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Solvay UCS180 Sealant tape

    • Product Name: Solvay UCS180 Sealant tape
    • Factroy Site: Yinchuan, Ningxia, China
    • Price Inquiry: sales8@ascent-chem.com
    • Manufacturer: Ascent Petrochem Holdings Co., Limited
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    Specifications
    HS Code 874026
    Product Name Solvay UCS180 Sealant Tape
    Manufacturer Solvay
    Product Type Sealant tape
    Function Corrosion inhibition and faying surface sealing
    Cure Mechanism Non-curing
    Color Gray
    Form Tape roll
    Fuel Resistance Yes
    Chromate Content Chromate-free
    Service Temperature Range -54°C to 121°C (-65°F to 250°F)
    Shelf Life 12 months
    Storage Temperature 27°C (80°F) or below
    Qualification Standard BMS 5-95 Type II

    As an accredited Solvay UCS180 Sealant tape factory, we enforce strict quality protocols—every batch undergoes rigorous testing to ensure consistent efficacy and safety standards.

    Packing & Storage
    Packing Solvay UCS180 Sealant Tape: one 1/2 in. × 1/8 in. × 12 ft roll per pack; 12 rolls per case.
    Container Loading (20′ FCL) 20′ FCL loading: Solvay UCS180 Sealant tape on pallets; dry, ventilated container; ambient temperature; cargo secured; avoid direct sunlight and moisture.
    Shipping Solvay UCS180 Sealant Tape is normally shipped as a non-hazardous, non-regulated material. Use sealed, labeled packaging and protect from heat, moisture, and contamination. If refrigerated with dry ice, mark/label as UN1845, Carbon dioxide, solid, Class 9. Always verify the current SDS and carrier requirements.
    Storage Store Solvay UCS180 Sealant Tape in a cool, dry, well-ventilated area away from heat, sparks, open flames, and direct sunlight. Keep rolls sealed in original packaging, upright, and protected from moisture and incompatible materials. Unless the SDS specifies otherwise—such as freezer storage—maintain the manufacturer-recommended temperature, typically 5–25°C (41–77°F). Observe shelf life and first-in, first-out use.
    Shelf Life Store frozen at -18°C (0°F) or below; shelf life is typically 12 months from date of manufacture in unopened packaging.
    Application of Solvay UCS180 Sealant tape

    Solvay UCS 180 sealant tape is supplied as a one-component thermosetting corrosion-inhibiting sealant tape in controlled thickness on release paper. The downstream application scope is limited to aerospace original equipment assembly and maintenance, repair, and overhaul where the tape is placed into faying surfaces, fastener rows, fuel tank closures, composite edge details, and transparency frames before mechanical fastening and heat cure. The six application zones below are not interchangeable; each imposes distinct thickness tolerance, compression ratio, surface preparation class, and cure profile. The material is handled as a formulated B2B intermediate rather than a free-flowing liquid sealant, and downstream consumption is therefore expressed as tape thickness, width, compression percentage, and mass per joint or per linear meter.

    Table 1. Process control ranges by application zone.

    Application zoneNominal tape thicknessPost-assembly compressionProcess control limit
    Fuselage lap splice0.040 in40–50%squeeze-out < 0.50 in
    Integral fuel tank access cover0.060 in40–60%perimeter gap < 0.10 in
    Wet fastener installation0.030 in die-cut washer0.15–0.35 g per fastenercontinuous head fillet
    Composite edge sealing0.030–0.045 in0.25 in overlap onto laminate faceno exposed laminate edge
    MRO patch repair0.040–0.080 inmatch removed sealant thicknessno pinholes after cure
    Canopy or glazing frame0.040–0.060 in40–60%no transparency edge crazing

    Fuselage Lap Splice and Longitudinal Stringer Sealing

    On commercial airframe assembly lines, the tape is introduced at the skin-to-stringer interface before riveting to create a continuous corrosion-inhibiting faying surface. Industry compliance standards: the installation is controlled by AMS 3277 and MIL-PRF-81733, with lap shear verified per ASTM D1002 and salt spray resistance per ASTM B117 or ISO 9227. Addition ratio: nominal tape thickness 0.040 in is applied over a width of 0.75–1.25 in; after panel mating and riveting, compression reduces the thickness to 0.020–0.025 in, equivalent to 40–50% squeeze-out from the original tape bed. Production planning for a single-aisle fuselage splice uses approximately 1.2–1.6 lb of tape per 100 linear feet, excluding die-cut skeleton scrap. Downstream production process: the tape is slit from master rolls with a slitting tolerance of ±0.005 in, hand-laid or applied with a pressure roller at 10–20 N wheel force, and release paper is removed immediately before panel mating to reduce particulate entrapment. Panels are positioned in assembly jigs, dowel-pinned, and riveted with squeeze force controlled to produce the target thickness; squeeze-out beyond 0.50 in is rejected because it indicates overwrap or excessive tape thickness. The splice is cured in a forced-air oven at 121°C for 60 min, or during a paint bake cycle with the same temperature and dwell. Terminal finished product types: single-aisle and wide-body fuselage panels, pressure bulkheads, business jet fuselage barrels, and empennage skin splices.

