Airbus A310
19,802 parts applicable to this airframe — widebody
| Part Number | Status |
|---|---|
| 0FV9500A01G01G | PMA |
| 0FV9600A01G01G | PMA |
| 0FV9700A01G01G | PMA |
| 1730792-00-44 | PMA |
| 19205031G | PMA |
| 20029-20 | PMA |
| 20040-30M | PMA |
| 229-10 | PMA |
| 229-20 | PMA |
| 32833 | PMA |
| 33194 | PMA |
| 400300-1 | OEM |
| 400300-2 | OEM |
| 427-VAC | PMA |
| 45533001G/ 45533003G | PMA |
| 51050-311 | PMA |
| 5500-C1A-BF20B | OEM |
| 78845R1G/ 78845R2G | PMA |
| 804-1250-10 | PMA |
| 809271-3G | PMA |
| 9-3169756-4 | PMA |
| 960-2227-005-001 | PMA |
| A32266KT | PMA |
| A35994KT | PMA |
| AR4707-1 | PMA |
| CM358474-1 | PMA |
| CM3614423-1 | PMA |
| D2547115520000G | PMA |
| G3N543-XX | PMA |
| P00263 | PMA |
| PMA1088A | PMA |
| PMA1697-10 | PMA |
| PMA1697-20 | PMA |
| PMA180-146B | PMA |
| PMA2510-0010-01 | PMA |
| PMA2510-0032-05 | PMA |
| PMA3510-0040-01 | PMA |
| PMA3510-0041-03 | PMA |
| PMA413-0001-1 | PMA |
| PMA416-0001-9 | PMA |
| PMA416-0201-11 | PMA |
| PMA420-0001-5 | PMA |
| PMA425-0001-11 | PMA |
| PMA425-0001-5 | PMA |
| PMA500-0001-1 | PMA |
| PMA50448 | PMA |
| PT72067000 | PMA |
| RGS2425-001G, -101G, -103G | PMA |
| TG3844038-4 | PMA |
| TG3844080-1 | 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.