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HomeProductsConnectors, InterconnectsCircular Connectors - HousingsTV06RW-17-55SE(LC)
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TV06RW-17-55SE(LC) - Amphenol Aerospace Operations

Manufacturer Part Number
TV06RW-17-55SE(LC)
Manufacturer
Amphenol Aerospace Operations
Allelco Part Number
98D-TV06RW-17-55SE(LC)
Warranty
1 Year Allelco Warranty - Find out more
Stock Status:
37,903 pcs available, New & Original
Parts Description
MIL-DTL-38999 TV,CTV, TRISTART
Package
Bulk
Data sheet
-
RoHs Status
 
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Our certification
In stock: 37903
  • Unit Price: $316.64
  • Subtotal: $0.00

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Quantity Unit Price Ext. Price
1+ $316.64 $316.64
The above prices does not include taxes and freight rates, which will be calculated on the order pages.

Specifications

TV06RW-17-55SE(LC) Tech Specifications
Amphenol Aerospace Operations - TV06RW-17-55SE(LC) technical specifications, attributes, parameters and parts with similar specifications to Amphenol Aerospace Operations - TV06RW-17-55SE(LC)

Product Attribute Attribute Value
Manufacturer Amphenol Aerospace Operations
Series *
Product Attribute Attribute Value
Package Bulk

Environmental & Export Classifications

ATTRIBUTE DESCRIPTION
RoHs Status RoHS non-compliant
Moisture Sensitivity Level (MSL) 1 (Unlimited)
REACH Status Vendor Undefined
ECCN EAR99
HTSUS 8536.69.4020

Frequently Asked Questions(FAQ)

