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 HNAA2023080700287Unknown · unknownE985328 L/H WINDSHIELD LATERAL POST UPPER ATTACH POINT SKIN CRACKED JUST FWD OF SPEAKER. RAR L/H WINDSHIELD LATERAL POST IAW EMB 145 SRM 51-40-02.Jul 9, 2023 · N644AE · Emb EMB145LRSDR YENA2023071100784Unknown · unknownDURING HEAVY MAINTENANCE: 'ELONGATED HOLES (5EA) LOCATED ON FRAME 50 BTW STRINGER 3L TO STRINGER 5L; REPAIRED ELONGATED HOLES AT THE FR50 BTW STGR 3L-5L IR IAW EC NO. A23-556-01 REF AEROMAN W/O:2023 134/1 NRC 2023 - 386506.'Jul 9, 2023 · N2086J · Airbus A321271NSDR YENA2023071100783Unknown · unknownDURING HEAVY MAINTENANCE: ELONGATED HOLES (7EA) LOCATED ON FRAME 50 BTW STRINGER 4R TO STRINGER 5R; REPAIRED ELONGATED HOLES AT THE FR50 BTW STGR 4R-5R IAW EC NO. A23-556-01. REF AEROMAN WO 2023 134/1 NRC 2023 - 386504.'Jul 9, 2023 · N2086J · Airbus A321271NSDR YENA2023071100779Unknown · unknownFLT#2534, PBI-DCA. 'A/C DAMAGED ON FWD BELLY, BELOW FWD CARGO COMPARTMENT DUE TO G/O RAN BELT LOADER UNDER THE A/C SKIN.' (SUPPLEMENTAL INFORMATION TO FOLLOW)Jul 9, 2023 · N179JB · Emb ERJ190100IGWSDR DALA2023071005552Unknown · unknownSHIP 3123 CRACK INDICATION FOUND ON LH CONTINUITY FITTING LOCATED ON WINDSHIELD CENTER LOWER NODE FRAME 2. CORRECTIVE ACTION: COMPLIED WITH ER/A 608962-14. (2856382)Jul 9, 2023 · N323NB · Airbus A319114SDR DALA2023071005551Unknown · unknownSHIP 3123 EXISTING REPAIR ON FASTENER HOLES (#4, #5 AND #6) DOCUMENTED ON ER/A 565843-14AD. CORRECTIVE ACTION: COMPLIED WITH ER/A 565843-14AD. (2856353)Jul 9, 2023 · N323NB · Airbus A319114SDR DALA2023071005538Unknown · unknownSHIP 0687 CORROSION ON FRAME CLIP BTW STGR 28RH AND 29RH OF STA 1701 AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: FRAME CLIP BTW STGR 28RH AND 29RH OF STA 1701 AT AFT CARGO COMPARTMENT WAS FABRICATED PER DRAWING 140N2002 AND REPLACED PER B757-200 SRM. (2857224Jul 9, 2023 · N687DL · Boeing 757232SDR HNAA2023080700292Unknown · unknownE985210 R/H #2 FLOORBOARD SUPPORT HAS CORROSION. REMOVED AND REPLACED WITH SERVICABLE R/H #2 FLOORBOARD SUPPORT IAW EMB 145 SRM 51-40-02.Jul 8, 2023 · N644AE · Emb EMB145LRSDR HNAA2023080700291Unknown · unknownE985209 R/H #1 FLOORBOARD SUPPORT HAS CORROSION. REMOVED AND REPLACED WITH SERVICEABLE R/H #1 FLOORBOARD SUPPORT IAW EMB 145 SRM 51-40-02Jul 8, 2023 · N644AE · Emb EMB145LRSDR HNAA2023080700290Unknown · unknownE985174 PAX DOOR ENTRENCE AFT FLOORBOARD SUPPORT HAS CORROSION. REMOVED AND REPLACED PAX DOOR ENTRANCE AFT FLOORBOARD SUPPORT IAW EMB145 SRM 51-40-02Jul 8, 2023 · N644AE · Emb EMB145LRSDR DALA2023071205661Unknown · unknownCORROSION ON RH ANGLE CUSP FROM STA Y=200 TO Y=219 AT PAX CABIN. SUMMARY OF NRC 00253: CORROSION LEVEL 2. RH ANGLE CUSP FROM STA Y=160 TO Y=219 WAS REPAIRED PER ERA 609394-14 REV ORIGINAL SECTION I. PERMANENT REPAIR. ASSOCIATED ER/A 14-609394 ADDED FOR AC 9535Jul 8, 2023 · N992AT · Boeing 717200SDR DALA2023071205660Unknown · unknownCORROSION ON CUSP ANGLE BTW STA Y=158/171 APROX, BTW STA Y=195/207 APROX AND BTW RBL=54/60 AT PAX CABIN (W1). SUMMARY OF NRC 00413: CORROSION LEVEL 2. CUSP ANGLE BTW STA Y=158/171 APROX, BTW STA Y=195/207 APROX AND BTW RBL=54/60 WAS REPAIRED PER ER/A 609285-14Jul 8, 2023 · N957AT · Boeing 717200SDR GTIA2023071037318Unknown · unknownA/C VIBRATION ABOVE FL 230 330 KTS. DEGRADED CLIMB PERFORMANCE 300-500FPM. REAR VIBRATIONS MORE INTENSE THAN FWD.-PERFORMED TS PER TSM 05-50-00-810-801-A. PERFORMED ELEVATOR FREE PLAY CHECK PER TSM 05-50-00-810-801-A. NO DEFECTS NOTED AT THIS TIME. REF LP 3176Jul 8, 2023 · N616NK · Airbus A320232SDR DALA2023071005577Unknown · unknownSHIP 3123 CRACKS FOUND IN HOLES 5 AND 6. CORRECTIVE ACTION: REPAIRED PER ER/A 565843-14. (2855648)Jul 8, 2023 · N323NB · Airbus A319114SDR DALA2023071005579Unknown · unknownSHIP 0687 CORROSION ON BEAM BOX STA 1660 TO 1681.8 RBL 52 IT IS OUT OF LIMITS. ORIGINAL THICKNESS IS 0.071IN AND MINIMUM REMAINING THICKNESS ON STA 1660 TO 1681.8 BOTH AT RBL 52 IS 0.038IN. CORRECTIVE ACTION: SUMMARY OF NRC 00744: BEAM BOX STA 1660 TO 1681.8 RJul 8, 2023 · N687DL · Boeing 757232SDR CALA2023071002213Unknown · unknownOPENED AMES WORK PACK N19141-2 FOR 8C + GEAR MAINTAINENCE CHECK.Jul 7, 2023 · N19141 · Boeing 757200SDR SWI2023F00136Unknown · corrodedMAIN CABIN FORWARD WET AREA CROSS BEAM FR 16 HAS A SPOT OF CORROSION. (C-CHECK RO 7/21/2023) REMOVED AND REPLACED PANEL SUPPORT AT FR16. REF EMB SRM 51-40-08Jul 6, 2023 · N213SY · Emb ERJ170200LRSDR SWI2023F00135Unknown · corrodedMAIN CABIN FORWARD WET AREA LEFT INBOARD SEAT TRACK HAS (2) SPOTS OF CORROSION. (C-CHECK RO 7/21/2023) REMOVED AND REPLACED MAIN CABIN FORWARD WET AREA LEFT INBOARD SEAT TRACK REF SRM 51-40-08. THIS REPAIR DOES NOT AFFECT AIRCRAFT WEIGHT AND BALANCE, SEJul 6, 2023 · N213SY · Emb ERJ170200LRSDR SWIA20230721006Unknown · corrodedMAIN CABIN FORWARD WET AREA RIGHT INBOARD SEAT TRACK HAS (2) SPOTS OF CORROSION. (C-CHECK RO 7/21/2023) REMOVED AND REPLACE MAIN CABIN FORWARD WET AREA RIGHT INBOARD SEAT TRACKREF EMB SRM 51-40-08. THIS REPAIR DOES NOT AFFECT AIRCRAFT WEIGHT AND BALANCEJul 6, 2023 · N213SY · Emb ERJ170200LRSDR DALA2023072005874Unknown · unknownSHIP 3576 DENT DAMAGE COMMON TO THE FWD CARGO DOOR SURROUND STRUCTURE (P/N: V5327405320800 ). THE DENT MEASURES 1.75" L X 8.5"W X .218" D. REF FIGURE (1-3). THE DENTED AREA WHICH IS OUT OF ITS ORIGINAL CONTOUR MEASURES. CORRECTIVE ACTION: REF ERA 610294-14. (4Jul 6, 2023 · N576DZ · Airbus A350941SDR SWI2023F00312Unknown · corrodedDATUM 4 INTERCOSTAL BETWEEN APPROX FS320 - FS338 HAS CORROSION (C-CHECK RO 9/6/2023) INSTALLED NEWLY DRILLED INTERCOSTAL D4 BETWEEN FS320 - FS338 REF CRJ200 SRM 51-42-06 REF CRJ200 SRM 51-42-21 AND DWG 601R31702 REV-N. COMPLIED WITH 51-900-1003-SKY AND Jul 5, 2023 · N978SW · Cndair CL6002B19SDR SWIA20230705Unknown · corrodedDATUM 5 INTERCOSTAL BETWEEN APPROX FS338 - FS347 HAS CORROSION (C-CHECK RO 9/6/2023) REMOVED AND REPLACED INTERCOSTAL D5 BETWEEN FS338 - FS347 REF CRJ200 SRM 51-42-06, DWG 601R31702 REV-N. COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECK GOOD. SEE CONTJul 5, 2023 · N978SW · Cndair CL6002B19SDR SWI2023F00137Unknown · corrodedAFT WET AREA, LH FLOOR BEAM DOUBLER CORRODED AT FR90 (C-CHECK RO 7/21/2023) REMOVED AND REPLACED AFT WET AREA, LH FLOOR BEAM DOUBLER AT FR90 REF: EMB SRM 51-40-08, RESTORED SURFACE PROTECTION REF: EMB SRM 51-23-06, CPM 51-25-00-910-001-A. SEE CONTINUATIJul 5, 2023 · N213SY · Emb ERJ170200LRSDR DALA2023071005531Unknown · unknownSHIP 0676 CRACK ON INNER CHORD FRAME AT UPPER HINGE CUTOUT OF PASSENGER ENTRY DOOR R2. CORRECTIVE ACTION: INNER CHORD FRAME AT UPPER HINGE CUTOUT OF PASSENGER ENTRY DOOR R2 WAS REPAIRED PER B757-200 SRM 52-10. (2850996)Jul 5, 2023 · N676DL · Boeing 757232SDR UIEA2023071000735Unknown · unknownCRACK DAMAGE ON THE WEB OF STA 2231 FRAME AT S-21L AND S-22L(<P>1. REMOVED AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02-06-0. REV 97. 2. REPAIRED DAMAGE AREA IAW SRM 53-60-15-2R-3 REPAIR 3 FIG 203 PARAGRAPH 5 REV 97. 3. INSTALLED FASTENERS IAW SRM 57-40-0Jul 5, 2023 · N445MC · Boeing 7474B5FSDR UIEA2023071000736Unknown · unknownREPAIR - SKIN MODIFICATION FOR STATION 1640 TO 1740 LEFT SIDE AT STRINGER 34 PER SB 747-53A2487(<P>1. ACCOMPLISHED JOB IAW EI T2023A53M-1374 REV 1. 2. ACCOMPLISHED EI 72023A53M-1374 REV 2. 3. JOB ACCOMPLISHED AND COND CHK NORMAL.</P>)Jul 5, 2023 · N445MC · Boeing 7474B5FSDR UIEA2023071000737Unknown · unknownCRACK ON FASTENER HOLE OF TENSION TIE AFT CHANNEL AT STA 740 RH SIDE(<P>1. REMOVED AFFECTED FASTENER TO GET ACCESS IAW 51-40-02-0G-0. REV 97. 