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 JJBA20220206006Not Reported · not reportedPOSSIBLE CORROSION ON CABIN LATERAL FLOOR SUPPORT FRAMES 41-48 STR 15R. REMOVED CORROSION AT LATERAL FLOOR SUPPORT FRAME 41-48 STR 15R.Feb 6, 2022 · N13202 · Emb EMB145XRSDR DALA2022020700774None · noneSHIP 3247 CRACK INDICATION ON FRAME 36 CWB FRONT SPAR VERTICAL STRINGER POSITION 5 AT OPEN FASTENER HOLE ZONE 2. CORRECTIVE ACTION: REPAIRED PER PRI 596350-14AD REV.0, REV.1 AND ERA 596350-14AD REV. ORIGINAL. (2112932)Feb 6, 2022 · N347NW · Airbus A320212SDR CALA2022020700332Intercostal · crackedSUPPORT TASK STA 1640 STR 10L WEB CRACKED AT AFT CTR HOLE ON INS TALL. WEB PN 146N8738-15, TRANSCRIBED FROM HAECO GSO NON ROUTINE 9281722 FABRICATED INTERCOSTAL WEB 146N8738-15 AND INSTALLED IAW B757-30 0 SRM 51-40-02 AND BAC DWG 146N8738 REV G. HAECO GSO MECHFeb 6, 2022 · N57870 · Boeing 75733NSDR JR2R20220206457Seat Track · corrodedLH FWD SEAT TRACK LUG CORRODEDFeb 6, 2022 · N88341 · Emb ERJ170200LRSDR JJBA20220205004Not Reported · not reportedSIGNS OF CORROSION AT MULTIPLE LOCATIONS ON THE GUSSET OF THE OMEGA BEAM Y=429.0 FROM FR 65 TO FR 68. REMOVED CORROSION AT FRAME 65-68 Y-479 BEAM GUSSET.Feb 5, 2022 · N13202 · Emb EMB145XRSDR EE4Y2022020515090Frame · crackedDESCRIPTION: DURING THE ALLEGIANT E.O. NO: E5316-0002 REV:00 INSPECTIONS AS RELATED TO THE REF. AD: 2019-20-10, ALI: 531103-01-01, SB: 53-1330, IT WAS FOUND INTERCOSTAL FITTINGS WITH CRACK AND FRAME WITH CORROSION ACTION INTERCOSTAL FITTING REPLACED PER Feb 5, 2022 · N311NV · Airbus A319111SDR EE4Y2022020515089Frame · crackedDURING SPECIAL DETAILED INSPECTION ON SERVICE DOOR FRAME FR16 AS PER REF. TASK CARD 531153-02-2-001 INSTRUCTIONS, IT WAS FOUND AT FWD SERVICE DOOR AREA, FR16 BETWEEN STR 10R-11R, FRAME OUTER FLANGE WITH CRACK AT DOOR STOP 7 LEVEL ACTION REPAIR WAS PERFORMED Feb 5, 2022 · N311NV · Airbus A319111SDR EE4Y2022020515088Beam · crackedDURING THE STRUCTURE INSPECTION, IT WAS FOUND THE SIDEBOX BEAM FLANGE AT LH IN S15 FR 43 AREA WITH CRACK ACTION: PERFORMED PERMANENT REPAIR AT THE SIDEBOX BEAM FLANGE AT LH IN S15 FR 43 AREA PER ALLEGIANT EO # E5331-0009 AND E5331-0010. THIS EO, BASED ON SB Feb 5, 2022 · N311NV · Airbus A319111SDR EE4Y2022020515087Angle · unknownPER ALLEGIANT AIR EO 5331-0008 AD 2019-08-07 MODIFICATION REPLACEMENT OF KEEL BEAM TITANIUM ANGLES BETWEEN FR40/42 LH/RH HAS BEEN ACOMPLISHED.Feb 5, 2022 · N311NV · Airbus