JASC 5100
Service difficulty reports · 4,235
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 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.SDR 2025FA0000052Unknown · unknownDURING MAINTENANCE SERVICES FROM THE LUBE CLUSTER OF AN AUXILLARY POWER UNIT THE BYPASS VALVES WHERE NOT TESTED IN ACCORDANCE WITH THE CMM REQUIREMENTS. THE VALVES WERE ONLY TESTED VISUAL AND FUNCTIONALLY AND NOT AS REQUIRED BY TEST PROCEDURE.SDR IPXA2025012193764None · none(FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R). COMPLIED WITH EO-82173. CONDITION CHECK OK.SDR SWAA2025012188028None · noneFUEL LEAK R SIDE<[01] PERFORMED IDLE LEAK CHECK PER M/M 71-00-00. NO LEAKS NOTED. ALL ENGINE PARAMETERS ARE NORMAL BETWEEN ENGINE 1 & 2. AFTER ENGINE RUNS; VERIFIED NO LEAKS WITHIN THE COWLINGS OR ON THE EXTERIOR. ALL FUEL TANK ACCESS PANELS VERIFIED TO BE DRYSDR CALA2025012101948Unknown · leakingFLT ATTNDT REPORT AFT GALLEY-SOAKED UNKNOWN SOURCE UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. MAC METER INITIATED FOR WITH VENDOR ID MAC RELATED WORK ORDER 000000003127511. INSPECTED AFT LAV TOILETS, SINKSSDR CALA2025012100145None · noneETOPS PRE-DEPARTURE SERVICE CHECK REQUIRED. ETOPS PDSC COMPLETED EPDSC EXPIRES . OIL SERVICE ACCOMPLISHED ENGINE 1: 00 CHECKED BY U349089 ENGINE 2: 00SDR YENA2025012100078None · noneDURING HEAVY MAINTENANCE: EXISTING REPAIR STRINGER 2 LH FR29 TO FR30 IN PASSENGER CABIN (FOR A320 AGING AIRCRAFT PROGRAM); (RESOLVED ON W/O: 1331840 TASKCARD: NR-00045) PERFORMED REPAIR ON STR 2 LH BTW FR28 TO FR31 IN PASSENGER CABIN IAW A320 SRM 53-21-13-300-SDR IPXA2025011826131None · noneREF HEAVY CHECK REPAIR T3F18E0056FMQ, HFEC AFTER TRIM OUT REQUIRES RII VERIFICATION. VERIFIED ACCOMPLISHMENT OF REPAIR PER EA 757-5360-27-A3769, REV- COMPLETED.COMPLIED WITH EO-92552. REVIEWED.SDR IPXA2025011826183None · noneREF HEAVY CHECK REPAIR T3F18E0056FHS, HFEC AFTER TRIM OUT REQUIRES RII VERIFICATION. VERIFIED ACCOMPLISHMENT OF REPAIR PER EA 757-5360-27-A3770, REV- COMPLETED.COMPLIED WITH EO-92553. REVIEWED.SDR IPXA2025012126292None · noneREF HEAVY CHECK REPAIR T3F18E004J5QK, HFEC AFTER TRIM OUT REQUIRES RII VERIFICATION. VERIFIED ACCOMPLISHMENT OF REPAIR PER EA 757-5360-27-A3771, REV- COMPLETED.COMPLIED WITH EO-92554. REVIEWED.SDR IPXA2025011826274Frame · no discrepancyREF HEAVY CHECK REPAIR T3F18E004SYHW, HFEC AFTER TRIM OUT REQUIRES RII VERIFICATION. COMPLIED WITH EO-92551. REVIEWED.SDR REXA2025012700092Frame · unknownWHILE PERFORMING SB 670BA-53-044 REVISION G DATED JUL05/2022 FOUND LH AND RH DOUBLERS PN CC670-34222-001SB AND CC670-34222-002SB AND LH AND RH STR12A FITTINGS PN CC670-34365-001SB AND CC670-34365-002SB CANNOT BE INSTALLED PER SERVICE BULLETIN INSTRUCTIONS