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 DALA2022121308074None · noneSHIP 3305 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR DOOR LOCATED INTERNAL AREA AT LEVEL FR62 TO FR63 IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: EXISTING REPAIR WAS REMOVED SINCE IT WAS DAMAGE. INSPECTION WERE EXECUTED WITH NIL FINDINGS AND A NEW REPAIR ISDR DALA2022121308073None · noneSHIP 3305 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED SLAT 5 ON LH WING. CORRECTIVE ACTION: EXISTING REPAIR INSTALLED PER NWA EA 33-214642 REV-A, APPROVED. AS PER ER/A603078-14 HAS BEEN COMPLIED WITH AND ER/A 603078-14. ( 2533436)SDR DALA2022121308072None · noneSHIP 3305 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR FUEL TANK LOCATED RIB6 AFT ON LH WING. CORRECTIVE ACTION: EXISTING REPAIR INSTALLED. REPAIR IS APPROVED PER AIRBUS REPAIR DRAWING R57257026 ACCORDING TO FAA AD 2006-22-14, PARA. (K) GUIDELINES. AS PER ER/SDR DALA2022121308071None · noneSHIP 3305 EXISTING ALTERATION INSTALLED PER 5320-01135. INSTALLATION IS APPROVED BY STC ST02455LA. STC IS APPROVED FOR DAMAGE TOLERANCE INACCORDANCE WITH FAR 25.47 AND 25.571. AS PER ER/A 603078-14. CORRECTIVE ACTION: EXISTING ALTERATION INSTALLED PER 5320-011SDR DALA2022121308070None · noneSHIP 3305 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED FR 30 TO FR31 BTW STR1L TO STR1R ON UPPER FUSELAGE. CORRECTIVE ACTION: EXISTING ALTERATION INSTALLED PER 2325-01059-03. STC IS APPROVED FOR DAMAGE TOLERANCEIN ACCORDANCE WITH FAR 25.SDR DALA2022121308065None · noneSHIP 3305 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR DOOR INNER SKIN AT FR23 TO FR23A IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: EXISTING REPAIR INSTALLED PER ER/A 539577-14. AS PER ER/A603078-14 PRI REV-0 HAS BEEN COMPLIED WITH AND ER/A 603078-14 REV-ORISDR DALA2022121308064None · noneSHIP 3305 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR INTERNAL STRUCTURE ON STRINGER 56R LOCATED FR70 IN AFT CARGO COMPARTMENT. CORRETIVE ACTION: EXISTING REPAIR INSTALLED PER ER/A 590986-14 AND A330 SRM 53-00-13-300-001, APPROVED AS A CATEGORY (A). AS PER ESDR DALA2022121308063None · noneSHIP 3305 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR OUTBOARD SIDE LOCATED EXTERNAL SKIN BTW RIB 8 TO RIB9 ON RH PYLON. CORREECTIVE ACTION: EXISTING REPAIR INSTALLED PER ER/A 582864-14AD AND A330 SRM 54-51-00-300-006. AS PER ER/A 603078-14 PRI REV-0 HAS BEESDR DALA2022121308062None · noneSHIP 3305 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR PASSENGER CREW DOOR 834 LOCATED LOWER AFT CORNER IN PASSENGER CABIN. CORRECTIVE ACTION: EXISTING REPAIR INSTALLED PER A330 SRM 52-13-00-300-013, WHICH IS A CATEGORY (B), AS PER ER/A 603078-14 PRI REV-0 HASDR DALA2022121308061None · noneSHIP 3305 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED FR.66 BTW STR50R TO STR56R AT LOWER FUSELAGE. CORRECTIVE ACTION: EXISTING REPAIR INSTALLED PER ER/A 523233-14 AND A330 SRM 53-41-11-300- 017. AS PER ER/A 603078-14 PRI REV-0 HAS BEENSDR DALA2022121308056None · noneSHIP 3417 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN AT FR60A BTW STR46R TO STR47R AT LOWER FUSELAGE . CORRECTIVE ACTION: REPLACED OVERHEAD EMERGY EXIT SIGN ASSY AT LOC 3L PER A330 AMM 33-51. (9458547)SDR DALA2022121308082None · noneSHIP 3305 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED FR.53 TO FR.54 BTW STR1L TO STR1R ON UPPER FUSELAGE. CORRECTIVE ACTION: EXISTING ALTERATION INSTALLED PER 2330-01325-01C. INSTALLATION IS APPROVED BY STC. STC ARE APPROVED FORDAMAGE SDR QMLA2023120920006None · noneAP MEL'D 2210-02 FOR INSPECTION DATA LOGGING, POSSIBLE ISSUES WITH AP.SEE SDR SUBMISSION QMLA2023111720005 FOR FURTHER DETAILS. THIS SDR SUBMISSION IS LATE DUE TO TROUBLE SHOOTING WITH BELL HELICOPTER AND OUR OWN ENGINEERING SUPPORT TEAM. 3 OTHER BELL 407 GXI SDR CALA2022120803344None · nonePLEASE COMPLY WITH IN-DEPTH SPILL CLEAN UP PER ECRA 2011-01000 IN FORWARD CARGO PIT DUE TO GREY WATER LINE PUNCTURE. BODY STATION 652 TO 748 IN THE FORWARD CARGO PIT, AIRCRAFT LEFT SIDE. WITHIN 36 MONTHS, ACCOMPLISH EC/RA 2011-01000, CARGO COMPARTMENT SPILL, SSDR CALA2022120803336None · noneAS REQUIRED BY AD 2012-25-11, ACCOMPLISH AN NDT INSPECTION OF THE FUSELAGE SKIN DOUBLER (INSTALLED PER EA 5330-04213 OP4) BEFORE 37,500 TOTAL AIRCRAFT CYCLES. AFTER THE ACCUMULATION OF 34,500 TOTAL AIRCRAFT FLIGHT CYCLES, BUT BEFORE 35,000 TOTAL AIRCRAFT FLIGHSDR 1E1R20221213R0174None · noneAFT CARGO RACK 9940VU REMOVAL (STS ST12314CH). MAJOR ALTERATION REPORTED AT CUSTOMER REQUEST.SDR ABXA2022128149None · noneRABBIT STRIKE ON T/O ABORTED 120KTS. AIRCRFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. INSPECTION C/O IAW AMM 05-41-01 NO DEBRIS FOUND, NO DAMAGE. SATISFACTORY. AIRCRAFT RETURNED TO SERVICESDR DALA2022120907951None · noneSHIP 3305 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR PASSENGER CREW DOOR 4L L OCATED LOWER AFT CORNER IN PASSENGER CABIN. ACCOMPLISHED DETAIL VISUAL INSPECTION ON REPAIR DOUBLER LOC. ON EXTERNAL SKIN AT DOOR AS REQUIRED PER AND ER/A 603078-14 AND NOT FOUNSDR CALA2022120703316None · noneTHE REPAIR INCORPORATED VIA ECRA 5360-01679 IS APPROVED AS TIME- LIMITED FOR 18 MONTHS PENDING THE RESULTS OF A DAMAGER TOLERANCE