Safety record in brief:1 NTSB accident (substantial damage, Sep 2018)6 ADs may apply155 service difficulty reports
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an encounter with severe turbulence, which caused the improperly secured cargo to shift and damage the airplane floor structure.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for DCA18CA303)
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.
EMPTY LEG REPOSITION FLIGHT FROM KYIP TO KCAK. CLIMBING THROUGH 14,000' AFTER DEPARTING KYIP THE EMERGENCY DC BUS #2 FAILED. EMERGENCY WAS DECLARED WITH ATC AND CREW REQUESTED DIVERSION BACK TO KYIP. LANDING GEAR COLLAPSED UPON LANDING AND AIRCRAFT EXITED THE RUNWAY. INVESTIGATION IS UNDERWAY WITH…
From FAA Service Difficulty Reports; matched by N-number and serial number.FABRICATED, LOCATED, AND DRILLED REPAIR DOUBLER (PER EMB120 SRM 51-40-04 REV 58 AND ETD 2019-120-067917). INSTALLED REPAIR DOUBLER (PER EMB120 SRM 51-40-02 REV 58 AND ETC 2019-120-067917). PN: 120-37974-001 RH INTERMEDIATE COWL SHIM
From FAA Service Difficulty Reports; matched by N-number and serial number.UPPER SURFACE OF LH FLOOR BOARD ATTACH ANGLE BETWEEN FRAMES 15A - 16A WAS FOUND TO HAVE CORROSION. REMOVED FLOOR SILL (REF. SRM 51-40-02 REV 58). INSTALLED NEW FLOOR SILL (REF. SRM 51-40-02 REV 58). PN: 120-05802-001 SILL
From FAA Service Difficulty Reports; matched by N-number and serial number.REMOVED FLOOR BEAM UPPER SURFACE (REF. SRM 51-25-00). INSTALLED NEW FLOOR BEAM AT FRAMES 17 - 18 (REF. SRM 51-40-02 REV 58). PN: 120-05805-603 BUTT STRAP REPLACES 120-05805-003
From FAA Service Difficulty Reports; matched by N-number and serial number.FLOOR BEAM SEGMENT CORRODED . INSTALLED A NEW FLOOR BEAM SEGMENT IAW SRM 51-40-02 REV 58.
From FAA Service Difficulty Reports; matched by N-number and serial number.REMOVAL AND INSTALLATION OF CARGO DOOR THRESHOLD COVER PLATE COMPLETE (PER ETD 2019-120-062528). PN: 120-16200-001 LOWER CARGO DOOR BEAM
From FAA Service Difficulty Reports; matched by N-number and serial number.REMOVED DAMAGED FRAME AND MATCH DRILLED NEW FRAME IAW SRM 51-40-02 REV 58. INSTALLED A NEW FRAME 30 SEGMENT IAW SRM 51-40-02 REV 58.
From FAA Service Difficulty Reports; matched by N-number and serial number.SHEAR TIE CORROED. REMOVED FR 19 SEGMENT FROM STR 1R-15R AND 2 DOUBLERS IAW SRM 51-40-02 REV 58. INSTALLED NEW FRAME AND 2 DOUBLERS IAW SRM 51-40-02 REV 08.
From FAA Service Difficulty Reports; matched by N-number and serial number.REMOVED DAMAGED AREA ON FRAME 35 BETWEEN STRINGERS 3 AND 4R IAW SRM 51-40-02, AND 53-00-04, REV 58. INSTALLED A REPAIRED DOUBLER IAW SRM 53-00-04, REV 58.
From FAA Service Difficulty Reports; matched by N-number and serial number.REWORKED DENT IAW SRM 51-7400 REV 58. CONFIRMED AFFECTED AREA CRACK FREE IAW NDIM 51-00-03 REV 3. TREATED, PRIMED, AND APPLIED TOPCOAT IAW CPM 51-21-04 REV 10.
From FAA Service Difficulty Reports; matched by N-number and serial number.Showing the 10 most recent of 155 reports.