DUE SDR CALA2025011601934Unknown · smokeTOWER REPORTED THATTHEY OBSERVED WHITE SMOKE FROM THE TIRE AREA ON TAKEOFF. PERFORMED A GVI OF THE BRAKING SYSTEM AND TIRE REF AMM 32-40-00-210-801-A & 32-41-00-210-002-A NO DEFECTS NOTED. PERFORMED A WALK AROUND THE AIRCRAFT FOR HYDRAULIC LEAKS NO DEFECTSDR HNAA2025011100023None · no discrepancyBIRDSTRIKE LEFT OUTBD FLAP. C/W BIRDSTRIKE INSP IAW AMM 05-50-08 CLEANED BIRD REMAINS NO DEFECTS NOTED.SDR HNAA2025011100022None · no discrepancyBIRD STRIKE ON LH SIDE OF NOSE. PERFORMED BIRDSTRIKE INSPECTION IRW AMM 05-50-08. NO DAMAGE NOTED. A/C OK FOR SERVICE.SDR SCNA20250114011SStop Fitting · no discrepancyOVERWING EMERGENCY EXIT DOORS (832, 833, 843) DOOR STOPS INSTALLED PROPERTY IN REF B737-800 AMM 52-22-01-400-801 T/W ID: 19-987 D.D: 12FEB2025 83090/83963 SAA024 01FEB2025. OVERWING EMERGENCY EXIT DOOR (842) DOOR STOPS INSTALLED PROPERLY IN REF. B737-800 AMSDR DALA2025011400330Skin · not reportedSHIP 6815 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 623325-14AD. CORRECTIVE ACTION: REF ERA 623325-14AD. (0756584)SDR DXTA2025011401926None · noneSEVERE TURBULENCE: AIRCRAFT ENCOUNTERED SEVERE TURBULENCE INFLIGHT. AIRCRAFT WAS CONFIGURED WITH THE FLAPS UP AND THE GEAR UP WITH AUTOPILOT ON, AUTOTHROTTLES ON, SPD FMS, VS ON. THERE WERE TWO SEVERE TURBULENCE EVENTS THAT HAPPEN BETWEEN FL240 AND FL200. THE SDR IPXA2025011317523Skin · pilot error*SDR FILED OPEN* TAIL STRIKE IDENTIFIED ON WALK AROUND INSPECTIONSDR DXTA2025011301921None · noneDAMAGE INSPECTION: SEVERE TURBULENCE WHILE ON RAVEN ARRIVAL IN TO MTN. APPROX 15,000-FL200. CORRECTIVE ACTION: PERFORMED INSPECTION. NO DEFECTS NOTED. IAW CE560XL AMM 05-50-00SDR DXTA2025011301907None · noneFUSELAGE STRUCTURE: ENCOUNTERED SEVERE TURBULANCE OVER KLIT AT FL390, CLEAN CONFUGURATION, M.75. AIRCRAFT DROPPED MAYBE 20' IN 1/2 SECOND, NO ROLLING MOTION. ALL OCCUPANTS SEATED AND BELTED AT THE TIME SO NO INJURIES, A FEW CABIN ITEMS AND PERSONAL ITEMS TOSSDR CALA2025011301887Unknown · noiseLOW SPD RTO FOR LOUD NOISE AND JOLT SEEMING TO COME FROM NOSE GE AR AREA AT STRT OF T/O ROLL WORK WITH L/P 3477239 (LEFT ENGINE SURGE T/SHOOTING). DEBRIEF WITH CREW ,SUSPECT THE SURGE OF LEFT ENGINE DUE TO HEAVY CROSSWINDS. BUT DID INSPECT FWD NOSE GEAR, FWD SDR HALA20250110016Lavatory · inoperativeDIV - ALL LAVS INOP REACHING FL330. WIRING CONTIUITY & SHORTS TO GROUND CHECK OK. FROM 40MG TO 300RH8 & 41MG TO 300 RHT. NO FAULTS NOTED. CLEANED TANK + LVL SENSOR. LEVEL SENSOR FAULTS INTERMITTENTLY. INSPECTED LEVEL SENSOR AND WASTE TANK FOUND DIRTY. RINSE ANSDR DALA2025011000231None · noneSHIP 5654 AD, AA, IN REF AMDS 5331-01282-03 STEP 2. TWO PREVIOUS REPAIRS WERE FOUND ON LAP SPLICE STR-14L STA .580 AND 620 AT