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 SWAA2023090596451Panel · damaged193B PANEL HAS SEVERAL ELONGATED FASTENER HOLES.<[01] REMOVE AND REPLACED THE 193B PANEL PER AMM 53-51-21.;[02] C/W INSPECTION.SDR CALA2023090402693Shear Plate · gougedAFT WET AREA AFT L/H SHEAR PLATE MULTIPLE HOLES ARE ELONGATED AND GOUGE (A3NB-53-3-6357) PER HAECO LCQ NON ROUTINE 9290574/40574 GENERATED BY V937268. REMOVED AND REPLACED LH SHEAR PLATE IAW A319 SRM 51-42-11 PAGE 6 ACMP BY MECH V944156 INSP BY V061771SDR CALA2023090402692Shear Plate · crackedAFT WET AREA AFT RH SHEAR PLATE CRACKED (A3NB-53-3-6357) PER HAE CO LCQ NON ROUTINE 9290567/40567 GENERATED BY V937268 REMOVED AND REPLACED RH SHEAR PLATE IAW A319 SRM 51-42-11 PAGE 6 AND 7. ACMP BY MECH V944156 INSP BY V061771SDR AALA202311071080Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK WINDSHIELD FRAMING RIGHT HAND CONTINUITY FITTING AT FR 2 AND Y0. REPLACED CONTINUITY FITTING PER EA 347841.SDR DALA2023090507225Unknown · unknownSHIP 3357 CRACK FOUND AT FRAME 40 VERTICAL WEB ABOVE THE CENTER WING BOX LOWER PANEL AT HOLE 260, AA 5716-01017, SB A330-57-3115 REV 02, AD 2019-16-07 CRACK DIRECTIONS ARE 6 OCLOCK AND 10 OCLOCK VIEW LOOKING AFT, DEPTH IS 0.149 INCH APPROX. ON RH SIDE. CORRECTSDR IPXA2023092691136Tee Fitting · corrodedFAULT: R/H WING TO BODY, T-CHORD STA 1200, AT RBL 63, FOUND EXFOLIATE CORROSION INSTALLED NEW T-CHORD STA 1200, AT RBL 63 IAW B757 SRM 51-40-02-0G REVIEWED.SDR IPXA2023092699104Tee Fitting · corrodedFAULT: THE T-CHORD FOR THE RAT DOOR HINGES, STA. 1180 - STA. 1240, RBL 58 HAS EXFOLIATING CORROSION. INSTALLED RAT DOOR IAW AMM 29-21-09-424-008. REVIEWED.SDR IPXA2023092691224Tee Fitting · corrodedFAULT: R/H WING TO BODY, T-CHORD STA 1220, AT RBL 63, FOUND EXFOLIATED CORROSION. INSTALLED OUTER CHORD AT STA 1220 RBL 63 AND NUT PLATES IAW SRM 51-40-02-0G. REVIEWED.SDR IPXA2023092688659Tee Fitting · corrodedFAULT: R/H, AFT WING TO BODY, T-CHORD, RBL 63, BETWEEN STA 1180 TO STA 1240 FOUND EXFOLIATED CORROSION. INSTALLED NEW T-CHORD I.A.W. SRM 51-40-02-0G. REVIEWED.SDR IPXA2023091488707Unknown · corroded**SDR FILED OPEN**FAULT: R/H WING TO BODY, T-CHORD, AT STA 1180, RBL 35 FOUND NUT PLATE HOLE, EXFOLIATED CORROSION. SDR AND CPCP SUBTASKS COMPLETED.SDR IPXA2023091888988Unknown · corroded**SDR FILED OPEN**FAULT: FWD, WING TO BODY T-CHORD STA 900 BETWEEN RBL 48 TO LBL 34, FOUND EXFOLIATED CORROSION AND CHAFFING, MARKED ON RED REVIEWED.SDR YENA2023090101027Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION IN LONGITUDINAL FLOOR BEAM LOCATED IN Y=300.0 BETWEEN FR 13/18 NI FWD FUS PASSENGER CABIN STRUCTURE; (RESOLVED ON W/O: 1225110 TASKCARD: NR-00013 ) CORROSION IN LONGITUDINAL FLOOR BEAM LOCATED IN Y=300.0 BETWEEN FR 13/18 IN SDR YENA2023090101026Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION ON FLOOR BEAM BTW FR87 AND FR88 AND Y: 300 RH