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 RMXA 145ECNone · odorSHORTLY AFTER LIFTOFF, CREWMEMBER SEATED IN THE PATIENT CARE SEAT NOTICED WHAT WAS DESCRIBED AS POSSIBLY A FAINT BURNING ELECTRICAL ODOR. COULD NOT SMELL IT FROM THE FRONT AND THE NURSE IN BACK STATED IT WAS NOT VERY NOTICEABLE. ABOUT THAT TIME I TURNED ON THSDR BCYR20110217001Planetary Gear · crackedOPERATOR DISCOVERED A LARGE CRACK THROUGH THE WEB SECTION OF THE PLANETARY GEAR WHILE CONDUCTING MPI EXAMINATION AS A NORMAL PART OF THE REPAIR PROCESS. MFG HAVE BEEN NOTIFIED AND THEY WILL BE CONDUCTING A FULL METALURGICAL INVESTIGATION.SDR QXEA2011021500156None · noneMOD - ACCOMPLISH TASK CARD 6-34-147 TCAS ANTENNA DOUBLER INSP/SELF LEVEL GREEN APPLICATION. REMOVED LOWER TCAS ANTENNA AND COMPLIED WITH INSP AND NECESSARY REPAIRS IAW TASK CARDS 6-34-147, 6-53-973. INSTALLED TCAS ANTENNA IAW AMM 34-43-11-400-801 AND 34-43-SDR DXTA2011020904458Unknown · unknownTHERES IS A LOUD RUMBLE/ KNOCKING NOISE COMING FROM UNDERNEATH THE FLOORBOARD NEAR THE EMERGENCY EXIT WHILE IN TURBULANCE. (CREW DEBRIEF HAPPENED ON CLIMBOUT, LIGHT TO MODERATE TURBULANCE)SDR IXXA110006OUnknown · unknownDURING TAKEOFF ROLL, ACFT PULLED HARD LEFT. CREW WAS UNABLE TO MAINTAIN DIRECTIONAL CONTROL WITH FULL RT RUDDER. THEY ABORTED TAKEOFF AND RETURNED TO BLOCKS WITH OUT FURTHER INCIDENT. MX INSPECTED THE NOSE GEAR, WHEELS, BRAKES, NOSE WHEEL STEERING, NOSE STEESDR FDEA201101130170Wedge · damagedNR 5 L/E SLAT UPPER SURFACE, T/E WEDGE, BETWEEN INBD TRACK AND MID-TRACK HAS A TEMP. REPAIR OF A DENT. (CURRENT SRM REQUIRES PERM. REPAIR AT C-CHECK) REPAIRED NR5 SLAT IAW SRM 57-43-02, REPAIR NR1. FINAL REPAIR DIMENSION IS 3" DIAMETER. THE SLAT ASSY P/N ISDR DALA1504530981Unknown · unknownINSTALLED TEMP REPAIR IAW SRM 57-06B-D, FIG 14, UPPER WING L/E SURFACE CRACK.SDR FDEA201010194104Unknown · multiple failSIGNIFICANT STATIC DISCHARGE EXPERIENCED WHICH RESULTED IN MOMENTARY WX RADAR FAILURE AND LVL ONE "ENG FIRE AGNT LO". AGT 1 LO & AGT 2 LOW ILLUMINATED FOR ENGS 1 & 3 AND AGT 2 LO ILLUMINATED FOR ENG 2. COMPLIED WITH LIGHTENING INSPECTION REF MM 05-53-00-6SDR GTIA1000049Unknown · unknownAIR RETURN DUE TO ENCOUNTERING BIRD STRIKE, JUST AFTER T/O AT ABOUT 2000' WE HIT A FLOCK OF BIRDS. THERE WERE AT LEAST 6 HITS. AUTO THRUST DISENGAGED AND WE HAD A SLIGHT FLAP OVERSPEED AT FLAPS 1, ALSO GOT AN ECAM ON AIRSPEED DIFFERENCE, ALL PROBLEMS CLEARED FSDR 