Aerospace RFID
RFID Aircraft Part Tags
MRO Lifecycle Traceability
Quick answer
RFID flyable aircraft part tags meet ATA Spec 2000 Chapter 9 requirements for permanent identification of aircraft components. From rotable parts and life-limited components to cabin furnishings and structural elements. Enable automated part identification, maintenance tracking and airworthiness documentation throughout the aircraft component lifecycle.
- ATA Spec 2000 compliant — meets airline industry standard for RFID part marking on flyable aircraft components.
- DO-160G environmental tested. Qualified for the vibration, temperature, altitude and humidity conditions of aircraft operation.
- High-memory chips — 2-64 KB user memory stores part number, serial, modification status and maintenance history on-tag.
Used in these industries
Deployments where this product is referenced on our industry landing pages.
At a glance
Use these short answers to decide whether this page matches the project before moving into the detail.
Chip options
NXP UCODE DNA / SL3S5002N0FUD (3,072-bit / 384-byte user memory + AES-128 cryptographic authentication per ISO/IEC 29167-10, EPC Gen2v2); Fujitsu MB97R803A (3,424-byte u...
Frequency / air interface
860-960 MHz UHF (RAIN RFID) per EPC Class 1 Gen 2 v2.1 / ISO/IEC 18000-63:2015. Regional use: FCC Part 15 Subpart C 902-928 MHz (US), ETSI EN 302 208 865-868 MHz (EU), A...
Next step
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Request aircraft part tag quote- Standards & marking method
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ATA Spec 2000 Chapter 9 — Automated Identification and Data Capture (Ch. 9-5 flyable UHF). FAA AC 20-162A — Airworthiness Approval and Operational Allowance of RFID Systems. EASA Certification Memorandum CM-AS-002 Issue 01. FAA 14 CFR Part 45 (part marking) acceptance of RFID as a marking method alongside data plate per OEM engineering order.
- Environmental qualification
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RTCA DO-160G / EUROCAE ED-14G tested: Sections 4 (Temperature & altitude -55 / +85 °C cabin, -55 / +200 °C engine zones), 5 (Temperature variation), 6 (Humidity), 7 (Operational shocks & crash safety), 8 (Vibration Cat. S / U / B / R), 11 (Fluids susceptibility — Skydrol, Jet A, de-icing fluid), 20 (RF susceptibility), 22 (Lightning indirect effects).
- Construction
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Ceramic-base (zirconia / alumina) or PEEK / PPS high-temp polymer housing with on-metal antenna tuning. Adhesive 3M VHB 5952 / VHB 4950 (cabin / cold zones), high-temp epoxy (engine zone), rivet-bonded stainless backing plate, or OEM-specified engineering-order attach. Laser-etched visual ATA part / serial alongside RFID for dual-identification redundancy.
- Sizes
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- 25 × 10 × 3 mm (compact — avionics, small LRUs)
- 50 × 15 × 3 mm (standard — rotables)
- 85 × 28 × 4 mm (large — engines, landing gear)
- Low-profile cabin variant (75 × 20 × 1.2 mm) for seats, IFE, bins
- Operating temperature
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-55 to +85 °C cabin / avionics zones (DO-160G Cat. A1 / A2); -55 to +200 °C engine zone variant (Cat. B2 / D2 thermal cycling); -40 to +150 °C wheel & brake zone. Bench-tested for 1,000 h accelerated-ageing per DO-160G §4 with no degradation of read range.
- Read range on metal
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1-3 m (compact 25 × 10 on metal, handheld UHF reader); 2-5 m (standard 50 × 15); 3-7 m (large 85 × 28 on landing gear). Chipless dock portals at MRO shop entrances achieve full-stack LRU read at 3-5 m with 99%+ read rate in pilot instrumentation.
- Data capacity & ATA 2000 elements
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ATA Spec 2000 Ch. 9-5 mandatory elements (P/N, S/N, CAGE/DUNS manufacturer code, manufacture date) fit in 96-384 bits; optional elements (modification status / SB compliance, cycles / hours remaining for LLPs, last shop visit, airworthiness status, Dispatch Deviation) require 2-8 KB; full engineering record 16-64 KB (Fujitsu FRAM).
