Except as provided in paragraph (1), this section
applies to the manufacture or rework of commercial, civil or military aerospace
vehicles or components at any facility which has the potential to emit 25 tons
per year of VOCs or more.
(1) This
section does not apply to cleaning and coating of aerospace components and
vehicles as follows:
(i) At any source
conducting research and development for the research and development
activities.
(ii) For quality
control and laboratory testing.
(iii) For production of electronic parts and
assemblies (except for cleaning and coating of completed assemblies).
(iv) For rework operations performed on
antique aerospace vehicles or components.
(2) Paragraph (3) does not apply to cleaning
and coating of aerospace components and vehicles in the following
circumstances:
(i) The use of touchup,
aerosol and Department of Defense "classified" coatings.
(ii) The coating of space vehicles.
(iii) At facilities that use separate
formulations in volumes less than 50 gallons per year to a maximum exemption of
200 gallons per year of all the coatings in aggregate for these
formulations.
(3)
Beginning April 10, 1999, a person may not apply to aerospace vehicles or
components, aerospace specialty coatings, primers, topcoats and chemical
milling maskants including VOC-containing materials added to the original
coating supplied by the manufacturer, that contain VOCs in excess of the limits
specified in Table II.
(i) Aerospace coatings
that meet the definitions of the specific coatings in Table II shall meet those
allowable coating VOC limits.
(ii)
All other aerospace primers, aerospace topcoats and chemical milling maskants
are subject to the general coating VOC limits for aerospace primers, aerospace
topcoats and aerospace chemical milling maskants.
TABLE IIAllowable Content of VOCs in Aerospace
Coatings
Weight of VOC Per Volume of Coating (Minus Water
and Exempt Solvents)
|
LIMIT
|
|
COATING TYPE
|
POUNDS PER GALLON
|
GRAMS PER LITER
|
| Specialty Coatings |
| (1) Ablative Coating |
5.0 |
600 |
| (2) Adhesion Promoter |
7.4 |
890 |
| (3) Adhesive Bonding Primers: |
| (a) Cured at 250°F or below |
7.1 |
850 |
| (b) Cured above 250°F |
8.6 |
1,030 |
| (4) Adhesives: |
| (a) Commercial Interior Adhesive |
6.3 |
760 |
| (b) Cyanoacrylate Adhesive |
8.5 |
1,020 |
| (c) Fuel Tank Adhesive |
5.2 |
620 |
| (d) Nonstructural Adhesive |
3.0 |
360 |
| (e) Rocket Motor Bonding Adhesive |
7.4 |
890 |
| (f) Rubber-Based Adhesive |
7.1 |
850 |
| (g) Structural Autoclavable Adhesive |
0.5 |
60 |
| (h) Structural Nonautoclavable Adhesive |
7.1 |
850 |
| (5) Antichafe Coating |
5.5 |
660 |
| (6) Chemical Agent-Resistant Coating |
4.6 |
550 |
| (7) Clear Coating |
6.0 |
720 |
| (8) Commercial Exterior Aerodynamic Structure
Primer |
5.4 |
650 |
| (9) Compatible Substrate Primer |
6.5 |
780 |
| (10) Corrosion Prevention Compound |
5.9 |
710 |
| (11) Cryogenic Flexible Primer |
5.4 |
645 |
| (12) Cryoprotective Coating |
5.0 |
600 |
| (13) Electric or Radiation-Effect Coating |
6.7 |
800 |
| (14) Electrostatic Discharge and Electromagnetic
Interference (EMI) Coating |
6.7 |
800 |
| (15) Elevated Temperature Skydrol Resistant
Commercial Primer |
6.2 |
740 |
| (16) Epoxy Polyamide Topcoat |
5.5 |
660 |
| (17) Fire-Resistant (Interior) Coating |
6.7 |
800 |
| (18) Flexible Primer |
5.4 |
640 |
| (19) Flight-Test Coatings: |
| (a) Missile or Single Use Aircraft |
3.5 |
420 |
| (b) All Other |
7.0 |
840 |
| (20) Fuel-Tank Coating |
6.0 |
720 |
| (21) High-Temperature Coating |
7.1 |
850 |
| (22) Insulation Covering |
6.2 |
740 |
| (23) Intermediate Release Coating |
6.2 |
750 |
| (24) Lacquer |
6.9 |
830 |
| (25) Maskants: |
| (a) Bonding Maskant |
10.2 |
1,230 |
| (b) Critical Use and Line Sealer Maskant |
8.6 |
1,020 |
| (c) Seal Coat Maskant |
10.2 |
1,230 |
| (26) Metallized Epoxy Coating |
6.2 |
740 |
| (27) Mold Release |
6.5 |
780 |
| (28) Optical Anti-Reflective Coating |
6.2 |
750 |
| (29) Part Marking Coating |
7.1 |
850 |
| (30) Pretreatment Coating |
6.5 |
780 |
| (31) Rain Erosion-Resistant Coating |
7.1 |
850 |
| (32) Rocket Motor Nozzle Coating |
5.5 |
660 |
| (33) Scale Inhibitor |
7.3 |
880 |
| (34) Screen Print Ink |
7.0 |
840 |
| (35) Sealants: |
| (a) Extrudable/Rollable/Brushable Sealant |
