N11106

Service difficulty reports · 136

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N11106' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR C2XA09CL092Inverter · faultyDURING ROUTINE MAINTENANCE THE EMERGENCY EXIT SIGN OVER THE FLIGHT ATTENDANTS SEAT WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 1 EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD.Jul 1, 2009 · N11106 · Emb EMB145XR · Emergency LightingSDR C2XA09IA111Ballast · inoperativeIAH - FLIGHT 2736, DURING PREFLIGHT INSPECTION THE CREW REPORTED A STRONG ELECTRICAL SMELL FROM THE LAVATORY. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE LAVATORY LIGHT BALLAST. OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS AApr 28, 2009 · N11106 · Emb EMB145XR · Passenger Compartment LightingSDR C2XA09SH129Floor Support · corrodedSHV - DURING C-CHECK CENTER OMEGA BEAM HAD CORROSION AT CROSSBEAM BETWEEN FRAME 48-49. MAINTENANCE REPAIRED CENTER OMEGA BEAM AT CROSSBEAM FRAME 48-49 IAW IC2009-145/02742. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 16, 2009 · N11106 · Emb EMB145XR · Fuselage Miscellaneous StructureSDR C2XA09SH128Floor Support · corrodedSHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT CROSSBEAM BETWEEN FRAMES 48-49. MAINTENANCE REPAIRED LT OMEGA BEAM AT CROSSBEAM BETWEEN FRAME 48-49 IAW EC5310-01466. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 16, 2009 · N11106 · Emb EMB145XR · Fuselage Miscellaneous StructureSDR C2XA09SH127Beam · corrodedSHV - DURING C-CHECK CARGO DOOR CUTOUT LOWER BEAM CORRODED. MAINTENANCE REMOVED AND REPLACED CARGO DOOR CUTOUT LOWER BEAM IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 16, 2009 · N11106 · Emb EMB145XR · Fuselage Miscellaneous StructureSDR C2XA09SH126Attach Bracket · migratedSHC - DURING C-CHECK RT PCA TO AILERON O/B ROD O/B HAT BUSHING MIGRATED. MAINTENANCE REMOVED AND REPLACED RT PCA TO AILERON ATTACHMENT BRACKET IAW EMB-145 SRM 51-40-02 AND EC5750-01177 REV B. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 16, 2009 · N11106 · Emb EMB145XR · AileronsSDR C2XA09SH125Attach Bracket · wornSHV - DURING C-CHECK LT PCA TO AILERON ATTACHMENT HAS MIGRATED BUSHING. MAINTENANCE REMOVED AND REPLACED LT PCA TO AILERON ATTACHMENT BRACKET IAW EMB-145 EC5750-01177 REV B. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 16, 2009 · N11106 · Emb EMB145XR · AileronsSDR C2XA09SH124Attach Bracket · gougedSHV - DURING C-CHECK LT AILERON PCA ATTACH POINT BRACKET O/B ROD ATTACHMENT I/B AND O/B HAT BUSHING HOUSINGS ARE GOUGED. MAINTENANCE REMOVED AND REPLACED LT PCA TO AILERON ATTACHMENT BRACKET IAW EMB-145 EC5750-01177 REV B. THE AIRCRAFT WAS APPROVED FOR RETURApr 16, 2009 · N11106 · Emb EMB145XR · AileronsSDR C2XA09SH123Attach Bracket · gougedSHV - DURING C-CHECK BRACKET ON THE RT AILERON THAT GOES TO THE PCA IS GOUGED. MAINTENANCE REMOVED AND REPLACED RT PCA TO AILERON ATTACHMENT BRACKET IAW EMB-145 SRM 51-40-02 AND EC5750-01177 REV B. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 16, 2009 · N11106 · Emb EMB145XR · AileronsSDR C2XA09SH122Attach Bracket · wornSHV - DURING C-CHECK RT AILERON TO PCA BRACKET MOST I/B HAT BUSHING MIGRATED. MAINTENANCE REMOVED AND REPLACED RT AILERON TO PCA ATTACHMENT BRACKET IAW EMB-145 SRM 51-40-02 AND EC5750-01177 REV B. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 16, 2009 · N11106 · Emb EMB145XR · AileronsSDR C2XA09SH121Attach Bracket · wornSHV - DURING C-CHECK RT PCA TO AILERON I/B ROD O/B HAT BUSHING MIGRATED. MAINTENANCE REMOVED AND REPLACED RT AILERON TO PCA ATTACHMENT BRACKET IAW EMB-145 SRM 51-40-02 AND EC5750-01177 REV B. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 16, 2009 · N11106 · Emb EMB145XR · AileronsSDR C2XA09SH120Attach Bracket · wornSHV - DURING C-CHECK RT PCA TO AILERON I/B ROD I/B HAT BUSHING MIGRATED. MAINTENANCE REMOVED AND REPLACED RT PCA TO AILERON ATTACHMENT BRACKET IAW EMB-145 SRM 51-40-02 AND EC5750-01177 REV B. