TASK 70-31-02-310-501-003 Argonarc Welding Repairs - Orbital Torch Welding

DMC:V2500-00-70-31-02-02A-627A-D|Issue No:001.00|Issue Date:2013-03-20

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 70-31-02-310-501-003 Argonarc Welding Repairs - Orbital Torch Welding

Table of Contents

Inspection Limits

Visual Inspection

Penetrant Inspection

Radiographic Inspection

Do a Pressure Test

Cut Back the Weld Bead

Ream the Weld Underbead

General

Orbital torch welding is an automatic argonarc welding operation where the workpiece is held stationary and the welding torch is turned. It is used to weld tube and tube fittings. Where specifc use of this type of equipment is necessary instructions will be given in the Engine Manual.

The pipe and fittings can be located by fixtures or tack-welds.

Tooling must provide a good ground connection (earth) as close to the weld as possible.

NOTE

Tube welds made mechanically or manually must be examined as specified in the SPM TASK 70-31-02-310-501-003. Unless specified differently in the Engine Manual.

NOTE

To identify the consumable materials refer to the PCI.

Preliminary Requirements

Pre-Conditions

NONE

Support Equipment

NONE

Consumables, Materials and Expendables

NameManufacturerPart Number / IdentificationQuantityRemark
CoMat 01-277 KEROSINELOCALCoMat 01-277

Spares

NONE

Safety Requirements

WARNING

IT IS THE RESPONSIBILITY OF THE OPERATOR TO OBTAIN AND OBSERVE THE MANUFACTURER'S MATERIAL SAFETY DATA SHEETS FOR CONSUMABLE MATERIALS. THESE CONTAIN INFORMATION SUCH AS, HAZARDOUS INGREDIENTS, PHYSICAL/CHEMICAL CHARACTERISTICS, FIRE, EXPLOSION, REACTIVITY, HEALTH HAZARD DATA, PRECAUTIONS FOR SAFE HANDLING, USE AND CONTROL MEASURES AND ALSO TO TAKE LOCAL REGULATIONS INTO CONSIDERATION.

Procedure

    1. SUBTASK 70-31-02-220-003 Inspection Limits of Orbital Torch Welds.

      1. Weld bead shape. See Figure.

      2. The weld crown and the underbead must have a smooth contour with the parent metal. There must be no sharp changes of section.

      3. The weld must be visible and fully penetrate its complete length. The maximum height of the crown or the underbead must not be more than 1t. The maximum thickness of the weld must not be more than 2.25t of the tube material thickness.

      4. The weld bead width must be between 2.5 and 5t.

      1. Defects in the weld that are not permitted.

      2. Cracks in the weld or heat affected zone.

      3. Lack of side fusion with the parent metal.

      4. Lack of penetration.

      5. Chain porosity (porosity in a continuous line).

      6. Oxidation of the crown or underbead.

      7. Incorrect weld bead geometry.

      8. Ballooning of the weld bead because internal argon pressure is too high.

      9. Unfused tack welds.

      10. Arc damage anywhere on the tube.

      1. Permitted defects in the weld.

      2. Undercut and sinkage is permitted to a maximum 0.1t, if there is no sharp change of section or sharp edges.

      3. Stop craters at the weld run out, if they are not more than 1t diameter and 0.25t deep.

        1. Subsurface porosity.

        2. 0.5t in the weld bead.

        3. 0.25t in the blend of the bead to the parent metal.

        4. For general porosity limits, refer to the SPM TASK 70-31-02-310-501-001, SUBTASK 70-31-02-260-001.

      4. Two tungsten inclusions, if they are not more than 0.75t in diameter and are fully in the weld bead. They must have a minimum distance of 0.2 in. (5 mm) between them.

      5. Misalignment of the tube and end fitting up to 0.15t or 0.005 inch (0.13 mm) whichever is greater.

      6. Smooth flaring up to 0.15t without loss of wall thickness.

    1. SUBTASK 70-31-02-220-004 Visual Inspection of Orbital Torch Welds.

    2. All welds must be visually examined as specified in Step. The weld crown must be examined visually without magnification aids and where possible examine the underbead with an intrascope.

    3. Where the geometry of the tube permits, the tube must be visually examined to make sure it is not blocked. If this is not possible a ball check must be done. To do this check, a sphere of applicable diameter is passed along the bore of the tube. Alternatively do a flow check with CoMat 01-277 KEROSINE.

    1. SUBTASK 70-31-02-230-002 Penetrant Inspection of Orbital Torch Welds.

    2. Subsequent to a visual inspection it is important that all welds are examined with an approved penetrant procedure. Refer to the SPM TASK 70-23-00-230-501.

    3. Inspect to the standard given in Step.

    1. SUBTASK 70-31-02-260-003 Radiographic Inspection of Oribital Torch Welds.

    2. Radiographic inspection of welds shows defects which cannot be found with visual or penetrant procedures. All tube assemblies must be radiographically examined. Refer to the SPM TASK 70-26-01-260-501.

      Inspect to the standard given in Step.

    3. Do as follows for a radiographic inspection of tubes with an internal diameter of less than 1.50 in. (38.1 mm). It is necessary to use a double-wall double image procedure with two exposures at right angles to each other. Refer to Figure this shows the beam angle for different tube diameters.

    4. Refer to the SPM TASK 70-26-01-260-501 for methods and control of Radiographic inspection.

    1. SUBTASK 70-31-02-780-001 Do a Pressure Test

    2. All tube assemblies must have a pressure test done after repair. The instructions will be given in the applicable Repair.

    1. SUBTASK 70-31-02-320-001 Cut Back the Weld Bead

    2. The weld bead can be cut back mechanically to make its geometry better and to remove small surface defects within the limitations of Step.Cutting back of the parent material is acceptable up to a maximum depth of 0.1t.

    1. SUBTASK 70-31-02-350-001 Ream the Weld Underbead

    2. Where the geometry of the tube permits, it is permitted to ream the underbead to the limits given in Step. The location of the reamer is important to make sure the underbead is reamed concentric with the tube wall. All swarf must be removed.

      Sharp edges remaining after the underbead is reamed must be removed. Make sure the weld bead geometry is in the specified limits.

      .

    1. SUBTASK 70-31-02-350-002 Rework

    2. With the exception of oxidised underbeads hand or automatic re-welding may be carried out but shall be limited to two rewlds only.

  1. Figure: Weld bead dimensions

    Weld bead dimensions

    Figure: Radiographic inspection of butt welded tubes

    Radiographic inspection of butt welded tubes

Requirements After Job Completion

Follow-On Conditions

NONE
Manufacturer Code:LOCAL
Enterprise Name:LOCALLY SUPPLIED
Manufacturer Code:LOCAL
Supply Number:CoMat 01-277
Type:sp01
Supply Short Name:CoMat 01-277 KEROSINE
Supply Name:CoMat 01-277 KEROSINE
Specification Groups:
Doc NumberType
OMAT: 101COMMERCIAL GRADE D.ENG.RD2494 MIL-T-5624 TYPE JP5
Suppliers:
ManufacturerRemarks
LOCAL
IE108