JASC 5100
Service difficulty reports · 4,243
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 YENA2024030500341Skin · noneDURING HEAVY MAINTENANCE: WINGS / LH WING / TE UPPER REAR SKIN / RIB 14-16 & RIB 17-19 / SRM DEVIATION - PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)SDR CALA2024030500641None · noneBIRD STRIKE ON TAKE OFF PICS ADDED. CLEANED AND INSPECTED BIRD STRIKE AREA PER AMM 05-51-18. NO DAMAGE NOTED OR DISCOVERED. BIRD DID NOT STRIKE OR DAMAGE THE RADOME.SDR DALA2024030102912None · noneSHIP 3361 OVERWEIGHT LANDING AT 419,200 LBS. TOUCHDOWN AT 300 FPM. CORRECTIVE ACTION: PER A330 05-51 TRIGGER CODE 4000 NO INSPECTION REQ'D. NORMAL LANDING. JOB COMPLETE. THIS WAS DUE TO #1 ENG FAILURE CAUSING THE OVERWEIGHT LANDING. (5279733)SDR DALA2024030402916None · noneSHIP 3271 DISC: CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR SKIN LOCATED FR48 TO FR5 0 BTW STR2L TO STR5L ON UPPER FUSELAGE. C/A: COMPLIED WITH ERA 575822-14 REV ORIGINAL, VALIDATED ER/A 575822-14 REV A AND MATCHES ERA 575822-14 REV ORIGINAL EXISTING ALTERATSDR DALA2024030102884None · noneSHIP 3271 DISC: CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED FR 72 AT STR 26 R AT LOWER FUSELAGE. C/A: COMPLIED WITH ERA 575822-14 REV ORIGINAL, VALIDATED ER/A 575822-14 REV A AND MATCHES ERA 575822-14 REV ORIGINAL EXISTING REPAIR INSTALSDR DALA2024030102883None · noneSHIP 3271 DISC: CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOC FR34 T O FR35 BTW STR33L TO STR34L AT LOWER FUSELAGE. C/A: COMPLIED WITH ERA 575822-14 REV ORIGINAL, VALIDATED ER/A 575822-14 REV A AND MATCHES ERA 575822-14 REV ORIGINAL EXISTING SDR DALA2024030102882None · noneSHIP 3271 DISC: CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR LOWER SILL LOCATED FR68 AND STR23R AT AFT GALLEY AREA. C/A: COMPLIED WITH ERA 575822-14 REV ORIGINAL, VALIDATED ER/A 575822-14 REV A AND MATCHES ERA 575822-14 REV ORIGINAL EXISTING REPAIR INSTALLED SDR DALA2024030102881None · noneSHIP 3271 DISC: CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOC. FR25 TO FR26 BTW STR42R TO STR43L AT LOWER FUSELAGE. C/A: COMPLIED WITH ERA 575822-14 REV ORIGINAL, VALIDATED ER/A 575822-14 REV A AND MATCHES ERA 575822-14 REV ORIGINAL EXISTING SDR DALA2024030102880None · noneSHIP 3271 DISC: CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR SKIN LOCATED FR52 TO FR5 3 BTW STR1 L TO STR1R ON UPPER FUSELAGE. C/A: COMPLIED WITH PRI 575822-14 REV 0, VALIDATED ER/A 575822-14 REV ORIGINAL MATCHES PRI 575822-14 REV 0. EXISTING ALTERATION INSTASDR DALA2024030102879None · noneSHIP 3271 DISC: CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR SKIN LOCATED FR35 TO FR3 6 BTW STR2L TO STR2R ON UPPER FUSELAGE. C/A: COMPLIED WITH ERA 575822-14 REV ORIGINAL, VALIDATED ER/A 575822-14 REV A