A319111SDR EE4Y2022020515086Skin Panel · corrodedDURING THE STRUCTURE INSPECTION, IT WAS FOUND REAR FUSELAGE PASSENGER/CREW DOOR LH CUT OUT AREA FROM FR68 TO FR69+150MM SILL WITH CORROSION. ACTION: PERFORMED PERMANENT REPAIR AT PAX/CREW DOOR LH LOWER SILL WEB FROM FR68 AND FR68+160MM, +Y 1260 IAW A319 SRFeb 5, 2022 · N311NV · Airbus A319111SDR EE4Y2022020515085Skin Panel · corrodedDURING THE STRUCTURE INSPECTION, IT WAS FOUND EXTERNAL LOWER REAR FUSELAGE BETWEEN 150MM AFT OF FR69 AND 200MM OF FR70, STRG 31R AND STRG 32R SKIN WITH CORROSION. ACTION: PERFORMED PERMANENT REPAIR AT REAR FUSELAGE BETWEEN 115MM AFT OF FR69 AND 175MM FWD OFeb 5, 2022 · N311NV · Airbus A319111SDR SWIA202264573None · crackedFR 52 EXTERNALSUPPORT ANGLE IS CRACKED THROUGH THE O/B FASTENER FWD OF THE LH MLG WHEEL WELL AREA AS MARKED. (C CHECK RO 02/21/2022) REMOVED AND REPLACED FR 52 EXTERNAL SUPPORT ANGLE FWD OF THE LH MLG WHEEL WELL REF SRM 51-40-08. SE CONTINUATION CARD FOR WOFeb 4, 2022 · N241SY · Emb ERJ170200LRSDR NACA2022020400001Not Reported · not reportedCRACK INDICATIONS AT BS 360+11 @ STRINGER 19R - 11/16 AND 1 3/4 INCHES. BS 727E +12 AND STR 23R - 2 5/16 INCHES. B727D+15 AND STR 23 R - 3 3/4 INCHES. REPAIR PERFORMED IAW SRM 53-00-01 REPAIR 31.Feb 4, 2022 · N360WA · Boeing 737300SDR UIEA2022020200083None · noneCRACK ON FWD UPPER CHORD AT STA 1809.5 BULKHEAD, STRINGER S-7LH.(<P ><SPAN>REPAIR WAS INSTALLED ON FWD UPPER CHORD AT STA 1809.5 AND STRINGERS S-6LH TO S-8LH PER 767 SRM 53-80-08 REPAIR 9</SPAN></P> / <P> </P>)Feb 4, 2022 · N1409A · Boeing 767306SDR UIEA2022020200087Splice · noneCORROSION ON SPLICE TEE P/N 145T8629-2 OF KEEL BEAM FAIRING PANEL AT STA 887 APPROXIMATELY(<P ><SPAN>AFFECTED SPLICE TEE P/N 145T8629-2 WAS REPLACED PER 767 SRM 51-10-02-0G-0 PAR. 9 & 767 IPC 53-52-54-01 ITEM 25</SPAN></P> / <P> </P>)Feb 4, 2022 · N1409A · Boeing 767306SDR CALA2022020700326Frame · crackedL/H AFT FR 68 DOORSTOP FITTING #3 O/B LOWER (D1) HAS CRACK INDIC ATION NOTED IN HOLE. IAW NTM 51-10-01 PT6. INSTALLED FREEZE PLUG AND WASHERS. REINSTA SHOLD FROM TIME OF ADL/REPAIR EMBODIMENT 24500 FC (FH NOT RELEVA ETHOD NTM 51-10-08 AND ROTO TEST REF TO AMM Feb 4, 2022 · N475UA · Airbus A320232SDR CALA2022020700325Frame · crackedL/H AFT FR 68 DOORSTOP FITTING #1 I/B LOWER (D1) HAS CRACK INDIC ATION NOTED IN HOLE IAW NTM 51-10-01 PT6. INSTALLED FREEZE PLUG AND WASHERS. REINSTA SHOLD FROM TIME OF ADL/REPAIR EMBODIMENT 24500 FC (FH NOT RELEVA ETHOD NTM 51-10-08 AND ROTO TEST REF TO AMM 5Feb 4, 2022 · N475UA · Airbus A320232SDR IXXA2022020403Skin · corrodedFUS.. SKIN DAMAGEDFeb 4, 2022 · N762CX · Boeing 767232SDR IXXA2022020402Stringer Fitting · corrodedSTRINGER FITTING CORRODED BEYOND LIMITSFeb 4, 2022 · N762CX · Boeing 767232SDR SWIA202264940None · crackedLH UPPER TRANSCOWL OUTER SKIN AND LATCH DOOR COAMING CRACKED FWD & AFT OF THE FWD LATCH CUTOUT. (C-CHECK RO 3/11/2022) REMOVED AND REPLACED CRACKED LATCH DOOR COAMING P/N CN624-2060-209. PERFORMED REPAIR TO CRACKS ON THE OUTER SKIN AND INNER PERFORATED Feb 3, 2022 · N732SK · Cndair CL6002C10SDR SWIA202264565None · crackedCRACK ON L/H WEB L-ANGLE BRACKET AT FR52 AS MARKED. (C CHECK RO 2/20/2022) / REMOVED AND REPLACED CRACKED L-ANGLE AT FR52 REF SRM 51-40-02.Feb 3, 2022 · N167SY · Emb ERJ170200LRSDR R61A2022021300135Gusset · corrodedWHILE AC WAS IN FOR HVY CK FOUND.CF3 FLOOR STRUCTURE CORROSION FOUND ON RH SPLICE GUSSET PLATE AT FR 89. MX REPLACED GUSSET PLATE PN 170-86125-001 IAW SRM 51-43-03.. AC REMAINS IN YQG FOR COMPLETION.Feb 3, 2022 · N744YX · Emb ERJ170200LRSDR R61A2022021300134Seat Track · corrodedWHILE AC WAS IN FOR HVY CK FOUND.FWD FUSELAGE FLOOR STRUCTURE CORROSION FOUND ON LH SEAT TRACK BTWN FR 19-20. MX REPLACED SEAT TRACK PN 170-03264-001 IAW SRM 51-41-01, 51-40-02, 51-43-03, 51-43-04. . AC REMAINS IN YQG FOR COMPLETION.Feb 3, 2022 · N744YX · Emb ERJ170200LRSDR R61A2022021300133Support · corrodedWHILE AC WAS IN FOR HVY CK FOUND. CF3 FLOOR STRUCTURE CORROSION FOUND ON RH FLOOR SUPPORT BTWN FR 88-90. MX REPLACED SUPPORT PN 170-86181-005 IAW SRM 53-23-10, 51-41-02. AC REMAINS IN YQG FOR COMPLETION.Feb 3, 2022 · N744YX · Emb ERJ170200LRSDR R61A2022021300132Beam · corrodedWHILE AC WAS IN FOR HVY CK FOUND. CF3 FLOOR STRUCTURE CORROSION FOUND ON RH UPPER BEAM AT FR 87. MX REPLACED BEAM PN 170-65669-004 IAW SRM 51-43-03, 51-41-01, 51-42-01. AC REMAINS IN YQG FOR COMPLETION.Feb 3, 2022 · N744YX · Emb ERJ170200LRSDR R61A2022021300131Shear Panel · corrodedWHILE AC WAS IN FOR HVY CK FOUND. CF3 FLOOR STRUCTURE CORROSION FOUND ON RH SHEAR PLATE BTWN FR87-88. MX REPLACED SHEAR PLATE PN 170-91919-001 IAW SRM 51-42-01, 51-42-02. AC REMAINS IN YQG FOR COMPLETION.Feb 3, 2022 · N744YX · Emb ERJ170200LRSDR R61A2022021300130Gusset · corrodedWHILE AC WAS IN FOR HVY CK FOUND. CF3 FLOOR STRUCTURE CORROSION FOUND ON RH GUSSETT PLATE AT FR 90. MX REPLACED GUSSET PLATE PN 