TM-55-1510-222-10 Army Model RC-12H Aircraft Manual

CHAPTER 1 INTRODUCTION - TM-55-1510-222-10_10
1-11.  AIRCRAFT DESIGNATION SYSTEM
CHAPTER 2 AIRCRAFT AND SYSTEMS DESCRIPTION AND OPERATION - TM-55-1510-222-10_12
Figure 2-1. General Arrangement - Exterior Right Side (Sheet 1 of 5)
Figure 2-1. General Arrangement - Exterior Left Side (Sheet 2 of 5)
Figure 2-1. General Arrangement - Exterior Front (Sheet 3 of 5)
Figure 2-1. General Arrangement - Exterior Top (Sheet 4 of 5)
Figure 2-1. General Arrangement - Interior (Sheet 5 of 5)
Figure 2-2. Principal Dimensions
Figure 2-3. Ground Turning Radius
Figure 2-4. Exhaust Danger Area
Figure 2-5. Subpanels
a. Landing Gear Control Switch.
Figure 2-6. Overhead Circuit Breaker Panel
f. Landing   Gear   Warning   Horn   Test   Switch.
Figure 2-7. Cockpit
2-8. PARKING BRAKE - TM-55-1510-222-10_26
Figure 2-8. Cabin and Cargo Doors
(1) Opening the cargo door.
2-10.  WINDOWS.
Section II. EMERGENCY EQUIPMENT - TM-55-1510-222-10_30
Section III. ENGINES AND RELATED SYSTEMS - TM-55-1510-222-10_31
Figure 2-10. PT6A-67 Engine (Sheet 1 of 2)
Figure 2-10. PT6A-67 Engine (Sheet 2 of 2)
2-21. ENGINE FUEL CONTROL SYSTEM
Figure 2-11. Control Pedestal And Pedestal Extension
Figure 2-12. Engine Fire Detection/Extinguisher System
2-26. ENGINE FIRE EXTINGUISHER SYSTEM
2-27. OIL SUPPLY SYSTEM
Figure 2-13. Overhead Control Panel
2-30. ENGINE STARTER-GENERATORS
Figure 2-14. Instrument Panels (Sheet 1 of 2)
Figure 2-14. Instrument Panels (Sheet 2 of 2)
Section IV. FUEL SYSTEM - TM-55-1510-222-10_43
Figure 2-15. Fuel System Schematic
Figure 2-16. Fuel Management Panel
Figure 2-17. Crossfeed Fuel Flow
Figure 2-18. Gravity Feed Fuel Flow
Figure 2-19. Auxiliary Fuel Tank Mechanical Fuel Gage
2-33. FUEL SYSTEM MANAGEMENT
Section V. FLIGHT CONTROLS - TM-55-1510-222-10_50
Figure 2-20. Control Wheels
Figure 2-21. Controls Lock
2-40. WING FLAPS.
2-42. FEATHERING PROVISIONS.
2-44. LOW PITCH STOP.
2-49. PROPELLER REVERSING - TM-55-1510-222-10_56
2-52. SURFACE DEICING SYSTEM.
2-54. PROPELLER ELECTRIC DEICE SYSTEM.
2-56. STALL WARNING SYSTEM
2-58. FUEL SYSTEM ANTI-ICING - TM-55-1510-222-10_60
2-61. OXYGEN SYSTEM. - TM-55-1510-222-10_61
Figure 2-22. Oxygen System Schematic
Table 2-4. Oxygen Flow Planning Rates vs Altitude
Table 2-5. Oxygen Duration In Minutes (140 Cubic Foot System)
b.   Oxygen masks.
2-62. WINDSHIELD WIPERS.
Figure 2-23. Cylinder Capacity vs Pressure and Temperature
Figure 2-24. Environmental System
(1) Bleed air flow control unit.
2-69. AIR CONDITIONING SYSTEM.
2-70. UNPRESSURIZED VENTILATION.
a.   Heating Mode
Section IX. ELECTRICAL POWER SUPPLY AND DISTRIBUTION SYSTEM - TM-55-1510-222-10_73
Figure 2-25. DC Electrical System (Sheet 1 of 3)
Figure 2-25. DC Electrical System (Sheet 2 of 3)
Figure 2-25. DC Electrical System (Sheet 3 of 3)
Figure 2-26. Single Phase AC Electrical System
Figure 2-27. Three Phase AC Electrical System
Figure 2-28. Mission Equipment DC Power System
Figure 2-29. Mission AC/DC Power Cabinet
b. Generator Switches. The two switches
2-74. AC POWER SUPPLY.
