Airbus A310
19,802 parts applicable to this airframe — widebody
| Part Number | Status |
|---|---|
| 353760WD | PMA |
| 378059WE | PMA |
| 52A442-13 | PMA |
| 52A442-3 | PMA |
| 52A442-5 | PMA |
| 52A442-7 | PMA |
| 52A442-9 | PMA |
| 561-515-0003(S) | PMA |
| 561-515-0004(S) | PMA |
| 561-515-0012(S) | PMA |
| 561-515-0013(S) | PMA |
| 561-515-0014(S) | PMA |
| 561-515-0015(S) | PMA |
| 6001-0237SD | PMA |
| 695-175 | PMA |
| 695-600 | PMA |
| 728775WD | PMA |
| 740801-6WD | PMA |
| 9-310726-4 | PMA |
| 9-3161453-3 | PMA |
| 9-3162059-2 | PMA |
| 9-3162467-1 | PMA |
| 9-3163809-6 | PMA |
| 9-3163811-7 9-3163811-7 | PMA |
| 9-3163812-12 | PMA |
| 9-3164707-1 | PMA |
| 9-3164709-2 | PMA |
| 9-3166458-1 | PMA |
| 9-3166459-2 | PMA |
| 9-3167312-1 | PMA |
| 9-3172594-2 | PMA |
| 9-3176646-1 | PMA |
| 9-3181650-1 | PMA |
| 9-3182176-1 | PMA |
| 9-3236158-1 9-3236158-1 | PMA |
| 9-690200-4 | PMA |
| 9-858886-14 | PMA |
| 9-858887-4 | PMA |
| 9-858888-3 | PMA |
| A731411B | PMA |
| AECI PN 24D507239P02AEC | PMA |
| AECI PN 3876024-6AEC | PMA |
| AECI PN 5909892AEC | PMA |
| AECI PN 813387-2AEC | PMA |
| AECI PN 813387-3AEC | PMA |
| P40810 | PMA |
| P40890 | PMA |
| P880500-1 | PMA |
| SP2570-00-10195 | PMA |
| SP2570-00-4045 | 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.