AT FLOOR STRUCTURE (W2); (RESOLVED ON W/O: 1225110 TASKCARD: NR-00014 ) REMOVED CORROSION ON FLOORBEAM BTW FR 87 AND FR 88 AND Y: 300 RH BLEND OUT FROM ORIGINAL THICKNESS OF .06SDR YENA2023090101025Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION ON CROSSBEAM LOCATED AT FR 11 BETWEEN Y= -370.0 AND Y= 370.0 COCKPIT FLOOR STRUCTURE; REMOVED CORROSION AND REPAIRED AREA PER EMB 190 SRM 51-12-01, SRM 51-10-03 AND REPAIRED PER EC# E23-707-01 REF. TOMX NR# 00141 FOR ALL WORSDR YENA2023090101024Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION ON FR 80 AT STR 27RH AND STR28RH AT AFT CARGO DOOR CUTOUT; REMOVED CORROSION ON FR 80 AT STR 27R TO STR 28R FOUND TO BE OUT OF LIMITS PER EMB SRM 53-23-60 PERFORMED A TEMPORARY REPAIR PER ETD 2023-190-018873 REV A, EC # E23-SDR YENA2023090101023Unknown · unknownDURING HEAVY MAINTENANCE: BOTTOM TAIL CONE FITTING HAS CORROSION; REMOVED CORROSION ON BOTTOM FITTING OF TAIL CONE. FOUND TO BE OUT OF LIMITS PER EMB-190 SRM 53-31-02 AD/54 PAR 4 AND 5 FIG 101. REMOVED AND REPLACED BOTTOM TAIL CONE FITITING IAW EMB-190 SRM 51-SDR YENA2023090101022Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION ON CUTOUT OF A/C WASTE SERVICE PANEL (REF TOMX NRC# 00009); CORROSION ON CUTOUT OF WASTE SERVICE PANEL WAS REMOVED AND FOUND TO BE OUT OF LIMITS PER EMB-190 SRM 53-23-60 PAR 4 TABLE 101. CUTOUT AREA OF WASTE SERVICE PANEL WASDR YENA2023090101021Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION ON SEAT TRACK (RH) BTW FR 79 AND FR 81 Y -100 REFERENCE TOMX NRC# 00173; REMOVED CORROSION FROM SEAT TRACK (RH) BTW FR79 AND FR81 AT Y-100 FOUND TO BE OUT OF LIMITS PER EMB 190-SRM 53-23-10/AD51. REMOVED AND REPLACED SEAT RASDR YENA2023090101017Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION ON FLOOR BEAM BTW FR87 AND FR88 AND Y: 300 RH AT FLOOR STRUCTURE (W2); REMOVED CORROSION ON FLOOR BEAM BTW FR 87 AND FR 88 AND Y: 300 RH BLEND OUT FROM ORIGINAL THICKNESS OF .063" WAS .026" WITH A REMAINING THICKNESS OF .03SDR DALA2023083107092Unknown · unknownSHIP 3330 MISDRILLED A HOLE AT FRAME 63 BETWEEN P1L AND P1R. CORRECTIVE ACTION: COMPLIED WITH PRI 611438-14. VALIDATED ER/A 611438-14 MATCHES PRI 611438-14. PERFORMED REPAIR INSTRUCTIONS ON FR 63 BTW STR 1L AND 1R AT PASSENGER CABIN AS PER ER/A 611438-14. (294SDR DALA2023083107091Unknown · unknownSHIP 3357 CORROSION INTERNAL STRUCTURE ON REINFORCER PLATE AT LEVEL FR 53.2 AND BTW STR 49R TO STR 50R IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: COMPLIED WITH PRI 611450-14. VALIDATED ER/A 611450-14 MATCHES PRI 611450-14. PERFORM REPAIR ON INTERNAL STRUCTURSDR BAGA2023091800010Unknown · unknownCORROSION AROUND FASTENER HOLES - PNL 192CR AT MULTIPLE LOCATIONS - ZONE 100 CORRECTIVE ACTION- PANEL REPLACEDSDR IPXA2023083094054Unknown · vibrationINSPECTION TYPE:NA*ATB* CLIMBING THRU 30,100 A/C BEGAN TO SHAKE. FELT LIKE IT WAS COMING