FUSELAGE SKIN. CORRECTIVE ACTION: SUMMARY OF NRC 00004. AREA ON LAP SPLICE STR-14L STA .580 AND 620 AT FUSELAGE SKIN WAS PROVIOUSLY RESDR DALA2025011900435None · noneSHIP3251 DISC: ER/A 604897-14 / SECTION III INSPECTIONS. C/A: ER/A 604897-14, REV C / AT, OR PRIOR TO 8,000 FLIGHT CYCLES FROM SECTION II REPAIR (43,171 TOTAL FLIGHT CYCLES), AND REPETITIVELY EVERY 1,500 FLIGHT CYCLES THEREAFTER, ACCOMPLISH SECTION II INSPECTISDR DALA2025010900186None · noneSHIP 5654 DTA MONITOR INSPECTION LOG REF ERA 623410-14 FUSELAGE / LAP SPLICE / BTW BSTA 580 AND BSTA 640 / S-14L / EXISTING REPAIR / INHIBITED INSPECTION. CORRECTIVE ACTION: REF ERA 623410-14AD. (0751772)SDR VNAA20250108026None · noneTEMP. REPAIR COMPLIED WITH PERMANENT REPAIR OF SKIN FS295-FS333, STR15-16R REPAIR IAW PSA EA:A1-670-53-00110 REV D DATED 2024-12-01.SDR VNAA20250108008Seat Track · corrodedSEAT TRACK IN AFT CARGO AT RBL27, FS1000 IS CORRODED. FOUND DISCREPANT SEAT TRACK TO BE OUT OF LIMITS DUE TO THERE BEING NO LIMITS PROVIDED IN THE SRM. COMPLIED WITH REO 670-53-00-00-755, REV --, DATED 2024-10-11, REPAIR B. FABRICATED NEW SEAT TRACK P/N BA67SDR IPXA2025010869446None · noneADD SDR FOR EO-82173-JIC001 (FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R) ACCOMPLISHED.SDR CALA2025010701834Seal · brokenAFT RIGHT FLIGHT ATTENDANCE EMERGENCY BATTERY SEAL BROKEN. REPLACED AFT RIGHT FLIGHT ATTENDANCE EMERGENCY BATTERY SEAL AS REQUIRED.SDR DXTA2025011001867None · noneENGINE FOD: ON SHORT FINAL, BIRD INGESTED INTO LEFT ENGINE. ACCOMPLISHED FOREIGN OBJECT DAMAGE INSPECTION. NO DEFECTS NOTED. IAW CE-700 AMM 5-50-00.SDR SWIA202501300005Access Panel · corrodedLH FUEL PANEL ACCESS DOOR LANDING AT 540BB HAS 2 AREAS OF MINOR PITTING, OUTBOARD AFT EDGE APPROX. 4" TOTAL AND SEMI-CENTER FWD APPROX 1". (FILED OPEN) REPAIRED CORROSION DAMAGE ON FUEL ACCESS PANEL OPENING 540BB, OUTBOARD AFT EDGE APPROX. 4" TOTAL AND SESDR DXTA2025010801845None · noneJUST AFTER WHEELS TOUCHED DOWN, SMALL BIRD MADE CONTACT WITH LEFT SIDE OF AIRCRAFT. DURING POST FLIGHT, FOUND FEATHERS AND BIRD REMAINS (BLOOD) IN L #2 ENGINE. PERFORMED BORESCOPE INSPECTION. NO EVIDENCE OF DAMAGE. PERFORMED ENGINE RUNS WITH NO DEFECTS NOTESDR DALA2025010800173None · noneRE-INSTALL PREVIOUSLY REMOVED FWD CARGO DOOR UPPER SCUFF PLATE. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 046-0001:5331-01297-01C/002 00616 ACCOMPLISHED INSTALLATION REF. NR 241 AND ASSOCIATED ER/A PRI 623164-14. (LPSDR IPXA2025010726757None · noneADD SDR FOR EO-82173-JIC001 (FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R) COMPLETED SDR.SDR IPXA2025010522565Frame · not reported*SDR FILED OPEN* REF FRAME REPAIR T3F18E005ERBT, CORRECTIVE ACTION 7. - SURFACE HFEC PERFORMED ON