- Security & counterfeit resistance
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NXP UCODE DNA AES-128 tag authentication (RFC 3394 key wrap); SHA-256 digital-thread hash linking tag EPC to OEM pedigree record; locked user-memory banks with killable passwords; GS1 SGTIN-96 or OEM-private EPC scheme; optional ARINC 816-compatible airline part-numbering overlay.
- Compliance framework
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ATA Spec 2000 Ch. 9 / iSpec 2200 · FAA AC 20-162A · EASA CM-AS-002 Issue 01 · FAA 14 CFR Part 21 (airworthiness) / Part 45 (identification & marking) / Part 145 (repair stations) · EASA Part 21 / Part 145 · SAE AS9100D · SAE AS5678 (Passive RFID for Aerospace) · ISO/IEC 18000-63:2015 · RTCA DO-160G / EUROCAE ED-14G · Boeing D6-81763 Rev E · Airbus A0094T0054 · IATA Resolution 753 (ULD tracking) · GS1 TDS 2.0 / EPCIS 2.0.
- Platform integration
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MRO / M&E: IFS Cloud for Aviation · Trax · Ramco Aviation · AMOS (Swiss-AS) · Sabre Flight Plan Manager · Boeing Insight Accelerator · Airbus Skywise · IBS iMRO · Rusada ENVISION. Supply chain: GE Aerospace Inventory Management · Accelya · SITA Logistics. Cabin / IFE: Panasonic Avionics Arc · Thales AVANT. Configuration: PTC Windchill · Siemens Teamcenter · Aras Innovator. Reader layer: Zebra FX9600 / MC3390xR · Impinj R700 / R780 · Alien Technology ALR-F800 · Keonn AdvanReader + certified aerospace-grade handhelds.
- MOQ / Lead time
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Cabin / LRU variant: 200 pcs / 20-30 business days. Engine-zone ceramic variant: 100 pcs / 30-40 business days. OEM engineering-order-specific: qualification 12-20 weeks (first article inspection + DO-160G report).
- Typical pricing
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USD 0.60–2.50 /pc by size (typical FOB Shenzhen range) — firm quote in one business day.
Commercial terms
- MOQ
- Varies by SKU — stock items from 100 pcs; custom production typically 200-1,000 pcs
- Lead time
- Production 2-3 weeks after artwork and encoding sign-off; reorders on a 3-4 week cycle
- Samples
- Free samples and RF test report with every order; courier at customer cost
- Payment
- 50% T/T deposit, 50% before shipment; Net 30/60 for established accounts; LC for large orders
- Shipping
- FOB Shenzhen / Yantian; DHL, FedEx or EMS air freight; sea LCL / FCL for volume
- Response
- Itemized quote within one business day, Mon-Fri (UTC+8)
Common challenges MRO shops and airlines face with aircraft part identification and traceability
- An aircraft contains 2-6 million individually serialized parts; manual identification using small data plates requires technicians to contort into confined spaces or use mirrors and lighting rigs, adding 5-15 minutes per part to incoming inspection and build documentation processes.
- Paper maintenance records and logbook entries for life-limited parts (LLPs) are lost, damaged or incorrectly transcribed at a rate that generates EASA/FAA findings in approximately 30% of airworthiness document audits. With consequences including grounded aircraft and unscheduled maintenance events.
- Counterfeit aircraft parts entering the supply chain cost the industry an estimated $2 billion annually; without a direct digital link between the physical part and its authenticated pedigree, visual inspection is the only available check. One that sophisticated counterfeit parts can pass.
- MRO shop turnaround time (TAT) for rotable components averages 15-30 days; a significant portion of that time is consumed by manual part identification, paper document retrieval and status verification that could be automated with on-tag data access.
- Modification status and applied service bulletin (SB/AD) records for fleet management require manual lookup in multiple systems per part number. Technicians spend 20-40 minutes per component reconciling physical part condition against database records before maintenance decisions can be made.
