Airbus A310
19,802 parts applicable to this airframe — widebody
| Part Number | Status |
|---|---|
| 110642-5 | PMA |
| 110842-5 | PMA |
| 129X58X132G | PMA |
| 14320-002C1 | OEM |
| 14320-002C2 | OEM |
| 1548T100-3A | PMA |
| 18J25-262, 18J25-387, 18J25-687, 18J25-737, 18J25-837 | PMA |
| 20122-560 | PMA |
| 20144-560 | PMA |
| 20176-560-1 | PMA |
| 20189-560 | PMA |
| 20E68-2, 20E68-3, 23E50-1, 23E50-2, 23E50-3 | PMA |
| 2100T100-3 | PMA |
| 2133T100-1 | PMA |
| 2135T100-1 | PMA |
| 2136T100-1 | PMA |
| 2137T100-1 | PMA |
| 2162T100-3 | PMA |
| 221-0001-501 | PMA |
| 221-0001-875 | PMA |
| 221-4001-501 | PMA |
| 221-4001-957 | PMA |
| 230-2-4 | PMA |
| 230-2-8, 230-2-9 | PMA |
| 267-1, 267-3, 267-5 | PMA |
| 30042-046-4 | PMA |
| 348-6-1, 348-7 | PMA |
| 400974-1 | PMA |
| 400974-3 | PMA |
| 4052510-972 | PMA |
| 4052510-973 | PMA |
| 4052510-974 | PMA |
| 4052510-975 | PMA |
| 51038 311 | PMA |
| 51208-311 | PMA |
| 51298-311 | PMA |
| 51387-311 | PMA |
| 51406-311 | PMA |
| 59019-263 | PMA |
| A2181030701100 | PMA |
| A2187407805000 | PMA |
| A2187412006000 | PMA |
| A2187633105200 | PMA |
| A2187648300800 | PMA |
| DEC92-003-505 | PMA |
| E10019-01 | PMA |
| H2954-1 | PMA |
| H3003-1 | PMA |
| H314619 | OEM |
| SHRI-1812HHSD604V2FP520LD Revision C | 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.