JASC 5100
Service difficulty reports · 4,244
Reports filed under 5100 · Standard Practices/Structures, 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 jasc_code = '5100' 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 jasc_code = '5100' 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 CALA2023031500755Floor Support · corrodedFOUND CORROSION ON L1 DOOR SURROUND STRUCTURE SILL (REF. AAR NR 99960159). REMOVED AND REPLACED INNER CHORD ON L1 DOOR IAW B737-800 SRM 51-40-02-0G-0 (WORK ACCOMPLISHED BY V937429 AND AAR QC A-75 V938209)SDR CALA2023031500749Angle · corrodedCORROSION ON THE APU AIR INLET DOOR INTERIOR FWD FLANGE, UNDER THE NUTPLATES, AND THE FWD FLANGE IS EXFOLIATED WITH CORROSION BETWEEN THE FLANGE AND FUSELAGE SKIN. REMOVED THE APU AIR INLET DOOR ASSY, AND FABRICATED AND REPLACED THE UPPER AND LOWER FLANGES, ANSDR NACA2023072003Unknown · unknownAFT CARGO COMPT.- SECTION 46 S-27L SPLICE WITH CORROSION STA 907.0. PERFORMED MAJOR REPAIR CATEGORY "A" ON AFT CARGO CAOMPARTMENT SECTION 45 STA 907.0, S-27L. REMOVED CORRODED SPLICE IAW B737 SRM 51-40-02 PAG 4, FABRICATED SPLICE FROM AL 7075 "0" 0.063 IAW B73SDR CALA2023031500743Beam · corroded(B737-53-3-0711) CORROSION AROUND FASTENER HOLES ALONG BS 328 RB L 14, 30, 39 ON MAIN DECK FLOOR STRUCTURE. STA 328 RBL30 CORROSION OUT LIMITS REPAIRED IAW B737-800 SRM 53- 10-51-2R07 REPAIR 7. SEE PARTIAL WORK FOR ACCOMPLISHED ON FORM 4 4-0008. DATA WAS TRANSSDR HNAA2023032400089Unknown · unknownFR 23 HAS ELONGATED RIVET HOLES WHERE LH OUTBOARD #1 FLOOR SILL ATTACHES. REPAIRED IAW SRM 51-40-02 AND 53-00-04SDR 2023FA0000141Unknown · unknownENROUTE FROM RDU TO EGE, DIVERTED TO DEN DUE TO FLAPS FAILURE ANNUNCIATION WHEN FLAPS SELECTED TO 5 '. SLATS EXTENDED, BUT FLAPS DID NOT FULLY EXTEND TO 5 '. RAN ABNORMAL CHECKLIST, FLAPS FAILED TO RESET. EMERGENCY WAS DECLARED IN ROUTE TO DEN AND AIRCRAFT LANSDR GTIA2023031337036None · noneFUME EVENT ON DESCENT, DIRTY SOCK SMELL -PERFOMED TSM 05-50-00, FOUND PACK 2 HAS EMITTING ODOR. PACK 1 HAS NO ODOR AT THIS TIMESDR YENA2023031300228Unknown · unknownFLT#942, LAX-SJC.' HIT A POCKET OF SEVERE TURBULENCE AT 12000FT; UPLOADED FOQA FOR SAFETY INVESTIGATION ANALYSIS RESULTS IAW AMM TASK 05-51-17-941-054-A, FOUND WITHIN LIMITS. NO FURTHER INSPECTION IS REQUIRED FOR THE SEVERE TURBULENCE PIREP. A/C OK FOR SERVICESDR JJBA20230315016Unknown · unknownLIGHTNING STRIKE DURING DECENT THROUGH 8,000. PERFORMED LIGHTNING STRIKE INSPECTION. ALL 5 DISPLAY UNITS MAGNETIZED DUE TO LIGHTNING STRIKE. REMOVED AND REPLACED ALL 5 DISPLAY UNITS. NO FURTHER DEFECTS. FO WINDSHIELD SHOWS SIGNS OF STRIKE. REMOVED AND REPLACESDR YENA2023031300230Unknown · unknownFLT#1759, JFK-KIN. 