Section X. LIGHTING - TM-55-1510-222-10_83
Figure 2-30. Exterior Lighting
b. Cabin Lighting.
Section XI. FLIGHT INSTRUMENTS - TM-55-1510-222-10_86
Figure 2-31. Pitot and Static System
Table 2-6. Warning Annunciator Panel Legend
Table 2-7. Caution/Advisory Annunciator Panel Legend (Sheet 2 of 2)
Table 2-8. Mission Control Panel Annunciator Legend
2-87. MISCELLANEOUS INSTRUMENTS.
Section XII. SERVICING, PARKING AND MOORING
Figure 2-32. Servicing Locations
Table 2-9. Approved Military Fuels, Oil, Fluids and Unit Capacities
Table 2-11. Standard, Alternate, and Emergency Fuels - TM-55-1510-222-10_95
2-91.  DRAINING MOISTURE FROM FUEL SYSTEM
2-95.  SERVICING THE HYDRAUL IC SYSTEM
Table 2-12. Recommended Fluid Dilution Chart
Figure 2-33. Oxygen System Servicing Pressure
2-102. GROUND HANDLING.
Figure 2-34. Parking, Covers, Ground Handling, and Towing Equipment
2-103. PARKING
2-105.   MOORING
Figure 2-36. Mooring the Aircraft
b. Mooring Procedures for High Winds
CHAPTER 3 AVIONICS - TM-55-1510-222-10_106
Section II. COMMUNICATIONS - TM-55-1510-222-10_107
Figure 3-1. Audio Control panel (Typical Pilot, Copilot)
3-7. UHF COMMAND SET
b. Controls and Functions
Figure 3-2. UHF Control Panel
3-9. BACK-UP   VOICE   ORDER    WIRE    (BU    VOW)
3-10.  VHF COMMUNICATIONS TRANSCEIVERS
Figure 3-3. VHF Control Panel
Figure 3-4. HF Control Panel
(3) Direct frequency tuning
3-12.  SINCGARS AN/ARC-201(V)
Figure 3-5. SINCGARS AN/ARC-201(V)
(3) PRESET Switch.
(6) Keyboard.
3-13.  EMERGENCY LOCATOR TRANSMITTER (ELT)
Figure 3-6. Emergency Locator Transmitter
Section III. NAVIGATION - TM-55-1510-222-10_123
Figure 3-7. Radio Magnetic Indicator
Figure 3-8. Pilot's Horizontal Situation Indicator
(13) Compass synchronization annunciator.
Figure 3-9. Copilot's Horizontal Situation Indicator
3-17.  PILOT'S    ATTITUDE    DIRECTOR    INDICATOR
Figure 3-10. Pilot's Attitude Director Indicator
3-18.  COPILOT'S GYRO HORIZON INDICATOR
Figure 3-11. Copilots Gyro Horizon Indicator (GH-14B)
Figure 3-12. Turn and Slip Indicator
Figure 3-13. Altitude Select Controller
3-23. VHF NAVIGATION RECEIVERS (VIR-32)
Figure 3-15. Navigation Receiver Control Unit
3-24. ADF RECEIVER (ADF-60).
Figure 3-16. ADF Control Unit (ADF-60)
Figure 3-17. TACAN Control Panel
Figure 3-18. TACAN Indicator
3-26. AUTOMATIC FLIGHT CONTROL SYSTEM
Figure 3-19. Flight Director Mode Selector (MS-400)
Figure 3-20. Flight Director Modes and Annunciators
(8) Pitch Hold Mode.
Figure 3-21. Autopilot Controller (PC-400)
Table 3-1. Autopilot System Limits (Sheet 1 of 2)
Table 3-1. Autopilot System Limits (Sheet 2 of 2)
3-27. INERTIAL NAVIGATION SYSTEM.
Figure 3-22. INS Mode Selector Unit
Figure 3-23. INS Control Display Unit
(12)     TO-FROM     display.
(1) Preflight Procedure.
(2) Insert present position
a.    Data selector L/L POS.
