N14953, cancelled Feb 3, 2016

Service difficulty reports · 72

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 = 'N14953' AND deregistration_id = 'N14953-2016-02-03'
  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 ASOA20140913278VSkin · dentedDURING C-CHECK, REAR FUSELAGE HAS DENT BETWEEN FRAME 77 AND SPLICE BETWEEN STRINGERS 18 - 19R, REPAIRED DENT IAW EC5330-02939. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Sep 13, 2014 · N14953 · Emb EMB145LR · Fuselage Main, Plate/SkinSDR ASOA20140911273Floor Support · corrodedDURING C-CHECK, CORROSION FOUND ON OMEGA BEAM NUTPLATE HOLES AT FRAME 59-61. MAINTENANCE R & R CENTER OMEGA BEAM BUTTSTRAP IAW EC5310-01473, REV D. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Sep 11, 2014 · N14953 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASOA20140909272Beam · corrodedDURING C-CHECK, CARGO DOOR LOWER CUTOUT CORRODED. R & R CARGO DOOR LOWER CUTOUT IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.Sep 9, 2014 · N14953 · Emb EMB145LR · Fuselage Main, StructureSDR ASOA20140906271Floor Support · corrodedDURING C-CHECK, RT OMEGA BEAM BETWEEN FRAMES 59-61 CORRODED. MAINTENANCE FABRICATED AND INSTALLED REPAIR PARTS ON RT OMEGA BEAM IAW EC5310-01473, REV D. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Sep 6, 2014 · N14953 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASOA20130708100Skin · crackedDURING 4A INSPECTION THE LT FUSELAGE 1 SKIN WAS FOUND TO BE CRACKED AT FRAME 75 IN 2 PLACES BELOW STRINGER 1R. MX PERFORMED A DOUBLER REPAIR IAW ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-02353, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Jul 8, 2013 · N14953 · Emb EMB145LR · Fuselage Main, Plate/SkinSDR ASOA20130708099Skin · crackedDURING 4A INSPECTION THE REAR FUSELAGE 1 SKIN WAS FOUND TO BE CRACKED AT FRAME 75 BETWEEN STRINGERS 1R AND 2R. MX PERFORMED A DOUBLER REPAIR IAW ENGINEERING CHANGE REPAIR AUTHORIZATION EC5330-02353, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Jul 8, 2013 · N14953 · Emb EMB145LR · Fuselage Main, Plate/SkinSDR ASOA20121018153Skin · crackedLT WING UPPER SKIN T/E WAS FOUND CRACKED AT THE LT GROUND SPOILER HINGE POINT. CUTOUT THE CRACKED AREA, FABRICATED AND INSTALLED DOUBLER AND TRIPLER. ACFT STILL IN C CHECKOct 17, 2012 · N14953 · Emb EMB145LR · Wing, Plate/SkinSDR ASOA20121017152Window Frame · corrodedLEFT & RIGHT WINDSHIELD FRAME HAS CORROSION IN SEVERAL HOLES. REMOVED CORROSION FROM BOLT HOLES AND SOME OF THE HOLES REQUIRED BUSHINGS TO BE INSTALLED IAW ETD2012-145-014418-A AND EC5310-01633. ACFT IS STILL IN C-CHECK.Oct 17, 2012 · N14953 · Emb EMB145LR · Fuselage Main, StructureSDR C2XA11IA185Uplock · inoperativeIAH - FLIGHT 2174, THE CREW REPORTED THAT THE LEFT MAIN LANDING GEAR INDICATION WAS SHOWING DASHES OF YELLOW AND GREEN, AND ALTERNATING BACK AND FORTH. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LT MLGAug 27, 2011 · N14953 · Emb EMB145LR · Landing Gear Position and WarningSDR C2XA11CL157Inverter · faultyGRR FLT 2904 THE CREW REPORTED THE OVERWING CEILING EXIT LIGHT DID NOT TEST. MAINTENANCE INSPECTED AND REPLACED THE NR 4 EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD.Jun 27, 2011 · N14953 · Emb EMB145LR · Emergency LightingSDR C2XA11RI113Controller · inoperativeFLIGHT 2287 - EWR - FLIGHT CREW REPORTED THAT, EN ROUTE FROM EWR TO CMH, FMS FAILED, BOTH PFD'S AND NAVS ALSO WENT OUT. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. EWR MX REMOVED AND REPLACED CAPT DC550 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AJun 20, 2011 · N14953 · Emb EMB145LR · Central DisplaySDR C2XA11TY028Shim · wornTYS - A/C WAS TAXI FOR TAKEOFF AND IN CLIMBOUT, WHEN GEAR STOWED, CREW REPORTED A RATTLING NOISE WHEN GEAR STOWED. A/C WAS FERRIED TO TYS FROM BNA WHERE MAINTENANCE REMOVED THE NOSE GEAR AND FOUND THAT GEAR NEEDED TO BE SHIM. MAINTENANCE MEASURED THE BEARINMar 15, 2011 · N14953 · Emb EMB145LR · Nose/Tail Landing GearSDR C2XA10SH372Fitting · crackedSHV - DURING C-CHECK NR 1 ENGINE FORWARD LOWER YOKE FORWARD FLANGE CRACKED. MAINTENANCE REMOVED AND REPLACED NR1 ENGINE FORWARD LOWER YOKE FITTING IAW EC5450-01028. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 29, 2010 · N14953 · Emb EMB145LR · Nacelle/Pylon, Attach FittingsSDR C2XA10SH371Floor Support · corrodedSHV - DURING C-CHECK LT OMEGA BEAM L-FLANGE AT FRAME 38 HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM L-FLANGE AT FRAME 38 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 29, 2010 · N14953 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR C2XA10SH370Floor Support · corrodedSHV - DURING C-CHECK LT OMEGA BEAM L-FLANGE BETWEEN FRAME 43-44 HAS CORROSION. MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM L-FLANGE BETWEEN FRAME 43-44 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 29, 2010 · N14953 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR C2XA10SH369Floor Support · corrodedSHV - DURING C-CHECK CENTER OMEGA BEAM L-FLANGE BETWEEN FRAME 43-44 HAS CORROSION. MAINTENANCE PERFORMED REPAIR ON CENTER OMEGA BEAM L-FLANGE BETWEEN FRAME 43-44 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 29, 2010 · N14953 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR C2XA10SH368Floor Support · corrodedSHV - DURING C-CHECK LT OMEGA BEAM L-FLANGE BETWEEN FRAME 49-50 HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM L-FLANGE BETWEEN FRAME 49-50 IAW EMB-145 SRM 51-00-10 AND RESTORED TO ORIGINAL FINISH IAW EMB-145 CPM 51-21-06. THE AOct 29, 2010 · N14953 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR C2XA10SH367Floor Support · corrodedSHV - DURING C-CHECK CENTER OMEGA BEAM L-FLANGE BETWEEN FRAME 49-50 HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON CENTER OMEGA BEAM L-FLANGE BETWEEN FRAMES 49-50 IAW EC5310-01466 REV ORIG. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 29, 2010 · N14953 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR C2XA10SH366Floor Support · corrodedSHV - DURING C-CHECK LT OMEGA BEAM L-FLANGE AT FRAME 54 HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM L-FLANGE AT FRAME 54 REPAIR IAW EMB-145 SRM 51-00-10. RESTORED TO ORIGINAL FINISH IAW EMB-145 CPM 51-21-06. THE AIRCRAFT WASOct 29, 2010 · N14953 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR C2XA10SH365Frame · corrodedSHV - DURING C-CHECK CORROSION (LEVEL 2 LOCAL) ON FRAME 65 STRINGER 16L-17L. MAINTENANCE PERFORMED REPAIR ON FRAME 65 STRINGER 16L-17L IAW EMB-145 EC5310-01529. