JASC 5300
Service difficulty reports · 8,204
Reports filed under 5300 · Fuselage Structure (General), 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 = '5300' 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 = '5300' 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 CALA2024082702286Structure · corrodedL2 DOOR CHORD CORRODED FROM STA 940 TRHU STA 996. L-2 DOOR CHORD REPLACED ON BAM N/R 002147108. THIS L/P IS FOR SDR/ ESFR REPORTING ONLY.SDR IPXA2024100844134Stringer · crackedSTRINGER CRACK, FWD SIDE OF STA 1960 S-38L (REPAIR). ACCOMPLISHED REPAIR I.A.W UPS EO-91518-REQ1 REV.1 AND SRM 53-60-03-2R-9 REV.43 AND EGAT WORK SHEET NO.40756.SDR IPXA2024100444585Stringer · crackedSTRINGER CRACK, AFT SIDE OF STA 740 S-6R (REPAIR). ACCOMPLISHED REPAIR I.A.W UPS EO-91579-REQ1 REV.1.SDR NACA2024082300002Structure · crackedFWD CARGO COMPT UPPER CHORD FOUND CRACK AT LBL 42 STA 412. REPAIRED IAW SRMSDR AALA202408272510Unknown · vibrationAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO BNA DUE TO THE FLIGHT CREW REPORTING THAT WHILE CLIMBING THERE WAS A SHARP JOLT FOLLOWED BY SEVERE LONG PERIOD VIBRATION. INITIAL JOLT YAWED AIRPLANE TO THE LEFT ABOUT 5 DEGREES. SEVSDR DALA2024082608453Fitting · damagedDEVIATIONS ON FR68 RHS FITTINGS 1, 3, 4. CORRECTIVE ACTION: REPAIRED PER ERA 619949-14AD. (0516249)SDR IPXA2024082676285Structure · brokenLOAD CREW FOUND CENTERLINE GUIDE AND AIRCRAFT STRUCTURE BROKEN AT STATION 1820-1840 (POSITION 9 AFT LOWER PIT) INSTALLED 2(EA) BALL MAT PANELS IN LWR AFT PIT AT STATIONS 1840 AND 1900 PER AMM 25-53-15-400-801, PDU OPS CHECK GOOD PER AMM SUBTASK 25-53-01-864-03SDR YENA2024082601156Fitting · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON INTERCOSTAL FITTING FASTENER HOLE H3 DOOR ST OP FITTING #7 AREA FR 16 LH. CRACK DIRECTION 3 OCLOCK. CRACK D= 2.54 M M; REF AEROMAN WO 2024 131/1 WCC 2024-336941. REMOVED AND REPLACED INTERCOSTAL FITTING LOC. SDR AALA202408198802Unknown · vibrationAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: DURING TAKEOFF, AFTER GEAR RETRACTION, NOTICED STRONG VIBRATION AND NOISE FROM NOSE WHEEL AREA; AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT GRU.SDR IPXA2024082088175Panel · crackedPANEL 513AB CRACKED AT NUTPLATE HOLE. CLEANED AREA AROUND CRACK AND REMOVED FASTENERS IAW A300-600 SRM 53-15-63 STEP 5.TREATED AND PRIMED DOUBLERS IAW A300-600 SRM 51-21-10 AND 51-75-10.SDR 2024FA0000600Structure · migratedAIRCRAFT IS CURRENTLY IN HANGAR FOR “C11” CHECK. DURING THE ACCOMPLISHMENT OF ADSI IB744530068 / IB744530171, 02-OFF CRACKS WERE FOUND BETWEEN STR 21L TO STR 22L, BS 2231 AND 01-OFF CRACK AT STR 26L, BS 2231.SDR CALA2024081300419Unknown · damaged25APR SFO CF -T :MAJOR REPAIR AT FR12 STR 6L. REPAIR WAS INSTALLED ON 08-26-2008 AT HMV2 LAKE CITY ON NR D8344Z PER SRM 5 3-11-11 FIG 212. REPAIR IS INACTIVE AND SUPERSEDED BY AND IS IN ACCORDANCE WITH SRM 53-00-11 FIG 232. INSPECTION INSTRUCTION REF IIR IS 53SDR CALA2024081300418Unknown · damaged25APR SFO CF -T :MAJOR REPAIR AT FR34 STR 10R REPAIR WAS IN STALLED ON 08-26-2008 AT HMV2 ON NR D8346Z