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 16, 2009 · N11106 · Emb EMB145XR · AileronsSDR C2XA09SH119Bracket · wornSHV - DURING C-CHECK LT AILERON DAMPNER BRACKET I/B HAT BUSHING MIGRATED. MAINTENANCE REMOVED AND REPLACED LT AILERON DAMPNER BRACKET IAW SRM 51-40-02. MAINTENANCE PREPPED, PRIMED AND PAINTED LT AILERON DAMPNER BRACKET IAW EMB-145 CPM 51-21-06. THE AIRCRAFTApr 16, 2009 · N11106 · Emb EMB145XR · AileronsSDR C2XA09SH082Cowling · crackedDENT JUST BELOW APU AIR INLET ON TAIL CONE. THE APU WAS DEACTIVATED AND CONSIDERED INOPERATIVE FOR TRIP TO SHV. UPON ARRIVING IN SHV MAINTENANCE REMOVED AND INSTALLED A NEW APU TAIL CONE IAW AMM 49-15-00. THE APU WAS REACTIVATED IAW AMM 49-13-00. OPS CHECKMar 16, 2009 · N11106 · Emb EMB145XR · APU Cowling/ContainmentSDR C2XA09IA052Sign · malfunctionedIAH - FLIGHT 2050, DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE INTERIOR LEFT EMERGENCY EXIT SIGN AT THE WING WAS INOPERATIVE. MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY TESTED THE EMERGENCY LIGHTS WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS AFeb 17, 2009 · N11106 · Emb EMB145XR · Emergency LightingSDR C2XA08CL049Actuator · malfunctionedCLE FLIGHT 2879 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL WHEN GEAR WAS SELECTED DOWN. MAINTENANCE INSPECTED AND REPLACED THE RIGHT NOSE GEAR DOOR ACTUATOR. OPERATIONAL CHECKS WERE GOOD.Apr 14, 2008 · N11106 · Emb EMB145XR · Landing Gear Door ActuatorSDR C2XA08IA052Electronic Unit · inoperativeIAH - FLIGHT 2271 - THE CREW REPORTED, RECEIVED A LANDING GEAR AIR GROUND FAILED EICAS MESSAGE WHEN THE GEAR WAS SELECTED DOWN, AND CLEARED WHEN GEAR EXTENDS. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECFeb 7, 2008 · N11106 · Emb EMB145XR · Landing Gear Retraction/Extension SystemSDR C2XA07SH056Panel · corrodedSHV - DURING C-CHECK MAINTENANCE FOUND RIGHT LOWER AILERON SHROUD WITH CORROSION AT BONDING PLATES. MAINTENANCE REPAIRED RIGHT LOWER AILERON SHROUD IAW EC 5750-01315 REV D. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.Aug 29, 2007 · N11106 · Emb EMB145XR · AileronsSDR C2XA07SH057Panel · corrodedSHV - DURING C-CHECK MAINTENANCE FOUND LT AILERON UPPER SHROUD WITH CORRODED BONDING PLATES. MAINTENANCE REPAIRED LEFT AILERON UPPER SHROUD IAW EC 5750-01315 REV D. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.Aug 29, 2007 · N11106 · Emb EMB145XR · AileronsSDR C2XA07SH059Shear Tie · corrodedSHV - DURING C-CHECK MAINTENANCE FOUND SHEAR CLIP AT FRAME 65 & CARGO DOOR CUTOUT LOWER BEAM WITH CORROSION. MAINTENANCE REPAIRED SHEAR CLIP AT FRAME 65 IAW EC 5330-01458 & REMOVED AND REPLACED CARGO DOOR CUTOUT SILL IAW EMB 145XR SRM 51-40-00. AIRCRAFT WAS Aug 29, 2007 · N11106 · Emb EMB145XR · Fuselage Internal Mounting StructureSDR C2XA07SH052Panel · corrodedSHV - DURING C-CHECK MAINTENANCE FOUND PANEL 197CL HAS CORRODED BONDING PLATES. MAINTENANCE REPAIRED PANEL 197CL IAW EC 5750-01315 REV D. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.Aug 29, 2007 · N11106 · Emb EMB145XR · Fuselage Main, StructureSDR C2XA07SH054Panel · corrodedSHV - DURING C-CHECK MAINTENANCE FOUND PANEL 197 AB HAS CORRODED BONDING PLATES. MAINTENANCE REPAIRED PANEL 197 AB IAW EC 5750-01315 REV D. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.Aug 29, 2007 · N11106 · Emb EMB145XR · Fuselage Main, StructureSDR C2XA07SH053Panel · corrodedSHV - DURING C-CHECK MAINTENANCE FOUND PANEL 197 DR HAS CORRODED BONDING PLATES. MAINTENANCE REPAIRED PANEL 197 DR IAW EC 5750-01315 REV D. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.Aug 29, 2007 · N11106 · Emb EMB145XR · Fuselage Main, StructureSDR C2XA07SH055Panel · corrodedSHV - DURING C-CHECK MAINTENANCE FOUND PANEL 193 AAB WITH BAD BONDING PLATES. MAINTENANCE REPAIRED PANEL 193 AAB IAW EMB 145 EC 5750-01315. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.Aug 29, 2007 · N11106 · Emb EMB145XR · Fuselage Main, StructureSDR C2XA07SH058Panel · corrodedSHV - DURING C-CHECK MAINTENANCE FOUND RIGHT TOP AILERON SHROUD WITH CORROSION AT BONDING PLATES. MAINTENANCE REPAIRED RIGHT TOP AILERON SHROUD IAW EC 5750-01315 REV D. