Aircraft Corrosion During Depaint Operations - PowerPoint PPT Presentation

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Aircraft Corrosion During Depaint Operations

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Pitting noted on wings and fuselage during routine depaint operations ... 4. Galvanic interaction between wing skin and steel rivets. May 2004 ... – PowerPoint PPT presentation

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Title: Aircraft Corrosion During Depaint Operations


1
Aircraft Corrosion During Depaint Operations
  • Presented By
  • C.S. Brossia, N. Sridhar, J.F. Dante, M. Dammann
  • Southwest Research Institute
  • San Antonio, TX

2
Background
  • Pitting noted on wings and fuselage during
    routine depaint operations
  • Root cause not obvious based on visual inspection
  • no apparent order (random)
  • found on clad and unlcad material
  • What is the cause?

3
Possible Causes of Pitting
  • 1. Pits existed prior to paint stripping from
    prior exposure/damage to coating
  • 2. Excessive stripper dwell time or by prior
    surface contamination by salts/corrosive agents
  • 3. High chloride and/or sulfate in rinse/dilution
    waters
  • 4. Galvanic interaction between wing skin and
    steel rivets

4
Approach - Panel Preparation
  • AA2014-T6, Clad AA2024-T3
  • Environmentally Friendly Oxidizing Acidic
    Stripper, Standard Alkaline Wash (301), Standard
    Brightener (31)
  • Replicate panels to gage variability
  • Painting performed at Kenedy Aircraft Inc
  • Alodine
  • Primer
  • Polyurethane Primer
  • Top Coat (White)
  • Aging Air dry for 1 week, 4 day bake at 210 F

5
Detectability of Pre-Existing Pits
  • Determine if pits (if present) could be detected
    during pre-strip inspection
  • Approach
  • Clad and unclad panels
  • Some with pinholes/scribes in coating (damage)
  • Exposure cyclic salt spray environment

6
Detectability of Pre-Existing Pits
  • No significant coating delamination/creep back at
    pinhole/scribe
  • Conclusion pits unlikely to have been present
    prior to stripping without detection during
    pre-depaint inspection

7
Excessive Stripper Dwell Time
  • Determine if long surface dwell time for acid
    stripper led to pitting
  • Approach
  • Subject panels to recommended 4 hr stripper time
    and for longest time experienced by aircraft (24
    hr)
  • Examine panels after stripping

8
Excessive Stripper Dwell Time
  • Conclusions
  • 4 h stripper time inadequate
  • 24 h better
  • No effect on corrosion/pitting noted

9
Dwell Time Contamination
  • Determine if long surface dwell time for acid
    stripper in combination with pre-existing surface
    contamination led to pitting
  • Approach
  • Prior to stripping, apply salt spray to painted
    panels
  • Subject panels to 4 and 24 hr stripper time
  • Examine panels after stripping

10
Dwell Time Contamination
  • No massive corrosion noted
  • 2-4 micron 0.08 - 0.16 mil pits noted after 24
    h stripping w/ prior salt contamination

11
Dwell Time Contamination
  • Pitting also noted with contaminated stripper on
    unpainted panels
  • Known to be a problem (NACE/SSPC committee)
  • Conclusion prior surface contaminants may have
    caused pitting
  • Recommendation washdown prior to stripping

12
Rinse/Dilution Water Chemistry
  • Determine if rinse/dilution water chemistry led
    to pitting
  • Approach
  • Examine two main water chemistries DI and
    simulated tap water (330 ppm chloride 180 ppm
    sulfate)
  • Look for differences in surface appearance
    resulting from different water chemistries used
    for rinse and/or dilution
  • Interactions between water chemistry and
    brightener and alkaline wash also examined

13
Rinse/Dilution Water Chemistry
  • 4 hr stripper dwell time

Alkaline Wash DI Brightener DI Rinse Water DI
Alkaline Wash ST Brightener DI Rinse Water DI
14
Rinse/Dilution Water Chemistry
  • 4 hr stripper dwell time

Alkaline Wash DI Brightener ST Rinse Water DI
Alkaline Wash DI Brightener DI Rinse Water ST
15
Rinse/Dilution Water Chemistry
22 4 hr stripper dwell time w/ 4 day delay
prior to alkaline wash (effective stripping
operation)
  • 4 hr stripper dwell time

Alkaline Wash ST Brightener ST Rinse Water ST
Alkaline Wash ST Brightener ST Rinse Water ST
16
Rinse/Dilution Water Chemistry
clad
unclad
  • With long stripper time and tap water, 3-7 micron
    0.12 - 0.28 mils pits noted on both clad and
    unclad
  • Conclusion
  • long stripper time along with high chloride and
    sulfate in tap water likely cause

17
Effect of Stripper Sequence
  • 22 4 hr stripper dwell time with and without
    delay

Alkaline Wash DI Brightener DI Rinse Water
DI 4-Day Delay Yes
Alkaline Wash DI Brightener DI Rinse Water
DI 4-Day Delay No
  • Conclusion delay in sequence does not cause
    pitting long stripper time along with high
    chloride and sulfate in tap water most likely
    cause

18
Rinse/Dilution Water Chemistry
  • Conclusions
  • Long stripper time along with high chloride and
    sulfate in tap water may have caused pitting
  • Dwell time along not sufficient to induce pitting
  • Recommendation use rinse waters low in
    dissolved salts or include additive

19
Summary and Conclusions
  • Based on Work Conducted
  • Pits unlikely to have already existed prior to
    stripping
  • Contamination prior to stripper application may
    have caused pitting
  • Long stripper times in combination with delay
    between stripping and alkaline wash along with
    high chloride and sulfate in tap water most
    likely to have caused pitting

20
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