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CHAPTER 1 INTRODUCTION - TM-55-1510-220-10_15
1-1 1. AIRCRAFT DESIGNATION SYSTEM
CHAPTER 2 AIRCRAFT AND SYSTEMS DESCRIPTION AND OPERATION - TM-55-1510-220-10_17
Figure 2-1. General Exterior Arrangement (Sheet 1 of 6)
Figure 2-1. General Exterior Arrangement (Sheet 2 of 6)
Figure 2-1. General Exterior Arrangement (Sheet 3 of 6)
Figure 2-1. General Exterior Arrangement (Sheet 4 of 6)
Figure 2-1. General Exterior Arrangement (Sheet 5 of 6)
Figure 2-1. General Exterior Arrangement (Sheet 6 of 6)
Figure 2-2. General Interior Arrangement (Sheet 1 of 2)
Figure 2-2. General Interior Arrangement (Sheet 2 of 2)
Figure 2-3. Principal Dimensions - TM-55-1510-220-10_26
Figure 2-4. Ground Turning Radius - TM-55-1510-220-10_27
Figure 2-5. Exhaust and Propeller Danger Areas - TM-55-1510-220-10_28
Figure 2-6. Subpanels - TM-55-1510-220-10_29
Figure 2-7. Cockpit
Figure 2-8. Control Pedestal
Figure 2-9. Cabin and Cargo Doors
b. Cargo Door.
2-10. WINDOWS - TM-55-1510-220-10_34
Figure 2-10. Pilot and Copilot Seats
Section II. EMERGENCY EQUIPMENT - TM-55-1510-220-10_36
Section III. ENGINES AND RELATED SYSTEMS - TM-55-1510-220-10_37
Figure 2-11. PT6A-41 Engine (Sheet 1 of 2)
Figure 2-11. P76A-41 Engine (Sheet 2 of 2)
2-23. POWER LEVERS.
2-27. ENGINE FIRE EXTINGUISHER SYSTEM.
Figure 2-12. Overhead Control Panel - TM-55-1510-220-10_42
2-33. ENGINE INSTRUMENTS
Section IV. FUEL SYSTEMS
Table 2-2. Fuel Quantity Data - TM-55-1510-220-10_45
Figure 2-13. Fuel System Schematic
Figure 2-14. Fuel Management Panel
Figure 2-15. Crossfeed Fuel Flow - TM-55-1510-220-10_48
Figure 2-16. Gravity Feed Fuel Flow
Figure 2-17. Auxiliary Fuel Tank Mechanical Fuel Gage
Section V. FLIGHT CONTROLS - TM-55-1510-220-10_51
Figure 2-18. Control Wheels
2-40. FLIGHT CONTROLS LOCK
Figure 2-19. Control Locks
Section VI. PROPELLERS - TM-55-1510-220-10_55
2-45. PROPELLER GOVERNORS
2-49. PROPELLER REVERSING - TM-55-1510-220-10_57
Section VII. UTILITY SYSTEMS - TM-55-1510-220-10_58
2-53. ANTENNA DEICING SYSTEM
2-55. PITOT AND STALL WARNING HEAT SYSTEM.
2-58. FUEL SYSTEM ANTI-ICING.
2-60. PRESSURIZATION SYSTEM
2-61. OXYGEN SYSTEM. - TM-55-1510-220-10_63
Figure 2-20. Oxygen System Schematic
able 2-4. Oxygen Flow Planning Rates vs Altitude
Table 2-5. Oxygen Duration
Figure 2-21. Oxygen System Cylinder Capacity
2-62. WINDSHIELD WIPERS.
2-63. MISSION OPERATOR SEATS.
Section VIII. HEATING, VENTILATION, COOLING, AND ENVIRONMENTAL CONTROL SYSTEM
Figure 2-22. Environmental System
2-69. AIR CONDITIONING SYSTEM.
2-70. UNPRESSURIZED VENTILATION
2-71. ENVIRONMENTAL CONTROLS.