'DESCENDING THROUGH 4000 FEET FA REPORTED ODOR THROUGHOUT CABIN, PERSISTED TO ENGINE SHUT DOWN; ACCOMPLISHED INFORMATION NOTICE 20-17-T015J. NO ODOR COMING FROM PK OR ENGINE IDENTIFIES THE ODOR AS VOMIT. A/C OK FOR SERVICE. MCC CHRIS.'SDR UIEA2023031000236None · noneSUSPECTED HARD LANDING(<P>COMPLETED PHASE 1 INSPECTION IAW B-767 AMM 05-51-01 PER MCC, NO DEFECTS NOTED AT THIS TIME.</P>)SDR NACA202307201003Unknown · unknownLH WING.- WING SKIN UPPER SURFACE CORRODED AT FORWARD SPAR WS 235.00. EFFECTED OEM FASTENER REMOVED AND NEW FASTENER INSTALLED IAW SRM 57-20-01 ALLOWABLE DAMAGE 4 TABLE II AND IAW BOEING REPAIR MESSAGE: NAC- NAC -23-0022-08B , DATED 13, APRIL 2023 RESTORED AERSDR NACA202307201002Unknown · unknownRH WING.- WING SKIN UPPER SURFACE CORRODED AT FORWARD SPAR WS 495.00. CORROSION DAMAGE REMOVED AT WING STATION 494.00 AT REAR SPAR R/H IAW BOEING REPAIR MESSAGE NAC-NAC 23-0022-08B, DATED 13, APRIL 2023, NOMINAL MATERIAL THICKNESS WAS 0.145 MAXIMUM MATERIAL RESDR NACA2023072010001Unknown · unknownRH WING.- WING SKIN UPPER SURFACE CORRODED AT REAR SPAR WS 495.00. CORROSION DAMAGE REMOVED FROM UPPER SURFACE WING STATION 495.00 AT FRONT SPAR R/H IAW BOEING REPAIR MESSAGE : NAC- NAC 23-0022-08B, DATED 13, APRIL 2023, NOMINAL MATERIAL THICKNESS WAS 0.150 MASDR HNAA2023032400090Unknown · unknownCROSSBEAM AT FR 20 IS CORRODED (LEVEL 2). REPAIRED IAW SRM51-40-02SDR JJBA20230313017Unknown · unknownCORROSION ON FLOOR BRACKET AT FS 21 AT SERVICE DOOR. REMOVED AND REPLACED FLOOR BRACKET AT FS 21 AT SERVICE DOOR.SDR CALA2023031000700Intercostal · corroded(B737-53-3-0711) BARE METAL ON AFT EDGE OF FLIGHT DECK AFT FLOOR ACCESS PANEL CUTOUT REMOVED CORROSION DAMAGE ON AFAT EDGE OF FLIGHT DECK AFT FLOOR A CCESS PANEL IAW B737-800 EC/RA #5321-01566. DATA WAS TRANSCRIBED FROM PAPER DOC AERSALE WO 3826 NR 24702 WORK SDR CALA2023030900670Oven · noneSMELL PLASTIC MELTING OUT OF FL180.TO BELOW 10 ON FLIHT DECK.DOO R2L/45 P310, P210, AND P110 PANEL IN THE E & E COMPARTMENT AND A VISUAL AREAS AND WENT INSIDE THE E&E COMPARTMENT AND STILL NO EVIDENCE INSPECTION OF THE AIRCRAFT BATTERY & CHARGER AND NO EVIDENCSDR IPXA2023040692663Floor Panel · damagedINSPECTION TYPE:CK1C*MAJOR REPAIR* PANEL 132FE DAMAGEDFABRICATED NEW PANEL PER SREO A300-5320-16407 REV. ESDR IPXA2023040692657Floor Panel · damagedINSPECTION TYPE:CK1C*MAJOR REPAIR* PANEL 132SG DAMAGEDFABRICATED NEW PANEL PER SREO A300-5320-16407 REV. ESDR IPXA2023040692656Floor Panel · damagedINSPECTION TYPE:CK1C*MAJOR REPAIR* PANEL 131FE DAMAGEDFABRICATED NEW PANEL PER SREO A300-5320-16407 REV. ESDR IPXA2023040692655Floor Panel · damagedINSPECTION TYPE:CK1C*MAJOR REPAIR* PANEL 131SG DAMAGEDFABRICATED NEW PANEL PER SREO A300-5320-16407 REV. E.SDR GTIA2023031037025Unknown · unknownFUME EVENT DESCENDING OUT OF FL 330. NOT IN CLOUDS BUT EVENRUALLY DID DECENT THROUGH CLOUDS-PREFORMED TSM 05-50-00-810-831-A. FOUND SORCE OF ODOR COMING FORM ENG BLEED 1. REF LOG PAGE 