170-60259-001 IAW SRM 53-30-10, 51-41-02. AC REMAINS IN YQG FOR COMPLETION.Feb 3, 2022 · N744YX · Emb ERJ170200LRSDR R61A2022021300129Threshold · corrodedWHILE AC WAS IN FOR HVY CK FOUND. FWD FUSELAGE FLOOR STRUCTURE CORROSION FOUND ON RH SILL DOUBLER BTWN FR 12-14. MX REPLACED SILL PN 170-05663-005 IAW SRM 51-43-04, 51-41-02. AC REMAINS IN YQG FOR COMPLETION.Feb 3, 2022 · N744YX · Emb ERJ170200LRSDR DALA2022020400726None · noneSHIP 1706 FOUND CRACK ON THE RIGHT SIDE OF THE FUSELAGE SKIN IN SECTION 48 BETWEEN FRAMES 1629-1654. CORRECTIVE ACTION: THE SKIN REPAIR CARRIED OUT AT STA1629 TO STA1654 STR14AR AS PER B767-300 SRM 53-80. (2108856)Feb 3, 2022 · N176DZ · Boeing 767332SDR DALA2022020400725None · noneSHIP 174 HFEC INSPECTION FOUND 01EA CRACK ON RH EXTERNAL SURFACE OF THE FUSELAGE SKIN AT S-14AR, STA1637. CORRECTIVE ACTION: CRACK AREA REPAIRED AS PER B767-300 SRM53-80 (2108832)Feb 3, 2022 · N174DN · Boeing 767332SDR CALA2022020400314Frame · corrodedFWD CARGO FR30 STGR41R-STGR40R CLEAT CORRODED(A3NB-53-3-6105)G ENERATED BY:V061629 @HAECO LCQ PER NON ROUTINE 9290301 (38301) REMOVED AND REPLACED CLEAT WITH NEW PART P/N:D532351320002, PO:1 PERFORMED BY: V932428 INSP BY:V892285 0728623 ON FWD CARGO COMPARTMENFeb 3, 2022 · N850UA · Airbus A319131SDR CALA2022020400312Stop Fitting · crackedRH AFT DOOR FR68 DOOR STOP FITTING #1 I/B LOWER HOLE HAS A CRACK INDICATION, HOLE IS CIRCLED IN BLACK. NEEDS TO BE REPAIRED BEFOR E FURTHER FLIGHT () L/H AFT DOOR STOP FITTING FR68 LOWER I/B HOLE REAMED TO 0.391 NO #1 (REMOVED FOR ACCESS) IAW SRM 51-42-11. ACCFeb 3, 2022 · N475UA · Airbus A320232SDR GTIA2022013136263None · noneDURING DESCENT SMOKE LAV SMOKE ECAM LASTED APPROX 3 SECONDS PAX-ADMITTED TO USING A VAP PEN-ACCOMPLISHED LAV SMOKE TEST IAW AMM 26-17-00.NO FAULTS DETECTED.A/C OKAY FOR SERVICE.Feb 3, 2022 · N682NK · Airbus A321231SDR GTIA2022013136262None · noneL2 DOOR ASSIST BOTTLE LOW PRESSURE -SVCD L2 DOOR ASSIST BOTTLE TO PROPER PRESSURE IAW AMM 52-22-00Feb 3, 2022 · N667NK · Airbus A321231SDR IXXA2022020305Intercostal · corrodedINTERCOSTAL CORRODED BEYOND LIMITSFeb 3, 2022 · N762CX · Boeing 767232SDR IXXA2022020304Panel · delaminatedPANEL DELAMINATEDFeb 3, 2022 · N762CX · Boeing 767232SDR IXXA2022020303Tear Strap · corrodedTEAR STRAP CORRODED BEYOND LIMITSFeb 3, 2022 · N762CX · Boeing 767232SDR IXXA2022020302Support · corrodedSUPPORT CORRODED BEYOND LIMITSFeb 3, 2022 · N762CX · Boeing 767232SDR