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 AALA201711309005Memory Device · smokeAIRCRAFT WAS NOT GROUNDED. FIRST OFFICERS YOKE MOUNTED MEMORY DEVICE BEGAN SMOKING AND EMITTED AN ELECTRICAL BURNING ODOR FOR SEVERAL MINUTES THEN STOPPED. REPLACED MEMORY DEVICE PER AMM 33-11-00. NO FURTHER DAMAGE NOTED.SDR DALA2018111906690None · noneSHIP 6704 WHILE IN FOR THE 2KU WIFI MODIFICATION AND DURING THE RADOME INSTALLATION PER GOGO DRAWING REV. C AT FS 620 BETWEEN STR 2R AND 3R, MTC FOUND SIX (6) EXISTING HOLES IN THE LOCATION WHERE THE TEE CLIP IS TO BE MOUNTED TO THE FRAME. ER/A 563725 AUTHORIZSDR DALA2018111906691None · noneSHIP 6701 AT STA 620 HAS 6 EA FASTENERS INTERFERES WITH INTERCOSTAL INSTALLATION. CORRECTIVE ACTION: REPAIRED PER ER/A 563545-14 REV ORIGINAL. (0304775)SDR DALA2018110806543None · none(AIRCRAFT 693, L/P 0301852) WHILE IN ATL FOR THE 2KU WIFI MODIFICATION AND DURING THE RADOME INSTALLATION PER GOGO DRAWING D18470-22207 REV. C (REFERENCE WORKCARD 2330-01349-01D) AT FR600 TO FR620 AND STR2R, MTC FOUND AN EXISTING LIGHTNING STRIKE REPAIR WITHINSDR DALA2018111906692None · noneSHIP 694 WHILE IN FOR THE 2KU WIFI MODIFICATION AND DURING THE RADOME INSTALLATION PER GOGO DRAWING REV. C AT FS 620 BETWEEN STR 2R AND 3R, MTC FOUND SIX (6) EXISTING HOLES IN THE LOCATION WHERE THE TEE CLIP IS TO BE MOUNTED TO THE FRAME. THE DRAWING REQUIRES SDR DALA2018111606663None · noneSHIP 6705 WHILE IN FOR 2KU WIFI MODIFICATION AND DURING THE RADOME INSTALLATION AT FS 620 BETWEEN STR 2R AND 3R, MTC FOUND SIX EXISTING HOLES IN THE LOCATION WHERE THE TEE CLIP IS TO BE MOUNTED TO THE FRAME. THE FOUR EXISTING INBOARD HOLES WILL BE LOCATED ON TSDR DALA2018111406631None · noneSHIP 6711 WHILE IN FOR THE 2KU WIFI MODIFICATION AT FS 620 BETWEEN STR 2R AND 3R, MTC FOUND SIX (6) EXISTING HOLES IN THE LOCATION WHERE THE TEE CLIP IS TO BE MOUNTED TO THE FRAME. THE DRAWING REQUIRES FOUR (4) HOLES TO BE USED FOR ATTACHING THE CLIP TO THE FRSDR DALA2018111406632None · noneSHIP 6714 WHILE IN FOR WIFI MODIFICATION AT FS 620 BETWEEN STR 2R AND 3R, MTC FOUND 6 EXISTING HOLES IN THE LOCATION WHERE THE TEE CLIP IS TO BE MOUNTED TO THE FRAME. FOUR HOLES WILL BE PLUGGED AND TWO NEW HOLES WILL BE DRILLED PER DRAWING. CORRECTIVE ACTION: SDR CALA2017102703797Unknown · vibrationAT FL280, HEARD VIBRATION NOISES LIKE PROPS OUT OF SYNC. THEN HEARD LOUD TONE NOISE FOR 4-5 SECONDS. THEN SMELLED AN ELECTRICAL BURNING ODOR FOR A FEW SECONDS. NO ECAMS OR ANY FAULTS. CREW REPORTED THE VIBRATION AND ODOR DISSIPATED.SDR DALA2018111906693None · noneSHIP 6700 WHILE IN FOR THE 2KU WIFI MODIFICATION AND DURING THE RADOME INSTALLATION PER GOGO DRAWING REV. C AT FS 620 BETWEEN STR 2R AND 3R, MTC REPORTED SIX (6) EXISTING FASTENER HOLES IN THE FRAME WHERE THE INTERCOSTAL T-CLIP IS TO BE INSTALLED. THE