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 DALA2024032103600Window Frame · noneSHIP 3251 DISC: DTA MONITOR INSPECTION, FUSELAGE / FRAMES / LHS LATERAL WINDOW FRAME / REPLACEMENT. C/A: REFERENCE ER/A 589221-14.SDR DALA2024032103597Window Frame · noneSHIP 3251 DISC: DTA MONITOR INSPECTION, FUSELAGE / FRAMES / FRONT WINDOW FRAMES / REPLACEMENT. C/A: REFERENCE ER/A 589219-14. (LP: 1722093)SDR DALA2024032103596Window Post · noneDTA MONITOR INSPECTION, FUSELAGE / FR 4 WINDSHIELD CENTER POST LOWER ATTACHMENT / CONTINUITYFITTINGS / REPLACEMENT. C/A: REFERENCE ER/A 589220-14. (LP: 1722079)SDR DALA2024032103599Door Frame · noneSHIP 3239 DISC: DTA MONITOR INSPECTION, FUSELAGE / FRAMES / FR68 RH / DOOR STOP FITTING # 1 / LOWER INBOARD HOLE / CRACKS. C/A: REF ERA 589181-14.SDR DALA2024032103598Door Frame · noneSHIP 3239 DISC: DTA MONITOR FUSELAGE / FRAMES / FR68 RH / DOOR STOP FITTING # 1 / LOWER INBOARD HOLE / CRACKS. C/A: ER/A 589181-14. (LP: 1712233)SDR K11A2021012200039Bracket · corrodedLT WING OUTBOARD MIDFLAP BALLNUT SCREW ATTACHMENT BRACKET INBOARD HAS BOLT HOLE WITH CORROSION ON THE INNER DIAMETERS.SDR DALA2024032103618Frame Splice · unknownSHIP 5815 ERA 589505-14AD SECTION I ISSUED FOR STA 1640 RH FRAME SPLICE. CORRECTIVE ACTION: REF ERA 589505-14AD. (1708572)SDR DALA2021070203659Not Reported · crackedSHIP 3243 CRACKS FOUND PER ER/A 588847-14AD. CORRECTIVE ACTION: REPAIRED PER ER/A 588847-14AD. (1698347)SDR YV3R2021011100420Cover · crackedCUSTOMER REPORTED COVER ASSEMBLY P/N: A312-6 WAS CRACKED.SDR YV3R2021011100418Panel · crackedCUSTOMER REPORTED PANEL ASSEMBLY P/N: A305-5 WAS CRACKED.SDR P5CA2021010200001None · noneBIRD STRIKE HALFWAY DOWN RW 27 JUST PRIOR TO ROTATE. MCC DIRECTED TO RETURN TO CVG FOR MX INSPECTION. BIRD STRIKE AREA IS NOSE/CARGO DOOR (RT SIDE) STA 200/RWL 250 AND RWL 312. AFFECTED AREA HAS BEEN CLEANED AND INSPECTED, NO DAMAGE FOUND. ENGINES AND AIRCRAFTSDR YENA2021010400006Not Reported · crackedDURING HEAVY MAINTENANCE, CRACKS FOUND DURING INSPECTION SB A320-53-1254. REPAIRED PER SB A320-53-1263 & FLIGHTSTAR EA 20046 & RDAS 80854592/003/2020.SDR DALA2024032603812None · noneER/A 564948-14 HAS BEEN REVISED TO 'A'. FOLLOW ON ACTION IS REQUIRED. PERFORM SECTION II PERMANENT REPAIR WITHIN SOONER OF 2400FC OR 1 5000FH FROM 21DEC2020. REQUIRES P/N V53694032004 OR EFFECTIVE EQUIVALENT FOR PERMANENT REPAIR. ASSOCIATED ER/A 14-564948 ADDESDR FDEA202012093083Floorboard · damagedZONE 230 FLOOR BOARD 232KG IS BROKEN. FABRICATED ZONE 230 FLOOR BOARD 232KG ON VTMAE TRAVELER NR T20/1524715, IAW DWG SRZ-25-005 REVISION R. MAJOR REPAIR.SDR FDEA202012033018None · noneR/H HORIZONTAIL STAB TIP T/E DAMAGED BY A/C STRIKE ALL WORK COMPLETED ON R/H HORIZONTAL STAB FAIRING. PART INSTALLED MADE SERVICABLE BY