JASC 5300

Service difficulty reports · 8,206

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 COMA0160796Frame · crackedR/H 718.00 FRAME UPPER AND LOWER FLANGE IS CRACKED BETWEEN STRINGER 11 AND 12.REMOVED CRACKED SECTION OF R/H 718.00 FRAME AND REPAIRED USING NEW SECITON OF FRAME I/A/W CANADAIR REO 601R-53-61-193 REV A.Oct 3, 2001 · N708CA · Cndair CL6002B19SDR COMA0160795Doubler · crackedL/H AFT DOUBLER AT F.S. 718.00 BETWEEN STRINGER 11 AND 12 IS CRACKED.REMOVED CRACKED L/H AFT DOUBLER AT F.S. 718.00 AND INSTALLED NEW DOUBLER I/A/W CANADAIR REO 601R-53-61-193 REV A.Oct 3, 2001 · N708CA · Cndair CL6002B19SDR COMA0160773Doubler · crackedR/H AFT DOUBLER AT F.S. 718.00 BETWEEN STRINGER 11 AND 12 IS CRACKED.REMOVED CRACKED R/H AFT DOUBLER AT F.S. 718.00 AND INSTALLED NEW DOUBLER I/A/W CANADAIR R.E.O. 601R-53-61-193 REV A.Oct 3, 2001 · N708CA · Cndair CL6002B19SDR COMA0160772Doubler · crackedL/H AFT DOUBLER AT F.S. 718.00 BETWEEN STRINGER 11 AND 12 IS CRACKED.REMOVED CRACKED L/H AFT DOUBLER AT F.S. 718.00 AND INSTALLED NEW DOUBLER I/A/W CANADAIR R.E.O. 601R-53-61-193 REV A.Oct 3, 2001 · N708CA · Cndair CL6002B19SDR COMA0160771Frame · crackedR/H 718.00 FRAME UPPER AND LOWER FLANGE IS CRACKED BETWEEN STRINGER 11 AND 12.REMOVED CRACKED SECTION OF R/H 718.00 FRAME AND REPAIRED USING NEW SECTION OF FRAME I/A/W CANADAIR R.E.O. 601R-53-61-193 REV. A.Oct 3, 2001 · N708CA · Cndair CL6002B19SDR COMA0160770SkinFLIGHT 5774. BIRDSTRIKE DURING T/O. T/O ABORTED.C/W BIRDSTRIKE INSPECTION. NO DAMAGE FOUND. C/W REJECTED T/O INSPECTION NO DAMAGE FOUND.Sep 30, 2001 · N784CA · Cndair CL6002B19SDR USAA011292Seat Track · corrodedCLT - FOUND SEAT TRACK CORRODED 1 INCH BY 1 INCH, RBL 45 BS 1013 FLOOR LEVEL. FABRICATED AND INSTALLED NEW SEAT TRACK PER SRM 51-10-2. (M)Sep 25, 2001 · N265AU · Boeing 737201SDR QXEA0101596Seal · dentedPDX - MAIN CABIN DOOR MATING FACE IS DENTED MIDWAY ALONG THE AFT LENGTH OF DOOR APERATURE. REPAIRED IAW EA R-53-02Sep 25, 2001 · N601QX · Cndair CL600*SDR QXEA0101592Seal · dentedPDX - MAIN CABIN DOOR SEAL MATING SURFACE DENTED MIDWAY ALONG THE AFT LENGH OF DOOR APERTURE. REPAIRED IAW EA R-53-03Sep 25, 2001 · N606QX · Cndair CL600*SDR COMA0160752StructureFLIGHT #5574. DURING CLIMB OUT OF GRB AIRCRAFT ENCOUNTERED MULTIPLE BIRD STRIKES, RETURNED TO THE FIELD.PERFORMED BIRD STRIKE INSPECTION, NO DAMAGE NOTED.Sep 25, 2001 · N995CA · Cndair CL6002B19SDR SIMA200126509Track · corrodedSBP - FOUND CARGO SEAT TRACK AT STATIONB BL 0.0 IS CORRODED ON THE FLANGE AND WEB, SPLICED IN NEW SECTION OF TRACK 67.75 INCHES IAW SAAB SRM 53-70-60. (M)Sep 21, 2001 · N305AE · Saab 340BSDR SIMA200126508Track · corrodedSBP - FOUND CARGO SEAT TRACK SECTION STATION 18.3 LEFT SIDE IS CORRODED ON THE FLANGE AND WEB, SPLICED IN NEW 67.75 INCHES OF TRACK IAW SAAB SRM 53-70-60. (M)Sep 21, 2001 · N305AE · Saab 340BSDR SIMA200126507Track · corrodedSBP - FOUND SEAT TRACK AT STATION 18.3 LEFT SIDE IS CORRODED AT FRONT SPLICE. REMOVED AND REPLACED SEAT