JASC 5100
Service difficulty reports · 4,235
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 AALA202410282014None · noneAIRCRAFT IN BASE MAINTENANCE: MODIFICATION OF CENTER WING SECTION FRONT SPAR LEFT HAND UNDER WING LONGERON FROM STA 993 TO STA 1045, FROM S35L TO S37L IS DUE PER EO 5722B008. MODIFICATION OF CENTER WING SECTION FRONT SPAR LEFT HAND UNDER WING LONGERON WAS ACCOSDR AALA202410282356None · noneAIRCRAFT IN BASE MAINTENANCE: MODIFICATION OF CENTER WING SECTION FRONT SPAR RIGHT HAND UNDER WING LONGERON FROM STA 993 TO STA 1045, FROM S35L TO S37L IS DUE PER EO 5722B008. MODIFICATION OF CENTER WING SECTION FRONT SPAR RIGHT HAND UNDER WING LONGERON WAS ACSDR CALA2024102900957None · noneSET EMERGENCY WELS LIGHT SYSTEM INTO SLEEP MODE FOR MAIN BATTERY DISCONNECTED, REF AMM 33-51-00-04A-510A. REACTIVATED EMERGENCY WELS LIGHT SYSTEM PER AMM 33-51-00-04A-730A.SDR CALA2024102900945None · noneNEED TO PERFORM CONDITIONAL INSPECTION PER AMM 05-51-58-910-801-C1 PERFORMED CONDITIONAL INSPECTION PER AMM05-51-58-910-801-C1, UP TO AND NOT INCLUDING STEP D AND ON.PER TOMC MIGUEL. NO FURTHER STEPS REQUIRED. ALL TESTS PASS BUT PUT RT RECIRC FAN AND FWD GALLESDR IPXA2024120438050Skin · no discrepancyFWD CREW DOOR NEED INTERNAL SKIN CLEANING AND CIC . 89-471. CLEANED AREA IAW AMM 12-21-12. CIC APPLIED ON ORIGINATING TASK CARD# T3F18E002PX4W.SDR DXTA2024102800939None · no discrepancyOVERWEIGHT LANDING: DURING EMERGENCY RETURN TO TEB DUE TO BATT OTEMP L, WE LANDED OVER WEIGHT. WEIGHT AT LANDING WAS APPROXIMATELY 28,400 POUNDS. CORRECTIVE ACTION; PERFORMED HARD OR OVER WEIGHT LANDING INSPECTION AS PER CE680A CH, 05-50-00. FOUND NO ABNORMALISDR ABXA20241023202Pin · no discrepancyON PUSH OUT TOW BAR LOCK SNAPED DUE TO BYPASS PIN NOT INSTALLED AC RETURNED TO GATE AND MTX GROUNDED AC AND COMPLIED WITH INSPECTION OF THE NLG IAW B767 AMM 05-51-29 AND NO DAMAGE NOTED .MTX RETURNED AC TO SERVICESDR CALA2024102300899None · leakingSMOKE OR FUMES IN CABIN SOURCE UNKNOWN FA REP STRNG GAS ODOR AISLE BETWN ROWS 7.8.10 FL 320...DISSIPATE D LESS THAN 10 MIN.D/N RTN PICS ATTACHED AFTER DEBRIEF OF FLIGHT AND CABIN CREW SOURCE OF ODOR WAS ISOLATED TO RH STOWBIN AT ROW 7 AND WAS ATTRIBUTED TO A PSDR CALA2024102300900None · sparksPAX 9G DROPPED CELL IN PHONE SPARKED SMOKED PHONE IN CONT BAG ST ABLE DEVICE WAS FOUND IN XL THERMAL CONTAINMENT KIT. SMOKE/ODOUR QUESTIONNAIRE COMPLETED BY CAPTAIN AND PURSER. REF DANGEROUS GOODS PROGRAM MANUAL 05-09-01 AND GMM 05-30-06 SECTION 10 THERMAL CONSDR IPXA2024102149159Drain · noneADD SDR FOR EO-82173-JIC001 (FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R) COMPLETED SDR.SDR VNAA2024101630022Drag Angle · crackedLH FWD DRAG ANGLE IS CRACKED.SDR CALA2024102200892None · noneETOPS PRE-DEPARTURE SERVICE CHECK REQUIRED. ALL PERSONNAL INVOLV ED WITH ACCOMPLISHING THE PDSC MUST HAVE THEIR EMPLOYEE NUMBER E