Table 3-2. Various Values For UTM Grid Coefficients
(5) To program destinations or TACAN coordinates
A load cycle
UTM data
14.    INSERT/ADVANCE    pushbutton
The normal geographic coordinates
(7) Designating fly-to destinations
(10)   Switching   from   aided   to   unaided   inertial operation.
Observe   drift   angle
(p)   Distance and time to waypoint other than next waypoint
If in aided TACAN operation
(u)   Magnetic heading
(b)   Extra precision geographic present position check and update
Extra precision values
Waypoint zero
(a)   Transient stops.
Table 3-3. Malfunction Code Check
Table 3-4. Malfunction Indications and Procedures
Table 3-6. INS Malfunction Codes
3-28. GLOBAL   POSITIONING   SYSTEM   (AN/ASN- 149 (B)3)
b. GPS Controls, Indicators, and Functions - TM-55-1510-222-10_174
3-23A. GPS Control/Display Unit (CDU)
3-23B. Observer Headset and GPS Key Panel
c. GPS System Modes of Operation - TM-55-1510-222-10_177
e. CHAALS Use of GPS and INS.
Section IV. RADAR AND TRANSPONDER - TM-55-1510-222-10_179
c. Weather Radar - Normal Operation.
Figure 3-24. Weather Radar Control-Indicator (AN/APN-215)
3-32. TRANSPONDER SET (APX-100)
Figure 3-25. Transponder Control Panel (AN/APX-100)
c. Transponder - Normal Operation - TM-55-1510-222-10_184
3-33. PILOT'S ALTIMETER INDICATOR
Figure 3-26. Pilots Altitude Indicator (BA-141)
3-34. COPILOT'S ENCODING ALTIMETER
Figure 3-27. Copilot's Encoding Altimeter (IDC 518)
CHAPTER 4 MISSION EQUIPMENT - TM-55-1510-222-10_189
Figure 4-1. Mission Control Panel - TM-55-1510-222-10_190
(7)   Dispenser control panel (DCP).
Figure 4-2. Flare Dispense Switch
Figure 4-3. Flare Dispenser Control Panel
11.  Perform the following operations
When the TEST SEQUENCE switch is turned to the START/HOME position
a. Ammunition Loading Procedure
4-7.RADAR    SIGNAL    DETECTING    SET    (AN/APR- 39(V)2)
Figure 4-4. Radar Signal Detecting Set Control Panel (AN/APR-39(V)1)
Figure 4-5. Radar Signal Detecting Set Control Panel (AN/APR-39(V)2)
Figure 4-7. Radar Warning Receiver Control Panel (AN/APR-44(V)3)
CHAPTER 5 OPERATING LIMITS AND RESTRICTIONS - TM-55-1510-222-10_201
Figure 5-1. Instrument Markings (Sheet 1 of 3) - TM-55-1510-222-10_202
Figure 5-1. Instrument Markings (Sheet 2 of 3) - TM-55-1510-222-10_203
Figure 5-1. Instrument Markings (Sheet 3 of 3) - TM-55-1510-222-10_204
5-10. FUEL SYSTEM LIMITS
Section III. POWER LIMITS - TM-55-1510-222-10_206
5-14. OVERTEMPERATURE AND OVERSPEED LIMITATIONS.
Section IV. LOADING LIMITS - TM-55-1510-222-10_208
Figure 5-2. Flight Envelope - TM-55-1510-222-10_209
Section VI. MANUEVERING LIMITS
5-32B.   ICING   LIMITATIONS   (SEVERE).
Section VIII. OTHER LIMITATIONS - TM-55-1510-222-10_213
Table 5-3. Required Equipment Listing (Sheet 1 of 4)
Table 5-3. Required Equipment Listing (Sheet 2 of 4)
Table 5-3. Required Equipment Listing (Sheet 3 of 4)
Table 5-3. Required Equipment Listing (Sheet 4 of 4)
CHAPTER 6 WEIGHT/BALANCE AND LOADING - TM-55-1510-222-10_218
Figure 6-1. Aircraft Compartments and Stations - TM-55-1510-222-10_219
LANDING GEAR DIMENSION
Table 6-2. Fuel Moments Table (Sheet 1 of 2)
Table 6-2. Fuel Moments Table (Sheet 2 of 2)
Table 6-3. Center of Gravity Limits Table (Sheet 1 of 3)
Table 6-3. Center of Gravity Limits Table (Sheet 2 of 3)
Table 6-3. Center of Gravity Limits Table (Sheet 3 of 3)
Section III.   FUEL/OIL
Figure 6-3. Density Variation of Aviation Fuel - TM-55-1510-222-10_227
Section VI. SURVIVABILITY EQUIPMENT - TM-55-1510-222-10_228
CHAPTER 7 PERFORMANCE - TM-55-1510-222-10_229
PERFORMANCE -cont
7-2. HOW TO USE GRAPHS.
b. Fahrenheit to Celsius Temperature Conversion.
