N14942, cancelled Nov 15, 2016
Service difficulty reports · 90
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 = 'N14942' AND deregistration_id = 'N14942-2016-11-15' 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.
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 = 'N14942' AND deregistration_id = 'N14942-2016-11-15' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR ASOA20130514070Inverter · inoperativeDURING 1A INSPECTION THE AFT GALLEY EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MX R & R THE AFFECTED LIGHT INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20130407050Skin · crackedDURING A-CK INSPECTION, THE RT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT FRAME 75 JUST BELOW STR2R. MX PERFORMED A DOUBLER REPAIR WITH DRAG ANGLE IAW ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-02353, AND ACFT APPROVED FOR SERVICE.SDR ASOA20121205164Skin · corrodedTHE FORWARD LOWER FUSELAGE INTERNAL SKIN WAS NOTED WITH CORROSION BEYOND LIMITS BETWEEN FRAMES 13 & 14, STRINGER 19L THRU 18R. R & R SKIN PANEL, REMAPPED LT & RT RVSM CRITICAL REGIONS. ACFT STILL IN C-CHECK.SDR ASOA20121128160Splice · corrodedLONGITUDINAL SKIN SPLICE STRAP CORRODED BETWEEN FRAME 13 AND 14, STRINGER 19L. REMOVED CORRODED SECTION OF STRAP, FABRICATED AND INSTALLED NEW STRAP.SDR ASOA20121128159Splice · corrodedCIRCUMFERENTIAL SKIN SPLICE STRAP CORRODED BETWEEN FRAME 13 & 14, STRINGER 21L THRU 18R. CUT-OUT CORRODED SECTION OF STRAP, FABRICATED AND INSTALLED NEW STRAP.SDR ASOA20120509070Socket · dirtyDURING MX INSPECTION, THE LT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MX CLEANED THE LIGHT BULB SOCKET, OPS TESTED WITH NO DEFECTS AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA201205068Light · inoperativeDURING MX INSPECTION OF THE EMERGENCY LIGHTS, THE AISLE PATH LIGHT STRIP AT ROW 12 WAS FOUND TO BE INOPERATIVE. MX R & R THE EMERGENCY LIGHT STRIP, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20120214020Terminal · looseTHE CREW REPORTED A STRONG ELECTRICAL ODOR COMING FROM BEHIND THE CAPTAINS SEAT. MX R & R BURNED LOOSE TERMINAL LUGS AT DC BUSS NR 1 BUSS BAR, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA11IA060Skin · crackedIAH - DURING MAINTENANCE INSPECTION THE CROWN SKIN PANEL ON THE CAPTAINS SIDE WAS FOUND TO BE CRACKED BETWEEN THE CAPTAINS DV WINDOW AND THE CAPTAINS WINDSHIELD. MAINTENANCE PERFORMED A DOUBLER REPAIR, LEAK CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVSDR C2XA10IA225Battery · overtempIAH - FLIGHT 2336, DURING TAXI THE CREW REPORTED A BATTERY TWO OVERTEMP. THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO BATTERY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICESDR C2XA10SH257Battery · overtempJAN - BATTERY NR 2 OVERTEMP. REMOVED AND REPLACED NR 2 BATTERY IAW EMB 145 AMM 24-36-01. OPS CHECK GOOD. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA10IA211Ballast · defectiveIAH - FLIGHT 2547, DURING PREFLIGHT INSPECTION THE CREW REPORTED A BURNING SMELL IN THE CABIN. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE GALLEY LIGHT BALLAST, OPERATIONALLY TESTED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TOSDR C2XA10IA204Ballast · overheatedIAH - FLIGHT 2034, DURING POST FLIGHT INSPECTION THE CREW REPORTED A STRONG BURNING SMELL IN THE GALLEY, AND THAT THE GALLEY LIGHT BALLAST WAS INOP. MAINTENANCE INSPECTED GALLEY AREA, REMOVED AND REPLACED THE GALLEY LIGHT BALLAST, OPERATIONALLY TESTED WITH NOSDR C2XA10SH199Skin · crackedSHV - DURING C CHECK IT WAS FOUND THAT THE VERTICAL STABILIZER INTERNAL FITTING WAS FRETTING WITH THE AFT FUSELAGE SKIN AT FRAME 75 BY STRINGER 1L. THE FRETTING CAUSED THE SKIN TO CRACK AND WAS DETECTED USING EDDY CURRENT. MAINTENANCE PERFORMED A DOUBLER REPSDR C2XA10SH198Attach Bracket · wornSHV - DURING C CHECK THE LT SPEED BRAKE CENTER ATTACH BRACKET WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHING. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 145 AMM 20-10-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA10SH197Attach Bracket · wornSHV - DURING C CHECK THE LT GROUND SPOILER ACTUATOR ATTACH BRACKET WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHING. MAINTENANCE PERFORMED A BUSHING REPAIR IAW EC5750-01415. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA10SH196Beam · corrodedSHV - DURING C CHECK THE PILOTS WINDSHIELD CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED AT SCREW HOLES 41, 43, 45, 49. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A BUSHING REPAIR IAW EC5310-01515. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA10SH195Floor Support · corrodedSHV - DURING C CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA10SH194Skin · crackedSHV - DURING C CHECK THE RT AFT SKIN WAS FOUND TO BE CRACKED AROUND FASTENER AT FRAME 75 BETWEEN STRINGERS 1-2R. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EC5330-02146. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA10SH189Beam · corrodedSHV-DURING C CHECK THE CARGO DOOR CUT-OUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EC 5320-01479. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA10SH188Stringer Splice · corrodedSHV - DURING C CHECK THE SPLICE ON STRINGER 18L WAS FOUND TO BE CORRODED BETWEEN FRAMES 60-61. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SPLICE IAW EMB 145 SRM 53-00-03. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA10TY011Skin · dentedTYS - A/C WAS A OVERNIGHT A/C WHEN INSPECTION FOUND MULTIPLE DENTS IN A SMALL AREA OUT OF LIMITS. MAINTENANCE CUT OUT THE DAMAGE AREA AND FAB A FILLER AND DOUBLER IAW ETD2009-145/10249. ALL WORK WAS ACCOMPLISHED AND RELEASED.SDR C2XA09IA199Wire · brokenIAH - DURING MAINTENANCE INSPECTION THE AISLE PATH LIGHT STRIP AT ROWS 16 & 17 WAS FOUND TO HAVE BROKEN WIRES. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICESDR C2XA09IA198Wire · brokenIAH - DURING MAINTENANCE INSPECTION THE AISLE PATH LIGHT STRIP AT ROW 8 & 9 WAS FOUND TO HAVE BROKEN WIRES. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09IA077Light · inoperativeIAH - DURING A-CK INSPECTION THE SERVICE DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE SERVICE DOOR EMERGENCY LIGHT, OPERATIONALLY TESTED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA08IA160Oil System · leakingIAH - FLIGHT 2684, THE CREW REPORTED THAT THE NUMBER ONE ENGINE OIL QUANTITY DROPPED TO 3 QTS IN FLIGHT WHILE PRESSURE AND TEMPERATURE REMAINED NORMAL. THE CREW SHUT DOWN THE NUMBER ONE ENGINE AS A PRECAUTION AND THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. SDR C2XA08CL011Structure · looseCLE FLIGHT 2532 - THE CREW REPORTED THE MAIN CABIN DOOR WAS HARD TO OPEN. MAINTENANCE INSPECTED AND TIGHTENED BOLTS ON THE MAIN CABIN DOOR INNER HANDLE BOX. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.SDR C2XA07SH063Panel · corrodedSHV - DURING C-CHECK MAINTENANCE FOUND LOWER AILERON SHROUDS BONDING STRIPS WITH CORROSION. MAINTENANCE REPAIRED LOWER AILERON SHROUD IAW EC5750-01315 REV D. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA07SH062Panel · corrodedSHV - DURING C-CHECK MAINTENANCE FOUND PNL 193 BONDING STRIPS WITH CORROSION. MAINTENANCE REPAIRED PNL 193 BONDING STRIPS IAW EC 5750-01315 REV D. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA07SH061Frame · crackedSHV - DURING C-CHECK MAINTENANCE FOUND FRAME 65 WITH CORROSION UNDER CARGO DOOR HOLD OPEN ROD SUPPORT BRACKET. MAINTENANCE REPAIRED CARGO DOOR HOLD OPEN ROD SUPPORT BRACKET IAW EC 5330-01719. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA07SH060Nut Plate · corrodedSHV - DURING C-CHECK MAINTENANCE FOUND 4 NUT PLATES LOCATED AT BOTTOM OF MAIN DOOR CORRODED. MAINTENANCE REPAIRED NUT PLATES AT THE BOTTOM OF THE MAIN DOOR IAW EC 5210-01152 ORIG. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA07RI006Engine · contaminatedFLT 4930 - IAD CREW REJECTED TAKE OFF DUE TO SMOKE IN COCKPIT. SMOKE OCCURRED WHEN THRUST WAS ADVANCED TO DETENT. SMOKE CLEARED WHEN THRUST WAS REDUCED AND AFTER ENGINES WERE SHUT DOWN. SMOKE WAS A BLUE/GRAY COLOR. IAD MX RAN NR 1 & 2 ENGINES WITH PAKS TO PURGSDR C2XA07TY007Engine · damagedTYS A/C HAD SMOKE ON CLIMBOUT AND THEN CLEARED. THEN ANOTHER TIME ON LEVELING OFF, AGAIN LEFT. A/C WAS CHECKED OUT AND FERRIED TO TYS. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE IAW RR TASKCARD 627100. OPS AND LEAK CHECKS WERE GOOD, RELEASED BACK TO SDR C2XA07CL015Engine · contaminatedCLE FLIGHT 2965 THE CREW REPORTED CLIMBING THRU 7500 FT. THE F/A REPORTED SMOKE FILLING THE CABIN. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND RAN ENGINES AND PACKS UNTIL SMOKE DISSIPATED. FOUND CAUSE TO BE DEISDR C2XA07IA027Relay · shortedFLIGHT 1281, PILOT REPORTED THAT A LAV SMOKE INDICATION ILLUMINATED DURING CLIMB OUT. A VISUAL INSPECTION WAS PERFORMED AND SMOKE, FIRE AND/OR UNUSUAL ODORS WERE NOT NOTICED. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE LAV SMOKE WARNING SYSTEM OPERATIONALLY TESSDR C2XA06CL050Inverter · inoperativeCLE FLIGHT 2808 THE CREW REPORTED THE FORWARD EMERGENCY SIGN OVER THE F/A'S SEAT WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 1 INVERTER. OPERATIONAL CHECKS WERE GOOD.SDR C2XA05CL075Light · inoperativeDURING ROUTINE MAINTENANCE, THE EMERGENCY LIGHT ON THE SERVICE DOOR WAS INTERMITTENT. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY ON THE SERVICE DOOR. OPERATIONAL CHECKS WERE GOOD.SDR C2XA05SH051Firewall · chafedSHV - DURING C-CHECK RIVET HEAD WEAR MARKS ON BOTTOM RT SIDE OF APU FIREWALL. MAINTENANCE REPAIRED THE APU FIREWALL AT FRAME 81 IAW EC 5310-01337. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA05SH050Floor Support · corrodedSHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT VARIOUS AREAS BETWEEN FRAMES 35-39. MAINTENANCE REPAIRED LT OMEGA BEAM BETWEEN FRAME 38 - FRAME 39 PER EC 5320-01247, NO FURTHER ACTION REQUIRED. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA05SH049Floor Support · corrodedSHV - DURING C-CHECK LT OMEGA BEAM HAS AREAS OF CORROSION BETWEEN FRAMES 45 & 53. MAINTENANCE REPAIRED LT OMEGA BEAM AT FRAME 49 PER EC 5320-01247, NO FURTHER ACTION REQUIRED. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA05SH048Floor Support · corrodedSHV - DURING C-CHECK LT OMEGA BEAM HAS VARIOUS AREAS OF CORROSION BETWEEN FRAMES 29-36. MAINTENANCE REPAIRED LT OMEGA BEAM AT FRAME 33 - FRAME 34 PER EC 5320-01247, NO FURTHER ACTION REQUIRED. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA05SH047Floor Support · corrodedSHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT VARIOUS AREAS BETWEEN FRAMES 22 & 29. MAINTENANCE REPAIRED LT OMEGA BEAM AT FRAME 29 PER EC 5320-01247, NO FURTHER ACTION REQUIRED. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA05SH046Floor Support · corrodedSHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT VARIOUS AREAS BETWEEN FRAMES 52 & 59. MAINTENANCE REPAIRED LT OMEGA BEAM AT FRAME 54 AND AT FRAME 59 PER EC 5320-01247, NO FURTHER ACTION REQUIRED. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA05SH045Floor Support · corrodedSHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION FR 39-45. MAINTENANCE REPAIRED LT OMEGA BEAM AT FR 44 PER EC 5320-01247, NO FURTHER ACTION REQUIRED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA05IA055Connector · dirtyIAH - FLIGHT 2638, THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHT ABOVE THE FA SEAT WAS INOPERATIVE. MAINTENANCE CLEANED THE ELECTRICAL CONNECTORS, OPERATIONALLY CHECKED THE EMERGENCY LIGHTS WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICSDR C2XA04IA135Wire · looseCREW REPORTED THE OVERHEAD EMERGENCY EXIT LIGHT AT THE EXIT ROW WAS INOPERATIVE. RESECURRED THE WIRE AT THE LIGHT. OPERATIONALLY CHECK OK. AIRCRAFT RETURNED TO SERVICE.SDR C2XA04CL058Sign · inoperativeTHE CREW REPORTED THE EMERGENCY EXIT SIGN ABOVE THE FLIGHT ATTENDANT JUMPSEAT WAS INOPERATIVE. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF THE EMERGENCY LIGHT SYSTEM. OPERATIONAL CHECKS WERE GOOD. NO DEFECTS WERE FOUND. THE AIRCRAFT RELEASED FOR SERVICE.SDR C2XA04SH202Wire Harness · pinchedIAH - FLIGHT 2064 THE CREW REPORTED A STRONG ELECTRIC BURNING ODOR WHEN THE WINDSHIELD HEAT WAS SELECTED ON. THE AIRCRAFT LANDED AT IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE PLACED THE WINDSHIELD HEAT ON MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN SDR C2XA03CL168Inverter · inoperativeDURING ROUTINE MAINTENANCE THE CENTER FUSELAGE CABIN EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE CENTER FUSELAGE CABIN EMERGENCY CEILING LIGHT INVERTER. OPERATIONAL CHECKS OF THE EMERGENCY LIGHTS WERE GOOD.SDR C2XA03BT094Light · faultyCREW REPORTED, OVERHEAD EMERGENCY EXIT LIGHT AFT SIDE, WILL NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ON THE AFT SIDE IAW EMB145 AMM . OPS CHECKED GOOD.
Back to N14942, cancelled Nov 15, 2016