ER/A AUTSDR HNAA2017092900340Unknown · noisePILOT REPORTED A LOUD NOISE SIMILAR TO WHATS HEARD DURING GEAR EXTENSION. NO GEAR INDICATION ANOMALIES. NOISE WENT AWAY AFTER FEELING MECHANICAL THUMP BELOW PILOTS FEET. PERFORMED GEAR EXTENSION AND RETRACTION, OPS CHECKED GOOD.SDR ASMF20171009007Unknown · vibrationAIRCRAFT REJECTED TAKE OFF AT 100 KTS, DUE TO HIGH VIBRATION DURING TAKE OFF RUN, MAINTENANCE PERFORMED WHEELS INSPECTION IAW DMC-B787-A-32-50-F1-56A-421A-A, NO DAMAGE FOUND.SDR O2GA2017090750301Unknown · unknownNORMAL FLIGHT, FLAPS SEVEN. SOME TURBULENCE DURING CLIMB OUT, NOTHING MORE THAN LIGHT TURBULENCE . NORMAL FLIGHT AND DESCENT. TOUCHED DOWN VERY LIGHTLY AND IT CAME UP AGAIN, SAT IT DOWN FOR A NORMAL LANDING, THE AIRPLANE DRIFTED A LITTLE RIGHT, CORRECTED, NOSDR QXEA2017081100515Unknown · vibrationAIRCRAFT VIBRATION DURING CLIMB AND CRUISE AT POWER LEVER SETTINGS ABOVE 55% TORQUE. AIRCRAFT REMOVED FROM SERVICE. C/W GVI OF NR 1 AND 2 ENGINE COMPRESSORS AND MOUNTS, NO OBVIOUS DEFECTS NOTED. C/W NR 1 AND 2 HTCS RESERVOIR INDICATIONS, CONFIRMED SHOWING GSDR GTIA2017080902144Unknown · noiseFLT ATTENDENT REPORTED AN AIR NOISE FROM UPPER AREA EMERGENCY EXIT ROW 13 LEFT SIDE. IAW MWI 22-60-95-202 SPEED TAPE APPLIED TO 191 BT PANEL ACFT OK TO CONTINUE SERVICE.SDR CNMA20170803001Unknown · unknownAFTER PUSHBACK AND BOTH ENGINES STARTED, RECIEVED NOTIFICATION FROM FROM FA LOCATED IN AFT CABIN THAT THERE WAS THE ODOR OF SMOKE. DURING THIS TIME A HIGH PITCH NOISE WAS HEARD THROUGHOUT CABIN. ENGINE SHUTDOWN AND NOISE ENDED. RAN BOTH ENGINES AND OPERATEDSDR UIEA2017071701233Unknown · noiseDURING CLIMB OUT AT 8000 MSL, HEARD A LOUD NOISE, SLIGHT YAW ALL PARAMETERS NORMAL, NO MESSAGES, NORMAL OPS. ACCOMPLISHED TEST, FIVE GROUND TEST MAX POWER ASSURANCE SATISFACTORY IAW AMM 71-00-00-735, PIMU BIT CHECKED GOOD IAW 77-35-00.SDR JJBA20170629014Panel · corrodedALL STRESS PANEL COUNTERSINKS HAVE PITTING. REPAIRED IAW RD8-57-2674.SDR JJBA20170629013Panel · damagedCOUNTERSINK HOLE DAMAGED ON FWD LT SIDE OF PANEL 522AT. REPAIRED IAW RD8-57-2674.SDR UIEA2017061901035Unknown · unknownAT APPLICATION OF TOGA, ON THE TAKEOFF ROLL WITH ALL ENGINES SPOOLED UP NORMALLY, THE AIRCRAFT VEERED VIOLENTLY TO THE RIGHT. ABORTED AT 30KTS. ACCOMPLISHED NOSE STEERING CHECK IAW AMM 32-51-00, ALL CHECKED NORMAL. ACCOMPLISHED BODY GEAR STEERING CHECK IAWSDR SWIA201743525Panel · damagedTWO OVERSIZED HOLES IN PANEL 131AL. REPAIRED TWO OVERSIZED HOLES IN PANEL 131AL AT 10 O'CLOCK AND 9 O'CLOCK POSITIONS IAW REO.SDR DALA2017050803626Bushing · corrodedCORROSION ON BUSHINGS AFT AT RT HEATER BLANKET. DAMAGED BUSHINGS WERE REPLACED IAW SRM 51-30-10.SDR AALA201705039035Lens · missingL2 DOOR, CABIN PRESSURE COVER MISSING. REPLACED LENS IAW AMM 52-73-12SDR DALA2017121508638None · noneSHIP 