. Minimum Static Takeoff Power (Flaps Approach).
(1)   Example 1 - Close-In Obstacle Clearance
Figure 7-1. Takeoff Path Profile
m.    Flight Planning Example.
EXAMPLE CRUISE TRUE AIRSPEEDS
(10) Zero Fuel Weight Limitation.
p. Enroute    Instrument    Corrections
Figure 7-2. Airspeed Calibration - Normal System - TM-55-1510-222-10_240
Figure 7-3. Airspeed Calibration - Normal System - TM-55-1510-222-10_241
Figure 7-4. Altimeter Correction - Normal System - TM-55-1510-222-10_242
Figure 7-5. Airspeed Calibration - Alternate System - TM-55-1510-222-10_243
Figure 7-6. Altimeter Correction - Alternate System - TM-55-1510-222-10_244
Figure 7-7. Indicated Outside Air Temperature Correction - TM-55-1510-222-10_245
Figure 7-8. ISA Conversion - TM-55-1510-222-10_246
Figure 7-9. Fahrenheit to Celsius Temperature Conversion - TM-55-1510-222-10_247
Figure 7-10. Minimum Static Take-Off Power at 1700 RPM - Flaps Up
Figure 7-11. Minimum Static Take-Off Power at 1700 RPM - Flaps Approach
Figure 7-12. Wind Components - TM-55-1510-222-10_250
Figure 7-13. Maximum Take-Off Weight - Flaps Up
Figure 7-14. Takeoff Speeds (KIAS) - Flaps Up
Figure 7-15. Take-Off Distance - Flaps Up
Figure 7-16. Accelerate-Stop - Flaps Up
Figure 7-17. Accelerate-Go - Flaps Up
Figure 7-18. Net Take-Off Flight Path - First Segment - Flaps Up
Figure 7-19. Net Take-Off Flight Path - Second Segment - Flaps Up
Figure 7-20. Horizontal Distance From Reference Zero To Third Segment Climb - Flaps Up
Figure 7-21. Close-In Take-Off Flight Path
DISTANT TAKE-OFF FLIGHT PATH - TM-55-1510-222-10_260
Figure 7-23. Maximum Take-Off Weight - Flaps Approach
Figure 7-24. Takeoff Speeds (KIAS) - Flaps Approach
Figure 7-25. Take-Off Distance - Flaps Approach
Figure 7-26. Accelerate-Stop - Flaps Approach
Figure 7-27. Accelerate-Go Distance - Flaps Approach
Figure 7-28. Net Take-Off Flight Path - First Segment - Flaps Approach
Figure 7-29. Net Take-Off Flight Path - Second Segment - Flaps Approach
Figure 7-30. Horizontal Distance from Reference Zero to Third Segment Climb - Flaps Approach
Figure 7-31. Net Takeoff Flight Path - Third Segment
Figure 7-32. Climb - Two Engines - Flaps Up
Figure 7-33. Climb - Two Engines - Flaps Approach
Figure 7-34. Climb - One Engine Inoperative
Figure 7-35. Service Ceiling - One Engine Inoperative
Figure 7-36. Time, Fuel, and Distance to Cruise Climb
Figure 7-37. Maximum Cruise Power - 1700 RPM - ISA -30C (Sheet 1 of 2)
Figure 7-37. Maximum Cruise Power - 1700 RPM - ISA -30C (Sheet 2 of 2)
Figure 7-38. Maximum Cruise Power - 1700 RPM - ISA -20C (Sheet 1 of 2)
Figure 7-38. Maximum Cruise Power - 1700 RPM - ISA -20C (Sheet 2 of 2)
Figure 7-39. Maximum Cruise Power - 1700 RPM - ISA -10C (Sheet 1 of 2)
Figure 7-39. Maximum Cruise Power - 1700 RPM - ISA -10C (Sheet 2 of 2)