PER SRM 53-21-11 FIG 214. REPAIR IS INACTIVE AND SUPERSEDED BY AND I N ACCORDANCE WITH SRM 53-00-11 FIG 232.REPAIR CATEGORY B INSPECT ION INSTRUCTION REF IIRSDR SWAA2024092024807Angle · crackedCRACK ANGLE - CLIP LOCATED STA500C AND STR26L FWD CARGO COMPARTMENT 2024-489239<[01] REPLACED CLIP LOCATED STA500C AND STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DRAWING 143A7505 SHEET 6 REV D.;[02] CORRECTED STEP 1 <BSDR AALA202408156403Unknown · vibrationAIRCRAFT WAS GROUNDED: FLIGHT ATTENDANTS REPORTED VIBRATION IN FLOOR AND BUZZING SOUNDAROUND ROW 11 AND 12. MORE PRONOUNCED ON INITIAL CLIMB OUT ANDCRUISE. SUBSIDED SOME TIME AROUND 2 HOURS INTO FLIGHT. NO ABNORMAL INDICATIONS ON FLIGHT DECK.**SUPPLEMENTAL SDR DALA2024081308083Access Door · damagedSHIP 3170 ACCESS DOOR OF CARGO OPENING SYS **DISPATCHER SELECT EXTENSION** FWD PANEL DAMAGED. CORRECTIVE ACTION: REPAIRED PER A319 AMM 52-31. (6044720)SDR IXXA2024080906Lock · corrodedL/H SIDE HAS CORRODED LOCK AT APPROX. STA. 1197+43SDR DALA2024080907962Access Door · corroded(LOG 0491983) WORK SHOP INTERIOR SHEET METAL: CORROSION ON TRIM UNDER OF THE DOOR ACCESS A417 (1EA) AND A423 (1EA) AT GALLEY 4. TRIM UNDER OF THE DOOR ACCESS A417 (1EA) AND A423 (1EA) AT GALLEY 4 WERE REPLACED PER ER/A NO. 619671-14 REV. ORIGINAL SECTION I: PESDR DALA2024080607792Structure · ground damageSHIP 3410 DURING BOARDING A LADDER CAME IN CONTACT WITH THE AIRCRAFT JUST AFT OF BULK CARGO DOOR. CORRECTIVE ACTION: COMPLIED WITH ERA 619702-14 REV C. OK FOR SERVICE. (6166042)SDR DALA2024080607791Structure · ground damageSHIP 3410 DURING BOARDING AC CAME IN CONTACT WITH WORK STAND JUST BELOW BULK CARGO DOOR. CORRECTIVE ACTION: COMPLIED WITH ERA 619772-14. (0485762)SDR CALA2024080502157Floorbeam · corrodedAFT WET AREA FLOOR STRUCTURE ;POSSIBLE CORROSION ON FLOOR BEAM S TA .947, RBL50.SDR IPXA2024080737544Floor Support · corrodedCORROSION - STRIP, LOWER FACE OF MAIN DECK CARGO FLOOR BEAM SUPPORT, STA 1920 RBL 23 (REPLACE). I.A.W AMM 20-51-01-912-008 REV 111 REPLACED PLATE. I.A.W AMM 51-24-13-607-010 REV 111 APPLY CORROSION PREVENTIVE COMPOUND.SDR CALA2024072902134Structure · crackedMAIN CABIN FWD WET AREA L/H INNER CHORD CRACK AT STA 309 REF AAR N/R 9892617 REMOVED AND REPLACED MAIN CABIN FWD WET AREA L/H INNER CHORD FROM STA 259.5-360 AS PER B737-900ER DWG 141A8110 AND SRM 51- 40-02-0G-0 AND TREATED AND PRIMED FASTENER HOLES AS PER B73SDR CALA2024072902132Structure · corrodedMAIN CABIN FWD WET AREA CORROSION AT R/H INNER CHORD UPPER SURFACE REF AAR N/R 9892613. REMOVED AND REPLACED R/H INNER CHORD FWD WET AREA FROM STA 259.5-260 AS PER SRM 51-40-02-0G-0 AND DWG 141A8320 AND TREATED AND PRIMED FASTNER HOLES AS PER AMM 51-21-41-37SDR CALA2024072902118Torque Box · corrodedAFT PIT TORSION BOX COVER CORRODED. REMOVED AND REPLACED TORSION BOX COVER AT AFT PIT IAW A320 SRM 5 1-42-11-001SDR CALA2024072400280Panel · missingPDA 1 RAMP FOUND AIRCRAFT ARRIVED WITH MISSING PANEL. PANEL IS NUMBER 194E. AIRCRAFT ARRIVED FROM RDU FLIGHT NUMBER 1878 ON 7-21-24. NO FURTHER DAMAGE ON AIRCRAFT FROM PANEL DEPARTING AIRCRAFT