5655 LIGHTNING STRIKE ON FUSELAGE LEFT SIDE AT STA 583 WL 210. CORRECTIVE ACTION: REPAIRED PER B757 AND INSTALLED SOLID RIVET PER B757 SRM. (2989794)SDR DALA2017121508637None · noneSHIP 5655 LIGHTNING STRIKE ON FUSELAGE LEFT SIDE AT STA 567 WL 208. CORRECTIVE ACTION: REPAIRED PER B757 SRM. INSTALLED SOLID RIVET PER B757 SRM. (2989785)SDR DALA2017121508636None · noneSHIP 5655 LIGHTNING STRIKE ON FUSELAGE LEFT SIDE AT STA 520 WL 196. CORRECTIVE ACTION: REPAIRED PER B757 SRM. INSTALLED SOLID RIVET PER 757 SRM (2989781)SDR DALA2017121508635Structure · handler errorSHIP 5655 STRIKE ON FUSELAGE STA 600 FWD OF UPPER BEACON. CORRECTIVE ACTION: REPAIRED PER B757 SRM. REMOVED BLIND FASTENER BETWEEN STA 540 TO STA 560 AND AND STR 1R AND 2R. PERFORMED HFEC OF FASTENER HOLES PER B757 SRM. (2989763)SDR ASAA2017041220439Unknown · unknownWHEN PRESSING TOGA, ONLY ONE POWER LEVER ENGAGES THEN AUTOTHROTTLES DISENGAGE. ACFT GROUNDED. RESET SYSTEM, OPS CHECKED GOOD IAW AMM 22-31-00-710-801, AND 22-31-00-710-802.SDR VNAA2017022500032Unknown · vibrationAT 60 AND 80 KNOTS THE AIRCRAFT SHUTTERED AND PULLED TO THE LEFT. THE CREW REJECTED THE TAKE-OFF FOR SAFETY REASONS. PERFORMED OPERATIONAL TEST OF THE BRAKE SYSTEM AND PERFORMED TAXI CHECK OF THE AIRCRAFT. NO DEFECTS NOTED.SDR P5CA2017011700027Unknown · leakingDURING WALK AROUND INSPECTION, FIRST OFFICER NOTED OIL LEAKING FROM LEFT ENGINE. PERFORMED INSPECTION OF EXTERNAL & INTERNAL ON LEFT ENGINE, NO OIL LEAK EVIDENCE FOUND AMM 79-00-00/601. ACFT OK TO SERVICE.SDR DALA2016122910133Blanket · meltedLEFT REAR LAVATORY SMOKE DETECTOR WENT OFF ON FINAL APPROACH. NO SMOKE OR FUMES OBSERVED. PAX NOTED BURNED RUBBER ODOR IN AFT CABIN. ENGINE AND AIRFRAME ANTI-ICE WERE ON. FOUND RT TAILCONE SECTION COVERED IN DE-ICING FLUID, FOUND RED FIRE BLANKET MELTED TOSDR SWIA201643003Panel · gougedPANEL 435AT IS GOUGED. REPAIRED IAW REO.SDR N6WA2016122301Fitting · corrodedRIGHT WINDSCREEN MOUNTING PLATE SHOWS SIGNS OF CORROSION. R & R THE INBD FLOOR FITTINGS.SDR AALA20161221024Unknown · vibrationAFTER TAKEOFF, A LOUD RUMBLING NOISE AND VIBRATION OCCURRED. PASSENGERS FELT VIBRATION IN MIDDLE OF AIRCRAFT AND REPORTED WATER DRIPPING FROM AIR CONDITIONING OUTLETS. ACCOMPLISHED TSM 05-50-00-810-801 AND 53-35-00-810. EMERGENCY DECLARED.AIRCRAFT WAS GROUNDESDR CALA2016120200994Switch · damagedEDP SWITCH SHOWING SIGNS OF HEAT DAMAGE.SDR 7AHR2016112100001Door Frame · chafedFWD ENTRY DOOR UPPER AFT FRAME CHAFED. REPAIRED FWD ENTRY DOOR UPPER AFT JAM (SEAL DEPRESSOR) PER FLIGHT VEHICLES CONSULTING DRAWING 53-16151-1, AND DC-9/MD-80 SRM 51-30-5 PAGES 12-14.SDR FDEA201611184112Adapter · gougedMAIN CABIN CLS ADAPTER IS GOUGED AT FR 58 BETWEEN -Y45 AND -Y95 REMOVED AND REPLACED MAIN CABIN CLS ADAPTER AT FR 58 BETWEEN -Y45 AND -Y95 PER A300-600 SRM 51-40-21SDR