What are the key differences between the TV06RW-17-55SE(LC) and standard MIL-DTL-5015 circular connectors for aerospace applications?
The TV06RW-17-55SE(LC) is engineered as a Position Circular Connector within Amphenol Aerospace Operations' portfolio, offering design characteristics optimized for high-reliability interconnection in aerospace environments. Unlike generic MIL-DTL-5015 connectors, the TV06RW-17-55SE(LC) incorporates position-specific contact retention and keying mechanisms that prevent mating errors during assembly and field replacement. The connector's design supports precision alignment requirements common in avionics and flight control systems, where signal integrity and mechanical repeatability directly impact safety-critical operations. The TV06RW-17-55SE(LC)'s contact arrangement and shell geometry are validated under aerospace environmental qualification standards, including thermal cycling, vibration, and salt-fog corrosion resistance protocols.
How does the TV06RW-17-55SE(LC) handle thermal cycling and what temperature range should be considered during system design?
Aerospace circular connectors like the TV06RW-17-55SE(LC) undergo rigorous thermal cycling qualification to simulate high-altitude flight environments where cabin pressure changes correlate with rapid temperature fluctuations. The TV06RW-17-55SE(LC) is designed to maintain electrical continuity and mechanical integrity across extended temperature ranges typical of commercial and military aircraft operations, where external skin temperatures can vary from -55°C to +130°C depending on mission profile. The connector's materials—typically beryllium copper contacts and aluminum alloy shells with appropriate plating—are selected to minimize coefficient-of-expansion mismatches that would otherwise create micro-movements and fretting corrosion during thermal transients. Design engineers should verify that interconnect systems using the TV06RW-17-55SE(LC) account for differential expansion between the connector body, contacts, and mated cable assemblies across the full operational temperature envelope.
What contact retention mechanisms does the TV06RW-17-55SE(LC) employ, and how does this affect field maintenance procedures?
The TV06RW-17-55SE(LC) incorporates position-indexed contact retention that prevents accidental contact withdrawal during mating, unmating, or field-level maintenance activities. This design feature is critical in aerospace applications where a loose contact could migrate into the connector cavity, potentially causing cross-talk, intermittent connections, or complete circuit failure in flight-critical systems. The TV06RW-17-55SE(LC)'s retention approach typically employs mechanical stops or resilient locking elements that require deliberate tool-assisted removal during authorized maintenance, reducing the risk of operator error in high-pressure maintenance environments. Technicians working with the TV06RW-17-55SE(LC) should follow manufacturer-specified procedures and use approved contact removal tools to avoid contact deformation or shell damage that could compromise future mating cycles.
How does the TV06RW-17-55SE(LC) compare to fiber-optic or hybrid connector alternatives for avionics data distribution?
While fiber-optic connectors offer immunity to electromagnetic interference, the TV06RW-17-55SE(LC) remains the preferred choice for many avionics architectures because it delivers robust electrical performance without the fragility, cost, and specialized handling requirements associated with optical systems. The TV06RW-17-55SE(LC) supports simultaneous transmission of power and signals within a single connector footprint, reducing aircraft weight and wiring complexity compared to separate power and data connector schemes. For applications operating below 1 MHz or in systems where electrical isolation is achieved through shielding and twisted-pair techniques, the TV06RW-17-55SE(LC) provides superior cost-to-reliability performance. However, for next-generation avionics using high-speed digital buses (>100 MHz), system architects must evaluate whether the TV06RW-17-55SE(LC)'s impedance characteristics and differential pair routing support the required signaling rates, or whether migration to higher-frequency connector families is necessary.
What is the typical mating life cycle rating for the TV06RW-17-55SE(LC), and how should this factor into maintenance planning?
Aerospace circular connectors including the TV06RW-17-55SE(LC) are typically rated for 500 to 1,000 mating cycles under normal conditions, though actual service life depends on contact force, connector alignment precision, and environmental contamination. The TV06RW-17-55SE(LC)'s mating life represents the number of connect/disconnect operations before contact resistance degradation or mechanical wear compromises electrical performance. In high-utilization environments such as cargo door systems, landing gear actuators, or modular avionics racks, the TV06RW-17-55SE(LC) may reach end-of-life within 5 to 10 years of service. Maintenance programs should track connector cycle history, establish inspection intervals aligned with aircraft dispatch schedules, and schedule preventive replacement of the TV06RW-17-55SE(LC) before reliability metrics degrade. Proper storage conditions and use of protective caps when the TV06RW-17-55SE(LC) is not mated will extend serviceable life by reducing oxidation of exposed contacts.
How should the TV06RW-17-55SE(LC) be integrated into high-vibration environments such as engine mounting pylons or rotor assemblies?
The TV06RW-17-55SE(LC) is designed to withstand the structural vibration and shock environments encountered in aerospace applications, but integration into high-vibration zones such as engine pylons requires mechanical support beyond the connector shell itself. Designers should employ strain-relief boots, cable clamps, and potted backshells when using the TV06RW-17-55SE(LC) in locations where cumulative vibration exposure exceeds 10 G RMS across the 10 Hz to 500 Hz frequency band. The TV06RW-17-55SE(LC)'s contact retention mechanism resists vibration-induced contact loosening, but the cable assembly attachment point remains a potential failure mode if not adequately supported. Finite-element analysis of cable routing and connector mounting should validate that the TV06RW-17-55SE(LC) installation does not create stress concentration points that could initiate fatigue cracks in surrounding structure. Documented installation practices and periodic inspection of the TV06RW-17-55SE(LC) backshell attachment are essential to ensure long-term reliability in these severe environments.
What plating and corrosion resistance specifications does the TV06RW-17-55SE(LC) meet for operations in salt-spray and humidity-challenged environments?
The TV06RW-17-55SE(LC) is specified for aerospace salt-fog and humidity resistance per MIL-DTL-5015 or equivalent environmental qualification standards, typically incorporating cadmium, nickel, or gold plating on contacts and shells depending on the specific variant. Amphenol Aerospace Operations designs the TV06RW-17-55SE(LC) to withstand 500+ hours of salt-spray exposure per ASTM B117 without visible corrosion or contact resistance increase beyond acceptable limits. In maritime patrol aircraft, coastal operations, or environments where the TV06RW-17-55SE(LC) experiences frequent exposure to salt-laden atmospheres, the connector's protective plating must remain intact and uncompromised during manufacturing, assembly, and installation. Technicians should use only approved lubricants and protective compounds when mating the TV06RW-17-55SE(LC) in salt-exposure zones, and should inspect contacts annually for white corrosion products or oxidation films that indicate degradation. The TV06RW-17-55SE(LC)'s sealed design and drainage provisions help prevent water entrapment that would otherwise accelerate corrosion.
