TCDS R00002LA
Current · Aircraft · Rotorcraft · Rev 2 (09/19/2003) · FAA TCDS database
San Joaquin Helicopters 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)
Airworthiness directives (6) · mandatory: an aircraft out of compliance is not airworthy
- 2014-26829 Airworthiness Directives; Various Restricted Category Helicopters 2014-11-14
- 2014-12737 Airworthiness Directives; Various Restricted Category Helicopters 2014-06-02
- 2012-17279 Airworthiness Directives; Various Restricted Category Helicopters 2012-07-23
- E6-12420 Airworthiness Directives; Rolls-Royce Corporation (Formerly Allison Engine Company, Allison Gas Turbine Division, and Detroit Diesel Allison) (RRC) 250-B and 250-C Series Turboshaft and Turboprop Engines 2006-08-03
- 06-5547 Airworthiness Directives; Rolls-Royce Corporation (Formerly Allison Engine Company, Allison Gas Turbine Division, and Detroit Diesel Allison) 250-B and 250-C Series Turboprop and Turboshaft Engines 2006-06-21
- 05-22437 Airworthiness Directives; Rolls-Royce Corporation (formerly Allison Engine Company, Allison Gas Turbine Division, and Detroit Diesel Allison) 250-B and 250-C Series Turboprop and Turboshaft Engines 2005-11-10
Certification basis — 14 CFR
Specific sections
- Sec. 36.1
- Sec. 137.3
- Sec. 21.25
- Sec. 21.101
- Sec. 91.313
- Sec. 27.1529
Former holders
- San Joaquin Helicopters
Fleet view · 1 registered tails · FAA registry, median and p10–p90
- Seats
- 5
- n=1
- Horsepower
- 420
- n=1
- Year of mfr
- 1970
- 1970–1970
Engines on the type, by tail count
- ALLISON 250-C20C 1
- NTSB events
- 0
- across all model variants
- Applicable ADs
- 6
- FAA airworthiness directives
- Per-tail rate
- 0.00 events / tail · 6.00 ADs / tail