IXXA2022020301Floor Support · corrodedSUPPORT CORRODED BEYOND LIMITSFeb 3, 2022 · N762CX · Boeing 767232SDR HNAA2022022300111Not Reported · not reportedE901506 - RH #1 (CENTER) FLOOR BEAM GUSSET CORRODED .... REMOVED AND REPLACED RH #1 (CENTER) FLOOR BEAM GUSSET IAW EMB145 SRM 51-40-02. RESTORED PROTECTIVE COATING AS REQUIREDFeb 2, 2022 · N658AE · Emb EMB145LRSDR JJBA20220202013Not Reported · not reportedAT CF 4 AREA, CORROSION FOUND ON CENTER OMEGA BEAM FLOOR STRUCTURE BTW FR 59 TO FR 60. CORROSION ON CENTER OMEGA BEAM BTW FR 59 TO 60 FOUND OUT OF LIMITS. CUT-OUT ON OMEGA BEAM PERFORMED. CENTER OMEGA BEAM BTW FR 59-60 REPAIRED WITH DOUBLERFeb 2, 2022 · N14148 · Emb EMB145XRSDR R61A2022021400141Shear Tie · corrodedCORRODED SHEAR CLIP, FR 17, STGR 27R-28R. EVALUATED SHEAR CLIP, FR 17, STGR 26R-27R REF. EMB SRM 51-10-02. 100% MATERIAL LOSS. REMOVED AND REPLACED SHEAR CLIP REF. EMB SRM 51-40-08Feb 2, 2022 · N826MD · Emb ERJ170200LRSDR R61A2022021400140Shear Tie · corrodedCORRODED SHEAR CLIP, FR 16, STGR 28R-29R. EVALUATED SHEAR CLIP, FR 16, STGR 27R-28R REF. EMB SRM 51-10-02. 100% MATERIAL LOSS. REMOVED AND REPLACED SHEAR CLIP REF. EMB SRM 51-40-08Feb 2, 2022 · N826MD · Emb ERJ170200LRSDR R61A2022021400139Shear Tie · corrodedCORRODED SHEAR CLIP, FR 17, STGR 28R-29R. EVALUATED SHEAR CLIP, FR 17, STGR 27R-28R REF. EMB SRM 51-10-02. 100% MATERIAL LOSS. REMOVED AND REPLACED SHEAR CLIP REF. EMB SRM 51-40-08Feb 2, 2022 · N826MD · Emb ERJ170200LRSDR R61A2022021400138Shear Tie · corrodedCORRODED SHEAR CLIP, FR 17, STGR 28L-29L. : EVALUATED SHEAR CLIP, FR 17, STGR 27L-28L REF. EMB SRM 51-10-02. 100% MATERIAL LOSS. REMOVED AND REPLACED SHEAR CLIP REF. EMB SRM 51-40-08Feb 2, 2022 · N826MD · Emb ERJ170200LRSDR R61A2022021400137Shear Tie · corrodedCORRODED SHEAR CLIP, FR 17, STGR 26L-27L REMOVED AND REPLACED DAMAGED SHEAR CLIP FR 17 STGR 26L-27L REF SRM 51-40-08, SEE WIP'S AND TASKS FOR WORK PERFORMED.Feb 2, 2022 · N826MD · Emb ERJ170200LRSDR IXXA2022020210Panel · crackedP33 PANEL CRACKEDFeb 2, 2022 · N443AZ · Boeing 767323SDR IXXA2022020208Stringer · corrodedSTRINGER CORRODED BEYOND LIMITS.Feb 2, 2022 · N762CX · Boeing 767232SDR IXXA2022020204Stringer Clip · corrodedSTRINGER CLIP CORRODED BEYOND LIMITSFeb 2, 2022 · N762CX · Boeing 767232SDR IXXA2022020203Scuff Plate · crackedAFT LOWER CARGO DOOR SCUFF PLATE CRACKED.Feb 2, 2022 · N762CX · Boeing 767232
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