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 DALA2025032702247Unknown · unknownAD/EM-EO TASK - RH WING W/C 5720-01102-06B STEP 29. TO GENERATE A STANDALONE "SDR" LOG PAGE AND ENSURE "SDR REPORTABLE" CHECKBOX IS MARKED ASSOCIATED WITH THE REPAIR. RH WING SEALANT APPLIED AS PER W/C 5720-01102-06B STEP 13. FOUND SATISFACTORY AND W/C STEP 29SDR FDEA202503250490Seat Track · noneMAIN DECK CARGO COMPARTMENT - EXISTING SEAT TRACK REPAIR AT Y2462 BETWEEN FR18 AND FR27 REQUIRES EVALUATION TO DETERMINE IF MAJOR OR MINOR AND IF REPAIR CONFORMS TO FAA APPROVED DATA. THE EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT SEAT TRACK AT Y2462 BSDR FDEA202503250485Repair · noneRIGHT HAND WING - EXISTING REPAIR DOUBLER AT FIXED LEADING EDGE CAVITY XOS 789.645 REQUIRES EVALUATION TO DETERMINE IF MAJOR OR MINOR AND IF THE REPAIR CONFORMS TO FAA APPROVED DATA. EXISTING DOUBLER AT FIXED LEADING EDGE CAVITY XOS 789.645 EVALUATED AND FSDR DXTA2025032702805None · noneDAMAGE REPORTED BY EJM VENDOR TO HAVE DAMAGE CAUSED BY N854QS STRIKING AIRCRAFT DURING HIGH WINDS. NEEDS EVALUATED COMPLIED WITH UNSCHEDULED AIRCRAFT IN STRONQ WIND OR WINDQUSTS €¢ DETAILED INSPECTION IAW CL350S AMM 05-51-43-210-801. NO DAMAQE FOUND EXCEPT FOSDR DXTA2025032602804Radome · ground damageAIRCRAFT JUMPED CHOCKS AND MADE CONTACT WITH OTHER AIRCRAFT EVALUATED DAMAQE AND SENT PICTURES TO MCC. FOUND NOSE RADOME TO BE DAMAQED OUT OF LIMITS. REPLACED NOSE RADOME IAW CE 700 AMM 53-10-5. PERFORMED GVI OF AIRFRAME, PAYINQ PARTICULAR ATTENTION TO ALL LEASDR CALA2025032503168None · noneDEACTIVATION OF SLIDE PERFORMED INSTALLED SAFETY SLIDE PIN AT POSITION (L3) DOOR IN THE SLIDE INFLATION BOTTLE REGULATOR ON SLIDE PACK ACCOMPLISHED SAFETY SLIDE PIN AT POSITION (L3) DOOR IN THE SLIDE INFLATION BOTTLE REGULATOR ON SLIDE PACK REMOVED & STOWED AWSDR CALA2025032503162None · no discrepancyDISARMED LEFT AND RIGHT OFF-WING ESCAPE SYSTEM PER AMM 25-65-00-042-001 FOR O/W SLIDE INSPECTION. BATTERY PACK M961 AND M962 DISCONNECTED IN CABIN AND LEFT AND RIGHT SPOILER OVERRIDE ACTUATORS DISCONNECTED AND CAPPED. REARMED LEFT AND RIGHT OFF WING ESCAPE SYSSDR CALA2025032403118None · noneINSTALLED THE LOCK PIN ASSEMBLY IN THE REGULATOR VALVE ASSEMBLY OF R/H OFFWING EMERGENCY DOOR SLIDE INFLATION RESERVIOR IAW AMM 25-62-00. REMOVED AND STOWED THE LOCK PIN IN THE POUCH R/H OFF WING INFLATION RESERVIOR IAW AMM 25-62-00. C/W RII FOR THE REACTIVATISDR CALA2025032103085None · none#3 LEFT HAND WINDOW FRAME POST E-F REPAIR PER ECRA 5310-08540. PER ECRA 5310?08540 PART 1 STEP 2 AFTER THE ACCUMULATION OF 49,900 TOTAL AIRCRAFT FLIGHT CYCLES, BUT BEFORE 50,000 TOTAL AIRCRAFT FLIGHT