NTERED ON THIS LOG PAGE. COMPLETED ETOPS PRE-DEPARTURE CHECK AS REQUIRED. REF. TASK CARD NO. 42-0000-1-0002. AIRCRAFT IS RELEASED SDR IPXA2024102139954Drain · none(FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R). C/W EO-82173.SDR HNAA2024100101050Skin · noneEXISTING DOUBLER REPAIR FOUND ON FUSELAGE SKIN BTW FR26~27, S-33R~35R COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707, INSPECTION OF EXISTING DOUBLER REPAIR ON FUSELAGE SKIN BTW FR26~27SDR FDEA202410181595Skin · noneEXISTING DOUBLER REPAIR FOUND ON FUSELAGE SKIN BTW FR26~27, S-33R~35R COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707, INSPECTION OF EXISTING DOUBLER REPAIR ON FUSELAGE SKIN BTW FR26~27SDR REXA2024102200914Bracket · noneWHILE INCORPORATING SB 670SH-53-043 REV C, WE ARE UNABLE TO GET PROPER EDGE DISTANCE ON BOTH VOLUMETRIC FUSE BRACKETS SH698-75359-1S AND SH698-75355-1S DUE TO EXISTING AIRCRAFT FASTENER PITCH. COMPLIED WITH MHIRJ EO SH698-75359 SNIEO S11.SDR DXTA2024102100877None · no discrepancyVERTICAL STABILIZER: BIRDSTRIKE AT THE TOP OF THE VERTICLE STAB. BECAUSE OF THE LOCATION WE ARE UNABLE TO EVALUATE IF ANY DANAGE HAS OCCURRED. CORRECTIVE ACTION; COMPLIED WITH UNSCHEDULED BIRD STRIKE INSPECTION, NO BIRDS STRIKES OR OTHER DISCREPANCIES NOTED ASDR CALA2024110102778Skin · unknownRESKIN AFT CARGO DOOR (REF: AAR NR 1000020132)SDR UIEA2024101100978Stringer · noneREPAIR-EXISTING REPAIR ON STRINGER S-39R BETWEEN STA 400 AND STA 420.(<P>1. ACCOMPLISH EL T2024A53M-2334 REV.2. 2. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)SDR UIEA2024101100979Stringer · noneREPAIR-EXISTING REPAIR ON STRINGER S-39R BETWEEN STA 360 AND STA 400.(<P>1. ACCOMPLISH EL NO. T2024A53M-2253 REV.2. 2. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)SDR UIEA2024101100980Stringer · noneREPAIR-EXISTING REPAIR ON STRINGER S-40R BETWEEN STA 380 AND STA 400.(<P>1. ACCOMPLISH EL T2024A53M-2254 REV.1. 2. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)SDR UIEA2024101100981Stringer · noneREPAIR-EXISTING REPAIR ON STRINGER S-38R BETWEEN STA 360 AND STA 400.(<P>1. ACCOMPLISH EL NO. T2024A53M-2166 REV.3. 2. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)SDR DALA2024101109994Repair · noneSHIP 3144 EXISTING REPAIR ON HOLE 6 LOCATED ON FR16 LH SIDE CONTACT LIAISON ENG INEERING. CORRECTIVE ACTION: COMPLIED WITH ER/A 580937-14AD. (0602059)SDR SWIA202412241009None · noneREMOVE FRAME FS909 STGR 20L-25L TO FACILITATE STGR 20L REPAIR. (C-CHECK RO 12/21/2024) (FILED OPEN)REMOVED FRAME FS909 STGR 20L-25L AND INSTALLED NEW FRAME WITH NEW FRAME SPLICE REF REO 670-53-51-317 REV.