/RE-ARM TEST - TM-55-1510-219-10_186
MANUAL SYSTEM RESET switch
When the test set is installed
4-5. AMMUNITION
Figure 4-3. Radar Signal Detecting Set Control Panel (AN/APR-39(V)1
Figure 4-4. Radar Signal Detecting Set Control Panel (AN/APR-39(V)2
Figure 4-5. Radar Signal Detecting Set Indicator - TM-55-1510-219-10_192
Section II. SYSTEM LIMITS
Figure 5-1. Instrument Markings (Sheet 1 of 3) - TM-55-1510-219-10_194
Figure 5-1. Instrument Markings (Sheet 2 of 3) - TM-55-1510-219-10_195
Figure 5-1. Instrument Markings (Sheet 3 of 3) - TM-55-1510-219-10_196
5-10. FUEL SYSTEM LIMITS.
Section III. POWER LIMITS - TM-55-1510-219-10_198
Section IV. LOADING LIMITS - TM-55-1510-219-10_199
Figure 5-2. Flight Envelope - TM-55-1510-219-10_200
Section VI. MANEUVERING LIMITS
SECTION VII. ENVIRONMENTAL RESTRICTIONS
5-31B. ICING LIMITATIONS (SEVERE)
Section VIII. OTHER LIMITATIONS - TM-55-1510-219-10_204
Table 5-3. Required Equipment Listing - TM-55-1510-219-10_205
Required Equipment Listing -cont - TM-55-1510-219-10_206
Required Equipment Listing -cont - TM-55-1510-219-10_207
Required Equipment Listing -cont - TM-55-1510-219-10_208
Required Equipment Listing -cont - TM-55-1510-219-10_209
CHAPTER 6 WEIGHT / BALANCE AND LOADING
Figure 6-1. Aircraft Compartments and Stations - TM-55-1510-219-10_211
Section II. WEIGHT AND BALANCE
Table 6-2. Fuel Moments
Table 6-3. Center of Gravity Moment Table - Moment / 100
Center of Gravity Moment Table - Moment / 100 (Continued) - TM-55-1510-219-10_215
Center of Gravity Moment Table - Moment / 100 (Continued) - TM-55-1510-219-10_216
Section III. FUEL/OIL - TM-55-1510-219-10_217
6-13. LOADING PROCEDURE
CHAPTER 7 PERFORMANCE - TM-55-1510-219-10_219
7-6. ACCELERATE-STOP (FLAPS 0%)
Figure 7-1. Accelerate-Go Flight Path
Cruise True Airspeeds At FI 220
7-10. RESERVE FUEL.
DISTANCE between the guide line above and the guide line below
Index of Figures
Index of Figures -cont - TM-55-1510-219-10_226
Index of Figures -cont - TM-55-1510-219-10_227
Figure 7-2. Airspeed Calibration - Normal System - TM-55-1510-219-10_228
Figure 7-3. Airspeed Calibration - Alternate System
Figure 7-4. Altimeter Correction - Normal System - TM-55-1510-219-10_230
Figure 7-5. Altimeter Correction - Alternate System - TM-55-1510-219-10_231
Figure 7-6. Indicated Outside Air temperature Correction
Figure 7-7. ISA Conversion - TM-55-1510-219-10_233
Figure 7-8. Fahrenheit to Celsius Temperature Conversion
Figure 7-9. Take-Off Weight - Flaps 0%, To Achieve Positive One-Engine Inoperative Climb at Lift-Off
Figure 7-10. Take-Off Weight - Flaps 40%, To Achieve Positive One-Engine Inoperative Climb at Lift-Off
Figure 7-11. Wind Components
Figure 7-12. Takeoff Distance - Flaps 0%
Figure 7-13. Take-Off Distance - Flaps 40%
Figure 7-14. Minimum Take-Off Power at 2000, RPM
Figure 7-15. Accelerate-Stop - Flaps 0%
Figure 7-16. Accelerate-Stop - Flaps 40
Figure 7-17. Accelerate-Go Distance Over 50-Ft Obstacle - Flaps 0%
Figure 7-18. Accelerate-Go Distance Over 50-Ft Obstacle - Flaps 40%
Figure 7-19. Time, Fuel, and Distance to Cruise Climb
Figure 7-20. Climb - Two Engines - Flaps 0%
Figure 7-21. Climb - Two Engines - Flaps 40%
Figure 7-22. Take-Off Climb Gradient - One-Engine Inoperative - Flaps 0%
Figure 7-23. Take-Off Climb Gradient - One-Engine Inoperative - Flaps 40%
Figure 7-24. Climb - One Engine Inoperative
Figure 7-25. Climb - Balked Landing
Figure 7-26. Service Ceiling - One Engine Inoperative
Figure 7-27. Maximum Cruise Power 1900 RPM, ISA -30C (Sheet 1 of 2)
Figure 7-27. Maximum Cruise Power 1900 RPM, ISA -30C (Sheet 2 of 2)
Figure 7-28. Maximum Cruise Power 1900 RPM, ISA -20C (Sheet 1 of 2)
Figure 7-28. Maximum Cruise Power 1900 RPM, ISA -20C (Sheet 2 of 2)
Figure 7-29. Maximum Cruise Power 1900 RPM, ISA - 10C (Sheet 1 of 2)
Figure 7-29. Maximum Cruise Power 1900 RPM, ISA -10C (Sheet 2 of 2)
Figure 7-30. Maximum Cruise Power 1900 RPM, ISA (Sheet 1 of 2)