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.Aug 29, 2007 · N11106 · Emb EMB145XR · AileronsSDR C2XA07RI031Glowstrip · missingFLT 2761 - EWR - CREW REPORTED FLUORESCENT STRIP IN GALLEY AREA MISSING. EWR MX INSTALLED EMERGENCY LIGHT STRIP AND PERFORMED OPERATIONAL TEST SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.May 7, 2007 · N11106 · Emb EMB145XR · Emergency EquipmentSDR C2XA06TY009Floorbeam · corrodedLEFT OMEGA BEAM CORRORED AT RAMP ANGLE CARBON BEAM. REMOVED CORRODED AREA, FABRICATED DOUBLER, DRILLED, COUNTERSUNK, INSTALLED, ALODINED, PRIMED AND PAINTED IAW EMB 145XR SRM 53-00-10. AIRCRAFT RELEASED AND RETURNED TO SERVICE.Feb 12, 2006 · N11106 · Emb EMB145XR · Fuselage Main, Floor BeamSDR C2XA05TY061Skin · dentedTYS - A DENT JUST FWD OF SKIN SPLICE BETWEEN FR 23 AND 24 AND STR 18R AND 19R WAS FOUND. MAINTENANCE PERFORMED A REPAIR TO THE DAMAGE SKIN IAW IC2005-145/7374, ALODINED, PRIMED AND PAINTED IAW CPM 51-21-07. LEAK CHECK WAS GOOD. AIRCRAFT WAS RELEASED TO SERVDec 12, 2005 · N11106 · Emb EMB145XR · Fuselage Main, Plate/SkinSDR C2XA05IA082Inverter · inoperativeDURING POST-FLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHT ON OVERHEAD PANEL IS INOP. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT INVERTER FOR THE AFFECTED LIGHT, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APJun 16, 2005 · N11106 · Emb EMB145XR · Emergency LightingSDR C2XA04TY152Floorbeam · corrodedDURING A SCHEDULED 1C INSPECTION, THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. THE CORRODED AREA WAS SUBSEQUENTLY REMOVED AND A FILLER AND DOUBLER WAS INSTALLED IAW THE EMB SRM. ACFT WAS RELEASED FOLLOWING COMPLETION OF THE 1C INSPECTION.Aug 13, 2004 · N11106 · Emb EMB145XR · Fuselage Main, Floor BeamSDR C2XA04TY151Attach Bracket · corrodedDURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE CABIN TO GALLEY STEP-UP PLATE. MAINTENANCE ACCOMPLISHED A BLEND OUT REPAIR IAW SRM 53-21-10 AND CPM 51-21-04,05,06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.Aug 10, 2004 · N11106 · Emb EMB145XR · Fuselage Main, Floor BeamSDR C2XA04TY146Seat Track · corrodedDURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON SEAT TRACK LF1 AT THE MOST FORWARD END. MAINTENANCE REMOVED AND REPLACED SEAT TRACK LF1 IAW MM 53-01-06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.Aug 10, 2004 · N11106 · Emb EMB145XR · Fuselage, Seat/Cargo Attach FittingsSDR C2XA04TY149Floorbeam · corrodedDURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE FORWARD DIGITAL JUST AFT OF THE COCKPIT DOOR STEP. MAINTENANCE ACCOMPLISHED A BLEND OUT REPAIR IAW SRM 53-21-10 AND CPM 51-21-04,05,06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.Aug 6, 2004 · N11106 · Emb EMB145XR · Fuselage Main, Floor BeamSDR C2XA04TY147Gusset · corrodedDURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE AFT GUSSET AT FRAME 15. MAINTENANCE ACCOMPLISHED A BLEND OUT REPAIR IAW SRM 53-21-10 AND CPM 51-21-04,05,06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.Aug 6, 2004 · N11106 · Emb EMB145XR · Fuselage Main, StructureSDR C2XA04TY148Floorbeam · corrodedDURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE CENTER OMEGA BEAM TOPCAP AT FRAME 22. MAINTENANCE ACCOMPLISHED A BLEND OUT REPAIR IAW SRM 53-21-10 AND CPM 51-21-04,05,06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.Aug 6, 2004 · N11106 · Emb EMB145XR · Fuselage Main, Floor BeamSDR C2XA04BT016Light · brokenEWR---CO2205, CREW REPORTED, (EMERGENCY LIGHTING STRIP BY MAIN CABIN DOOR MISSING AND GALLEY STRIP IS BROKEN). MAINTENANCE REPLACED MISSING EMERGENCY LIGHT FLOOR STRIP AND BROKEN EMERGENCY LIGHT FLOOR STRIP. IAW EMB145 MM NR 33-50-12, OPS. CHECKED EMERGENCYJan 31, 2004 · N11106 · Emb EMB145XR · Emergency Lighting
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