CYCLES, PERFORM AN INSPECTION OF THE LH HAND WINDOW FRAME POSDR DALA2025032402181Frame · none(LOG 0870016) THIS WORK CARD INSTALLS A NEW SHIM BETWEEN THE LEFT SIDE OF STA 727 FRAME INNER CHORD AND S-18A WEB. AD 2023-06-15 REQUIRES INSPECTING THE STA 727 FRAME INNER CHORD AT STRINGERS S-18A FOR EXISTING REPAIRS, INSPECTING THE AREA FOR CRACKING AND PERSDR DALA2025032402180Frame · none(LOG 0870000) THIS WORK CARD INSTALLS A NEW SHIM BETWEEN THE RIGHT SIDE OF STA 727 FRAME INNER CHORD AND S-18A WEB. AD 2023-06-15 REQUIRES INSPECTING THE STA 727 FRAME INNER CHORD AT STRINGERS S-18A FOR EXISTING REPAIRS, INSPECTING THE AREA FOR CRACKING. AND PSDR FDEA202503210468Repair · not enteredAGING AIRCRAFT - EXISTING REPAIR AT RH WING FIXED LEADING EDGE SKIN FUEL ACCESS PANEL FORWARD INBOARD CORNER STATION XOS 610.844. EXISTING REPAIR DOUBLER REMOVED AND REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-01-2R REPAIR 18 FIGURE 201 SHEET 2. EO # 1-5100SDR GTIA2025032438811None · nonePAX PHONE FIRE ONBOARD USED 1 PBE AND 2 HALONS-REMOVED AND REPLACED PORTABLE FIRE EXTINGUISHERS (7522MM) AND (7520MM) IAW AMM 26-24-41. PERFORMED PAX SEAT INSP. IAW CMM 25-20-94. NO DEFECTS NOTED. REF. LOG PAGES 3615637-1/2 FOR FURTHER CORRECTIVE ACTIONS.SDR DALA2025032102128None · noneNEW SPLICE CHANNEL AT STA 955-STA 977 RBL 85.9 INTERFERS WITH EXISTING REPAIR DOUBLER. THE SPLICE CHANNEL AT STA 955-STA 977 RBL 85.9 INTERFERENCE WITH EXISTING REPAIR DOUBLER WAS REPAIRED PER PRI 624520-14 REV 2. COMPARED AND COMPLIED WITH ER/A 624520-14 REV SDR DXTA2025032102752None · noneA FEW SECONDS AFFER PLACING THE GEAR DOWN, WE HAD A BIRD STRIKE. A GOOD SOLID "THUMP" AND NOISE WAS HEARD. AFTER SHUTTING DOWN ON THE RAMP WE SAW THE BIRD IN THE NOSE GEAR WELL. WE ALSO SAW TRACES OF BLOOD ON THE WING ROOT AND THE LEFT NACELL. ; VERIFIED BISDR CALA2025032003018Slide · not reportedFORWARD DOOR ESCAPE SLIDE PACK ASSEMBLY INSTALL {A3NB-25-3-0020} - RETURN DOOR 1R TO NORMAL AFTER SLIDE REPLACEMENT REF AMM 52-10-00-860-002-A. REACTIVATEDD DOOR 1R. REF AMM 52-10-00-860-002-A. DOOR R 1 ACTIVATED FOR ABOVE AMM , REF GMM 09-25-05.SDR DXTA2025031902735None · no discrepancyON DESCENT THROUGH 17000FT AT 295 KIAS, WE ENCOUNTERED SEVERE TURBULENCE FOR APPROXIMATELY 10SECONDS. WE HAD THE FLAPS AND GEAR UP, CLEAN CONFIGURATION, BUT THE AIRCRAFT ACCELERATED TO 310KIAS FOR THE DURATION OF THE EVENT. CORRECTIVE ACTION; ACCOMPLISHED 560XSDR DALA2025032002124None · none(LOG 6895384) SUSPECTED LIGHTNING STRIKE AT GATE. APU GEN CYCLED ON AND OFF THEN ON FOLLOWED BY ELECTRICAL BURNING SMELL FOR 1 MINUTE IN FLIGHT DECK AND 5 MINUTES IN AFT GALLEY. FOUND APU START GEN SHOWS SIGNS OF ARCING. R/R APU START GEN REF B737 AMM 49-11. OSDR DXTA2025032002706None · noneFUSELAGE STRUCTURE: WHILE ENROUTE AT 21,000 FT WE ENCOUNTERED SEVERE TURBULENCE THAT LASTED FOR APPROX. 