N19141
Service difficulty reports · 138
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 = 'N19141' 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.
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 = 'N19141' AND registry_match = 'registration' 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 CALA2026082418821Lamp · inoperativeEMERGENCY LIGHTS PANEL BACKLIGHT INOPERATIVE, OVERHEAD EMERGENCY LIGHTS, PAX OXYGEN PANEL LIGHT PLATE DARK. SOLDERED & REPLACED THE LAMPS IN LIGHT PLATE IAW AMM 33-13-01. OPS CHECK GOOD.SDR CALA2026071417789Computer · faultyTCAS RA CLIMBING THRU 5000..CLIMB FOR 2000 FOLLOWED BY DESCEND WITH NO VISIBLE TRAFFIC, WORK WITH FIM 34-45 TASK 801. MTX WORKING ITEM REF LP 9587435 FOR WORK PERFORMED TCAS RA CLIMBING THRU 5000. CLIMB FOR 2000 FOLLOWED BY DESCEND WITH NO VISIBLE TRAFFIC RESDR CALA2026052116440Frame · dentedAFT CARGO BAY BS 1220, STR 26L , FRAME HAS DENT ON FREE FLANGE AREA. REPAIR PARTS FABRICATED. ACCOMPLISHED BS 1220, STR 26L FRAME REPAIR IAW ECRA 5360-021 45 AND VT MAE EA 757-5360-13-A4444 REV-.SDR CALA2026051416240Web · dentedSTABILIZER COMPARTMENT, THROUGH ACCESS 311AL, CLOSE TO STA 1862.70, STABILIZER CUTOUT, LH SIDE, WEB HAS A DENT. REF NR 145862. REMOVED AND REPLACED DENTED WEB BY NEW WEB PN UA-148N7309-23 FRO M TAB SHOP TRAVELER# T26/1863849 IAW B757-200 SRM 51-40-02-0G-0, RSDR CALA2026051116134Threshold · crackedREMOVED AND INSTALLED THRESHOLD ON FWD CARGO COMP. IAW AMM 53-13 -02-004 AND AMM 53-13-02-424-005 NR: 145675 REPLACEMENT OF THRESHOLD WAS DUE TO CRACK NOTED , NEW THRESHOLD FWD CARGO THRESHOLD CRACKED AT PREVIOUS WELD. REMOVED AND INSTALLED THRESHOLD ON FWD CSDR CALA2026051116128Support Angle · gougedVERTICAL STAB LT SIDE ACCESS PANEL 324AL LOWER SUPPORT ANGLE GOUGED. REMOVED AND REPLACED DAMAGED ANGLE BY NEW ANGLE IAW SRM 51-40-02 RESTORED SURFACE PROTEC ION AT AREA IAW AMM TASK 51-21-15-370-801 STA 1804.81SDR CALA2026051116124Skin · crackedLEFT WING NR 2 SLAT COVE SKIN AROUND INBD MAIN TRACK CRACKED. REMOVED, FABRICATED, REPLACED COVE. SKIN COMMON TO NR 2 SLAT IAW SRM 51-40-02-0G-1 AND REF DWG 114N7076.SDR CALA2026051116122Skin · crackedNUMBER 10 SLAT OTBD COVE SKIN CRACKED NEAR 652BB COVER PANEL. REMOVED, FABRICATED, INSTALLED COVE SKIN COMMON TO NR 10 SLAT OTBD IAW SRM 51-40-02-0G AND DWG 114N4075.SDR CALA2026051116120Skin · crackedRIGHT WING, NR 10 SLAT, INNER SURFACE, CLOSE TO INBD TRACK, SKIN HAS A CRACK. REMOVED, FABRICATED, INSTALLED COVE SKIN COMMON TO NR 10 SLAT IAW SRM 51-40-02-0G AND DWG 114N4075.SDR CALA2026051016092Skin · crackedRIGHT WING, NR 