How Proud Tek ATA Spec 2000 RFID tags streamline aircraft part identification and compliance
Commodity on-metal RFID tag
- IP-rated industrial tag with no DO-160G test evidence
- 96-bit EPC only — no on-tag ATA 2000 data elements
- No aerospace fluids (Skydrol / Jet A) or lightning §22 testing
- No cryptographic tag authentication → visual-check counterfeit gap
- No OEM engineering-order attachment method specification
Proud Tek ATA Spec 2000 Ch. 9-5 aerospace tag
- DO-160G / ED-14G test report (Sections 4, 5, 6, 7, 8, 11, 20, 22) per variant
- 96-384 bit mandatory ATA 2000 Ch. 9-5 + 2-64 KB optional engineering record
- Aerospace fluid immersion §11, lightning indirect §22, RF susceptibility §20 data
- NXP UCODE DNA AES-128 authentication + SHA-256 digital-thread pedigree hash
- Attachment spec aligned to Boeing D6-81763 Rev E and Airbus A0094T0054, ready for OEM engineering order
- RTCA DO-160G / EUROCAE ED-14G qualification confirms tag survival through the full range of aircraft operational conditions (vibration Cat. S/U/B/R, temperature -55 to +200 °C, altitude, humidity Cat. A/B, fluids per §11 including Skydrol and Jet A) so the tag remains the part's permanent digital identity throughout its service life.
- High-memory chip options (NXP UCODE DNA 3,072-bit / 384-byte user memory with AES-128 authentication; Fujitsu MB97R8110 8 KByte FRAM, or Fujitsu AIT-64K tag product reaching 64 KByte FRAM at the tag level) store mandatory ATA 2000 Ch. 9-5 data elements (P/N, S/N, CAGE/DUNS manufacturer code, manufacture date) plus optional elements (modification / SB compliance status, LLP cycles / hours remaining, last shop visit, airworthiness status) directly on the tag — enabling offline data access without a network connection to the MRO system.
- On-metal optimised antenna designs achieve 1-7 m read range on metal aircraft components (tag size dependent), allowing technicians to identify parts in confined locations without physical access to the data plate.
- ATA Spec 2000 Chapter 9 compliance with FAA AC 20-162A and EASA CM-AS-002 Issue 01 means the tag is treated as a part-marking method under FAA 14 CFR Part 45 and EASA Part 21. No separate STC / TSO is required beyond the component's existing maintenance-data approval via OEM engineering order.
- UCODE DNA AES-128 tag authentication plus SHA-256 digital-thread hashing creates a cryptographic link from the physical part to its authenticated OEM pedigree record — raising the counterfeit-detection bar beyond visual / data-plate inspection.
Cross-buyer reference notes — ATA Spec 2000 Chapter 9-5 flyable-RFID
TAT compression, audit-finding reduction and counterfeit-detection outcomes all vary with fleet type, MRO shop footprint, reader infrastructure and the mix of ATA 2000 data elements carried on-tag versus looked up in the M&E system, so what follows is the shape of the work airline and OEM integrators sequence on a Chapter 9-5 deployment — not client-specific numbers. The sequencing is anchored to ATA Spec 2000 Chapter 9 (Automated Identification and Data Capture), FAA AC 20-162A (Airworthiness Approval and Operational Allowance of RFID Systems), EASA Certification Memorandum CM-AS-002 Issue 01, RTCA DO-160G / EUROCAE ED-14G, FAA 14 CFR Part 45 and SAE AS5678 Passive RFID for Aerospace Applications.
Directional benchmarks published in ATA Spec 2000 Ch. 9 implementation notes, the Boeing Insight Accelerator RFID programme references and Airbus Skywise Industry Insights describe incoming-inspection time on rotable LRUs moving from manual-data-plate retrieval to single-scan read, LLP logbook-transcription error from paper-driven audit findings to digital-thread hash verification, and counterfeit-pedigree detection moving from visual-only to cryptographic AES-128 — the direction programmes should expect, with magnitudes settled per shop during first-article qualification and pilot-line instrumentation.
- Weeks 1-4 · Component scope + engineering-order map
Confirm tag targets (engine LRU / landing gear / avionics / cabin / wheel-brake), lock OEM engineering-order attach method against Boeing D6-81763 Rev E or Airbus A0094T0054, decide which ATA 2000 Ch. 9-5 data elements are carried on-tag vs looked up. Lodge SAE AS9100D supplier qualification if first-time OEM supply.
- Weeks 5-12 · First Article + DO-160G test programme
Issue first-article inspection (FAI) per AS9102, run DO-160G / ED-14G §4, §5, §6, §7, §8, §11, §20, §22 test report on the target variant, freeze chip option (UCODE DNA / Fujitsu FRAM / Impinj M775). Issue FAA AC 20-162A / EASA CM-AS-002 documentation pack.