Section IX. ELECTRICAL POWER SUPPLY AND DISTRIBUTION SYSTEM - TM-55-1510-220-10_75
Figure 2-23. DC Electrical System (Sheet 1 of 3)
Figure 2-23. DC Electrical System (Sheet 2 of 3)
Figure 2-23. DC Electrical System (Sheet 3 of 3)
Figure 2-24. Single Phase AC Electrical System
Figure 2-25. Three Phase AC Electrical System
Figure 2-26. Mission Equipment DC Power System
b. Generator Switches.
Figure 2-27. Overhead Circuit Breaker Panel
Section X. LIGHTING - TM-55-1510-220-10_84
Figure 2-28. Exterior Lighting
2-76. INTERIOR LIGHTING
2-77. EMERGENCY LIGHTING
Section XI. FLIGHT INSTRUMENTS - TM-55-1510-220-10_88
Figure 2-29. Pitot and Static System
Figure 2-230. Instrument Panel (Sheet 1 of 2)
Figure 2-30. Instrument Panel (Sheet 2 of 2)
2-86. STANDBY MAGNETIC COMPASS
Table 2-6. Warning Annunciator Panel Legend - TM-55-1510-220-10_93
Table 2-7. Caution/Advisory Annunciator Panel Legend (sheet 1 of 2)
Table 2-7. Caution/Advisory Annunciator Panel Legend (sheet 2 of 2)
Table 2-8. Mission Control Panel Annunciator Legend - TM-55-1510-220-10_96
(3) Trip or flight timer.
Section XII. SERVICING, PARKING, AND MOORING - TM-55-1510-220-10_98
Table 2-10. Approved Fuels - TM-55-1510-220-10_99
Table 2-11. Standard, Alternate and Emergency Fuels
Figure 2-31. Servicing Locations
2-94. SERVICING OIL SYSTEM
2-97. SERVICING THE ELECTRIC TOILET
2-98. ANTI-ICING, DEICING AND DEFROSTING PROTECTION
Table 2-12. Recommended Fluid Dilution Chart
2-102. GROUND HANDLING
Figure 2-32. Oxygen System Servicing Pressure
Figure 2-33. Parking, Covers, Ground Handling, and Towing Equipment
2-103. PARKING
2-105. MOORING.
Figure 2-34. Mooring the Aircraft
9. Secure propellers
CHAPTER 3 AVIONICS - TM-55-1510-220-10_113
Section II. COMMUNICATIONS - TM-55-1510-220-10_114
Figure 3-1. Audio Control Panel (C-499) (Typical Pilot, Copilot) - TM-55-1510-220-10_115
e. Normal Operation
Figure 3-2. Marker Beacon Audio Control Panel
Figure 3-3. UHF Control Panel (AN/ARC-164)
c. Normal Operation. - TM-55-1510-220-10_119
(5) Transmitter operating procedure
3-10. VOICE ORDER WIRE (AN/ARC-164).
3-12. VHF AM-FM COMMAND SET (AN/ARC-186)
Figure 3-5. VHF AM-FM Control Panel ( AN/ARC-186)
(7) 0.025 MHz selector.
(1) Emergency AM Mode
Figure 3-6. TSEC/KY-58 Voice Security System
Figure 3-7. HF Control Panel (718 U-5)
3-15. VOICE SECURITY SYSTEM (TSEC/KY75).
Figure 3-8. Voice Security Control Panel (TSEC/KY-75)
c. TSEC/KY-75 Operating Procedures
3-16. EMERGENCY LOCATOR TRANSMITTER (ELT)
Figure 3-9. Emergency Locator Transmitter ( Narco 03716-0300)
Section III. NAVIGATION - TM-55-1510-220-10_133
Figure 3-11. Pilot's Horizontal Situation Indicator (331A-8G)
Figure 3-12. Copilot's Horizontal Situation Indicator (331A-8P).
(9) COURSE selector.
3-20. FLIGHT DIRECTOR INDICATOR.
Figure 3-13. Flight Director Indicator (329B-9A)
Figure 3-14. Pilot's Turn and Slip Indicator (329T-1)
Figure 3-15. Copilot's Gyro Horizon Indicator (GH-14)
Figure 3-16. VOR Control Panel (VIR-30AGM, VIR-30AG)
b. Controls/Indicators and Functions, NA V I1 Control Panel
(2) Localizer (LOC) operation
Figure 3-17. ADF Control Panel (DF-203)
d. ADF Normal Operation
Figure 3-18. Tacan Distance Indicator
Figure 3-19. Tacan Control Panel (AN-ARN-136)
e. Avionics TACAN Operation.
