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 HNAA2018110800279None · nonePDIS 695 05-50 1614951 06NOV18 PWM CLOSE
SEVERE TURBULENCE ENCOUNTERED AT 29K FT. WITH A/C
CLIMB AND THEN PITCH DOWN.
FACT 06NOV18 21:50 PWM
C/W SEVERE TURBULENCE INSP. PER AMM 05-50-27. NO
DISCREPANCIES NOTSDR HNAA2018110800278None · nonePDIS 648 23-60 1699793 06NOV18 ROC CLOSE
POSSIBLE LIGHTING STRIKE.
25549 00 PCS
FACT 06NOV18 13:26 ROC
PERFORMED LIGHTING STRIKE INSPECTION I/A/W AMM
05-50-01. NO DEFECSDR DALA2018110706530None · none(AIRCRAFT 664, L/P 0816032) WHILE WORKING WORK CARD 2330-01349-01D FOUND INTERFERENCE WITH EXISTING REPAIR DOUBLER INSTALLED PER ER/A 091884 AT FS560 AT STR2R AND FLUSH REPAIR PER SRM 53-00-01 BETWEEN FS 560-580 AND STR 2R-2L. ACCOMPLISH PRI 571779-14 FOR INSTSDR DALA2018110706528None · none(AIRCRAFT 664, L/P 0816016) WHILE WORKING WORK CARD 2330-01349-01D FOUND INTERFERENCE WITH EXISTING REPAIR DOUBLER INSTALLED PER SRM 53-00-01 BETWEEN FS 640-660 AND STR 2L-2R. ACCOMPLISH PRI 571780-14 FOR INSTRUCTIONS. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTINSDR DALA2018110706527None · none(AIRCRAFT 664, L/P 0815872) WHILE WORKING AA WORK CARD 2330-01349-01D IDENTIFIED AREA OF PREVIOUS REWORK 5.75" AFT OF AREA OF #4 LUG DOUBLER, 1.150" AFT OF BS 620 AND 5.30 " INBD OF S3-R, MAX DEPTH IS 0.005". SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARYSDR DALA2018110706526None · none(AIRCRAFT 664, L/P 0815870) WHILE WORKING WORK CARD 2330-01349-01D FOUND INTERFERENCE WITH EXISTING REPAIR DOUBLER INSTALLED PER SRM 53-00-01. ACCOMPLISH PRI 571786-14 FOR INSTRUCTIONS. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL SDR DALA2018110706522None · none(AIRCRAFT 664, L/P 0815697) DURING ACCOMPLISHMENT OF EO 2330-01349-01D FOUND INTERFERENCE WITH EXISTING SKIN REPAIRS AT BS452,STR 2R,BS445 STR3R,BS473 STR 3R WITH D36197-22007 ACL LIGHT INSTALLATION. ACCOMPLISH PRI571782-14 FOR INSTRUCTIONS. ACCOMPLISH PRI 571SDR DALA2018110706521None · none(AIRCRAFT 664, L/P 0815708) WHILE WORKING WORK CARD 2330-01349-01D FOUND INTERFERENCE WITH EXISTING REPAIR DOUBLER INSTALLED PER SRM 53-00-01 BETWEEN FS 580-600 AND STR 3R. ACCOMPLISH PRI 571785-14 FOR INSTRUCTIONS. ACCOMPLISHED PRI 571785-14 REV 0,1,2,3. COMPSDR ASOA201811081511Skin · mechanic errorREF BOMBARDIER TUCSON AIR CENTER JOB# 2743351 DURING JACKING OF AIRCRAFT NOSE JACK PAD SLIPPED, DENTING FUSELAGE SKIN AT APPROX. FS 280.00, BL0. C/A REPAIRED PER BOMBARDIER REO 601R-53-11-3320 REV -- DATED 2018-10-29SDR SWIA201845187None · noneOUTBOUND PILOT REPORTS A DENT IN THE RT. WING LEADING EDGE DUE TO A BIRD STRIKE. FLIGHT # 7389 FO: 10/29/2018. CLOSED REMOVED AND REPLACED RT O/B LEADING EDGE SKIN IAW SRM.SDR DALA2018111606642None · noneDURING LIGHTNING STRIKE INSPECTION, FOUND DAMAGE AND CORROSION TO THE RIGHT ELEVATOR AND TAB ASSEMBLY. ALSO FOUND CORROSION