2010FA0001098Rotor · damaged(HZ3R) PUMP ASSY HAD SEVERE DAMAGES, SUCH AS GEAR BUSHING BROKE AND GEAR SHAFT DISASSEMBLE FROM NORMAL POSITION (STILL MOUNTED IN THE ROTOR) STATOR ASSY - SEVERE DAMAGES FROM ROTOR ASSY END BELL ASSY - LINER HAS BEEN DISINTEGRATED. LINER MOUNTING STRUCTURES ASDR 2010FA0001050Spar · crackedDURING ANNUAL INSP, REF AD 2000-25-02 R1, FOUND 3 AREAS WHERE THERE WERE CRACKS. ACFT IS NOT AIRWORTHY UNTIL THE SPAR IS REPLACED.SDR CA100916009Lever · mismarkedCUSTOMER REQUIRED C6FS2665-1, RECEIVED FROM MFG (1)EA C6FS3648-1 MISIDENTIFIED AS C6FS2665-1 FROM WO-76093/1. MFG HAS CONTACTED END USER TO HAVE THE PART RETURNED AND REPLACED.SDR DALA1502930978Longeron · unknownNOSE LONGERON REPAIRED IAW EA 09-069225-12.SDR HALA2010090100386Unknown · unknownETOPS SIGNIFICANT SYS - RAN PACKS AND TROUBLESHOT PACK SYS IAW FIM 21-51-00-1 ALL CHECKS WERE NORMAL-PACK TEMP CONTROLLER BITE HAD NO FAULTS-OK FOR SERVICE. RAN PACKS AND TROUBLESHOT PACK SYS IAW FIM 21-51-00-1. ALL CHECKS WERE NORMAL-PACK TEMP CONTROLLER BISDR IPXA10B62831Skin · unknownINSPECTION TYPE:C, SURVEY SEQ NR 580-F1-10 FUSELAGE BETWEEN BS 737 TO 756 & S33-38R EXISTED REPAIR TO BE REMOVED & ACCOMPLISHED THE NEW REPAIR. SKIN REPAIR IAW SRM 53-00-01, REPAIR 16, DETAIL II, REV 57. FINAL CUTOUT IS 16.25"X2.875" AT OVERLAPPING & 27.25"X1SDR 2010FA0000847Pump · failed(HZ3R) PUMP ASSY HAD SEVERE DAMAGES, SUCH AS GEAR BUSHINGS BROKE AND GEAR SHAFT DISASSEMBLED FROM NORMAL POSITION (STILL MOUNTED IN THE ROTOR). STATOR ASSY - SEVERE DAMAGES FROM ROTOR ASSY. END BELL ASSY - LINER HAS BEEN DISINTEGRATED. LINER MOUNTING STRUCSDR FDEA201008092884Unknown · unknownFLT 5034/06, FLIGHT CREW STATED THE ACFT ENCOUTERED SEVERE TURBULENCE AT 10,000 FT MSL. THE CAPTAIN REPORTS LOOSING 700 FT AND EXPERIENCING MOMENTARY STICK SHAKER. COMPLY WITH MM 05-51-01-6 EXCESSIVE MANEUVER OR TURBULENCE - OVERLOAD CONDITON. COMPLY WITH ASDR CA100709001Ferrule · defective(CAN) MS9382-04 FERRULES WERE DIMENSIONALLY DEFECTIVE.SDR FDEA201007082404Unknown · multiple failAFTER TAKEOFF GEAR WOULD NOT RETRACT USING SYS 2 OR SYS1. TRANSPONDER REPORTED INOP BY DEPARTURE. ACFT WOULD NOT PRESSURIZE. AUTO THROTTLES INOP. AUTOPILOTS WHEN SELECTED ON , REVERTED TO CONTROL WHEEL STEERING. BOTH CAPT AND F/O SPD TAPE WENT AWAY. WHESDR HNAA2010050100150Unknown · dentedSCRATCH IN DENT NR 53-11- AT X 342.3 BETWEEN STA 19 AND 19S. MADE .25 CUTOUT REPAIRED DAMAGE IAW EO8-53-10-0211.SDR