ANALYSIS (DTA). REMOVE THE AIRCRAFT FROM SERVICE ON OR BEFORE MA Y 09, 2024, UNLESS ANOTHER 8110-3 FORM IS RECEIVED FINDING APPRO SDR CALA2022120703315None · nonePLANNING TO CONTACT ENGINEEERING AFTER 02APR23, BUT BEFORE 02MAY23 FOR EC/RA 5341-01359 PART 2 STEP 2 INSPECTION REQUIREMENTS. ITEM PLACED ON DIP OK TO CARRY PER ECRA 5341-01359, PLANNING TO CONTACT ENGINEERING TOMC-APPROVAL FROM SC1ELBYC COMMENT AFTER 02-APRISDR CALA2022120703314None · noneFR66 AND FR68 DOOR STOPS RH EXISTING UNDOCUMENTED REPAIRS. REPAIR IS EXPECTED TO BE A PERMANENT SOLUTION WITH INSPECTION OF THE LATEST REVISION OF EC/RA 5341-01359 ON OR BEFORE THE REQUIRED. ACCOMPLISH INSPECTION REQUIREMENTS PER PART 2, STEP 1 AIRCRAFT REACHSDR CALA2022120703313None · nonePLANNING TO CONTACT ENGINEEERING AFTER 25635 TOTAL FLIGHT CYCLES, BUT BEFORE 25685 TOTAL FLIGHT CYCLES FOR EC/RA 5341-01359 PART 2 STEP 1 INSPECTION REQUIREMENTS. ITEM PLACED ON DIP OK TO CARRY PER ECRA 5341-01359, PLANNING TO CONTACT ENGINEERING TOMC-APPROVALSDR CALA2022120703312None · noneFR66 AND FR68 DOOR STOPS LH EXISTING UNDOCUMENTED REPAIRS. REPAIR IS EXPECTED TO BE A PERMANENT SOLUTION WITH INSPECTION OF THE LATEST REVISION OF EC/RA 5341-01359 ON OR BEFORE 02JUN23. REQUIRED. ACCOMPLISH INSPECTION REQUIREMENTS PER PART 2, STEP 2 LH FR66 &SDR CALA2022120703311None · noneTHE REPAIR INCORPORATED VIA ECRA 5310-08079 IS APPROVED AS TIME LIMITED UNTIL 37,500 TOTAL AIRCRAFT FLIGHT CYCLES PENDING THE RESULTS OF A DAMAGE TOLERANCE ANALYSIS (DTA). REMOVE THE AIRCRAFT FROM SERVICE ON OR BEFORE 37,500 TOTAL AIRCRAFT FLIGHT CYCLES, UNLESSDR CALA2022120703310None · noneTHE REPAIR INCORPORATED VIA ECRA 5360-5360-01680 STATION 1440 FUSELAGE FRAME BETWEEN S-29R AND S-29L STRINGERS IS APPROVED AS TI ME LIMITED UNTIL 50,000 TOTAL AIRCRAFT FLIGHT CYCLES PENDING THE RESULTS OF A DAMAGE TOLERANCE ANALYSIS (DTA). REMOVE THE AIRCRA FTSDR 1E1R20221206R0151None · noneE2571-0005 80VU RACK SPECIAL DETAILED INSPECTION REPAIR.SDR CALA2022120703307None · noneTHE REPAIR INCORPORATED VIA EC/RA 5360-01678 BS 1420 FRAME, S24L & S27L. APPROVED AS TIME LIMITED UNTIL 25,600 TOTAL AIRCRAFT FLIGHT CYCLES PENDING THE RE SULTS OF A DAMAGE TOLERANCE ANALYSIS (DTA). REMOVE ACFT FROM SERVICERE 25,600 TOTAL AIRCRAFT FLIGHT CYCSDR CALA2022120703306None · noneR4 PAX DOOR OUTER SKIN AFT LOWER CORNER FOUND REPAIR WITHOUT RECORD DURING INSPECTION AS PER EA 5100-02345 OP019. REMOVED EXISTING DOUBLER AND PERFORMED NDT CHECK NO CRACK FOUND. PERFORMED REPAIR PER ECRA 5210-03239. REFER TO HAECO CARD NO.LDL 2754. DMG ITEM CSDR CALA2022120503297None · noneDURING FATIGUE CRITICAL