TO THE TORSION BAR SPINES. REPLACED THE UPPER AND LOWER ELEVATOR SKINS PER SRM 51-70-13-2R AND REPLACED THE TORSION BAR PER CMM 27-30-1 SDR DALA2023080106223Unknown · unknownSHIP 3357 INSPECTION OF #1 LHS DOOR CORNER. CORRECTIVE ACTION: REF ER/A 572476-14AD. (0797591)SDR DALA2019102206065None · noneSHIP 652 ERA 571971-14 SECTION I WAS ACCOMPLISHED IN MSP 23OCT18. FOLLOW ON ACTION IS REQUIRED FOR SECTION II. CORRECTIVE ACTION: REF ERA 571971-14 REV A. COMPLETE DTE RESULTS, SECTION II DT INSPECTIONS IS ADDED.SDR SWIA2018110245210Panel · gougedPANEL 326CR GOUGED. REPAIRED THE PANEL IAW REO 601R-55-32-384.SDR HNAA2018092600229None · nonePDIS 634 05-51 1691272 21SEP18 ILM CLOSE
BIRD STRIKE R/H SIDE OF NOSE AREA, NO EVIDENCE OF IN
GESTION NOTICED
21584 00 EK
FACT 21SEP18 00:22 ILM
ACCOMPLISH DETAILED VISUAL INSDR DALA2018113006947None · none(LP# 0674165) /ERA 570292-14AD HAS BEEN UPDATED TO REV A TO INCORPORATED NEW RDAS APPROVAL. PERMANENT WITH NO FOLLOW ON ACTION REQUIRED. . 28NOV CLOSED LOG AND REMOVED MONITOR.SDR 2018FA0000294Unknown · noiseAFTER TAKEOFF THRUST WAS SET AND AIRCRAFT WAS ROLLING AFT 20KTS A VERY STRONG NOISE OR EXPLOSION WAS HEARD ON THE RT SIDE OF THE ACFT NO ECAMS / COD 52.SDR S3SA202001220000Actuator · contaminatedPILOTS REPORTED INERTIAL SEPARATOR TRIPPING CB. FAILED PART REMOVED AND FOUND FULL OF LIQUID (WATER) NO SIGN OF EXTERNAL DAMAGE OR POINT OF WATER INTRUSION.SDR YENA201806143246Control Unit · failedAT 18,000 FT, ECAM DATALINK ATSU FAULT WITH STRONG ELECTRICAL ODOR IN THE COCKPIT. PULLED CIRCUIT BREAKERS L-15 & 16 AND THE ODOR DISSIPATED SLOWLY. ACCOMPLISHED TSM 24-00-00-810-803-A, IDENTIFIED ATSU COMPUTER TO HAVE THE BURNING ODOR INTERNALLY. NO DEFESDR DALA2018053103718Cable · deterioratedKEVLAR CABLE FOUND DETERIORATED BE LT GROMMET. R/I KEVLAR CABLE PER MD88 AMM 53-53 & WORKCARD 5350-01077-0101 STEP 14. (LP4247373)SDR AALA2018051649033Unknown · unknownAFTER TAKEOFF, AT ROTATION, A LOUD BANG TO LEFT. BANG WAS ALSO ON LEFT SIDE. ENGINE INSTUMENTS LOOKED GOOD, CONTINUED TAKEOFF. GEAR RETRACTED NORMALLY. EMERGENCY DECLARED DUE POSSIBLE BLOWN TIRE. FLIGHT LANDED WITHOUT FURTHER INCIDENT, NO TIRE DAMAGE FOUND. SDR WVER201807160245Panel · gougedPANELS 443BB AND 443BT ARE GOUGED ON AFT END. REPAIRED PANELS 443BB AND 443BT IAW EC/TC EO CL600-2C-10-54-L05664 AND EO CL600-2C10-54-L05665.SDR SWIA2018033044442Not Reported · dentedDENT FOUND AT BS 258, STRINGER 20R. DRESSED BACK THE DENT TO ORIGINAL CONTOUR IAW REO.SDR SWIA2018033044441Not Reported · dentedDENT FOUND AT BS 690, STRINGER 23L. REPAIRED IAW SRM AND REO.SDR SWIA2018033044439Not Reported · dentedDENT AT BS 271, STRINGER 22R. REPAIRED .SDR SIMA20180223001Unknown · unknownDURING CLIMBOUT, A LOUD CRACKELING SOUND WAS HEARD IN THE FLIGHT DECK. SOUNDED LIKE FROM EXTERIOR, LASTED APPROXIMATELY 5 MINUTES. PERFORMED GVI INSPECTION