CASR FPI Engineering Studies: Cleaning in Preparation for FPI

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CASR FPI Engineering Studies: Cleaning in Preparation for FPI Lisa Brasche Center for Nondestructive Evaluation Iowa State University lbrasche@iastate.edu (515) 294-5227 http://www.cnde.iastate.edu/faa-casr/fpi/index.html

Cleaning Objectives: Why is it important? Visual appearance and inspection Remove deposits and prepare surfaces Reduce or prevent corrosion Reduce mechanical cleaning (media blasting) Enhance nondestructive testing performance (FPI, MPI, EC UT) Subsequent special processes require clean surface (heat treatment, weld, braze, thermal spray, paint, plate, etc.) (Ref: Terry Kessler)

How Clean is Clean? You will know... If it looks or feels oily or greasy If dirt wipes off on your finger If the part shows heat scale remaining... If water beads up If FPI penetrant beads up (Ref: Terry Kessler) IT IS NOT CLEAN ENOUGH!!!!

Cleaning Methods Chemical and mechanical cleaning tools Selected based on contamination/soils to be removed Consideration given to alloy (corrosion resistance, removal rates, etc.)

Objectives Determine the effect of chemical cleaning, mechanical cleaning, and drying processes on the detectability of low cycle fatigue cracks in titanium and nickel alloys Establish the effect of local etching on detectability and provide guidance on best practices for removal of local surface damage from FOD and other surface anomalies Update existing specifications to reflect the improved processes and provide best practices documents for use by the OEM s and airlines

Field Studies Requires access to typical drying and cleaning methods used in commercial aviation Delta Airlines provided access to their facilities June 18 2001 October 18 2001 February 4 2002 Access to cleaning lines for Ti and Ni as well as mechanical blasting facilities FPI line for sample processing Inspection booth for characterization and brightness measurements

Cleaning Study Cleaning Studies - matrix of contaminants Part 1 October 2001 Penetrating oil applied over crack Anti-galling compound applied to side of crack RTV compound applied to side of crack High temperature sealant (Ni) applied to side of crack Baked-on contamination Dec 01 Jan 02 Part 2 February 2002 Soot generated using forced air furnace at HW Varnish generated using forced air furnace at HW Oxidation and scale generated using forced air furnace at HW

Cleaning Study

Contaminants: Penetrating Oil Antigallant compound RTV/Sealant Cleaning Study Contaminants: Oxidation/scale Soot Varnish Oil Cleaning Methods B1 40 psi Plastic media blast B1 80 psi Plastic media blast B6 50 psi - Walnut shell C1 Aqueous degreaser, cold rinse C2a Ti alkaline derust, short soak, high concentration C2b Ti alkaline derust, long soak, low concentration C3 Ni one step alkaline C6 Ti degreaser followed C7a Ni UT with alkaline derust C8 Rubber stripper Cleaning Methods B1 40 psi Plastic media blast B2 Wet glass bead B3 240 grit Al 2 O 3 B4 320 grit Al 2 O 3 Baked on B5 500 grit Al 2 O 3 contaminants B6 50 psi - Walnut shell C1 Aqueous degreaser, cold rinse C2a Ti alkaline derust, short soak, high concentration C2b Ti alkaline derust, long soak, low concentration C3 Ni one step alkaline C4 Ni four step alkaline/acid C5 Alkaline gel cleaner C6 Ti degreaser C7a Ni UT with alkaline derust C8 Rubber stripper

Cleaning Study New Used Plastic media Walnut shell Wet glass bead Al 2 O 3 320 grit Al 2 O 3 500 grit

