FAA · Type Certificate Data Sheet
TCDS R00008RD
Bell Helicopter Textron Canada Limited
Models covered (1)
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 ST0118DS-R-A-1 Proof of Structure, Landing Gear Limit Drop Test and Reserve Energy Absorption Drop Test
Specific sections
- Sec. 21.29
- Sec. 27.7
- Sec. 21.183
- Sec. 21.185
- Sec. 27.307
- Sec. 27.723
- Sec. 27.725
- Sec. 27.995
- Sec. 27.1545
Former holders
- Bell Helicopter Textron Canada Limited\Bell Helicopter Textron Canada Limited
- Bell Helicopter Textron Canada Limited
Fleet view · 63 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
5
n=63
Horsepower
460
460–505
Year of mfr
2018
2017–2019
Engines on the type, by tail count
- SAFRAN ARRIUS 2R 38
- TURBOMECA ARRIUS 2R 11
- AMA/EXPR UNKNOWN ENG 1
NTSB events
40
across all model variants
Applicable ADs
23
FAA airworthiness directives
Per-tail rate
0.63 events / tail · 0.37 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.