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 DALA2024072207319None · noneSECTION III: REPETITIVE INSPECTION PER ER/A 616273-14AD REV A ISSUED FOLLOWING PERMANENT REPAIR ACCOMPLISHMENT OF THE LHS STA 1640 FRAME WEB AT THE LOWER HINGE INTERCOSTAL TEE CLIP. REF ERA 616273-14 REV A. (0457159)SDR HNAA2024090400223None · noneUNRECORDED REPAIR FOUND ON L/H OMEGA BEAM BTW FR 22-23.SDR HNAA2024090400222None · noneUNRECORDED REPAIR FOUND ON L/H OMEGA BEAM BTW FR 49-50.SDR CALA2024071802062Unknown · unknownMRD ISSUED MRD *ORD 01-2230Z* FOR AIRCRAFT 0231 ISSUED ON 16JUL24 15:30:21 ON FLIGHT 1784 FROM ORD TO DEN. NO FURTHER MAINTENANCE ACTION NEEDEDSDR CALA2024071800244Pump · unknownR ELEC HYD DEMAND PUMP AUTO INOP THE PUMP RH DEMAND OPS NORMAL IN ON POSITION. REQUEST DEFERRAL MEL 2911K APPROVED FOR MEL 2911K PLACED RH ELEC HYD DEMAND PUMP ON MEL 2911K AS REQUESTED. DDP FOLLOWED. THIS IS NOT A SDR REPORTABLE EVENT PER THE GMM. ATTEMPTINGSDR IPXA2024071742841Stabilizer · ground damageAIRCRAFT COLLISION TO RH HORIZONTAL TIPSDR CALA2024071800246A/C Pack · nonePREVIOUS UPDATES SUGGESTED THIS ITEM CAN BE CLEARED. CONFIRMED THE RH PACK IS OPERATIONAL AND THE MEL CAN BE CLEARED RAN AND OPS CHECKED REF AMM 21-51-00-730-802. RH PACK HAS BEEN RE-ACTIVATED AND OK FOR SERVICE. THIS ITEM WAS FLAGGED BY TECH FLAGGED MAJOR REPSDR CALA2024071602050None · noneBIRD STRIKE. INSPECTION REQUIRED PER AMM. BIRD STRIKE ON RIGHT SIDE LOWER NOSE DURING TAKEOFF. NO ABNOR MAL INSTRUMENT INDICATIONS. CW BIRD STRIKE INSP REF AMM 05-51-14 NO DAMAGE OR BIRD STRIKE FOUND. OK FOR SVCSDR YENA2024071601024None · noneDURING HEAVY MAINTENANCE: TC A2522070-01 ASSIGNED EMERGENCY EQUIPMENT INSTALLATION OF EASA COMPLIANCE 2ND SURVIVAL ELT; MAJOR ALTERATION EC A2522070-01 ACCOMPLISHED INSTALLATION OF 2ND SURVIVAL ELT.SDR AALA202407168528None · noneAIRCRAFT WAS GROUNDED: AT FL280 DURING THE INITIAL DESCENT, THE AIRCRAFT VIOLENTLY BANKED 30 DEGREES TO THE RIGHT WITH AN ANNUNCIATION ON THE PFD "ROLL AUTHORITY" WITH THE VERBAL AURAL. AUTOPILOT WAS DISENGAGED AND MAINTAINED CONTROLLED OF THE AIRCRAFT. BOEINSDR DXTA2024071212339None · noneBIRD STRIKE ON TAKEOFF FROM KRKD, AFTER LANDING INSPECTION SHOWED LEFT PITOT TUBE WAS STRUCK AND POSSIBLE ENGINE INGESTION. COMPLIED WITH AMM 05-51-45 GVI AFTER BIRD STRIKE. FOUND BIRD REMAINS ON LT PITOT PROBE & IN TIP OF PROBE. CLEANED PROBE FULLY & DIDN`TSDR IPXA2024071041602Inspection · none*SUPPLEMENTAL SDR* FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R) C/W EO-82173.SDR YENA2024071200995None · noneDURING HEAVY MAINTENANCE: A TEST FLIGHT WAS REQUIRED DUE TO FLIGHT CONTROL HARDWARE PREVENTIVE MAINTENANCE WHERE THE WORKSCOPE INCLUDED THE DISASSEMBLY OF SYSTEMS AND COMPONENTS THAT AFFECT THE OPERATIONAL CHARACTERISTIC OF THE AIRCRAFT THE AIRCRAFT PASSED SDR SWIA20241108709None · noneCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA74310-670-54-22-037 N787SK MXCODEID59647-PR - ENLARGED HOLES, LOG NUMBER 56115, LINE NO. 11. PERFORMED