JASC 5100
Service difficulty reports · 4,230
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 MASA2025021900013None · noneFWD POB USED AT 600 PSI - SERVICED.SDR MASA2025021900012None · noneEEMK USED - PLACED ON MEL FOR 1 FCSDR DALA2025022101371Repair · noneSHIP 5814 AD, A.A , IN REF TO AMDS 5311-01218-01A STEP 4 EXISTING REPAIR WAS FOUND IN THE INSPECTION AREA AT STA 1640 BTW S-9L TO S-17L ER/A 590442-14AD REV ORIGINAL CORRECTIVE ACTION: SUMMARY OF NRC 00063:IN ACORDING WITH DELTA ENGINEERING NO FURTHER ACTIONS SDR HNAA2025021700087None · noneSEVERE TURBULENCE AND WINDSHEAR ON APPROACH TO PGV AND IN TO CLT FACT 16FEB25 14:20 CLT PERFORMED SEVERE TURB INSP IAW AMM 05-50-27 REAPPLIED MISSING EROSION TAPE ON R/H AND L/H MLG A/C OK FOR SERVICE AT THIS TIMESDR HNAA2025021700085Gpu · smokeWHILE AT GATE GPU CONNECTED SAW GPU SMOKING. DESELECTED GPU AND AFTER A/C SHUT DOWN AND POWERED UP. FOUND SOMEBODY TO DISCONNECT GPU AND NOTICED STRONG SMOKE SMELL IN A/C. PERFORMED EXTERNAL POWER TEST IAW 24-40-00-700-801-A OPS CHECK'D OK. VISUALLY INSP GROUSDR DALA2025021901256None · none(LOG 0812954) A.A IN REF AMDS 5732-01015-02A-01: OBTAIN VA FROM FLEET ENGINEERING. WINGLET MOD SUMMARY OF NRC:00354 VA 90996 REV C WAS PERFORMED IN CONJUNCTION WITH AA 5732-01015-02A-01.SDR DALA2025021301118None · none(LOG 0808942) WHILE IN QRO FOR MTC, AN INTERNAL DOUBLER IS LOCATED IN THE MFEC AREA (SEE WORK CARD 5330-2575) OF THE ICA FOR THE GOGO WIFI INSTALLATION AREA (AA 2330-01344) AND THE MFEC CANNOT BE ACCOMPLISHED. THE EDGE OF THE DOUBLER EXTENDS UP ONTO THE CHEM-MSDR AALA202504111008Fitting · noneAIRCRAFT IN BASE MAINTENANCE: DUE TO THE MAJOR REPAIR BEING ACCOMPLISHED ON THE FLIGHT DECK CENTER WINDSHIELD FRAMING THE RIGHT HAND CONTINUITY FITTING AT FR 2 AND Y0 MUST BE REPLACED PER INSTRUCTIONS OUTLINED IN EO 5319Y017-002. REPLACED CONTINUITY FITTING PESDR REXA2025021700199Fitting · noneWHILE PERFORMING SB 670BA-53-044 REVISION G, DATED JUL 05/2022 FOUND LH FITTING PN CC670-33563-001SB AND RH FITTING PN CC670-33562-001SB AT STR12A CANNOT BE INSTALLED IN ACCORDANCE WITH SERVICE BULLETIN INSTRUCTIONS DUE TO EXISTING AIRCRAFT RIVET PATTERN. COSDR DALA2025021401158None · noneSHIP 6707 AMOC MONITOR INSPECTION LOG REF ERA 511579-14AD REV A FUSELAGE / SKIN / STA 600 TO 640 / S-14L TO S-19L / SKIN SPLICE. CORRECTIVE ACTION: REF ERA 511579-14AD REV A. (0808279)SDR DALA2025021201090None · noneIN REFERENCE NRC 00924: LEVEL AND SHORE AIRCRAFT IN ACORDANCE WITH AMM 07-11-00 AS WELL AS PER FIGURE 4 OF BOEING SERVICE SKETCH 3268E PER PRI 621176-14 REV 0 STEP 1 A) AND PERFORM DAILY CHECK UNTIL REMOVED. SUMMARY NRC 00981: SHORINGS WERE INSTALLED AND VERIFSDR SCNA20250212049SNone · noneSUPPLEMENT: DEFECT 717580: - HOURS CYCLES UPDATED/INCLUDED.SDR IPXA2025020955694None · none*SDR FILED OPEN* ADD SDR FOR EO-82173-JIC001 (FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R)SDR HNAA2025021000081None · noneBIRD STRIKE ON LEFT SIDE AIRCRAFT ON TAKE OFF ROLL FACT 09FEB25 04:13 ROA CLEANED AND INSPECTED IAW AMM 05-50-08 NO DEFECTS NOTEDSDR IPXA2025020716359None · noneADD SDR FOR EO-82173-JIC001 (FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF STA 1725.5 BETWEEN S-36L AND S-36R) [T3F18E0013XJ0] ACCOMPLISHED SDR. REVIEWED.SDR 2025FA0000088Nut · failedTORQUE SENSOR ASSEMBLY [PN: 3101726-3, SN: P-8423, TSO: 3,059.5] HEXAGON PLAIN NUT [PN: 867349-1] BACKED OFF DURING FLIGHT.SDR FDEA202502050225Structure · noneEXISTING REPAIR ON RH FWD DOOR LOWER FWD CORNER SKIN FR14-FR14A REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON RH FWD DOOR LOWER FWD CORNER SKIN FR14-FR14A WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM52-11-00-201-2 FIG.206. ONE MISSSDR HALA20250205052None · noneATB - BIRDSTRIKE @ 1500' AGL ON DEPARTURE RWY 16L. ACCOMPLISHED BIRDSTRIKE INSPECTION IAW AMM 05-51-14-200-803-A, NO DAMAGE FOUND, CLEANED FUSELAGE OF ORGANIC MATTER, A/C OK FOR CONTINUED SERVICESDR IPXA2025022264222None · noneTIME LIMITED REPAIR N251UP TAIL AFT BODY SECTION CORROSION BETWEEN STA 2119.685 AND 2163.681 AND BETWEEN L32R -L35R. ACCOMPLISHED REPAIR PER EO-92893-REQ1 AND VT-SAA EA 011-5330-01-B0375, REV. IR. REVIEWEDSDR IPXA2025020563373Unknown · unknownREMOVE L3 DOOR FOR STR. MAINT. ATA 52-10 OK TO WORKSDR IPXA2025020563391Unknown · unknownREMOVE R3 DOOR FOR STR. MAINT. OK TO WORKSDR AALA202503185329Fork · noneAIRCRAFT IN BASE MAINTENANCE: DUE TO THE MAJOR REPAIR BEING ACCOMPLISHED ON THE AFT AVIONIC COMPARTMENT RACK 80VU LEFT HAND LATERAL FOREND FITTING PER EA 361764, THE RIGHT HAND LATERAL FORKEND FITTING BETWEEN FR 23 AND FR24 AT S32R MUST BE REPLACED AS OUTLINEDSDR DALA2025020400814None · none-AD- COMPLY WITH ERA 623716-14AD REV ORIGINAL. SUMMARY NRC 002-0001:0514-2001/008 00009: COMPLIED WITH ER/A 623716-14AD REV 0, PRI REV 0, 1, AND 2. ENSURED PRI AND FINAL ERA MATCH. (LP #0794140)SDR FDEA202502020168None · noneEXISTING REPAIR ON LH WING I/B FLAP UPPER SKIN RIB1C - RIB3 S2.1 - S2.2 REQUIRES EVALUATION FOR CONFORMITY THE EXISITING REPAIR ON LH WING I/B FLAP UPPER SKIN RIB1C-RIB3 S2.1-S2.2 WAS EVALUATED AND FOUND IN CONFORMITY WITH EA 6-5752-114869. TITLE: STRUCTURSDR MASA2025020100011None · noneMEDICAL EMERGENCY CAUSED AN OVERWEIGHT LANDING.SDR MASA2025020150009None · noneOVERWEIGHT LANDINGSDR DALA2025020600922None · none-AD- EXISTING REPAIR FOUND. CONTACT LIAISON ENGINEERING FOR REPAIR PROCEDURE PRIOR