N18102, cancelled Mar 13, 2025
Service difficulty reports · 69
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 = 'N18102' AND deregistration_id = 'N18102-2025-03-13' 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 = 'N18102' AND deregistration_id = 'N18102-2025-03-13' 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 RAIA2019080631001Angle · corrodedAFT CARGO DOOR CUTOUT FWD LATERAL "L" SHAPE ANGLE HAVE CORROSION AT FRAME 65 LOWER CORNER IN 3 PLACES. REMOVED AND REPLACED L ANGLESDR RAIA201905190001Control System · inoperativeE1 OPERATING 9% BELOW N1 RATING DURING CLIMBOUT. A/C IS STILL IN WORK. SUPPLIMENTAL INFORMATION FROM ORIGINAL ENTRY. R&R CONTROL STAND ASSEMBLY. OPS CHECK GOOD.SDR RAIA2018082960001Fuel Cell · leakingLEFT WING HAD FLUID COMING FROM IT DURING FLT. FOUND FUEL TO BE LEAKING FROM BOTTOM OF LT WING 18 INCHES FWD OF THE JACK POINT FROM SKIN JOINT. CLASSIFIED AS RUNNING LEAK IN TYPE I AREA. SEALED THE INNER SKIN OF FUEL TANK. LEAK CHECKED GOOD.SDR RAIA201806050001Fan · malfunctionedCOCKPIT RECIR FAN INOP IN FLIGHT. R&R RECIRC FAN OPS TEST GOOD.SDR RAIA201803160001Hydraulic System · malfunctionedIN FLIGHT, THE NR 1 HYDRALIC PUMP FAILED, CAUSING THE NR 1 HYDRAULIC SYSTEM TO FAIL. INSPECTED THE NR 1 HYDRALIC SYSTEM FLUID LEVEL, FOUND GOOD. GV INSPECTED BOTH PUMPS, RAN BOTH PUMPS INDIVIDUALLY AND TOGETHER MOVING FLIGHT CONTROLS AND APLYING BRAKES. ASDR RAIA201705120001Bolt · brokenLG LEVER DISAGREE EICAS WARNING AFTER DEPARTURE WITH A RED HATCHED BOX OVER LEFT MAIN LANDING GEAR INDICATOR. REMOVED AND REPLACED BROKEN TOP BOLT OF LT SHOCK ABSORBER. FERRIED AIRCRAFT TO STL. REMOVED AND REPLACED LT MAIN LANDING GEAR LEG STRUCTURE ASSY DUE TSDR RAIA201612210001Bulb · inoperativeCEILING EMERGENCY LIGHT AT ROW 18 INOPERATIVE. R & R THE BULB. OPS CHECKED GOOD.SDR RAIA201605170001Radar · inoperativeRADAR WILL PAINT AN IMAGE ON THE RT SWEEP BUT ERASES EITHER SOME OR ALL OF THE IMAGE ON THE LT SWEEP. THIS OCCURED ON ALL RANGES AND ON BOTH MFD'S. R & R WEATHER RTA ASSEMBLY. OPS CHECK GOOD.SDR RAIA201605070001Control Panel · inoperativeALL EMERGENCY LIGHTS WILL NOT COME ON WITH SWITCH ON F/A'S CONTROL PANEL. R & R F/A CONTROL PANEL. OPS CHECK GOOD.SDR RAIA201603220001Engine · leakingON TAKEOFF AT 100 KNOTS, STRONG SMOKE/BURNING ODOR WITH A LIGHT BLUE HAZE IN THE COCKPIT, ALSO NOTICED IN THE CABIN, EMERGENCY LANDING. MAINTENANCE REPLACED NR 1 ENGINE, LEAK AND OPS CHECK GOOD.SDR RAIA201603170001Light · inoperativeLARGE EMERGENCY EXIT LIGHT ON SIDEWALL PANEL AT ROW 18A IS INOPERATIVE. MAINTENANCE DISCONNECTED CONNECTORS, INSPECTED, RECONNECTED CONNECTORS, NO DEFECTS NOTED, OPS CHECK GOOD.SDR RAIA201602280001Hydraulic System · unknownSTEADY LOSS OF HYDRAULIC FLUID