Safety record in brief:1 NTSB incident (Feb 2000)6 ADs may apply101 service difficulty reports
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Moisture contamination of the elevator trim actuator units resulting in their failure to operate at below freezing temperatures
From NTSB records; matched by serial number.Read NTSB report (search CAROL for LAX00IA106)
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.
PILOT REPORTED AFTER DEPARTURE FROM BQN DURING CLIMB OUT AT APPROX 11,000FT THE LEFT ENGINE TORQUE DROPPED TO 0, ENGINE OIL PRESSURE DROPPED TO 0 SUBSEQUENTLY ENGINE SHUTDOWN. AIRCRAFT RETURNED TO BQN AND LANDED WITHOUT INCIDENT. BQN MX ATTEMPTED TO MOTOR ENGINE, STARTER ROTATED, ENGINE DID NOT…
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING MAJOR INSPECTION, FOUND FPI CRACK INDICATION IN FILLET RADIUS OF BLADE SHANK.
From FAA Service Difficulty Reports; matched by N-number and serial number.RED EMERGENCY LIGHTS ARE INOPERATIVE NEAR THE CABIN MAIN ENTRY DOOR. R & R THE LIGHT SOCKET ASSY AND REPAIRED WIRING, OPS CHECKED GOOD, IAW AMM AND WDM.
From FAA Service Difficulty Reports; matched by N-number and serial number.NR 4 FLOOR WHITE EMERGENCY LIGHT STRIP INOPERATIVE. REPLACED THE LAMP IN NR 4 FLOOR WHITE EMERGENCY LIGHT STRIP IAW AMM.
From FAA Service Difficulty Reports; matched by N-number and serial number.GOUGE APPROXIMATELY 3.5 INCHES LONG, .2500 INCHES WIDE, .0625 INCHES DEEP ON AFT FUSELAGE AT CARGO DOOR, WITHIN .2500 INCHES OF RIVETS BETWEEN SKIN EDGE AND RIVET ROW. OUT OF LIMITS IAW SRM. REMOVED DAMAGE SECTION AND INSTALLED DOUBLER ON EXTERNAL SKIN AFT OF CARGO DOOR CUT OUT SURROUNDING IAW ETD.
From FAA Service Difficulty Reports; matched by N-number and serial number.RIGHT PROPELLER SPEED WENT TO 103.7 PERCENT RPM. CHANGED PCU AND TRANSFER TUBE. OPS CHECK GOOD.
From FAA Service Difficulty Reports; matched by N-number and serial number.OXYGEN MASK DEPLOYED DURING FLIGHT. RESTOWED.
From FAA Service Difficulty Reports; matched by N-number and serial number.LT NACELLE FLAP INBD INTERIOR VERTICAL SUPPORT CRACKED. C-CHECK REPLACED LT NACELLE FLAP INTERIOR VERTICAL SUPPORT IAW SRM.
From FAA Service Difficulty Reports; matched by N-number and serial number.RT WING LOWER SMALL CLIP CRACKED AT RIB 15 2ND FROM FWD. C-CHECK REPLACED RT WING LOWER SMALL CLIP AT RIB 15, 2ND FROM FWD IAW SRM.
From FAA Service Difficulty Reports; matched by N-number and serial number.RT WING UPPER CLIP CRACKED 2ND FROM FWD AT RIB 20. C-CHECK REPLACED UPPER WING CLIP AT RT WING 2ND FROM FWD AT RIB 20, IAW SRM.
From FAA Service Difficulty Reports; matched by N-number and serial number.Showing the 10 most recent of 101 reports.