Airbus A310
19,802 parts applicable to this airframe — widebody
| Part Number | Status |
|---|---|
| 04320073-0005B | PMA |
| 100565-1KT | PMA |
| 108685-1KT | PMA |
| 184465-1WE | PMA |
| 19GD122AI-4-1 | PMA |
| 19GD122WI-3-1 | PMA |
| 2000-21 | PMA |
| 221-4110-507SD | PMA |
| 230-2-9 | PMA |
| 27114-3WE | PMA |
| 2977-1 | PMA |
| 30-5000130-50001 | PMA |
| 3163812-10WE | PMA |
| 3169407-1WE | PMA |
| 3169407-2WE | PMA |
| 3173837-2WE | PMA |
| 3179383-1KT | PMA |
| 3183560-1WE | PMA |
| 38101AA-1 | PMA |
| 3880326AA-13 | PMA |
| 3880614AA-17 | PMA |
| 436005006EH | PMA |
| 580-292-040 | PMA |
| 580-292-041 | PMA |
| 70200-202 | PMA |
| 717001-1 | PMA |
| 7373057 | PMA |
| 7473011 | PMA |
| 87-05546-001 | PMA |
| 887986-3JA | PMA |
| 887986-4JA | PMA |
| 90421-101 | PMA |
| Able-2839-1 | PMA |
| ADP38028-9 | PMA |
| ADV-3575-1251-07 | PMA |
| CS298-409EH | PMA |
| HSP800A67KT | PMA |
| M806022-02 | PMA |
| MDL-808-00 | PMA |
| P4-01-0019F-120 | PMA |
| RD-AM6618-5 | PMA |
| RD-AM6733-43 | PMA |
| RD-AM6775-63 | PMA |
| RD-AM6832-14 | PMA |
| RD-AM8126A2EK02 | PMA |
| RD-AM8126A2EK04 | PMA |
| SP2510-00-1020F | PMA |
| SP2510-00-1025D | PMA |
| SP2510-08-1025A | PMA |
| TAE0528-2 | 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.