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
Pre SBE 72-0241
Common Information
TASK 72-44-50-840-002 HPT Stage 1 Cooling (TOBI) Duct - Provide A New HPT Stage 1 Cooling (TOBI) Duct, Rework-002 - SBE 72-0241
General
You must do the rework on the stage 1 HPT blade assembly given in TASK 72-45-14-840-001, SBE 72-0242, REWORK 001 before or at the same time as you do the rework given in this procedure.
You must do the rework on the stage 1 HPT duct segments given in TASK 72-44-60-840-002, SBE 72-0241, REWORK 002 at the same time you do the rework given in this procedure.
The practices and processes referred to in the procedure by the TASK number are in the SPM.
Refer to the indicated Service Bulletin for specific application requirements.
Preliminary Requirements
Pre-Conditions
NONESupport Equipment
NONEConsumables, Materials and Expendables
NONESpares
NONESafety Requirements
NONEProcedure
Do the procedure given in TASK 72-44-50-300-010, VRS3177 (REPAIR-010).
Do a modification to get the airflow level of 2A3180. Add plug welds as necessary. The required flow parameter is 1.152. The required average is 1.533.
SUBTASK 72-44-50-350-067 Adjust the Airflow of the Stage 1 HPT Cooling Duct Assembly (01-010)
No cracks are permitted.
Refer to the SPM TASK 70-23-03-230-501.
Fluorescent penetrant inspect the duct.
SUBTASK 72-44-50-230-055 Examine the Stage 1 HPT Cooling Duct Assembly (01-010)
Refer to the SPM TASK 70-09-00-400-501.
Number before - 2A2141-01.
New number - 2A3180-01.
Make a mark adjacent to the old part number to show the new part number. Use the vibration peen method.
SUBTASK 72-44-50-350-068 Identify the New Stage 1 HPT Cooling Duct Assembly (01-010)
Refer to the SPM TASK 70-09-00-400-501.
Number before - 2A4300.
New number - 2A8600.
When you assemble the new turbine nozzle group (which includes the new stage 1 HPT cooling duct assembly and the new stage 1 HPT duct segments), identify the new turbine nozzle group. Make a mark adjacent to the old part number to show the new part number. Use the vibration peen method.
SUBTASK 72-44-50-350-069 Identify the New Turbine Nozzle Group
Figure: Location of the stage 1 HPT cooling duct assembly
Location of the stage 1 HPT cooling duct assembly

Figure: Modification of the stage 1 HPT cooling duct assembly
Modification of the stage 1 HPT cooling duct assembly

Figure: Modification of the stage 1 HPT cooling duct assembly
Modification of the stage 1 HPT cooling duct assembly

Figure: Modification of the stage 1 HPT cooling duct assembly
Modification of the stage 1 HPT cooling duct assembly