OF AIRCRAFT ACCESS PANEL, MLG DOORS, HUMP SEALS, WIPERS, BONDING JUMPER, STATIC WICKS FLIGHT DECK PASDR AALA201801239015Shade · damagedEMERGENCY EXIT DOOR WINDOW SHADE ON SEAT 14F DAMAGED. REPLACED EMERGENCY EXIT DOOR WINDOW SHADE ON SEAT 14F PER AMM 25-21-12.SDR SIMA20171224001None · noneAFTER CLIMBING THRU 1000 FT AGL, CAPTAIN AND FIRST OFFICER BEGAN SMELLING FUMES AND WITHIN SECONDS A MASTER WARNING SMOKE AFT LAV MESSAGE. RAN EPC AND APPRC CHECKLISTS. MESSAGE WENT AWAY AND RETURNED BRIEFLY AFTER COMPLETION OF CHECKLISTS. MESSAGE WENT AWAYSDR GTIA2017121802294Unknown · unknownLOUD WHISTLE SOUND IN COCKPIT DURING FLIGHT, APPEARS TO COME FROM OVERHEAD JUST FWD OF COCKPIT DOOR. PERFORMED AN INSPECTION OF ALL COCKPIT WINDOW SEALS NO DEFECTS NOTED. LUBRICATED THE SLIDING WINDOWS IAW AMM 56-12-11SDR CALA2017121604475None · noneSUPPORT TASK-EXISTING DOUBLER REPAIR AT FR60 STR 41L-STR 42L REQUIRES EVALUATION & ARCHIVE. REMOVED EXISTING REPAIR AT FR 60 STRINGER 41L-42L. FABRICATED NEW DOUBLER MADE OF CLAD 2024-T3-.080" PER SRM 53-41-11-300-037 PARA 2 (A) FIGURE 20129. THIS REPAIR REQUISDR FDEA201712163403None · noneNEED TO ACCOMPLISH SKIN REPAIR ON L/H CENTER FLAP BETWEEN RIB #26 AND #27 FOR ACCESS TO RIB REPAIR. REPAIRED PER SRM 57-50-00, FIG 205, DOUBLER INSTALLED ON L/H CENTER FLAP BETWEEN RIBS 26 AND RIB 27, BETWEEN THE REAR SPAR AND STRINGER 2.3 BOTTOM SKIN IAW SDR FDEA201712163402None · noneNEED TO ACCOMPLISH SKIN REPAIR ON L/H CENTER FLAP ADJACENT TO RIB #12 FOR ACCESS TO RIB REPAIR. REPAIR PER SRM 57-50-00, FIG 205, DOUBLER INSTALLED ON L/H CENTER FLAP BETWEEN RIBS 11 AND 12 AND BETWEEN THE REAR SPAR AND STRINGER 2.1, BOTTOM SKIN IAW SRM 51SDR FDEA201712163401None · noneNEED TO ACCOMPLISH SKIN REPAIR ON R/H CENTER FLAP ADJACENT TO RIB #19 FOR ACCESS TO RIB REPAIR. REMOVED FASTENERS FOR REPAIR DOUBLER ON RIGHT WING CENTER FLAP RIB #19, FABRICATED REPAIR DOUBLER IAW SRM 57-50-00, INSTALLED REPAIR DOUBLER IAW SRM 51-40- 21,SDR FDEA201712163398None · noneNEED TO ACCOMPLISH SKIN REPAIR ON R/H CENTER FLAP ADJACENT TO RIB #25 FOR ACCESS TO RIB REPAIR. REMOVED FASTENERS FOR REPAIR DOUBLER ON CENTER FLAP AT RIB #25 R/H, FABRICATED DOUBLER REPAIR IAW A300-600 SRM 57-50-00 PAGE 217, LOCATED AND DRILLED DOUBLER IASDR 2018F00053None · noneREPAIR OF OVERSIZED DOOR ROD PIN HOLE IN RIGHT MAIN LANDING GEAR TRUNNION. REPORT NO. S-680-0230/02RD DATED DECEMBER 6, 2017 WITH FAA FORM 8100-9 DATED DECEMBER 8, 2017.SDR 2018F00052None · noneREPAIR OF DRILL STARTS IN RIGHT WING LEADING EDGE SKIN. REPORT NO. S-680-0230/03RD DATED DECEMBER 6, 2017 WITH FAA FORM 8100-9 DATED DECEMBER 7, 2017.SDR 2018F00051None · noneMAIN CABIN DOOR SPADE DOOR HINGE ATTACH NUT-PLATES. MEMO 10436M1 DATED DECEMBER 7, 2017.SDR FDEA201712123382None · noneREPAIR ASSESSMENT: LOWER FUSELAGE SKIN, STA. 1781, LONG. 41R, AFT LOWER SIDE OF CENTER CARGO DOOR