TEMPORARY REPAIR OF ENLARGED HOLES BY ACCOMPLISHING INSTRUCTIONS IN REO 670-54-22-037,. FINAL HOLE IS 0.354. INSDR AALA202409108763Fitting · no discrepancyAIRCRAFT 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 EA 356051. REPLACED RIGHT-HAND CONTINUITY FITTISDR DALA2024071006998None · noneAD/EM-EO TASK - RH WING W/C 5720-01102-05B STEP 24. TO GENERATE A STANDALONE "ADR" LOG PAGE AND ENSURE "SDR REPORTABLE" CHECKBOX IS MARKED ASSOCIATED WITH THE REPAIR. RH WING SEALANT APPLIED AS PER W/C 5720-01102-05B STEP 11. FOUND A SATISFACTORY AND W/C STEP SDR DALA2024071006997None · noneAD/EM-EO TASK - LH WING W/C 5720-01102-05A STEP 24. TO GENERATE A STANDALONE "SDR" LOG PAGE AND ENSURE "SDR REPORTABLE" CHECKBOX IS MARKED ASSOCIATED WITH THE REPAIR. LH WING SEALANT APPLIED AS PER W/C 5720-01102-05A STEP 11. FOUND SATISFACTORY AND W/C STEP 24SDR UIEA2024070980599None · noneDEVIATION FOUND DURING PERFORMING SB 777-57A0122 MODIFICATION.(<P>REMOVE DAMAGE PARTS I.A.W. SRM 51-40-02-0G-0, REV47. PERFORM EI NO T2024A57M-1552 REV 0. ACCOMPLISHED EI NO: T2024A57M-1552 REV 1. CONDITION CHECK NORMAL AND JOB COMPLETED. </P>)SDR AALA202407104770Window Frame · noneAIRCRAFT IN BASE MAINTENANCE: DUE TO THE MAJOR REPAIR BEING ACCOMPLISHED TO THE FLIGHT DECK CENTER WINDSHIELD LEFT HAND FRAME CENTER POST LOWER NODE ATTACHMENT, INTERNAL AREA LEFT HAND VERTICAL FLANGE THE RIGHT-HAND FRAME AT FR 2 AND Y0. NEEDS TO BE MODIFIED BSDR YENA2024070800942None · noneFLT#170, FLL-BOS. 'F/A'S REPORTED BURNING RUBBER SMELL MID CABIN; ACCOMPLISHED AMM TASK 05-50-00-831-A; ODOR CLASSIFICATION IS TYPE 10 CABIN ODOR AND CENTERED AROUND ROWS 14-15 ABC/DEF.REPLACED LIGHT ASSEMBLY AT 14 ABC/DEF AS PRECAUTIONARY REF AMM 33-22-11-86SDR EE4Y2024070420376Skin Panel · noneEXISTING REPAIR DOUBLER WITH MISSING RECORDS (MATERIAL TRACEABILITY), FOUND AT THE LH WING, AT LOWER SKIN, RIB 10, COO EVALUATED THE AFFECTED AREA AND SOME DEVIATIONS TO REF. ETD2017-190-088798 REV A DTD NOV / 13 / 2017 WERE FOUND, DUE TO THIS, WE CONTACTED ERSDR EE4Y2024070420377Skin · noneDURING THE ACTUAL MAINTENANCE LABOURS, HAS BEEN NOTICED THAT THE REPAIR INSTALLED BETWEEN FR 9 AND FR 11 BETWEEN STR 15L AND STR 18L DOES NOT HAVE THE REPAIR MATERIAL TRACEABILITY DATA. REMOVED EXISTING DOUBLER AS PER ERJ190 SRM PART II 51-41-01 PARAG. 4 FIG. SDR HNAA2024090500235Repair · not enteredAT FR 10, BTW STR 20L-21L UNRECORDED ROUND PATCH FOUND.SDR HNAA202409050234Repair · not enteredUNRECORDED PATCH BTW FR24-25 AND BTW STR18L-20L.SDR CALA2024070800147None · noneTECH SUPPORT UPDATE ON CHRONIC R/H RAM AIR DOOR FULL OPEN LIGHT STAYING ON IN THE AIR. NOTE THE FWD ACT WAS REPLACED 6-26 AND AFT ON 6-17 PLZ PERF OPS CHECK A/C IN AIR MODE AND CYCLE FLAPS CHECK RAM AIR DOOR FOR ANY BINDING AND FOR CORRECT POSITION COMPARE TO SDR CALA2024070500144None · noneMULTIPLE BIRD STRIKE ON TAKEOFF APPROX 500FT RIGHT WING AND FUSELAGE 2. ACP BIRDSTRIKE INSPECTION, FOUND BIRD STRIKES ON RH AND LH OB WING LE AND SCIMITAR, NOSE RADOME AND