JASC 5100
Service difficulty reports · 4,224
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 DXTA2025063004068None · no discrepancyJUST BEFORE ROTATION SPEED EXPERIENCED BIRD STRIKE. ON POSTFLIGHT NOTED SMALL BIRD REMAINS AT THE NOSE LANDING GEAR LEFT DOOR FORWARD HINGE. NO OBVIOUS DAMAGE BUT UNABLE TO CONCLUDE THERE WAS NO DAMAGE TO THE NOSE LANDING GEAR LEFT DOOR WITH THE GEAR DOWN. DIDSDR DALA2025062604794Angle · not reportedSHIP 9546 C/W LH WING BULKHEAD CLIP XRS164 PART MANUFACTURE ERA 626984-14 REV ORIG. CORRECTIVE ACTION: COMPLIED WITH LH WING BULKHEAD CLIP XRS164 PART MANUFACTURE ER/A 626894-14 REV A. (1043812)SDR DALA2025062504751None · noneER/A 627199-14AD REV A REQUIRES SECTION II FOLLOW-ON INSPECTIONS FOR CONTINUED AIRCRAFT AIRWORTHINESS. CORRECTIVE ACTION: C/W ERA 627199.SDR DALA2025062504750Repair · no discrepancyEXISTING REPAIR FOUND. CONTACT LIASON ENGINEERING FOR REPAIR PROCEDURES PRIOR TO FURTHER FLIGHT (R/H WING). PER ENGINEERING C/W ERA 619064-14AD REV B SEC II STEP 3. NO ISSUES NOTED.SDR DXTA2025062704029Seal · leakingDURING CRUISE WE NOTICED AN AUDIBLE SQUEAL COMING FROM THE EMERGENCY EXIT DOOR AREA. THERE WAS NO PRESSURIZATION ISSUES NOTED. AS WE DESCENDED THE SQUEAL WENT AWAY AROUND 27000 FEET WITH A PSI OF 8.6. NO VISIBLE ISSUES WITH THE EMERGENCY EXIT DOOR FROM INSISDR CALA2025062605921None · noneREF. LP 5268054. PER SRM 53-00-01-2R-12 SEC. 5(B), AFTER 50,000 TOTAL AIRPLANE CYCLES, PERFORM INTERNAL HFEC INSPECTIONS AT 15,0 00 FLIGHT CYCLE INTERVALS AROUND RIVET HEADS OF THE TWO OUTER RI VET ROWS OF THE INNER SKIN AND THE OUTER ROW OF THE OUTER SKIN. RESDR CALA2025062605920None · nonePER SRM 53-00-01-2R-12 SEC. 5(B), AFTER 50,000 TOTAL AIRPLANE CYCLES, PERFORM INTERNAL DETAILED VISUAL (DET) IN SPECTIONS AT 15,000 FLIGHT CYCLE INTERVALS OF THE REPAIR AREA FO R SKIN CRACKS AT THE OUTER PERIMETER ROW OF FASTENERS COMMON TO THE REPAIR DOUBLER SDR DALA2025081105990None · noneSHIP 9563 LOGPAGE CREATED TRACKING SECTION II INSPECTIONS TO ER/A 610356- 14AD. CORECTIVE ACTION: C/W ER/A 571712-14AD. (1037974)SDR AALA202506240936Unknown · noiseAIRCRAFT WAS GROUNDED: DURING ENG 2 START IN CLT WE HEARD A THUMP AND FELT A VIBRATIONIN THE RUDDER PEDALS. WE CHECKED THE CONTROLS AND DID NOT EXPERIENCE ANY THING ELSE OUT OF THE ORDINARY DURING TAXI OUT. AFTER DEPARTURE THE FO STATED THAT HE HEARD A BANG. SDR AALA202506232064Doubler · noneAIRCRAFT IN BASE MAINTENANCE: DUE TO THE MAJOT REPAIR BEING ACCOMPLISHED ON FR 16 RIGHT AND DOOR STOP #5 THE UPPER CORNER DOUBLER AT FR 16 RIGHT NEEDS TO BE REPLACED AS OUTLINED IN THE INSTRUCTIONS ON EA 363979. REPLACED UPPER CORNER DOUBLER PER EA 363979.SDR IPXA2025062722010Antenna · no discrepancySUPPORT STRUCTURE INSTALLATION FOR SATCOM HGA-7001 ANTENNA. PAPER CHECK OK.SDR CALA2025062605927Inspection · noneACCOMPLISH AN NDT INSPECTION OF THE BEAR STRAP AND INNER CHORD, IN THE AREA OF THE REPAIR (INSTALLED PER EA 5330-04213 OP 2), BEFORE 50,000 TOTAL AIRCRAFT CYCLES. AFTER THE ACCUMULATION OF 