TCDS 2A8
Historical · Aircraft · Small Airplane · Rev 20 (11/30/2000) · FAA TCDS database
Latino American De Aviacion (Lavia) S.A. TCDS PDF (direct) ↗ drs.faa.gov ↗
The TCDS PDF on drs.faa.gov is authoritative for design-as-certified weight limits, performance, equipment and operating limitations.
Models covered (3)
SAIBs (2)
Certification basis — 14 CFR
Specific sections
- Sec. 21.29
- Sec. 21.183
- Sec. 21.185
Former holders
- Piper Aircraft, Inc., The New
Engineering specs · extracted from TCDS PDF, union across models
- Vne · never exceed
- 118 kt
- Vno · max struct cruise
- 94 kt
- Va · maneuvering
- 104 kt
- Vfe · flaps extended
- 83 kt
- Max gross
- 2,300 lbs
- Seats
- 1
- Fuel
- 40 gal
- Oil
- 2 gal
Engines (per TCDS)
- — Lycoming O-320-A1A
- — Lycoming O-540-B2B5 or O-540-B2C5 with carburetor setting
- — Lycoming O-540-G1A5 or O-540-G2A5 with carburetor setting
Fuel grade 80/87 minimum grade aviation gasoline
Fleet view · 456 registered tails · FAA registry, median and p10–p90
- Seats
- 1
- n=456
- Horsepower
- 250
- 180–250
- Cruise (kts)
- 93
- 81–93
- Year of mfr
- 1966
- 1959–1979
Engines on the type, by tail count
- LYCOMING 0-540 SERIES 333
- LYCOMING 0-320 SERIES 44
- LYCOMING O-540-B2B5 18
- LYCOMING O-540-B2C5 12
- LYCOMING O-540-G1A5 4
- LYCOMING 0-540F1 SERIE 4
- CONT MOTOR E225 SERIES 3
- LYCOMING O-320-A2B 3
- NTSB events
- 260
- across all model variants
- Applicable ADs
- 118
- FAA airworthiness directives
- Per-tail rate
- 0.57 events / tail · 0.26 ADs / tail