3-28. AUTOMATIC FLIGHT CONTROL SYSTEM
Figure 3-20. Autopilot Mode &elector Panel (614E-42A)
Figure 3-21. Aileron High Torque Test Switch and Annunciation
Figure 3-23. Autopilot Pitch-Turn Control Panel
(a) Heading mode.
i. Autopilot Operation
j. Before takeoff
o. Automatic Approach, Front Course
3-29. INERTIAL NAVIGATION SYSTEM
Figure 3-24. INS Mode Selector Unit (C-IV-E)
Figure 3-25. INS Control Display Unit (C-IV-E)
(3) Data display, left and right
d. INS Normal Operating Procedures
Passenger or cargo loading
Values for various spheroids
Table 3-1. Various Values for UTM Grid Coefficients - TM-55-1510-220-10_164
(4) Insert present position
(b) To insert geographic coordinates of aircraft present position
2. Thumbwheel
(b) Insertion of geographic waypoint coordinates - TM-55-1510-220-10_168
a) Insertion of UTM TACAN station data
The computer will convert coordinates in overlap area
(b) Insertion of geographic TACAN station data - TM-55-1510-220-10_171
Altitude inputs - TM-55-1510-220-10_172
(7). Designating fl-to destinations on TACAN
(11) Switching from aided to unaided inertial operation.
(n) Geographic present inertial position display
(q) Distance and time between any two waypoints
(s) Coordinates of any waypoint
(u) True heading.
(b) Extra precision geographic present position check and update
8. Load longitude by pressing keys
The extra precision values
(14) Flight course changes.
(a) Realignment INS operating
Table 3-2. Malfunction Code Check - TM-55-1510-220-10_184
(20) Malfunction indications and procedures
Table 3-3. Malfunction Indications and Procedures
Table 3-5. Malfunction Codes (Sheet I of 2)
Table 3-5. Malfunction Codes (Sheet 2 of 2)
b. GPS Controls, Indicators, and Functions - TM-55-1510-220-10_189
Figure 3-25A. GPS Control/Display Unit (CDU)
c. GPS System Modes of Operation - TM-55-1510-220-10_191
Figure 3-25B. GPS Key, Load, and Zeroize Panel
(b) GPS quick start.
Section IV. TRANSPONDER AND RADAR
Figure 3-26. Weather Radar Control-Indicator (AN/APN-215)
c. Weather Radar Normal Operation
3-31. TRANSPONDER SET (APX-100)
Figure 3-27. Transponder Control Panel (AN/APX-100)
c. Transponder Normal Operation
3-32. PILOTS ENCODING ALTIMETER
Figure 3-28. Pilot's Encoding Altimeter
CHAPTER 4 MISSION EQUIPMENT - TM-55-1510-220-10_202
Figure 4-1. Mission Control Panel - TM-55-1510-220-10_203
Figure 4-3. Flare and Chaff Dispenser Control Panel
(4) Flare dispenser switch.
4-4. SYSTEM DAILY PREFLIGHT/RE-ARM TEST - TM-55-1510-220-10_206
When the test set is installed on the dispenser assembly and 28 volts DC aircraft power has been applied
When the TEST SEQUENCE switch is turned to the START/HOME position
4-5. AMMUNITION.
b. Ammunition Unloading Procedure
Figure 4-5. Radar Signal Detecting Set Indicator - TM-55-1510-220-10_212
Figure 4-6. Radar Receiver Control Panel (AN/APR-44( ) (V3))
CHAPTER 5 OPERATING LIMITS AND RESTRICTIONS - TM-55-1510-220-10_214
Figure 5-1. Instrument Markings (Sheet 1 of 3) - TM-55-1510-220-10_215
Figure 5-1 Instrument Markings (Sheet 2 of 3)
Figure 5-1 Instrument Markings (Sheet 3 of 3)
5-10. FUEL SYSTEM LIMITS
Section III. POWER LIMITS - TM-55-1510-220-10_219
Table 5-1. Engine Operating Limitations - TM-55-1510-220-10_220
Section IV. LOADING LIMITS - TM-55-1510-220-10_221
Figure 5-2. Flight Envelope
SECTION VI. MANUEVERING LIMITS
5-30B. ICING LIMITATIONS (SEVERE).