- Weeks 13-24 · Pilot line + MRO wiring
Deploy on one component family (e.g., fleet of landing-gear LRUs), wire reader network (Zebra FX9600 / Impinj R700) into MRO platform (IFS Cloud for Aviation / Trax / AMOS / Ramco / Rusada), validate ATA 2000 element propagation into maintenance records, exercise UCODE DNA AES-128 authentication on incoming inspection.
- Month 7+ · Fleet scale-out + digital-thread loop
Extend to remaining component families (engine LRU / wheel-brake / cabin), link tag lifecycle data into PTC Windchill or Aras Innovator configuration record, publish digital-thread hash into Boeing Insight Accelerator / Airbus Skywise and close the counterfeit-pedigree loop with OEM SUP audit.
Why RFID for aircraft parts
- An aircraft contains 2-6 million parts, many of which are individually serialized, life-limited and subject to airworthiness directives.
- Manual part identification (reading small data plates, paper forms, logbook entries) is slow and error-prone.
- RFID enables instant identification: technician scans the part tag to pull up the complete maintenance record, modification status and remaining life.
- Regulatory acceptance: EASA (CM-AS-002 Issue 01) and FAA (AC 20-162A) accept RFID as an approved marking method alongside the data plate under ATA Spec 2000 Ch. 9-5.
- MRO efficiency: reduce turnaround time by automating incoming inspection, parts kitting and build documentation.
- Counterfeit prevention: the RFID tag creates a cryptographically protected digital thread linking the physical part to its authenticated pedigree (AES-128 tag authentication + SHA-256 OEM-record hash).
ATA Spec 2000 data elements
| Data element | Description | Stored on-tag |
|---|---|---|
| Part number (P/N) | Manufacturer's part number | Yes (mandatory) |
| Serial number (S/N) | Unique serial for the individual part | Yes (mandatory) |
| Manufacturer code | CAGE / DUNS code of the OEM | Yes (mandatory) |
| Manufacturing date | Date of manufacture or last shop visit | Yes |
| Modification status | Applied service bulletins and ADs | Yes (high-memory chips) |
| Cycles / hours remaining | For life-limited parts (LLPs) | Yes (if tracking on-tag) |
| Last shop visit | Date, facility, work performed | Yes (high-memory chips) |
| Airworthiness status | Serviceable, unserviceable, condemned | Yes |
| Digital-thread hash | SHA-256 link to OEM authenticated pedigree | Yes (high-security variant) |
Tag placement by component type
| Component | Tag size | Mounting | Environment |
|---|---|---|---|
| Engine LRU (Line Replaceable Unit) | 50 × 15 mm | High-temp epoxy or rivet on housing | High temp (DO-160G Cat. B2), vibration Cat. U/R |
| Landing gear component | 85 × 28 mm | Rivet-bonded stainless backing | Extreme temp, FOD risk, Skydrol per §11 |
| Avionics box | 25 × 10 mm | 3M VHB 5952 on enclosure | Pressurised cabin, EMI §20, altitude §4.6 |
| Cabin furnishing (seat, bin, IFE) | 50 × 15 or 75 × 20 (low profile) | 3M VHB 4950 adhesive or screw | Cabin environment Cat. A1 |
| Wheel / brake assembly | 50 × 15 mm | High-temp epoxy or rivet | Braking heat +200 °C, de-icer fluid §11 |
| Structural panel | 25 × 10 mm | Embedded or adhesive | External skin, pressure cycling §4.6, lightning §22 |
Useful next pages
Use these linked product, guide and comparison pages to keep the next click specific and practical.
Related industrial tags
Other ruggedized RFID solutions.
Industry applications
Industry deep-dives where this SKU is commonly specified.
FAQ
Are these tags approved for use on flying aircraft?
Yes. Our tags are designed and tested per RTCA DO-160G / EUROCAE ED-14G environmental conditions for airborne equipment. ATA Spec 2000 Chapter 9-5 defines the flyable UHF RFID marking standard accepted by EASA (CM-AS-002 Issue 01) and FAA (AC 20-162A) for aircraft parts. The tag is classified as a part-marking method under FAA 14 CFR Part 45 and does not require a separate STC / TSO — the tag attach method must be approved as part of the component's maintenance data (via the OEM's Component Maintenance Manual or engineering order, typically aligned to Boeing D6-81763 Rev E or Airbus A0094T0054).