    Where integral fuel tank access covers close against wing spar interfaces, the tape is installed as a continuous perimeter seal before fastener torque. Industry compliance standards: installations are governed by MIL-PRF-81733 Type II fuel tank sealant requirements, with fuel immersion testing per ASTM D471 and neutral salt spray per ISO 9227. The addition ratio for the perimeter seal is a continuous strip of 0.060 in thickness and 0.50–0.75 in width; after the cover is installed and fasteners are torqued to 25–45 in-lb, the tape compresses to 0.024–0.036 in, representing 40–60% thickness reduction. Linear consumption is approximately 1.8–2.4 g per inch of cover perimeter. Downstream production process: the spar flange is solvent-cleaned to a total hydrocarbon contamination level below 25–45 ppm before tape placement; release paper is removed, the tape is laid without gaps larger than 0.10 in, and the cover is lowered with a fixture that prevents shear slippage. Fasteners are wet-installed through the tape, torque is applied with calibrated drivers, and squeeze-out is inspected at the outer edge before cure. The tank assembly is cured at 121°C for 60 min before fuel pressure testing. Terminal finished product types: integral wing fuel tanks, fuselage fuel cells, auxiliary fuel tanks, and wing spar access doors for commercial and military transport aircraft.

    What Makes Tape Preferred Over Liquid Sealant for Wet Fastener Installation?

    Wet fastener installation shifts from liquid sealant to pre-formed tape when assembly rates require consistent placement without the static mixing, pot life, and purge variability of two-part liquid sealants. Industry compliance standards: the tape used for fastener shank and head sealing is qualified to AMS 3277 and SAE AS5127, with tensile properties per ASTM D412 and lap shear per ASTM D1002. Formulation addition ratio for fastener installation is 0.15–0.35 g of tape per fastener for 3/16 in and 1/4 in diameter fasteners, using die-cut washers or punched discs with a nominal thickness of 0.030 in and an outer diameter 2.0–2.5× the shank diameter. On wing plank and fuselage frame programs, this consumption converts to 1.5–2.2 kg of tape per 1,000 installed fasteners, including skeleton scrap from die conversion. Downstream production process: tape is converted on hollow-die presses at 20–30% relative humidity to limit static adhesion to tooling; washers are placed under fastener heads or on the shank immediately before insertion. Rivet squeeze force is maintained between 3,000–5,000 lbf for 3/16 in solid rivets to force sealant into the countersink and prevent head gapping. Installed fasteners are inspected for a continuous sealant fillet around the head. Cure follows the airframe oven cycle at 121°C for 60 min. Terminal finished product types: wing plank splices, fuselage frames, pressure bulkhead chords, floor grid attachment rows, and empennage torque box assemblies.

    After trimming and ultrasonic inspection of flight-control composite edges, the exposed laminate periphery is covered with a pre-formed moisture-barrier tape to prevent hydraulic fluid and water ingress into the core or ply stack. Industry compliance standards: the process is controlled by the airframe structural repair manual, with material substitution allowed only where the tape meets AMS 3277 or the OEM edge-seal specification; moisture resistance is evaluated under RTCA DO-160 humidity and rain test conditions when the component is an external flight surface. The addition ratio for edge sealing is a 0.030–0.045 in tape strip over-wrapped 0.25 in onto each laminate face; linear consumption is 2.5–3.2 g per meter for a 3 mm laminate edge. Downstream production process: edges are abraded with 180–240 grit, solvent-wiped to remove release agent, and hand-laid with a PTFE roller at 5–10 N force, with corner folds staggered to avoid a single overlap node. The component is vacuum bagged to consolidate the tape to the edge, then cured at 121°C for 60 min. The use of general-purpose sealing tape without fuel and hydraulic fluid resistance qualification is not acceptable on laminate edges exposed to service chemicals. Terminal finished product types: composite ailerons, rudders, elevators, winglets, radomes, and engine nacelle acoustic panels.

