FAA · Type Certificate Data Sheet
TCDS A60EU
EADS SOCATA
Models covered (1)
Special Airworthiness Information Bulletins (12)
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 ACE-14-01 Cockpit Controls Location and 14 CFR 23.781(b), Shape Single Power Lever
Specific sections
- Sec. 21.21
- Sec. 21.29
- Sec. 21.93
- Sec. 23.49
- Sec. 21.183
- Sec. 23.561
- Sec. 23.562
- Sec. 23.783
- Sec. 23.785
- Sec. 23.807
- Sec. 23.811
- Sec. 23.1301
- Sec. 23.1308
- Sec. 23.1309
- Sec. 23.1311
- Sec. 23.1322
- Sec. 23.1323
- Sec. 23.1331
- Sec. 23.1353
- Sec. 23.1365
- Sec. 23.1431
- Sec. 23.207
- Sec. 23.777
- Sec. 23.781
- Sec. 23.1306
- Sec. 23.1529
- Sec. 23.1305
Former holders
- EADS SOCATA
- EADS SOCATA\SOCATA
Fleet view · 647 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
7
n=647
Horsepower
850
700–850
Year of mfr
2010
1990–2018
Engines on the type, by tail count
- P&W CANADA PT6A66D 196
- P&W PT6A66D 164
- P&W PT6A SER 93
- P&W CANADA PT6A-64 87
- P&W CANADA PT6A-66 SER 59
- P&W CANADA PT6A-6 SERIES 18
- P&W CANADA PT6A-66 7
- P&W CANADA PT6A-60A 4
NTSB events
80
across all model variants
Applicable ADs
13
FAA airworthiness directives
Per-tail rate
0.12 events / tail · 0.02 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.