Airbus A310
19,802 parts applicable to this airframe — widebody
| Part Number | Status |
|---|---|
| 1378M86P01WD | PMA |
| 20-624102-002 | PMA |
| 26542 | PMA |
| 2739 | PMA |
| 2739-2 | PMA |
| 31-1816-1SD | PMA |
| 31-1816-2SD | PMA |
| 3210-005WN011 | PMA |
| 341960WD | PMA |
| 34600006 | PMA |
| 34600016 | PMA |
| 35200002 | PMA |
| 35203375 | PMA |
| 3860180AA-6 | PMA |
| 427-F-AA | PMA |
| 439009239EH | PMA |
| 607428-0001 | PMA |
| 611053EH | PMA |
| 617-6559-002 | PMA |
| 717001-3 | PMA |
| 728775JP | PMA |
| 7373041 | PMA |
| 74728-01 | PMA |
| 910020-5140 | PMA |
| 914004 | PMA |
| A2181229304800 | PMA |
| A2181232600400 | PMA |
| A2181267300400 | PMA |
| A2181274400200 | PMA |
| A2181274600500 | PMA |
| A2187441700400 | PMA |
| A2187441711200 | PMA |
| A35304KT | PMA |
| A35994 | OEM |
| AA630124-04 | PMA |
| AA64206-7 | PMA |
| AAD17851-27 | PMA |
| AAD17851-29CW | PMA |
| Able-2852-2 | PMA |
| IFE89106 | PMA |
| KT5908745 | PMA |
| LA00700X250A20B6 | PMA |
| P00436 | PMA |
| PF3101874-1 | PMA |
| PF3844012-3 | PMA |
| PF3844038-4 | PMA |
| PF3844080-1 | PMA |
| PF3844080-2 | PMA |
| SP20141B | PMA |
| UL10-05VSP1 | 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.