    When MRO Patch Repair Replaces Aged Sealant, Thickness Match Becomes the Process Control Variable

    MRO patch repair of pressurized fuselage and nacelle structure requires removal of degraded sealant tape and reapplication at the same thickness to preserve faying-surface clamp-up and load transfer. Industry compliance standards: repair instructions are issued under FAA AC 43.13-1B, Chapter 2, or the OEM structural repair manual; sealant replacement is acceptable when the new tape meets AMS 3277 class and fuel resistance requirements. Addition ratio for replacement tape is matched to the original engineering drawing, commonly 0.040–0.080 in on lap joints and 0.060 in around access panels; consumption is estimated at 1.0–1.5× the removed sealant volume to account for squeeze-out and trim scrap. Downstream production process: degraded material is removed with plastic scrapers and solvent softening, followed by aluminum surface preparation to a 0.5–1.0 mil profile; the new tape is applied only after the substrate passes water-break-free testing. Oven cure at 121°C for 60 min is used where the part can be removed; for on-aircraft repairs, heat blankets with thermocouple feedback are set to the same cure profile. Post-cure inspection includes tap hammer and feeler gauge checks for voids. Incompatibility: do not combine with uncured polysulfide remnants; sulfur contamination can interfere with the tape cure and adhesion. Terminal finished product types: repaired nacelle fan cowl panels, flap track fairings, fuselage doublers, and wing-root fillet panels.

    For pressurized defense airframe glazing and canopy frame interfaces, installation tolerances are tighter because the tape must seal without imparting stress into transparent acrylic or polycarbonate. Industry compliance standards: the installation is governed by MIL-PRF-81733 for corrosion-inhibiting sealant and MIL-STD-810 for environmental exposure, including temperature shock and rain; tensile and shear properties are verified per ASTM D412 and ASTM D1002. The addition ratio for glazing channels is a continuous 0.040–0.060 in tape strip placed in the frame channel with a width of 0.50–0.75 in; after transparency insertion and fastener torque to 15–25 in-lb, compression is held to 40–60% of original thickness. Production data show that exceeding 60% compression on thin acrylic transparencies increases the incidence of edge crazing, so torque is monitored with calibrated drivers. Downstream production process: the frame channel is primed where required by the OEM, tape is laid without stretching, and the transparency is lowered using a contour-controlled fixture to avoid shear. The assembly is heated to 121°C only when the transparency material is approved for that cure temperature; where the acrylic or polycarbonate cannot withstand 121°C, published data for this specific configuration is limited and the lower-temperature cure cycle must be validated on the glazing stack. Alcohol-based cleaners are kept away from acrylic surfaces before cure because they can induce stress crazing. Terminal finished product types: fighter aircraft canopies, helicopter windshields, crew entrance door windows, and sensor window frames.

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    Certification & Compliance
    More Introduction

    Solvay UCS180 Sealant Tape is a synthetic-rubber-based, non-silicone vacuum-bag sealant tape supplied as a continuous extruded profile on release paper. The product is used to seal nylon, polyethylene, and polyimide vacuum-bag films to aluminum, steel, and cured composite tool surfaces during vacuum-bag-only, oven, and autoclave cure cycles. The nominal continuous service temperature is 180 °C; short-term excursions above 180 °C may cause localized softening, residue transfer, and loss of seal integrity during the cooling phase. The formulation is silicone-free to limit pre-bond surface contamination after bag removal. Standard roll widths are 12.7 mm and 25.4 mm, with a nominal bead thickness of 3.2 mm. Product-specific values for tack, peel, and outgassing should be confirmed against the current Solvay UCS180 technical datasheet because independent product-specific published data for this configuration is limited. Representative values for non-silicone 180 °C-class vacuum-bag sealant tapes are listed below.