Figure 7-30. Maximum Cruise Power 1900 RPM, ISA (Sheet 2 of 2)
Figure 7-31. Maximum Cruise Power 1900 RPM, ISA + 10C (Sheet 1 of 2)
Figure 7-31. Maximum Cruise Power 1900 RPM, ISA + 10C (Sheet 2 of 2)
Figure 7-32. Maximum Cruise Power 1900 RPM, ISA +20C (Sheet 1 of 2)
Figure 7-32. Maximum Cruise Power 1900 RPM, ISA +20C (Sheet 2 of 2)
Figure 7-33. Maximum Cruise Power 1900 RPM, ISA +30C (Sheet 1 of 2)
Figure 7-33. Maximum Cruise Power 1900 RPM, ISA +30C (Sheet 2 of 2)
Figure 7-34. Maximum Cruise Power 1900 RPM, ISA +37C (Sheet 1 of 2)
Figure 7-34. Maximum Cruise Power 1900 RPM, ISA +37C (Sheet 2 of 2)
Figure 7-35. Maximum Cruise Speeds @ 1900 RPM
Figure 7-36. Maximum Cruise Power @ 1900 RPM
Figure 7-37. Fuel Flow at Maximum Cruise Power @ 1900 RPM - TM-55-1510-219-10_271
Figure 7-38. Maximum Cruise Power One-Engine Inoperative 1900 RPM, ISA -30C (Sheet 1 of 2)
Figure 7-38. Maximum Cruise Power One-Engine Inoperative 1900 RPM, ISA -30C (Sheet 2 of 2)
Figure 7-39. Maximum Cruise Power One-Engine Inoperative 1900 RPM, ISA -20C (Sheet 1 of 2)
Figure 7-39. Maximum Cruise Power One-Engine Inoperative 1900 RPM, ISA -20C (Sheet 2 of 2)
Figure 7-40. Maximum Cruise Power One-Engine Inoperative 1900 RPM, ISA - -10C (Sheet 1 of 2)
Figure 7-40. Maximum Cruise Power One-Engine Inoperative 1900 RPM, ISA -10C (Sheet 2 of 2)
Figure 7-41. Maximum Cruise Power One-Engine Inoperative 1900 RPM, ISA (Sheet 1 of 2)
Figure 7-41. Maximum Cruise Power One-Engine Inoperative 1900 RPM, ISA (Sheet 2 of 2)
Figure 7-42. Maximum Cruise Power One-Engine Inoperative 1900 RPM, ISA + 10C (Sheet 1 of 2)
Figure 7-42. Maximum Cruise Power One-Engine Inoperative 1900 RPM, ISA + 10 C (Sheet 2 of 2)
Figure 7-43. Maximum Cruise Power One-Engine Inoperative 1900 RPM, ISA +20C (Sheet 1 of 2)
Figure 7-43. Maximum Cruise Power One-Engine Inoperative 1900 RPM, ISA +20C (Sheet 2 of 2)
Figure 7-44. Maximum Cruise Power One-Engine Inoperative 1900 RPM, ISA +30C (Sheet 1 of 2)
Figure 7-44. Maximum Cruise Power One-Engine Inoperative 1900 RPM, ISA +30C (Sheet 2 of 2)
Figure 7-45. Maximum Cruise Power One-Engine Inoperative 1900 RPM, ISA +37C (Sheet 1 of 2)
Figure 7-45. Maximum Cruise Power One-Engine Inoperative 1900 RPM, ISA +37C (Sheet 2 of 2)
Figure 7-46. Maximum Cruise Power 1700 RPM, ISA -30C (Sheet 1 of 2)
Figure 7-46. Maximum Cruise Power 1700 RPM, ISA -30C (Sheet 2 of 2)
Figure 7-47. Maximum Cruise Power 1700 RPM, ISA -20C (Sheet 1 of 2)
Figure 7-47. Maximum Cruise Power 1700 RPM, ISA -20C (Sheet 2 of 2)
Figure 7-48. Maximum Cruise Power 1700 RPM, ISA - 10C (Sheet 1 of 2)
Figure 7-48. Maximum Cruise Power 1700 RPM, ISA - 10C (Sheet 2 of 2)
Figure 7-49. Maximum Cruise Power 1700 RPM, ISA (Sheet 1 of 2)
Figure 7-49. Maximum Cruise Power 1700 RPM, ISA (Sheet 2 of 2)
Figure 7-50. Maximum Cruise Power 1700 RPM, ISA 10C (Sheet 1 of 2)
Figure 7-50. Maximum Cruise Power 1700 RPM, ISA + 10C (Sheet 2 of 2)
Figure 7-51. Maximum Cruise Power 1700 RPM, ISA +20C (Sheet 1 of 2)
Figure 7-51. Maximum Cruise Power 1700 RPM, ISA +20C (Sheet 2 of 2)
Figure 7-52. Maximum Cruise Power 1700 RPM, ISA +30C (Sheet 1 of 2)
Figure 7-52. Maximum Cruise Power 1700 RPM, ISA +30C (Sheet 2 of 2)
Figure 7-53. Maximum Cruise Power 1700 RPM, ISA +37C (Sheet 1 of 2)
Figure 7-53. Maximum Cruise Power 1700 RPM, ISA +37C (Sheet 2 of 2)
Figure 7-54. Maximum Cruise Power @ 1700 RPM
Figure 7-55. Maximum Range Power @ 1700 RPM, ISA-30C (Sheet 1 of 2)
Figure 7-55. Maximum Range Power @ 1700 RPM, ISA-30C (Sheet 2 of 2)
Figure 7-56. Maximum Range Power @ 1700 RPM, ISA-200C (Sheet 1 of 2)
Figure 7-56. Maximum Range Power @ 1700 RPM, ISA-20C (Sheet 2 of 2)
Figure 7-57. Maximum Range Power @ 1700 RPM, ISA-10C (Sheet 1 of 2)
Figure 7-57. Maximum Range Power @ 1700 RPM, ISA- 10C (Sheet 2 of 2)
Figure 7-58. Maximum Range Power @ 1700 RPM, ISA (Sheet 1 of 2)
Figure 7-58. Maximum Range Power @ 1700 RPM, ISA (Sheet 2 of 2)
