FAA · Type Certificate Data Sheet
TCDS T00063IB
Airbus SAS
Special Conditions + ELOS findings
Certification-time deviations: SCs add requirements where the design is novel; ELOS allows alternative compliance. Most modern types have both.
- SC 25-873-SC Special Conditions: Aerocon Engineering Company, Airbus Model A350-941 Airplane; Forward Lower Lobe Crew Rest Compartment Installation
- ELOS ST19206IB-T -25.251(b) Equivalent Level of Safety (ELOS) Finding for Vibration/Buffeting Compliance Criteria, Large Antenna Installation
- ELOS AT12025IB-T-F-23 Equivalent Level of Safety (ELOS) Finding for Vibration/Buffeting Compliance Criteria, Ka Band Satcom System Installation
- ELOS ST11630IB-T-F-1 Equivalent Level of Safety (ELOS) Finding for Vibration/Buffeting Compliance Criteria, Ka Band Satcom System Installation
- ELOS ST11631IB-T-F-1 Equivalent Level of Safety (ELOS) Finding for Vibration/Buffeting Compliance Criteria, Ka Band Satcom System Installation
- ELOS AT11173IB-T-25.1443-1 quivalent Level of Safety (ELOS) Finding for Airbus Model A350, Portable First Aid Oxygen Equipment
- ELOS AT11145IB-T-25.1563-1 Airspeed Placard
- ELOS AT11003IB-T-CS-1015 Finding for Type A-plus emergency exits on a Model A350
- ELOS TC0544IB-T-P-7 Throttle Motion During Reduced Thrust (Flexible) Takeoff or Soft Go-Around
Certification basis — 14 CFR
Specific sections
- Sec. 21.29
- Sec. 43.16
- Sec. 21.101
- Sec. 25.107
- Sec. 25.331
- Sec. 25.341
- Sec. 25.365
- Sec. 25.471
- Sec. 25.473
- Sec. 25.477
- Sec. 25.479
- Sec. 25.481
- Sec. 25.485
- Sec. 25.491
- Sec. 25.493
- Sec. 25.495
- Sec. 25.499
- Sec. 25.503
- Sec. 25.507
- Sec. 25.511
- Sec. 25.519
- Sec. 25.562
- Sec. 25.671
- Sec. 25.723
- Sec. 25.779
- Sec. 25.783
- Sec. 25.795
- Sec. 25.801
- Sec. 25.803
- Sec. 25.807
- Sec. 25.809
- Sec. 25.811
- Sec. 25.812
- Sec. 25.813
- Sec. 25.831
- Sec. 25.841
- Sec. 25.843
- Sec. 25.856
- Sec. 25.933
- Sec. 25.934
- Sec. 25.963
- Sec. 25.979
- Sec. 25.981
- Sec. 91.403
- Sec. 25.1191
- Sec. 25.1193
- Sec. 25.1195
- Sec. 25.1203
- Sec. 25.1301
- Sec. 25.1305
- Sec. 25.1309
- Sec. 25.1317
- Sec. 25.1329
- Sec. 25.1383
- Sec. 25.1411
- Sec. 25.1415
- Sec. 25.1419
- Sec. 25.1438
- Sec. 25.1441
- Sec. 25.1443
- Sec. 25.1447
- Sec. 25.1457
- Sec. 25.1529
- Sec. 25.1535
- Sec. 25.1549
- Sec. 21.50
Former holders
- Airbus
Fleet view · 13 registered tails
Engineering specs aggregated from the FAA Aircraft Registry — what every actually-flying tail under this TCDS reports. Median + 10th–90th-percentile range across the active fleet.
Seats
442
n=13
Year of mfr
2018
2017–2020
Engines on the type, by tail count
- ROLLS-ROYC TRENT XWB-84 13
NTSB events
1
across all model variants
Applicable ADs
50
FAA airworthiness directives
Per-tail rate
0.08 events / tail · 3.85 ADs / tail
The TCDS PDF on drs.faa.gov is the authoritative document for design-as-certified weight limits, performance, equipment, AD compliance times, and operating limitations. Open on drs.faa.gov ↗ DRS frequently breaks — when it does, the fleet view above and the cross-links below are usually what you actually need.