    ParameterRepresentative value or rangeTest method
    Nominal bead thickness3.2 mmCalibrated drop micrometer
    Standard roll widths12.7 mm, 25.4 mmRoll dimension
    Application temperature15 °C to 35 °CProcess specification
    Continuous service temperature-18 °C to 180 °CManufacturer thermal stability test
    Total mass loss<1.0 %; CVCM <0.1 %ASTM E595-15
    180° peel adhesion to stainless steel2.5 N/cm to 4.5 N/cmASTM D3330/D3330M-04 Method A
    Shelf life at 21 °C12 monthsManufacturer storage stability

    Lot acceptance for UCS180 typically includes measurement of bead thickness, width, initial 180° peel adhesion to stainless steel, and outgassing mass loss. Thickness is determined with a dead-weight micrometer at 21 °C. A production lot with peel adhesion below 2.0 N/cm is commonly rejected for autoclave use because it may not survive pressure cycling. Field experience indicates that moisture condensation on tool surfaces below 10 °C reduces initial tack more significantly than ordinary batch variation; therefore tooling should be brought to at least 15 °C before tape application. The synthetic-rubber matrix also shows viscoelastic recovery; after a 4-hour cure at 180 °C, the bead may retain a slight adhesive shear strength that must be overcome by peeling at an angle between 90° and 180°. Rapid peeling at low temperature is not recommended because cohesive splitting can leave residue on the tool.

    Incoming lots should also be qualified by adhesion and outgassing tests when the tape is used on certified aerospace tooling. Batch-to-batch variation in initial tack has been observed on multiple production lines; the typical corrective action is to condition the roll at 20 °C to 25 °C for 8 hours before application. Storage at 10 °C to 27 °C and 20% RH to 60% RH is recommended. Exposure to high humidity above 60% RH or prolonged ozone may oxidize the outer layer and reduce tack. REACH and RoHS declarations for the supplied formulation should be verified through the current vendor compliance certificate at lot level, particularly for export documentation.

    What limits the sealing window for UCS180 in autoclave cure cycles?

    In autoclave processing, UCS180 is subjected to simultaneous vacuum differential, external gas pressure, and tool-surface expansion. The practical upper boundary is not always the rated 180 °C service temperature; it is the cold-flow resistance of the bead under elevated pressure. As the material softens above approximately 120 °C, a 3.2 mm bead compressed by a 6 bar autoclave cycle may spread laterally beyond a narrow tool flange. If the flange width is less than 25 mm, the bead can extrude past the bag edge and reduce the contact area available to maintain vacuum during cooling. This failure mode has been recorded on production-scale autoclave tools where edge-seal leaks occur preferentially at vacuum-port pass-throughs and at sharp radii where bead thickness is reduced below 1.5 mm. In those locations, a second bead or wider overwrap tape is used to restore seal cross-section. The vacuum system should be capable of holding a pressure differential of at least 85 kPa; a pressure-decay rate greater than 34 mbar/min after initial drawdown typically indicates incomplete adhesion, tool residue, or inadequate bead thickness. Tool surfaces must be cleaned with an approved solvent such as methyl ethyl ketone or isopropyl alcohol and dried before tape application. Silicone-containing release agents must be removed because UCS180 is non-silicone; residual silicone reduces tack and creates a preferential leak path at the bag-to-tool interface. Heating ramp rates between 1 °C/min and 3 °C/min allow the bag film and sealant bead to track tool expansion without excessive displacement. Ramp rates above 5 °C/min have been associated with bag wrinkling and local sealant overcompression in thick laminate zones. During autoclave pressurization, the vent to atmosphere should remain open until the bag film is fully seated; premature closure can trap air and impose a pressure gradient across the sealant bead that exceeds its initial tack.

    Geometric analysis of a compressed 3.2 mm bead indicates that contact width increases to approximately 8 mm to 10 mm when the bead is compressed to 1.6 mm thickness. On a 25 mm flange, this leaves a residual bead margin of 15 mm to 17 mm before edge extrusion. That margin is generally sufficient for a 6 bar autoclave cycle if the tape is centered and the bag film is not shifted during vacuum drawdown. Manual centering errors on large tools have been measured at ±3 mm; therefore some facilities use 25.4 mm-wide tape on flanges narrower than 30 mm to compensate for placement variation. The bead temperature should be monitored at the tool flange on complex cure schedules because the sealant can lag the autoclave air temperature by 20 °C to 40 °C during steady ramps; this lag must not be assumed to justify sustained operation above the rated continuous service temperature.