AND MATCHES ERA 575822-14 REV ORIGINAL EXISTING ALTERATSDR DALA2024030102878None · noneSHIP 3271 DISC: CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOC. FR56 TO FR57 BTW STR40L TO STR44L AT LOWER FUSELAGE. C/A: COMPLIED WITH ERA 575822-14 REV ORIGINAL, VALIDATED ER/A 575822-14 REV A AND MATCHES ERA 575822-14 REV ORIGINAL EXISTING SDR DALA2024030102877None · noneSHIP 3271 DISC: CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR SKIN LOCATED FR58 TO FR5 9 BTW STR18L TO STR21L ON UPPER FUSELAGE. C/A: COMPLIED WITH ERA 575822-14 REV ORIGINAL, VALIDATED ER/A 575822-14 REV A AND MATCHES ERA 575822-14 REV ORIGINAL EXISTING ALTERSDR DALA2024030102876None · noneSHIP 3271 DISC: CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR SKIN LOCATED FR48 TO FR5 0 BTW STR2R TO STR5R ON UPPER FUSELAGE. C/A: COMPLIED WITH ERA 575822-14 REV ORIGINAL, VALIDATED ER/A 575822-14 REV A AND MATCHES ERA 575822-14 REV ORIGINAL EXISTING ALTERATSDR DALA2024030102875None · noneSHIP 3271 DISC: CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR SKIN LOCATED FR58 TO FR5 9 BTW STR18R TO STR21R ON UPPER FUSELAGE. C/A: COMPLIED WITH ERA 575822-14 REV ORIGINAL, VALIDATED ER/A 575822-14 REV A AND MATCHES ERA 575822-14 REV ORIGINAL EXISTING ALTERSDR DALA2024030102874None · noneSHIP 3271 DISC: CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR SKIN LOCATED FR29 TO FR3 0 BTW STR1L TO STR1R ON UPPER FUSELAGE. C/A: COMPLIED WITH ERA 575822-14 REV ORIGINAL, VALIDATED ER/A 575822-14 REV A AND MATCHES ERA 575822-14 REV ORIGINAL EXISTING ALTERATSDR DALA2024030102873None · noneSHIP 3271 DISC: 1 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED FR 69 TO FR70 BTW STR31R TO STR32R AT LOWER FUSELAGE. C/A: COMPLIED WITH ERA 575822-14 REV ORIGINAL, VALIDATED ER/A 575822-14 REV A AND MATCHES ERA 575822-14 REV ORIGINAL EXSDR DALA2024030102872None · noneSHIP 3271 DISC: CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED FR 36 TO FR37 BTW STIFFENER1 TO STIFFENER 2 IN CENTER FUEL TANK. C/A: COMPLIED WITH ERA 575822-14 REV ORIGINAL, VALIDATED ER/A 575822-14 REV A AND MATCHES ERA 575822-14 REV ORISDR DALA2024030102871None · noneSHIP 3271 DISC: CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR LOWER SILL LOCATED AT LE VEL STR23R FR66 AT AFT GALLEY AREA. C/A: COMPLIED WITH ERA 575822-14 REV ORIGINAL, VALIDATED ER/A 575822-14 REV A AND MATCHES ERA 575822-14 REV ORIGINAL EXISTING REPAIR INSTSDR DALA2024022902826None · noneSHIP 3171 AIRPLANE IS COVERED IN VOLCANIC ASH INBOUND CREW REPORTED SULFER SMELL FAN BLADES IN BOTH MOTORS ARE SEVERELY DAMAGED. CORRECTIVE ACTION: C/W BORO SCOPE OF #1 AND #2 ENGINES. FOUND NO EVIDENCE OF VOLCANIC ASH INGESTION PER A319 AMM 72-00 INSTALLED BOSDR YENA2024030500311None · noneDURING HEAVY MAINTENANCE: EVALUATED EXISTING REWORK. P1 LOC. AT FR52L PLUS 4 INCH AND STR28L PLUS 3.500 INCH AND P2 LOC. AT FR52L PLUS 8.500 INCH AND STR28L PLUS 4 INCH AND FOUND WITHIN ALLOWABLE DAMAGE LIMITS I.A.W A321 NEO SRM 53-41-11-283-024 FIGURE 001 (SHSDR YENA2024022900302None · noneDURING HEAVY MAINTENANCE: EVALUATED EXISTING REWORK. P1 LOC. AT FR52L PLUS 4 INCH AND STR28L PLUS 3.500 INCH AND P2 LOC. AT FR52L PLUS 8.500 INCH AND STR28L PLUS 4 INCH AND FOUND WITHIN ALLOWABLE DAMAGE LIMITS I.A.W A321 NEO SRM 53-41-11-283-024 FIGURE 001 (SHSDR DALA2024022702697None · noneSHIP 1605 DURING PERFORM WIFI DE-MOD THE SIZE OF THE DOUBLER IS TOO SMAL. CORRECTIVE ACTION: THE DOUBLER FABRICATED AND INSTALLED AS PER PRI: 615977-14 REV.0 . COMPARED AND COMPLIED WITH ER/A: 615977-14 REV.ORIGINAL. NO DEVIATION. (0220272)SDR AALA202403075669Rib · noneAIRCRAFT IN BASE MAINTENANCE: MODIFICATION OF AILERON CLOSURE RIB AT RIGHT WING REAR SPAR STATION 1230 DUE. ACCOMPLISHED RIB MODIFICATION PER EA 351007. THIS ACCOMPLISHES BOEING SB B787-81205-SB570027-00.SDR DALA2024022602691Unknown · unknownSHIP 6805 DURING GOGO DEMOD FORWARD CROWN AREA FOUND ERA STICKER # 590389- 14 HOLE SIZE .305 . CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 005-0001:2330-01322- 21D/001 00004 ACCOMPLISHED ER/A 590389-14 REV B. (0216355)SDR DALA2024022702745None · noneNRC #600-045. AD/EM-EO TASK - RH WING W/C 5720-01102-02B STEP 6 DETAILED INSPECTION CARRIED OUT FOUND SATISFACTORY. STEP 25 CURRENTLY NO SEALANT REPAIR N/A STEP 12, COMPLIED VA #101182ADMA REV A. IN CONJUNCTION WITH W/C 5720- 01102-02B. ASSOCIATED AA 5720-0SDR DALA2024022702742None · noneNRC #500-043. AD/EM-EO TASK - LH WING W/C 5720-01102-02A STEP 6 DETAILED INSPECTION CARRIED OUT FOUND SATISFACTORY. STEP 25 . CURRENTLY NO SEALANT REPAIR N/A STEP 12, COMPLIED VA #101182ADMA REV A. IN CONJUNCTION WITH W/C 5720- 01102-02A. (LP# 0215614)SDR UIEA2024022100104Floorbeam · noneDEVIATION- DURING PERFORM SB 4453A087 PART 2, AT R/H STA 340 UPPER DECK FLOOR BEAM STRAP HAVE 1 EA FASTENER CAN'T REMOVED.(<P>1) PERFORM JOB IAW EI T2024A53M-248, SEQUENCE A REV 0 2) ACCOMPLISHED EI T2024A53M-248, REV-1 3) JOB COMPLETED AND COND CHK NML.</P>)SDR UIEA2024022100105Floorbeam · noneDEVIATION- DURING PERFORM SB 4453A087 PART 2, AT R/H STA 500 UPPER DECK FLOOR BEAM STRAP HAVE 2 EA FASTENER CAN'T REMOVED.(<P>1) PERFORM JOB IAW EI T2024A53M-249, SEQUENCE A REV 0 2) ACCOMPLISHED EI T2024A53M-249, REV 1 3) JOB COMPLETED AND COND CHK NML.</P>)SDR UIEA2024022100106Floorbeam · noneDEVIATION- DURING PERFORM SB 4453A087 PART 2, AT L/H STA 340 UPPER DECK FLOOR BEAM STRAP HAVE 1 EA FASTENER CAN'T REMOVED.(<P>1) PERFORM JOB IAW EI T2024A53M-246, SEQUENCE A REV 0 2) ACCOMPLISHED EI T2024A53M-246, REV 1 3) JOB COMPLETED AND COND CHK NML.