2. PERFORM EI T2023A53M-1451 REV 0 SEQUENCE A. 3. REINSTALL FASTENERS IAW SRM 51-40-02-0G-0. REV 97 AND DWG 14241023 SJul 5, 2023 · N445MC · Boeing 7474B5FSDR UIEA2023071000738Unknown · unknownCRACK ON FASTENER HOLE OF TENSION TIE AFT CHANNEL STA 760 RH SIDE(<P>1. REMOVED AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02-0G-0, REV 97. 2. PERFORM EI T2023A53M-1450, REV 0 SEQUENCE A. 3. REINSTALL FASTENERS IAW SRM 51-40-02-0G-0, REV 97 AND DWG 1424102Jul 5, 2023 · N445MC · Boeing 7474B5FSDR UIEA2023071000739Unknown · unknownFWD FLOOR STRUCTURE SUBSTITUTE TRACK CRACK AT M/D STA 980 LBL 75.92(<P>1. REMOVED FASTENERS IAW SRM 51-40-02-0G-0 REV97. 2. REPAIR SUBSTITUTE TRACK IAW SRM 53-00-52-2R-13. REPAIR 13 REV 97. 3. INSTALL REPAIR PARTS IAW SRM 53-00-52-2R-13. REPAIR 13 REV 97 AND DJul 5, 2023 · N445MC · Boeing 7474B5FSDR UIEA2023071000740Unknown · unknownDUE TO EO INSP WASHERS WERE NOT FOUND UNDER EACH FASTENER HEAD. REQUEST ADD EO PART 2 AND PART 5. PERFORMED NOSE WW FWD CORNER DOUBLER MODIFICATION NEAR STA 240, S-39 TO S-45(<P>1. PERFORM EI T2023A53M-1504 SEQUENCE A REV 0. 2. ACCOMPLISHED REPAIR AREA IAW EI Jul 5, 2023 · N445MC · Boeing 7474B5FSDR UIEA2023071000741Unknown · unknownFOUND FLOOR STRUCTURE SUBSTITUTE TRACK CRACK AT M/D STA 1540 RBL 75.92(<P>1. REMOVED FASTENERS IAW SRM 51-40-02-0G-0 REV 98. 2. REPAIR TRACK IAW SRM 53-00-52-2R-13 REPAIR 13 REV 98. 3. INSTALL REPAIR PARTS IAW SRM 53-00-52-2R-13 REPAIR 13 REV 98 AND DWG 65B382Jul 5, 2023 · N445MC · Boeing 7474B5FSDR UIEA2023071000744Shear Tie · unknownCRACK ON THE SHEAR TIE AT 1000 LBL 33.99 SB 747-53A2904(<P>1. REMOVED DAMAGE PART IAW SRM 51-40-02-0G-0 REV 97. 2. ACCOMPLISHED EI T2023A53M-1550 REV 0 AND SB 747-53A2904 FIG 8 & 9 REV 0 AND IAW EO 4453C024 PART 4 REV 3. 3. ACCOMPLISHED EI NO T2023A53M.1550 REJul 5, 2023 · N445MC · Boeing 7474B5FSDR UIEA2023071000745Shear Tie · unknownCRACK ON THE SHEAR TIE AT STA 1000 RBL 33.99 SB 747 53A2904(<P>1. REMOVED DAMAGE PART IAW SRM 51.40.02.0G.0 REV 97. ACCOMPLISHED EI T2023A53M-1550 REV 0, SB 747-53A2924 FIG 21, 22 REV0 AND EI ATTACHED TO W/O 8402500 (319) AND IAW EO 4453C024 PART 8 REV 3. 3. JJul 5, 2023 · N445MC · Boeing 7474B5FSDR UIEA2023071000746Fitting · unknownCRACK ON THE INTERCOSTAL LUG FITTING AT STA 1000 RBL 11.33, SB 747-53A2904(<P>1. REMOVED DAMAGE PART IAW SRM 51-40-02-0G-0 REV 97. 2. ACCOMPLISHED EI NO T2023A53M-1550 REV 0 AND SB 747-53A2904 FIG 17 & 18 REV 0 AND EI ATTACHED TO W/O 8402504 (319) AND EO 4453CJul 5, 2023 · N445MC · Boeing 7474B5FSDR UIEA2023071000747Cap · unknownCORROSION - FOUND MAIN DECK CGO FLOOR BEAM CAP CORROSION STA 2360 RBL 3.