TRACK AND U-BEAM IAW SAAB SRM 53-70-60. (M)Sep 21, 2001 · N305AE · Saab 340BSDR SIMA200126506Track · corrodedLAVATORY TRACK AND PROFILE ARE CORRODED. REMOVED AND REPLACED LAVATORY TRACK AND PROFILE IAW SAAB SRM 51-40-21. (M)Sep 21, 2001 · N305AE · Saab 340BSDR SIMA200126504Track · corrodedSBP - AIRSTAIR TRACK CORRODED, REMOVED AND REPLACED AIRSTAIR TRACK IAW SAAB SRM 51-40-21 AND 51-40-22. (M)Sep 21, 2001 · N305AE · Saab 340BSDR ASOA01179Skin Panel · corrodedDURING SCHEDULED MAINTENANCE IN MCN, CORROSION WAS FOUND ON THE SKIN AT FRAMES 22 AND 23, BETWEEN STRINGERS 20 LEFT AND 20 RIGHT. MAINTENANCE REPAIRED AIRCRAFT IAW ASA EO120-53-0167. THIS EO STATES REPAIR SPECIFICATIONS FOR FRAME 22 AND 23 SKIN CORROSION REPSep 20, 2001 · N501AS · Emb EMB120ERSDR USAA011242SkinCLT - FOUND SKIN CRACKED 1.25 INCH, BS 727D STRINGER 23L. INSTALLED DOUBLER PER TR NR 53-60-03. (M)Sep 18, 2001 · N531AU · Boeing 7373B7SDR COMA0160748Threshold · corrodedTHE THRESHOLD/SILL PANEL FORWARD OF THE SERVICE DOOR IS CORRODED.REMOVED CORRODED THRESHOLD AND REPLACED WITH FABED THRESHOLD I/A/W WVAC EO 601R-53-2716.Sep 17, 2001 · N969CA · Cndair CL6002B19SDR COMA0160747Angle · corrodedTHE THRESHOLD SUPPORT ANGLE AT THE PASSENGER DOOR IS CORRODED.REMOVED CORRODED THRESHOLD SUPPORT ANGLE. FABED NEW THRESHOLD SUPPORT ANGLE AND INSTALLED I/A/W WVAC EO 601R-53-2717.Sep 17, 2001 · N969CA · Cndair CL6002B19SDR COMA0160746Doubler · corrodedTHE DOUBLER FORWARD OF THE SERVICE DOOR IS CORRODED P/N 601R38669-49.REMOVED AND REPLACED DOUBLER FORWARD OF SERVICE DOOR WITH NEW P/N 601R38669-49 I/A/W WVAC EO 601R-53-2719.Sep 17, 2001 · N969CA · Cndair CL6002B19SDR COMA0160744Angle · crackedTHE VERTICAL J ANGLE CLIP LOCATED INSIDE OF CBP1 AT LBL9 L/II SIDE WAS FOUND CRACKED.REMOVED AND REPLACED VERTICAL J ANGLE CLIP INSIDE OF DBPJ WITH NEW ANGLE P/N 600-34017-723S I/A/W WVAC EO 601R-53-2720.Sep 17, 2001 · N969CA · Cndair CL6002B19SDR COMA0160743Angle · corrodedTHE FORWARD J ANGLE AT F.S. 280.00 BETWEEN LBL9 AND RBL9 IS CORRODED.REMOVED AND REPLACED FORWARD J ANGLE AT F.S.280.00 BETWEEN LBL9 AND RBL9 WITH NEW P/N 6000-34017-351 ANGLE I/A/W WVAC EO 601R-53-2718.Sep 17, 2001 · N969CA · Cndair CL6002B19SDR COMA0160726Threshold · corrodedTHE THRESHOLD/SILL PANEL FORWARD OF THE SERVICE DOOR IS CORRODED.REMOVED CORRODED THRESHOLD AND REPLACED WITH FABED THRESHOLD I/A/W WVAC EO 601R-53-2716.Sep 17, 2001 · N969CA · Cndair CL6002B19SDR COMA0160725Angle · corrodedTHE THRESHOLD SUPPORT ANGLE AT THE PASSENGER DOOR IS CORRODED.REMOVED CORRODED THRESHOLD SUPPORT ANGLE. FABED NEW THRESHOLD SUPPORT ANGLE AND INSTALLED I/A/W WVAC EO 601R-53-2717.Sep 17, 2001 · N969CA · Cndair CL6002B19SDR COMA0160724Angle · corrodedTHE FORWARD J ANGLE AT F.S. 280.00 BETWEEN LBL9 AND RBL9 IS CORRODED.REMOVED AND REPLACED FORWARD J ANGLE AT F.S. 280.00 BETWEEN LBL9 AND RBL9 WITH NEW P/N 6000-34017-351 ANGLE I/A/W WVAC EO 601R-53-2718.Sep 17, 2001 · N969CA · Cndair CL6002B19SDR COMA0160723Angle · crackedTHE