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TURBINE ENGINE CLEANER

YELLOW/GREEN
|
CLEANERS
|
PTC-2003C
PTI has divested its specialty coatings and solvents, including the PTI and Certified Coatings product lines, to SOCOMORE. Click here for more details on the acquisition, click here to place an order or register, or reach out directly at csr-na@socomore.com.
PTC-2003C
TURBINE ENGINE CLEANER

TURBINE ENGINE CLEANER
Part Number: PTC-2003C
Military Specification: MIL-PRF-85704C TYII & TYIII

PTC-2003C is the concentrate version of PTI’s Turbine engine gas path cleaner  MIL-PRF-85704C TYII & TYIII. This product has been formulated as an aqueous cleaner, concentrate for “off-line” (crank wash) and “on-line” (fired wash) cleaning of turbine engines. This cleaner also works well with prop engines. THIS IS A COMPLETELY 0 VOC CLEANER.

PRODUCT SPECIFICATIONS
PTI PART NUMBER
PTC-2003C
PRODUCT TYPE:
CLEANERS
COLOR:
YELLOW/GREEN
BMS SPECIFICATION:
None
MIL-SPEC:
MIL-PRF-85704C TYII & TYIII
OTHER SPECIFICATIONS
None
UNIT SIZE
None

Extended Description

No items found.

PT-402 Acid Etching Primer, when properly reduced with PT-1045 Reducer, meets and exceeds MIL-C-8514C.PT-402 is a polyvinyl butyral zinc chromate formulation that may be used to prime all plain or plated metallic surfaces. Priming surfaces with PT-402 Acid Etching Primer prior to priming with epoxy primer MIL-PRF23377or by itself will ensure maximum adhesion and protection of all bake or air-dry finish coats (including lacquerfinish coats). The finely ground emulsions of zinc chromate pigments, resins and phosphoric acid hardeners are virtually non-settling. Once applied, the Acid Etching Primer requires no sanding and has a pot life of 8 hours. Extreme humidity can affect the bonding of the coating.

SPECIFICATIONS

  • DOD-P-15328D
  • MIL-C-8514C / PT-1045 Reducer

COLORS

This coating can be provided Yellow and Green.

COATING PROPERTIES & CHARACTERISTICS

  • Mix Ratio: by volume 4 part Base to 1 part Catalyst by volume
  • Reducer: PTI-1045 reduce, 1 part paint to 2 – 3 parts reducer
  • Recommended Dry Film Thickness: 0.2 mil
  • Admixed Viscosity: 14 seconds, max #4 Ford
  • Admixed Weight: per Gallon 11.5 lbs.
  • Theoretical Coverage: 1600 sq. ft.²/gal.Pot Life 8 hoursCoatings VOC Below 340 g/L

SHELF LIFE

Shelf life is only applicable for materials stored in unopened and undamaged original factory filled containers.1 year when stored between 50⁰-85⁰ Fahrenheit.

SURFACE PREPARATION INSTRUCTIONS

  • Scuff the surface with scotch bright pads.
  • Dust off the surface with an air hose and wand.
  • Wipe of the substrate with IPA or Acetone to remove grime and oils
  • Remove all remaining dust and debris by lightly wiping the substrate with a tack or “cheese” cloth

MIXING INSTRUCTIONS

  • Shake component A in a paint shaker for 5 – 10 minutes for optimal results.
  • Admix by volume:
  • 1. Stir or shake both component “A” and “B” well before mixing
  • 2. Add 4 parts of Component “A” to 1 part of Component “B” by volume and stir thoroughly. Stir each well before mixing.
  • 3. Reduce with PT-1045. Dilution ratio is 1 part admixed primer to 2 – 3 parts PT-1045.4. Mix only an amount that can be used in one day.

APPLICATION

This product can be applied using conventional air spray equipment, HVLP spray system. Please consult with a PTI representative for specific equipment recommendations and settings.

  • 1. Make sure pots, guns, and lines are purged and cleaned.
  • 2. Mix both base and catalyst thoroughly and filter/strain before spray application.
  • 3. HVLP Spray Pressure: 7-10psi. Convention spray equipment 15-30psi
  • 4. Always air-blow and tack wipe the surfaces to be painted. Aircraft should be grounded to prevent static.
  • 5. Best application results: apply 1 fog/tack coat at 0.2 mil thickness.
  • 6. Recommended Dry Film Thickness is 0.2 mils.

NOTE: Application of PTI products requires the use of all OSHA approved safety equipment, including proper ventilation. Additionally, PTI products require the recommended temperature/humidity conditions and film thickness ranges for optimal performance. The material, hangar, and aircraft skin temperatures should be no lower than 75⁰ F / 25⁰ C before, during and after application.DRYING & CURING SCHEDULEDry times are based on the dry film thickness of 0.2 mils (25-50 microns).

Product Data Sheet & Safety Data Sheet Unavailable Online For This Product
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