2.0 |
240 |
| (b) Sprayable Sealant |
5.0 |
600 |
| (36) Self-Priming Topcoat |
3.5 |
420 |
| (37) Silicone Insulation Material |
7.1 |
850 |
| (38) Solid Film Lubricant |
7.3 |
880 |
| (39) Specialized Function Coating |
7.4 |
890 |
| (40) Temporary Protective Coating |
2.7 |
320 |
| (41) Thermal Control Coating |
6.7 |
800 |
| (42) Wet Fastener Installation Coating |
5.6 |
675 |
| (43) Wing Coating |
7.1 |
850 |
| Aerospace Primers, Aerospace Topcoats and
Aerospace Chemical Milling Maskants |
| (1) Primers |
2.9 |
350 |
| (2) Topcoats |
3.5 |
420 |
| (3) Chemical Milling Maskants (Type I/II) |
1.3 |
160 |
(4) The mass of VOC per combined volume of
VOC and coating solids, less water and exempt compounds shall be calculated for
each coating by the following equation:
Click to view image
Where:
VOC = VOC content in grams per liter (g/l) of each
coating less water and exempt solvents,
Wv = Weight of total volatiles,
% (100%-Weight % Nonvolatiles),
Ww = Weight of water,.
Wex = Weight of exempt
solvent,.
Dc = Density of coating, g/l at
25°C,
Dw = Density of water, 0.997 x
103 g/l at 25°C, and
Dex = Density of exempt solvent,
g/l, at 25°C.
To convert from grams per liter (g/l) to pounds per
gallon (lb/gal), multiply the result (VOC content) by 8.345 x
103 (lb/gal/g/l).
(5) Except as provided in paragraph (6),
beginning April 10, 1999, a person shall use one or more of the following
application techniques in applying primer or topcoat to aerospace vehicles or
components:
(i) Flow/curtain coat.
(ii) Dip coat.
(iii) Roll coating.
(iv) Brush coating.
(v) Cotton-tipped swab application.
(vi) Electrodeposition (DIP)
coating.
(vii) High volume low
pressure (HVLP) spraying.
(viii)
Electrostatic spray.
(6)
The following situations are exempt from application equipment requirements
listed in paragraph (5):
(i) Any situation
that normally requires the use of an airbrush or an extension on the spray gun
to properly apply coatings to limited access spaces.
(ii) The application of specialty
coatings.
(iii) The application of
coatings that contain fillers that adversely affect atomization with HVLP spray
guns and that the applicant has demonstrated and the Department has determined
cannot be applied by any of the application methods specified in paragraph
(5).
(iv) The application of
coatings that normally have a dried film thickness of less than 0.0013
centimeter (0.0005 in.) when the applicant has demonstrated and the Department
has determined cannot be applied by any of the application methods specified in
paragraph (5).
(v) The use of
airbrush application methods for stenciling, lettering and other identification
markings.
(vi) The use of hand-held
spray can application methods.
(vii) Touch-up and repair
operations.
(7) Except as
provided in paragraph (8), beginning April 10, 1999, a person may not use
solvents for hand-wipe cleaning of aerospace vehicles or components unless the
cleaning solvents do one of the following:
(i)
Meet the definition of "aqueous cleaning solvent" in §
121.1 (relating to
definitions).
(ii) Have a VOC
composite vapor pressure less than or equal to 45 millimeters (mmHg) at
20°C.
(iii) Is composed of a
mixture of VOCs and has a maximum vapor pressure of 7 millimeters (mmHg) at
20°C (3.75 inches water at 68°F) and contains no hazardous air
pollutants (HAP) or ozone depleting compounds.
(8) The following aerospace vehicle and
component solvent cleaning operations are exempt from paragraph (7):
(i) Cleaning during the manufacture,
assembly, installation, maintenance or testing of components of breathing
oxygen systems that are exposed to the breathing oxygen.
(ii) Cleaning during the manufacture,
assembly, installation, maintenance or testing of parts, subassemblies or
assemblies that are exposed to strong oxidizers or reducers (for example,
nitrogen tetroxide, liquid oxygen, hydrazine).
(iii) Cleaning and surface activation prior
to adhesive bonding.
(iv) Cleaning
of electronics parts and assemblies containing electronics parts.
(v) Cleaning of aircraft and ground support
equipment fluid systems that are exposed to the fluid, including air-to-air
heat exchangers and hydraulic fluid systems.
(vi) Cleaning of fuel cells, fuel tanks and
confined spaces.
