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Textron Bell 212 User Manual
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BHT-212-MM-1
5-00-00
Page 120
Rev. 14
26 JUN 2013
Export Classification C, ECCN EAR99
3.
Remove any hanger bearin
g from service where the
witness marks indicate th
at the grease shield has moved.
SPECIAL INSPECTIONS
5-21.
EACH 25 HOURS FOR THE NEXT FOUR INSPECTION
S (CONT)
DA
T
A
REFERENCE
INSPECTION T
ASK DESCRIPTION
INITIAL
MECH OTHER
142
144
Table of Contents
Default Chapter
16
Airworthiness Limitations Schedule
16
Mandatory Airworthiness Limitations Schedule
17
Inspections
24
Table of Contents
24
Figures List
26
General
28
Inspections - the Requirements
28
Chapter 5 - Inspections
29
Inspection Requirements
29
Crash Damage
29
Types of Inspections
29
Definitions
30
Inspection and Overhaul Tolerance
31
Scheduled Inspections
34
Daily Inspection
36
Data Reference
37
Daily Inspection - Part a
37
Chapter 4 100 Hours/12 Calendar Months Inspections
52
Date
52
Facility
52
Helicopter S/N
52
Registry no
52
Total Time
52
Signature
52
Each Listed Inspection Item or Maintenance Function Is to be
52
Overhaul Periods
53
Note
52
For Helicopters on the Part a Inspection Program
52
Initial Other
53
Fuselage Tailboom Attachment Inspection
73
Inspection of Beam Caps
74
1000 Hours Inspection
76
1000 Hours - Part a
76
3000 Hours/5 Years Inspection
78
25 Hours/30 Days Inspection
84
300 Hours Inspections
102
300 Hours - Part B
102
600 Hours/12 Months Inspections
114
3000 Hours/5 Years Inspections
122
Collective Stick Tube View
127
Daily Inspection
128
Special Inspection
128
Daily or each 10 Hours of Flight Operation, Whichever Occurs
128
First until 250 Hours
128
Torque Check Requirements
129
Daily Inspection (Special)
130
Inspection of Main Rotor Hub Grip Tangs, Barrel and Drag Brace Attachment Lugs
131
Daily/Each 10 Hours of Flight Operation, Whichever Occurs First
132
Spiral Bevel Gears Serial Numbers
134
Inspection of Spiral Bevel Gear
135
Between 5 and 10 Hours of Flight after each Installation
138
Fin Spar Cap Inspection Every 8 Hours
140
Each 25 Hours for the Next Four Inspections
142
Each 25 Hours of Flight Operation
144
Tail Rotor Blade - Detailed Inspection
151
Each 7 Days in a Corrosive Environment and each 30 Days in a
152
50 Hours after Installation of Components
154
Each 50 Hours of Component Operation
156
Each 100 Hours of Main Rotor Blade Operation - Deleted
158
Each 100 Hours/12 Months of Transmission Operation
160
Each 100 Hours/12 Months of Intermediate Gearbox Operation
162
Each 100 Hours/12 Months of Tail Rotor Gearbox Operation
164
Each 100 Hours/12 Months of Battery System Operation
166
100 Hours after Installation of Tailboom
168
Each 150 Hours of Starter Generator P/N 200SG119Q Operation
170
Fin Spar Cap Inspection Every 300 Hours
172
Each 300 Hours/12 Months of Transmission Operation
174
Each 300 Hours/3 Months of Driveshaft Operation
176
Each 300 Hours/12 Months Inspection of Tail Rotor Control Tube/Bearing
178
Main Rotor Grip Ultrasonic Inspection
180
Each 500 Hours/6 Months of Blade Service
182
Each 600 Hours of Transmission Operation
184
600 Hours/6 Months of Tail Rotor Driveshaft Coupling Operation
186
600 Hours/12 Months of Main Driveshaft Operation
188
Each 600 Hours/12 Months Inspection of Magnetic Brake Assembly
190
600 Hours/12 Months Inspection of Fire Extinguisher Discharge Tubes
192
Each 1000 Hours of Component Operation
194
First 1000 Hours of Component Time and each 3000 Hours
196
Each 1000 Hours/12 Months of Main Rotor Blade Operation
200
Each 1200 Hours/24 Months of Component Operation
202
5-7 Inspection of Main Rotor Hub Grip (1200 Hours/24 Months)
205
Every 12 Months/2500 Landings High Forward Crosstube Deflection Check
208
Every 12 Months/5000 Landings High Forward Crosstube Penetrant
210
Each 24 Months of Flight Control System Bolt Operation
212
Each 3000 Hours of Component Operation
216
10,000 Hour Total Airframe Time
222
Each 300 Hours/12 Months Main Beam Cap Operation
222
Conditional Inspections
224
After Hard Landing
226
After Blade Strike or Other Rotating System Torque Spike
232
After Overspeed
240
After Overtorque
244
After Engine Compression Stall or Surge
248
After Lightning Strikes
254
After Engine Combining Gearbox Clutch Nonengagement/In-Flight Slippage
262
Component Overhaul Schedule
266
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Textron Bell 212 Specifications
General
Brand
Textron
Model
Bell 212
Category
Toy
Language
English
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