Mo. Code Regs. Ann. tit. 10, § 10-5.295
PURPOSE: This rulemaking will reduce volatile organic compound emissions from aerospace manufacture and/or rework facilities located in the St. Louis nonattainment area. This rulemaking is required to comply with the Clean Air Act Amendments of 1990.
PUBLISHER’S NOTE: The publication of the full text of the material that the adopting agency has incorporated by reference in this rule would be unduly cumbersome or expensive. Therefore, the full text of that material will be made available to any interested person at both the Office of the Secretary of State and the office of the adopting agency, pursuant to section 536.031.4, RSMo. Such material will be provided at the cost established by state law.
(1) Applicability.
(2) Definitions.
(A) Definitions of individual specialty coatings specified in this rule are incorporated by reference from 40 CFR 63 subpart GG, Appendix A, with the following modifications:
mold surface to prevent the mold piece from sticking to the mold as it is removed, or to an aerospace component for purposes of creating a form-in-place seal; and
A semi-solid material that is used to aerodynamically smooth exterior vehicle surfaces or fill cavities such as bolt hole accesses. A material shall not be classified as a caulking and smoothing compound if it can be classified as a sealant.
used for corrosion prevention, protection from the environment, functional fluid resistance, and adhesion of subsequent coatings. Primers that are defined as specialty coatings are not included under this definition.
(1) layer of identical coating formulation may be applied to the vehicle or component.
(3) General Provisions.
(A) No person shall cause, permit, or allow the emissions of volatile organic compounds (VOC) from the coating of aerospace vehicles or components to exceed—
liter) of coating, excluding water and exempt solvents, delivered to a coating applicator that applies primers. For general aviation rework facilities, the VOC limitation shall be 4.5 10 CSR 10-5
pounds per gallon of coating, excluding water and exempt solvents, delivered to a coating applicator that applies primers;
liter) of coating, excluding water and exempt solvents, delivered to a coating applicator that applies topcoats (including self-priming topcoats). For general aviation rework facilities, the VOC limit shall be 4.5 pounds per gallon (540 grams per liter) of coating, excluding water and exempt solvents, delivered to a coating applicator that applies topcoats (including self-priming topcoats);
Table I expressed in pounds per gallon of coating, excluding water and exempt solvents, delivered to a coating applicator that applies specialty coatings; Adhesives: Commercial Interior Adhesive Cyanoacrylate Adhesive Fuel Tank Adhesive Nonstructural Adhesive Rocket Motor Bonding Adhesive Rubber-Based Adhesive 6.3 760 8.5 1020 5.2 620 3.0 360 7.4 890 7.1 850 applies Type II chemical milling maskants.
(B) The emission limitations in paragraph (3)(A)1. of this rule shall be achieved by—
technology where each and every coating meets the specified applicable limitation
ating procedures, and/or the manufacturer’s
| Rain Erosion-Resistant Coating | 7.1 | 850 | 7. High volume low pressure (HVLP) | ||||||
|---|---|---|---|---|---|---|---|---|---|
| Rocket Motor Nozzle Coating | 5.5 | 660 | spraying; | ||||||
| Scale Inhibitor | 7.3 | 880 | 8. Electrostatic spray application; or | ||||||
| Screen Print Ink | 7.0 | 840 | 9. Other coating application methods | ||||||
| Sealants: | that achieve emission reductions equivalent to | ||||||||
| Extrudable/Rollable/Brushable Sealant | 2.3 | 280 | HVLP | or | electrostatic | spray | application | ||
| Sprayable Sealant | 5.0 | 600 | methods, as determined by the director. | ||||||
| Silicone Insulation Material | 7.1 | 850 | (D) | Each | owner | or | operator | of | an |
| Solid Film Lubricant | 7.3 | 880 | aerospace manufacturing and/or rework oper- | ||||||