3019660-2SDR CALA2023030900655Frame · corrodedA SMALL FRAME IS EXFOLIATED CORRODED ON ITS AFT SIDE, AT STA 1445 ABOVE STR 27R. AS VIEWED THROUGH THE E-6 RACK DOOR IN THE ALC. 100% MATERIAL LOSS, REMOVED AND REPLACED SMALL FRAME AT STA 1445 S27R IAW B757 SRM 51-40-02 PARA 4, PARA 7, BOEING PROPRIETARY DOC#SDR DALA2024031503360None · noneSHIP 5802 ER/A 597639-14 / SECTION III. CORRECTIVE ACTION: DAMAGE AREA WAS REPAIRED PER PRI 597639-14 REV 1 AND ER/A 597639-14. (2659740)SDR 2023FA0000116Alternator · inoperativeLEFT HAND ALTERNATOR LIGHT CAME ON, TAXING ON RUNWAY FOR TAKE OFF.SDR VNAA202302040028Vane · damagedELONGATED HOLE ON ACCESS PANEL 684ETSDR HNAA2023032400087Unknown · unknownSERVICE DOOR CUTOUT CORRODED (LEVEL 2) AT AFT LOWER DOOR STOP. REPAIRED IAW SRM51-40-02SDR GTIA2023030937018None · noneON DESCENT HAD DIRTY SOCK SMELL FUME EVENT. ISOLATED PACK 1 AND SMELL WENT AWAY. AT THE GATE SMELL CAME BACK WITH APU BLEED.-CONFIRMED PACK 1 SOURCE OF ODOR IAW TSM 05-50-00-810-831-A. SEE LOGPAGE 3040573-2 FOR CORRECTIVE ACTION.SDR SCNA20230307093None · noneDEFECT 744450: MULTIPLE RAMP STAFF ADVISED THE CREW THEY SAW SPARKS COMING FROM THE #2 ENGINE UPON PARKING WHEN UNDER POWER MC NOTIFIED WB 10281. RESOLUTION: PERFORMED GVI INSPECTION OF ENGINE #2 IAW AMM 05-41-04-210-806.SDR FDEA202303060379Rib · crackedLH WING LEADING EDGE, MAINT TRACK RIB BETWEEN OSS 491-499, FRONT AND LOWER RADII WITH CRACK OF 0.480" LH WING LEADING EDGE MAIN TRACK RIB BETWEEN OSS 491-499 FRONT AND LOWER RADI WAS REPAIRED I.A.W. E.A. #H-5740-T0373203 RELASE DATE MAR 05, 2023SDR CALA2023030600636Vortex Gen · missingPDA 3 ONE LH AFT BODY VORTEX GENERATOR MISSING. REMOVED BROKEN V.G. AND INSTALLED A NEW V.G. REF. SRM 51-40-02 REMOVED CDL INOP SPEAKER.SDR IPXA2023040692671Floor Panel · damagedINSPECTION TYPE:CK1C*MAJOR REPAIR* PANEL 151LG DAMAGEDFABRICATED NEW PANEL PER SREO A300-5320-16407 REV. E.SDR IPXA2023040692669Floor Panel · damagedINSPECTION TYPE:CK1C*MAJOR REPAIR* PANEL 152MG DAMAGEDFABRICATED NEW PANEL PER SREO A300-5320-16407 REV. ESDR IPXA2023040692668Floor Panel · damagedINSPECTION TYPE:CK1C*MAJOR REPAIR* PANEL 15VF DAMAGEDFABRICATED NEW PANEL PER SREO A300-5320-16407 REV. ESDR IPXA2023040692667Floor Panel · damagedINSPECTION TYPE:CK1C*MAJOR REPAIR* PANEL 151KG DAMAGEDFABRICATED NEW PANELPER SREO A300-5320-16407 REV. ESDR IPXA2023040692666Floor Panel · damagedINSPECTION TYPE:CK1C*MAJOR REPAIR* PANEL 152LG DAMAGEDFABRICATED NEW PANEL PER SREO A300-5320-16407 REV. ESDR 2023FA0000113None · noneL/H WING, SPOILER #6 - LARGE EDGE DELAMINATION ON OUTBD FWD CORNER.SDR YENA2023030600205None · noneFLT#771, BOS-CUN. 