DALA1503659228Bulkhead · unknownSTA 1344, TEE BULKHEAD REPAIR BETWEEN L30 & 23R, SRM 53-10-02.SDR 2010FA0000316Unknown · unknown(SPUY) DURING ROUTINE C-CHECK INSPECTION, R & R EXISTING REPAIR LOCATED FS 1180.000- 1200.000, L36 WITH A REPAIR IAW APPROVED DATA (SRM) LIST ANY AND ALL REINSPECTIONS ON THE NON-ROUTINE.SDR FDEA201003190934None · noneBS1640 FLOORBEAM PREVIOUS REPAIR INTERFERES WITH PTF CONVERSION. (IN-PROCESS).SDR 2010FA0000284None · none(JGVR) THESE CONTROL COLUMNS WERE REMOVED FOR ACCESS FOR AN EPIC INSTALLATION. UPON REINSTALLATION, IT WAS NOTICED THAT IF THE AILERON PUSH-PULL TUBE BOLT IS INSTALLED IAW ILLUSTRATION IN THE MM AND THE IPC. THE THREADS FROM THE BOLT WILL CONTACT THE CONTROLSDR QXEA2010031800176None · noneSTRONG POSSIBLE ELECTRICAL SMELL IN FWD CARGO P4. PERFORMED GVI OF FWD CARGO COMPARTMENT, NO DEFECTS FOUND. INSPECTED CARGO DOOR INSIDE & OUT, FOUND SMELL COMING FROM SEALANT AROUND DOOR SUROUND OF OUTSIDE CARGO DOOR. SEALANT APPEARS TO BE FRESHLY APPLIED. SDR 2010FA0000133Pivot · crackedPIVOT CRACKED AT INBD END OF SHAFT.SDR DL75E100229Unknown · unknownWHEN ADVANCING THROTTLES BOTH BLEEDS TRIPPED OFF AND LT BOOST PUMP STARTED FLASHING.SDR QMLA2009121009048Bolt · misinstalledFOUND HARDWARE INSTALLED INCORRECTLY CAUSING: WEAR IN THE HYD PACK AND MOUNT HOLES. CRACKS IN THE CABIN FLOOR AND CROSS STRUCTURE SUPPORT IN THE CABIN CEILING UNDER THE HYD PACK. AFT HYD MOUNT ON DECK HAS WEAR IN THE BUSHING HOLES 0.100" THICK, FITTING DAMAGESDR DXTA2009110603850Unknown · vibrationAFTER COMPLETEING A MISSED APPROACH AND RETRACTING THE GEAR, FLAPS AND LANDING LIGHTS, WE EXPERINCIED A PERODIC VIBRATION THAT WOULD LAST 5-15 SEC AND WAS AUDIBLE. WE COULD NOT DETERMINE ITS ORIGIN. JACKED AND SWUNG GEAR MAINS AND NOSE, INSPECTED DOORS FOR SESDR DXTA2009110203837None · noneBIRDSTRIKE LEFT SIDE OF RADOME, PITOT TUBE, AOA VANE, ENGINE INLET AND FAN BLADES. UPON IMPACT, MACH TRIM FAIL LIGHT ILLUMINATED AND YELLOW IAS BOXES ILLUMINATED ON BOTH PFD'S. AIRSPEED SPLIT OF 10KTS PILOT TO CO-PILOT. SMALL FEATHERS ARE VISIBLE ON LEFT PITOTSDR FDEA200909223356None · noneACFT DOES NOT MATCH DWG 657N3160 FIG E, SHT 2 , REV D AT STA 1640, LBL 60 -62. DWG SHOWS 4 EA EXISTING FASTENERS BUT THE ACFT HAS 5 EA AT STA 1640; LBL 60 - 62. REPAIR WAS ACCOMPLISHED, DUE TO DISCREPANCY EFECTING THE PTF CONVERSION, ON MAE MOD W/C 118350399SDR FDEA200909223354None · noneACFT DOES NOT MATCH DWG