15 SECONDS. THERE DOESN'T APPEAR TO BE ANY VISUAL DAMAGE TO THE AIRCRAFT. CORRECTIVE ACTION; COMPLETED UNSCHEDULED: SEVERE TURBULENCE INSPECTION/CHECK. PERSDR DXTA2025031702705Structure · no discrepancyDAMAGE INSPECTION: AIRCRAFT OVER SPEED CROSSING A LINE OF WEATHER AT FLIGHT LEVEL 450 DESCENDING TO FLIGHT LEVEL 430 WE ENCOUNTERED MODERATE TURBULENCE IN CLEAR AIR. AIRPLANE ACCELERATED RAPIDLY AND OVERSPEED APPROXIMATELY 10 KTS AND WE RECEIVED ONE HIGH-SPEEDSDR CALA2025031802917None · noneREMOVED DOOR SLIDE PACK AND PARTIALLY REMOVED DOOR LINER ON DOOR R4, FOR ACCESS IAW AMM 52-13-31/401, PER MAINTENANCE CONTROL REQUEST FOR INSPECTION REFERRENCE LOG PAGE 4176767 WILL REQUIRE INSPECTION FOR INSTALLATION. REINSTALLED DOOR LINER AND SLIDE PACK AT SDR CALA2025031802915None · noneINSTALLED RH SLIDE SAFETY LOCKPIN IAW AMM TASK 25-62-00 REMOVED RH OFF-WING SLIDE SAFETY LOCK PIN IAW AMM TASK 25-62-00. C/W RII FOR THE REACTIVATION OF THE RT OVERWING SLIDE PER THE GMMSDR DXTA2025031702695Structure · no discrepancySEVERE TURBULENCE: ON APPROACH INTO KGPT AT 2000 FEET. ENCOUNTERED MODERATE TO SEVERE TURBULENCE. AIRSPEED WAS INITIALLY AT 220 SLOWED TO 200 WHEN TURBULENCE GOT WORSE. AND CONTINUED SLOWING BACK TO 190 KNOT. GEAR WAS UP AND FLAPS WERE AT 1. AS WE PROCEEDESDR CALA2025031702845None · noneWATER SUPPLY IN LAVATORY POOR QUALITY AFT LH LAV D TESTED WATER QUALITY IN ALL LAVS AND FOUND NO BAD SMELL OR BAD QUALITY WATER. ALL ARE FINE. ASKED 2 FLIGHT ATTENDANTS AND 2 OTHER WORKERS AND THEY ALL AGREED. FIM REF: 38-10 TASK 810.SDR DXTA2025031802687None · no discrepancySEVERE TURBULENCE ENCOUNTERED ON DESCENT INTO THERMAL. AIRSPEED WAS 210KTS AT TIME OF ENCOUNTER. SEVERE DOWNDRAFTS AND UPDRAFTS OCURRED DURING ENCOUNTER CORRECTIVE ACTION; COMPLIED WITH UNSCHEDULED SEVERE AIR TURBULENCE OR SEVERE MANEUVERS INSPECTION IAW MM SDR DXTA2025031702689Structure · no discrepancyFUSELAGE STRUCTURE: AT FLIGHT LEVEL 200 AT APPROXIMATELY 270 KN IN CRUISE, EXPERIENCED SEVERE TURBULENCE LASTING APPROXIMATELY THREE SECONDS. NO OVER SPEED OR EXCESSIVE BANK CORRECTIVE ACTION; PERFORMED SEVERE AIR TURBULENCE OR SEVERE MANEUVERS INSPECTION. ALLSDR CALA2025031402839None · nonePRESS GAUGE ON 2L/2R ARE BORDERLINE INSPECTED DOOR SLIDE PRESSURES. BOTH ARE WITHIN LIMITS REF. AMM 25-66-01.SDR CALA2025031402835Slide · not reportedTRACKING PURPOSES ONLY: R2 DOOR SLIDE PN# AND SN# OFF AND ON. SUPPORT TASK NSA EMX NR 00170 INITIATE REMOVED R2 SLIDE PN 5A3307-701, SN BNG18622 