46,500 TOTAL AIRCRAFT FLIGHT CYCLES, BUT BEFORE 47,000 TOTAL AIRCRAFT FSDR FDEA202506201013Skin · wornAGING AIRCRAFT - EXISTING REPAIR ON DOUBLER EDGE AT FUSELAGE SKIN FWD CARGO DOOR CUTOUT AFT JAMB BS 1002 BETWEEN L38R TO L42R. (BLENDOOUT REPAIR). EXISTING REPAIR DOUBLER AT FUSELAGE SKIN FWD CARGO DOOR CUTOUT AFT JAMB BS 1002 BETWEEN L38R TO L42R EVALUATED SDR DALA2025063004853None · noneSHIP 9508 TRACKING FOR DTE FOR 24 MONTHS FROM DATE OF REPAIR APPROVAL. CORRECTIVE ACTION: C/W ERA ERA 626897-14 REV ORIGINAL. (1033207)SDR DALA2025063004855None · noneSHIP 9575 DTE, 624256-14AD. CORRECTIVE ACTION: ACCOMPLISH DTE FOR ERA 622844-14AD (1033944)SDR DALA2025062604791Inspection · noneSHIP 9575 AMOC, ERA 624259-14AD. CORRECTIVE ACTION: CURRENT AMOC APPROVAL IS LIMITED TO 24 MONTHS. ADDITIONAL ERA REVISION IS REQUIRED FOR AMOC APPROVAL BEYOND 17-JUN-2027 FOR ERA 624259-14AD (1033908)SDR FDEA202506190998Repair · not reportedCTR CARGO - TO REMOVE AND REPAIR EXISTING REPAIR AS REQUIRED ON T/C T 1-5330-T0301688 A P5.SDR YENA2025062500651Not Reported · not reportedFLT#1134, SJU-MCO.(AIRCRAFT DECLARED AN EMERGENCY AND PERFORMED AN AIR TURNBACK TO SJU) "BIRD STRIKE BEFORE V1" (SUPPLEMENTAL INFORMATION TO FOLLOW)SDR UIEA2025061200749Frame · unknownPER CUSTOMER INSTRUCTIONS IN REFERENCE AT BOEING RECOMENDATION REPLACE RH FRAME FITTING AND FAIL SAFE STRAP ASSY AT STATION 663.75 PER ENGINEERING DRAWING 144A2400-28 FRAME INSTALLATION.(<P>PERFORMED RH STA 663.75 FRAME FITTING AND SAFE STRAP REPLACEMENT AND BSDR UIEA2025061200751Stringer · nonePERFORM CUTTING AND SPLICING OF STRINGER 10 L/H FOR STA 663.75 FRAME FITTING ASSEMBLY REPLACEMENT AS PER BOEING REF COO-TLS -25-0061 DATED 08 MAY 25 AND BOEING DRAWING # 002A 0084 SHEET 14.(<P>PERFORMED SPLICE REPAIR OF FUSELAGE STRINGER 10LH BTWN STA 663.75 ASDR UIEA2025061200752Stringer · nonePERFORM CUTTING AND SPLICING OF STRINGER 14 L/H FOR STA 663.75 FRAME FITTING ASSEMBLY REPLACEMENT AS PER BOEING REF COO-TLS -25-0062 DATED 08 MAY 25 AND BOEING DRAWING # 002A 0084 SHEET 24.(<P><SPAN LANG="EN-US">PERFORMED SPLICE REPAIR OF FUSELAGE STGR 14L BTWSDR UIEA2025061200753Stringer · nonePERFORM CUTTING AND SPLICING OF STRINGER 10 R/H FOR STA 663.75 FRAME FITTING ASSEMBLY REPLACEMENT AS PER BOEING REF COO-TLS -25-0063 DATED 08 MAY 25 AND BOEING DRAWING # 002A 0084 SHEET 14.<BR>(<P>PERFORMED SPLICE REPAIR OF FUSELAGE STINGER 10 RH, BETWEEN STA SDR UIEA2025061200754Stringer · nonePERFORM CUTTING AND SPLICING OF STRINGER 14 R/H FOR STA 663.75 FRAME FITTING ASSEMBLY REPLACEMENT AS PER BOEING REF COO-TLS -25-0064 DATED 08 MAY 25 AND BOEING DRAWING # 002A 0084 SHEET 24. PERFORMED SPLICE REPAIR OF FUSELAGE STGR 14R BETWEEN B/S 663.75 AND BSDR DALA2025062504752None · noneDTA ER/A 626583-14 SECTION II MONITOR LOG REQUIRES DTA APPROVAL. CORRECTIVE ACTION: C.W ERA 626583.SDR FDEA202506170977Repair · no discrepancyEXISTING REPAIR ON RH O/B FLAP L/E SKIN BETWEEN RIB1 AND RIB2 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON RH O/B FLAP L/E SKIN BETWEEN RIB1 AND RIB2 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM57-50-00-201 FIG.208. EO 6-5100-7-5000SDR YENA2025061600614None · noneFLT#81, JFK-RNO. 