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 29, 2010 · N14953 · Emb EMB145LR · Fuselage Main, FrameSDR C2XA10SH364Fitting · corrodedSHV - DURING C-CHECK CORROSION (LEVEL 2 LOCAL) ON SHEAR CLIP FRAME 65 STRINGER 16L-17L. MAINTENANCE PERFORMED REPAIR ON SHEAR CLIP FRAME 65 STRINGER 16L-17L IAW EMB-145 EC5320-01494. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 29, 2010 · N14953 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR C2XA10CL096Proximity Switch · out of adjustCLE FLT 2632 - THE CREW REPORTED AN AIR/GROUND FAIL MESSAGE. MAINTENANCE INSPECTED AND COULD NOT DUPLICATE BUT CHANGED THE LGEU, ADJUSTED 1 PROXIMITY SWITCH ON LEFT AND RIGHT GEAR AND ADJUSTED NOSE PROXIMITY SWITCH TARGET ON THE NOSE GEAR AND CHANGED THE NOSEJun 14, 2010 · N14953 · Emb EMB145LR · Landing Gear Position and WarningSDR C2XA10RI002Charger · defectiveFLIGHT 2531 - EWR - FLIGHT CREW REPORTED EMERGENCY LIGHT WOULD NOT TURN OFF. EWR MX REMOVED AND REPLACED NR 2 BATTERY CHARGER ASSY AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.Jan 5, 2010 · N14953 · Emb EMB145LR · Emergency LightingSDR C2XA09TY265Battery · dischargedTYS - A/C WAS IN FOR A SERVICE CHECK WHEN INSPECTION FOUND THE AED DEFIBRILLATOR BATTERY INOP. MAINTENANCE REMOVED AND REPLACED THE AED DEFIBRILLATOR BATTERY IAW EC 2560-01065. A/C RELEASED BACK TO SERVICE.Oct 27, 2009 · N14953 · Emb EMB145LR · Emergency EquipmentSDR C2XA09IA263Inverter · inoperativeMCI - DURING MAINTENANCE INSPECTION THE NUMBER FOUR AND FIVE AISLE PATH LIGHT STRIPS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FIVE EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS. AIRCRAFT WAS APPROVED FOR RETUOct 14, 2009 · N14953 · Emb EMB145LR · Emergency LightingSDR C2XA09RI148Altimeter · malfunctionedFLIGHT 2790 - EWR - DURING DESCENT, FLIGHT CREW REPORTED AN AMBER INDICATION FOR RADIO ALTIMETER ON PFD WITH LANDING GEAR AURAL SOUND FOR 5 SECONDS THEN CLEARED. EWR MX RESET BOTH RA C/B'S AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO REAug 19, 2009 · N14953 · Emb EMB145LR · Altimeter, Barometric/EncoderSDR C2XA09TY107Proximity Switch · brokenTYS - AIRCRAFT WAS EN ROUTE TO IAH FROM EWR WITH A STOP AT TYS, WHEN LEAVING TYS THE LDG WOULDN'T RETRACT SO CREW RETURN TO BASE. MAINTENANCE REMOVED AND REPLACED THE NLG PROX SWITCH IAW EMB 145 AMM 32-63-02 AND OPS CHECK GOOD. RELEASED BACK TO SERVICE.Jun 16, 2009 · N14953 · Emb EMB145LR · Landing Gear Position and WarningSDR C2XA09TY106Bulb · failedACFT IN OVERNIGHT FOR A 2A CHECK, WHEN INSP FOUND THE RT OVERWING EMERGENCY LIGHT INOP. MX REMOVED AND REPLACED THE THE BULB FOR THE LIGHT IAW AMM 33-50-07, OPS CHECK GOOD AND WAS RELEASED.Jun 16, 2009 · N14953 · Emb EMB145LR · Emergency LightingSDR C2XA09RI043Power Supply · dischargedFLIGHT 2996 - EWR - FLIGHT CREW REPORTED FORWARD EMERGENCY LIGHT INOPERATIVE ABOVE F/A SEAT. EWR MX REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.Mar 20, 2009 · N14953 · Emb EMB145LR · Emergency LightingSDR C2XA08CL101Warning System · activatedDSM FLIGHT NR 2636 THE CREW REPORTED A FUEL 