STRUCTURE REINFORCING REPAIR SURVEY,R2 PAX DOOR OUTER SKIN SURFACE AFT LOWER CORNER FOUND EXISTING REPA IR DOUBLER REFER HAECO NON-ROUTINE NO.9498617 - ORIGINATED BY EM P V902615 EA5100-02345 REV E OP019 PEFORMED BY EMP V905037 FUS PAX SDR CALA2022120503296None · noneDURING FATIGUE CRITICAL REINFORCING REPAIR SURVEY,FWD CARGO DOOR OUTER SKIN SURFACE AFT LOWER EDGE FOUND EXISTING REPAIR DOUBLER REFER HAECO NON-ROUTINE NO.9498619. EA5100-02345 REV E OP019 THE EXISTING REPAIR DOUBLER AT FWD CARGO DOOR OUTER SKIN SURFACE AFT SDR DALA2022120707880Skin · noneDURING INSPECTION FOUND FCS REPAIR EXTERNAL SKIN DOOR LOCATED 17 INCHES UPPER EDGE AND 21 INCHES FWD EDGE AT AFT CARGO BAY. PERFORMED REPAIR INSTRUCTIONS ON EXTERNAL SKIN DOOR IAW SRM 52-00-01-2R AND SRM 52-00-01-2R-3 AND DWG 146A6110.SDR GTIA2022120536820None · noneDOUBLER BTW FR 81-83 STGR 2 RH RAF 3082720-02 CREATED FOR FURTHER EVALUATION-VERIFIED NR # 5001195484-0010 AND TC # 1003864642-0010 REPAIR WAS PERFORMED AS PER SPIRIT EO 5351- 2267 REVISION 00.SDR DALA2022120507768Power Supply · failedSHIP 3418 ASPSU BAD CLASS 1 FAULT. CORRECTIVE ACTION: REPLACED/INSTALLED ASPSU PER A330 AMM TASK 52-71. (9681247)SDR FDEA202212012954None · noneEXISTING MAJOR REPAIR, EXTERNAL DOUBLER FOUND ON THE LH WING OUTBD AILERON, INBARD END AND LOWER SURFACE REPAIR REQUIRES EVALUATION TO DETERMINE IF REPAIR IS IN ACCORDANCE WITH APPROVED DATA. REMOVED EXISTING REPAIR DOUBLER, FABRICATED AND REPLACED DOUBLERSDR FDEA202212012910None · noneEXISTING MAJOR REPAIR, EXTERNAL DOUBLER FOUND ON DROOP LEADING EDGE UPPER SURFACE REPAIR REQUIRES EVALUATION TO DETERMINE IF REPAIR IS IN ACCORDANCE WITH APPROVED DATA EXISTING REPAIR AT RH WIG DROOP LE AT BETWEEN STA IDLE=309-934-IDLE=329 LOCATION EVALASDR DALA2022120107683None · noneDOCUMENT WORK FOR LOG 2455907 ACCOMPLISH ER/A 602362-14. ACCOMPLISHED AND RECORDED WTBF MODIFICATION PER PRI 602362-14 REV 0, REV 1, REV 2, REV 3, AND REV 4 AND VERIFIED WORK ACCOMPLISHED WITH FINAL ER/A 602362-14AD REV C SECTION I. REPAIR IS CLASSIFIED MAJOR SDR DALA2022120707875None · noneFOUND THE BRACKET THAT IS INSTALLED ON THE AFT SIDE OF FRAME BS 1260 STRINGER 1, INTERFERING WITH INSTALLATION OF TWO SHEAR TIES. CORRECTIVE ACTION: REF ERA 604110-14. (2518542) NOT AN SDR.SDR DALA2022120207719Not Reported · crackedDURING H CHECK , WHILE EXECUTION OF JC 5716-01019-01 & 02 IN ORDER TO PERFORM INSPECTIONS REQUIRED BY SB A330-57-3129 REV 01, A CRACK INDICATION WAS DETECTED IN HOLES H260 LHS AND RHS. THE INITIAL DIAMETER OF HOLES WAS OF 0.348". AS PER JC AND AIB SB, WHEN CRASDR DALA2022120207717None · noneLIGHTNING