Airbus A310
19,802 parts applicable to this airframe — widebody
| Part Number | Status |
|---|---|
| 113063-01G | PMA |
| 20-00343 | PMA |
| 20030-560 | PMA |
| 20074-560 | PMA |
| 20133-560 | PMA |
| 20204-560 | PMA |
| 30039-046-1 | PMA |
| 30090-046, -1, -2 | PMA |
| 379103D-15 | PMA |
| 41422001G | PMA |
| 43022-169 | PMA |
| 45001-510 | PMA |
| 45099-510 | PMA |
| 51242-311-13 | PMA |
| 51293-311 | PMA |
| 51306-311 | PMA |
| 51331-311 | PMA |
| 51337-311 | PMA |
| 51338-311 | PMA |
| 51340-311 | PMA |
| 59029-263 | PMA |
| 638-0776 | PMA |
| 638-0777 | PMA |
| 8102-411NW | PMA |
| 814893-401G | PMA |
| 822619-403G | PMA |
| 9541-11G | PMA |
| A2181030700400 | PMA |
| A2181201004400 | PMA |
| A2181229301200 | PMA |
| A2181230700100 | PMA |
| A2181231100200 | PMA |
| A2181255200400 | PMA |
| A2181256000200 | PMA |
| A2181265400600 | PMA |
| A2181265500900 | PMA |
| A2181270400200 | PMA |
| A2181275900500 | PMA |
| A2183177100000 | PMA |
| A2187441803600 | PMA |
| A2188526706000 | PMA |
| AC9780F15Y25 | PMA |
| GI1975-1 | PMA |
| GI1979 | PMA |
| H10003314 | PMA |
| H5100-2-115-164 | PMA |
| L45003-401G | PMA |
| SG-A310-E200 | PMA |
| SG-A310-F200 | PMA |
| SG-A310-S200 | 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.