Export Control
EAR Export Classification: Not subject to the EAR per 15 C.F.R. Chapter 1, Part 734.3(b)(3), except for the following Service Bulletins which are currently published as EAR Export Classification 9E991: SBE70-0992, SBE72-0483, SBE72-0580, SBE72-0588, SBE72-0640, SBE73-0209, SBE80-0024 and SBE80-0025.Copyright
© IAE International Aero Engines AG (2001, 2014 - 2021) The information contained in this document is the property of © IAE International Aero Engines AG and may not be copied or used for any purpose other than that for which it is supplied without the express written authority of © IAE International Aero Engines AG. (This does not preclude use by engine and aircraft operators for normal instructional, maintenance or overhaul purposes.).Applicability
All
Common Information
TASK 72-32-16-200-009 Gearbox Driven Bevel Gearshaft (56T) - Examine, Inspection-009
General
This TASK gives the procedure for the inspection of the 56T pinion bevel gearshaft. For the other internal gearbox driven gear assembly parts, refer to TASK 72-32-16-200-000 (INSPECTION-000).
Fig/item numbers in parentheses in the procedure agree with those used in the IPC.
The policy that is necessary for inspection is given in the SPM TASK 70-20-01-200-501.
All the parts must be cleaned before any part is examined. Refer to TASK 72-32-16-100-000 (CLEANING-000).
All parts must be visually examined for damage, corrosion and wear. Any defects that are not identified in the procedure must be referred to IAE.
The procedure for those parts which must have a crack test is given in Step. Do the test before the part is visually examined.
Do not discard any part until you are sure there are no repairs available. Refer to the instructions in the repair before a discarded part is used again or oversize parts are installed.
Parts which should be discarded can be held although no repair is available. The repair of a discarded part could be shown to be necessary at a later date.
All parts must be examined to make sure that all the repairs have been completed satisfactorily.
The practices and processes referred to in the procedure by the TASK numbers are in the SPM.
References
Refer to the SPM for data on these items.
Definitions of Damage, SPM TASK 70-02-02-350-501
Inspection of Parts, SPM TASK 70-20-01-200-501
Some data on these items is contained in this TASK. For more data on these items refer to the SPM.
Method of Testing for Crack Indications
Chemical Processes
Surface Protection
NOTE
Preliminary Requirements
Pre-Conditions
NONESupport Equipment
NONEConsumables, Materials and Expendables
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| CoMat 06-011 MAGNETIC PARTICLES, FLUORESCENT, DRY POWDER | LOCAL | CoMat 06-011 |
Spares
NONESafety Requirements
NONEProcedure
Clean the part. Refer to TASK 72-32-16-100-000 (CLEANING-000).
NOTE
During magnetic inspection, it is recommended to use CoMat 06-011 MAGNETIC PARTICLES, FLUORESCENT, DRY POWDER.Do the crack test on the part that follows. Use the applicable magnetic inspection procedure.
PART IDENT
PROCEDURE
CURRENT/INSPECT
TASK/SUBTASK
56T pinion bevel gearshaft
TB using continuous wet or simultaneous inking with the CoMat 06-011 MAGNETIC PARTICLES, FLUORESCENT, DRY POWDER
1000 amp.
Shaft outside diameter.
Visually examine for longitudinal and radial defects.
Do a check for doubtful indications using low power magnification.
If necessary, examine under white light at 15X binocular
3000 amp.
Flange area.
Examine as for shaft outside diameter
SPM
Solenoid continuous wet or simultaneous inking
6000 A/T.
Do again the magnetization and inspection along nut length
Visually examine for circumferential defects. Do a check for doubtful indications using low power magnification. If necessary, examine under white light at 15X binocular
SUBTASK 72-32-16-240-052 Examine the 56T Pinion Bevel Gearshaft (01-750) for Cracks
Refer to Figure.
Repair, VRS1208 TASK 72-32-16-300-003 (REPAIR-003)
Nicked, dented or scratched
Examine all the surfaces which do not include the identified locations.
SUBTASK 72-32-16-220-059 Examine the 56T Pinion Bevel Gearshaft (01-750) all the Surface
Refer to Figure.
Repair, VRS1208 TASK 72-32-16-300-003 (REPAIR-003)
Pick-up
SUBTASK 72-32-16-220-061 Examine the 56T Pinion Bevel Gearshaft (01-750) Threads at Location 2
Refer to Figure.
Repair, VRS1208 TASK 72-32-16-300-003 (REPAIR-003)
Galled or scored
SUBTASK 72-32-16-220-062 Examine the 56T Pinion Bevel Gearshaft (01-750) Splines at Location 3
Refer to Figure.
SUBTASK 72-32-16-220-063 Examine the 56T Pinion Bevel Gearshaft (01-750) Oil Holes at Location 4
Refer to Figure.
Repair, VRS1208 TASK 72-32-16-300-003 (REPAIR-003)
Burred
SUBTASK 72-32-16-220-064 Examine the 56T Pinion Bevel Gearshaft (01-750) Grooves at Location 5
Refer to Figure.
Repair, VRS1208 TASK 72-32-16-300-003 (REPAIR-003)
Galled
Examine the snap diameter at location 6.
Repair, VRS1208 TASK 72-32-16-300-003 (REPAIR-003)
Galled
Examine the snap diameter at location 7.
Repair, VRS1208 TASK 72-32-16-300-003 (REPAIR-003)
Galled
Examine the snap diameter at location 8.
SUBTASK 72-32-16-220-065 Examine the 56T Pinion Bevel Gearshaft (01-750) Snap Diameters at Locations 6, 7 and 8
Refer to Figure.
Repair, VRS1208 TASK 72-32-16-300-003 (REPAIR-003)
Galled at location 9, 10 and 11
SUBTASK 72-32-16-220-066 Examine the 56T Pinion Bevel Gearshaft (01-750) Bearing Location Diameter, at Locations 0501, 0505, 0507, 9, 10 and 11
Figure: Locations on the 56T pinion bevel gearshaft
Locations on the 56T pinion bevel gearshaft