| Specialized Function Coating | 7.4 | 890 | ation shall ensure that all application devices | ||||||
| Temporary Protective Coating | 2.7 | 320 | used to apply primers and topcoats (including | ||||||
| Thermal Control Coating | 6.7 | 800 | self-priming topcoats) are operated according | ||||||
| Wet Fastener Installation Coating | 5.6 | 675 | to company procedures, local specified oper- | ||||||
| Wing Coating | 7.1 | 850 |
| system has a VOC reduction efficiency of | |||||||||
|---|---|---|---|---|---|---|---|---|---|
| High-Temperature Coating | 7.1 | 850 | eighty-one percent (81%) or greater. | ||||||
| Insulation Covering | 6.2 | 740 | (C) | Each | owner | or | operator | of | an |
| Intermediate Release Coating | 6.3 | 750 | aerospace manufacturing and/or rework oper- | ||||||
| Lacquer | 6.9 | 830 | ation shall apply all non-exempt primers and | ||||||
| Maskant: | topcoats using one (1) or more of the appli- | ||||||||
| Bonding Maskant | 10.3 | 1230 | cation techniques specified below— | ||||||
| Critical Use and Line Sealer Maskant | 8.5 | 1020 | |||||||
| 1. Flow/curtain application; | |||||||||
| Seal Coat Maskant | 10.3 | 1230 | |||||||
| 2. Dip coat application; | |||||||||
| Metallized Epoxy Coating | 6.2 | 740 | |||||||
| Mold Release | 6.5 | 780 | 3. Roll coating; | ||||||
| Optical Anti-Reflective Coating | 6.3 | 750 | 4. Brush coating; | ||||||
| Part Marking Coating | 7.1 | 850 | 5. Cotton-tipped swab application; | ||||||
| Pretreatment Coating | 6.5 | 780 | 6. Electrodeposition (dip) coating; | ||||||
| Rain Erosion-Resistant Coating | 7.1 | 850 | 7. High volume low pressure (HVLP) |
| exempt solvents, stated in subsection (3)(A) | |||
|---|---|---|---|
| Cryogenic Flexible Primer | 5.4 | 645 | |
| of this rule; averaging is not allowed for spe- | |||
| Cryoprotective Coating | 5.0 | 600 | |
| cialty coatings, and averaging is not allowed | |||
| Dry Lubricative Material | 7.3 | 880 | |
| between primers, topcoats (including self- | |||
| Electric or Radiation-Effect Coating | 6.7 | 800 | |
| priming topcoats), Type I milling maskants, | |||
| Electrostatic Discharge and Electromagnetic Interference | |||
| (EMI) Coating | 6.7 | 800 | and Type II milling maskants or any combi- |
| Elevated Temperature Skydrol Resistant Commercial Primer | 6.2 | 740 | nation of the above coating categories; or |
| Epoxy Polyamide Topcoat | 5.5 | 660 | 3. Control equipment, including but not |
| Fire-Resistant (interior) Coating | 6.7 | 800 | limited to incineration, carbon adsorption |
| Flexible Primer | 5.3 | 640 | and condensation, with a capture system |
| Flight-Test Coatings: | approved by the director, provided that the | ||
| Missile or Single Use Aircraft | 3.5 | 420 | owner or operator demonstrates, in accor- |
| All Others | 7.0 | 840 | dance with subsection (5)(C), that the control |
| Fuel-Tank Coating | 6.0 | 720 | system has a VOC reduction efficiency of |
| Structural Autoclavable Adhesive | 0.5 | 60 | expressed in pounds of VOC per gallon of | ||||
|---|---|---|---|---|---|---|---|
| Structural Nonautoclavable Adhesive | 7.1 | 850 | coating, excluding water and exempt solvents, | ||||
| Antichafe Coating | 5.5 | 660 | stated in subsection (3)(A) of this rule; | ||||
| Bearing Coating | 5.2 | 620 | 2. The application of low solvent coating | ||||
| Caulking and Smoothing Compounds | 7.1 | 850 | technology | where | the | monthly | volume- |
| Chemical Agent-Resistant Coating | 4.6 | 550 | weighted average VOC content of each speci- | ||||
| Clear Coating | 6.0 | 720 | fied coating type meets the specified applica- | ||||
| Commercial Exterior Aerodynamic Structure Primer | 5.4 | 650 | ble limitation expressed in pounds of VOC | ||||
| Compatible Substrate Primer | 6.5 | 780 | per gallon of coating, excluding water and | ||||
| Corrosion Prevention Compound | 5.9 | 710 |
| Pounds per Grams per | 4. 5.2 pounds per gallon (620 grams per | ||
|---|---|---|---|
| Table I: Specialty Coating VOC Limitations | |||
