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.

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.Sep 2, 2023 · N7881A · Boeing 7377CTSDR 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 V061771Sep 2, 2023 · N816UA · Airbus A319131SDR 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 V061771Sep 2, 2023 · N816UA · Airbus A319131SDR 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.Sep 1, 2023 · N808AW · Airbus A319132SDR 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. CORRECTSep 1, 2023 · N857NW · Airbus A330223SDR 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.Aug 31, 2023 · N433UP · Boeing 75724APFSDR 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.Aug 31, 2023 · N433UP · Boeing 75724APFSDR 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.Aug 31, 2023 · N433UP · Boeing 75724APFSDR 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.Aug 30, 2023 · N433UP · Boeing 75724APFSDR 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.Aug 30, 2023 · N433UP · Boeing 75724APFSDR 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.Aug 30, 2023 · N433UP · Boeing 75724APFSDR 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 Aug 30, 2023 · N228JB · Emb ERJ190100IGWSDR 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 .06Aug 30, 2023 · N228JB · Emb ERJ190100IGWSDR 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 WORAug 30, 2023 · N228JB · Emb ERJ190100IGWSDR 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-Aug 30, 2023 · N228JB · Emb ERJ190100IGWSDR 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-Aug 30, 2023 · N228JB · Emb ERJ190100IGWSDR 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 WAAug 30, 2023 · N228JB · Emb ERJ190100IGWSDR 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 RAAug 30, 2023 · N228JB · Emb ERJ190100IGWSDR 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 .03Aug 30, 2023 · N228JB · Emb ERJ190100IGWSDR 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. (294Aug 30, 2023 · N830NW · Airbus A330302SDR 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 STRUCTURAug 30, 2023 · N857NW · Airbus A330223SDR BAGA2023091800010Unknown · unknownCORROSION AROUND FASTENER HOLES - PNL 192CR AT MULTIPLE LOCATIONS - ZONE 100 CORRECTIVE ACTION- PANEL REPLACEDAug 29, 2023 · N128BZ · Emb ERJ190100IGWSDR 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 INCREASEDAug 29, 2023 · N136UP · Airbus A300F4622RSDR 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 SAug 29, 2023 · N669DN · Boeing 757232SDR VNAA2023082905Angle · corrodedCLIP CORRODED AT FRAME AT FS295 AND STRG21R.Aug 29, 2023 · N511AE · Cndair CL6002C10SDR VNAA2023082908Doubler · corrodedDOUBLER FOR AFT POTABLE WATER LINES CORRODED BETWEEN FS 1031.00 AND FS 1047.00 STR 26R.Aug 29, 2023 · N511AE · Cndair CL6002C10SDR VNAA202308290007Joint · corrodedF.S. 280 CIRCUMFERENTIAL JOINT IS CORRODED BETWEEN STGR 24L AND STGR 23L.Aug 29, 2023 · N524AE · Cndair CL6002C10SDR VNAA202308290006Angle · corrodedCORROSION FOUND ON PAX DOOR UPPER SILL ANGLE.Aug 29, 2023 · N524AE · Cndair CL6002C10SDR 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 UNCONTAINEAug 28, 2023 · N109BC · Urocop EC135T1SDR 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-A01Aug 28, 2023 · N555NN · Cndair CL6002D24SDR 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.Aug 28, 2023 · N642AE · Emb EMB145LRSDR 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.Aug 28, 2023 · N916SC · Boeing 7378SDR 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.Aug 28, 2023 · N916SC · Boeing 73786JSDR 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.Aug 28, 2023 · N916SC · Boeing 73786JSDR 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.Aug 28, 2023 · N916SC · Boeing 73786JSDR 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.Aug 28, 2023 · N916SC · Boeing 73786JSDR 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.Aug 28, 2023 · N916SC · Boeing 73786JSDR 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) PERFOAug 28, 2023 · N446MC · Boeing 7474B5FSDR 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.Aug 28, 2023 · N1439A · Boeing 76733ASDR 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.Aug 27, 2023 · N433UP · Boeing 75724APFSDR 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)Aug 25, 2023 · N362NB · Airbus A319114SDR 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.Aug 25, 2023 · N966WN · Boeing 7377H4SDR 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.Aug 25, 2023 · N404QX · Bombdr DHC8402SDR 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-0Aug 25, 2023 · N76508 · Boeing 737824SDR SWAA2023082893490Access Door · deformedEGPR DOOR IS DEFORMED.<[01] R AND R EXTERNAL POWER RECEPTACLE ACCESS DOOR IAW M/M REF. 52-49-02.Aug 25, 2023 · N7715E · Boeing 7377BDSDR JJBA20230825025Unknown · unknownRF1, CARGO DOOR SURROUND STRUCTURE AFT L-SHAPE AT FR 68 FOUND CORRODED. SHEAR CLIP REPAIRED WITH A SPLICEAug 25, 2023 · N11192 · Emb EMB145XRSDR K11A2023092700229Unknown · corrodedEVIDENCE OF CORROSION FOUND LH W/W CEILING CHORD LOWER SURFACE AT APPROX STA 707 LBL 5.Aug 24, 2023 · N405CK · Boeing 737436SDR 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.Aug 24, 2023 · N433UP · Boeing 75724APFSDR 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.Aug 24, 2023 · N7886A · Boeing 737752SDR 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 :1Aug 24, 2023 · N37528 · Boeing 7379
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