LINER, INNER, FLIGHT TUBE, 10044806, 0020-98878

PART DETAILS

0020-98878
LINER, INNER, FLIGHT TUBE, 10044806, 0020-98878

OEM P/N: 

0020-98878

ESCT P/N: 

ES227-0099

PART TYPE:

2nd

OEM: 

AMAT
MORE INFO

Inner flight tube liner (OEM P/N 0020-98878), beamline drift-region liner for AMAT ion implanter systems

ESCT P/N ES227-0099 · AMAT-compatible inner liner for the flight tube / beam transport region

The Inner Flight Tube Liner (AMAT OEM P/N 0020-98878, ESCT P/N ES227-0099) is a sacrificial inner sleeve fitted along the bore of the flight tube, the evacuated drift region through which the extracted ion beam travels between the analyser magnet and the downstream beamline optics on Applied Materials ion implanter platforms. In an XR80/9500-class architecture the flight tube forms a long, electrically defined vacuum conduit, and the inner liner is the surface that the beam halo, neutralised species and sputtered material actually see. By presenting a replaceable, high-purity barrier between the energetic beam and the structural tube wall, the liner protects an expensive permanent assembly while keeping the immediate beam environment clean and electrically predictable.

Although it carries no moving parts and draws no power, the inner flight tube liner is a genuine performance component rather than a passive shroud. Its position deep inside the beam transport path means that any contamination it sheds, any charge it accumulates and any geometry change it suffers is communicated directly to the beam. A liner in good condition keeps the drift region’s effective aperture consistent, suppresses particle generation and helps maintain the vacuum and electrical conditions that stable, repeatable implants depend on.

Because it sits in a high-energy, high-vacuum line-of-sight to the beam, the liner is treated as a scheduled consumable. It is one of the components that fab engineers inspect, clean or replace during beamline preventive maintenance, and sourcing a form-fit-function equivalent quickly is central to keeping implant tools at full availability.

Functional role of the inner flight tube liner in AMAT ion implanter platforms

Within the beamline, the inner flight tube liner performs several overlapping jobs that together preserve beam quality through the drift region between analysis and the end station:

  • Shields the structural flight tube wall from direct beam halo strike, neutral-beam impingement and sputter erosion, so wear is concentrated on a cheap replaceable part rather than the permanent tube.
  • Defines a clean, dimensionally consistent inner bore that establishes the effective drift-region aperture and keeps the beam envelope unobstructed.
  • Acts as a controlled, high-purity surface for capturing sputtered species and redeposited material, reducing the chance of metallic or cross-species contamination reaching the wafer.
  • Provides a predictable boundary condition for the electrical and potential environment along the beam path, helping to manage stray charge and secondary electrons.
  • Helps maintain local vacuum integrity by limiting outgassing and particle release from beam-struck surfaces in the transport region.
  • Simplifies preventive maintenance by concentrating deposit build-up onto a removable liner that can be cleaned or exchanged without disturbing the tube assembly itself.

Material and process performance

High-purity construction for the beam environment

Beamline liners of this class are manufactured from high-purity, vacuum-compatible refractory materials, typically fine-grain graphite or comparable beam-tolerant stock, chosen because they withstand continuous energetic-ion and neutral bombardment without melting, gross outgassing or rapid breakdown. Material purity is critical: the liner sits in the beam’s line of sight, so trace contaminants in the bulk material can be sputtered loose and carried toward the wafer.

  • Refractory, low-vapour-pressure construction that tolerates sustained beam strike and elevated local temperatures.
  • High bulk purity to minimise the risk of liner-sourced metallic contamination in the implant.
  • Stable dimensions across thermal cycling so the effective bore does not drift between maintenance intervals.
  • Surface and grain characteristics selected to limit particle shedding and flaking of redeposited films.

Behaviour under beam loading and deposition

In service the liner gradually accumulates sputtered and redeposited material on its inner face while simultaneously losing its own surface to erosion where the beam halo is most intense. Managing this balance is the heart of liner maintenance: an eroded or heavily caked liner alters the local geometry and contamination profile, so its condition is tracked against process drift and particle data.

  • Predictable, gradual erosion that keeps wear on the liner rather than the tube wall.
  • Tolerance to deposit build-up without premature flaking that would generate particles.
  • Resistance to thermal shock as beam current is ramped and parked during recipe changes.
  • Compatibility with the cleaning regimes used during scheduled beamline preventive maintenance.

Impact on tool performance and yield

Because the inner flight tube liner sits directly in the beam transport path, its condition is felt across beam transmission, contamination control and tool uptime. A degraded liner rarely fails dramatically; instead it erodes process margin in ways that show up as drift and particle excursions:

  • Particle excursions and yield loss when caked deposits flake from a worn liner and travel downstream toward the wafer.
  • Metallic or cross-species contamination if a low-purity or eroded liner sheds material into the beam path.
  • Beam-transmission and dose-uniformity drift if liner geometry or charging conditions change the effective drift-region aperture.
  • Increased risk of unplanned downtime when liner degradation forces an unscheduled beamline vent and clean.
  • Faster wear of the permanent flight tube if a missing or failed liner exposes the structural wall to direct beam strike.

Common wear and failure modes

Erosion and thinning from beam strike

The dominant wear mechanism is sputter erosion where the beam halo and neutral flux strike the liner most intensely. Over many beam-hours the inner surface thins and the bore opens up locally, eventually compromising the liner’s ability to protect the tube wall and maintain a consistent aperture. This is expected, end-of-life wear rather than a defect, and it sets the liner’s replacement interval.