AND INSTALLED PN 5A3307-701 AND BNG13478 DUP.SDR CALA2025031402834Slide · no discrepancyREMOVED RF DOOR SLIDE IN ERROR REINSTALLED RF DOOR SLIDE. REF. AMM 25-66-01-400-803. VERIFIED REINSTALLATION OF R-1 DOOR SLIDE PER AMM 25-66-01-400-803SDR CALA2025031402833Slide · no discrepancyREMOVED L1 DOOR SLIDE REF AMM 25-66-01 AND GMM 02-30-25 INSTALLED DOOR 1L SLIDE AMM REF 25-66-01 GMM 02-30-25 VERIFIED L1 SLIDE INSTALL REF AMM 25-66-01 AND GMM 09-25-05SDR CALA2025031402832None · noneNEED TO VERIFY DOOR 4 LT IS ARMED BEFORE DEPARTURE. VERIFIED DOOR 4 LT IS ARMED AND ENGAGEDSDR CALA2025031402823Not Reported · not reported4L NEEDS TO BE VERIFIED ARMED AGAIN. DOOR WAS OPENED. COMPLIED WITH REQUIREMENTS AS CONTAINED IN LOG PAGE NUMBER 4104624,VERIFIED GIRT BAR ENGAGEMENT PER MEL CARD 25200 MAINTENANCE PROCEDURE STEP A.SDR FDEA202503140404Repair · noneEXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR57.2 - FR59 SEAT TRACK AT Y1456 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR57.2 - FR59 SEAT TRACK AT Y1456 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600F SRSDR FDEA202503140403Repair · noneEXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR74 - FR77 SEAT TRACK AT Y1137.1 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR74 - FR77 SEAT TRACK AT Y1137.1 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600F SRSDR FDEA202503140402Repair · noneEXISTING REPAIR ON MAIN CARGO COMPARTMENT FR65 - FR69 SEAT TRACK AT -Y1456 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR65 - FR69 SEAT TRACK AT - Y1456 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600F SRM 53-1SDR FDEA202503140401Seat Track · noneEXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR26 - FR30 SEAT TRACK AT -Y953 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR26 - FR30 SEAT TRACK AT -Y953 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600F SRM5SDR FDEA202503140400Seat Track · noneEXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR26-FR30 SEAT TRACK AT -Y450 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR26 - FR30 SEAT TRACK AT -Y450 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600F SRM53-SDR FDEA202503140399Repair · noneEXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR71-FR73 SEAT TRACK AT Y0 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR71-FR73 SEAT TRACK AT Y0 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600F SRM53-10-16-201 SDR FDEA202503140394Skin · misrepairedEXISTING REPAIR ON FUSELAGE SKIN FR59-FR60 S38R-S41R REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE SKIN FR59 - FR60 S38R - S41R WAS EVALUATED AND FOUND NOT IN CONFORMITY WITH A300-600F