NR 657N3160 FIG. E , SHT 2, REV D AT STA 1640, RBL 60 - 62. DWG SHOWS 4 EA EXISTING FASTENERS, BUT THE ACFT HAS 5 EA AT STA: 1640; RBL 60 - 62 WAS REPAIRED IAW EA 757-5362-16-F2251, DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION ON MASDR FDEA200909223353Structure · unknownUPPER CORD AT BL-0;900 -1080 HAS AN EXISTING FASTENER BREAKING OUT ON EDGE OF CHORD AT STA 925. IF THIS HOLE IS PICKED-UP IN THE NEW CHORD PN 111N5207-10 WE WILL DUPLICATE THE PROBLEM. AT STA 925, BL-0 , EA 757-5345-16-F2226, WAS COMPLIED WITH AND ACCOMPLISSDR FDEA200909213344Seat Track · unknownSEAT TRACK 657N3318-7 AT LBL 24.5, STA 1280 - 1320 CAN NOT BE LOCATED AND DRILLED DUE TO ACFT CONFIGURATION NOT MATCHING UP TO DWG AT STA 1280 LBL 24, PREVIOUSLY INSTALLED REPAIR CONFLICTED WITH ACCOMPLISHMENT OF PTF CONVERSION. NEW REPAIR WAS ACCOMPLISHED ATSDR FDEA200909213343Floorbeam · noneBS 377, LBL 58, FLOORBEAM HAS EXISTING REPAIR THAT INTERFERES WITH INSTALLATION OF RCB, ON MOD W/C 118350472RCBR08 AND W/C 118350431AZ2R03. REMOVED PREVIOUS REPAIR AND CUT OUT DAMAGED AREA AT BS 377, LBL70-RBL 34, IAW SRM 53-00-51, FIG 201, REPAIR NR 3. FABRISDR FDEA200909173322Seat Track · noneSEAT TRACK 657N3318-7 AT LBL 45.5, STA 1280 - 1320 CAN NOT BE LOCATED AND DRILLED DUE TO ACFT CONFIGURATION NOT MATCHING UP TO DWG AT STA 1280 - 1320, SEAT TRACK REPAIR WAS ACCOMPLISHED, DUE TO WRONG CONFIGURATION EFFECTING THE PTF CONVERTION, ON MAE W/C NRSDR ASOA200900968Unknown · unknownWORKING APU DOOR POS UNKNOWN PER DML 478158-3SDR ZY8R20110722001Unknown · noisyEXPERIENCED AUDIBLE NOISE APPROX 2 HOURS IN TO ACOUSTIC ANALYSIS TEST FLIGHT THAT WAS BOTH HEARD AND DETECTED. THE NOISE RESONATED BETWEEN 70 AND 80 DECIBELS. AFTER REDUCING ENGINE POWER AND DESCENDING TO A LOWER ALTITUDE, THE NOISE WAS NO LONGER PRESENT.SDR C2XA09IA184Hose · leakingDURING CLIMB THE CREW REPORTED A PACK 1 FAIL WHILE THE NR 2 PACK WAS ON MEL. ACFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MX REMOVED AND REPLACED THE 4 HOSES ON THE TORQUE MOTOR DUAL VALVE, OPS AND LEAK CHECKED WITH NO DEFECTS, AND THE ACFT WAS APPSDR HALA2009071700309None · noneETOPS SIGNIFICANT SYSTEM - LEFT ENGINE IDLE N2 69%. RIGHT ENGINE IDLE N2 70%. OPERATION OF NR 1 AND 2 ENGINES CHECKS OK. WITHIN LIMITS PER AMM 71-01-02.SDR FDEA200906302423Floorbeam · unknownWHILE DELETING PARTS IAW PTF AFT PALLET MOD WC PRODUCTION FOUND NUMEROUS HOLES AT STA 1640, STA 1640, LBL60-67, WHERE