1 LOW LEVEL MSG IN FLIGHT. THE FLIGHT DIVERTED IN DSM AND LANDED WITHOUT INCIDENT. THE FUEL QUANTITY INDICATOR WAS ACCURATE. THE SYSTEM WAS PLACED ON MEL SUPPLEMENT TO FOLLOW.Aug 27, 2008 · N14953 · Emb EMB145LR · Fuel Indicating SystemSDR C2XA08RI084Handle · unsecureFLIGHT 2807 - EWR - FLIGHT CREW REPORTED MAIN CABIN DOOR WOULD NOT OPEN OR CLOSE FROM INSIDE. EWR MAINTENANCE SECURED MAIN CABIN DOOR HANDLE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (S)Jun 13, 2008 · N14953 · Emb EMB145LR · Passenger/Crew DoorsSDR C2XA08IA044Skin · crackedIAH - DURING PREFLIGHT INSPECTION THE RIGHT WING SKIN WAS FOUND TO BE CRACKED AT THE CENTER HINGE POINT CUTOUT FOR THE GROUND SPOILER. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE CRACK ON A 500FC DMI, WITH RE-INSPECTIONS TO BE MADE AT EVER 50FC, AND THEJan 29, 2008 · N14953 · Emb EMB145LR · Wing, Plate/SkinSDR C2XA08IA029Fuse · blownIAH - FLIGHT 2099 DURING PREFLIGHT INSPECTION SOME EMERGENCY LIGHTS WERE INOP. MAINTENANCE REMOVED AND REPLACED A FUSE, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Jan 17, 2008 · N14953 · Emb EMB145LR · Emergency LightingSDR C2XA07TY065Handle · failedLANDING GEAR FAILED TO RETRACT. REPLACED LANDING GEAR HANDLE IAW EMB 145 MM 32-32-02, OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.Oct 31, 2007 · N14953 · Emb EMB145LR · Landing Gear SelectorSDR C2XA07CL092Computer · shortedCLEVELAND MAINTENANCE REPORTED THE GUIDANCE CONTROL UNIT (GC-550) HAD SMOKE COMING FROM IT. MAINTENANCE INSPECTED AND REPLACED THE GUIDANCE CONTROL COMPUTER. OPERATIONAL CHECKS WERE GOOD.Oct 30, 2007 · N14953 · Emb EMB145LR · Autopilot ComputerSDR C2XA07TY060Doubler · missingTYS - A/C WAS FOUND WITH A NUT PLATE MISSING AND THE HOLE ELONGATED ON THE RUDDER 2. MAINTENANCE FABRICATED A FILLER AND A INTERNAL DOUBLER. ALODINED AND EPOXY PRIMED THE PARTS. INSTALL FABRICATED PARTS ON THE RUDDER IAW EC 5540--01077. ALL WORK WAS ACCOMPOct 15, 2007 · N14953 · Emb EMB145LR · Rudder, Plate/SkinSDR C2XA07RI052Light · malfunctionedFLT 2774 - DAY - CREW REPORTED MAIN CABIN DOOR EMERGENCY LIGHT INOPERATIVE. DAY MX RECYCLED BATTERY SWITCHES AND PERFORMED OPERATIONAL TEST SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.Jul 3, 2007 · N14953 · Emb EMB145LR · Emergency LightingSDR C2XA07IA047Light · malfunctionedIAH - FLT NR 3116, DURING A TEST THE EMERGENCY EXIT LIGHTING FAILED TO ILLUMINATE. MAINTENANCE RESET THE EMERGENCY LIGHTING SYSTEM AND OPERATIONALLY TESTED THE SYSTEM. THE DISCREPANCY COULD NOT BE DUPLICATED AND WAS THEN CLEARED.Feb 26, 2007 · N14953 · Emb EMB145LR · Emergency LightingSDR C2XA06IA141Wire · looseIAH - DURING A-CHECK INSPECTION, THE EMERGENCY EXIT LIGHT ABOVE THE F/A SEAT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED THE SIGN, RE-SECURED THE CONNECTORS, AND RE-INSTALLED THE SIGN. OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVEDAug 27, 2006 · N14953 · Emb EMB145LR · Light System WiringSDR C2XA06IA053Acm · overheatedFLT 2862 - CREW REPORTED SMOKE IN THE CABIN AFTER REACHING 10,000 FT CLIMBOUT. THE AIRCRAFT LANDED AT IAH WHERE MAINTENANCE FOUND THE NR 2 ACM TO BE OVERHEATING. THE ACM WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.Apr 