Figure 7-40. Maximum Cruise Power - 1700 RPM - ISA (Sheet 1 of 2)
Figure 7-40. Maximum Cruise Power - 1700 RPM - ISA (Sheet 2 of 2)
Figure 7-41. Maximum Cruise Power - 1700 RPM - ISA +10C (Sheet 1 of 2)
Figure 7-41. Maximum Cruise Power - 1700 RPM - ISA +10C (Sheet 2 of 2)
Figure 7-42. Maximum Cruise Power - 1700 RPM - ISA +20C (Sheet I of 2)
Figure 7-42. Maximum Cruise Power - 1700 RPM - ISA +20C (Sheet 2 of 2)
Figure 7-43. Maximum Cruise Power - 1700 RPM - ISA +30C (Sheet 1 of 2)
Figure 7-43. Maximum Cruise Power - 1700 RPM - ISA t 30C (Sheet 2 of 2)
Figure 7-44. Maximum Cruise Power - 1700 RPM - ISA +37C (Sheet 1 of 2)
Figure 7-44. Maximum Cruise Power - 1700 RPM - ISA +37C (Sheet 2 of 2)
Figure 7-45. Maximum Cruise Speeds
Figure 7-46. Maximum Cruise Power
Figure 7-47. Fuel Flow at Maximum Cruise Power
Figure 7-48. Range Profile - Maximum Cruise Power
Figure 7-49. Normal Cruise Power - 1500RPM - ISA -30C (Sheet 1 of 2)
Figure 7-49. Normal Cruise Power - 1500 RPM - ISA -30C (Sheet 2 of 2)
Figure 7-50. Normal Cruise Power - 1500 RPM - ISA -20C (Sheet 1 of 2)
Figure 7-50. Normal Cruise Power - 1500 RPM - ISA -20C (Sheet 2 of 2)
Figure 7-51. Normal Cruise Power - 1500 RPM - ISA -10C (Sheet 1 of 2)
Figure 7-51. Normal Cruise Power - 1500 RPM - ISA -10C (Sheet 2 of 2)
Figure 7-52. Normal Cruise Power - 1500 RPM - ISA (Sheet 1 of 2)
Figure 7-52. Normal Cruise Power - 1500 RPM - ISA (Sheet 2 of 2)
Figure 7-53. Normal Cruise Power - 1500 RPM - ISA +10C (Sheet 1 of 2)
Figure 7-53. Normal Cruise Power - 1500 RPM - ISA +10C (Sheet 2 of 2)
Figure 7-54. Normal Cruise Power - 1500 RPM - ISA +20C (Sheet 1 of 2)
Figure 7-54. Normal Cruise Power - 1500 RPM - ISA +20C (Sheet 2 of 2)
Figure 7-55. Normal Cruise Power - 1500 RPM - ISA +30C (Sheet 1 of 2)
Figure 7-55. Normal Cruise Power - 1500 RPM - ISA +30C (Sheet 2 of 2)
Figure 7-56. Normal Cruise Power - 1500 RPM - ISA +37C (Sheet 1 of 2)
Figure 7-56. Normal Cruise Power - 1500 RPM - ISA +37C (Sheet 2 of 2)
Figure 7-57. Normal Cruise Speeds - 1500 RPM
Figure 7-58. Normal Cruise Power - 1500 RPM
Figure 7-59. Fuel Flow at Normal Cruise Power - 1500 RPM
Figure 7-60. Range Profile - Normal Cruise Power - 1500 RPM
Figure 7-61. Maximum Range Power - 1500 RPM - ISA -30C (Sheet 1 of 2)
Figure 7-61. Maximum Range Power - 1500 RPM - ISA -30C (Sheet 2 of 2)
Figure 7-62. Maximum Range Power - 1500 RPM - ISA -20C (Sheet 1 of 2)
Figure 7-62. Maximum Range Power - 1500 RPM - ISA -20C (Sheet 2 of 2)
Figure 7-63. Maximum Range Power - 1500 RPM - ISA -10C (Sheet 1 of 2)
Figure 7-63. Maximum Range Power - 1500 RPM - ISA -10C (Sheet 2 of 2)
Figure 7-64. Maximum Range Power - 1500 RPM - ISA (Sheet 1 of 2)
Figure 7-64. Maximum Range Power - 1500 RPM - ISA (Sheet 2 of 2)