COMPLETION OF EA G-5510-T0358408. O/K FOR SERVICE.SDR QXEA2020112300327Unknown · noiseFLIGHT ATTENDANT REPORTS LOUD METAL GRINDING NOISE ON THE L2 (AFT LEFT) DOOR DURING CRUISE AND CLIMB. NO PRESSURIZATION ISSUE NOTED IN FLIGHT DECK, DIVERTED. REMOVED FROM SERVICE. PERFORMED GVI OF ALL ACCESS AND SERVICE DOORS. FOUND ALL TO BE SECURE. PERFSDR UIEA2020111602403Unknown · noiseIMMEDIATELY AFTER TAKEOFF A DEAFENING ROAR MADE COMMUNICATIONS BETWEEN PILOTS AND BETWEEN PILOTS AND ATC ALMOST IMPOSSIBLE. UNABLE TO DETERMINE WHERE THE NOISE CAME FROM. ONCE THE CABIN DIFF PRESSURE REACHED 6.0 THE NOISE SLOWLY ABATED. GENERAL VISUAL OF AISDR P5CA2020100200327None · noneLIGHTNING STRIKE-SKIN, UPPER FUSELAGE EXTERNAL SURFACE STA 496, S-22R. ACCOMPLISHED THE REPAIR, IAW EI NO T2020A53M-2409 REV 1 AND REPAIR DATA ATTACHING WITH WO 4988234. CONDITION CHECK NORMAL AND JOB COMPLETED.SDR P5CA2020100200326None · noneLIGHTNING STRIKE-SKIN, UPPER FUSELAGE EXTERNAL SURFACE STA 500 S-21R TO S-22R. ACCOMPLISHED THE REPAIR, IAW EI NO T2020A53M-2409 REV 1. CONDITION CHECK NORMAL AND JOB COMPLETED.SDR SIMA20200923001Unknown · noiseHEARD INTERMITTENT WHISTLING NOISE IN CABIN AND COCKPIT, MOSTLY DURING CLIMB AND DESCENT. C/A: CLEANED MAIN CABIN DOOR SEAL, IAW EMB-145 AMM 52-00-04. PRESSURIZED A/C, IAW EMB-145 AMM 21-31-00. NO AIR LEAK NOTED AT THIS TIME.SDR Y2PA2020090220015Beam · corrodedDISCREPANCY: DURING C-CHECK AT KDHN, CORROSION WAS FOUND ON THE FORWARD CARGO LOWER FUSELAGE BEAM AT STATION 579R – 579L ON THE FORWARD AND AFT ENDS. CORRECTIVE ACTION: COMMERCIAL JET CUT OUT THE DAMAGED SECTION OF THE FLOOR BEAM AT STATION 579 RBL 38.0 TO SDR UIEA2020081701794Unknown · leakingFLUID LEAKING FROM TAIL SECTION AROUND APU VISUAL INSPECTION CLEANED THE APU AREA IAW MM 49-05-03. NO LEAKS NOTED AT THIS TIME.SDR FDEA202007311738None · nonePDIS 674 05-50 2102 31JUL20 MEM OPEN U LOGPAGES:3283567 RECEIVED A FLAPS SYS 1 AND 2 ON T/O. FLAPS AND SLATS FROZE AT 15/20. MAX SPEED IN THIS CONFIGURATION IS 205 KN. DID NOT GET THE SPEED TAPE AND OVERSPEED FLAPS TO 210 KN. 210 KN FOR ABOUTSDR UIEA2020072701620Unknown · noiseLOUD NOISE IN AFT GALLEY WITH APU AIR SELECTED ON(<P>PERFORMED DVI AND APU BLEED LEAK TEST IAW AMM 36-11-00, NO DEFECTS. REMOVED, INSPECTED, REINSTALLED APU BLEED CHECK VALVE IAW AMM 36-11-11, NO DEFECTS. INSPECTED APU AIR SUPPLY VALVE AND OPS TEST IAW AMM 36-SDR U2RA2020090840003Transfer Sys · damagedDURING ACCOMPLISHMENT OF TASK CARD 25-054-01-01, DAMAGE WAS NOTED ON FORWARD CARGO LOADING SYSTEM BALL TRANSFER UNIT. - ACCOMPLISHED REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC. ENGINEERING ORDER NUMBER 20287.SDR 9WGA2020061984301Unknown · noiseLOUD "POP" SOUND FOLLOWED BY EXTREME LOUD HUMING, DIVERTED TO ICN.SDR DALA2023111509409Unknown · unknownSHIP 1603 ER/A 575582-14 REV A SECTION III INSPECTION IS REQUIRED. CORRECTIVE ACTION: JOB ACCOMPLISHED AS PER ER/A 575582-14AD REV A SECTION III. A/C OK TO CONTINUE FOR SERVICE. (1533914)SDR YENA2020022400193Unknown · vibrationFT # 1460, FLL-BDL. DIVERTED TO MCO. ON CLIMB OUT ACCELERATING TO 335 KNT A/C PERFORMED MODERATED VIBRATION CLIMB TROUGH FL 240. VIBRATION WAS IN AFT OF A/C . LEVELED OFF FL 260 SLOWING DOWN TO 250 KTS, VIBRATING REDUCED BUT WAS STILL NOTICEABLE. SPED UP TO 33SDR DALA2020021401165None · noneSHIP 3230 - ATB - DUE TO AFT CARGO SMOKE INDICATION. CARGO FIRE EXTINGUISHER DISCHARGED BY CREW. SUSPECT SMOKE WAS CAUSED BY USE OF GSE EQUIPMENT NEAR THE CARGO DOOR PRIOR TO FLIGHT THAT RESULTED IN ACCUMULATION OF FUMES IN THE COMPARTMENT. CORRECTIVE ACTION: SDR 2A6D2020021002Cable · unknownTHE METAL FUEL CABLE FROM THE NEW CRFT. L/H INBOARD LOWER AFT LEG ON XFRAME, MAX DEPTH OF .009
APPROX LOCATION OF Z-2867 , X-3705, Y(-398)SDR GTIA202001243961Access Panel · damagedFOUND DAMAGE ON LH THS T/E ACCESS PANEL 334BB. RAF# 2457548-1-REVIEWED LTPR UC#1003062375-0010 AND HAS BEEN ACCOMPLISHED.EO 5510-2001 REV.00 DATE DEC.16,2019 WO#147942,ACCOMPLISHEDSDR FDEA2020012190167Unknown · noiseAIR TURN BACK. DURING CLIMB ( 14000-16000) A LOUD BANGING SOUND STARTED. WE WERE AT ( 280-290 KTS). SLOWED SOUND STOPPED. AROUND 250 KTS FO'S WINDSHIELD WIPER WAS VIBRATING OPERATED WINDSHIELD WIPERS IAW AMM 30-42-00-5. WINDSHIELD WIPERS OPERATED NORMASDR DALA2024060905895None · noneSHIP 3226 DISC: ER/A 558689-14AD HAS BEEN UPDATED TO REV. 'C' TO INCORPORATE NEW RDAS APPROVAL PER DTE REQUIREMENTS. THE SUBJECT REPAIR IS CLASS IFIED AS CAT. 'B' PERMANENT WITH FOLLOW ON INSPECTION. C/A: ACCOMPLISHED PRI 558689-14AD REV 0, AND 1,2 AND ER/A558SDR DALA2023012400567Skin · crackedDURING INSPECTION PER WC 5724-01010-41B, EM 5724-01010, AD 2018- 11-14, A CRACK WAS FOUND IN HOLE NO. 1 & 2. THE CRACKS WERE REPAIRED PER ER/A 584203-14AD PER AN AMOC FROM BOEING. THE AMOC REQUIRES REPETITIVE INSPECTIONS. ER/A 584203-14AD REVISED TO REV. B. SDR DALA2023011000192None · noneTRACKING FOR SECTION II: REPETITIVE INSPECTION - ERA 584135-14AD. ER/A 584135-14AD REVISED TO REV. A. ACCOMPLISH ER/A 584135-14AD REV A SECTION II INSPECTIONS.SDR CALA2019121602211Unknown · noiseCREW REPORTS LOUD NOISE UNDER FLOOR JUST AFT OF FLIGHT DECK DOOR. TRIED TURNING OFF RH AND LH RECIRC FANS NO HELP OPBLM HANN FLIGHT CREW REPORTED VERBALLY TO TECH SOUND COMING FWD OF FLT DECK DOOR. INSPECTED BOTH E&E COMPARTMENTS FOUND NO OBVIOUS DAMAGE WHEN RSDR UIEA2019112195934None · noneRADAR GROUND CLUTTER SUPPRESSION (GCS) SWITCH DOES NOT LOCK DOWN IN THE GROUND CLUTTER SUPPRESSION MODE. ALL MODES APPEAR TO OPERATE ON THE RADAR DISPLAY.