5-34. CRACKED CABIN WINDOW/WINDSHIELD
Section VIII. OTHER LIMITATIONS - TM-55-1510-220-10_227
Section IX. REQUIRED EQUIPMENT FOR VARIOUS CONDITIONS OF FLIGHT - TM-55-1510-220-10_228
Figure 5-4. Required Equipment Listing (1 of 5)
Figure 5-4. Required Equipment Listing (2 of 5)
Figure 5-4. Required Equipment Listing (3 of 5)
Figure 5-4. Required Equipment Listing (4 of 5)
Figure 5-4. Required Equipment Listing (5 of 5)
CHAPTER 6 WEIGHT/BALANCE AND LOADING - TM-55-1510-220-10_234
Figure 6-2. Basic Weight and Balance Record DD Form 365-3 - TM-55-1510-220-10_235
Figure 6-2. Basic Weight and Balance Record DD Form 365-3 - TM-55-1510-220-10_236
Figure 6-3. Weight and Balance Clearance, DD Form 365-4
Table 6-1. Occupant Useful Load, Weights and Moments
Table 6-2. Fuel Center-of-Gravity Moments
Center of Gravity Moment Table - Moment/100 (Continued) - TM-55-1510-220-10_240
Center of Gravity Moment Table - Moment/100 (Continued) - TM-55-1510-220-10_241
Center of Gravity Moment Table - Moment/100 (Continued) - TM-55-1510-220-10_242
Center of Gravity Moment Table - Moment/100 (Continued) - TM-55-1510-220-10_243
Figure 6-4. Density Variation of Aviation Fuel
Section III. FUEL/OIL - TM-55-1510-220-10_245
CHAPTER 7 PERFORMANCE - TM-55-1510-220-10_246
7-3. Pressure Altitude
Figure 7-1. Takeoff Flight Path
CRUISE TRUE AIRSPEEDS AT FL 260
For flight planning
7-14. Zero Fuel Weight Limitation
7-17. PERFORMANCE AMENDMENTS FOR THE RC- 12G AIRCRAFT
Figure 7-2. Airspeed Calibration - Normal System - TM-55-1510-220-10_255
Figure 7-3. Altimeter Correction - Normal System
Figure 7-4. Airspeed Calibration - Alternate System
Figure 7-5. Altimeter Correction - Alternate System - TM-55-1510-220-10_258
Figure 7-6. Free Air Temperature Correction
Figure 7-7. ISA Conversion - TM-55-1510-220-10_260
Figure 7-8. Fahrenheit to Celsuis Temperature Conversion
Figure 7-9. Minimum Take-off Power at 2000RPM
Figure 7-10. Maximum Take-off Weight Permitted by Enroute Climb Requirement
Figure 7-11. Take-off Weight - Flaps 0%, to Achieve Positive One-Engine Climb
Figure 7-12. Takeoff Weight - Flaps 40%, to Achieve Positive One-Engine Climb
Figure 7-13. Wind Components
Figure 7-14. Takeoff Distance - Flaps 0%
Figure 7-15. Accelerate Stop - Flaps 0%
Figure 7-15A. Stopping Distance Factors
Figure 7-16. Accelerate - Go Distance Over 50-Ft Obstacle - Flaps 0%
Figure 7-17. Takeoff Climb Gradient - One-Engine-Inoperative - Flaps 0%
Figure 7-18. Takeoff Distance - Flaps 40%
Figure 7-19. Accelerate-Stop - Flaps 40%
Figure 7-20. Accelerate-Go Distance Over 50-Ft Obstacle - Flaps 40%
Figure 7-21. Takeoff Climb Gradient - One-Engine-Inoperative - Flaps 40%
Figure 7-22. Climb Two-Engine - Flaps 0%
Figure 7-23. Climb Two-Engine - Flaps 40%
Figure 7-24. Climb One-Engine Inoperative
Figure 7-25. Service Ceiling One-Engine-Inoperative
Figure 7-26. Time, Fuel, and Distance to Cruise Climb
