Airbus A310
19,802 parts applicable to this airframe — widebody
| Part Number | Status |
|---|---|
| 071-50013-0200 | PMA |
| 071-50014-0203 | PMA |
| 071-50015-0100 | PMA |
| 071-50016-0100 | PMA |
| 071-50017-0100 | PMA |
| 1003547-1AFI | PMA |
| 14J30-350 | PMA |
| 153DH1R197 | PMA |
| 18J24-338 | PMA |
| 18J25-262 | PMA |
| 18J25-287 | PMA |
| 18J25-387 | PMA |
| 18J25-687 | PMA |
| 18J25-737 | PMA |
| 18J25-837 | PMA |
| 20050-40M | PMA |
| 2151 | PMA |
| 240-11-1 | PMA |
| 300-80185-0002 | PMA |
| 369-1 | PMA |
| 3A3180-2 | PMA |
| 4-60001H883-00AEC | PMA |
| 44520 and 44570 | PMA |
| 44560 | OEM |
| 452MR17 | PMA |
| 45980 and 45990 | PMA |
| 45980-1 and 45990-1 | PMA |
| 53100-2 | PMA |
| 53100-3 | PMA |
| 58163-4WE | PMA |
| 58163-7WE | PMA |
| 733899-1AFI | PMA |
| 754327-2AFI | PMA |
| 7593802-101 | PMA |
| 77865-1 | PMA |
| 9143FR-2400 | PMA |
| 980-3008-006 | PMA |
| AR-30 | PMA |
| E1R643-XX | PMA |
| E2N122-XX | PMA |
| G1R323-XX | PMA |
| G3N542-XX | PMA |
| IC3882933-1 | PMA |
| LA555015 | PMA |
| MDL 12119 | PMA |
| P00084 | PMA |
| Report 20001 | PMA |
| TA71000415 | PMA |
| TA71000417 | PMA |
| TA71000437 | 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.