CUTOUT ON FRAME 1460 RH SIDE IN AFT PIT REQUIRES RII AUTHORIZATION ACCOMPLISH REPAIR PER EA 757-5360-27-A3756, REV- PRIOR TO FURTHER FLIGHT.SDR QXEA2025010600002None · noneREJECTED TAKEOFF AT APPROXIMATELY 65-70 KNOTS DUE TO POSSIBLE BIRDSTRIKE NORMAL DECELLERATION WITH NO BRAKE OVERHEAT INDICATION. NO OBSERVED BIRDSTRIKE EVIDENCE DURING POST FLIGHT. ABORTED TAKE OFF. REMOVED FROM SERVICE. PERFORMED BIRDSTRIKE INSPECTION IAW E17SDR CALA2025010601822None · noneEMERGENCY EQUIPMENT INSTALLATION - INSTALLATION OF EXTINGUISHER, FIRE, HALOTRON AT LOCATION F/F (1L S21 CLOSET) FOR TRACKING PURPOSES DUE TO AC INDUCTION. INSTALLED NEW EXTINGUISHER, FIRE, HALOTRON AT LOCATION F/F (1L S21 CLOSET) REF TASK CARD NUMBER 2500-1258SDR AALA202501062005Fitting · noneAIRCRAFT IN BASE MAINTENANCE: AFT AVIONIC COMPARTMENT RACK 80VU LEFT HAND LATERAL FITTING BETWEEN FR 23 AND FR 24 AT S32L REQUIRES REPLACEMENT DUE TO THE MAJOR REPAIR BEING ACCOMPLISHED ON THE RIGHT HAND SIDE OF THE AFT AVIONIC COMPARTMENT RACK 80VU. MAINTENASDR DALA2025020500870None · none-AD- WHILE IN MAINTENANCE, AA WORK CARD 5720-01103-01B RH WING XRS 164, REAR SPAR AND LWR SKIN INSPECTION WAS COMPLETED WITH NO FINDINGS. DAL BELIEVES ADDITIONAL INSPECTIONS BEYOND THE SCOPE OF AA WC 5720-01103-01B ARE NECESSARY TO VERIFY NO DAMAGE IS PRESENT SDR DALA2025010600113Unknown · unknownDTE, ER/A 612109-14AD REV B REQUIRES STAGE 3 DTA APPROVAL. A220-100 / FUSELAGE / REAR BARREL / FR70 TO FR72 AND STR23L TO STR25L / DENT. ER/A 612109-14AD REV B REQUIRES STAGE 3 DTA APPROVAL ON OR BEFORE 30,000 FLIGHT CYCLES FROM SECTION III REPAIR EMBODIMENT OSDR YENA2025010300011Cids · faultedFLT#20, LHR-JFK. (ETOPS) ' CIDS 2 CLASS MX MSG ( CLASS II MX MSG DISPLAYED - CIDS ); PERFORMED FULL RESET OF CIDS PER AMM 23-73-00. TEST OK NO FAULTS PRESENT. MDDR CLEARED MX-4 UPDATED.'SDR SWAA2025010681941None · noneINFO ONLY CB P18-3 B-10 LIGHTING R AFT EMER CHGR POPPED.SDR DALA2025010312129None · noneSHIP 184 WORKING PRI 623121-14AD. CORRECTIVE ACTION: FINAL ERA ISSUED WITH AMOC 24-198 C/W FINAL ERA ISSUED WITH AMOC 24-198 ERA NO. 623121-14AD REV ORIGINAL (0736919)SDR UIEA2024123001194None · noneHIT BIRDS ON TAKE OFF. HIGH SPEED REJECT AT 110 KTS(<P>PERFORMED HIGH ENERGY STOP CONDITIONAL INSPECTION IAW AMM 05-51-07, NO DEFECTS NOTED. PERFORMED BIRD STRIKE CONDITIONAL INSPECTION IAW AMM 05-51-18, NO SIGN OF INGESTION ON ENG CORE. NO DENTS OR OTHER DEFESDR DXTA2025010201766None · noneFUSELAGE STRUCTURE: BIRD STRIKE ON RIGHT WING NEAR FUSELAGE. SMUDGE ON INSIDE OF RIGHT ENGINE NACELLE INDICATES IT WENT INTO THE ENGINE. CORRECTIVE ACTION: VISUAL INSPECTION COMPLETED. NO DAMAGE NOTED IAW CE680A AMM 5-50-00
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