WAS FOUND. ACCOMPLISHED CONDITIONAL INSPECTION FOR WHEN PARTS DEPASDR AALA202407250498Panel · crackedAIRCRAFT IN BASE MAINTENANCE: DURING LEADING EDGE PANEL REMOVAL FOUND PANEL 521QB CRACKED AT CORNER NEXT TO SCREW HOLE. CHECKED AND ACCOMP PANEL EDGE REPAIR. PER SRM 51-70-10-2R-1 REPAIR 1SDR IPXA2024073144072Shroud · damagedLH INBD SHROUD BOX LOWER T/E IS DAMAGED.REMOVED BOOM STRAP PANEL SKIN FROM LH WING TRAILING EDGE LOWER SKIN. IAW A300-600 SRM 51-40-21.INSTALLED NEW SKIN I.A.W. A300-600 SRM 51.40.21.SDR IPXA2024081513492Support Plate · corrodedCORROSION - PLATE, MAIN DECK FLOOR PNL SUPPORT PLATE, STA 1782 & 1798 RBL 90. (REPLACE). I.A.W AMM 20-51-01-912-008 REV 111 REPLACED PLATE TOTAL 2 EA. I.A.W AMM 51-24-13-607-010 REV 111 APPLY CORROSION PREVENTIVE COMPOUND.SDR IPXA2024073198210Support Plate · corrodedCORROSION - PLATE, MAIN DECK CARGO FLOOR PNL SUPPORT PLATE, STA 1500 LBL 10. (REPAIR) INSTALL FABRICATE PART I.A.W. SRM 51-40-02-0G REV.101 AND BOEING DWG NO:65B38407 SH 1 REV.C. PAPER CHECK OK.SDR YENA2024072301029Fitting · unknownDURING HEAVY MAINTENANCE: REMOVE AND REPLACE CONTINUITY FITTING LH & RH SIDE LOCATED BTW FR 1 AND FR 2 IN COCKPIT; REF AEROMAN N/R 2024-349053, REMOVE AND REPLACE CONTINUITY FITTINGS LH AND RH SIDE LOCATED BTW FRAME 1 AND FRAME 2 IN COCKPIT IAW EC A24-844-01, SDR IPXA2024081265808Floorbeam · corroded*SDR FILED OPEN* FAULT - CORROSION - CHORD, MAIN DECK FLOOR BEAM UPPER CHORD, STA 740 LBL 5 ~ 10 (REPAIR) CHECK NORMAL.SDR DALA2024071807267Structure · corrodedAIRCRAFT 3059, CORROSION ON HOLE LOC FR68 AT LEVEL STR23R AT LOWER SILL AFT GALLEY AREA. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON LOWER SILL LOC. AT FR68 AT LEVEL STR23R AFT GALLEY AREA AS PER A321 SRM 53-41-14-300-001 STEP 2.A; FIGURE 001; SHEET 3.SDR DALA2024071607183Unknown · unknown(LOG 0447493) REPAIRED PER WORK CARD 2526-01236-02B INSTRUCTIONS, REF SUPPORTING AA 2526-01236.SDR SWIA20240710Splice Plate · mechanic errorWARRANTY- WHILE DRILLING REPLACEMENT SEAT TRACK P/N 170-86082-005 MIS DRILL OF TOOLING HOLE IN FWD SPLICE PLATE CAUSING DAMAGE TO STIFFENING RIDGE AREA OF SEAT TRACK. (C-CHECK RO 7/22/2024) PERFORMED SPLICE REPAIR ON R/H I/B SEAT TRACK FR 74-84 REF ETD2SDR DALA2024070906964Structure · corrodedSHIP 3132 CORROSION LAVATORY A ASSY G672001-101. CORRECTIVE ACTION: REPLACED PER ER/A 618085-14. (0434886)SDR FDEA202407061002Angle · chafedQA SURVEILLANCE ITEM AFT CGO COMP'T RH SIDE PROFILE CORNER GOT SCRATCH AT FR58- FR59A POSITION. REPLACED THE SCRATCHED CORNER PROFILE WITH A NEW ONE. I.A.W A300-600F SRM 51-72-10-001 PAGE 2. AT AFT CARGO COMPARTMENT RH SIDE, FR58~FR59A POSITION. REPAIR IS SDR CALA2024071001997Floorbeam · corrodedB737-06-3-0049, MAIN CABIN ST 986.3 APPROX LBL 44 TO RBL 44 FLOOR STRUCTURE HAS CORROSION AT FASTENER HOLES. MAIN CABIN STA 986.3 APPROX LBL 44 TO RBL 44 FLOOR SUPPORT STRUCTURE CORROSION REPAIRED REF ECRA 5370-01129. SEE PARTIAL WORK FOR WORK ACCOMPLISHED.SDR YENA2024070800952Fitting · unknownDURING HEAVY MAINTENANCE: REMOVE AND REPLACE CONTINUITY FITTINGS LH AND RH SIDE LOCATED BTW FRAM E 1 AND FRAME 2 IN COCKPIT DUE TO AIRBUS DOSSIER REFERENCE 81254114; (RESOLVED ON W/O: 1301763 TASKCARD: NR-00053) REF AEROMAN WO 2024 159/1 NR 2024-277245 REMOVE SDR SWAA2024070206515Panel · delaminatedPANEL 193AR MATING SURFACE HAS DELAMINATION.