Figure 7-59. Maximum Range Power @ 1700 RPM, ISA + 10C (Sheet 1 of 2)
Figure 7-59. Maximum Range Power @ 1700 RPM, ISA + 10C (Sheet 2 of 2)
Figure 7-60. Maximum Range Power @ 1700 RPM, ISA +20C (Sheet 1 of 2)
Figure 7-60. Maximum Range Power @ 1700 RPM, ISA +20C (Sheet 2 of 2)
Figure 7-61. Maximum Range Power @ 1700 RPM, ISA+30C (Sheet 1 of 2)
Figure 7-61. Maximum Range Power @ 1700 RPM, ISA +30 C (Sheet 2 of 2)
Figure 7-62. Maximum Range Power @ 1700 RPM, ISA +37C (Sheet 1 of 2)
Figure 7-62. Maximum Range Power @ 1700 RPM, ISA +37C (Sheet 2 of 2)
Figure 7-63. Maximum Endurance Power @ 1700 RPM, ISA-30C (Sheet 1 of 2)
Figure 7-63. Maximum Endurance Power @ 1700 RPM, ISA-30C (Sheet 2 of 2)
Figure 7-64. Maximum Endurance Power @ 1700 RPM, ISA-20C (Sheet 1 of 2)
Figure 7-64. Maximum Endurance Power @ 1700 RPM, ISA-20C (Sheet 2 of 2)
Figure 7-65. Maximum Endurance Power @ 1700 RPM, ISA-10C (Sheet 1 of 2)
Figure 7-65. Maximum Endurance Power @ 1700 RPM, ISA- 10C (Sheet 2 of 2)
Figure 7-66. Maximum Endurance Power @ 1700 RPM, ISA (Sheet 1 of 2)
Figure 7-66. Maximum Endurance Power @ 1700 RPM, ISA (Sheet 2 of 2)
Figure 7-67. Maximum Endurance Power @ 1700 RPM, ISA + 10C (Sheet 1 of 2)
Figure 7-67. Maximum Endurance Power @ 1700 RPM, ISA + 10C (Sheet 2 of 2)
Figure 7-68. Maximum Endurance Power @ 1700 RPM, ISA +20C (Sheet 1 of 2)
Figure 7-68. Maximum Endurance Power @ 1700 RPM, ISA +20 C (Sheet 2 of 2)
Figure 7-69. Maximum Endurance Power @ 1700 RPM, ISA +30C (Sheet 1 of 2)
Figure 7-69. Maximum Endurance Power @ 1700 RPM, ISA +30C (Sheet 2 of 2)
Figure 7-70. Maximum Endurance Power @ 1700 RPM, ISA +37C (Sheet I of 2)
Figure 7-70. Maximum Endurance Power @ 1700 RPM, ISA +37C (Sheet 2 of 2)
Figure 7-71. Range Profile-Maximum Cruise Power @ 1900 RPM
Figure 7-72. Range Profile-Maximum Range Power @ 1700 RPM
Figure 7-73. Range Profile-542 Gallons Usable Fuel
Figure 7-74. Endurance Proflie-542 Gallons Usable Fuel
Figure 7-75. Time, Fuel, and Distance to Descend
Figure 7-76. Landing Distance Without Propeller Reversing-Flaps 0%
Figure 7-77. Landing Distance Without Propeller Reversing-Flaps 100%
Figure 7-78. Landing Distance With Propeller Reversing-Flaps 0%
Figure 7-79. Landing Distance With Propeller Reversing-Flaps 100%
Figure 7-80. Stopping Distance Factors
CHAPTER 8 NORMAL PROCEDURES - TM-55-1510-219-10_347
Figure 8-1. Exterior Inspection - TM-55-1510-219-10_348
g. Flow indicator-Check
WAYPOINT SELECTION - TM-55-1510-219-10_350
19. Electric elevator trim and autopilot/flight director operation-Check
20. Avionics-Check
8-8. LEFT WING, AREA 1
8-11. CENTER SECTION, LEFT SIDE
8-14. RIGHT WING CENTER SECTION
8-17. RIGHT WING, AREA 3
8-20. FUSELAGE, LEFT SIDE, AREA 6
8-23. FIRST ENGINE START (BATTERY START).
8-24. SECOND ENGINE START (BATTERY START)
8-28. SECOND ENGINE START (GPU START).
8-31. ENGINE RUNUP.
8-32. BEFORE TAKEOFF
8-35. AFTER TAKEOFF
8-38. DESCENT
8-42. GO-AROUND.
Section III. INSTRUMENT FLIGHT - TM-55-1510-219-10_366
Section IV. FLIGHT CHARACTERISTICS - TM-55-1510-219-10_367
Figure 8-2. Stall Speeds
Section V. ADVERSE ENVIRONMENTAL CONDITIONS - TM-55-1510-219-10_369
8-55. DESERT OPERATION AND HOT WEATHER OPERATION.
8-56. TURBULENCE AND THUNDERSTORM OPERATION
8-57. ICE AND RAIN (TYPICAL)
8-57A. ICING (SEVERE).
Section VI. CREW DUTIES
8-59. DEPARTURE BRIEFING
CHAPTER 9 EMERGENCY PROCEDURES - TM-55-1510-219-10_376
Figure 9-1. Emergency Exits and Equipment - TM-55-1510-219-10_377
d. Engine Malfunction after Liftoff.
9-8. ENGINE SHUTDOWN IN FLIGHT.
9-9. ENGINE CLEANUP
9-13. LANDING WITH TWO ENGINES IN- OPERATIVE
Figure 9-2. Maximum Glide Distance - TM-55-1510-219-10_383
9-18. ENGINE BLEED AIR SYSTEM MALFUNCTION
9-22. SINGLE-ENGINE BEFORE LANDING
(2) Engine fire in flight (fire pull handle light illuminated)
9-27. FUEL SYSTEM.
9-28. ELECTRICAL SYSTEM EMERGENCIES.
9-29. EMERGENCY DESCENT.
9-30. LANDING EMERGENCIES.
9-31. CRACKED WINDSHIELD.
