Airbus A310
19,802 parts applicable to this airframe — widebody
| Part Number | Status |
|---|---|
| 0202221-003 | PMA |
| 106295 | PMA |
| 108280-17 | PMA |
| 108280-19 | PMA |
| 108280-21 | PMA |
| 108351-1 | PMA |
| 110790 | PMA |
| 13060606-0131 | PMA |
| 24060608-0304 | PMA |
| 35059-009 | PMA |
| 35059-010 | PMA |
| 35059-012 | PMA |
| 35059-013 | PMA |
| 35059-014 | PMA |
| 35059-015 | PMA |
| 35059-016 | PMA |
| 35059-017 | PMA |
| 35059-018 | PMA |
| 35059-019 | PMA |
| 35059-020 | PMA |
| 3826099-1NTMT | PMA |
| 3826099-1TMT | PMA |
| 440-0150-1 | OEM |
| 51000608-0200 | PMA |
| 51262604-0306 | PMA |
| 51262606-0094 | PMA |
| 51262606-0106 | PMA |
| 51262606-0171 | PMA |
| 51262606-0260 | PMA |
| 51262606-0295 | PMA |
| 717001-2 | PMA |
| 717001-4 | PMA |
| 7373038 | PMA |
| 7374849 | PMA |
| 9633M07P08WD | PMA |
| H5000-2-072-188 | OEM |
| HSP115P094-1550 | PMA |
| S009196 | PMA |
| S0608100200 | PMA |
| S145000006-0143M | PMA |
| S245061505-0150M | PMA |
| S3868 | PMA |
| S7064 | PMA |
| S7319 | PMA |
| S7447 | PMA |
| S7555 | PMA |
| S7663 | PMA |
| S7748 | PMA |
| S7763 | PMA |
| S8853 | PMA |
Utilization & cargo trend(US carriers, 2015–2025)
A310 family rollup — BTS T-100, domestic + international
US carriers only (BTS T-100, domestic + international segments) — foreign-carrier flying is excluded, so global utilization runs higher. Fleet size is reconstructed from the FAA registry (built on or before each year, not yet deregistered) — an approximation. Freighter share counts departures with zero passengers and freight aboard — a proxy for freighter/combi operations, not a tail-by-tail conversion count. Missing years render as gaps.
USM supply — retirements & teardowns(2023–2026)
A310 family — FAA registry deregistrations
FAA registry data. Domestic deregistration is a teardown proxy — it also captures re-registrations and some unflagged exports, so it is not a confirmed part-out count; exported aircraft left the US fleet intact and are not USM supply. ATA shares reflect where this directory's parts for the family concentrate (parts in parentheses) — a coverage signal, not the aircraft's bill of materials or a teardown-yield forecast.
Engine-program supply pressure(since 2023)
FAA registry — US-registered fleet
Engines account for roughly half of all MRO spend, so engine programs shedding aircraft are where retirement supply carries the most value.
| Engine model | Active tails | Engine units | Retired since ’23 | Exported | Avg age at dereg |
|---|---|---|---|---|---|
| GE CF6-80 series | 237 | 571 | 13 | 2 | 36.9 yr |
| P & W JT9D series | 13 | 37 | 3 | 0 | 41.7 yr |
FAA registry data, US-registered aircraft only. Counts reflect the engine model as registered — generic “series” rows coexist with thrust-variant rows, so per-variant figures are partial. Retired = domestic deregistrations (a teardown proxy, not a confirmed part-out); exported aircraft left the US fleet intact. Active tails span every family the engine flies on, not just this one.
Airworthiness Directive activity
FAA / EASA public regulatory data
- EASA AD 2024-0092-R1effective Jul 17, 2024Prohibition
EASA Safety Publications Tool
- EASA AD 2023-0092effective May 19, 2023Mixed actions
EASA Safety Publications Tool
- EASA AD 2023-0018effective Feb 6, 2023Mixed actions
EASA Safety Publications Tool
- EASA AD 2022-0195effective Oct 7, 2022Mixed actions
EASA Safety Publications Tool
- EASA AD 2022-0193effective Oct 7, 2022Mixed actions
EASA Safety Publications Tool
Directives linked to this airframe family in the FAA / EASA regulatory corpus we have processed — not a complete historical AD list. An AD is a compliance requirement that drives scheduled work (inspections, replacements, modifications) across the fleet; inspection directives are not replacement directives, and none of this is a prediction that any part will fail.