FAA · Type Certificate Data Sheet
TCDS H7EU
Leonardo S.p.A.
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 27-051-SC Special Conditions: AgustaWestland Philadelphia Corporation, Leonardo S.p.A. \nModel A119 and AW119 MKII Helicopters; Pressure Refueling and Fueling \nProvisions
Specific sections
- Sec. 21.29
- Sec. 21.50
- Sec. 27.29
- Sec. 27.33
- Sec. 27.65
- Sec. 27.71
- Sec. 27.151
- Sec. 27.161
- Sec. 27.173
- Sec. 27.175
- Sec. 27.307
- Sec. 27.321
- Sec. 27.337
- Sec. 27.339
- Sec. 27.351
- Sec. 27.361
- Sec. 27.391
- Sec. 27.395
- Sec. 27.397
- Sec. 27.427
- Sec. 27.501
- Sec. 27.563
- Sec. 27.571
- Sec. 27.602
- Sec. 27.603
- Sec. 27.613
- Sec. 27.663
- Sec. 27.672
- Sec. 27.727
- Sec. 27.779
- Sec. 27.783
- Sec. 27.807
- Sec. 27.863
- Sec. 27.917
- Sec. 27.923
- Sec. 27.927
- Sec. 27.955
- Sec. 27.967
- Sec. 27.975
- Sec. 27.977
- Sec. 27.997
- Sec. 27.1027
- Sec. 27.1041
- Sec. 27.1043
- Sec. 27.1045
- Sec. 27.1141
- Sec. 27.1143
- Sec. 27.1145
- Sec. 27.1189
- Sec. 27.1193
- Sec. 27.1305
- Sec. 27.1327
- Sec. 27.1337
- Sec. 27.1411
- Sec. 27.1415
- Sec. 27.1501
- Sec. 27.1525
- Sec. 27.1545
- Sec. 27.1547
- Sec. 27.1559
- Sec. 29.45
- Sec. 29.49
- Sec. 29.51
- Sec. 29.53
- Sec. 29.55
- Sec. 29.59
- Sec. 29.60
- Sec. 29.61
- Sec. 29.62
- Sec. 29.64
- Sec. 29.65
- Sec. 29.67
- Sec. 29.75
- Sec. 29.77
- Sec. 29.79
- Sec. 29.81
- Sec. 29.85
- Sec. 29.87
- Sec. 21.183
- Sec. 21.185
- Sec. 29.571
- Sec. 29.861
- Sec. 29.901
- Sec. 29.903
- Sec. 29.908
- Sec. 29.923
- Sec. 29.927
- Sec. 29.953
- Sec. 29.1027
- Sec. 29.1045
- Sec. 29.1047
- Sec. 29.1181
- Sec. 29.1187
- Sec. 29.1189
- Sec. 29.1191
- Sec. 29.1193
- Sec. 29.1195
- Sec. 29.1305
- Sec. 29.1309
- Sec. 29.1323
- Sec. 29.1331
- Sec. 29.1351
- Sec. 29.1587
- Sec. 27.1317
- Sec. 29.86
- Sec. 29.90
- Sec. 29.1197
- Sec. 29.1199
- Sec. 29.1201
Former holders
- Agusta S.p.A.
Fleet view · 350 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
8
n=350
Horsepower
900
450–900
Year of mfr
2019
1980–2025
Engines on the type, by tail count
- P&W CANADA PT6B-37A 187
- P&W CANADA PW207C 48
- P&W CANADA PW206C 41
- ALLISON 250-C20 SER 18
- ROLLS-ROYC 250-C20R/1 6
- P&W PT6 SERIES 5
- P&W CANADA PW206A 4
- AMA/EXPR UNKNOWN ENG 3
NTSB events
16
across all model variants
Applicable ADs
75
FAA airworthiness directives
Per-tail rate
0.05 events / tail · 0.21 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.