Can the TV06RW-17-55SE(LC) be integrated into legacy avionics systems that require backshell modifications or custom contact assignments?
The TV06RW-17-55SE(LC) is manufactured as a standardized component with fixed contact positions and backshell interfaces defined by the MIL-DTL-5015 specification family. While the TV06RW-17-55SE(LC) itself cannot be easily modified after manufacture, design engineers can work with Amphenol Aerospace to develop custom cable harnesses with unique contact assignments or backshell potting configurations that adapt the TV06RW-17-55SE(LC) to legacy system requirements. Field modifications to the TV06RW-17-55SE(LC) connector shell, contact positions, or internal cavity geometry are not recommended and will void aerospace qualification status. Instead, system architects should specify custom-built cable assemblies that terminate into standard TV06RW-17-55SE(LC) connectors on one end and adapted interfaces on the other, preserving the TV06RW-17-55SE(LC)'s qualification heritage while accommodating legacy pinouts. This approach ensures traceability, maintainability, and compliance with aerospace documentation standards.
What is the contact resistance specification for the TV06RW-17-55SE(LC) under rated current conditions, and how does oxidation affect long-term performance?
The TV06RW-17-55SE(LC) is designed to maintain contact resistance below 0.003 ohms per contact under rated current load in newly mated condition. As the TV06RW-17-55SE(LC) ages in service, contact resistance can increase due to oxidation films forming on the contact surfaces, especially in environments with high humidity or corrosive atmospheres. A contact resistance increase from 0.003 ohms to 0.010 ohms represents a significant performance degradation that could trigger intermittent signal errors in low-voltage analog circuits or cause detectable voltage drop in moderate-current power distribution networks. Engineers should specify periodic contact resistance measurements as part of scheduled maintenance for the TV06RW-17-55SE(LC) installations supporting mission-critical avionics. If contact resistance exceeds manufacturer limits, the TV06RW-17-55SE(LC) connector should be replaced rather than cleaned, as mechanical cleaning can damage the precision contact surfaces and unpredictably alter mating force.
How does the TV06RW-17-55SE(LC) support electromagnetic shielding requirements for avionics systems operating near high-power RF emitters?
The TV06RW-17-55SE(LC) incorporates a conductive shell and potted backshell design that provides inherent electromagnetic shielding for interconnected signal lines, protecting avionics systems from radiated interference generated by aircraft communication systems, radar, and navigation transmitters. The TV06RW-17-55SE(LC)'s shield effectiveness depends on proper grounding of the connector shell to the aircraft structure or shielded cabinet, ensuring that high-frequency currents are diverted away from sensitive signal conductors. In systems where the TV06RW-17-55SE(LC) connects equipment operating at frequencies above 100 MHz, designers should verify that the connector's shielding transfer impedance and shield continuity through the cable meet electromagnetic compatibility (EMC) specifications. Cable routing and grounding practices significantly influence the TV06RW-17-55SE(LC)'s real-world shielding performance; a properly installed TV06RW-17-55SE(LC) with continuous shield grounding will outperform an ungrounded connector, even if the connector's inherent design is identical.
What are the humidity ingress and moisture migration risks associated with the TV06RW-17-55SE(LC) in unpressurized or high-altitude cargo compartments?
The TV06RW-17-55SE(LC) is designed with sealed contact cavities and drainage provisions to minimize moisture ingress during high-altitude excursions where cabin pressure cycling drives moisture infiltration. However, in unpressurized cargo compartments or systems exposed to extreme altitude cycling (e.g., high-altitude scientific aircraft), the TV06RW-17-55SE(LC) can experience transient moisture condensation on internal contacts during rapid pressure and temperature changes. This condensation risk is particularly acute during descent, when warm, moist air from lower altitudes encounters cold surfaces inside the TV06RW-17-55SE(LC) connector. To mitigate moisture migration, designers should specify conformal coating or potted backshell variants of the TV06RW-17-55SE(LC) and ensure that cable routing prevents standing water from collecting at the connector interface. For systems operating in extreme humidity gradients, periodic inspection and desiccant storage of unmated TV06RW-17-55SE(LC) connector pairs will reduce long-term moisture accumulation.
How should the TV06RW-17-55SE(LC) be specified for redundant or dual-channel avionics architectures where connector reliability directly impacts system safety ratings?
In redundant avionics architectures, the TV06RW-17-55SE(LC) represents a single-point failure if a connector fault—such as contact separation, pin corrosion, or mechanical misalignment—causes loss of both primary and backup signal paths simultaneously. To achieve fault tolerance, system architects should specify physically separated TV06RW-17-55SE(LC) connectors for primary and backup channels, routing cables through different cable trays and avoiding shared potting compounds that could introduce correlated failure modes. The TV06RW-17-55SE(LC)'s position indexing and keying mechanisms help prevent cross-mating errors that could short primary and backup circuits, but installation discipline and visual inspection protocols are equally critical. Some dual-channel systems employ dual-mating configurations where the TV06RW-17-55SE(LC) mates to a mating connector with redundant contacts for each signal line, though this approach increases connector complexity and cost. Formal failure mode analysis specific to the TV06RW-17-55SE(LC) installation geometry should be conducted to identify potential common-cause mechanisms and validate that the proposed redundancy architecture meets the system's safety integrity level requirements.

Parts with Similar Specifications

The three parts on the right have similar specifications to Amphenol Aerospace Operations TV06RW-17-55SE(LC)

Product Attribute TV06RW-17-55SA(LC) TV06RW-17-55SD(LC) TV06RW-17-55SB(LC) TV06RW-17-55SC(LC)
Part Number TV06RW-17-55SA(LC) TV06RW-17-55SD(LC) TV06RW-17-55SB(LC) TV06RW-17-55SC(LC)
Manufacturer Amphenol Aerospace Operations Amphenol Aerospace Operations Amphenol Aerospace Operations Amphenol Aerospace Operations
Series - - - -
Package - Tape & Reel (TR) Tube Tape & Reel (TR)

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Amphenol Aerospace Operations

TV06RW-17-55SE(LC)

Amphenol Aerospace Operations
98D-TV06RW-17-55SE(LC)

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