(vii) Surface
cleaning of solar cells, coated optics and thermal control surfaces.
(viii) Cleaning during fabrication, assembly,
installation and maintenance of upholstery, curtains, carpet and other textile
materials used in or on the interior of the aircraft.
(ix) Cleaning of metallic and nonmetallic
materials used in honeycomb cores during the manufacture or maintenance of
these cores, and cleaning of the completed cores used in the manufacture of
aerospace vehicles or components.
(x) Cleaning of aircraft transparencies,
polycarbonate or glass substrates.
(xi) Cleaning and solvent usage associated
with research and development, quality control or laboratory testing.
(xii) Cleaning operations, using nonflammable
liquids, conducted within 5 feet of any alternating current (AC) or direct
current (DC) electrical circuit on an assembled aircraft once electrical power
is connected, including interior passenger and cargo areas, wheel wells and
tail sections.
(xiii) Cleaning
operations identified in an essential use waiver under section 604(d)(1) of the
Clean Air Act (42 U.S.C.A.
§
7671c(d)(1)) or a
fire suppression or explosion prevention waiver under section 604(g)(1) of the
Clean Air Act which has been reviewed and approved by the EPA and the voting
parties of the International Montreal Protocol Committee.
(9) Cleaning solvents, except for semiaqueous
cleaning solvents, used in the flush cleaning of aerospace vehicles,
components, parts, and assemblies and coating unit components, shall be emptied
into an enclosed container or collection system that is kept closed when not in
use or captured with wipers which comply with the housekeeping requirements of
paragraph (11). Aqueous cleaning solvents are exempt from these
requirements.
(10) Spray guns used
to apply aerospace coatings shall be cleaned by one of the following:
(i) An enclosed spray gun cleaning system
that is kept closed when not in use. Leaks, including visible leakage, misting
and clouding, shall be repaired within 14 days from when the leak is first
discovered. Each owner or operator using an enclosed spray gun cleaner shall
visually inspect the seals and all other potential sources of leaks at least
once per month. The results of each inspection shall be recorded, and the
record shall indicate the date of the inspection, the person who conducted the
inspection and whether components were leaking. Records of the inspections
shall be maintained for at least 2 years. Each inspection shall occur while the
spray gun cleaner is in operation. If the leak is not repaired by the 15th day
after detection, the solvent shall be removed and the enclosed cleaner shall be
shut down until the leak is repaired or its use is permanently
discontinued.
(ii) Unatomized
discharge of solvent into a waste container that is kept closed when not in
use.
(iii) Disassembly of the spray
gun and cleaning in a vat that is kept closed when not in use.
(iv) Atomized spray into a waste container
that is fitted with a device designed to capture atomized solvent
emissions.
(11) The owner
or operator of an affected facility shall implement the following housekeeping
measures for cleaning solvents:
(i) Fresh and
used cleaning solvents, except aqueous and semiaqueous cleaning solvents, used
in solvent cleaning operations shall be stored in nonabsorbent, nonleaking
containers. The containers shall be kept closed at all times except when
filling or emptying.
(ii) Cloth and
paper, or other absorbent applicators, moistened with cleaning solvents, except
aqueous cleaning solvents, shall be stored in closed, nonabsorbent, nonleaking
containers. Cotton-tipped swabs used for very small cleaning operations are
exempt.
(iii) Handling and transfer
procedures shall minimize spills during filling and transferring the cleaning
solvent, except aqueous cleaning solvents, to or from enclosed systems, vats,
waste containers and other cleaning operation equipment that holds or stores
fresh or used cleaning solvents.
(12) The owner or operator of an affected
facility may comply with this section by using approved air pollution control
equipment provided that the following exist:
(i) The control system has combined VOC
emissions capture and control equipment efficiency of at least 81% by
weight.
(ii) The owner or operator
received approval from the Department of a monitoring plan that specifies the
applicable operating parameter value, or range of values, to ensure ongoing
compliance with this section. The monitoring device shall be installed,
calibrated, operated and maintained in accordance with the manufacturer's
specifications, good air pollution control practices that minimize VOC
emissions, and the Department's approval.
(iii) The owner or operator shall record
monitoring parameters as specified in the approved monitoring plan.
(13) The owner or operator of an
affected facility shall maintain records in accordance with §§
129.51 and
129.52 (relating to general; and
surface coating processes) including:
(i) A
current list of coatings in use categorized in accordance with Table II showing
VOC content as applied and usage on an annual basis.
(ii) A current list of cleaning solvents used
and annual usage for hand wiping solvents including the water content of
aqueous and semiaqueous solvents and the vapor pressure and composite vapor
pressure of all vapor pressure compliant solvents and solvent blends.
(iii) A current list and annual usage
information for exempt hand-wipe cleaning solvents with a vapor pressure
greater than 45 millimeters of mercury (mmHg) used in exempt hand-wipe cleaning
operations.