TO FURTHER FLIGHT REF FC5720-01103. AMOC 24-160 TO AD 2024-21-01 PARA(G) W/C 5720-01103-01B AND ERA 621136-14AD REV ORIGINAL ALREADY APPROVED AND PROVIDE AMOC TO SUBJECT AD FOR SDR CALA2025020202165None · noneAFT FORWD LAV D NEEDS CLEANING. BODELY FLUIDS ON FLOOR. CLEANER REMOVED ALL SIGNS OF BODIY FLUID AND SMELLS. AIRCRAFT OK TO CONTINUE WITH FLIGHTSDR AALA202504023755Fitting · noneAIRCRAFT IN BASE MAINTENANCE: DUE TO THE MAJOR REPAIR BEING ACCOMPLISHED ON THE FLIGHT DECK CENTER WINDSHIELD FRAMING THE LEFT HAND CONTINUITY FITTING BETWEEN FR 1 AND FR 3 AT Y0 MUST BE REPLACED PER INSTRUCTIONS OUTLINED IN EO 5319Y017-002. REPLACED LEFT HANDSDR CALA2025020302173Slide · no discrepancyAFTER INSTALLATION OF L1 EMERGENCY DOOR SLIDE L1 EMERGENCY DOOR SLIDE WAS DEPLOYED WHILE PERFORMING OPERATIONAL CHECK. REMOVED SLIDE PACK S/N A9661RP IAW AMM 25-62-44-000-002-A, AND REINSTALLED SLIDE PACK S/N M13196 IAW AMM 25-62-44-400-006-A. ALL OPS CHECKS GSDR CALA2025020202161None · noneCREW REPORTS SMELL OF SMOKE FROM CELL PHONE AT SEAT 6D. PHONE SMOKE CONTAINED VIA HALLON AND WATER SUPPRESSION METHODS. PHONE CONTAINED IN THERMAL CONTAINMENT BAG. ON ARRIVAL PHONE, PHONE AND THERMAL CONTAINMENT BAG CONFISCATED BY LOCAL FIRE AUTHORITY. SEE PICSDR DALA2025020200769Support Fitting · noneSHIP 3276 DISC: ERA 623985-14AD REV ORIG FOR 80VU AVIONICS RACK SUPPORT FITTINGS REQUIRES FOLLOW ON ACTIONS. C/A: ACCOMPLISH SECTION II REPEAT INSPECTIONS EVERY 500 FC UNTIL SECT ION III PERMANENT REPAIR. PERMANENT REPAIR SECTION III REQUIRED WITHIN 4500 FC. ASDR BAGA2025013100009None · noneAMBER FUEL LEAK SUSPECTED" MESSAGE AFTER TAKE OFF IN CLIMB. RETURNED TO THE DEPARTURE AIRPORT. PERFORMED INSPECTION OF AIRCRAFT WITH NO EVIDENCE OF FUEL LEAK, VERIFIED FUEL LOAD PER FIM. NO FAULTS NOTED.SDR SCNA20250131041None · noneDEFECT 796649: FA'S REPORTED INJURIES DUE TO HARD LANDING IN LAS. HARD LANDING INSP NEEDS TO BE COMPLETED. RESOLUTION: PERFORMED HARD LANDING INSPECTION REF AMM 5-51-37 NO DEFECTS NOTED AT THIS TIMESDR DALA2025013000723None · noneSHIP 3142 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR. CORRECTIVE ACTION: PERFORMED REPAIR PER ER/A 570263-14. (1224604)SDR CALA2025013102146Carpet · saturatedFLIGHT ATT REPORT WATER LEAK COMING FROM FLOOR BETWEEN AFT LAVS FLIGHT CREW REPORTED WATER COMING FROM CARPET BETWEEN AFT LAVS. NO WATER PRESENT IN LAVS OR GALLEY FLOOR. CREW SHUT OFF WATER IN LAVS. RE ACTIVATED WATER IN LAV A AND RAN SINKS AND FLUSHED TOILETSSDR DALA2025012900693None · noneSHIP 6708 ER/A 518639-14 REV C FUSELAGE / SKIN / STA 500-520, S-27L ? S-28R / ATG4 WIFI ANTENNA INSTALLATION / PROXIMITY TO EXISTING REPAIR DOUBLER , SECTION III: ANTENNA REMOVAL