<[01] REPAIRED DELAMINATION DAMAGE ON PANEL 193AR IAW SRM 51-70-05-2R-6.;[02] VERIFIED JOB COMPLETESDR SWAA2024062504956Panel · delaminatedPANEL 193AR HAS COMPOSITE DELAMINATION<[01] COMPLIED WITH SRM 53-40-70; DELAMINATION SPOT OF PANEL 193AR HAS BEEN COVERED WITH SPEED TAPE.;[02] COMPLIED WITH EA 24-153-01717.;[03] CHANGED REF PER E113616 VIA TELECOMSDR UIEA2024061400521Structure · corrodedCENTER SECTION AFT FACE FOUND CORROSION ( NEAR LH O/J PUMP BONDING AREA )(<P>CENTER SECTION AFT FACE CORROSION REMOVED IAW SRM 51-10-02 AND REPROTECTED IAW SRM 51-20-01 AND MEASURED. REMAIN 0.783" ORG 0.806" WIDTH 1.4, LENGTH 2" WITHIN SRM 57-10-10-1A-2 ALLOWASDR UIEA2024062000558Panel · corrodedM/D BELOW FSK STOWAGE PNL FOUND CORROSION(<P>M/D - BELOW FSK STOWAGE PNL REPAIR IAW FVCI EO - 24090-1, 2A, 3. NO FURTHER DEFECTS NOTED.</P>)SDR VNAA20240726006Mount · corrodedCORROSION ON ANGLE, MOUNTING BTW FS 319.70 AND FS 349.00 AT SERVICE DOOR SURROUND STRUCTURE. CORROSION ON ANGLE, MOUNTING BTW FS 319.70 AND FS 349.00 AT SERVICE DOOR SURROUND STRUCTURE WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-23-101-002-A02 AND REPLASDR CALA2024061700005Panel · missingFOUND PANEL MISSING DIRECTLY BEHIND GEAR BAY IN CENTER OF BELLY. FOUND NO OTHER DAMAGE ON AIRCRAFT. ALL SCREWS EXCEPT FORWARD MOST 4 STILL INSTALLED PANEL 194E PANEL PARTS INFORMATION ADDED. IPC 53-51-00-15 UPDATED SDR CAREFULY CHECKED ADJACENT STRUCTURE AND FSDR CALA2024062000038Structure · fireWHEEL WELL FIRE LIGHT IN FLT. LIGHT CLEARED AFTER GEAR EXT. PERFORMED FIM TASK 26-18 TASK 802. BITE TEST 26-18 TASK 801 FAULT CODE 84. CHECKED WHEEL WELL CEILING LOOPS, NO NOTABLE DAMAGE NOTED. CLEARED OVERHEAT DETECTOR CONTROL MODULE, FAULT DID NOT RETURN.SDR UIEA2024051000379Beam · chafedAFT CARGO STA 1912 LBL 18" CABLE HOLE FOUND CHAFING (CONTACT WITH PDU CONTROL CABLE)(<P>BEAM CHAFING AREA REPAIRED AS PER RI-53-60-16863 REV.A. NO FURTHER DEFECTS NOTED.</P>)SDR SWAA2024061299847Panel · delaminatedPANEL 194CL HAS TWO DENTS WITH DELAMINATION FROM IMPACT DAMAGE. AREAS MARKED.<[01] REMOVED PANEL 194CL FOR FOM PER SRM 51-40-02.;[02] NEW PANEL 194CL SANDED RED PANT AND REPAINT WITH HEART BLUE COLOR PER AMM 51-21-99;[03] INSTALLED PNL PER SRM 51-40-02SDR UIEA2024060500479Not Reported · corrodedMAIN DECK CARGO, BTW STA 1329 AND 1351, STRG 19L WITH CORROSION(<P>CORROSION ON FUSELAGE SECTION 46 BETWEEN STA 1329 / 1351 AND STGR 19L WAS REPAIRED PER CMA-TLS 24-0166-02B. NO FURTHER DEFECT NOTED.</P>)SDR SWAA2024061100575Unknown · unknownDURING CLIMB PASSING FL340; POP / THUD FELT RIGHT SIDE OF AIRCRAFT. ALL ENG INDICATIONS AND CONTROL NORMAL. PERFORMED AIRCRAFT WALKAROUND INSPECTION; OBSERVING ALL FLIGHT CONTROLS; ENGINES; PANELS; OPENING; FUSELAGE AND WHEEL WELL AREAS. NOTHING ABNORMAL FOUN
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