Airbus A310
19,802 parts applicable to this airframe — widebody
| Part Number | Status |
|---|---|
| 0016BM001612A60 | OEM |
| 0060-0085 | PMA |
| 0060-0094 | PMA |
| 2651-269-2 | PMA |
| 4259-20 | PMA |
| 86605-001SD | PMA |
| 86656-003SD | PMA |
| A2181029100200 | PMA |
| A2181029201400 | PMA |
| A2181031100700 | PMA |
| A2181048700500 | PMA |
| A2181055100200 | PMA |
| A2181065600200 | PMA |
| A2187120800000 | PMA |
| A2187403808200 | PMA |
| A2187411202600 | PMA |
| A2187413009400 | PMA |
| A2187416201600 | PMA |
| A2187418604400 | PMA |
| A2187418612800 | PMA |
| A2187428800000 | PMA |
| A2187493408000 | PMA |
| A2187495502400 | PMA |
| A2187496801400 | PMA |
| A2187496805800 | PMA |
| A2187496812200 | PMA |
| A2187496905600 | PMA |
| A2187498402400 | PMA |
| A2187630200000 | PMA |
| A2187634300600 | PMA |
| A2187640100000 | PMA |
| A2187642005200 | PMA |
| A2187646207600 | PMA |
| A2187646606600 | PMA |
| A2187648605600 | PMA |
| A2187651400000 | PMA |
| A2187653400800 | PMA |
| A2187654005600 | PMA |
| A2187660100000 | PMA |
| A2527158800600 | PMA |
| C21874088266 | PMA |
| ML-6839LL | PMA |
| ML-8GH004554-28 | PMA |
| S9413-011KT | PMA |
| S9413-014KT | PMA |
| S9413-113KT | PMA |
| S9413-114KT | PMA |
| S9413-149KT | PMA |
| S9413-151KT | PMA |
| S9413-558KT | 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.