8 SLAT, INNER SURFACE SKIN HAS A CRACK. REMOVED, FABRICATED, REINSTALL NEW COVE SKIN O/T NO. 8 SLAT IAW DWG 114N4077 AND SRM 51-40-02-0G MATERIAL 7075 T6.056 THICK, NO DEVIATION IAW OPS CHECK AMM 27-81-02-424-021.SDR CALA2026051016090Angle · crackedLEFT MLG W/W STA 1037 BEAM ANGLE CRACKED AT LBL 64 BEHIND ACCESS PANEL 197AL. THE ANGLE WAS REMOVED IAW B757-300 SRM 51-40-02-0G, ANGLE WAS FABRICATED IAW DWG 149N7553 REV N AND PL LOCATED AND DRILLED NEW ANGLE IAW SRM 51-40-05-0G, NEW ANGLE WAS TREATED PRIMESDR CALA2026050816079Transition Panel · corrodedFWD CARGO BETWEEN STA 620 TO 640 RT TRANSITION PANEL WITH CORROSION. REMOVED AND REPLACED TRANSITION PANEL IAW SRM 51-40-02-0G-0, & SRM 51-40-05-06-0.SDR CALA2026050716052Support · damagedAFT CARGO COMPT. STA. 1200, LBL 24.75 CEILING PLATE SUPPORT BROKEN. CEILING SUPPORT WAS REMOVED IAW B757-200 SRM 51-40-02-0G NEW SUPPORT WAS FABRICATED , LOCATED AND DRILLED IAW SRM 51-20-05-0G SUPPORT WAS TREATED, PRIMED AND PAINTED IAW AMM 51-21-04, AMM 5SDR CALA2026050516007Support Bracket · crackedFWD CARGO STA 740 RH SIDE SUPPORT BRACKET THAT ATTACH SIDWALL IS BENT. CHANNEL SUPPORT AND 06EA NUTPLATE WERE REMOVED IAW B757-200 SRM 51-40-02-0G, PART FABRICATION PERFORMED IN-HOUSE, HEAT TREATMENT ACCOMPLISHED, HARDNESS: 84, CONDUCTIVITY: 48.0, IAW BA C560SDR CALA2026050515973Splice Angle · corrodedACCESS PANEL 139CL FORWARD KEEL BEAM REQUIRE FURTHER CLEANING AT PANEL ATTACH FRAMES AND CHECK ON CORROSION. CLEANED AREA IAW BOEING SOPM 20-30-03, REMOVED CORROSION ON LH A ND RH TEE BEAM BTW 995-1040 IAW B757-200 SRM 51-10-02-0G-0. ORIG INAL THICKNESS .130SDR CALA2026050515971Splice Angle · corrodedACCESS PANEL 139AL FORWARD KEEL BEAM REQUIRE FURTHER CLEANING AT PANEL ATTACH FRAMES AND CHECK ON CORROSION. CLEANED AREA IAW SOPM 20-30-03. REMOVED CORROSION IAW SRM 51-10-02-0G-0. ORIGINAL THICKNESS .130", REMAINING THI CKNESS .123" FOUND TO BE WITHIN LIMISDR CALA2026050515969Splice Angle · corrodedACCESS PANEL 139BL FORWARD KEEL BEAM REQUIRE FURTHER CLEANING AT PANEL ATTACH FRAMES AND CHECK ON CORROSION. CLEANED AREA IAW BOEING SOPM 30-30-03, REMOVED CORROSION ON LH A ND RH TEE BEAM BTW STA 965-995 IAW 51-10-02-0G-0. ORIGINAL THICK NESS .130" REMAININGSDR CALA2026050515966Support · crackedLEFT CEILING SUPPORT AT STA 1640-1681 CRACKED IN NUMEROUS LOCATIONS. REMOVED AND REPLACED LT CEILING SUPPORT AT BS 1640-1681, IAW SRM 51-40-02-0G -0 AND SRM 51-40-05-0G-0.SDR CALA2026050415964Support · crackedRT CEILING SUPPORT AT STA 1640-1681 CRACKED. REMOVED AND REPLACED L/H CEILING SUPPORT AT BS 1640-1681 BY NEW