IN FLIGHT. DID A FULL HYDRAULIC TEST AND LEAK CHECK OF NR 1 SYSTEM HYDRAULICS. NO DEFECTS FOUND AT THIS TIME. SERVICE HYDRAULIC FLUID TO FULL.SDR RAIA201507280002Light · unknownPAX DOOR SWING ARM EMERGENCY LIGHT IS INOPERATIVE. OPS CHECKED EMERGENCY LIGHT. OPS CHECKED GOOD.SDR ASOA20121117132Frame · crackedDURING C-CHECK, FRAME 10 CRACKED UNDER RT DV WINDOW CUTOUT. VERIFIED WITH EDDY CURRENT. MX R & R FRAME 10 IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20121117131Frame · crackedDURING C-CHECK, FRAME 10 CRACKED UNDER LT DV WINDOW CUTOUT. VERIFIED WITH EDDY CURRENT. MX R & R FRAME 10 UNDER LT DV WINDOW IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20121117130Frame · bentDURING C-CHECK, FRAME 72 BENT AT STRINGER 15L-16L. MX R & R FRAME 72, BETWEEN 16L AND 13R IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20121117129Frame Splice · crackedDURING C-CHECK, FRAME 72 SPLICE CRACKED AT STRINGER 15L-16L. MX R & R FRAME 72 SPLICE AT FRAME 72, STRINGER 15L AND 16L IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20121117128Frame · crackedDURING C-CHECK,K FRAME 72 CRACKED AT RIVET ON STRINGER 16L. MX R & R FRAME 72 BETWEEN STRINGER 16L AND 13R IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20121117127Floorbeam · corrodedDURING C-CHECK CENTER FLOORBEAM AT FRAME 49 AREA HAS CORROSION . MX COMPLETED AND INSTALLED THE FABRICATED REPAIR DOUBLER AT CENTER FLOORBEAM AT FRAME 49 AREA IAW EC5310-01466. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20121117126Floorbeam · corrodedDURING C-CHECK, LT FLOORBEAM AT FRAME 38 CROSSBEAM AREA HAS CORROSION. MX COMPLETED REPAIR ON LT FLOORBEAM AT FRAME 38 IAW SRM 53-00-10. DETERMINED TO BE A MINOR IAW SOP 5702. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20121117125Floor Support · corrodedDURING C-CHECK, LT OMEGA BEAM AT FRAME 59 CROSSBEAM AREA HAS CORROSION. MX COMPLETED INSTALL OF LT OMEGA BEAM REPAIR AT FRAME 59 CROSSBEAM AREA IAW EC5310-01466 ORIG AND IAW SRM 53-00-10. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20121117124VFloor Support · corrodedDURING C-CHECK , RT OMEGA BEAM AT FRAME 23 IS CORRODED AT NUTPLATE. MX FABRICATED AND INSTALLED REPAIR DOUBLER AT RT OMEGA BEAM AT FRAME 23 AT NUTPLATE IAW EC5320-01443, REV C. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA201112140008Control Unit · failedADC 1 WENT OUT IN FLIGHT. R & R NR 1 COMMS UNIT IAW AMM 23-00-01. OPS CHECKED GOOD, ACFT RELEASED AND RETURNED TO SERVICE.SDR C2XA11IA220Apu · malfunctionedIAH - FLIGHT 2373 THE CREW REPORTED THAT THE APU FAILED ON ROTATION OUT OF JAX WITH AN APU OIL LO PRESS MESSAGE AND A BURNING OIL ODOR. THE AIRCRAFT CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE APU AND PLACED IT ON MEL 49-00-0SDR