    Because UCS180 is formulated for elevated-temperature cure cycles, it differs from general-purpose butyl tapes in cold-flow resistance, volatile content, and post-cure residue transfer. A 120 °C-class butyl sealant tape will soften excessively and may leave a tacky residue on aluminum tools after a 4-hour hold at 180 °C; UCS180 is formulated to maintain a continuous, removable bead under these conditions. Compared with silicone-based high-temperature tapes, UCS180 avoids siloxane migration that can interfere with subsequent bonding or painting operations; silicone contamination is a known cause of water-break failure and adhesive bond-line weakness on composite parts. Silicone tapes with service temperatures above 260 °C remain the appropriate choice for polyimide bagging operations above 180 °C, but their use in bonding zones should be restricted unless post-cure surface activation is performed. Relative to liquid or paste sealants applied to bag peripheries, UCS180 requires no mixing, has no pot life, and can be removed more cleanly from tool flanges. The tape form also permits rapid layups on large tooling where a continuous bead must be established before vacuum drawdown. However, the product is not intended for direct contact with fuel, hydraulic fluid, or strong mineral acids; solvent or fluid immersion can plasticize the synthetic-rubber matrix and reduce sealing force. When the bagging cycle requires contact with aggressive chemical environments, compatibility with the specific fluid should be verified under the expected time–temperature profile.

    Comparative sealant categories for vacuum-bag processing
    CategoryTypical continuous service temperatureTape formSilicone contentPrimary limitation
    General-purpose butyl tape107 °C to 120 °CExtruded tapeNoCold flow above 120 °C
    UCS180 class non-silicone high-temperature tape180 °CExtruded tapeNoNot for sustained exposure above 180 °C
    Silicone high-temperature tape260 °C to 300 °CExtruded tapeYesSiloxane contamination risk
    Liquid/paste sealantVaries by chemistryNon-tapeVariesMixing, pot life, cleanup

    Tool-side adhesion, residue boundaries, and leak-path formation

    UCS180 is applied to the tool flange as a continuous bead, then the bagging film is pressed onto the bead with a hand roller or rounded squeegee. Tool-side adhesion is influenced by substrate roughness and surface energy. On aluminum tooling with a surface finish of 0.8 µm Ra to 1.6 µm Ra, mechanical interlock contributes to initial tack; on polished steel or epoxy tooling with lower roughness, adhesion relies more on the viscoelastic response of the synthetic-rubber matrix. A minimum application temperature of 15 °C is recommended because cold tape exhibits reduced conformability and may fail to fill tool-surface microgrooves. At temperatures above 35 °C, the bead may become overly soft and difficult to handle without stretching or thinning. The release paper should be removed without tensioning the tape to avoid reducing the cross-section below the nominal 3.2 mm thickness. Joints between successive tape lengths should be overlapped by 20 mm to 25 mm and rolled firmly; butt joints are not acceptable on autoclave cycles because they create a direct leak path. For vacuum ports and thermocouple pass-throughs, the bead is split or pierced, and the penetration is sealed with a secondary patch of UCS180 rather than with silicone putty. This practice maintains the non-silicone boundary of the bagging system. After cure, residue transfer is evaluated by visual inspection and water-break testing per ASTM F22-13. If residue remains on the tool flange, it can be removed with methyl ethyl ketone or a manufacturer-approved cleaning agent; abrasive pads are not recommended on polished tool surfaces because scratching creates leak-prone topography. The operational boundary for UCS180 is defined by the combination of vacuum level, temperature, pressure, and tool-flange width; at 180 °C and 6 bar, a flange width below 25 mm may require a wider tape or a secondary tacky bead.

    When lower-temperature bagging films require a sealant with reduced cold flow

    In oven-cure cycles where nylon bagging film is used and the maximum part temperature remains below 120 °C, a lower-temperature butyl tape may be sufficient and may leave less residue on unheated tool flanges. UCS180 becomes the preferred sealing medium when the cure cycle exceeds 120 °C or when the tooling is subjected to multiple consecutive hot cycles. Polyimide bagging films, which are used up to 400 °C, transfer more heat to the sealant bead at the flange; the use of a 180 °C-class non-silicone tape such as UCS180 is limited by the bead temperature, not the film temperature. In practice, the sealant bead is placed under the bag film and shielded from direct oven airflow, so its temperature can lag the air temperature by 20 °C to 40 °C during ramps; this lag permits short excursions above the rated service temperature on thin tool flanges, but sustained exposure above 180 °C is not recommended. When the cure schedule requires 204 °C for epoxy or bismaleimide systems, UCS180 is not a direct substitute for a silicone-based high-temperature tape unless a thermal break or insulative overwrap reduces the bead temperature below 180 °C. Published data for this specific configuration is limited, so thermocouple instrumentation of the tool flange is recommended before extending the operational envelope. The product can also be used as a temporary mask for off-part surfaces during plasma or grit-blast operations, but adhesion should be tested on the specific substrate because the tape is not designed as a high-adhesion masking product. In such applications, the tape must be removed before the surface temperature exceeds 50 °C to avoid cohesive splitting and residue entrapment.

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