</P>)SDR R61A2024022200083None · noneNOSEWHEEL STRUCK A FOX AT ROTATION SPEED, 132KTS. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. PERFORMED GVI OF NLG AND DOORS, NO DAMAGE NOTED.SDR AALA202402236124None · noneAIRCRAFT IN BASE MAINTENANCE: MODIFICATION OF CENTER WING SECTION RIGHT HAND FRONT SPAR LOWER CHORD IS DUE PER EO 5722B008-010. MODIFICATION OF CENTER WING SECTION RIGHT HAND FRONT SPAR LOWER CHORD WAS ACCOMPLISHED PER EO 5722B008-010. THIS ACCOMPLISHES BOEINGSDR AALA202402231602Spar · noneAIRCRAFT IN BASE MAINTENANCE: MODIFICATION OF CENTER WING SECTION LEFT HAND FRONT SPAR LOWER CHORD IS DUE PER EO 5722B008-005. MODIFICATION OF CENTER WING SECTION RIGHT HAND FRONT SPAR LOWER CHORD WAS ACCOMPLISHED PER EO 5722B008-005. THIS ACCOMPLISHES BOEING SDR DALA2024022102440None · noneAD/EM-EO TASK - RH WING W/C 5720-01102-05B STEP 24. TO GENERATE A STANDALONE "SDR" LOG PAGE AND ENSURE "SDR REPORTABLE" CHECKBOX IS MARKED ASSOCIATED WITH THE REPAIR. LOG-PAGE UPDATED @ 19FEB24 2301 UTC 02 CORR BY SIN 19FEB24 ATA 5723 RII: N ENTR 00631881 W RSDR DALA2024022102439None · noneAD/EM-EO TASK - LH WING W/C 5720-01102-05A STEP 24. TO GENERATE A STANDALONE "SDR" LOG PAGE AND ENSURE "SDR REPORTABLE" CHECKBOX IS MARKED ASSOCIATED WITH THE REPAIR. LOG-PAGE UPDATED @ 19FEB24 2256 UTC 02 CORR BY GOH 00631881 SIN 19FEB24 ATA 5723 RII: N ENTR SDR AALA202402234231Fitting · noneAIRCRAFT IN BASE MAINTENANCE: AS PART OF THE MAJOR REPAIR BEING ACCOMPLISHED ON THE FLIGHT DECK WINDSHIELD FRAMING PER EA 350076 THE RIGHT HAND CONTINUITY FITTING AT FR 2 AND Y0 NEEDS TO BE REPLACED. REPLACED RIGHT HAND CONTINUITY FITTING PER EA 350076.SDR ABXA2024021900632Doubler · noneDURING C-24 MAINTENANCE CHECK AT HAECO AMERICAS, MAINTENANCE REPORTED A REPAIR DOUBLER WAS FOUND THAT HAVE NO RECORD OF ACCOMPLISHMENT ON THE STA 1582 AFT PRESSURE BULKHEAD, APPROXIMATELY AT TS5 / RS11. THE 8767-200 SRM 53-80-08, REPAIR 7 CANNOT BE PERFORMED, SDR ABXA2029021900631Web · noneDURING C-24 MAINTENANCE CHECK AT HAECO AMERICAS, MAINTENANCE REPORTED A REPAIR DOUBLER WAS FOUND THAT HAVE NO RECORD OF ACCOMPLISHMENT ON THE STA 1582 AFT PRESSURE BULKHEAD. THE REPAIR FOR A BLEND TO THE 148T2610-100 WEB IS LOCATED AT FASTENERS COMMON TO RSLL,SDR SWIA20241108215None · noneCOMPLY WITH: 670BA-53-040 - FUSELAGE - CENTER FUSELAGE, PRIMARY STRUCTURE FS280.00 TO FS295.00 - INSPECTION AND REINFORCEMENT OF LINTEL STRINGER 3 OF THE MAIN PASSENGER DOOR REV C PART(S) B (C-CHECK RO 11-6/2024) COMPLIED WITH: 670BA-53-040 - FUSELAGESDR REXA2024103101319Fitting · unknownWHILE PERFORMING SB 670BA-53-044 REV G PART B & C - PRIMARY STRUCTURE FS 144 TO FS 280 - REINFORCEMENT OF THE LH & RH SIDES OF THE FS 202.75 BULKHEAD ABOVE THE FLOOR AND NLG BOX WE FOUND THE R/H STRINGER 12A FITTING