ALTERATION REQUIRED. CORRECTIVE ACTION: REF ERA 518639-14. (0782960)SDR MASA2025012500005None · noneRETURN TO FIELD DUE TO MEDICAL EMERGENCY DECLARED OVERWEIGHT LANDING. INSPECTION PERFORMED, NO DEFECTS FOUND.SDR J6B2025F00002None · nonePAX DOOR, LOWER AFT CORNER BRACKET (ON THE AIRFRAME SIDE) AT FS 349.00 HAS BEEN REMOVED TO FOM (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESSSDR CALA2025012702055Unknown · unknownFA JACKET STUCK IN 2L ON TAKEOFF. RETURNED OVERWEIGHT TO REMOVE REMOVED STUCK FLIGHT ATTENDANT JACKET FROM DOOR. NO DEFECTS FOUND. CLOSED DOOR. A/C OK TO CONTINUE.SDR QXEA2025012400012Unknown · unknownFLIGHT 2214. ON POSTFLIGHT WALK AROUND APU OFF, GPU CONNECTED RECIEVED STATIC SHOCKS WHEN RUNNING HAND ON AIRCRAFT SKIN IN PORT ADP SMOOTH AREA. REMOVED FROM SERVICE. C/W MCN E240028-01 ISSUE 2 DISCONNECTED GPU AC NO LONGER SHOCKING PERSONAL. RETURNED TO SERVISDR REXA2025020500130None · noneWHILE PERFORMING SB 670BA-53-044 REVISION G DATED JUL 05/2022 FOUND FITTINGS PN CC670-33563-001SB AND CC670-33562-001SB AT STR12A LH AND RH SIDES CANNOT BE INSTALLED PER SERVICE BULLETIN INSTRUCTIONS DUE TO EXISTING AIRCRAFT FASTENER LOCATIONS REPAIRED IAW MHSDR IPXA2025012936292None · noneRH OUTBOARD ELEVATOR FRONT SPAR AND RIB REINFORCEMENT. ACCOMPLISHED EO-85445-JIC2. ACCOMPLISHED SDRSDR IPXA2025012335979None · noneLH OUTBOARD ELEVATOR FRONT SPAR AND RIB REINFORCEMENT. ACCOMPLISHED EO-85445-JIC. ACCOMPLISHED SDERSDR CALA2025012402032None · noneOIL LEAK SPOTTED BOTTOM INSIDE LEFT ENG COWL DURING PREFLIGHT SUBSTANCE HAD SMELL AND CONSISTANCY OF TYPE I DEICING FLUID. INSPECTED FAN INLET SECTION AND DID NO OBSERVE ANY LEAKS AT THIS TIME.SDR IPXA2025012336292None · noneRH OUTBOARD ELEVATOR FRONT SPAR AND RIB REINFORCEMENTSDR UIEA2025011600077Structure · noneCONTAMINATED EWIS WITH CIC OF NOSE LANDING GEAR WHEEL WELL.<BR>(<P>NOSE LANDING GEAR WHEEL WELL EWIS WAS CLEANED IAW SWPM 20-10-04 REV 87. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025011700082Structure · noneMISSING CIC ON SEVERAL AREAS OF NOSE LANDING GEAR WHEEL WELL.(<P>MISSING CIC ON SEVERAL AREAS OF NOSE LANDING GEAR WHEEL WELL. DAMAGED CIC WAS REMOVED AND AREA CLEANED FOR APPLICATION, CIC IS APPLIED CORRECTLY. AMM 51-24-09-377-008 REV 143 AND AMM 51-24-09-917SDR DXTA2025012702084Skin · ground damageTHE RH OUTBOARD LEADING EDGE CAME IN CONTACT WITH A PARKED MANLIFT.SDR WX0A2025012332277Cover · damaged(AIRCRAFT NOT GROUNDED) EPSU COVER PANEL LH SIDE BETWEEN ROW 12 AND 14 DAMAGED. / INSTALLED NEW STUDS TO SECURE EPSU COVER PANEL AT LH SIDE ROW 12-14 IAW AMM 25-23-44. EPSU COVER NOW SECURE NO FURTHER DEFECTS NOTED.
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