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Textron Bell 212 - Page 25

Textron Bell 212
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BHT-212-MM-1
5-00-00
Page 2 Rev. 16 15 NOV 2018 Export Classification C, ECCN EAR99
TABLE OF CONTENTS (CONT)
Paragraph Chapter/Section Page
Number Title Number Number
5-35 Each 300 Hours/3 Months of Driveshaft Operation ....................... 5-00-00 151
5-35A Each 300 Hours/12 Months Inspection of Tail Rotor
Control Tube and Bearing.............................................................. 5-00-00 152A
5-36 Main Rotor Grip Ultrasonic Inspection. .......................................... 5-00-00 153
5-37 Each 500 Hours/6 Months of Blade Service .................................. 5-00-00 155
5-38 Each 600 Hours of Transmission Operation.................................. 5-00-00 157
5-39 600 Hours/6 Months of Tail Rotor Driveshaft Coupling
Operation ....................................................................................... 5-00-00 159
5-40 600 Hours/12 Months of Main Driveshaft Operation...................... 5-00-00 161
5-40A Each 600 Hours/12 Months Inspection of Magnetic Brake
Assembly ....................................................................................... 5-00-00 162A
5-40B Each 600 Hours/12 Months Inspection of Fire Extinguisher
Discharge Tubes............................................................................ 5-00-00 162C
5-41 Each 1000 Hours of Component Operation .................................. 5-00-00 163
5-42 First 1000 Hours of Component Time and Each 3000 Hours
Thereafter of Component Time...................................................... 5-00-00 165
5-43 Each 1000 Hours/12 Months of Main Rotor Blade Operation........ 5-00-00 169
5-44 Each 1200 Hours/24 Months of Component Operation................. 5-00-00 171
5-45 Each 1200 Hours of Main Rotor Hub Pin Operation — Deleted.... 5-00-00 175
5-45A Every 12 months/2500 Landings High Forward Crosstube
Deflection Check............................................................................ 5-00-00 176A
5-45B Every 12 months/5000 Landings High Forward Crosstube
Fluorescent Penetrant Inspection .................................................. 5-00-00 176C
5-46 Each 24 Months of Flight Control System Bolt Operation.............. 5-00-00 177
5-47 Each 3000 Hours of Component Operation................................... 5-00-00 181
5-48 10,000 Hour Total Airframe Time and Each 300 Hours/12 Months
Main Beam Cap Operation ............................................................ 5-00-00 187
CONDITIONAL INSPECTIONS
5-49 Condition Inspection ...................................................................... 5-00-00 189
5-50 After Hard Landing......................................................................... 5-00-00 191
5-51 After Blade Strike or Other Rotating System Torque Spike........... 5-00-00 197
5-52 After Overspeed............................................................................. 5-00-00 205
5-53 After Overtorque ............................................................................ 5-00-00 209
5-54 After Engine Compressor Stall or Surge........................................ 5-00-00 213
5-55 After Lightning Strikes.................................................................... 5-00-00 219
5-56 After Engine Combining Gearbox Clutch Nonengagement,
Misengagement, or In-flight Slippage ............................................ 5-00-00 227
COMPONENT OVERHAUL SCHEDULE
5-57 Component Overhaul Schedule..................................................... 5-00-00 231

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