| gallon | liter | liter) of coating, excluding water and exempt | |
| Ablative Coating | 5.0 | 600 | solvents, delivered to a coating applicator that |
| Adhesion Promoter | 7.4 | 890 | applies Type I chemical milling maskant; and |
| Adhesive Bonding Primers: | 5. 1.3 pounds per gallon (150 grams per | ||
| Cured at 250°F or below | 7.1 | 850 | liter) of coating, excluding water and exempt |
| Cured above 250°F | 8.6 | 1030 | |
| solvents, delivered to a coating applicator that |
Specific to the St. Louis Metropolitan Area
specifications, whichever is most stringent, at all times. Equipment modified by the owner or operator shall maintain a transfer efficiency equivalent to HVLP or electrostatic spray application techniques.
(E) Each owner or operator of an aerospace manufacturing and/or rework operation shall comply with the following housekeeping requirements for any affected cleaning operation, unless the cleaning solvent used is an aqueous cleaning solvent, low vapor pressure hydrocarbon-based cleaning solvent, or contains less than one percent (1%) VOC by weight:
other absorbent applicators used for cleaning shall be placed in bags or other closed containers upon completing their use. These bags and containers must be kept closed at all times except when depositing or removing these materials from the container. The bags and containers used must be of such a design so as to contain the vapors of the cleaning solvent. Cotton-tipped swabs used for very small cleaning operations are exempt from this requirement;
except semi-aqueous solvent cleaners, used in aerospace cleaning operations shall be stored in closed containers; and
solvent to or from enclosed systems, vats, waste containers, and other cleaning operation equipment that hold or store fresh spent cleaning solvents shall be conducted in such a manner that spills are minimized.
(F) Each owner or operator of an aerospace manufacturing and/or rework operation utilizing hand-wipe cleaning operations excluding the cleaning of spray gun equipment performed in accordance with subsection (3)(G) shall comply with one (1) of the following:
are classified as an aqueous cleaning solvent and/or a low vapor pressure hydrocarbonbased cleaning solvent; or
have a composite vapor pressure of forty-five (45) mmHg or less at twenty degrees Celsius (20°C).
(G) Each owner or operator of an aerospace manufacturing and/or rework operation shall clean all spray guns used in the application of primers, topcoats (including self-priming topcoats), and specialty coatings utilizing one or more of the following techniques:
cleaned in an enclosed system that is closed at all times except when inserting or removing the spray gun. Cleaning shall consist of forcing cleaning solvent through the gun. If leaks in the system are found, repairs shall be made as soon as practicable, but no later than fifteen (15) days after the leak was found. If the leak is not repaired by the fifteenth day after detection, the cleaning solvent shall be removed and the enclosed cleaner shall be shut down until the leak is repaired or its use is permanently discontinued;
shall be cleaned by placing cleaning solvent in the pressure pot and forcing it through the gun with the atomizing cap in place. No atomizing air is to be used. The cleaning solvent from the spray gun shall be directed into a vat, drum, or other waste container that is closed when not in use;
Spray guns shall be cleaned by disassembling and cleaning the components by hand in a vat, which shall remain closed at all times except when in use. Alternatively, the components shall be soaked in a vat, which shall remain closed during the soaking period and when not inserting or removing components; and
be cleaned by forcing the cleaning solvent through the gun and directing the resulting atomized spray into a waste container that is fitted with a device designed to capture the atomized cleaning solvent emissions.