Figure 7-65. Maximum Range Power - 1500 RPM - ISA + 10C (Sheet 1 of 2)
Figure 7-65. Maximum Range Power - 1500 RPM - ISA + 10C (Sheet 2 of 2)
Figure 7-66. Maximum Range Power - 1500 RPM - ISA + 20C (Sheet 1 of 2)
Figure .7-66.Maximum Range Power - 1500 RPM - ISA + 20C (Sheet 2 of 2)
Figure 7-67. Maximum Range Power - 1500 RPM - ISA + 30C (Sheet 1 of 2)
Figure 7-67. Maximum Range Power - 1500 RPM - ISA + 30C (Sheet 2 of 2)
Figure 7-68. Maximum Range Power - 1500 RPM - ISA + 37C (Sheet 1 of 2)
Figure 7-68. Maximum Range Power - 1500 RPM - ISA + 37C (Sheet 2 of 2)
Figure 7-69. Range Profile - Maximum Range Power - 1500 RPM
Figure 7-70. Loiter Power - 1700 RPM - ISA -30C (Sheet 1 of 2)
Figure 7-70. Loiter Power - 1700 RPM - ISA -30C (Sheet 2 of 2)
Figure 7-71. Loiter Power - 1700 RPM - ISA -20C (Sheet 1 of 2)
Figure 7-71. Loiter Power - 1700 RPM - ISA -20C (Sheet 2 of 2)
Figure 7-72. Loiter Power - 1700 RPM - ISA -10C (Sheet 1 of 2)
Figure 7-72. Loiter Power - 1700 RPM- ISA -10C (Sheet 2 of 2)
Figure 7-73. Loiter Power - 1700 RPM - ISA (Sheet 1 of 2)
Figure 7-73. Loiter Power - 1700 RPM - ISA (Sheet 2 of 2)
Figure 7-74. Loiter Power - 1700 RPM - ISA + 10OC (Sheet 1 of 2)
Figure 7-74. Loiter Power - 1700 RPM - ISA + 10C (Sheet 2 of 2)
Figure 7-75. Loiter Power - 1700 RPM - ISA + 20C (Sheet 1 of 2)
Figure 7-75. Loiter Power - 1700 RPM - ISA + 20C (Sheet 2 of 2)
Figure 7-76. Loiter Power - 1700 RPM - ISA + 30C (Sheet 1 of 2)
Figure 7-76. Loiter Power - 1700 RPM - ISA + 30C (Sheet 2 of 2)
Figure 7-77. Loiter Power - 1700 RPM - ISA + 37C (Sheet 1 of 2)
Figure 7-77. Loiter Power - 1700 RPM - ISA + 37C (Sheet 2 of 2)
Figure 7- 78. Endurance Profile - Loiter Power 1700 RPM
Figure 7-79. Range Profile - Full Main Tanks
Figure 7-80. Endurance Profile - Full Main Tanks
Figure 7-81. Range Profile - Full Main and Aux Tanks
Figure 7-82. Endurance Profile - Full Main and Aux Tanks
Figure 7-83. One-Engine-Inoperative Maximum Cruise Power - 1700 RPM - ISA -30C (Sheet 1 of 2)
Figure 7-83. One-Engine-Inoperative Maximum Cruise Power - 1700 RPM - ISA -30C (Sheet 2 of 2)
Figure 7-84. One-Engine-Inoperative Maximum Cruise Power - 1700 RPM - ISA -20C (Sheet 1 of 2)
Figure 7-84. One-Engine-Inoperative Maximum Cruise Power - 1700 RPM - ISA -200C (Sheet 2 of 2)
Figure 7-85. One-Engine-Inoperative Maximum Cruise Power - 1700 RPM - ISA -10C (Sheet 1 of 2)
Figure 7-85. One-Engine-Inoperative Maximum Cruise Power - 1700 RPM - ISA -10C (Sheet 2 of 2)
Figure 7-86. One-Engine-Inoperative Maximum Cruise Power - 1700 RPM - ISA (Sheet 1 of 2)
Figure 7-86. One-Engine-Inoperative Maximum Cruise Power - 1700 RPM - ISA (Sheet 2 of 2)
Figure 7-87. One-Engine-Inoperative Maximum Cruise Power - 1700 RPM - ISA + 1OC (Sheet 1 of 2)
Figure 7-87. One-Engine-Inoperative Maximum Cruise Power - 1700 RPM - ISA + 10C (Sheet 2 of 2)