(<P>THIS IS NON-LATCHING COMPONENT IAW S/B 34-45-32, PN 622-5130-005. PERFORMED OPS CHECK OF THE WX RADAR SDR IPXA2019112099161None · noneINSPECTION TYPE:SVFUSELAGE SKIN REPAIR BETWEEN FR 20-20A, STGR 38 R-40R REQUIRED IAW EO A300-5330-74688-P1REPAIRED PER UPS EO A300-5330-74688-P1SDR FDEA2019111532940None · nonePDIS 857 05-50 9138 13NOV19 SEA OPEN U LOGPAGES:3182688 FLEW INTO A VERY THIN, RAGGED VOLCANIC ASH CLOUD @ FL340 AT APPROX 2350Z NOTICED A SMALL, BUT STEADY EGT CLIMB AT A FIXED N1. EGT MAXED OUT AT 710 DEGREES BEFORE MAEUVERING OUT OF CLOUD.SDR HALA2019111400484None · noneATB - BIRD STRIKE ON DEPARTURE. RIGHT SIDE OF AIRCRAFT. // ACCOMPLISHED AMM TASK 05-51-14-200-803-A. FOUND EVIDENCE OF BIRD STRIKE ON INBOARD RH FLAP. WILDLIFE SVC COLLECTED EVIDENCE. CLEANED AREA. NO DEFECTS NOTED. A/C OK FOR SVC.SDR SIMA20191113001None · noneSTRONG ELECTRICAL SMELL ON THE FLIGHT DECK-C/A-VERIFIED WITH FLIGHT CREW THAT ELECTRICAL SMELL TO BE PAU EXHAST COMING INTO THE AIRCRAFT. NO DEFECTS NOTEDSDR REXA2019111421591Unknown · noneWHILE INCORPORATING SB607BA-57-020, CLEARANCE ISSUES WITH 1 FASTENER EACH SIDE UNDER FITTING.
COMPLIED WITH BOMBARDIER REO 690-57-21-322 REV. DATED 2019-11-08. WVAC EMP STAMP 771.SDR QXEA2019111300413None · noneCALL WAS RECEIVED FROM FLIGHT ATTENDANT "A" ADVISING THAT SMOKE WAS COMING OUT OF THE FORWARD GALLEY TRASH BIN. THE FORWARD GALLEY FIRE EXTINGUISHER WAS USED. THE SMELL OF SMOKE WAS DETECTED BY OUR FLIGHT ATTENDANT "A" AND A FIRST CLASS PASSENGER. REMOVED FROMSDR TX9220191122001Rivet · wrong partA BRIEF DESCRIPTION OF APPARENT VIOLATION:
THE MANUFACTURER (PRECISION FORM INC) HAS INCORRECTLY MARKED DIFFERENT RIVETS WHICH ARE VERY SIMILAR IN PHYSICAL APPEARANCE AND SOLD THEM TO KLX INC'S WHO THEN SOLD THEM TO STAECO. AND UNFORTUNATELY, SOME OF THESE RISDR YV3R201911220214Sensor · defectiveCUSTOMER REPORTED SENSOR ASSEMBLY P/N: G768-3 IS DEFECTIVE.SDR DALA2023011200256None · noneSHIP 6716 MONITOR INSPECTION LOG REFERENCE ER/A 582788-14. CORRECTIVE ACTION: REF ERA 582788-14. (1345686)SDR SWIA2019122747184Panel · crackedPANEL 261BLW CRACKED. REPLACED THE PANEL.SDR FDEA201911152806None · noneEXISTING REPAIR ON MDCC SEAT TRACK AT Y0 BETWEEN FR53 AND FR54 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MDCC SEAT TRACK AT Y0 BETWEEN FR53 AND FR54 WAS EVALUATED. THE REPAIR WAS PERFORMED PER EA: 6-5310-T0322392 A. THE REPAIR BETWEEN FR5SDR DALA2019112616918Unknown · unknownWORKING PRI 582587-14 C/W PRI 582587-14 REV0, REV1, REV2, REV 3. C/W ERA 582587-14 REV ORIG (1340022)SDR SIMA201910232002None · noneBIRD STRIKE ON T/O ROLL ON NOSE CONE AN 2 RH WING LEADING EDGE HIGH SPEED ABORT LESS THAN 110 KT-C/A-C/W BIRD STRIKE INSPECTION WORK CARD 05-200-07 NO DAMAGE NOTED OK FOR SERVICE
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