Airbus A310
19,802 parts applicable to this airframe — widebody
| Part Number | Status |
|---|---|
| 2120-03 | PMA |
| 22M1018-501, 22M1018-503, 22M1018-505 | PMA |
| 22M1022 | PMA |
| 32800-1710 | PMA |
| 4296-6 | PMA |
| 9704 | PMA |
| A21810658008 | PMA |
| A2187634605000 | PMA |
| A2187648101200 | PMA |
| A2187657710200 | PMA |
| ABG7V-102 | PMA |
| ACR-6-33/*PMA | PMA |
| ACR-6-34/*PMA | PMA |
| AG4VCRP1 | PMA |
| AMBK3-4007 | PMA |
| AMBK4-4015 | PMA |
| AMBK4-4016 | PMA |
| AMBK4-4017 | PMA |
| AMBK4-4018 | PMA |
| AMBK4-4019 | PMA |
| AMBK4-4054 | PMA |
| AMBK4-4058 | PMA |
| AMBK4-4059 | PMA |
| AMBK4-4060 | PMA |
| AMBK4-4062 | PMA |
| AMBK4-4063 | PMA |
| AMBK4-4078 | PMA |
| AR138 | PMA |
| AR13852 | OEM |
| AR146 | PMA |
| AR2510 | PMA |
| AR2510-4S69 | PMA |
| AR2518 | PMA |
| AR2713-2-091-091 | PMA |
| AR2713-2-374-413 | PMA |
| AR34 | PMA |
| AR52 | PMA |
| CS4003-2 | PMA |
| DEC31-141-501 | PMA |
| DEC31-141-503 | PMA |
| DEC31-142-501 | PMA |
| DEC31-143-501 | PMA |
| DS-961596 | PMA |
| HT4V-102 | PMA |
| JL-J7A | PMA |
| MDL-92-06-001 | PMA |
| V2651D516C00 | PMA |
| V2651D516COA | PMA |
| WSI-333-() | PMA |
| WSI-4-() | 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.