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
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Common Information
TASK 70-23-02-230-501 Medium Sensitivity Water-Washable Fluorescent Penetrant Crack Inspection
Introduction
This procedure details the requirements for Medium Sensitivity Water-washable (AMS 2644 Level 2 Method D) Fluorescent Penetrant Inspection.
In order to maintain consistent results within a set of parts once a process to undertake the Non-Destructive Inspection of a part has been established by the responsible Level 3 qualified person, the process is not to be varied or changed.
Aerospace Materials Specification AMS 2647 is an acceptable alternative document for the procedures used to prepare engine parts for fluorescent penetrant inspection and for procedure control instructions.
SPM TASK 70-23-01-230-501 Medium Sensitivity Post-Emulsified Fluorescent Penetrant Inspection is a permitted alternative to SPM TASK 70-23-02-230-501 Medium Sensitivity Water-Washable Fluorescent Penetrant Inspection on static parts. When one of these procedures is specified for a static part in the engine manual, you can use the alternative procedure with the appropriate consumables for the task. The exception to the alternative use of the procedure would be on components where the emulsifier may be difficult to remove such as air cooled turbine vanes or cases with cavities.
To identify the specified consumable materials, refer to the Consumable Materials Index.
NOTE
Preliminary Requirements
Pre-Conditions
NONESupport Equipment
NONEConsumables, Materials and Expendables
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| CoMat 01-031 ACETONE (CH3)2CO | LOCAL | CoMat 01-031 | ||
| CoMat 01-124 ISOPROPYL ALCOHOL | LOCAL | CoMat 01-124 | ||
| CoMat 01-499 CLEANER / REMOVER - FLUORESCENT PENETRANT | 37676 | CoMat 01-499 | ||
| CoMat 06-030 NON AQUEOUS DEVELOPER | 01PQ6 | CoMat 06-030 | ||
| CoMat 06-032 DRY DEVELOPER | 37676 | CoMat 06-032 | ||
| CoMat 06-064 FLUORESCENT PENETRANT (WATER WASHABLE MEDIUM SENSITIVITY) | X222X | CoMat 06-064 |
Spares
NONESafety Requirements
WARNING
Procedure
Refer to SPM TASK 70-23-00-230-501.
SUBTASK 70-23-02-230-001 The Control of Equipment and Materials
Surface contamination will cause the penetrant to stay on the surface, which will give incorrect indications.
NOTE
If degreasing is not carried out in the penetrant facility, or there is a delay between degreasing/aqueous processing and applying the penetrant, be sure to protect parts from airborne/handling contamination.
The parts to be inspected must be fully cleaned. The cleaned surface must be free also from cleaning agents. Remove residue oil, grease, dirt and scale, unwanted material, or other surface contaminants by the cleaning method specified in the engine manual.
General.
Put the part in clean hot water at 150 °F to 200 °F (66 °C to 93 °C) for the necessary time to increase the temperature of the part sufficiently to flash dry.
NOTE
The necessary time in the hot water is dependent on the number of parts in the water, and on the size and mass of the parts.Remove the part from the hot water. If the part has cavities and recesses, rotate the part as soon as possible to flash off the water, or use suction to remove the pooled water. Blow off remaining water from these areas.
NOTE
If the water on the part does not flash off when the part comes out of the hot water, then the time interval that the part stayed in the hot water was too short.
Flash Dry Procedure:
Oven dry at 158 °F - 248 °F (70 °C - 120 °C) for one hour minimum.
Oven dry at 257 °F - 275 °F (125 °C - 135 °C) for 30 minutes minimum.
Do one of the subsequent procedures:
Oven Dry Procedure:
NOTE
It is not permitted to use this procedure as an alternative to the hot water flush procedures or the flash dry procedures in SPM chemical cleaning tasks or SPM abrasive cleaning tasks.Vacuum-Assisted Oven Dry Procedure:
NOTE
The Vacuum-Assisted Oven Dry Procedure can use lower temperatures and shorter drying times than the Oven Dry Procedure.NOTE
It is not permitted to use this procedure as an alternative to the hot water flush procedures or the flash dry procedures in SPM chemical cleaning tasks or SPM abrasive cleaning tasks.Dry the part in a vacuum-assisted oven. Refer to SPM TASK 70-23-00-230-501, SUBTASK 70-23-00-180-002.
If you use one or more aqueous chemical procedures to remove coatings from the part or to clean the part before FPI, it is necessary to use one of the procedures in the subsequent list to do the final dry in the last aqueous chemical procedure before FPI.
Drying of parts after aqueous chemical procedures to prepare parts for FPI.
SUBTASK 70-23-02-230-002 Initial Preparation
The part surface temperature must be 40 °F - 125 °F (4 °C - 52 °C).
NOTE
It is permitted to do this step in ultra-violet light (UV light) to make sure that penetrant coverage is complete.NOTE
It is not permitted to mix the selected CoMat letter suffix penetrant material with other CoMat letter suffix penetrant materials.Apply CoMat 06-064 FLUORESCENT PENETRANT (WATER WASHABLE MEDIUM SENSITIVITY) to the part by one of the procedures that follow:
Examine the part with ultra-violet light (UV light) for total coverage of the part with the penetrant.
Apply the penetrant.
Let the part drain for 20 to 60 minutes. Draining can be done by suspending the part over the immersion tank. If the penetrant is drained into a separate drop tray, it must not be re-used unless it is re-checked to the manufacturer's instructions and found acceptable. However, it is generally best to discard the collected drained solution.
