FAA · Type Certificate Data Sheet
TCDS A35EU
Airbus SAS
Models covered (69)
- A300 B4-103
- A300 B4-2C
- A310-203
- A300 B2K-3C
- A300 B4-622R
- A300 F4-605R
- A300 B4-601
- A300 B2-203
- A310-204
- A310-221
- A300 B4-603
- A300 B4-622
- A310-324
- A300 F4-622R
- A300 B4-620
- A300 C4-605R Variant F
- A310-322
- A300 B4-605R
- A310-325
- A310-304
- A310-222
- A300 B4-203
- A300B4-603
- A300B4-605R
- A300 Model B2-1A
- A300B4-620
- A300F4-605R
- A300 Model B2K-3C
- A300B4-601
- A300 Model B4-103
- A300F4-622R
- A300 Model B2-203
- A300 Model B2-1C
- A300 Model B4-203
- A300 Model B4-2C
- A300B4-622R
- A300; Model C4-605 Variant F
- A300; Model B4-622
- A300 B2-1C
- A300 B2-1A
- A300 Model B4-600R Series
- A300 Model F4-600R Series
- A300 Model B4-600 Series
- A310 Model 325
- A310 Model 300 Series
- A310 Model 200 Series
- A300; Model B4-601
- A310; Model 222
- A300; Model F4-605R
- A300; Model F4-622R
- A300; Model C4-605R Variant F
- A310; Model 204
- A300; Model B2-1A
- A300; Model B2-203
- A300; Model B4-103
- A310; Model 221
- A300; Model B2K-3C
- A310; Model 324
- A310; Model 304
- A300; Model B2-1C
- A310; Model 322
- A300; Model B4-605R
- A300; Model B4-2C
- A310; Model 203
- A300; Model B4-622R
- A300; Model B4-603
- A310; Model 325
- A300; Model B4-203
- A300; Model B4-620
Special Airworthiness Information Bulletins (4)
Advisory bulletins on these airframes. Not mandatory like ADs — but operators tracking AD compliance often miss the SAIB on the same component.
Special Conditions + ELOS findings
Certification-time deviations: SCs add requirements where the design is novel; ELOS allows alternative compliance. Most modern types have both.
- ELOS AT0007IB-T-P-102 Equivalent Level of Safety (ELOS) Finding for Airbus Model A300F4-622R airplane, FAA Project # AT0007IB-T
- ELOS TD0754IB-T-A-1 Repairs to Alteration Structure
- ELOS TD0754IB-T-A-2 Repairs to Alteration Structure
- ELOS TD0360IB-T-P-103 Thrust reverser design
- ELOS TD0797IB-T-P-104 Airbus project on Models A300-600, A300-600(R), A310-200, A310-300
Certification basis — 14 CFR
Specific sections
- Sec. 21.29
- Sec. 26.11
- Sec. 26.33
- Sec. 21.101
- Sec. 21.183
- Sec. 21.185
- Sec. 25.173
- Sec. 25.175
- Sec. 25.305
- Sec. 25.321
- Sec. 25.331
- Sec. 25.333
- Sec. 25.335
- Sec. 25.341
- Sec. 25.349
- Sec. 25.351
- Sec. 25.473
- Sec. 25.479
- Sec. 25.481
- Sec. 25.483
- Sec. 25.485
- Sec. 25.491
- Sec. 25.561
- Sec. 25.571
- Sec. 25.631
- Sec. 25.786
- Sec. 25.787
- Sec. 25.788
- Sec. 25.789
- Sec. 25.790
- Sec. 25.801
- Sec. 25.807
- Sec. 25.813
- Sec. 25.841
- Sec. 25.853
- Sec. 25.855
- Sec. 25.857
- Sec. 25.858
- Sec. 25.933
- Sec. 25.959
- Sec. 125.509
- Sec. 129.111
- Sec. 129.117
- Sec. 25.1419
- Sec. 25.1535
- Sec. 121.1111
- Sec. 121.1117
- Sec. 25.854
- Sec. 25.856
Former holders
- Airbus Industrie\Airbus
- Airbus
- Airbus Industrie
Comments
TC for A300, Model B2-1A & Model B2-1C was surrendered on 08/09/2023 and is indicated on the TCDS.
Fleet view · 124 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
380
347–380 (n=124)
Year of mfr
1999
1983–2007
Engines on the type, by tail count
- P & W PW4158 65
- GE CF6-80 SERIES 35
- P&W PW4000 SER 7
- GE CF6-80C2A5F 6
- GE CF6-80C2A5 3
- P & W JT9D SERIES 2
- GE CF6-6 2
- P & W PW2040 1
NTSB events
2
across all model variants
Applicable ADs
42
FAA airworthiness directives
Per-tail rate
0.02 events / tail · 0.34 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.