Airbus A310
19,802 parts applicable to this airframe — widebody
| Part Number | Status |
|---|---|
| 1011104-6 | PMA |
| 11056-1EH | PMA |
| 1830T100-3 | PMA |
| 2088197-0010WD | PMA |
| 221-0746-502SD | PMA |
| 240233EH | PMA |
| 24D507239P02EH | PMA |
| 3059103-9 | PMA |
| 3575-1252-05EH | PMA |
| 3613827-1WE | PMA |
| 3617447-1WE | PMA |
| 695-450 | PMA |
| 695-500 | PMA |
| 695-700 | PMA |
| 728886-1WE | PMA |
| 9-3179505-1 | PMA |
| 9-3182175-1 | PMA |
| 9-975943-1 | PMA |
| AF2000 | PMA |
| AF302 | PMA |
| AF644 | PMA |
| AF648 | PMA |
| AF688 | PMA |
| AF788 | PMA |
| AG0605 | PMA |
| AG0606 | PMA |
| AG0623 | PMA |
| AG0674 | PMA |
| AG0720 | PMA |
| AG0759 | PMA |
| AG0794 | PMA |
| AG0796 | PMA |
| AG0825 | PMA |
| AG0830 | PMA |
| AG0834 | PMA |
| AG0847 | PMA |
| AG0854 | PMA |
| AG0857 | PMA |
| AG0862 | PMA |
| AG1914 | PMA |
| B5457-01 | PMA |
| CS4003-02 | PMA |
| H412505 | PMA |
| H555015 | PMA |
| H555070 | PMA |
| SP3816-14-1010 | PMA |
| SP3816-14-1240 | PMA |
| SP3816-14-1260 | PMA |
| SP3816-14-1280 | PMA |
| SP3816-14-1290 | 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.