Drain the part.
The maximum permitted spray time for each area of the part is 90 seconds.
For manual FPI lines, keep the spray gun nozzle at a minimum distance of 12 in. (304.8 mm) from the part. Always be careful with closed areas, such as undercuts, blocked holes, and oilways.
The spray gun nozzle must be adjusted to give a low velocity, moderately fine spray.
The maximum permitted air pressure is 25 psi (172 kPa), and the maximum permitted water pressure is 25 psi (172 kPa).
Spray the part with water to remove excess penetrant . The water temperature must be 50 °F to 100 °F (10 °C to 38 °C).
Put the part in a water bath for a time of 90 seconds maximum. The water temperature must be 50 °F to 100 °F (10 °C to 38 °C).
NOTE
It is permitted to do this step in ultra-violet light (UV light) to monitor the removal of penetrant from the part surface.Rinse by one of the procedures that follow:
Final Wash Procedure.
Examine the part with UV light for satisfactory removal of surface penetrant.
Examine part for removal of surface penetrant.
It is necessary to apply the developer in two hours or less after the Final Wash Procedure. If you do not apply the developer in two hours or less after the Final Wash Procedure is completed, it necessary to clean and dry the part, and then do this task again.
When the part is fully dry, immediately apply CoMat 06-032 DRY DEVELOPER to the inspection area, and permit the developer to stay on the part for a minimum of 10 minutes.
NOTE
For aluminum castings and carbon liners, it is important to have a 10 to 30 minutes penetrant bleed-out time and then apply dry developer only to indications you are not sure of. Make an analysis immediately.
Apply CoMat 06-032 DRY DEVELOPER.
For each indication or area that you are not sure of, use the penetrant 'wipe off' procedure given in Step.
NOTE
Some defects seen by penetrant with UV light cannot be seen with white light; if this occurs, it is necessary to get relevant help.
Circle indications and areas you are not sure of, use one of the approved temporary marking procedures in SPM TASK 70-09-01-400-501. If it is not possible to make a mark around an indication or an area that you are not sure of, make a mark adjacent to the indication or the area that you are not sure of.
Apply CoMat 06-030 NON AQUEOUS DEVELOPER by spray to each local area to get a developer layer of approximately equal thickness that is sufficient to see the developer layer on the part surface but is not sufficient to fully obscure the color of the part.
Do the supplemental inspection in one hour or less after you apply the non-aqueous developer.
NOTE
Removal of developer is necessary only, if it interferes with subsequent processes or part function.
After you do the inspection of the part with dry developer, it is permitted to apply non-aqueous developer to local areas of the part to do supplemental inspection:
Inspection Requirements.
Inspection of Parts.
If you use a non-aqueous developer, remove by SPM TASK 70-11-26-300-503.
Removal of developer.
If necessary to prevent rust or corrosion, apply corrosion inhibitor by SPM TASK 70-38-05-380-501.
Temporary protection.
SUBTASK 70-23-02-230-003 Inspection Procedure
Use a cotton bud made moist with CoMat 01-031 ACETONE (CH3)2CO or CoMat 01-124 ISOPROPYL ALCOHOL or CoMat 01-499 CLEANER / REMOVER - FLUORESCENT PENETRANT to lightly clean the penetrant indication.
NOTE
The solvent will dry quickly.If the indication immediately shows again, then the indication is the result of a discontinuity. If you cannot easily see the initial mark around or adjacent to the indication, apply a new mark around or adjacent to the indication.
Apply CoMat 06-030 NON AQUEOUS DEVELOPER by spray to get a developer layer of approximately equal thickness that is sufficient to see the developer layer on the part surface but is not sufficient to fully obscure the color of the part.
If the indication shows again in three minutes or less after you applied the non-aqueous developer, then a discontinuity is the cause of the indication. If you cannot easily see the initial mark around or adjacent to the indication, apply a new mark around or adjacent to the indication.
If the inspection with 3X - 10X magnification in white light finds a discontinuity that caused the initial indication, and you cannot easily see the initial mark around or adjacent to the indication, apply a new mark around or adjacent to the indication.
If the inspection with 3X - 10X magnification in white light does not find a cause for the initial indication, then it is permitted to ignore the initial indication, and to remove the mark around or adjacent to the indication by SPM TASK 70-11-26-300-503.
If the indication does not show again in three minutes or less after you applied the non-aqueous developer, do an inspection of the area with 3X - 10X magnification in white light for the cause of the initial indication.
Examine the indication area again in UV light.
If the indication does not immediately show again, do the subsequent procedure:
Let the surface of the part dry, then examine the area again in UV light.
Examine each marked indication with 3X - 10X magnification in white light to identify the type of discontinuity.
SUBTASK 70-23-02-230-004 Penetrant 'Wipe-off' Procedure

CAUTION
IT IS NECESSARY TO BE CAREFUL DURING THE PENETRANT WIPE-OFF PROCEDURE BECAUSE IF THERE IS NO SECOND INDICATION, IT IS POSSIBLE THAT THE FIRST INDICATION SHOWED A CRACK THAT HAS A VOLUME THAT IS TOO SMALL TO HOLD SUFFICIENT PENETRANT FOR A SECOND INDICATION.NOTE
You can use this procedure only one time for each indication.