JJBA20161006009Unknown · unknownPOSSIBLE SMOKE WITH FUEL LEAK NR 1 ENGINE NACELLE DRAIN. PERFORMED THREE ENGINE RUNS FOR 20 MINUTES EACH WITH NO LEAKS NOTED.SDR A6WA2016080144136Unknown · unknownABORTED TAKE OFF DUE TO STRONG PULL TO THE RIGHT, BTMS READS 4,5,3,2 ABORTED AT 50 KNOTS.SDR FDEA201607152453Spar · crackedAFTER PANEL 364RR, EMPENNAGE, INSIDE PANEL 364RR AFT SPAR WEB FOUND CRACK AT STA Y = 2164.SDR DALA2016071205239Structure · unknownFOUND RAISED SHARP EDGES AT LOWER SECTION OF THE ACME SCREW. COMPLIED WITH PRI/ERA 54850-14AD.SDR QXEA2016041300250Housing · damagedGPU CONNECTOR HSG CASTING, PN 80080104, REQUIRES REPLACEMENT. GPU CONNECTOR HSG DOOR REMOVED REF SRM 51-41-00. GPU CONNECTOR HSG DOOR INSTALLED REF SRM 51-41-00. FASTENERS COMMON TO SKIN/STRINGER 11P, GPU HSG CASTING REMOVED REF SRM 51-42-05. CONTINUED REMOSDR ASAA2016040116207Unknown · unknownIAW F/O REPORT, ACFT VEERED RT, DISCONNECTED AUTOPILOT TO LAND BY PILOT. ACFT GROUNDED. ACCOMPLISHED FAULT REVIEW, REF FIM 22-11, TASK 801, GROUP 20, NO FAULTS NOTED. ACCOMPLISHED DFCS LAND VERIFY TEST, GROUP 49, REF AMM 22-11-00/201, OPS CHECK NORMAL.SDR CVGA201603250088Unknown · failedHIGH SPEED ABORTED TAKEOFF NEAR VI FOR MAIN TIRE FAILURE. CREW ABORTED TAKEOFF AND REGAINED DIRECTIONAL CONTROL AFTER SWERVING RIGHT. USED EMERGENCY BRAKE TO ASSIST IN STOPPING ACFT AND OTHER MAIN TIRE FAILED. THE DETERMINATION OF WHICH COMPONENT/ASSEMBLY CAUSDR SWIA201641945Panel · chafedPANEL 699AB HAS CHAFE. REMOVED AND INSTALLED PANEL 699AB IAW SRM.SDR T17A201602238011Unknown · vibrationDURING CLIMB, AT APPROXIMATELY 6,000 FT MSL, THE CREW NOTICED A PRONOUNCED, ABNORMAL HIGH FREQUENCY VIBRATION PRESENT IN THE ACFT. THEY LEVELED OFF AT 7,000 FT MSL AS INSTRUCTED BY ATC AND ENGAGED THE ACFT’S AUTOPILOT AND BEGAN TO INVESTIGATE IN AN ATTEMPT TO SDR JTAA2016FA0000026Bearing · corrodedWHEN REMOVING BEAM, LT AND RT SIDES, IT WAS FOUND THAT BOTH OTBD BEARINGS WERE SEVERELY CORRODED. RT BEARING WAS SEIZED WITH NO VISIBLE INDICATIONS OF SEIZURE AND LT 1 WAS STIFF WITH RUST COMING OUT OF BEARING SEALS.SDR DALA2016012000443Access Panel · damagedDAMAGE FLAME SPRAY ON ACCESS PLATE 6504A0. ACCESS PLATE 6504A WAS REPAIRED IAW SRM 51-70-1AD, PAR 23, AND CARD 2000-8149-01, JOB 000-002.SDR AALA20151216002Unknown · unknownDURING APPROACH, AT APPROX 2300 FEET, ACFT WENT TO TOGA-GIA MODE AT MANNED SPEED SELECTION. ABORTED APPROACH. DURING GO AROUND MADE SEVERAL ATTEMPTS DISCONNECT TOGA FROM AUTO THRUST SYS, EACH TIME POWER WENT BACK TO TOGA. AUTOPILOT 1 DISCONNECTED SEVERAL TIMSDR DALA2015120207315Access Panel · corrodedACCESS PANEL 1456C WAS FOUND CORRODED OUT OD LIMITS IAW SRM 51-22-2A. ACCESS PANEL WAS REPLACED AND WILL BE INSTALLED UNDER CARD 2800-0390, JOB 001-0454.
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