'DIRTY SOCK SMELL ON DESCENT REPORTED BY IN FLIGHT AFTER FLIGHT; PERFORMED PACK BURN WITH ENG #2 IAW INFO NOTICE 2017-T015J. NO MORE ODOR WAS DETECTED. CLEAR.'SDR GTIA2023030637012None · noneAFT FLIGHT ATTENDANTS REPORT POSSIBLE FUME EVENT, WET MOLDY SOCK SMELL-INSPECTED APU & BLEED DUCTS,RAN BOTH ENGS PACK BURNED OUT ISOLATED PACKS 1+2 NO ODOR NOTED, AC OK FOR SVC IAW TSM 05-50-00SDR GTIA2023030637010None · noneSTRONG ELECTRICAL SMOKE SMELL COMING FROM ROE 16.-PERFORMED IDENTIFICATION FOR CAUSE OF CABIN ELECTRIC SMELL PER TSM 05-50-00-810-831-A TYPE 9.REMOVED ALL CEILING & SIDEWALL PANELS AROUND ROW 16 & PERFORMED INSPECTION. NO ELECTRICAL SMELL AT THIS TIME. RE-INSSDR CALA2023030300620None · noneSERVICE ENGINES & APU OIL PER AMM. ENTER ZERO(0) IF NONE ADDED. LOG CREATED TO RECORD ENGINE OIL SERVICE OIL SERVICE ACCOMPLISHED AT EWR FOR FLT 0187 ON 22 FEB 05:26:05 ENGINE 1: 05 ADDED BY U178499 ENGINE 2: 05 ADDED BY U178499 ENGINE 3: ENGINE 4: APU: 00SDR CALA2023030300617Frame · corrodedRH AFT EMERGENCY EXIT DOOR LOWER FRAME CORROSION PER HAECO LCQ N ON ROUTINE 9292719/40719 GENERATED BY V798788 REMOVED AND REPLACED DOOR FRAME AND CURVE EDGE ON R/H EMERGENCY EXIT DOOR I/A/W A320 SRM 51-72-11-911-001 PER MECH V075620SDR DALA2023052204088Unknown · unknown(LOG 2650925) DURING ACCOMPLISHMENT OF AIRCRAFT 3953, IT WAS FOUND THAT THE CURRENT DESIGN OF THE RETAINER PLATE DOES NOT ALLOW THE QUARTER TURN RETAINERS ON THE LEFT-HAND SIDE OF COMPARTMENT 414 IN GALLEY G4C TO TURN CORRECTLY AND THAT THERE IS AN OVERHANG OFSDR CALA2023030100591Panel · corrodedCORROSION AT STA 294 TO 312 RBL 22 ON PANEL BREAK (REF: AAR NR 99960033) EVALUATED DAMAGE CORROSION ORIGINAL THICK: 0.080" MATERIAL REM: (REF: WORK ACCOMPLISHED BY V940184 AND AAR QC A-82 V931568) 0.065",MATERIAL LOSS: 0.015", FOUND TO BE OUT OF LIMITS IAW B73SDR FDEA202302280349None · noneSTRONG ORDER OF PAINT THINNER AT LEVEL OFF. COMPLIED WITH FUMES CHECKLIST IN QRH. USED 100% OXYGEN FOR REMAINDER OF FLIGHT. EMERGENCY DECLARED. CONFIRMED SPILL IN D.G. CONTAINER. (ENTERED FOR FLIGHT CREW MEMBER 5148579 OVER PHONE. GMM: 03-4-200 METSDR VNAA202302040027Access Panel · corrodedCORROSION ON ACCESS PANEL 542BZSDR GTIA2023022737000None · nonePACK 1 MILD ODOR, MOSTLY SMELL ON DESENT AT 4000 FT. AIR Q REPORT.-PERFORMED INSPECTION OF COS. FOUND TO BE TYPE 10 MISCELLANEOUS. FOUND VOMIT AT SR 22L TO 24 L. REF AMM TSM 05-50-00-810-831. CLEAN CREW NOTIFIED.SDR YENA2023027100196None · noneFLT#421, BOS-PBI.' ODOR EVENT DURING INITIAL DESCENT UNTIL GEAR DOWN ON FINAL; ACCOMPLISHED INFO NOTICE 2017-T015J FOUND TO BE A TRANSIENT ENVIRONMENTAL SYSTEM ODOR. SECTION B2 DECONTAMINATION LEVEL 1A PER TSM 05-50-00. A/C OK FOR SERVICE.'SDR SCNA20230321110Shield · corrodedDEFECT: AFT CARGO SHIELD AT STA 847-867 RBL25 WL162 HAS CORROSION. RESOLUTION: REMOVED DAMAGED AND REPLACED AFT CARGO SHIELD AT STA 847 TO 867 RBL 25 WL162 IAW B737 SRM 51-40-05-0G-0, 51-40-02-0G-0, BOEING DWG 146A8127-8.
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