'SEVERE TURBULENCE AT FLT 360 FOR 5 SECONDS A/C OVERSPEED 10 KTS;.' (SUPPLEMENTAL INFORMATION TO FOLLOW)SDR VNAA2025061711102Unknown · noiseAFTER TAKEOFF LOUD ELECTRIC CRACKLING/BUZZING NOISE FROM FO SIDE OF FLIGHT DECK / INSPECTED NOSE COMPARTMENTS/AVIONICS BAY FOR ANY LOOSE ITEMS. PRESSURIZED PLANE IAW CRJ700 AMM 21-31-00-910-801-A01-PSA TO ~4.0 DELTA AND USED RADIOS TO CONTACT TOWER. OPS CHECKSDR FDEA202506140976Flap · misrepairedEXISTING REPAIR ON LT O/B FLAP L/E SKIN BETWEEN RIB13 AND RIB15 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON LH O/B FLAP L/E SKIN BETWEEN RIB13 AND RIB15 WAS EVALUATED AND FOUND NOT IN CONFORMITY WITH A300-600 SRM57-50-00-201 FIG.208. RE-REPAIRESDR FDEA202506130975Repair · no discrepancyEXISTING REPAIR ON FUSELAGE STRINGER S52R BETWEEN FR67 AND 68 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON FUSELAGE STRINGER S52R BETWEEN FR67 AND 68 WAS EVALUATED AND FOUND IN CONFROMITY WITH A300-600 SRM53-10-14-201 FIG.201. EO6-5100-7-5000SDR FDEA202506130974Repair · no discrepancyEXISTING REPAIR ON FUSELAGE STRINGER S51R BETWEEN FR67 AND 68 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE STRINGER S51R BETWEEN FR67 AND 68 WAS EVALUATED AND FOUND IN CONFROMITY WITH A300-600 SRM53-10-14-201 FIG.201. EO6-5100-7-5000 SDR FDEA202506130973Repair · no discrepancyEXISTING REPAIR ON FUSELAGE STRINGER S50R BETWEEN FR67 AND 68 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE STRINGER S50R BETWEEN FR67 AND FR68 WAS EVALUATED AND FOUND IN CONFROMITY WITH A300-600 SRM53-10-14-201 FIG.201. EO6-5100-7-500SDR FDEA202506130928Seat Track · noneAGING AIRCRAFT - EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK BETWEEN STATION 1531 TO STATION 1551 X = -47.5 RIGHT HAND SIDE. EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK BETWEEN STATION 1531 TO STATION 1551 X = -47.5 SDR FDEA202506130927Skin · noneAGING AIRCRAFT - EXISTING REPAIR AT RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER STATION XOS 993.237 EXISTING REPAIR AT RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER STATION XOS 993.237 EVALUATED AND FOUND REPAIRED NOT IAW SDR QR9R2025061300001Torque Box · uncalibratedPART RECEIVED NEW FROM SUPPLY. DURING OPERATIONAL CHECK, FOUND TORQUE BOX ASSEMBLY WOULD NOT CALIBRATE.SDR YENA2025061700615Unknown · faultedFLT#312, ORD-BOS. 'UPON TOUCHDOWN A/C VEERED LEFT W/ NO INPUTS TO STEERING FROM RUDDER. A/C EXITED RUNWAY LEFT SIDE INTO GRASS; C/W INSPECTION, REF LOG PAGES 4321399-2 (COMPLIED WITH SPECIAL IRREGULAR INSPECTION PER AMP 05-51-20 STEP 4, NO DEFECTS NOTED, INSPESDR DALA2025061404501Unknown · unknownSHIP 3274 DISC: ON TAKEOFF, STRUCK RAISED ARRESTING CABLE @ APPROX. 