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 7-27. 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 Power @ 1900 RPM
Figure 7-36. Maximum Cruise Speeds @ 1900 RPM
Figure 7-37. Fuel Flow at Maximum Cruise Power @ 1900 RPM - TM-55-1510-220-10_299
Figure 7-38. Range Profile - Maximum Cruise Power @ 1900 RPM
Figure 7-38A. Maximum Cruise Power @ 1700 RPM ISA -30C (Sheet 1 of 2)
Figure 7-38A. Maximum Cruise Power @ 1700 RPM ISA -30C (Sheet 2 of 2)
Figure 7-38b. Maximum Cruise Power @ 1700 RPM ISA -20C (Sheet 1 of 2)
Figure 7-38B. Maximum Cruise Power @ 1700 RPM ISA -20C (Sheet 2 of 2)
Figure 7-38C. Maximum Cruise Power @ 1700 RPM ISA -10C (Sheet 1 of 2)
Figure 7-38C. Maximum Cruise Power @ 1700 RPM ISA -10C (Sheet 2 of 2)
TM-55-1510-220-10_307
Figure 7-38D. Maximum Cruise Power @ 1700 RPM ISA (Sheet 2 of 2)
Figure 7-38E. Maximum Cruise Power @ 1700 RPM ISA +10C (Sheet 1 of 2)
Figure 7-38E. Maximum Cruise Power @ 1700 RPM ISA +10C (Sheet 2 of 2)
Figure 7-38F. Maximum Cruise Power @ 1700 RPM ISA +20C (Sheet 1 of 2)
Figure 7-38F. Maximum Cruise Power @ 1700 RPM ISA +20C (Sheet 2 of 2)
Figure 7-38G. Maximum Cruise Power @ 1700 RPM ISA +30C (Sheet 1 of 2)
Figure 7-38G. Maximum Cruise Power @ 1700 RPM ISA +30C (Sheet 2 of 2)
Figure 7-38H. Maximum Cruise Power @ 1700 RPM ISA +37C (Sheet 1 of 2)
Figure 7-38H. Maximum Cruise Power @ 1700 RPM ISA +37C (Sheet 2 of 2)
Figure 7-38I. Maximum Cruise Power
Figure 7-39. Maximum Range Power @ 1700 RPM ISA -30C (Sheet 1 of 2)
Figure 7-39. Maximum Range Power @ 1700 RPM ISA -30C (Sheet 2 of 2)
Figure 7-40. Maximum Range Power @ 1700 RPM ISA -20C (Sheet 1 of 2)
Figure 7-40. Maximum Range Power @ 1700 RPM ISA -20C (Sheet 2 of 2)
Figure 7-41. Maximum Range Power @ 1700 RPM ISA -10C (Sheet 1 of 2)
Figure 7-41. Maximum Range Power @ 1700 RPM ISA -10C (Sheet 2 of 2)
Figure 7-42. Maximum Range Power @ 1700 RPM ISA (Sheet 1 of 2)
Figure 7-42. Maximum Range Power @ 1700 RPM ISA (Sheet 2 of 2)
Figure 7-43. Maximum Range Power @ 1700 RPM ISA +10C (Sheet 1 of 2)
Figure 7-43. Maximum Range Power @ 1700 RPM ISA +10C (Sheet 2 of 2)
Figure 7-44. Maximum Range Power @ 1700 RPM ISA +20C (Sheet 1 of 2)
Figure 7-44. Maximum Range Power @ 1700 RPM ISA +20C (Sheet 2 of 2)
Figure 7-45. Maximum Range Power @ 1700 RPM ISA +30C (Sheet 1 of 2)
Figure 7-45. Maximum Range Power @ 1700 RPM ISA +30C (Sheet 2 of 2)
Figure 7-46. Maximum Range Power @ 1700 RPM ISA +37C (Sheet 1 of 2)
Figure 7-46. Maximum Range Power @ 1700 RPM ISA +37C (Sheet 2 of 2)
Figure 7-47. Maximum Endurance Power @ 1700 RPM ISA -30C (Sheet 1 of 2)
Figure 7-47. Maximum Endurance power @ 1700 RPM ISA - 30C (Sheet 2 of 2)
Figure 7-48. Maximum Endurance Power @ 1700 RPM ISA -20C (Sheet 1 of 2)
Figure 7-48. Maximum Endurance Power @ 1700 RPM ISA -20C (Sheet 2 of 2)
Figure 7-49. Maximum Endurance Power @ 1700 RPM ISA -10C (Sheet 1 of 2)
Figure 7-49. Maximum Endurance Power @ 1700 RPM ISA -10C (Sheet 2 of 2)
