Safety record in brief:1 NTSB accident (substantial damage, Sep 2017)6 ADs may apply2 service difficulty reports
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Individual owners are shown by city and state only.
The bus driver's failure to maintain clearance from the standing airplane during dark night conditions. Contributing to the accident was the airport's lack of an escort for the bus.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for CEN17LA350)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2025-02-09 | Fuselage | Mar 18, 2025 | Airframe (EMB-120ER) |
| 2017-10-04 | Landing Gear | Jun 29, 2017 | Airframe (EMB-120ER) |
| 2012-26-08 | Pratt & Whitney Canada Corp. Turboprop Engines | Feb 15, 2013 | Engine (PW118)Serial numbers per P&WC ASB No. PW100-72-A21813 Rev 3, PW100-72-A21802 Rev 4, and PW100-72-A21798 Rev 5. Only with: Engines with propeller shafts having serial numbers listed in the referenced P&WC ASBs. |
| 2008-04-18 R1 | EMBRAER Model EMB-120, -120ER, -120FC, -120QC, and -120RT Airplanes | Nov 16, 2009 | Airframe (EMB-120ER) |
| 2007-26-21 | EMBRAER Model EMB-120, -120ER, -120FC, -120QC, and -120RT Airplanes | Feb 20, 2008 | Airframe (EMB-120ER) |
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2003-21-03 | Pratt & Whitney Canada Models PW118, PW120, PW120A, and PW121 Turboprop Engines | Nov 20, 2003 | Engine (PW118) |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
THE FOLLOWING CORRODED PARTS WERE REMOVED AND REPLACED: (1) FRAME 16, RH T-CHANNEL CORRODED. REMOVED AND REPLACED T-CHANNEL PER SRM 51-40-02 PN 120-08896-001 SN NSN. (2) RH CENTER “T” PROFILE AT FRAME 40 CORRODED. REMOVED AND REPLACED AFT RH “T” PROFILE PER SRM 51-40-02 PN 120-04449-001 SN NSN.…
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING FLIGHT RH ENGINE EEC FAILURE ANNUNCIATED WITH POWER REDUCTION TO ZERO PERCENT TORQUE. CREW PERFORMED QRH PROCEDURE, UNABLE TO RESTORE POWER ABOVE FLT IDLE. AIRCRAFT DIVERTED TO SUITABLE AIRPORT WITH PROPELLER IN FEATHER. AFTER LANDING ENGINE POWER AND EEC SYSTEM CHECKED, COULD NOT…
From FAA Service Difficulty Reports; matched by N-number and serial number.