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 73-22-49-300-003 Fuel System Sensing Air Tubes - Blend Repair Surface Damage, Repair-003 (VRS6225)
Effectivity
FIG./ITEM | PART NO. |
09-100 | 6A2133 |
09-500 | 6A2122 |
09-500 | 6A6007 |
10-100 | 6A2126 |
10-500 | 6A1692 |
11-100 | 6A1693 |
12-100 | 6A2135 |
Material of component
PART IDENT | SYMBOL | MATERIAL |
Tube | EBS | Chromium/nickel steel tube |
Adaptor | LAH | Chromium/nickel steel |
General
The practices and processes referred to in the procedure by the TASK number are in the SPM.
NOTE
Preliminary Requirements
Pre-Conditions
NONESupport Equipment
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| Workshop inspection equipment | LOCAL | Workshop inspection equipment | ||
| Penetrant Crack Test Equipment | LOCAL | Penetrant crack test equipment |
Consumables, Materials and Expendables
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| CoMat 05-106 ABRASIVE STONE | K6835 | CoMat 05-106 | ||
| CoMat 05-110 EMERY POLISHING PAPER | 0AM53 | CoMat 05-110 | ||
| CoMat 05-111 EMERY POLISHING PAPER | 06565 | CoMat 05-111 |
Spares
NONESafety Requirements
NONEProcedure
Refer to SPM TASK 70-23-01-230-501.
Do a penetrant crack test
SUBTASK 73-22-49-230-063-001 Examine the Repair Area of the Tube for Cracks
Refer to SPM TASK 70-23-03-230-501.
Do a penetrant crack test
SUBTASK 73-22-49-230-063-002 Examine the Repair Area of the Tube for Cracks
The maximum depth of damage to be removed must not be more than 0.002 in. (0.051 mm). Blend the area to remove the sharp edges.
Refer to SPM TASK 70-35-21-350-501.
Remove the damage
Polish the area to make it smooth and remove the dressing marks.
Polish the repair area
SUBTASK 73-22-49-350-060 Remove the Tube Damage
Refer to Inspection-000 TASK 73-22-49-200-100.
Do a visual and dimensional inspection.
SUBTASK 73-22-49-220-106 Examine the Repair Area of the Tube
Refer to SPM TASK 70-23-01-230-501.
No cracks are permitted
Do a penetrant crack test
SUBTASK 73-22-49-230-064-001 Examine the Repair Area of the Tube for Cracks
Refer to SPM TASK 70-23-01-230-501.
No cracks are permitted.
Do a penetrant crack test.
SUBTASK 73-22-49-230-064-002 Examine the Repair Area of the Tube for Cracks
