Airbus A310
19,802 parts applicable to this airframe — widebody
| Part Number | Status |
|---|---|
| 10101000CN | PMA |
| 160186 | PMA |
| 160192 | PMA |
| 35059-031 | PMA |
| 35059-033 | PMA |
| 35059-034 | PMA |
| 35059-035 | PMA |
| 35059-108 | PMA |
| 3606004-1WD | PMA |
| 3880160-4 | PMA |
| 396387WD (.003 oversize) | PMA |
| 396388WD (.005 oversize) | PMA |
| 396389WD (.007 oversize) | PMA |
| 396390WD (.010 oversize) | PMA |
| 5904761 | OEM |
| 5MA1703-1 | PMA |
| 70100-1 | PMA |
| 70100-3 | OEM |
| 70200-101 | OEM |
| 70200-102 | OEM |
| 70400-3 | OEM |
| 70600-2 | OEM |
| 72878-1 | PMA |
| 72878-2 | PMA |
| 72878-4 | PMA |
| 742140WD | PMA |
| 986120-1 | PMA |
| AD-774-034-44-1 | PMA |
| AN960C6 | OEM |
| AR2713-2-291291 | PMA |
| AR4754-2 | PMA |
| AR47541 | OEM |
| AR47543 | OEM |
| AR4764-1 | PMA |
| C62270 | OEM |
| C62866 | OEM |
| CRA50551 | OEM |
| D04705 | OEM |
| D68063 | OEM |
| Honeywell P/N: 358504-1 used in Honeywell Temperature Control Valves | OEM |
| HT50007 | PMA |
| J500ZZ20000-000 | PMA |
| J500ZZ21000-000 | PMA |
| J540AI1-110 | PMA |
| J540AI73000-000 | PMA |
| MS51957-28 | OEM |
| P00298 | PMA |
| P00315 | PMA |
| P00367 | PMA |
| PMA53100578-1, PMA53100578-2, PMA53100578-3, PMA53100578-4, PMA53100578-5 | 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.