SRM 53-17-12-201-2 FIG 201. REPAIRED IT PER A300-6SDR FDEA202503140393None · noneEXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE LOWER STRINGER DOUBLER STATION XOS 906.5607. EXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE LOWER STRINGER DOUBLER STATION XOS 906.5607 EVALUATED AND FOUND REPAIRED IAW MD-11 SRM 57-40-03-2R REPAIRSDR AALA202503178634Angle · noneAIRCRAFT IN BASE MAINTENANCE: MODIFICATION OF CENTER WING SECTION FRONT SPAR RIGHT HAND UNDER WING LONGERON AT STA 1035, S36L IS DUE PER EO 5722B008. MODIFICATION OF SPAR CHORD ANGLE ACCOMPLISHED PER EO 5722B008. THIS ACCOMPLISHES AD 2023-17-14 AND BOEING SB 7SDR QMLA2025031220034Unknown · leakingWATER POURING IN FROM THE CEILING AND ONTO THE PATIENT GURNEY. WATER WAS VERY CLOSE TO OVERHEAD RADIOS.SDR UIEA2025031200260Skin · no discrepancyLIGHTNING STRIKE AT 17000 FT. SUSPECT STRIKE IMPACT ON CAPTAIN'S SIDE IN THE VICINITY OF THE NOSE.(<P>PERFORMED LIGHTNING STRIKE DAMAGE PHASE INSPECTION IAW B767 AMM 05-51-19. FOUND LIGHTNING IMPACT AND POSSIBLE EXIT POINT AT 2 TO 3 O'CLOCK POSITION BETWEEN STSDR UIEA2025031200261None · noneDEVIATION ON LH UNDERWING LONGERON FOUND DURING PERFORMING SB 777-57A0122 MODIFICATION.(<P>1. ACCOMPLISHED EI NO: T2025A57M-332 REV=1. 2. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)SDR DALA2025031301966None · noneSHIP 6702 AMOC MONITOR INSPECTION LOG REF ERA 508964-14AD REV B. CORRECTIVE ACTION: REF ERA 508694-14AD. (0854369)SDR FDEA202503120371Seat Track · wornEXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT SEAT TRACK BETWEEN STATION 1129 TO STATION 1189 X= 8.5 LEFT HAND SIDE. EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT SEAT TRACK BETWEEN STATION 1129 TO STATION 1189 X = 8.5 LEFT HAND SIDE EVALUATED AND FOUNSDR DALA2025041702982Not Reported · not reportedSHIP 3133 DISC: PERMANENT REPAIR REQUIRED PER ER/A 513509-14AD REVISION A ADDL TIME RLTD MON. C/A: ACCOMPLISH PERMANENT REPAIR PER ER/A 513509-14AD REVISION A SECTION 4 WITHIN 36,640 TOTAL FLIGHT CYCLES. ASSOCIATED ER/A 00-513509 ADDED FOR AC 3133SDR DALA2025031201955None · none(LOG 0852677) ACCOMPLISH AMDS 5311-01251-02B R/H STA 727 FRAME INNER CHORD, 737 REPAIR. COMPLIED WITH AMDS CARD 5311-01251-02B. INSTALL A NEW SHIM R/H SIDE STA 727 FRAME INNER CHORD S-18A.SDR DALA2025031201954None · none(LOG 0852651) ACCOMPLISH AMDS 5311-01251-02A L/H STA 727 FRAME INNER CHORD, 737 REPAIR. COMPLIED WITH AMDS CARD 5311-01251-02A. INSTALL A NEW SHIM L/H SIDE STA 727 FRAME INNER CHORD S-18A.SDR DALA2025031201926None · noneSHIP 6708 DTA MONITOR INSPECTION LOG REF ERA 513904-14 REV A. CORRECTIVE ACTION: REF ERA 513904-14AD. (0852568)
Back to JASC 5100