JAMB, HAS AN EXISTING REPAIR DOUBLER. DOT 17. EXISTING MAJOR REPAIR WAS PREVIOUSLY INSTALLED PER SRM 53-50-00 FIG. 26 SH.3 VOL.1. REF. E.A. 8-5100-T0336013 "RSDR FDEA201712113360None · noneEXISTING DOUBLER STA 1743-1768 S6L-8L DOES NOT COMPLY WITH SRM REPAIR. ALL WORK ACCOMPLISHED IAW FEDEX EA F-5330-T0337293 P1 FUSELAGE - PLATES & SKINS- FUSELAGE SKIN REPAIR BETWEEN STA 1743 AND 1768 BETWEEN STRINGERS S-6L AND S-8LSDR SIMA20171211001None · noneSERVICE DOOR "EMER" LIGHT REMAINS LIGHTED IN OFF + ARMED POSITION-C/A-FOUND LIGHTS TO BE COURTESY LIGHTS IN THE ON POSITION. NO DEFECTS NOTED IN EMERGENCY LIGHTING SYSTEM.SDR DALA2017121208608None · noneSHIP 7006 2L DOOR WILL NOT CLOSE PROPERLY. CORRECTIVE ACTION: RE-CYCLED DOOR SEVERAL TIMES. OPS CK GOOD (4016484).SDR AALA20171211002None · noneAIRCRAFT WAS GROUNDED. FOUND COCKPIT OVERHEAD ELECTRONIC DEVICE SWITCH CAUSING EMERGENCY LIGHTS TO COME ON. TESTED EMERGENCY LIGHTS PER AMM 33-51-00-710-009-A. NO PED SWITCH FIN # 190RH MUST BE IN OFF POSITION IS A PRE REQUISITE FOR EMERGECNY EXIT LIGHTS TEST.SDR DALA2017120808493None · none(AIRCRAFT 684, L/P 0329050) EXISTING DOUBLERS INTERFERE WITH LUG DOUBLERS 5,6 BETWEEN FR 620 THRU 660 STR 2R. REFERENCE NR CARD 17 FOR CORRECTIVE ACTION REF SCEPTER LOG NBR 0329034.SDR DALA2017120808492None · none(AIRCRAFT 684, L/P 0329034) C/W PRI 563966-14. COMPLIED WITH PRI 563966-14 ( REV 2 ) A. RECEIVED FINAL ER/A 563966-14 REV A.SDR FDEA201712063357None · noneREPAIR ASSESSMENT: UPPER FUSELAGE, MAIN DECK , AT APPROXIMATE STA. 905, RBL 47, HAS AN EXISTING SEAT TRACK PLUG REPAIR. DOT 94. EXISTING SEAT TRACK REPAIR PREVIOUSLY INSTALLED IN REFERENCE TO SRM 53-70-00 FIGURE 2, SHEET 1,2.SDR FDEA201712063355None · noneREPAIR ASSESSMENT: UPPER FUSELAGE, MAIN DECK, AT APPROXIMATE STA. 1331, RBL 47, HAS AN EXISTING SEAT TRACK PLUG REPAIR. EXISTING SEAT TRACK REPAIR PREVIOUSLY INSTALLED IN REF. TO SRM 53-70-00 FIGURE 2 SHEET1SDR FDEA201712053366None · noneREPAIR ASSESSMENT: LEFT WING, FIXED LEADING EDGE, UPPER SURFACE, AT APPROX. STA. XFS 235, HAS AN EXISTING DOUBLER, APPROX. 10X7 INCHES. DOT 17. REPAIR WAS PREVIOUSLY INSTALLED PER SRM 57-10-00 FIG. 15A SH.1 VOL.1 . REF E.A. 8-5100- T0336014 "REPAIR CATALOG SDR FDEA201712053356None · noneREPAIR ASSESSMENT: LEFT WING, INBOARD FLAP, LOWER SURFACE, AT APPROX. STA. XIFH 190, HAS AN EXISTING SKIN SPLICE REPAIR. DOT 22. EXISTING REPAIR PREVIOUSLY INSTALLED IN REFERENCE TO SRM 57-10-00 FIG 3.SDR ASAA2017113022728Frame · mechanic errorL1 DOOR FWD LOWER PANEL BELOW LOWER GUIDE PLATE ISOLATER FASTENERS DRILLED THROUGH AND INSTALLED INTO FRAME. GROUNDED - YES. REPAIRED STA 303.9 FRAME INNER CHORD IAW ASA EA 800-53EA-19551 REV 00 DATED 29NOV17. THIS IS A CATEGORY B REPAIR WITH STAGE 1 AND 2 APPSDR HALA2017113000287None · noneATB - MEDICAL EMERGENCY
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