FROM THE TAIL. SLOWED DOWN FROM 302 TO 290. THEN 280 KTS. LEVEL AT FL 320, VIBRATION LESSENED BUT DIDNT DISSIPATE COMPLETELY. DESCENDING THROUGH 14,500 VIBRATION INCREASEDSDR DALA2023082907050Unknown · unknownSHIP 0669 CORROSION ON WEB BTW RBL 10 TO RBL 40 FROM STA 1701 TO 1720 AT PAX FLOOR STUCTURE (W4) ZONE 250 (GALLEY SETTLEMENT). CORRECTIVE ACTION: SUMMARY OF NRC 00689. WEB BTW RBL 10 TO RBL 40 FROM STA 1701 TO 1720 AT PAX FLOOR STUCTURE (W4) ZONE 250 (GALLEY SSDR VNAA2023082905Angle · corrodedCLIP CORRODED AT FRAME AT FS295 AND STRG21R.SDR VNAA2023082908Doubler · corrodedDOUBLER FOR AFT POTABLE WATER LINES CORRODED BETWEEN FS 1031.00 AND FS 1047.00 STR 26R.SDR VNAA202308290007Joint · corrodedF.S. 280 CIRCUMFERENTIAL JOINT IS CORRODED BETWEEN STGR 24L AND STGR 23L.SDR VNAA202308290006Angle · corrodedCORROSION FOUND ON PAX DOOR UPPER SILL ANGLE.SDR B1EA20231127109BCUnknown · unknownSHORTLY AFTER TAKEOFF PILOT/CREW HEARD A BANG. PILOT NOTICED #1 ENGINE TOT RISING RAPIDLY AND DETERMINED THERE WAS AN ENGINE FAILURE. PILOT TURNED THE AIRCRAFT AROUND TO RETURN TO THE AIRFIELD. UNKNOWN TO THE PILOT, BUT CAUGHT ON VIDEO, THERE WAS AN UNCONTAINESDR VNAA202310100003Fitting · wornPERM REPAIR - JACKING PAD HELICOIL INSERT, RHS CW PERM REPAIR PER REO INSTRUCTIONS. JACK FITTING PAD RH WING WAS REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01SDR HNAA2023091800325Unknown · unknownE993888 SHEAR CLIP CRACKED AT FR 8 BTW STGR 9L AND WINDSHIELD LOWER FRAME. ACCOMPLISHED REPAIR OF FR 8 STGR 9L TO LOWER WINDSHIELD FRAME SHEAR CLIP IAW ETD# ETD2023-145-021990 AND EO1-53-23-0271.SDR I5EA2023083000030Unknown · unknownLIGHTNING STRIKE AT STR 4L STA 500B+17. W/O NUMBER: HT339 – 30004. REPAIR OF LIGHNING STRIKE DAMAGE USING SRM GUIDELINES AND CUSTOMER SERVICE REPAIR INSTRUCTIONS DOC# CS-30498-004, AT STR 4L STA 500B+17.SDR I5EA2023083000029None · noneLIGHTNING STRIKE BETWEEN STR 4L AND STR 5L STA 500+4. W/O NUMBER: HT339 – 30005. REPAIR OF LIGHNING STRIKE DAMAGE USING SRM GUIDELINES AND CUSTOMER SERVICE REPAIR INSTRUCTIONS DOC# CS-30498-004, BETWEEN STR 4L AND STR 5L STA 500+4.SDR I5EA2023083000028Unknown · unknownLIGHTNING STRIKE BETWEEN STR 4L AND STR 5L STA 480+3. W/O NUMBER: HT339 – 30006. REPAIR OF LIGHNING STRIKE DAMAGE USING SRM GUIDELINES AND CUSTOMER SERVICE REPAIR INSTRUCTIONS DOC# CS-30498-004, BETWEEN STR 4L AND STR 5L STA 480+3.SDR I5EA2023083000027Unknown · unknownLIGHTNING STRIKE AT STR 1L STA 440+16. W/O NUMBER: HT339 – 30011. REPAIR OF LIGHNING STRIKE DAMAGE USING SRM GUIDELINES AND CUSTOMER SERVICE REPAIR INSTRUCTIONS DOC# CS-30498-004, AT STR 1L STA 440+16.SDR I5EA2023083000026Unknown · unknownLIGHTNING STRIKE AT STR 1L STA 400+6. W/O NUMBER: HT339 – 30007. REPAIR OF LIGHNING STRIKE DAMAGE USING SRM GUIDELINES AND CUSTOMER SERVICE REPAIR INSTRUCTIONS DOC# CS-30498-004, AT STR 1L STA 400+6.SDR I5EA2023083000025Unknown · unknownLIGHTNING STRIKE AT BL-0 STA 328+12. W/O NUMBER: HT339 – 30008. REPAIR OF LIGHNING STRIKE DAMAGE USING SRM GUIDELINES AND CUSTOMER SERVICE REPAIR INSTRUCTIONS DOC# CS-30498-004, AT BL-0 STA 328+12.SDR UIEA2023082900809Unknown · unknownDUE TO EO INSP, WASHERS WERE NOT FOUND UNDER EACH FASTENER HEAD, REQUEST ADD EO PART 2 AND PART 5. PERFORM NOSE W/W FWD CORNER DOUBLER MODIFICATION NEAR STA 240, S39 TO S45, SB 747-53A2851 REV O(<P>1) REMOVED DOUBLER PART IAW SRM 51-40-02-0G-0 REV 98. 2) PERFOSDR IXXA2023082802Roller Tray · corrodedROLLER TRAY CORRODED AT STA 654+88 RBL 20 AT LOCK. COMPLETED ROLLER TRAY SPLICE REPAIR IAW B767 SRM 53-00-53 REPAIR 1 DETAIL 4 REF. AMES DOC 47574REA01.SDR IPXA2023091048144Unknown · unknown*SDR FILED OPEN* *MAJOR REPAIR* FAULT: 1 EA DENT FOUND ON LH FRAME STA 800 AT STR 26L REF STEP 31. OUT FOF SEQUENCE. INSPECTED AND VERIFIED SHEAR TIE AND STRINGER IS INSTALLED. JOB COMPLETED. INSPECTION COMPLETED.SDR DALA2023090707324Unknown · unknownSHIP 3162 MIS-DRILLED DAMAGE WAS NOTED ON THE #6 FITTING AFT OUTBOARD FASTENER. CORRECTIVE ACTION: REPAIRED PER ERA 601771-14 REV A. (2936192)SDR SWAA2023083193370Panel · crackedACCESS PANEL 193AL IS SHOWING A CRACK AT I/B SURFACE AREA<[01] REPAIRED ACCESS PANEL 193AL I/B SURFACE; PER REF B737 SRM 51-70-04-2R-1; MATERIAL USED PO.1791128 AND PO.1473815;[02] FINAL INSPECTION; VERIFIED STEP #1. CRACKED REPAIRED.SDR QXEA202308300121Doubler · corrodedFWD LAV INTERNAL DOUBLER CORRODED. FWD LAV DOUBLER REPLACED IAW SRM REV 21 TASKS 51-42-05-02-01, 51-40-15-02-01, 51-23-00-00-01.SDR CALA2023082802650Unknown · crackedLT SIDE FLOOR INNER CHORD BS 303 HAS A CRACK REF AAR N/R 9206631 REMOVED AND REPLACED THE INNER CHORD AT LT SIDE FLOOR BS303 REF B737 SRM 51-40-02-0G-0SDR SWAA2023082893490Access Door · deformedEGPR DOOR IS DEFORMED.<[01] R AND R EXTERNAL POWER RECEPTACLE ACCESS DOOR IAW M/M REF. 52-49-02.SDR JJBA20230825025Unknown · unknownRF1, CARGO DOOR SURROUND STRUCTURE AFT L-SHAPE AT FR 68 FOUND CORRODED. SHEAR CLIP REPAIRED WITH A SPLICESDR K11A2023092700229Unknown · corrodedEVIDENCE OF CORROSION FOUND LH W/W CEILING CHORD LOWER SURFACE AT APPROX STA 707 LBL 5.SDR IPXA2023092421339Panel · corroded*** SUPPLEMENTAL SDR *** FAULT: REMOVE THE #2 R/H TRANSITION PANEL TO FOM FOR SUSPECTED CORROSION BELOW PANEL AT STA 1380 INSTALLED NEW TRANSITION PANEL IAW SRM 51-40-02. REVIEWED.SDR SWAA2023090693205Panel · crackedPANEL 195CL HAS A CRACK IN THE AFT EDGE LOWER RADIUS<[01] REPAIRED CRACK DAMAGE IN THE AFT EDGE LOWER RADIUS OF PANEL 195CL IAW SRM 51-70-05-2R-6.;[02] FINAL INSPECTION. JOB COMPLETE.SDR CALA2023090402701Unknown · damagedRAMP REPORTS PIT DAMAGE. RT SIDE PANEL STA 500D MOST 8-10 SCREW HOLES TORN. SDR FLAGGED. ACP PERMANENT REPAIR REF AMM 50-10-01-340-801. PARTS USED: 40-0608-3-0147,QTY :1
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