C2XA11TY125Case · fodTYS - A/C WAS FERRIED FRON BNA TO TYS FOR FOD DAMAGE WHERE MAINTENANCE REMOVED AND REPLACED THE FAN CASE (PN-145-75001-409-SN-NC1476); MULTIBLE BYPASS VANES (PN-23067033) BOROSCOPE NR 1 ENGINE IAW RR MM 05--50-200-804 AND RR MM 72-50-00-801, NO DAMAGE OR DEFECSDR C2XA11RI085Controller · defectiveFLIGHT 2398 - EWR - FLIGHT CREW REPORTED PRESSURIZATION DIFFERENTIAL READS ABOUT 1-2 PSI LOWER THAN IT SHOULD AT ALL ALTITUDES - FL350- 5.9 PSI. EWR MX REMOVED AND REPLACED DIGITAL AND MANUAL PRESSURIZATION CONTROLLERS. EWR MX PERFORMED OPERATIONAL CHECK SUCSDR C2XA11RI084Controller · defectiveFLIGHT 2398 - EWR - FLIGHT CREW REPORTED PRESSURIZATION DIFFERENTIAL READS ABOUT 1-2 PSI LOWER THAN IT SHOULD AT ALL ALTITUDES - FL350- 5.9 PSI. EWR MX REMOVED AND REPLACED DIGITAL AND MANUAL PRESSURIZATION CONTROLLERS. EWR MX PERFORMED OPERATIONAL CHECK SUCSDR C2XA11SH046Floor Support · corrodedSHV - DURING C-CHECK CENTER OMEGA BEAM HAS CORROSION AT FR 20. REPLACED OMEGA BEAM IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA11SH045Skin · crackedSHV - DURING C-CHECK FUSELAGE SKIN IS CRACKED AROUND RIVETS AT FR 80. REPAIRED SKIN IAW EC5330-02364. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA10RI153Controller · inoperativeFLIGHT 2451 - STL - FLIGHT CREW REPORTED AUTO PRESS INOP IN FLIGHT AND DECLARED EMERGENCY DESCENT INTO STL. IAH MX REMOVED AND REPLACED AUTO PRESS CONTROLLER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA09TY200Sill · corrodedTYS - A/C CURRENTLY IN C-CHECK WHEN INSPECTION FOUND CORROSION ON THE RIGHT FLOOR SILLS FROM FRAME 29 THRU FRAME 48 OUT OF MFG LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOOR SILLS IAW EMB 145XR SRM 51040-02. A/C WILL BE RELEASED AT THE END OF THE CHECK.SDR C2XA09TY198Sill · corrodedTYS - A/C CURRENTLY IN A C-CHECK STATUS WHEN INSPECTION FOUND THE LEFT FLOOR SILLS FROM FRAME 19A TO FRAME 36 CORRODED BEYOND MFG'S LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOOR SILLS IAW EMB 145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASDR C2XA09TY205Floor Support · corrodedLT OMEGA BEAM TOP CAP IN LAV BETWEEN FRM 59-62 IS CORRODED AROUND RIVETS AND NUT PLATES. BLENDED OUT CORROSION AND IS WITHIN LIMITS, ALODINED, PRIMED AND PAINTED.SDR C2XA09TY204Mount · corrodedLT FRM MOUNT FOR LT CARBON FIBER BEAM BULKHEAD SUPPORT AT FRM 61 HAS CORROSION AT LOWER EDGE. BLENDED CORRODED AREA, FABRICATED EXTERNAL DOUBLERS, ALODINED, PRIMED AND PAINTED IAW EC5320-01462.SDR C2XA09TY202Flange · corrodedNR 1 ENG INLET ATTACH FLANGE HAS CORROSION AROUND BOLT HOLES. REAMED AND INSTALLED BUSHING IAW EC5420-01158.SDR C2XA09TY196Sill · corrodedRT FLOORBOARD SILL BETWEEN FRM 53-60 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SILL.SDR