Cleaning Study

Cleaning Study

Cleaning Study

Cleaning Study Cleaning Studies Part 1 Penetrating Oils C1 Aqueous degreaser C2a and C2b Alkaline De-rust Solution (A and B) C3 Alkaline one step C6 Steam with aqueous degreaser Anti-Galling Compound C2a and C2b Alkaline De-rust Solutions (A and B) C7a Ultrasonic w/alkaline De-rust Solution B B1 Plastic media blast (at 80 and 40 psi) for 30 sec using pressure cabinet B6 Shell blast (at 50 psi) for 1 min using pressure cabinet RTV Compound and High Temperature Sealant B1 Plastic media blast (at 80 and 40 psi) for 30 sec using pressure cabinet B6 Shell blast (at 50 psi) for 1 min using pressure cabinet

Oil Contamination Penetrating oil applied over crack and allowed to sit overnight prior to cleaning C1 Aqueous degreaser C2a and C2b Alkaline De-rust Solution (A and B) C3 Alkaline one step C6 Steam with aqueous degreaser C7a Alkaline De-rust with UT agitation C1, C3 and C6 were found to be effective cleaners Hot and cold water rinse were found to be equally effective for C3 C2a/C2b and C7a did not provide consistent cleaning action

01-029 Ni 01-029 Oct Pre BL BT =107.4 01-029 Oct Post BL BT = 121 01-029 After oil + C1 BT = 92.5

Oil followed by C3 with cold water rinse 00-105 Oct Pre BL BT = 136.2 00-105 After oil + C3 cold BT = 192 00-105 Oct Post BL BT = 181.4 01-022 Oct Pre BL BT = 16 01-022 After oil + C3 cold BT = 10.9 01-022 Oct Post BL BT = 19 00-055 Oct Pre BL BT = 27.5 00-055 After oil + C3 cold BT = 37.2 00-055 Oct Post BL BT = 27.5

Oil followed by C3 with hot water rinse 00-124 Oct Pre BL BT = 187 00-124 After oil + C3 hot BT = 126.3 00-124 Oct Post BL BT = 250 01-020 Oct Pre BL BT = 20 01-020 After oil + C3 hot BT = 26.4 01-020 Oct Post BL BT = 33.8 01-025 Oct Pre BL BT = 25.3 01-025 After oil + C3 hot BT = 28.8 01-025 Oct Post BL BT = 29

C7a for Oil Contamination 00-127 Oct Pre BL BT = 67.9 00-127 Oil + C7a BT = 3.9 00-127 Oct Post BL BT = 79.8 01-026 Oct Pre BL BT = 13.8 01-026 Oil + C7a BT = 20 01-026 Oct Post BL BT = 40.1 01-034 Oct Pre BL BT = 0.9 01-034 Oil + C7a BT = 1.5 01-034 Oct Post BL BT = 1.4

Oil contamination C2a process was not effective for oil removal from Ti samples C2a process used for titanium utilizes similar chemistries and concentrations as C3 process for nickel. However, Ti parts are in alkaline for shorter duration. Given better performance for C3 than C2, additional work is needed to understand if this is an alloy effect or a cleaning time effect.

Coating Removal All cleaning methods used to remove service coatings (anti-gallant compound, RTV and high temperature sealant) were effective in removal of the coatings However, reductions in FPI indication response did occur in some cases

Mechanical Cleaning Wet glass bead blast Al 2 O 3 500 grit Al 2 O 3 320 grit Al 2 O 3 240 grit Walnut shell blast

Plastic Media Blast Typical blast pressures are 40 psi Study looked at both 40 and 80 psi PMB at 40 psi was found to be effective cleaner with better performance if followed by a wet process Remove PMB residue from surface and/or cracks PMB at 80 psi led to surface damage and is not recommended as a process to proceed parts that will undergo FPI

01-052 Pristine crack 01-052 Ti 01-052 Oct Pre BL BT=43.8 Surface changes indicate removal of sanding marks with B1-80 treatment. Lower image is after soot and subsequent B1-40 treatment. Additional surface changes not evident. 01-052 After B1-80 01-052 After B1-80 BT = 50.9 01-052 Oct BL BT = 44.9 01-052 Post studies 01-052 After B1-40 BT = 68.3