9-33. DITCHING
Table 9-1. Personnel Procedures During Ditching
Figure 9-3. Emergency Body Positions
APPENDIX A REFERENCES - TM-55-1510-219-10_396
APPENDIX B ABBREVIATIONS AND TERMS - TM-55-1510-219-10_397
METEOROLOGICAL TERMINOLOGY - TM-55-1510-219-10_398
CONTROL AND INSTRUMENT TERMINOLOGY.
WEIGHT AND BALANCE TERMINOLOGY. - TM-55-1510-219-10_400
MISCELLANEOUS ABBREVIATIONS - TM-55-1510-219-10_401
1-11. AIRCRAFT DESIGNATION SYSTEM
CHAPTER 2 AIRCRAFT AND SYSTEMS DESCRIPTION AND OPERATION - TM-55-1510-219-10_12
Figure 2-1. General Exterior Arrangement (Sheet 1 of 7)
Figure 2-1. General Exterior Arrangement (Sheet 2 of 7)
Figure 2-1. General Exterior Arrangement (Sheet 3 of 7)
Figure 2-1. General Exterior Arrangement (Sheet 4 of 7)
Figure 2-1. General Exterior Arrangement (Sheet 5 of 7)
Figure 2-1. General Exterior Arrangement (Sheet 6 of 7)
Figure 2-1. General Exterior Arrangement (Sheet 7 of 7)
Figure 2-2. General Interior Arrangement
Figure 2-3. Principal Dimensions - TM-55-1510-219-10_21
Figure 2-4. Ground Turning Radius - TM-55-1510-219-10_22
Figure 2-5. Exhaust and Propeller Danger Areas - TM-55-1510-219-10_23
b. Landing Gear Down Position Indicator Lights.
Figure 2-6. Subpanels - TM-55-1510-219-10_25
f. Landing Gear Warning Horn Test Switch.
2-9. ENTRANCE AND EXIT PROVISIONS.
Figure 2-7. Cabin and Cargo Doors
(1) Opening cargo door.
2-11. WINDOWS.
Figure 2-9. Cockpit
Figure 2-10. PT6A-41 Engine (Sheet 1 of 2)
Figure 2-10. PT6A-41 Engine (Sheet 2 of 2)
Section III. ENGINES AND RELATED SYSTEMS - TM-55-1510-219-10_34
Figure 2-11. Pedestal
2-20. ENGINE ICE PROTECTION SYSTEMS.
2-22. POWER LEVERS
2-27. OIL SUPPLY SYSTEM.
2-30. ENGINE IGNITION SYSTEM.
Section IV. FUEL SYSTEM - TM-55-1510-219-10_40
Table 2-2. Fuel Quantity Data - TM-55-1510-219-10_41
Figure 2-12. Fuel System Schematic
Figure 2-13. Fuel Management Panel and Auxiliary Tank Mechanical Gage
Figure 2-14. Gravity Feed Fuel Flow
Figure 2-15. Crossfeed Fuel Flow - TM-55-1510-219-10_45
Table 2-3. Fuel Sump Drain Locations - TM-55-1510-219-10_46
Section V. FLIGHT CONTROLS - TM-55-1510-219-10_47
Figure 2-16. Control Wheels
2-41. TRIM TABS.
Figure 2-17. Control Locks
Section VI. PROPELLERS - TM-55-1510-219-10_51
2-45. PROPELLER GOVERNORS.
Section VII. UTILITY SYSTEMS - TM-55-1510-219-10_53
2-52. SURFACE DEICER SYSTEM.
2-54. PROPELLER ELECTROTHERMAL ANTI-ICE SYSTEM
2-56. PITOT AND STATIC SYSTEM.
2-58. FUEL SYSTEM ANTI-ICING - TM-55-1510-219-10_57
Figure 2-78. Overhead Control Panel
2-61. OXYGEN SYSTEM. - TM-55-1510-219-10_59
Figure 2-19. Oxygen System Schematic
Table 2-4. Oxygen Flow Planning Rates vs Altitude
(4) Oxygen supply pressure gage
Table 2-5. Oxygen Duration in Minutes 128 Cubic Foot System
Figure 2-20. Cylinder Capacity vs Pressure and Temperature
Section VIII. HEATING, VENTILATION, COOLING, AND ENVIRONMENTAL CONTROL SYSTEM - TM-55-1510-219-10_65
Figure 2-21. Environmental Systems
2-68. AIR CONDITIONING SYSTEM.
2-69. UNPRESSURIZED VENTILATION.
a. Heating Mode
Section IX. ELECTRICAL POWER SUPPLY AND DISTRIBUTION SYSTEM - TM-55-1510-219-10_70
Figure 2-22. DC Electrical System (Sheet 1 of 3)
Figure 2-22. DC Electrical System (Sheet 2 of 3)
Figure 2-22. DC Electrical System (Sheet 3 of 3)
Figure 2-23. Single Phase AC Electrical System - TM-55-1510-219-10_74
Figure 2-23. Single Phase AC Electrical System - TM-55-1510-219-10_75
Figure 2-25. Mission Equipment Power System
Figure 2-26. Overhead Circuit Breaker Panel
2-73. AC POWER SUPPLY.
Section X. LIGHTING - TM-55-1510-219-10_79
Figure 2-27. Exterior Lighting
2-76. EMERGENCY LIGHTING.
Section XI. FLIGHT INSTRUMENTS - TM-55-1510-219-10_82
2-85. MISCELLANEOUS INSTRUMENTS.
Figure 2-28. Instrument Panel (Sheet 1 of 2)
Figure 2-28. Instrument Panel (Sheet 2 of 2)
Table 2-6. Annunicator Panels
Annunicator Panels (Continued)
Section XII. SERVICING, PARKING, AND MOORING.
2-88. FILLING FUEL TANKS
Figure 2-29. Servicing Locations
Table 2-7. Fuel, Lubricants, Specifications and Capacities
Table 2-8. Approved Fuels (Continued)
2-95. SERVICING THE ELECTRIC TOILET.