ONE ABOVE FLIGHT DECK WINDOWS, CLEANED SURFACES, NO DAMAGE TO AIRCRAFT STRUCTURE WAS FOSDR IPXA2024070337674Drain · noneFUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R. EO-82173-JIC001 WAS ACCOMPLISHED.SDR SWAA2024080821406Unknown · unknownTHICKNESS MEASUREMENT OF GAP BETWEEN INNER CHORD AND WEB S-18A BS 727 RIGHT SIDE IS 0.024 INCH 2024-405139<[01] FAULT RESOLVED ON OTHER FAULT TTG8Q00UBC80;[02] FAULT RESOLVED ON OTHER FAULT TTG8Q00UBC80 ; RIISDR SWAA2024080821405Unknown · unknownTHICKNESS MEASUREMENT OF GAP BETWEEN INNER CHORD AND WEB S-18A BS 727 LEFT SIDE IS 0.037 INCH 2024-405138<[01] FAULT RESOLVED ON OTHER FAULT TTG8Q00UBC7V;[02] FAULT RESOLVED ON OTHER FAULT TTG8Q00UBC7V ; RIISDR CALA2024070201949None · noneBIRDSTRIKE, EXCEPT AT ENGINE INLET STRIKE ON LOWER NOSE LEFT SIDE. INSPECTED SUSPECTED AREA, NO DAMAGE NOTED. FOUND SMALL BLOOD STAIN UNDER PILOT WINDOW. NO BIRD CARCASS OR FEATHERS FOUND. INSPECTED REF AMM 05-51-18SDR SIMA20240629002None · noneFLAP OVERSPEED FLAPS 1 235 KTS 30 SECONDS DUE TO TURBULENCE. C/W PHASE-1 INSPECTION PER EMB 175 AMM 05-50-07 NO DEFECTS NOTED. PHASE-II INSPECTED DEFERRED FOR 10 FC ISSUED TDMI 054T05138. DEFERRED PER AMM REF 05-50-07 TDMI AUTHORIZATION NUMBER 054T05138.SDR YENA2024070100926Flap · unknownFLT#938, SJD-JFK. (AIRCRAFT DECLARED AN EMERGENCY INTO JFK) ' FLAP OVERSPEED WARNING ON CLIMB OUT. FLAPS RETRACTED ON SCHEDULE. ACTUAL SPEED WAS NOT ON OVERSPEED TAPE AS IT WAS NOT DISPLAYED ON PFD. INDICATED SPEED 235KTS WHEN WARNING CAME ON. NO LONGER THAN 5SDR DXTA2024070112220None · noneONE OF THE INTERIOR EMERGENCY EXIT LIGHTS UNDER THE DIVAN IS INOPERATIVE. OPS TESTED EMER LIGHTS AND FUNCTION NORMALLY CYCLED POWER MULTIPLE TIMES AND EVERY TIME THE FUNCTION NORMALLY. WORK DONE IAW CL 350 AMM TASK 33-51-00-710-801 REV 32.SDR HNAA2024070100497None · noneDURING TAKE-OFF AT APROX 80 KTS HIT A SEAGULL ON NOSE OF AIRCRAFT. FACT 29JUN24 10:19 INSP'D A/C FOR BIRD STRIKE. FOUND SMUDGE ON NOSE. NO SIGNIFICANT DEFECTS NOTED. PER EMB AMM 05-50-08-200-802-A. OK FOR SERVICE.SDR CALA2024071001995None · noneRH # 1 WINDOW FROM PREVENTATIVE MOD. REF AAR N/R 9891222. COMPLIED WITH SDR FORM 46-0024 PAGE 1-3.SDR CALA2024071001994None · noneLH # 1 WINDOW FROM PREVENTATIVE MOD. REF AAR N/R 9891221. COMPLIED WITH SDR FORM 46-0024 PAGES 1-3.SDR CALA2024070300115Interface Unit · inoperativeREF L/P 8335328, UNABLE TO CREATE NEW CLIENT CREDENTIALS FOR AID-FWD. FOUND EXISTING ACTIVE FAULT 46-52003.AIRCRAFT INTERFACE DEVICE-FORWARD (AID-FWD WA DOES NOT RESPOND TO NFS COMMANDST/S PER FIM 46-13 TASK 857, NO HELP. SUSPECT AID INOP. M&E 61-4613-9-0001 NSDR CALA2024070300114None · noneCREATE ESFR FOR REPORTING PURPOSES ONLYSDR DALA2024062706565Fitting · noneSHIP 3331 NRC 200-284 EM-EO TASK - WHILE ACCOMPLISHING STEP 13 FOUND FITTING ASSY P/N: F534-91907-008-00 AS PER DWG F53985080, SHT 05 FOUND QTY 06 PILOT HOLES MISMATCHED EXISTING HOLES ON SKIN. CORRECTIVE ACTION: COMPLIED WITH DELAT AIR LINES DOCUMENT VA NO.10SDR