Accident
Feb 25, 2011 · New York, NYImproper latching of the aft galley cart prior to landing.
- Injuries
- Serious
- Report
- DCA11CA036
From NTSB records; matched by serial number.Read NTSB report (search CAROL for DCA11CA036)
Safety record in brief:1 NTSB accident (Feb 2011)20 ADs may apply132 service difficulty reports
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Improper latching of the aft galley cart prior to landing.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for DCA11CA036)
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 |
|---|---|---|---|
| 2023-21-11 | Embraer S.A. (Type Certificate Previously Held by Yaborã Indústria Aeronáutica S.A.… | Dec 26, 2023 | Airframe (ERJ 190-100 IGW) |
| 2022-16-01 | Windows | Aug 15, 2022 | Airframe (ERJ 190-100 IGW)Only with: Equipped with any NORDAM passenger window having PMA P/N NP00038-3. |
| 2022-05-08 | Turbine Engine Oil System | Apr 11, 2022 | Engine (CF34-10E6)Only with: Stationary oil seal P/N B1316-00453 or B1316-01274 installed at No. 1 forward bearing that was repaired, overhauled, or entered service after August 2014 and has used high thermal stability or high performance capability oil for 56 FHs or more. |
| 2021-25-02 | Nacelles/ pylons | Jan 20, 2022 | Airframe (ERJ 190-100 IGW) |
| 2020-25-08 | Flight controls | Jan 21, 2021 | Airframe (ERJ 190-100 IGW)Serial numbers per ANAC AD 2020-05-01 (ERJ 170) and ANAC AD 2020-05-02 (ERJ 190) |
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2020-12-12 | Nacelles/ pylons | Aug 13, 2020 | Airframe (ERJ 190-100 IGW) |
| 2020-05-21 | Indicating/ recording systems | Apr 24, 2020 | Airframe (ERJ 190-100 IGW)Serial numbers per ANAC Brazilian AD 2019-10-01 |
| 2019-24-16 | Embraer S.A. Airplanes | Feb 3, 2020 | Airframe (ERJ 190-100 IGW)Certain serial numbers: 19000002; 19000004; 19000006–19000213; 19000215–19000276; 19000278–19000466; 19000468–19000525; … |
| 2019-19-03 | Fuselage | Oct 31, 2019 | Airframe (ERJ 190-100 IGW)Serial numbers per Embraer Service Bulletins SB170-53-0142 Rev 01, SB190-53-0098 Rev 01, and SB190LIN-53-0072 Rev 01 |
| 2019-03-21 | Landing Gear | Apr 2, 2019 | Airframe (ERJ 190-100 IGW) |
| 2017-21-09 | Fuselage | Nov 27, 2017 | Airframe (ERJ 190-100 IGW)Serial numbers per Embraer Service Bulletin 170-53-0051, Revision 03 (ERJ 170); Embraer Service Bulletin 190-53-0019, Revision 03 (ERJ 190) |
| 2016-12-14 | Pneumatic | Jul 27, 2016 | Airframe (ERJ 190-100 IGW) |
| 2013-25-04 | Embraer S.A. Airplanes | Feb 10, 2014 | Airframe (ERJ 190-100 IGW)Only with: ERJ 170 airplanes equipped with Goodrich escape slides P/N 4A4030-5; ERJ 190 airplanes equipped with Goodrich escape slides P/N 104003-2. |
| 2013-16-22 | Fuselage | Sep 27, 2013 | Airframe (ERJ 190-100 IGW)Serial numbers per Embraer Service Bulletins 170-53-0093 Rev 01, 190-53-0054 Rev 01, and 190LIN-53-0059 Rev 01, dated March 16, 2012 |
| 2013-11-17 | Pneumatic | Aug 6, 2013 | Airframe (ERJ 190-100 IGW)Only with: Having Hamilton Sundstrand low pressure check valve (LPCV) P/N 1001447-3 or 1001447-4 installed. |
| 2013-11-07 | Landing gear | Jul 9, 2013 | Airframe (ERJ 190-100 IGW)Serial numbers per EMBRAER Service Bulletin 190-57-0036, Revision 02, dated August 12, 2011; EMBRAER Service Bulletin 190LIN-57-0016, dated June 10, 2011 |
| 2013-05-12 | Fire Protection | May 3, 2013 | Airframe (ERJ 190-100 IGW)Serial numbers per Embraer Service Bulletins 170-26-0011 Rev 02, 190-26-0011 Rev 02, and 190LIN-26-0006 Rev 02 |
| 2013-03-13 | Doors | Mar 19, 2013 | Airframe (ERJ 190-100 IGW)Serial numbers per EMBRAER Service Bulletins 170-52-0055 Rev 01, 190-52-0038 Rev 01, and 190LIN-52-0020 |
| 2012-16-09 | Air Conditioning | Sep 21, 2012 | Airframe (ERJ 190-100 IGW) |
| 2012-15-03 | Landing Gear | Sep 4, 2012 | Airframe (ERJ 190-100 IGW) |
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.
