FAA · Type Certificate Data Sheet
TCDS H1CE
The Enstrom Helicopter Corporation
Models covered (14)
Special Airworthiness Information Bulletins (3)
Advisory bulletins on these airframes. Not mandatory like ADs — but operators tracking AD compliance often miss the SAIB on the same component.
- SW-12-10R1 Fuel Level Indication
- SW-05-81
- SW-09-30 Cracked Pylons
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 AT09299CH-R-P-1 Equivalent Level of Safety (ELOS) Finding for Crash Resistance Fuel System Components
Specific sections
- Sec. 27.2
- Sec. 21.25
- Sec. 27.337
- Sec. 27.351
- Sec. 27.775
- Sec. 3.4
- Sec. 21.50
- Sec. 27.29
- Sec. 27.395
- Sec. 27.401
- Sec. 27.501
- Sec. 27.613
- Sec. 27.629
- Sec. 27.663
- Sec. 27.685
- Sec. 27.727
- Sec. 27.783
- Sec. 27.861
- Sec. 27.1541
Fleet view · 340 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
3
3–5 (n=340)
Horsepower
205
180–420
Cruise (kts)
75
75–75
Year of mfr
1988
1966–2026
Engines on the type, by tail count
- LYCOMING HIO-360 SER 92
- LYCOMING HI0-360 SER 52
- ROLLS-ROYC 250-C20W 45
- LYCOMING HIO-360-F1AD 31
- LYCOMING I0360 SER 28
- ALLISON 250 SER 8
- LYCOMING HIO-360-E1AD 5
- LYCOMING I0-360-B1E 4
NTSB events
143
across all model variants
Applicable ADs
158
FAA airworthiness directives
Per-tail rate
0.42 events / tail · 0.46 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.