AALA202408166513Fitting · noneAIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK CENTER WINDSHIELD FRAMING RIGHT HAND CONTINUITY FITTING BETWEEN FR 1 AND FR 4 AT Y0 REQUIRES REPLACEMENT DUE TO THE MAJOR REPAIIR BEING ACCOMPLISHED PER EA 355317. REPLACED CONTINUITY FITTING PER EA 355317.SDR AALA202407015200Fitting · noneAIRCRAFT IN BASE MAINTENANCE: DUE TO THE MAJOR REPAIR BEING ACCOMPLISHED ON THE AFT AVIONIC COMPARTMENT RACK 80VU RIGHT LOWER LATERAL ATTACH FITINGS REPORTED ON (AALA202407017159 AND AALA202407011959) THE LOWER LEFT LATERAL ATTACH FITING AT FR 24, +Y1263 AND ZSDR AALA202407018026Fork · noneAIRCRAFT IN BASE MAINTENANCE: DUE TO THE MAJOR REPAIR BEING ACCOMPLISHED ON THE AFT AVIONIC COMPARTMENT RACK 80VU RIGHT LOWER LATERAL ATTACH FITINGS REPORTED ON (AALA202407017159 AND AALA202407011959) THE LOWER LEFT LATERAL ATTACH FITING FORK END CLEVIS AT FR SDR DALA2024062606524None · noneSHIP 661 REF. RC 5311-01247-01A, STEP 6: FOUND EXISTING REPAIR AT LH STA 1640; REF: ERA 570342-14AD REV A. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 114-0001:5311-01247- 01A/001 00135 COMPLIED WITH VA 91497MA. (0413021)SDR IPXA2024062507531None · noneFUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R. ACCOMPLISHED EO-82173-JIC001.SDR 4DPA2024062400001Antenna · failedCREW REPORTED- ON INITIAL DEPARTURE FROM KSDL, AT 4000’ MSL MASTER WARNING LIGHT ILLUMINATED AND DOUBLE BELL SOUNDED WITH AN AURAL “WARNING, GEAR” THAT WOULD NOT SILENCE. THERE WAS NO EICAS WARNING, AND ALL THREE GEAR SHOWED UP AND LOCKED. CONTINUED THROUGH 60SDR QMLA2024062620072None · noneAFTER LANDING MEDICAL CREW NOTICED OIL LEAKING FROM CEILING OF THE CREW COMPARTMENT. REMOVED THE CENTER OVERHEAD INTERIOR PANEL AND THEN THE MAIN TRANSMISSION DRIP PAN. THERE WAS SOME RESIDUAL OIL THAT DIDN’T SEEM TO MAKE IT DOWN THE DRAIN HOLES, BUT THE OIL PSDR DALA2024062406450None · noneREMOVE AND RE-INSTALL GIRT BAR ONLY PURPOSE ADJUSTMENT DOOR 831,841,83 2 AND 842. REMOVED AND RE-INSTALLED GIRT BAR IN DOOR 831,832 AT PASSENGER CABIN AS PER A320FAM AMM 25-62-44-000-012-A AND AMM25-62-44-400- 007-A AND DOOR 841,842 AS PER A320FAM AMM 25-62-SDR SWI2024F0000595None · nonePERFORMED CUT--LINES TO STR23L AND STR23R TO ACCESS AND REMOVE FRAME 280.00 THIS PROCEDURE HAS BEEN DETERMINED TO BE A MAJOR REPAIR PER GMM 3-26 (FILED CLOSED) REPAIRED STR23L AND STR23R AT FS FRAME 280.00 IN REF TO REO 670-53-11-1967 REV-- DATED 2024-SDR FDEA202406210829None · noneEXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR56 - FR57.2 SEAT TRACK AT Y1959 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR56-FR57.2 SEAT TRACK AT Y1959 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53SDR FDEA202406210828None · noneEXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR59 - FR60 SEAT TRACK AT Y1959 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR59-FR60 SEAT TRACK AT Y1959 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-1
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