PART IAW B757-200 SRM 51-40-02AND SRM 51-40-05.SDR CALA2026043015885Floorbeam · corrodedLOWER FUSELAGE AT BS 900 LBL 0 TO RBL 12 T-CHORD WITH EXFOLIATED AND DELAMINATED. REPAIRED T-CHORD ON LOWER FUSELAGE WTB STRUCTURE AT STA 900 LBL 12 - RBL 12 IAW SRM 51-70-12-0G-0.SDR CALA2026043015883Intercostal · crackedAFT CARGO COMPT. BS 1200 CEILING AREA BL 0, INTERCOSTAL WEB IN FWD CORNER IN FWD CORNER CRACKED. THE DAMAGED INTERCOSTAL WAS REMOVED AND REPLACED, NEW INTE RCOSTAL WAS POSITIONED AND DRILLED IAW SRM 51-40-05-0G, AND NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-40SDR CALA2026042815766Angle · crackedRT MLG W/W FAIRING STRUCTURE ANGLE CORNER AT STA 1094 CRACKED. NR# 145213 ESFR INFORMATION ENTERED REMOVED AND REPLACED ANGLE CORNER AT RT MLG W/W FAIRING STRUCTURE AT BS 1094 IAW B757-200 SRM 51-40-02-0G-0.SDR CALA2026042815749Angle · crackedAFT CARGO CEILING BS 1420 - 1440, RBL 14.25 CRACKED CEILING ANGLE COMMON TO INTERCOSTAL. REMOVED AND REPLACED CEILING ANGLE AT AFT CARGO CEILING BS 1420 - 1440, RBL 14.25 COMMON TO INTERCOSTAL. IAW SRM 51-40-02-OG-0.SDR CALA2026042415674Angle · crackedAFT CARGO CEILING STA 1580 RBL 14.25: CRACKED CEILING ANGLE COMMON TO INTERCOSTAL. REMOVED AND REPLACED SUPPORT ANGLE IAW SRM 51-40-02-0G -0, APPLIED CIC IAW AMM 51-24-03-277-008.SDR CALA2026022614071O-Ring · damagedONE EMERGENCY FLASHLIGHT HAS A DAMAGED O-RING AT FWD FLIGHT ATTENDANT SEAT. REMOVED & REPLACED FLASHLIGHT.SDR CALA2026010612723Apu · faultedAFTER STARTING APU & DISCONNECTING GROUND POWER, CREW & PAX SAW & SMELLED SMOKE. WAS WHITE & HAD A BURNING ELECT ODOR. APU SHUTDOWN AUTOMATICALLY & CREW POWERED DOWN ADDITIONAL SYS. PERFORMED APU MAGNETIC CHIP DETECTOR INSP, FOUND METAL ON COMPRESSION BEARINSDR CALA2026010512668Slide · faultyLEVEL-2 CHRONIC DOOR L4 ARMING ISSUES. DUE REPEATED FAULTS OF D OOR L4 HARD TO ARM WITH REPEAT FINDINGS OF GIRT MATERIAL IMPENDI NG WITH ARMING FUNCTION. ALONG WITH REPEATED FINDINGS OF DAMAGE TO BUSTLE ASSY. THESE FAULTS STARTED AFTER THIS SLIDE WAS RECENT LYSDR CALA2025110310852Girt Bar · out of adjustL4 DOOR WILL NOT ARM, GIRT BAR WAS CLEANED ON FLOOR AND ADJUSTED MECHANISM IAW AMM 25-66-00. OPS CHECKED ARMED-DISARMED LEVER, DOOR SLIDE WAS SATISFACTORY. OK TO CONTINUE.SDR CALA2025102110345Fire Loop · faultedMULTIPLE INTERMITTENT RT ENGINE FIRE WARNINGS DURING CLIMB/CRUISE. RT ENGINE FIRE LOOP 2 INITIALLY INOPERATIVE IAW MEL, FIRE WARN WOULD HAVE WENT OFF DUE TO FAULT IN LOOP 1. FOUND POSITIVE FIX FOR RT ENG. FIRE LOOP 2. MEL CLEARED. NO FAULTS NOTED FOR RT ENG SDR CALA2025092409205Bottle · no discrepancyDOOR 2L SLIDE GAUGE IN THE RED PAST THE GREEN BAND. INSPECTED INFLATION CYLINDER ON DOOR 2L REF AMM 25-66-01-206-024, NEEDLE IS NOT MORE THAN HALF THE WIDTH OFF THE GREEN MARKER, PRESSURE REMAINS STABLE. OK FOR SERVICE.SDR CALA2025091508875Fuse · inoperativeEMERGENCY LIGHTS, OPERATIONAL TEST WITH THE TEST SWITCH PROCEDURE, DOOR 3R EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE POWER SUPPLY FUSE IAW AMM 33-51-07-962-071 OPS CHECKED GOOD. REPLACE LIGHT ASSEMBLY AS REF. AMM 33-51-06-962-049-001.SDR CALA2025091508894Girt Bar · fodDOOR 4R SLIDE LIGHT INOPERATIVE. REMOVED DEBRIS FROM GIRT BAR AREA. SLIDE LIGHT OPS NORMALSDR CALA2025091108781Lamp · inoperativeINOP SLIDE LIGHT IS ON DOOR 3R. REPLACED 3R SLIDE LIGHT OPS CHECK GOOD IAW AMM 33-51-06.SDR CALA2025081107530Unknown · odorSTRONG ODOR OF OIL IN COCKPIT, ON INSPECTION OF FLIGHT DECK VENT, TRACE OF OIL SMELL COMING FORM VENTS OK TO CONTINUE.SDR CALA2025073107177Wire · brokenEMERGENCY LIGHTS - OPERATIONAL TEST WITH THE TEST SWITCH PROCEDURE - AISLE PATH LIGHTING AT ROW 31 DOES NOT ILLUMINATE. FOUND BROKEN GROUND WIRE AT SPLICE LOCATED UNDER SEAT ROW 31. RESPLICED WIRE UNDER SEAT ROW 31 IN REF. SWPM 20-30-12 AND DRAWING BR2013-P-75SDR CALA2025062305805Battery Pack · no testEMERGENCY LIGHTS - OPERATIONAL TEST WITH THE TEST SWITCH PROCEDURE - DOOR 3L EMERGENCY LIGHT IS INOP RELAMP NO HELP, REF AMM 33-51-06-962-001-001. UPON FURTHER INSPECTION, REMOVED AND REPLACED RESPECTED BATTERY , LIGHT CAME ON OPPOSITE GOOD OK FOR OPERATION.SDR CALA2025051304647Governor · faultyLEFT ENG FAILED TO GET 1.60 EPR ON TAKEOFF ONLY REACHED 1.30 REJ ECTED AT 80KTSPERFORMED FIM 77-11 FAULT TREE 805. REMOVED AND REPLACED E1 EPR TRANSMITER IN REFF WITH AMM TASK 77-11-01. REQUIRES HIGH POWER RUN DUE TO E1 EPR DID NOT PASS 1.3.PARTS USED: 19-771SDR CALA2025032002999Battery · dischargedEMERGENCY LIGHTS - OPERATIONAL TEST WITH THE TEST SWITCH PROCEDURE - EXTERIOR RIGHT OVERWING EGRESS AFT EMERGENCY LIGHT (2 TOTAL) WILL NOT TEST. REF WDM 33-51-14-902, FOUND CONNECTOR M10699J AT SEAT ROW 28DEF (SEE PICTURE). NEED BATTERY PACK ME#75-3351-3-0041SDR CALA2025032002992Bulb · inoperativeEMERGENCY LIGHTS - OPERATIONAL TEST WITH THE TEST SWITCH PROCEDURE - EXTERIOR AT DOOR 2L EMERGENCY LIGHT WILL NOT TEST EVEN AFTER LIGHT BULB (767) REPLACEMENT. REF WDM 33-51-15-902, LOCATED M736 & M737 JUST BEHIND AFT GLY AREA LIGHT. SWAPPED CONNECTOR BUT NOSDR CALA2025022402433Cooling Fan · shortedSTRONG ELECTRICAL BURN SMELL IN FLIGHT FOUND CB FWD EQUIP COOL SUPPLY FAN 1 (F17) ON THE P6 PANEL POPPED. RESET