Figure 7-50. Maximum Endurance Power @ 1700 RPM ISA (Sheet 1 of 2)
Figure 7-50. Maximum Endurance Power @ 1700 (Sheet 2 of 2)
Figure 7-51. Maximum Endurance Power @ 1700 RPM ISA +10C (Sheet 1 of 2)
Figure 7-51. Maximum Endurance Power @ 1700 RPM ISA +10C (Sheet 2 of 2)
Figure 7-52. Maximum Endurance Power @ 1700 RPM ISA +20C (Sheet 1 of 2)
Figure 7-52. Maximum Endurance Power @ 1700 RPM ISA +20C (Sheet 2 of 2)
Figure 7-53. Maximum Endurance Power @ 1700 RPM ISA +30C (Sheet 1 of 2)
Figure 7-53. Maximum Endurance Power @ 1700 RPM ISA +30C (Sheet 2 of 2)
Figure 7-54. Maximum Endurance Power @ 1700 RPM ISA +37C (Sheet 1 of 2)
Figure 7-54. Maximum Endurance Power @ 1700 RPM ISA +37C (Sheet 2 of 2)
Figure 7-55. Range Profile - Long Range Power @ 1700 RPM
Figure 7-56. Range Profile - 542 Gallons Useable Fuel
Figure 7-57. Endurance Profile - 542 Gallons Useable Fuel
Figure 7-57A. One Engine-Inoperative Maximum Cruise Power 1900 RPM ISA -30C (Sheet 1 of 2)
Figure 7-57A. One Engine-Inoperative Maximum Cruise Power 1900 RPM ISA -30C (Sheet 2 of 2)
Figure 7-57B. One-Engine-Inoperative Maximum Cruise Power 1900 RPM ISA -20C (Sheet 1 of 2)
Figure 7-57B. One Engine-Inoperative Maximum Cruise Power 1900 RPM ISA -20C (Sheet 2 of 2)
Figure 7-57C. One Engine-Inoperative Maximum Cruise Power 1900 RPM ISA -10C (Sheet 1 of 2)
Figure 7-57C. One Engine-Inoperative Maximum Cruise Power 1900 RPM ISA -10C (Sheet 2 of 2)
Figure 7-57D. One Engine-Inoperative Maximum Cruise Power 1900 RPM ISA (Sheet 1 of 2)
Figure 7-57D. One Engine-Inoperative Maximum Cruise Power 1900 RPM ISA (Sheet 2 of 2)
Figure 7-57E. One Engine-Inoperative Maximum Cruise Power 1900 RPM ISA +10C (Sheet 1 of 2)
Figure 7-57E. One Engine-Inoperative Maximum Cruise Power 1900 RPM ISA +10C (Sheet 2 of 2)
Figure 7-57F. One Engine-Inoperative Maximum Cruise Power 1900 RPM ISA +20C (Sheet 1 of 2)
Figure 7-57F. One Engine-Inoperative Maximum Cruise Power 1900 RPM ISA +20C (Sheet 2 of 2)
Figure 7-57G. One Engine-Inoperative Maximum Cruise Power 1900 RPM ISA +30C (Sheet 1 of 2)
Figure 7-57G. One Engine-Inoperative Maximum Cruise Power 1900 RPM ISA +30C (Sheet 2 of 2)
Figure 7-57H. One Engine-Inoperative Maximum Cruise Power 1900 RPM ISA +37C (Sheet 1 of 2)
Figure 7-57H. One Engine-Inoperative Maximum Cruise Power 1900 RPM ISA +37C (Sheet 2 of 2)
Figure 7-58. Time, Fuel, and distance to Descend
Figure 7-59. Climb-Balked Landing
Figure 7-60. Normal Landing Without Propeller Reversing - Flaps 100%
Figure 7-61. Landing distance Without Propeller Reversing - Flaps 0%
Figure 7-62. Landing Distance With Propeller Reversing Flaps 0%
Figure 7-63. Landing Distance With Propeller Reversing Flaps 100%
CHAPTER 8 NORMAL PROCEDURES - TM-55-1510-220-10_375
Section II. OPERATING PROCEDURES AND MANEUVERS - TM-55-1510-220-10_376
Figure 8-1. Exterior Inspection - TM-55-1510-220-10_377
8-13. FUEL SAMPLE.