00-106 Pristine crack 00-106 - Ni 00-106 Oct Pre BL BT = 50.9 00-106 After B1-80 BT = 8.7 00-106 Oct Post BL BT = 47.8 00-106 Post B1-80 SEM 00-106 Plastic media particles

B1-40 applied to Coke/varnish samples 01-027 Oct BL BT = 93.2 01-027 After PMB No indication 01-027 After PMB + C3 BT = 65.9 01-027 After PMB + C3 + C4 BT = 99.3 01-035 Oct BL BT = 4.7 01-035 After B1-40 BT = 3.2 01-035 After PMB + C3 BT = 2.6 01-035 After PMB + C3 + C4 BT = 5.4 01-056 Oct BL BT = 2.8 01-056 After B1-40 BT = 0.1 01-056 After PMB + C3 No indication 01-056 After PMB + C3 + C4 BT = 3.2

Wet Glass Bead Blast 01-009 Pristine crack 01-009 Ni 01-009 Oct BL BT = 7.2 01-009 After Wet glass bead Indication not found after B2 treatment 01-009 After B2 + C4 BT = 4.4

00-087 Pristine crack Al 2 O 3 240 grit - 00-087 Ti 00-087 Oct BL BT = 92.5 00-087 Post studies SEM 50X 150X 00-087 Feb ace BT = 76.1 500X 00-087 After B3 BT = 3.4 1500X

Al 2 O 3 320 grit 01-029 Ni 01-029 Oct BL BT = 121.3 SEM 50X 150X 01-029 Pristine crack 0.083 01-029 Feb acetone BT = 65.7 Indication not found after 320 grit process 500X 1500X

Al 2 O 3 500 grit - 00-067 Ti 00-067 Pristine crack 00-067 Oct Pre BL BT = 114.3 00-067 B5 BT = 108.5 00-067 After B5 00-067 Oct Post BL BT = 97.1

Al 2 O 3 500 grit 00-093 Ti 00-093 Oct Bl BT=66.7 00-093 Pristine crack 00-093 After B5 00-093 After B5 BT =.01 00-093 After B5 and C2b BT = 0.1

01-037 Ti Walnut Shell Media Blast 01-037 Pristine crack 01-037 Oct Pre BL BT = 7.2 01-037 After B6 BT = 2.4 01-037 Oct BL BT = 6.1 01-037 After B6

Mechanical Cleaning Methods Continue maximum allowable PMB pressure of 40 psi Wet glass bead, Al 2 0 3 240 and 320 grit processes should not be used on parts that will undergo FPI Al 2 0 3 500 grit, walnut shell blast, and PMB are all effective cleaning methods for removal of surface contamination Recommend that all mechanical blasting processes be followed by a wet process to remove residue from the blast media Mechanical methods are not effective in removing baked-on contaminants from inside the crack

Chemical Cleaning Methods Alkaline cleaners used for Ti were not found to be effective with baked-on contaminants Inconclusive as to whether related to alkaline contamination, poor cleaning, or combination Further documentation of the effect of alkaline on contamination is needed Additional cleaning methods needed for Ti The four step process for Ni parts showed the best performance Consider development of similar process for Ti Determine if lack of performance for the one-step alkaline process and the alkaline gel process was related to alkaline contamination or ineffective cleaning

Ti Cleaning Study Evaluation Based on Phase I results which indicated problems with cleaning of Ti, initiated incremental cleaning study Determine hot water rinse (150F or greater) of at least 15 minutes provides better FPI performance Efforts underway to modify engine SOP documents

Adequate cleaning methods exist for nickel components Chemical cleaning of titanium should be followed by a hot water rinse of 150F and 15 minutes Changes to allowable mechanical cleaning methods are warranted given the reductions in FPI response and surface changes Full report available at: http://actlibrary.tc.faa.gov Conclusions