FLOORBEAM AND FRAME MEET AT FRAME. REPAIR WAS ACCOMPLISHED DUE TO THE DISCREPANCY EFFECTING THE PTF CONVERSION, MAE MOD W/C 118350399EZ2R02,SDR FDEA200906302421Skin · unknownAPPROX STA 660, STR 6L TO 14L, EXCESSIVE CONTOUR MISMATCH. AT BS 660, S6L- S14L, NEW DSS SKIN WAS ACCOMPLISHED DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION, ON MAE MOD W/C 118250277DSSR06, AMD MAE EA 757-5331-16-F2064, REV A, MAY 27, 2009. THIS NON ROUTINSDR FDEA200906302420Splice · unknownDUE TO EXISTING FASTENER PITCH ON WEB AT STA 1620-1640, LBL 60. SPLICE CHANNEL (657N4308-1) CAN NOT BE LOCATED. REPLACED SPLICE CHANNEL (657N4308-1) BET STA 1620- 1640, LBL 60. ACCOMPLISHED DUE TO DISCREPANCY AFFECTING THE PTF CONVERSION ON MAE MOD W/C 1183SDR KNNA20090007Unknown · unknownJUST AFTER ROTATION, A LOUD BANG WAS HEARD AND THE ACFT HAD A NOTICEABLE SHUDDER. DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. LANDING WAS UNEVENTFUL. SUSPECTED BIRD STRIKE.SDR E0X2009F00001Unknown · unknownACFT WAS ON A REPOSITIONING FLIGHT. APPROX 1 HR INTO FLIGHT, ATC CLEARED ACFT FROM FL390 TO FL240 AND A DESCENT OF 3000 FPM WAS STARTED. AFTER A FEW MINUTES INTO DESCENT BOTH PFD AIRSPEED TAPES FAILED. CREW NOTED POSSIBLE PITOT TUBE ICING AND TOOK EMERGENCYSDR 2009FA0000448Check Valve · failedUPON INTERNAL INSP OF HEADER TANK FOUND SWING CHECK VALVES FRAGMENTING AND FALLING OFF PARENT MATERIAL. REPLACED ALL SWING VALVES WITH NEW AND CLEANED INTERNAL HEADER TANK. (K)SDR FDEA200904021164None · noneAT BEGINNING OF TAKEOFF ROLL, LEVEL 1 'UNABLE RNP'. DURING TAX IN, RNP INDICATED 4.1 NM. UPON RETURN TO BLOCKS, TROUBLESHOT THE CFDS/ MCDU: NO FAULTS PERFORMED RTS ON ADIRU 1,2, AND 3; MMR 1,2, AND 3, NO FAULTS FOUND. ALL TESTS PASS POS REF SHOWS 6 SAT'S, GSDR HALA2009022300064Unknown · unknownETOPS SIGNIFICANT SYSTEM, AT 4+30 IN FLIGHT MX LEVEL EICAS MSG IDG OUT TEMP DISPLAYED IDG OUT L 57 R 82 RISE L 9 R RISE 9. TROUBLESHOT PER FIM 24-20-00. NO FAULTS NOTED OK FOR SERVICE.SDR C8GA20090052Plenum · corrodedWHILE IN HEAVY MAINTENANCE IT WAS NOTED THAT THE LT RAM AIR PLENUM LOWER WING SKIN CORRODED AT PREVIOUS REPAIR. REMOVED FASTENERS, CLEANED CORROSION, PERFORMED NDT INSPECTIONS AND REWORKED FASTENER HOLES. FABRICATED DOUBLER, TRIPLER, QUADRUPLER AND FILLER. SDR SWIA200921251Bearing · corrodedC-CHECK, RIGHT THRUST FITTING CORRODED AT SPHERICAL BEARING. REPLACED PER AMM.
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