80 KTS. C/A: PERFORMED WALKAROUND OF AIRCRAFT WITH NO DEFECTS NOTED. PERFORMED INSPECTION OF ALL WHEEL + TIRE ASSYS PER A320 AMM 32- 41-11. NO DEFECTS NOTED. (LP: 5712658)SDR AALA202506138559Fitting · no discrepancyAIRCRAFT IN BASE MAINTENANCE: DUE TO THE MAJOR REPAIR BEING ACCOMPLISHED ON THE FLIGHT DECK CENTER WINDSHIELD FRAMING THE LEFT HAND CONTINUITY FITTING FR 2 AND Y0 MUST BE REPLACED PER INSTRUCTIONS OUTLINED IN EA 363982. REPLACED LEFT HAND CONTINUITY FITTING PESDR AALA202506137071Fitting · no discrepancyAIRCRAFT IN BASE MAINTENANCE: DUE TO THE MAJOR REPAIR BEING ACCOMPLISHED ON THE FLIGHT DECK CENTER WINDSHIELD FRAMING THE RIGHT HAND CONTINUITY FITTING FR 2 AND Y0 MUST BE REPLACED PER INSTRUCTIONS OUTLINED IN EA 363982. REPLACED RIGHT HAND CONTINUITY FITTING SDR CALA2025061305537Slide · no discrepancy4R DOOR SLIDE PRESSURE GAGE IN THE RED FOUND SLIDE PRES OK FO SVC PER 25-66-01-206-041SDR CALA2025061305529None · no discrepancyPOSSIBLE BIRD STRIKE ON NOSE OF AIRCRAFT PERFOMED GVI OF NOSE OF AIRCRAFT. NO EVIDENCE OF BIRD STRIKE.SDR DALA2025061704568None · noneER/A 623771-14 REV B SECTION X 3D WIDGET REACTIVATION. ACCOMPLISHED ER/A 623771-14 REV B SECTION X 3D WIDGET REACTIVATION IN CONFORMANCE TO STC ST12040AT. (LP# 6728072)SDR CALA2025061305531None · no discrepancyDOOR 2L SLIDE PRESSURE IN RED ZONE, FOUND TO BE WITHIN LIMITS IN ACCORDANCE WITH AMM 25-66-01.SDR CALA2025061305530None · noneREMOVED FWD LH EXIT HATCH IAW AMM 52-21-11-000-001-A AND INSTALLED LOCKPIN ON LH INFLATION RESERVOIR IAW AMM 25-62-00-481-001-A INSTALLED FWD LH EXIT HATCH IAW AMM 52-21-11-400-001-A AND REMOVED LOCKPIN FROM LH INFLATION RESERVOIR IAW AMM 25-62-00-081-001-A INSDR CALA2025061205522None · none2L AND 2R SLIDE SIGHT GAUGES APPEAR ABOVE GREEN BAND PERFORMED DOOR 2L AND 2R INFLATION PRESSURE CHECK REFERENCE AMM TASK 25-66-02-206-001 SUBTASK 25-66-02-226-011 AND CHECK GOOD.SDR CALA2025061205492None · noneDOOR BUSTLE INSPECTION POST INSTALL REF LOG 5137002 DOOR 1L BUSTLE INSTALLED AS PER AMM 25-66-01-424-070 RII INSPECTION REQUIRED RII OF PASSENGER SERVICE DOOR BUSTLE C/O REF AMM: 26-66-01-404-072. VERIFIED INSTALLED CORRECTLY, NO OTHER SYSTEMS DISTURBED. RENDESDR DALA2025061004414None · noneSHIP 3417 NEED TO RE-INSPECT PER ERA 626805-14 REV ORIG. CORRECTIVE ACTION: COMPLIED WITH ERA 626805-14 REV ORIG. (1014351)SDR CALA2025061205490None · none1R DOOR BOTTOM RIGHT BRACKET WHICH HOLDS SLIDE ARM/DISARM IS LOO SE BRACKET IS SECURED. NO LOOSE PART. OPS CHECK DOOR. ARM & DISARM GIRTBAR CHECK GOOD. OK TO SERVICE.SDR CALA2025061205486Bottle · no discrepancyDOOR L1 SLIDE PRESSURE APPEARS LOW DOOR L1 SLIDE CONFIRMED WITHIN LIMIT.SDR CALA2025061205485Girt Bar · no discrepancyDOORS L1 AND L2 GIRT BARS DIFFICULT TO PLACE IN ARM POSITION CREW REPORTS BOTH L1 AND R1 DOOR SLIDES DIFFICULT TO ARM, ARMED BOTH SLIDES MULTIPLE TIMES WITH NO ISSUE. VERRIFED GIRT BAR RECESSES WERE CLEAN AND OPERATED SMOOTHLY, NO FURTHER MAINT ACTION NEEDED ASDR CALA2025061205483Slide · no discrepancyDOOR 1R SLIDE-PACK NEEDS INSPECTION. MATERIAL HANGS LOW. INSPECTED 1R DOOR. NO DEFECTS NOTED.
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