(<P>1. REMOVED DAMAGE PARTS IAW 51-40-02-0G-0 REV98. 2. INSTALL NEW PARTS IAW SRM 51-40-02-0G-0 REV98 AND BOEING DWG NO. 65B02634 SH 22 REV 4 AND DNG NO 65B06161 SH2 REV E, DWG NO. 65B3875Jul 5, 2023 · N445MC · Boeing 7474B5FSDR UIEA2023071000748Fitting · unknownCORROSION - 2EA CGO TRACK CORROSION AT R/H STA 2360 MAIN DECK FLOOR(<P>1. IAW AMM SUBTASK 53-44-00-212-001, REV107 REMOVE CGO TRACK 2. IAW AMM SUBTASK 53-44-00-020-001 REV 107 AND REFRENCE EI T2023A53M-1566, REV 0. INSTALL CGO TRACK. 3. JOB COMPLETED AND COND Jul 5, 2023 · N445MC · Boeing 7474B5FSDR CALA2023070702183Fitting · crackedWINDSHIELD LH CONTINUITY FITTING HAS A CRACK INDICATION AT UPPER FLANGE BEGINNING OF RADIUS PER HAECO LCQ N/R 9298605/44605 GEN BY V892444 REVISION. ON OR BEFORE 58900 TOTAL FLT CYCLES. PERFORM REPEAT THEREAFTER. INSPECTIONS AT INTERVALS NOT TO EXCEED 8800 FLTJul 5, 2023 · N825UA · Airbus A319131SDR SWAA2023081074776Support · corrodedFLOOR TO SIDEWALL SUPPORT HAS CORROSION BS 727A+5 - 727E+3 LBL 20 WL 156<[01] VERIFIED APPLICABILITY FOR ALLOWABLE DAMAGE LIMITS OF ACB FLOOR TO SIDEWALL SUPPORT; BS727A+5 727E+3 LBL 20 WL 156 IAW SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2.;[05] FABRIACATED LOCATED Jul 4, 2023 · N965WN · Boeing 7377H4SDR SWAA2023080480713Filler · missingMISSING FILLER STRUCTURE LOCATED BS727 LOWER STRUCTURE WING TO BODY FAIRING LOWER FUSELAGE 2 E/A 2023-422544<[01] REPLACED FILLER STRUCTURE LOCATED BS727 LOWER STRUCTURE WING TO BODY FAIRING LOWER FUSELAGE 2 E/A IAW B737-700 SRM 51-10-02 AND DWG AND DWG149A751Jul 4, 2023 · N228WN · Boeing 7377H4SDR SWAA2023070675187Panel · delaminatedFOUND DELAMINATION ON PANEL 194FR<[01] SEE TASK 23-153-02086 FOR WORK PERFORMED.Jul 4, 2023 · N214WN · Boeing 7377H4SDR SWIA20230724003Unknown · corrodedCORROSION, AFT WET AREA, ON RH LONGITUDINAL FLOOR BEAM AT FRAME 87 WHERE THE BEAM PASSES BETWEEN THE CENTER AND RH SHEAR PANELS. (C-CHECK RO 7/21/2023) REPAIRED AFT WET AREA, ON RH LONGITUDINAL FLOOR BEAM AT FRAME 87 WHERE THE BEAM PASSES BETWEEN THE CEJul 3, 2023 · N181SY · Emb ERJ170200LRSDR DXTA2023070390280Unknown · unknownVIBRATION IN AIRFRAME OR ENGINE. TAKE OFF WAS NORMAL COMING THROUGH 5000FT I STARTED TO NOTICE WHAT SEEMED LIKE LIGHT CHOP. CONTINUED CLIMB UP TO 15000FT LEVELED OFF AND IMEDIATLY NOTICED VIBRATION. THERE WAS NO CAS MESSAGE. WE RAN THE ENGINE VIBRATION CHECKJul 3, 2023 · N368QS · Cessna 680CESDR NACA2023070100003Unknown · unknownSX NR 6500161621 - PITTING CORROSION FOUND ON THE FUSELAGE EXTERNAL SKIN