1, 2006 · N14953 · Emb EMB145LR · Cabin Cooling SystemSDR C2XA05TY004Fitting · corrodedTYS, DURING A SCHEDULED INSPECTION, THE VERTICAL STAB TO FUSELAGE FITTING ATTACH BRACKET WAS FOUND FRETTING ON SKIN AT FRAME 75. MAINTENANCE REMOVED THE STAB FITTING AT FRAME 75, CLEANED AND INSPECTED THE SKIN AND FITTING (NO CORROSION OR DAMAGE WAS FOUND), AJan 13, 2005 · N14953 · Emb EMB145LR · Vertical Stabilizer, Attach FittingsSDR C2XA05TY003Sill · corrodedTYS, DURING A SCHEDULED INSPECTION THE SERVICE DOOR SILL WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE DOOR SILL IAW EMB-145-AMM-21-31-00 / 135/145 SRM 51-40-00 AND 52-20-03, CABIN LEAKAGE AND FUNCTIONAL CHECKED GOOD.Jan 13, 2005 · N14953 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR C2XA05TY002Hinge · wornDURING A 4C INSPECTION THE RT AND LT VERTICAL STABLIZER SPHERICAL BEARING HOUSINGS WERE FOUND WORN. MAINTENANCE REAM AND INSTALL NEW BUSHINGS IAW EC5510-01107.Jan 4, 2005 · N14953 · Emb EMB145LR · Ventral StructureSDR C2XA04BT110Battery · inoperativeBTV, DURING SERVICE AND ROUTINE CHECK ON RON, MAINTENANCE FOUND THE PASSENGER DOOR EMERGENCY LIGHT TO BE INOPERATIVE. REMOVED AND REPLACED NR 1 EMERGENCY LIGHT BATTERY POWER SUPPLY IAW EMB145 AMM 33-50-04. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.Oct 17, 2004 · N14953 · Emb EMB145LR · Emergency LightingSDR C2XA04CL044Controller · failedBTV FLIGHT NR 2441 THE CREW REPORTED SMOKE COMING FROM THE DIGITAL PRESSURE CONTROLLER. MAINTENANCE REPLACED THE DIGITAL PRESSURE CONTROLLER. OPERATIONAL CHECKS WERE GOOD.Apr 28, 2004 · N14953 · Emb EMB145LR · Cabin Pressure ControllerSDR C2XA03IA105Lamp · looseDURING SCHEDULED MAINTENANCE THE LEFT AFT EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND RE-SECURED THE LAMP IN THE LIGHT FIXTURE. THE LIGHT OPERATIONALLY CHECKED GOOD.Nov 20, 2003 · N14953 · Emb EMB145LR · Emergency LightingSDR C2XA03BT064Bulb · burned outDURING 3A INSPECTION MAINTENANCE FOUND PASSENGER DOOR EMERGENCY LIGHT TO BE INOPERATIVE. REMOVED AND REPLACED PASSENGER DOOR EMERGENCY LIGHT BULB IAW EMB145 AMM 33-50-00. OPS CHECKED GOOD.Jun 6, 2003 · N14953 · Emb EMB145LR · Emergency LightingSDR C2XA03SH082Sill · corrodedDURING C-CHECK FOWARD SILL HAS CORROSION BETWEEN FRAMES 18 AND 20. MAINTENANCE REMOVED DAMAGE AND MADE A DOUBLER REPAIR ON AFFECTED SILL IAW EMB 145 SRM 53-21-01. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.Mar 31, 2003 · N14953 · Emb EMB145LR · Fuselage Main, StructureSDR C2XA03SH081Skin · gougedDURING C-CHECK SKIN WAS FOUND GOUGED UNDER GPU ACCESS PANEL BETWEEN FRAMES 6 AND 8. MAINTENACE REMOVED DAMAGE AND REPAIRED SKIN IAW EMB 145 SRM 53-11-01. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.Mar 31, 2003 · N14953 · Emb EMB145LR · Fuselage Main, Plate/SkinSDR C2XA03SH080Support · corrodedDURING C-CHECK THE SUPPORT PLATE BETWEEN LT OMEGA BEAM AND LT SILL WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 60 AND 61. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT PLATE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.Mar 31, 2003 · N14953 · Emb EMB145LR · Fuselage Miscellaneous Structure
Back to N14953, cancelled Feb 3, 2016