(I) The following activities are exempt from this section:
trodeposition of paints; 10 CSR 10-5
cleaning and coating of composite parts or components that become part of an aerospace vehicle or component as well as composite tooling that comes in contact with such composite parts or components prior to cure;
except for cleaning and topcoating of completed assemblies;
cies;
and assemblies not critical to the vehicle’s structural integrity or flight performance;
space vehicles designed to travel beyond the limit of the earth’s atmosphere, including but not limited to satellites, space stations, and the space shuttle;
cialty coatings, cleaning solvents, chemical milling maskants, and strippers containing VOC at concentrations less than 0.1 percent for carcinogens or 1.0 percent for noncarcinogens;
and Department of Defense classified coatings;
aerospace vehicles and components; and
ponents if the holder of the Federal Aviation Administration design approval, or the holder’s licensee, is not actively manufacturing the aircraft or aircraft components.
(K) The following situations are exempt from the requirements of subsections (3)(D) and (3)(E):
the use of an airbrush or an extension on the spray gun to properly reach limited access spaces;
ing;
tain fillers that adversely affect atomization with HVLP spray guns and that cannot be applied by any of the application methods specified in subsection (3)(C) of this rule;
mally have dried film thickness of less than 0.0013 centimeter (0.0005 in.) and that cannot be applied by any of the application methods specified in subsection (3)(C) of this rule;
ods for stenciling, lettering, and other identification markings;
cation methods; and
(L) The following cleaning operations are exempt from the requirements of subsection (3)(F) of this rule:
assembly, installation, maintenance, or testing of components of breathing oxygen systems that are exposed to the breathing oxygen;
assembly, installation, maintenance, or testing of parts, subassemblies, or assemblies that are exposed to strong oxidizers or reducers (e.g., nitrogen tetroxide, liquid oxygen, or hydrazine);
to adhesive bonding;
assemblies containing electronic parts;
port equipment fluid systems that are exposed to the fluid including air-to-air heat exchangers and hydraulic fluid systems;
confined spaces;
ing optics, and thermal control surfaces;
bly, installation, and maintenance of upholstery, curtains, carpet, and other textile materials used in the interior of the aircraft;
materials used in honeycomb cores during the manufacture or maintenance of these cores, and cleaning of the completed cores used in the manufacture or maintenance of aerospace vehicles or components;
polycarbonate, or glass substrates;
ed with research and development, quality control, and laboratory testing;
flammable liquids, conducted within five feet (5') of energized electrical systems; and
essential uses under the Montreal Protocol for which the U.S. Environmental Protection Agency has allocated essential use allowances or exemptions.
(4) Reporting and Record Keeping.
(B) Record Keeping Requirements.
aerospace manufacture and/or rework operation that applies coatings listed in subsection (3)(A) of this rule shall—
in use with category and VOC content as applied;
on a monthly basis; and
ume-weighted average VOC content for each coating type included in averaging for coating operations that achieve compliance through coating averaging under paragraph (3)(B)2. of this rule.
aerospace manufacture and/or rework operation that uses cleaning solvents subject to this rule shall—
corresponding water contents for aqueous and semi-aqueous hand-wipe cleaning solvents;
solvents in use with their respective vapor pressure or, for blended solvents, VOC composite vapor pressure for all vapor pressure compliant hand-wipe cleaning solvents. This list shall include the monthly amount of each applicable solvent used; and
hand-wipe cleaning processes for all cleaning solvents with a vapor pressure greater than forty-five (45) mmHg used in exempt handwipe cleaning operations. This list shall include the monthly amount of each applicable solvent used.
(5) Test Methods.
(B) An owner or operator of an aerospace manufacture and/or rework operation shall determine compliance for cleaning solvents using the following:
ing solvents manufacturers’ supplied data shall be used to determine the water content; or
quired in subsection (3)(F) of this rule, manufacturers’ supplied data or standard engineering reference texts or other equivalent methods shall be used to determine the vapor pressure or VOC composite vapor pressure for blended cleaning solvents.
AUTHORITY: section 643.050, RSMo Supp. 1998.* Original rule filed July 15, 1999, effective Feb. 29, 2000. *Original authority: 643.050, RSMo 1965, amended 1972, 1992, 1993, 1995.