2-96. ANTI-ICING, DEICING AND DEFROSTING PROTECTION.
Table 2-10. Recommended Fluid Dilution Chart
2-99. GROUND HANDLING
Figure 2-30. Oxygen System Servicing Pressure
Figure 2-31. Parking, Covers, Ground Handling, & Towing Equipment
2-100. INSTALLATION OF PROTECTIVE COVERS.
Figure 2-32. Mooring the Aircraft
2-102. PARKING
b. The control lock
CHAPTER 3 AVIONICS - TM-55-1510-219-10_103
Section II. COMMUNICATIONS - TM-55-1510-219-10_104
(3) Transmitter select switch
Figure 3-1. Audio Control Panel (C-499) (Typical pilot, copilot) - TM-55-1510-219-10_106
Figure 3-2. Radio Control Panel
Figure 3-3. UHF Control panel (AN/ARC- 164)
(5) Volume - Adjust.
3-10. VHF-AM COMMUNICATIONS (VHF-20B).
Figure 3-4. VHF-AM Control Panel (VHF-20B)
Figure 3-5. VHF AM/FM Control Panel (AN/ARC- 186)
c. Normal Operation
3-12. VOICE SECURITY SYSTEM TSEC/KY-28 (PROVISIONS ONLY)
Figure 3-6. Voice Security Control Indicator (C-8157/ARC) (KY-28)
b. Controls and Indicators.
Figure 3-7.HF Control Panel (718 U-5)
3-15. EMERGENCY LOCATOR TRANSMITTER (ELT)
Figure 3-8. Emergency Locator Transmitter (ELT-10)
Section III. NAVIGATION - TM-55-1510-219-10_120
3-18. HORIZONTAL SITUATION INDICATORS
b. Controls and Indicators - Pilot's HSI.
Figure 3-11. Copilot's Horizontal Situation Indicator (331A-6P)
3-19. HORIZON REFERENCE INDICATOR
Figure 3-12. Horizon Reference Indicator (329B-9A)
Figure 3-13. Pilot's Turn and Slip Indicator (329T- 1)
Figure 3-14. Copilot's Gyro Horizon Indicator (GH-14)
3-23. VOR/LOC NAVIGATION SYSTEM
Figure 3-15. Dual NAV 1 - NAV 2 Control Panel (VIR-30AGM, VIR-30AG)
c. Operation
3-24. MARKER BEACON
Figure 3-16. ADF Control Panel (DF-203)
3-26. TACAN SYSTEMS.
Figure 3-17. TACAN Control Panel and Range Indicator (ID-2218)
3-27. AUTOMATIC FLIGHT CONTROL SYSTEM.
b. Controls and Indicators.
Figure 3-18. Autopilot Mode Selector Panel (614E-42A)
Figure 3-20. Autopilot/Flight Director Annunciator Panel
(3) Pedestal extension.
(c) Navigation mode.
e. Autopilot Operation.
f. Takeoff and Climb Out.
h. Automatic Approach Front Course.
3-28. INERTIAL NAVIGATION SYSTEM.
Figure 3-22. Mode Selector Unit (C-IV-E)
Figure 3-23. INS Control Display Unit (C-IV-E)
The INS can provide test signals - TM-55-1510-219-10_147
c. INS - Normal Operating Procedures.
Passenger or cargo loading
2) (CDU) AUTO/MAN/TEST switch Press and hold
Table 3-1. Various Values for UTM Grid Coefficients - TM-55-1510-219-10_151
The INS can provide test signals - TM-55-1510-219-10_152
Extra precision values
(8) To insert magnetic variation. (Only if compass is not operational)
(b) Insertion of geographic waypoint coordinates - TM-55-1510-219-10_155
(a) Insertion of UTM TACAN station data
UTM data
(b) Insertion of geographic TACAN station data - TM-55-1510-219-10_158
Altitude inputs - TM-55-1510-219-10_159
(12) Designating fly-to-destinations or TACAN
(15) Switching from aided to unaided inertial. operation.
(n) Geographic present inertial position display
(r) Distance to any TACAN station
(t) TACAN station data
(17) INS updating.
(c) Extra precision geographic present position check and update
(d) UTM present position check and update
(18) Flight course changes.
(20) Transient stops.
Table 3-2. Malfunction Code Check - TM-55-1510-219-10_170
Table 3-3. Malfunction Indications and Procedures (Continued)
(e) To determine corrective action
Table 3-5. Malfunction Codes
3-29. WEATHER RADAR SET (AN/APN-215).
c. Normal Operation. - TM-55-1510-219-10_175
(3) Test procedure.
Figure 3-25. Transponder Control Panel (AN/APX - 100)
c. Transponder - Normal Operation - TM-55-1510-219-10_178
3-31. PILOT'S ENCODING ALTIMETER
Figure 3-26. Pilot's Encoding Altimeter
CHAPTER 4 MISSION EQUIPMENT - TM-55-1510-219-10_181
Figure 4-1. Mission Control Panel - TM-55-1510-219-10_182
Table 4-2. Mission Control Switches
Figure 4-2. Chaff/Flare Dispenser Control Panel
(8) Ammunition for dispenser.
4-4. SYSTEM DAILY PREFLIGHT/RE-ARM TEST - TM-55-1510-219-10_186
MANUAL SYSTEM RESET switch
When the test set is installed
4-5. AMMUNITION
Figure 4-3. Radar Signal Detecting Set Control Panel (AN/APR-39(V)1
Figure 4-4. Radar Signal Detecting Set Control Panel (AN/APR-39(V)2
Figure 4-5. Radar Signal Detecting Set Indicator - TM-55-1510-219-10_192
Section II. SYSTEM LIMITS
Figure 5-1. Instrument Markings (Sheet 1 of 3) - TM-55-1510-219-10_194
Figure 5-1. Instrument Markings (Sheet 2 of 3) - TM-55-1510-219-10_195
Figure 5-1. Instrument Markings (Sheet 3 of 3) - TM-55-1510-219-10_196
5-10. FUEL SYSTEM LIMITS.