8-14. LEFT WING, AREA 1
8-17. CENTER SECTION, LEFT SIDE.
8-20. CENTER SECTION, RIGHT SIDE
8-23. RIGHT WING, AREA 3
8-27. * INTERIOR CHECK
8-28. BEFORE STARTING ENGINES
Alternate static source
8-29. * FIRST ENGINE START (BATTERY START)
8-31. ABORT START.
8-34. * SECOND ENGINE START (GPU START).
3. AC/DC power Check
8-36. * TAXIING
4. Overspeed governors Check
8-38. *BEFORE TAKEOFF.
8-41. AFTER TAKEOFF.
8-43. CRUISE.
8-44. DESCENT.
8-47. OBSTACLE CLEARANCE APPROACH AND MINIMUM RUN LANDING.
8-49. GO-AROUND
8-52. BEFORE LEAVING AIRCRAFT
Section III. INSTRUMENT FLIGHT - TM-55-1510-220-10_399
Section IV. FLIGHT CHARACTERISTICS - TM-55-1510-220-10_400
Figure 8-2. Stall Speed
8-63. DIVING.
Section V. ADVERSE ENVIRONMENTAL CONDITIONS - TM-55-1510-220-10_403
8-69. DESERT OPERATION AND HOT WEATHER OPERATION
8-70. TURBULENCE AND THUNDERSTORM OPERATION
8-71. ICE AND RAIN (TYPICAL)
8-71A. ICING (SEVERE).
Section VI. CREW DUTIES - TM-55-1510-220-10_409
8-74. ARRIVAL BRIEFING.
CHAPTER 9 EMERGENCY PROCEDURES - TM-55-1510-220-10_411
Figure 9-1. Emergency Exits and Equipment - TM-55-1510-220-10_412
b. Engine Malfunction During And After Takeoff.
f. Engine Malfunction During Final Approach.
k. Engine Restart During Flight (Not Using Starter).
Figure 9-2. Maximum Glide Distance
9-10. DUCT OVERTEMP CAUTION ANNUNCIATOR LIGHT ILLUMINATED.
9-13. LOSS OF PRESSURIZATION (ABOVE 10,000 FEET)
9-17. SINGLE-ENGINE LANDING CHECK.
Figure 2-12. Overhead Control Panel - TM-55-1510-220-10_420
9-21. FUEL SYSTEM
9-22. ELECTRICAL SYSTEM EMERGENCIES.
g. Battery Charge Caution Annunciator Light Illuminated.
9-23. EMERGENCY DESCENT.
d. Landing With Nose Gear Unsafe.
9-26. CRACKED WINDSHIELD.
Table 9-1. Ditching - TM-55-1510-220-10_427
Figure 9-4. Wind Swell Ditch Heading Evaluation - TM-55-1510-220-10_428
9-30. FLIGHT CONTROLS MALFUNCTION.
APPENDIX A REFERENCES - TM-55-1510-220-10_430
APPENDIX B ABBREVIATIONS AND TERMS - TM-55-1510-220-10_431
METEOROLOGICAL TERMINOLOGY - TM-55-1510-220-10_432
4. CONTROL AND INSTRUMENT TERMINOLOGY
6. WEIGHT AND BALANCE TERMINOLOGY.
7. MISCELLANEOUS ABBREVIATIONS
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