CB PER GMM 05-30-05 AND PERFORMED OPS TEST OF FWD EQUIP COOL SUPPLY FAN REF AMM 21-58-06. CB IMMEDIATELY POPS WHEN EQUIP COOLING SWITCH IS DEPRESSEDSDR CALA2025021002270Girt Bar · fodDOOR 1R VERY STICKY AND HARD TO DISARM AND ARM. INSPECTED R1 DOOR PER AMM 52-11-01. FOUND PAPER IN THE GRIT BAR REMOVED UNWANTED MATERIAL. OPERATIONAL CHECK GOOD ON DOOR DISARMING AND ARMING.SDR CALA2025020402197Lanyard · out of position2L UNABLE TO ARM OR DISARM REMOVED OBSTRUCTION, SLIDE LANYARD, FROM GIRT BAR TRACK. ARMED AND REARMED DOOR 2L. FLIGHT CREW ARMED AND DISARMED DOOR 2L. NO COMPLAINTS. DOOR 2L ARMS AND DISARMS. NO DEFECTS NOTED.SDR CALA2025012301995Girt Bar · fodDOOR 1R WILL NOT ARM REMOVED DEBREE UNDER GIRT BAR AREA ,ARM AND DISARM DOOR OPS CHECKS NORMAL ,SUBTASK 25-66-01-094-102 ITEM 6 OK TO CONTINUESDR CALA2025010600028Charger · inoperativeDURING CABIN WALK AROUND FOUND EMERGENCY LIGHT INOP FROM SEAT ROW 32-41 REMOVED AND REPLACED BATTERY ASSY. IAW B757-200 AMM 33-51-07. OPERATIONAL CHECK GOOD.SDR CALA2024100400753Probe · faultedR ENG PROBE HEAT STATUS AFTER ENG START SUSPECT RT ENG PROBE M&E 19-7321-3-0002 MEL 3034B DISPATCH ADVISES THERE IS ICING NEAR BOS. ON DEFERRAL R&R ENG 2 P1 PROBE PER AMM TASK 73-21-04 AND OPS CHECKED GOOD AND PERFORMED IDLE RUN TO MAKE MSG DID NOT COME BACKSDR CALA2024080100343Computer · faultyACFT DIVERTED WITH MULTPLE GPWS RELATED FAULTS REMOVED AND REPLACED THE GPWS COMPUTER REF AMM 34-46-01 LOADED CURRENT TERRAIN DB VERSION 640 REF AMM 34-46-00 OPS CHECKS NORMAL.PARTS USED: 64-3446-9-0002,QTY :1 PARTS USED: 64-3446-9-0002,QTY :1 ROTABLE PARTS CSDR CALA2024032700883Access Panel · missingOIL FILLER DOOR MISSING UPON ARRIVAL. #1 ENGINE L/H OIL FILLER ACCESS PANEL. REPLACED MISSING OIL FILLER DOOR IN REFERENCE TO AMM 71-11-04-308-075-R00. AIPC REF 71-11-04-03.SDR CALA2023122203709Cover · out of positionWHEN SQUIB TEST BUTTON PRESSED TO NUMBER "1" POSITION BOTH WING SLIDE LIGHTS DO NOT ILLUMINATE. UPON FURTHER INVESTIGATION FOUND L/H AND R/H OVERWING SLIDE ARMING PANELS IN WRONG POSITIONS. SWAPPED PANELS TO PROPER CONFIGURATION REF AMM 25-65-11. AS STATED INSDR CALA2023121803661Liner · incorrectLEFT OVERWING ARM/DISABLE HANDLE COVER FOUND TO BE IN CLOSE AND FLUSH POSTION WITH SLIDE DISARMED LEFT OVERWING DISABLE HANDLE COVER FOUND TO BE IN THE INCORRECT LINING INSTL-HATCHWAY LS REFERENCE: 52-22-02-25 ITEM 280 POSITION. DOOR HANDLE WILL NOT BE ABLE TOSDR CALA2023071002213Unknown · unknownOPENED AMES WORK PACK N19141-2 FOR 8C + GEAR MAINTAINENCE CHECK.
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