VERTICAL J ANGLE CLIP LOCATED INSIDE OF CBP1 AT LBL 9 L/H SIDE WAS FOUND CRACKED.REMOVED AND REPLACED VERTICAL J ANGLE CLIP INSIDE OF CBP1 WITH NEW ANGLE P/N 600-34017-723S I/A/W WVAC E.O. 601R-53-2720.Sep 17, 2001 · N969CA · Cndair CL6002B19SDR COMA0160722Doubler · corrodedTHE DOUBLER FORWARD OF THE SERVICE DOOR IS CORRODED P/N 601R38669-49.REMOVED AND REPLACED DOUBLER FORWARD OF SERVICE DOOR WITH NEW P/N 601R38669-49 I/A/W WVAC EO 601R-53-2719.Sep 17, 2001 · N696CA · Cndair CL6002B19SDR USAA011255Frame · crackedPIT - FOUND FRAME CRACKED .125 INCH CRACK, STATION 787 AT RIVET HOLD ABOVE S9R. CLEANED UP CRACK, INSTALLED .25 INCH RIVET PER TYPICAL REPAIR 53-14-01. (M)Sep 16, 2001 · N387US · Boeing 7373B7SDR DL72S011531Web · crackedCRACK AT UPPER FASTNER VERTICAL WEB L/H SIDE STA 1223 REPAIRED PER M/M 57-11-000-8Sep 14, 2001 · N517DA · Boeing 727232SDR USAA011234Intercostal · crackedCLT - FOUND INTERCOSTAL 1.5 INCH, BS 180 WL 195 RBL 26. REMOVED AND REPLACED INTERCOSTAL PER EO 5300V157. (M)Sep 12, 2001 · N275AU · Boeing 7372B7SDR USAA011227Frame · dentedFOUND FRAME DENTED .75 INCH BY 1.25 INCH, AFT CARGO BS 1540. INSTALLED REPAIR DOUBLER PER EA NR 85390. (M)Sep 10, 2001 · N633AU · Boeing 7572B7SDR USAA011224Web · crackedCLT - FOUND WEB CRACKED .75 INCH, BS 178, LBL 10, WL 234. REPAIR DOUBLER INSTALLED PER EA 85403. (M)Sep 10, 2001 · N275AU · Boeing 7372B7SDR COMA0160709RadomeFLIGHT #5420. DURING TAKE OFF AT CVG AIRCRAFT ENCOUNTERED MULTIPLE BIRD STRIKES ON RADOME, TAKE OFF WAS ABORTED AND RETURNED TO THE GATE.PERFORMED BIRD STRIKE AND HIGH ENERGY STOP INSPECTION, NO DEFECTS NOTES.Sep 10, 2001 · N952CA · Cndair CL6002B19SDR COMA0160696Angle · crackedPERFORMED A MAJOR REPAIR TO THE L/H AND R/H VERTICAL J-ANGLES AT F.S. 280, BL 9.0 L/H AND R/H BY REMOVING THE CRACKED ANGLES AND INSTALLING FABRICATED ANGLES I/A/W WVAC EO 601R-53-2705.Sep 8, 2001 · N948CA · Cndair CL6002B19SDR ASOA01168Seat Track · corrodedDURING C-CHECK INSPECTION IN BNA, MAINTENANCE DISCOVERED CORROSION ON THE RIGHT OUTBOARD SEAT TRACK AND FLANGES (TOP AND BOTTOM) SURFACES BETWEEN FRAMES 29 AND 36. MAINTENANCE REPAIRED CORROSION IAW ASA EO 72-53-0115. (M)Sep 6, 2001 · N632AS · Aerosp ATR72SDR USAA011211SkinCLT - FOUND SKIN PLUG FLUCH PATCH 1 INCH, STATION 475 AT 30-29R E/E MAIN BAY DOOR. PREVIOUSLY INSTALLED REPAIR (FLUCH PATCH) PER SRM 52-40-01 FIG 201. (M)Sep 5, 2001 · N601AU · Boeing 757225SDR DL72W011490Angle · cracked1 IN. CRACK GUSSET ANGLE AFT SIDE STA 1263 R/H TORQUE BOX REPAIRED PER M/M 53-11-000-8Sep 5, 2001 · N296WA · Boeing 727247SDR USAA011202Frame · corrodedCLT - FOUND FRAME CORRODED 5 INCHES, BS 415 STRINGER 25R. REMOVED DAMAGED SECTION OF STRINGER 25R, ADD STRINGER SPLICE J CHANNEL DOUBLER AND CENTER U-CHANNEL EA 85157, SRM 53-10-3. (M)Sep 4, 2001 · N264AU · Boeing 737201SDR COMA0160683Angle · crackedTHE INTERCOSTAL FLANGE AT RBL36 AND ANGLES AT BL 27LH AND RH ARE CRACKED.REMOVED AND REPLACED CRACKED ANGLES I/A/W WVAC E.O. 601R-53-2675A.Sep 