Section III. POWER LIMITS - TM-55-1510-219-10_198
Section IV. LOADING LIMITS - TM-55-1510-219-10_199
Figure 5-2. Flight Envelope - TM-55-1510-219-10_200
Section VI. MANEUVERING LIMITS
SECTION VII. ENVIRONMENTAL RESTRICTIONS
5-31B. ICING LIMITATIONS (SEVERE)
Section VIII. OTHER LIMITATIONS - TM-55-1510-219-10_204
Table 5-3. Required Equipment Listing - TM-55-1510-219-10_205
Required Equipment Listing -cont - TM-55-1510-219-10_206
Required Equipment Listing -cont - TM-55-1510-219-10_207
Required Equipment Listing -cont - TM-55-1510-219-10_208
Required Equipment Listing -cont - TM-55-1510-219-10_209
CHAPTER 6 WEIGHT / BALANCE AND LOADING
Figure 6-1. Aircraft Compartments and Stations - TM-55-1510-219-10_211
Section II. WEIGHT AND BALANCE
Table 6-2. Fuel Moments
Table 6-3. Center of Gravity Moment Table - Moment / 100
Center of Gravity Moment Table - Moment / 100 (Continued) - TM-55-1510-219-10_215
Center of Gravity Moment Table - Moment / 100 (Continued) - TM-55-1510-219-10_216
Section III. FUEL/OIL - TM-55-1510-219-10_217
6-13. LOADING PROCEDURE
CHAPTER 7 PERFORMANCE - TM-55-1510-219-10_219
7-6. ACCELERATE-STOP (FLAPS 0%)
Figure 7-1. Accelerate-Go Flight Path
Cruise True Airspeeds At FI 220
7-10. RESERVE FUEL.
DISTANCE between the guide line above and the guide line below
Index of Figures
Index of Figures -cont - TM-55-1510-219-10_226
Index of Figures -cont - TM-55-1510-219-10_227
Figure 7-2. Airspeed Calibration - Normal System - TM-55-1510-219-10_228
Figure 7-3. Airspeed Calibration - Alternate System
Figure 7-4. Altimeter Correction - Normal System - TM-55-1510-219-10_230
Figure 7-5. Altimeter Correction - Alternate System - TM-55-1510-219-10_231
Figure 7-6. Indicated Outside Air temperature Correction
Figure 7-7. ISA Conversion - TM-55-1510-219-10_233
Figure 7-8. Fahrenheit to Celsius Temperature Conversion
Figure 7-9. Take-Off Weight - Flaps 0%, To Achieve Positive One-Engine Inoperative Climb at Lift-Off
Figure 7-10. Take-Off Weight - Flaps 40%, To Achieve Positive One-Engine Inoperative Climb at Lift-Off
Figure 7-11. Wind Components
Figure 7-12. Takeoff Distance - Flaps 0%
Figure 7-13. Take-Off Distance - Flaps 40%
Figure 7-14. Minimum Take-Off Power at 2000, RPM
Figure 7-15. Accelerate-Stop - Flaps 0%
Figure 7-16. Accelerate-Stop - Flaps 40
Figure 7-17. Accelerate-Go Distance Over 50-Ft Obstacle - Flaps 0%
Figure 7-18. Accelerate-Go Distance Over 50-Ft Obstacle - Flaps 40%
Figure 7-19. Time, Fuel, and Distance to Cruise Climb
Figure 7-20. Climb - Two Engines - Flaps 0%
Figure 7-21. Climb - Two Engines - Flaps 40%
Figure 7-22. Take-Off Climb Gradient - One-Engine Inoperative - Flaps 0%
Figure 7-23. Take-Off Climb Gradient - One-Engine Inoperative - Flaps 40%
Figure 7-24. Climb - One Engine Inoperative
Figure 7-25. Climb - Balked Landing
Figure 7-26. Service Ceiling - One Engine Inoperative
Figure 7-27. Maximum Cruise Power 1900 RPM, ISA -30C (Sheet 1 of 2)
Figure 7-27. Maximum Cruise Power 1900 RPM, ISA -30C (Sheet 2 of 2)
Figure 7-28. Maximum Cruise Power 1900 RPM, ISA -20C (Sheet 1 of 2)
Figure 7-28. Maximum Cruise Power 1900 RPM, ISA -20C (Sheet 2 of 2)
Figure 7-29. Maximum Cruise Power 1900 RPM, ISA - 10C (Sheet 1 of 2)
Figure 7-29. Maximum Cruise Power 1900 RPM, ISA -10C (Sheet 2 of 2)
Figure 7-30. Maximum Cruise Power 1900 RPM, ISA (Sheet 1 of 2)
Figure 7-30. Maximum Cruise Power 1900 RPM, ISA (Sheet 2 of 2)
Figure 7-31. Maximum Cruise Power 1900 RPM, ISA + 10C (Sheet 1 of 2)
Figure 7-31. Maximum Cruise Power 1900 RPM, ISA + 10C (Sheet 2 of 2)
Figure 7-32. Maximum Cruise Power 1900 RPM, ISA +20C (Sheet 1 of 2)
Figure 7-32. Maximum Cruise Power 1900 RPM, ISA +20C (Sheet 2 of 2)
Figure 7-33. Maximum Cruise Power 1900 RPM, ISA +30C (Sheet 1 of 2)
Figure 7-33. Maximum Cruise Power 1900 RPM, ISA +30C (Sheet 2 of 2)
Figure 7-34. Maximum Cruise Power 1900 RPM, ISA +37C (Sheet 1 of 2)