C2XA09TY195Sill · corrodedLT FLOORBOARD SILL BETWEEN FRMS 53-60 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FLOOR SILL.SDR C2XA09TY194Floor Support · corrodedRT OMEGA BEAM TOP CAP IN LAV HAS CORROSION UNDER CARBON BEAM AT FRM 61. REMOVED AND REPLACED TOP CAP.SDR C2XA09TY191Floor Support · corrodedLT OMEGA BEAM TOPCAP IN LAV BETWEEN FRMS 59-62 IS CORRODED AROUND RIVETS AND NUT PLATES. BLENDED OUT CORROSION, IS WITHIN LIMITS. ALODINED, PRIMED AND PAINTED.SDR C2XA09TY190Sill · corrodedLT SIDE FLOORBOARD SILL BETWEEN FRM 41-48 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SILL.SDR C2XA09TY189Sill · corrodedRT FLOORBOARD SILL BETWEEN FRM 48-53 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FLOOR SILL.SDR C2XA09TY188Sill · corrodedLT SIDE OF FLOOBOARD SILL BETWEEN FRM 29-35 HAS CORROSION BEYOND LIMITS. REMOVED AND REPLACED FLOOR SILL.SDR C2XA09TY183Sill · corrodedTYS - THE RIGHT FLOOR SILL BETWEEN FR 59 THRU 61 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE RIGHT FLOOR SILL IAW 145XR SRM 51-40-02 AND CPM 51-21-03, 04, 06.SDR C2XA09TY182Bracket · corrodedTYS - THE LAV FLOOR TOPCAP HAS SURFACE CORROSION UNDER THE POTABLE WATER OVERFILL B-NUT. MAINTENANCE REMOVED AND REPLACED THE WATER POTABLE SUPPORT BRACKET IAW EMB 145XR SRM 51-40-02, 03, 04 AND CPM 51-21-O5. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPSDR C2XA09TY181Sill · corrodedTYS - CORROSION WAS FOUND ON THE LEFT SILL BETWEEN FR 59 TO FR 60. MAINTENANCE REMOVED AND REPLACED THE SILL IAW EMB A45XR SRM 51-40-02 AND CPM 51-21-04-05-06. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.SDR C2XA09TY172Attach Fitting · corrodedNR 2 ENG INLET ATTACH FLANGE HAS CORROSION AROUND 9 NUT PLATE HOLES. REAMED TO REMOVE CORROSION AND INSTALLED BUSHINGS IAW EC5420-01158.SDR C2XA09TY168Skin · chafedTYS - A/C IN A C-CHECK STATUS WHEN THE VENTRAL TANK WAS FOUND CHAFING THE LOWER FORWARD EDGE OF BELLY SKIN. MAINTENANCE BLENDED AREA AND FOUND TO BE WITHIN LIMITS. WORK WAS ACCOMPLISHED IAW EMB 145XR SRM 51-10-03. ALODINED, PRIMED AND PAINTED IAW CPM 51-21-SDR C2XA09SH192Inverter · inoperativeRIGHT OVERWING EXIT SHROUD EXIT IDENTIFIER SIGN INOPERATIVE. REMOVED AND REPLACED NR 3 DC/AC INVERTER P/N 7824-1, S/N ILLEGIBLE WITH P/N 7824-1 S/N PT4563 IAW EMB145XR AMM 33-50-11 AND OPS CHECKED GOOD.SDR C2XA09RI122Light · brokenFLIGHT CREW REPORTED EMERGENCY LIGHT STRIP BROKEN. MX REMOVED AND REPLACED LIGHT STRIP AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA09TY082Fuse · blownTYS - DURING ROUTINE MX BOTH OVERWING EMERGENCY LIGHTS WERE FOUND INOP. THE NR 4 BATTERY FUSES WERE REMOVED AND REPLACED AND OPS CHECKED GOOD IAW RADIANT POWER CORP VCMM 25-60-03.
Back to N18102, cancelled Mar 13, 2025