2, 2001 · N966CA · Cndair CL6002B19SDR 2001UALA01949Intercostal · corrodedBODY STATION 317 LBL 12 WL 110 INTERCOSTAL CORRODED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED DOUBLER.Aug 31, 2001 · N603UA · Boeing 767222SDR USAA011177Skin · crackedTPA - FOUND SKIN CRACKED 1.3 INCHES, STATION 947.5 LOWER FORWARD CORNER OF HINGE CUT OUT. INSTALLED DOUBLERS PER SRM 53-60-01 FIG 208. (M)Aug 30, 2001 · N340US · Boeing 737301SDR ABXA010460Structure · vibrationTHERE WAS A LOUD NOISE ON BOTH SIDES OF THE COCKPIT AND AIRFRAME VIBRATION AT AIRSPEEDS ABOVE 310 AT 10,000 TO 20,000 FOOT ALTITUDES. INSPECTED FLAPS, GEAR WELL AREAS, FLIGHT CONTROLS. RAN FLIGHT CONTROLS THRU. PRESSURIZED AIRCRAFT TO 6 PSI. INSPECTED MEC Aug 30, 2001 · N787AX · Boeing 767281SDR USAA011169Frame · corrodedCLT - FOUND FRAME CORRODED, BS 807 STRINGER 17R TO STRINGER 27R, CORROSION LEVEL 1 TASK NR C53-100-01. (M)Aug 29, 2001 · N264AU · Boeing 737201SDR USAA011161Web · crackedCLT - FOUND WEB CRACKED .5 INCH, BS 178 BULKHEAD WL 2.8, LBL 11.7. CUT OUT DAMAGE FABRICATED FILLER AND DOUBLER PER EA 85310 AND SRM 53-10-08 FIG 211. (M)Aug 29, 2001 · N273AU · Boeing 7372B7SDR USAA011159Web · crackedCLT - FOUND WEB CRACKED .6 INCHES, BS 178, WL 188 AT RBL .5 AND LBL .5 INCH. INSTALLED WEB REPAIR PER EA 85310, EO 5300V152. (M)Aug 29, 2001 · N273AU · Boeing 7372B7SDR SIMA200124204Floor Support · corrodedSAW - DURING CPCP2 INSPECTION, FOUND CORROSION ON THE LEFT AND RIGHT FLOOR SUPPORTS FROM FRAME 36 TO FRAME 38. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW ATR SRM 51-25-01 AND 51-25-02. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Aug 29, 2001 · N242AT · Aerosp ATR42300SDR SIMA200124205Sill · corrodedSAW - DURING CPCP4 INSPECTION, FOUND CORROSION ON PASSENGER ENTRY SILL AND THE SERVICE DOOR SILL PLATES. THE SILLS WERE REMOVED AND REPLACED IAW ATR72 SRM 51-25-01 AND 51-25-02. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Aug 29, 2001 · N536AT · Aerosp ATR72212ASDR SIMA200124207Seat Track · corrodedSAW - DURING CPCP4 INSPECTION, FOUND CORROSION ON THE LEFT AFT OUTBOARD, RIGHT AFT OUTBOARD, LEFT F/A, RT F/A AND LT AFT CARGO SEAT TRACKS. THE SEAT TRACKS WERE REMOVED AND REPLACED IAW EO E2-53MR-115. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Aug 29, 2001 · N536AT · Aerosp ATR72212ASDR SIMA200124208Floor Support · corrodedSAW - DURING CPCP4 INSPECTION, FOUND CORROSION ON THE LT FLOOR SUPPORT BETWEEN FRAMES 36 AND 38. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-25-02. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Aug 29, 2001 · N536AT · Aerosp ATR72212ASDR SIMA200124209Seat Track · corrodedSAW - DURING CPCP4 INSPECTION, FOUND CORROSION ON THE LEFT AFT INBOARD, LEFT AFT OUTBOARD AND RIGHT FLIGHT ATTENDANT SEAT TRACKS. THE SEAT TRACKS WERE REMOVED AND REPLACED IAW EO E2-53-115R1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Aug 29, 2001 · N538AT · Aerosp ATR72212A
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