Figure 7-34. Maximum Cruise Power 1900 RPM, ISA +37C (Sheet 2 of 2)
Figure 7-35. Maximum Cruise Speeds @ 1900 RPM
Figure 7-36. Maximum Cruise Power @ 1900 RPM
Figure 7-37. Fuel Flow at Maximum Cruise Power @ 1900 RPM - TM-55-1510-219-10_271
Figure 7-38. Maximum Cruise Power One-Engine Inoperative 1900 RPM, ISA -30C (Sheet 1 of 2)
Figure 7-38. Maximum Cruise Power One-Engine Inoperative 1900 RPM, ISA -30C (Sheet 2 of 2)
Figure 7-39. Maximum Cruise Power One-Engine Inoperative 1900 RPM, ISA -20C (Sheet 1 of 2)
Figure 7-39. Maximum Cruise Power One-Engine Inoperative 1900 RPM, ISA -20C (Sheet 2 of 2)
Figure 7-40. Maximum Cruise Power One-Engine Inoperative 1900 RPM, ISA - -10C (Sheet 1 of 2)
Figure 7-40. Maximum Cruise Power One-Engine Inoperative 1900 RPM, ISA -10C (Sheet 2 of 2)
Figure 7-41. Maximum Cruise Power One-Engine Inoperative 1900 RPM, ISA (Sheet 1 of 2)
Figure 7-41. Maximum Cruise Power One-Engine Inoperative 1900 RPM, ISA (Sheet 2 of 2)
Figure 7-42. Maximum Cruise Power One-Engine Inoperative 1900 RPM, ISA + 10C (Sheet 1 of 2)
Figure 7-42. Maximum Cruise Power One-Engine Inoperative 1900 RPM, ISA + 10 C (Sheet 2 of 2)
Figure 7-43. Maximum Cruise Power One-Engine Inoperative 1900 RPM, ISA +20C (Sheet 1 of 2)
Figure 7-43. Maximum Cruise Power One-Engine Inoperative 1900 RPM, ISA +20C (Sheet 2 of 2)
Figure 7-44. Maximum Cruise Power One-Engine Inoperative 1900 RPM, ISA +30C (Sheet 1 of 2)
Figure 7-44. Maximum Cruise Power One-Engine Inoperative 1900 RPM, ISA +30C (Sheet 2 of 2)
Figure 7-45. Maximum Cruise Power One-Engine Inoperative 1900 RPM, ISA +37C (Sheet 1 of 2)
Figure 7-45. Maximum Cruise Power One-Engine Inoperative 1900 RPM, ISA +37C (Sheet 2 of 2)
Figure 7-46. Maximum Cruise Power 1700 RPM, ISA -30C (Sheet 1 of 2)
Figure 7-46. Maximum Cruise Power 1700 RPM, ISA -30C (Sheet 2 of 2)
Figure 7-47. Maximum Cruise Power 1700 RPM, ISA -20C (Sheet 1 of 2)
Figure 7-47. Maximum Cruise Power 1700 RPM, ISA -20C (Sheet 2 of 2)
Figure 7-48. Maximum Cruise Power 1700 RPM, ISA - 10C (Sheet 1 of 2)
Figure 7-48. Maximum Cruise Power 1700 RPM, ISA - 10C (Sheet 2 of 2)
Figure 7-49. Maximum Cruise Power 1700 RPM, ISA (Sheet 1 of 2)
Figure 7-49. Maximum Cruise Power 1700 RPM, ISA (Sheet 2 of 2)
Figure 7-50. Maximum Cruise Power 1700 RPM, ISA 10C (Sheet 1 of 2)
Figure 7-50. Maximum Cruise Power 1700 RPM, ISA + 10C (Sheet 2 of 2)
Figure 7-51. Maximum Cruise Power 1700 RPM, ISA +20C (Sheet 1 of 2)
Figure 7-51. Maximum Cruise Power 1700 RPM, ISA +20C (Sheet 2 of 2)
Figure 7-52. Maximum Cruise Power 1700 RPM, ISA +30C (Sheet 1 of 2)
Figure 7-52. Maximum Cruise Power 1700 RPM, ISA +30C (Sheet 2 of 2)
Figure 7-53. Maximum Cruise Power 1700 RPM, ISA +37C (Sheet 1 of 2)
Figure 7-53. Maximum Cruise Power 1700 RPM, ISA +37C (Sheet 2 of 2)
Figure 7-54. Maximum Cruise Power @ 1700 RPM
Figure 7-55. Maximum Range Power @ 1700 RPM, ISA-30C (Sheet 1 of 2)
Figure 7-55. Maximum Range Power @ 1700 RPM, ISA-30C (Sheet 2 of 2)
Figure 7-56. Maximum Range Power @ 1700 RPM, ISA-200C (Sheet 1 of 2)
Figure 7-56. Maximum Range Power @ 1700 RPM, ISA-20C (Sheet 2 of 2)
Figure 7-57. Maximum Range Power @ 1700 RPM, ISA-10C (Sheet 1 of 2)
Figure 7-57. Maximum Range Power @ 1700 RPM, ISA- 10C (Sheet 2 of 2)
Figure 7-58. Maximum Range Power @ 1700 RPM, ISA (Sheet 1 of 2)
Figure 7-58. Maximum Range Power @ 1700 RPM, ISA (Sheet 2 of 2)
Figure 7-59. Maximum Range Power @ 1700 RPM, ISA + 10C (Sheet 1 of 2)
Figure 7-59. Maximum Range Power @ 1700 RPM, ISA + 10C (Sheet 2 of 2)
Figure 7-60. Maximum Range Power @ 1700 RPM, ISA +20C (Sheet 1 of 2)
Figure 7-60. Maximum Range Power @ 1700 RPM, ISA +20C (Sheet 2 of 2)
Figure 7-61. Maximum Range Power @ 1700 RPM, ISA+30C (Sheet 1 of 2)
Figure 7-61. Maximum Range Power @ 1700 RPM, ISA +30 C (Sheet 2 of 2)
Figure 7-62. Maximum Range Power @ 1700 RPM, ISA +37C (Sheet 1 of 2)
