FAA · Type Certificate Data Sheet
TCDS A18SO
Piper Aircraft Inc.
Models covered (1)
Applicable airworthiness directives (11)
ADs joined from the FAA Federal Register by (Piper Aircraft Inc. × model). Click any AD to see the full Federal Register record. Mandatory; flying out of compliance grounds the airplane.
- 06-957 Airworthiness Directives; Aero Advantage ADV200 Series (Part Numbers ADV211CC and ADV212CW) Vacuum Pumps 2006-02-07
- 05-10864 Airworthiness Directives; Precise Flight, Inc. Models SVS I and SVS IA Standby Vacuum Systems 2005-06-07
- 05-9366 Airworthiness Directives; Aero Advantage ADV200 Series (Part Numbers ADVPL211CC and ADVPL212CW) Vacuum Pumps 2005-05-11
- 05-4239 Airworthiness Directives; Precise Flight, Inc. Models SVS I and SVS IA Standby Vacuum Systems 2005-03-04
- 01-29325 Airworthiness Directives; GARMIN International GNS 430 Units 2001-12-03
- 01-19094 Airworthiness Directives; GARMIN International GNS 430 Units 2001-08-06
- 99-30519 Airworthiness Directives; Precise Flight, Inc. Model SVS III Standby Vacuum Systems 1999-11-30
- 99-16911 Airworthiness Directives; Precise Flight, Inc. Model SVS III Standby Vacuum Systems 1999-07-07
- 98-30170 Airworthiness Directives; Parker Hannifan Airborne Dry Air Pumps, Conversion Kits, and Coupling Kits 1998-11-17
- 98-2776 Airworthiness Directives; The New Piper Aircraft Corporation Model PA-38-112 Airplanes 1998-02-11
- 97-11778 Airworthiness Directives; The New Piper Aircraft, Inc. Model PA- 38-112 Airplanes 1997-05-07
Certification basis — 14 CFR
Specific sections
- Sec. 23.1545
Fleet view · 442 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
2
n=442
Horsepower
115
n=417
Cruise (kts)
183
183–183
Year of mfr
1978
1978–1982
Engines on the type, by tail count
- LYCOMING 0-235 SERIES 409
- LYCOMING O-235-L2C 4
- LYCOMING 0-320 SERIES 2
- LYCOMING R680E SERIES 1
- CONT MOTOR A50 SERIES 1
NTSB events
131
across all model variants
Applicable ADs
11
FAA airworthiness directives
Per-tail rate
0.30 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.