CC670-33562-001SB WILL ONLY PICK UP TWO FASTSDR DALA2024021502260None · noneSHIP 6819 A.A. AD 5311-01218-01B, EXISTING REPAIR WAS FOUND IN THE INSPECTION AREA AT STA 1640, S-14R. CORRECTIVE ACTION: SUMMARY OF NRC 00049 ADDITIONAL INSPECTIONS ON EXISTING REPAIR AT STA 1640, S-14R WERE PERFORMED PER PRI NO.597390-14 REV.0 AND ER/A NO.59SDR GE202402130001Combust Chamber · misrepairedCF6-80C2-B6F ENGINE SERIAL NUMBER 704469 WAS RETURNED TO SERVICE BY GE EVERGREEN ENGINE SERVICES CORPORATION (GEEVES) UNDER FAA REPAIR STATION CERTIFICATE 5G3Y679D AFTER COMPLETION OF A COMBUSTOR LINER REPAIR THAT WAS NOT CONTAINED IN THE APPLICABLE INSTRUCTIOSDR AALA202402145963None · noneAIRCRAFT WAS NOT GROUNDED: PERFORM EMERGENCY LIGHT OPERATIONAL TEST. **SUPPLEMENTAL REPORT WILL BE SUBMITTED**(OPEN).SDR DALA2024021302105Door · handler errorAIRCRAFT 3082, DURING LAYOVER IN MSP, A CATERING TRUCK CONTACTED THE AIRCRAFT AFT OF THE L4 DOOR. THE UPPER AND LOWER FR69 SUSTAINED DAMAGE BETWEEN S-27L/S-28L AND S-29L/S-31L. CORRECTIVE ACTION: ACCOMPLISH TRIM OUT OF THE UPPER (LOCATION #1) AND LOWER (LOCATISDR 29GA2024020900001None · handler errorDURING RELOCATION AIRCRAFT COLLIDED WITH VEHICLE DAMAGE TO LOWER LEFT SECTION AFT OF PASSENGER DOOR. MAPPED THE EXTERNAL FUSELAGE AREA BETWEEN FRAME 39 AND 42. LAV REMOVED FOR ACCESS TO INTERNAL SIDE. DENT JUST AFT OF FRAME 41 BETWEEN STRINGER 14L AND 15L FSDR QMLA2024020820012None · noneTHIS AIRCRAFT HAS BEEN RETURNED TO REVENUE SERVICE. REF #0346.020824.0708.BCSDR AALA202402096951Oven · handler errorAIRCRAFT WAS GROUNDED: CATERING LEFT PAPERS IN OVEN RACK, WHEN OVEN WAS TURNED ON TO HEAT FOOD THE PAPERS STARTED TO SMOKE WITH SMALL IGNITION. FLIGHT ATTENDANTS EXTINGUISHED WITH HALON. CLEANED AND PERFORMED OPERATIONAL TEST PER AMM 25-35-00. OPERATIONAL TESTSDR UIEA2024020100065None · noneACCOMPLISHMENT OF EO 4453A301 REV.11, WE FOUND ONE EACH FREEZE PLUG INSTALLED ON UPPER DECK R/H STA 880 FRAME AREA.(<P>FRAME REPAIRED AS PER RI NO. RI-53-20-16702 REV.A. NO FURTHER DEFECTS NOTED.</P>)SDR DALA2024020401515Not Entered · damagedSHIP 3242 DISC: LH FUSELAGE HAS MULTIPLE LIGHTNING STRIKE MARKS BETWEEN FR24 AND FR35. C/A: REPAIRED LIGHTNING STRIKE MARKS PER A320 SRM 53-21. (LP: 0185816)SDR SWAA2024020548298Unknown · unknownLOUD POP/BANG ON TAKEOFF ROLL REJECTED TAKEOFF AT 120 KNTS. BRAKE COOL RETURNED 27.0M FT POUNDS. NO ABNORMAL ENGINE INDICATION OR WARNINGS. NO BIRDS WITNESSED ON TAKEOFF ROLL. NO ENGINE OR AIRFRAME VIBRATIONS NOTED<[01] PERFORMED BIRD STRIKE INSPECTION PER AMMSDR DALA2024020601552None · noneSHIP 1200 ERA 605516-14AD REV A. CORRECTIVE ACTION: AMOC APPROVAL TO AD 2021-10-19 IS REQUIRED AT OR PRIOR TO 50,000 TOTAL AIRFRAME FLIGHT CYCLES. (0182785)
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