Figure 7-62. Maximum Range Power @ 1700 RPM, ISA +37C (Sheet 2 of 2)
Figure 7-63. Maximum Endurance Power @ 1700 RPM, ISA-30C (Sheet 1 of 2)
Figure 7-63. Maximum Endurance Power @ 1700 RPM, ISA-30C (Sheet 2 of 2)
Figure 7-64. Maximum Endurance Power @ 1700 RPM, ISA-20C (Sheet 1 of 2)
Figure 7-64. Maximum Endurance Power @ 1700 RPM, ISA-20C (Sheet 2 of 2)
Figure 7-65. Maximum Endurance Power @ 1700 RPM, ISA-10C (Sheet 1 of 2)
Figure 7-65. Maximum Endurance Power @ 1700 RPM, ISA- 10C (Sheet 2 of 2)
Figure 7-66. Maximum Endurance Power @ 1700 RPM, ISA (Sheet 1 of 2)
Figure 7-66. Maximum Endurance Power @ 1700 RPM, ISA (Sheet 2 of 2)
Figure 7-67. Maximum Endurance Power @ 1700 RPM, ISA + 10C (Sheet 1 of 2)
Figure 7-67. Maximum Endurance Power @ 1700 RPM, ISA + 10C (Sheet 2 of 2)
Figure 7-68. Maximum Endurance Power @ 1700 RPM, ISA +20C (Sheet 1 of 2)
Figure 7-68. Maximum Endurance Power @ 1700 RPM, ISA +20 C (Sheet 2 of 2)
Figure 7-69. Maximum Endurance Power @ 1700 RPM, ISA +30C (Sheet 1 of 2)
Figure 7-69. Maximum Endurance Power @ 1700 RPM, ISA +30C (Sheet 2 of 2)
Figure 7-70. Maximum Endurance Power @ 1700 RPM, ISA +37C (Sheet I of 2)
Figure 7-70. Maximum Endurance Power @ 1700 RPM, ISA +37C (Sheet 2 of 2)
Figure 7-71. Range Profile-Maximum Cruise Power @ 1900 RPM
Figure 7-72. Range Profile-Maximum Range Power @ 1700 RPM
Figure 7-73. Range Profile-542 Gallons Usable Fuel
Figure 7-74. Endurance Proflie-542 Gallons Usable Fuel
Figure 7-75. Time, Fuel, and Distance to Descend
Figure 7-76. Landing Distance Without Propeller Reversing-Flaps 0%
Figure 7-77. Landing Distance Without Propeller Reversing-Flaps 100%
Figure 7-78. Landing Distance With Propeller Reversing-Flaps 0%
Figure 7-79. Landing Distance With Propeller Reversing-Flaps 100%
Figure 7-80. Stopping Distance Factors
CHAPTER 8 NORMAL PROCEDURES - TM-55-1510-219-10_347
Figure 8-1. Exterior Inspection - TM-55-1510-219-10_348
g. Flow indicator-Check
WAYPOINT SELECTION - TM-55-1510-219-10_350
19. Electric elevator trim and autopilot/flight director operation-Check
20. Avionics-Check
8-8. LEFT WING, AREA 1
8-11. CENTER SECTION, LEFT SIDE
8-14. RIGHT WING CENTER SECTION
8-17. RIGHT WING, AREA 3
8-20. FUSELAGE, LEFT SIDE, AREA 6
8-23. FIRST ENGINE START (BATTERY START).
8-24. SECOND ENGINE START (BATTERY START)
8-28. SECOND ENGINE START (GPU START).
8-31. ENGINE RUNUP.
8-32. BEFORE TAKEOFF
8-35. AFTER TAKEOFF
8-38. DESCENT
8-42. GO-AROUND.
Section III. INSTRUMENT FLIGHT - TM-55-1510-219-10_366
Section IV. FLIGHT CHARACTERISTICS - TM-55-1510-219-10_367
Figure 8-2. Stall Speeds
Section V. ADVERSE ENVIRONMENTAL CONDITIONS - TM-55-1510-219-10_369
8-55. DESERT OPERATION AND HOT WEATHER OPERATION.
8-56. TURBULENCE AND THUNDERSTORM OPERATION
8-57. ICE AND RAIN (TYPICAL)
8-57A. ICING (SEVERE).
Section VI. CREW DUTIES
8-59. DEPARTURE BRIEFING
CHAPTER 9 EMERGENCY PROCEDURES - TM-55-1510-219-10_376
Figure 9-1. Emergency Exits and Equipment - TM-55-1510-219-10_377
d. Engine Malfunction after Liftoff.
9-8. ENGINE SHUTDOWN IN FLIGHT.
9-9. ENGINE CLEANUP
9-13. LANDING WITH TWO ENGINES IN- OPERATIVE
Figure 9-2. Maximum Glide Distance - TM-55-1510-219-10_383
9-18. ENGINE BLEED AIR SYSTEM MALFUNCTION
9-22. SINGLE-ENGINE BEFORE LANDING
(2) Engine fire in flight (fire pull handle light illuminated)
9-27. FUEL SYSTEM.
9-28. ELECTRICAL SYSTEM EMERGENCIES.
9-29. EMERGENCY DESCENT.
9-30. LANDING EMERGENCIES.
9-31. CRACKED WINDSHIELD.
9-33. DITCHING
Table 9-1. Personnel Procedures During Ditching
Figure 9-3. Emergency Body Positions
APPENDIX A REFERENCES - TM-55-1510-219-10_396
APPENDIX B ABBREVIATIONS AND TERMS - TM-55-1510-219-10_397
METEOROLOGICAL TERMINOLOGY - TM-55-1510-219-10_398
CONTROL AND INSTRUMENT TERMINOLOGY.
WEIGHT AND BALANCE TERMINOLOGY. - TM-55-1510-219-10_400
MISCELLANEOUS ABBREVIATIONS - TM-55-1510-219-10_401