-- DATED 2024-10-27, CRJ700 SRM 51-42-06-001-001-A01, DWSDR DALA2024101310017Flange · noneSHIP 3253 DISC: WEB HORIZONTAL FLANGE / CRACK. ER/A 616797-14AD REV A REQUIRES SECTION II FOLLOW-ON INSPECTIONS FOR CONTINUED AIRCRAFT AIRWORTHINESS. C/A: ER/A 616797-14AD REV A SECTION II FOLLOW-ON INSPECTIONS ARE REQUIRED ON OR BEFORE 55,400 TOTAL AIRFRAME FSDR EE4Y2024100820972Skin · no discrepancyDURING MAPPING PROCESS, THE COSTUMER REQUEST REVIEW THE TWO INTERNAL EXISTING REPAIRS, AFTER EXISTING DOCUMENTATION REVIEW AND INSPECTION OF THE AFFECTED AREA WE HAVE THE FOLLOWING COMMENTS: 1.ONLY ONE REPAIR HAS TECHNICAL RECORD UNDER ETD2010-190/01224 BUT DUSDR DALA2024100909897Repair · no discrepancySHIP 690 TRACKING PERMANENT REPAIR FOR ER/A 518895-14 REVISION B, SECTION III. CORRECTIVE ACTION: ACCOMPLISH PERMANENT REPAIR FOR ER/A 518895-14 REVISION B. (0597286)SDR IPXA2024100795837Rib · no discrepancy*SDR FILED OPEN* ADD SDR FOR EO-85445-JIC2 (B747-8: RH OUTBOARD ELEVATOR FRONT SPAR AND RIB REINFORCEMENT)SDR IPXA2024100795833Spar · no discrepancy*SDR FILED OPEN* ADD SDR FOR EO-85445-JIC1 (B747-8: LH OUTBOARD ELEVATOR FRONT SPAR AND RIB REINFORCEMENT)SDR REXA2024101500871Bracket · noneWHILE INCORPORATING SB 670SH-53-043 REV C, WE ARE UNABLE TO GET PROPER EDGE DISTANCE ON BOTH VOLUMETRIC FUSE BRACKETS SH698-75359-1S AND SH698-75355-1S DUE TO EXISTING AIRCRAFT FASTENER PITCH. FABRICATED AND INSTALLED BRACKETS IAW MHIRJ SNIEOS KSH670-35829-S8SDR SCNA20241203389Repair · temp repairWORK ORDER 90721, NR00007: REF W/O 87630 N/R 11 . TEMP REPAIR INSTALLED ON WING CENTER SECTION REAR SPAR VERTICAL PRESSURE DECK WEB AT STA. 663 BETWEEN RBL 40 AND 45.64 REQUIRES REPLACEMENT BEFORE 6000 FLT CYCLES OR 24 MONTHS. ( DAMAGE TOLERANCE EVALUATION FROSDR DALA2024100809784Slat Track · no discrepancyRH WING #5 SLAT TRACK LOWER AFT SURFACE REQUIRES NDT INSP. PER AMDS W/C 5742-01028-02B. ACCOMPLISHED EDDY CURRENT INSPECTION PER A220 ANDTP 51-01-353. NO CRACKS FOUND. (LP# 0592280)SDR DALA2024100809783Slat Track · no discrepancyRH WING #4 SLAT TRACK UPPER FWD SURFACE REQUIRES NDT INSP. PER AMDS W/C 5742-01028-02B. ACCOMPLISHED EDDY CURRENT INSPECTION PER A220 ANDTP 51-01-353. NO CRACKS FOUND. (LP# 0592273)SDR DALA2024100809781Slat Track · no discrepancyRH WING #2 SLAT TRACK UPPER FWD SURFACE REQUIRES NDT INSP. PER AMDS W/C 5742-01028-02A. ACCOMPLISHED EDDY CURRENT INSP. PER A220 ANDTP 1-01-353. NO CRACKS FOUND. (LP# 0592252)SDR DALA2024100809780Slat Track · no discrepancyLH WING #1 SLAT TRACK LOWER AFT SURFACE REQUIRES NDT INSP. PER AMDS W/C 5742-01028-02A. ACCOMPLISHED EDDY CURRENT INSP. PER A220 ANDTP 1-01-353. (LP# 0592245)SDR IPXA2024100444475Unknown · unknownSDR REQUIRED FOR AIR TURN BACK C/W SDR. REF BARCODED T3F18E005AD1T FOR WORK PERFORMEDSDR AALA202410038712None · noneAIRCRAFT IN BASE MAINTENANCE: DUE TO THE MAJOR REPAIR BEING ACCOMPLISHED ON THE FLIGHT DECK CENTER WINDSHIELD FRAMING THE LEFT HAND CONTINUITY FITTING AT FR 2 AND Y0 MUST BE REPLACED PER INSTRUCTIONS OUTLINED IN EA 356971. REPLACED LEFT HAND CONTINUITY FITTINGSDR AALA202410037759None · noneAIRCRAFT IN BASE MAINTENANCE: DUE TO THE MAJOR REPAIR BEING ACCOMPLISHED