STRIKE WINDOW 12 CUTOUT ON UPPER FUSELAGE. COMPLETED WITH ER/A #603881-14 REV. ORIGINAL MATCHES WITH ALL STEPS ON PRI # 603881-14 REV. 0 IT IS BEEN VALIDATED. PERFORMED REPAIR INSTRUCTIONS ON WINDOW 12 CUTOUT ON UPPER FUSELAGE AS PER ER/A 603881-14SDR DALA2022120207716None · noneLIGHTNING STRIKE WINDOW 13 RH CUTOUT ON UPPER FUSELAGE. COMPLETED WITH ER/A #603881-14 REV. ORIGINAL MATCHES WITH ALL STEPS ON PRI # 603881-14 REV. 0 IT IS BEEN VALIDATED. PERFORMED REPAIR INSTRUCTIONS ON WINDOW 13 RH CUTOUT ON UPPER FUSELAGE AS PER ER/A 603SDR DALA2022113007655None · noneSHIP 3228 NEED TO COMPLY WITH ERA 599238-14 REV A CRACK INSPECTION. CORRECTIVE ACTION: COMPLIED WITH INSPECTION. CONTINUE ON MONITOR. (2516893)SDR ASAA2022112840963None · noneCAPTAIN'S WEATHER DISPLAY DOES NOT REMOVE GROUND CLUTTER IN AUTO MODE. FIRST OFFICERS FUNCTIONS NORMALLY IN ALL MODES AND CAPTAINS WILL DISPLAY FO'S DATA WHEN TFR IS SELECTED. BOTH SIDES OPERATE NORMALLY IN MANUAL MODES. GROUNDED - YES. PERFORMED B737-900 FIM SDR DALA2022120107681None · noneAMOC AD 2021-22-17 ER/A 602362-14AD REV A INCLUDES INSTRUCTION FOR MODIFICATION OF THE WTBF ON 8129. SEC II TRACKS LIMIT FOR THE NEXT DUE AD 2021-22-17 INSPECTION. AMOC APPROVING TERMINATING ACTION MUST BE ACQUIRED PRIOR TO REACHING THIS LIMIT. *AMOC* REVISE ESDR QMLA2022120120081None · noneDURING PREFLIGHT PILOT FOUND CRACK IN TRAILING EDGE OF VERTICAL FIN UPPER AREA. AREA RECENTLY REPAIRED.SDR DALA2022120507762None · noneSHIP 3305 IN PREPARATION FOR ACCOMPLISHMENT OF 5310-01461-01, IT WAS IDENTIFIED THAT THE CAPITAL TOOL KIT CALLED OUT IN THE WORK INSTRUCTIONS, P/N FTIA330533273-1, FOR COLD WORKING DOES NOT ALIGN WITH THE DAL ATICTS TOOLING P/N. THE CAPITAL KIT CONTAINS STANDASDR DALA2022112807579None · noneSHIP 5641 AMOC FOR AD 2013-19-23. CORRECTIVE ACTION: REF ERA 603900-14 REV ORG. (2509572) NOT AN SDR.SDR CALA2022112503211None · noneCREW HEARD A LOUD BANG ON CLIMBOUT THROUGH 8000 FT NOISE NOTICED FWD OF DOOR 1LEFT . DISCOVERED BIRD STRIKE BELOW AND AFT OF L3 COCKPIT WINDOW. PERFORMED BIRD STRIKE INSP PER AMM 05-15-18-210-801. NO DAMAGE OR EVIDENCE OF ADDITIONAL BIRD STRIKES FOUND ON AIRCRSDR DALA2023012200464None · noneWORK CARDS REQUIRE REVISION FOR AA 2500-01853. ACCOMPLISH VA 97747MA REV IR IN CONJUNCTION WITH AA 2500-01853.SDR DALA2022112507525None · none(LOG 2508107) AA 2500-01854 REQUIRED REVISIONS. ACCOMPLISH VA 97746MA REV IR WITH AA 2500-01854.SDR DALA2022112507529None · none(LOG 2507629) AA 2500-01853 WORK CARDS REQUIRE REVISION. ACCOMPLISH VA 97747MA REV IR WITH AA 2500-01853.
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