-------------------------------------------------------------------------------
| DAMAGE | LIMITATION | ACTION | |-----------------------------------------------------------------------------| | | (e.g. zigzag fashion) | the aircraft. | | | | | | DEFORMATION | 2. Undulation of the tread surface | 2. Keep the tire on | | | (e.g. waved surface) | the aircraft. | | | | | | | 3. Blisters | 3. Remove the tire. | | | | | | | 4. Bulges | 4. Remove the tire. | -------------------------------------------------------------------------------
(3) Sidewalls
 -------------------------------------------------------------------------------| DAMAGE | LIMITATION | ACTION | |-----------------------------------------------------------------------------| | | Radial and bias tires | | | | 1. Radial cuts | | | | (Deviation from radial direction| | | | is less than 30 deg.) | | | | | | | | depth less than 2 mm and do not | | | | go as far as the carcass and: | | | | length less than 150 mm | Keep the tire on the | | | | aircraft. | | | | | | CRACKS | length more than or equal to 150 mm| Remove the tire. | | OR | | | | SPLITS | depth more than or equal to 2 mm | Remove the tire. | | | or go as far as the carcass. | | | | | | | | 2. Inclined cuts | Keep the tire on the | | | (Deviation from radial | aircraft. | | | direction is more than 30 deg.)| | | | | | | | Do not go as far as the carcass | | | | and : | | | | length less than 150 mm | Keep the tire on the | | | | aircraft. | | | length more than or equal to 150 mm| Remove the tire. | | | | | | | Go as far as the carcass | Remove the tire. | |---------------|------------------------------------|------------------------| | FABRIC | Radial and bias tires | Remove the tire. | | SEPARATION | | |
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 -------------------------------------------------------------------------------| DAMAGE | LIMITATION | ACTION | |-----------------------------------------------------------------------------| |---------------|------------------------------------|----------------------- | | BLISTERS OR | Radial and bias tires | Remove the tire. | | BULGES | | | -------------------------------------------------------------------------------
(4) Beads
 -------------------------------------------------------------------------------| DAMAGE | LIMITATION | ACTION | |-----------------------------------------------------------------------------| | EXPOSURE | Radial and bias tires | | | OF BEAD | | Remove the tire. | | WIRES | | | |---------------|------------------------------------|------------------------| | | Radial and bias tires | | | DEFORMATION | Deformation of beads or bead wires | Remove the tire. | | | | | |---------------|------------------------------------|------------------------| | | Radial and bias tires | | | CRACKS | Cracks in upper part of bead zone | Remove the tire. | | | depth of the crack more than | | | | 1 mm | | |---------------|------------------------------------|------------------------| | | Radial and bias tires | | | WEAR | The wear of the tire surface near | Remove the tire. | | | the upper edge of the rim | | | | depth of the worn area more than | | | | 2 mm | | |---------------|------------------------------------|------------------------| | | Radial and bias tires | | | BLISTER | Blister in upper part of bead zone | Remove the tire. | | | length or diameter more than | | | | 10 mm | | -------------------------------------------------------------------------------
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 TASK 32-41-00-210-003 Inspection/Check of the Pressure of Tires
 1.
 Reason for the Job

__________________
 Refer to the MPD TASK: 324100-01

 2.
 Job Set-up Information

______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific pressure gage
 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 32-41-11-000-006 Removal of the MLG Wheel (2649GM,2650GM,2651GM,2652GM) 32-41-11-400-006 Installation of the MLG Wheel
 (2649GM,2650GM,2651GM,2652GM) 32-41-12-000-001 Removal of the NLG Wheel (2659GM,2660GM) 32-41-12-400-001 Installation of the NLG Wheel (2659GM,2660GM)
 3. Job Set-up
__________ Subtask 32-41-00-860-052
 A. Not Applicable
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