Figure 7-88. One-Engine-Inoperative Maximum Cruise Power - 1700 RPM - ISA + 20C (Sheet 1 of 2)
Figure 7-88. One-Engine-Inoperative Maximum Cruise Power - 1700 RPM - ISA- + 20C (Sheet 2 of 2)
Figure 7-89. One-Engine-Inoperative Maximum Cruise Power - 1700 RPM - ISA + 30C (Sheet 1 of 2)
Figure 7-89. One-Engine-Inoperative Maximum Cruise Power - 1700 RPM - ISA + 30C (Sheet 2 of 2)
Figure 7-90. One-Engine-Inoperative Maximum Cruise Power - 1700 RPM - ISA + 37C (Sheet 1 of 2)
Figure 7-90. One-Engine-Inoperative Maximum Cruise Power - 1700 RPM - ISA + 37C (Sheet 2 of 2)
Figure 7-91. Time, Fuel, and Distance to Descend
Figure 7-92. Climb - Balked Landing
Figure 7-93. Normal Landing Distance Without Propeller Reversing - Flaps Down
Figure 7-94. Landing Distance Without Propeller Reversing - Flaps Up
Figure 7-95. Landing Distance - One Engine Inoperative - Flaps Down
CHAPTER 8 NORMAL PROCEDURES - TM-55-1510-222-10_374
Section II. OPERATING PROCEDURES AND MANEUVERS - TM-55-1510-222-10_375
8-10. FUEL SAMPLE
Figure 8-1. Exterior Inspection - TM-55-1510-222-10_377
A cold oil check
e. Fuselage Underside
i. Right Main Landing Gear
8-12.* INTERIOR CHECK
5. Magnetic compass
8-14.* FIRST ENGINE START (BATTERY START)
8-18.*FIRST ENGINE START (GPU START)
8-20.  BEFORE TAXIING
b. Autopilot - TM-55-1510-222-10_386
8-22. ENGINE RUNUP
8-23. *BEFORE TAKEOFF
8-25. TAKEOFF
8-27.  CLIMB
8-33.  TOUCH-AND GO/STOP-AND GO LANDING
Section III. INSTRUMENT FLIGHT
Section IV. FLIGHT CHARACTERISTICS
Figure 8-2. Stall Speeds -Power Idle
Section V. ADVERSE ENVIRONMENTAL CONDITIONS - TM-55-1510-222-10_395
8-53. DESERT OPERATION AND HOT WEATHER OPERATION
8-54 TURBULENCE AND THUNDERSTORM OPERATION
8-55. ICE AND RAIN (TYPICAL)
8-55A. ICING (SEVERE).
Section VI. CREW DUTIES
CHAPTER 9 EMERGENCY PROCEDURES - TM-55-1510-222-10_402
Figure 9-1. Emergency Exits and Equipment - TM-55-1510-222-10_403
9-7. ENGINE SHUTDOWN IN FLIGHT
9-9.   ENGINE   RESTART   DURING   FLIGHT   (USING STARTER)
9-11. MAXIMUM GLIDE
Figure 9-2. Maximum Glide Distance - TM-55-1510-222-10_407
9-19. DUCT OVERTEMPERATURE CAUTION ANNUNCIATOR ILLUMINATED
9-25. FIRE
9-26. FUEL SYSTEM
9-27. ELECTRICAL SYSTEM EMERGENCIES.
9-28. EMERGENCY DESCENT.
9-31. CRACKED WINDSHIELD
Figure 9-3. Ferry Chair Occupant Emergency Body Positions
Figure 9-4. Wind Swell Ditch Heading Evaluation - TM-55-1510-222-10_415
APPENDIX A REFERENCES - TM-55-1510-222-10_416
REFERENCES -cont - TM-55-1510-222-10_417
APPENDIX B ABBREVIATIONS AND TERMS - TM-55-1510-222-10_418
METEOROLOGICAL TERMINOLOGY - TM-55-1510-222-10_419
POWER TERMINOLOGY - TM-55-1510-222-10_420
GRAPH AND TABULAR TERMINOLOGY - TM-55-1510-222-10_421
WEIGHT AND BALANCE TERMINOLOGY. -cont

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