How much data can be stored on the tag?
Standard tags with NXP UCODE DNA store 3,072 bits (384 bytes) of user memory — enough for mandatory ATA 2000 Ch. 9-5 elements (P/N, S/N, CAGE / DUNS manufacturer code, dates) plus a compact modification-status flag. High-memory tags with Fujitsu MB97R8110 FRAM (8 KByte user bank per Ramxeed/Fujitsu datasheet) cover most maintenance-record use cases; the Fujitsu AIT-64K Metal Mount Tag product reaches 64 KByte FRAM at the tag level for complete maintenance history, modification records and operational parameters. Choose the memory size based on how much data you want to carry on the part itself versus looking up in your MRO / M&E system (IFS Cloud for Aviation, Trax, AMOS, Ramco).
What read range do the tags achieve on metal aircraft parts?
Our on-metal aerospace tags achieve 1-7 m read range with a handheld UHF reader on metal aircraft components. The compact 25 × 10 mm variant reads at 1-3 m, the standard 50 × 15 mm at 2-5 m, and the large 85 × 28 mm at 3-7 m on landing gear. Read range is sufficient for technicians to identify parts without physically accessing the data plate, which may be in a hard-to-reach location — and dock-portal readers at MRO shop entrances achieve stacked-LRU read at 3-5 m with high read-rate in pilot instrumentation.
Sources & references
Primary standards, OEM datasheets and regulatory documents cited by this article. All URLs were verified on the access date shown below.
- ATA Spec 2000 — Chapter 9: Automated Identification and Data Capture (Chapter 9-5 Passive UHF Flyable RFID Tag)
Industry standard for aircraft-part RFID marking — defines the flyable UHF tag profile, data elements and authentication framework used across Boeing / Airbus / Embraer / Bombardier programmes.
- FAA Advisory Circular 20-162A — Airworthiness Approval and Operational Allowance of RFID Systems
FAA guidance on airworthiness approval and operational allowance of RFID systems on aircraft — the FAA-side gate for Ch. 9-5 flyable tags.
- EASA Certification Memorandum CM-AS-002 Issue 01 — Design Considerations for Radio Frequency Identification (RFID) Installations
EASA certification memorandum on RFID installation design — the EASA equivalent of FAA AC 20-162A for on-aircraft RFID.
- RTCA DO-160G — Environmental Conditions and Test Procedures for Airborne Equipment
Standard environmental test procedures referenced by every flyable aerospace electronics component; Sections 4, 5, 6, 7, 8, 11, 20 and 22 exercised for RFID part tags.
- SAE AS5678 — Passive RFID Tags Intended for Aircraft Use
SAE Aerospace Standard defining RFID tag performance and environmental requirements for flyable aircraft application.
- 14 CFR Part 45 — Identification and Registration Marking
Federal regulation on part identification and marking — the regulatory basis for accepting RFID as an aircraft-part marking method alongside the data plate.
- ISO/IEC 18000-63:2015 Information technology — RFID for item management — Part 63: Parameters for air interface communications at 860 MHz to 960 MHz Type C
UHF air-interface standard aligned with EPC Class 1 Gen 2 v2.1 — the radio protocol of all ATA Spec 2000 Ch. 9-5 flyable tags.
- SAE AS9100D — Quality Management Systems - Requirements for Aviation, Space, and Defense Organizations
Quality-management framework required for aerospace suppliers — the basis for RFID-tag OEM supplier qualification and FAI per AS9102.
- FAA Advisory Circular 21-29D — Detecting and Reporting Suspected Unapproved Parts
FAA guidance on Suspected Unapproved Parts (SUP) programme — the counterfeit-pedigree framework RFID digital-thread authentication supports.
- NXP UCODE DNA — Cryptographic RFID IC reference implementation (AES-128 tag authentication)
UCODE DNA product reference defining AES-128 tag authentication per ISO/IEC 29167-10 — the cryptographic basis for aerospace digital-thread pedigree verification.
Proud Tek is a Shenzhen-based RFID & NFC manufacturer supplying hotel chains, transit operators, event venues and retail brands worldwide. Every order includes free samples, RF testing and dedicated project support.
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