Deposit build-up and flaking

Sputtered and redeposited material accumulates as films and flakes on the inner face. When these deposits grow thick or are stressed by thermal cycling, they can delaminate and break loose, becoming a particle source in the beam path. Flaking is a leading reason liners are cleaned or replaced before they reach their erosion limit.

Thermal and mechanical distortion

Repeated heating from beam loading and cooling during idle periods can warp or crack a liner, particularly once erosion has weakened a section. A distorted liner may no longer seat correctly in the tube, can intrude into the beam envelope and accelerates both erosion and particle generation, so visible cracking or deformation warrants replacement.

Installation and replacement guidance

Replacing the inner flight tube liner is a beamline preventive-maintenance task that must follow Applied Materials safety procedures and your fab’s local work instructions. The outline below is general guidance only:

  • Place the implanter in the correct maintenance mode, observe all high-voltage lockout/tagout requirements and confirm the beamline is de-energised.
  • Vent the relevant beamline section to a clean, dry inert gas and allow components to reach a safe handling temperature.
  • Open the flight tube access and withdraw the worn liner, noting its orientation and seating so the replacement can be fitted identically.
  • Inspect the exposed tube wall, mating surfaces and any retaining features for erosion, deposits or damage, and clean as required.
  • Handle the new liner with clean, powder-free gloves, keeping it free of skin oils and particulates, then install it in the correct orientation and seat it fully.
  • Reassemble the flight tube, verify that the bore is clear and the liner does not intrude into the beam envelope, and confirm there are no loose particles.
  • Pump down, leak-check, and recover the beam, then verify transmission, dose uniformity and particle levels against baseline before returning to production.

Spare parts strategy for AMAT ion implanter beamlines

Beamline liners are scheduled consumables, so the practical question is not whether you will replace 0020-98878 but how quickly you can do so without holding excessive capital on the shelf. ESCT Fab Support helps fabs keep implanters running by supplying form-fit-function equivalents with a clear sourcing and lead-time picture:

  • A defined nominal lead time of approximately 2.5 weeks, supporting planned preventive-maintenance scheduling and buffer-stock decisions.
  • Parts verified to the original form, fit and function so they drop into existing beamline procedures without process requalification beyond your standard checks.
  • Clear OEM and ESCT cross-referencing (AMAT 0020-98878 / ESCT ES227-0099) to remove ambiguity at the point of order.
  • A cost-effective alternative to OEM list pricing for a part that is, by design, regularly consumed.
  • Support for consolidating beamline consumables with a single responsive supplier to reduce purchase-order overhead.

Frequently asked questions

What does the inner flight tube liner actually do?

It is a sacrificial inner sleeve fitted along the bore of the flight tube, the evacuated drift region the ion beam travels through between the analyser magnet and the downstream beamline. It protects the permanent tube wall from beam strike and sputter erosion, presents a clean high-purity surface to the beam, and helps keep the drift-region aperture and electrical conditions consistent.

Is this an original OEM part?

No. This is supplied as a new, OEM-compatible part that is cross-referenced to AMAT 0020-98878 and verified to the original form, fit and function. It is not an original Applied Materials branded part and is not sold as such; it is an independent equivalent intended as a direct replacement.

Which AMAT P/N and ESCT P/N does this cover?

It corresponds to Applied Materials OEM P/N 0020-98878 and ESCT P/N ES227-0099. Quoting both numbers on your order gets the correct liner matched to your beamline configuration.

How often does the liner need replacing?

The liner is a consumable whose life depends on beam current, species and duty cycle, so there is no single fixed interval. In practice it is inspected during scheduled beamline preventive maintenance and replaced when erosion, deposit flaking or distortion indicate it can no longer protect the tube or maintain a clean, consistent bore.

How do I know the liner is worn out?

Typical indicators are visible thinning or erosion where the beam halo strikes, heavy or flaking deposit build-up on the inner face, cracking or warping, and process symptoms such as particle excursions or drift in beam transmission and dose uniformity that trace back to the beam transport region.

What is the lead time?

The nominal lead time is approximately 2.5 weeks. Because the liner is a planned consumable, many fabs hold a small buffer stock and reorder against this lead time to keep preventive-maintenance schedules on track. Contact ESCT Fab Support to confirm current availability for your requirement.

Summary

The Inner Flight Tube Liner (AMAT 0020-98878, ESCT ES227-0099) is a high-purity sacrificial sleeve that protects the flight tube and maintains a clean, dimensionally stable drift region inside AMAT ion implanter beamlines. By absorbing beam-halo erosion and capturing sputtered material, it safeguards an expensive permanent assembly while protecting implant cleanliness, beam transmission and yield. As a scheduled consumable subject to erosion, deposit flaking and thermal distortion, it is best managed with a reliable, fast-turnaround supply, which is exactly what ESCT Fab Support provides with verified form-fit-function equivalents and a defined lead time.

Disclaimer: This part is supplied by ESCT Fab Support as a new, OEM-compatible second-source component, verified to the form, fit and function of Applied Materials part number 0020-98878. It is not an original OEM part and is not sold as one. It is not manufactured by, endorsed by, or affiliated with Applied Materials, and all manufacturer names and part numbers are quoted for identification and compatibility purposes only.

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