AIRCRAFT WAS GROUNDED: 45 PERCENT YAW TRIM LEFT REQ. TO CENTER YAW INDICATION IN FLIGHT. T/S IAW FIM 27-20-00-810-806-A. FOUND TRIM OF RUDDER TO BE 2.5 DEG. LEFT WITH SURFACE CENTERED ON TAILCONE. C/W RUDDER RIGGING IAW AMM 27-20-00-820-801-A.TO NULL OUT RUDDER TRIM. ALL FLIGHT CONTROL SURFACES…
From FAA Service Difficulty Reports; matched by N-number and serial number.AIRCRAFT WAS GROUNDED: TO MAINTAIN COORDINATED FLIGHT YAW TRIM REQUIRED BETWEEN 40-50 PERCENT INPUT ON YAW TRIM DURING CLIMB OUT AND CRUISE. FOUND LH IB FLAP NO.1 MECHANISM UPPER ROD BENT AND LH IB TRAILING FLAP OUT OF RIG. REMOVED AND REPLACED LH IB FLAP NO.1 AND NO.2 MECHANISM UPPER AND LOWER…
From FAA Service Difficulty Reports; matched by N-number and serial number.AIRCRAFT WAS GROUNDED: LANDING GEAR AURAL WARNING IN FLIGHT . ACCOMPLISHED QHR TO CLEAR. PERFORMED RADIO ALT TEST IAW TASK # 34-31-00-710-801-A , ALSO PERFORMED TASK 22-11-00-811-997-A , TESTED OK.
From FAA Service Difficulty Reports; matched by N-number and serial number.AIRCRAFT WAS GROUNDED: EMERGENCY LIGHT BATTERY FAULT EICAS MSG DISPLAYED WHEN LIGHTS TESTED DURING PREFLIGHT 2 OVERHEAD CABIN EMERG LIGHTS DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED EMERG LT BATTERY AT PANEL 243 OVERHEAD. OPS CHECK NORMAL.
From FAA Service Difficulty Reports; matched by N-number and serial number.AIRCRAFT WAS GROUNDED: PILOT REPORTS ELECT SMELL IN COCKPIT THRUOUT A/C CABIN, VERY STRONG IN FIRST CLASS SMELL REPORTED BY FA 1. RETURN TO THE GATE. MAINTENANCE ACCOMPLISHED JOB CARD 43L00021001. FOUND LEFT RECIRCU FAN BAD. REMOVE & REPLACED LEFT RECIRCULATION FAN IAW AMM 21-24-01. REMOVED &…
From FAA Service Difficulty Reports; matched by N-number and serial number.AIRCRAFT NOT GROUNDED: MAINTENANCE REPORTS R1 SLIDE PARTIALLY DEPLOYED, ASSIST BOTTLE DEPLETED. REPLACED DIAPHRAGM AND SLIDE ASSEMBLY IAW JOB CARD 43L00025001.
From FAA Service Difficulty Reports; matched by N-number and serial number.THE PILOT DECLARED AN EMERGENCY DUE TO A FLAPS FAILED EICAS MESSAGE. FLAPS FAILED TO RETRACT PROPERLY FROM 1 TO 0 AFTER TAKE OFF, AND AT EXTENSION FOR LANDING THE FLAPS FAILED AGAIN AND STAYED AT FLAPS 3 WITH FULL FLAPS SELECTED. MAINTNENANCE REMOVED AND REPLACED THE LT FLAP POSITION SENSOR UNIT…
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING APPROACH, IN ICING CONDITIONS AT 2500 FEET, THE AIRCRAFT EXPERIENCED VIOLENT ROLL. AP & AT DISCONNECTED AND EICAS MESSAGES WERE DISPLAYED AT FAIL, WIND SHEAR FAIL, STALL PROT FAIL, AND THE AOA LIMIT FAIL. AFTER LANDING, ADS PROBE 3+1 FAIL, DISPLAYED. REPLACED SMART PROBE IAW AMM 34-13-01.
From FAA Service Difficulty Reports; matched by N-number and serial number.AFT PASSENGER DOOR EMERGENCY SLIDE RELEASE PIN THREAD IS BROKEN OFF. REPLACED AFT PASSENGER DOOR EMERGENCY SLIDE. AIRCRAFT WAS GROUNDED.
From FAA Service Difficulty Reports; matched by N-number and serial number.AIRCRAFT IS IN BASE, WEAR ON LEFT WING INBOARD FLAP TRACK 2A INBOARD. REPLACED LEFT WING INBOARD FLAP TRACK 2A INBOARD PER AMM 57-54-25.
From FAA Service Difficulty Reports; matched by N-number and serial number.Showing the 10 most recent of 132 reports.