ON THE FLIGHT DECK CENTER WINDSHIELD FRAMING THE RIGHT HAND CONTINUITY FITTING AT FR 2 AND Y0 MUST BE REPLACED PER INSTRUCTIONS OUTLINED IN EA 356971. REPLACED RIGHT HAND CONTINUITY FITTISDR IPXA2024102287628None · none(FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R)SDR IPXA2024100287628None · noneFUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R) OK TO WORKSDR IPXA2024100929642Drain · noneADD SDR FOR EO-82173-JIC001 (FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R). ACCOMPLISHED SDR. PERFORM MODIFICATION & ACCOMPLISHED UPS EO-82173-JIC001SDR IPXA2024100829642Drain · none**SDR FILED OPEN** ADD SDR FOR EO-82173-JIC001 (FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R) ACCOMPLISHED SDRSDR DALA2024100209615Unknown · no discrepancy-AD RELATED- AMDS 5720-01103-01A: PERFORM STEP 13. SUMMARY NRC 00919: (ET) HFEC INSPECTION WAS PERFORMED. NO CRACKS WERE FOUND PER B717 CARD 5720-01103-01A, STEP 13 AND B717 DC/MD NDT SPM PART 6, 06-10-01.001. ASSOCIATED AA 5720-01103 ADDED FOR AC 9546. (LP #0SDR DALA2024100209614Unknown · no discrepancy-AD RELATED- AMDS 5720-01103-01A: PERFORM STEP 15 AND 16. SUMMARY NRC 00921: SEALANT WAS REMOVED AND APPLIED PER B717 AMM 20-60-01 PER AMDS 5720-01103-01A ALSO (ET) HFEC INSPECTION WAS PERFORMED. NO CRACKS WERE FOUND PER B717 CARD 5720-01103-01A, STEP 16 AND BSDR DALA2024100209613Unknown · no discrepancy-AD RELATED- AMDS 5720-01103-01A: PERFORM STEP 14. SUMMARY NRC 00920: (ET) HFEC INSPECTION WAS PERFORMED. NO CRACKS WERE FOUND PER B717 CARD 5720-01103-01A, STEP 14 AND B717 DC/MD NDT SPM PART 6, 06-10-01.001. ASSOCIATED AA 5720-01103 ADDED FOR AC 9546. (LP #0SDR DALA2024092609441None · noneSHIP 3160 OFFWING ESCAPE SLIDE ENCLOSURE LEFT LABEL INFORMATION OVERHAUL MISSING. CORRECTIVE ACTION: REPLACED OFFWING ESCAPE SLIDE ENCLOSURE LEFT ON SERVICEABLE. (0575934)SDR DALA2024092609462None · none(LOG 0576123) "A.A IN REF AMDS 5732-01015-01B-01: OBTAIN VA FROM FLEET ENGINEERING". SUMMARY OF NRC: 00599 VA 90996 REV C WAS ACCOMPLISHED IN CONJUNCTION WITH AA 5732-01015-01B-01.SDR DALA2024092609461None · none(LOG 0576156) " A.A IN REF AMDS 5732-01015-01A-01: OBTAIN VA FROM FLEET ENGINEERING". SUMMARY OF NRC:00598 VA 90996 REV C WAS ACCOMPLISHED IN CONJUNCTION WITH AA 5732-01015-01A-01.SDR DALA2024092709486None · noneSHIP 3155 CAP AND PLUG ALL PRESSURE AND RETURN LINES TO ALL 3 RUDDER SERVO CONTROLS TO FOM. CORRECTIVE ACTION: RECONNECTED ALL PRESSURE AND RETURN HYD. LINES GOING TO ALL 3 RUDDER SERVO CONTROLS REF. A319 AMM 27-24-51 AFTER MAINTENANCE WAS COMPLETED. LEAK CHECSDR FDEA202409231339Angle · crackedCOMPLY WITH EA 6-5310-T0380417 P1 JACKING AND SHORING THE AIRCRAFT AND REPAIRED THE DIAMETER DEVIATION HOLES COMPLIED WITH EA 6-5310-T0380417 P1 COMPLETED JACKING AND SHORING THE AIRCRAFT AND REPAIRED THE DIAMETER DEVIATION HOLES, TITLE: FUSELAGE - MAINFRA
Back to JASC 5100