ABOUT 2" AFT OF STA1832 AND 9" ABOVE THE RH SIDE APU DOOR HINGE. THE CORROSION REMOVED AND MEASURED: THE ORIGINAL THICKNESS T=0.030", THE DEPTH OF CLEANUP X=0.002" < 15%T. FOUND WITHIN LIJul 3, 2023 · N399CM · Boeing 767323SDR UIEA2023070600718Unknown · unknownDEVIATION - DURING PERFORMING TASK CARD 4453A087 PART 2, THE EXISTING CONDITION IS DIFFERENT WITH DWG AT STA 440 LH SIDE(<P>1) ACCOMPLISHED JOB IAW EI T2023A53M-1564 REV 0. 2) ACCOMPLISHED IAW EI T2023A53M-1564 REV 1. 3) JOB COMPLETED AND CONDITION CHECK NORMAJul 3, 2023 · N450PA · Boeing 74746NFSDR UIEA2023070600717Unknown · unknownDEVIATION - DURING PERFORMING TASK CARD 4453A087 PART 2 EXISTING CONDITION IS DIFFERENT WITH DWG AT STA 340 RH SIDE(<P>1) ACCOMPLISHED JOB IAW EI T2023A53M-1571 REV 0. 2) ACCOMPLISHED IAW EI T2023A53M-1571 REV 1. 3) JOB COMPLETED AND CONDITION CHECK NORMAL</P>Jul 3, 2023 · N450PA · Boeing 74746NFSDR UIEA2023070600714Unknown · unknownDEVIATION - DURING PERFORMING TASK CARD 4453A087 PART 2 EXISTING CONDITION IS DIFFERENT WITH DWG AT STA 340 LH SIDE(<P>1) ACCOMPLISHED JOB IAW EI T2023A53M-1572 REV 0. 2) ACCOMPLISHED EI T2023A53M-1572 REV 1. 3) JOB COMPLETED AND CONDITION CHECK NORMAL</P>)Jul 3, 2023 · N450PA · Boeing 74746NFSDR UIEA2023070600713Unknown · unknownDEVIATION - DURING PERFORMING TASK CARD 4453A087 PART 2 EXISTING CONDITION IS DIFFERENT WITH DWG STA 500 RH SIDE(<P>1) ACCOMPLISHED JOB IAW EI T2023A53M-1557 REV 0. 2) ACCOMPLISHED EI T2023A53M-1557 REV 1. 3) JOB COMPLETED AND CONDITION CHECK NORMAL</P>)Jul 3, 2023 · N450PA · Boeing 74746NFSDR UIEA2023070600712Unknown · unknownFOUND L5 DOOR FRAME WEB CRACK AT STA 2231 S21L - S22L(<P>1) REMOVED AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02-0G-0 REV 97. 2) REPAIRED DAMAGE AREA IAW SRM 53-60-15-2R-3 REPAIR 3 REV 97 AND EI T2023A53M-1537 REV 0. 3) INSTALLED FASTENERS IAW SRM 53-60-1Jul 3, 2023 · N450PA · Boeing 74746NFSDR DALA2023070405373Unknown · unknownCORROSION ON DOOR JAMB SEVERAL POINTS AT AFT COMPARTMENT (C2). SUMMARY OF NRC 00176: CORROSION LEVEL 2. DOOR JAMB AT AFT COMPARTMENT WAS REPLACED PER B717 SRM 51-41-02-0G & 51-41-05-0G. (LP #2848116)Jul 3, 2023 · N992AT · Boeing 717200SDR DALA2023070405371Unknown · unknownDURING REMOVAL OF FLOOR SUPPORT, CRACK AND CORROSION ON CUSP WEB Y=199 TO Y=160 X54 (CPAX) WAS FOUND. SUMMARY OF NRC 00598: CORROSION LEVEL 2. CUSP WEB WAS REPAIRED PER B-717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #2847871)Jul 3, 2023 · N924AT · Boeing 717200
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