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 IXXA2022012013Stringer · corrodedSTRINGER CORRODED BEYOND LIMITS.Jan 20, 2022 · N763CX · Boeing 767232SDR IXXA2022012012Shear Tie · corrodedSHEAR TIE CORRODED BEYOND LIMITSJan 20, 2022 · N763CX · Boeing 767232SDR IXXA2022012011Shear Tie · corrodedSHEAR TIE CORRODED OUT OF LIMITSJan 20, 2022 · N763CX · Boeing 767232SDR IXXA2022012010Stringer · corrodedSTRINGER CORRODED BEYOND LIMITSJan 20, 2022 · N762CX · Boeing 767232SDR IXXA2022012009Floor Skin · corrodedFLOOR WEB CORRODED BEYOND LIMITS.Jan 20, 2022 · N762CX · Boeing 767232SDR 2A6D20220120005None · chafedAC 7015 HAS CHAFE DAMAGE TO THE L/H X-FRAME’S AFT LOWER LEG LOCATED AT APPROXIMATELY STA 3650, WL 2305, AND BL 430L. THE DAMAGE MEASURES .21” LONG AND .2” WIDE WITH A MAX DEPTH OF .019”.Jan 20, 2022 · N810LF · Snias AS350B3SDR 2A6D20220120003Bulkhead · gougedTHE L/H LATERAL BAGGAGE COMPARTMENT WE IDENTIFIED THE LANDING GEAR’S L/H VIBRATION DAMPENER FITTING WAS GOUGED. DAMAGE LOCATED AT APROX. STA 2700, WL 2550, BL 600L. THE DAMAGE MEASURES L=0.600”, W=0.300”, D=0.025”.Jan 20, 2022 · N810LF · Snias AS350B3SDR 2022FA0000038None · gougedRH FUSELAGE SKIN HAS 1 DRILL START AT APPROXIMATELY FS 440.81 BEHIND SPLICE STRAP. ACCOMPLISHED MINOR REPAIR TO RIGHT TAILCONE SKIN P/N: 7412023-12 IAW TEXTRON AVIATION ENGINEERING MEMO DQ33188M1 DATED 1/19/22.Jan 20, 2022 · N690QS · Cessna 680ASDR 2A6D20220120002Bulkhead · chafedDAMAGE TO THE 15 DEGREE BULKHEAD LH WEB (PN: 350A21-1032.60 IN THE FORM OF CHAFES. THE FIRST CHAFE DAMAGE AREA WAS FOUND NEAR THE X-FRAME AND WAS MEASURED TO BE APPROXIMATELY 0.40” X 0.39” AND 0.015” DEEP; THE SECOND CHAFE DAMAGE AREA WAS FOUND ON THE STIFFENIJan 20, 2022 · N810LF · Snias AS350B3SDR 2A6D20220120001Bulkhead · chafedAIRCRAFT HAS CHAFE DAMAGE ON THE AFT SIDE OF THE 15 DEGREE BULKHEAD LOCATED IN THE L/H LATERAL BAGGAGE COMPARTMENT IN TWO DIFFERENT LOCATIONS. THE DAMAGE IS LOCATED AT APPROXIMATELY STA 2700, WL 2300, AND BL 500L. THE OB DAMAGE MEASURES.2” LONG AND .11” WIDE WJan 20, 2022 · N810LF · Snias AS350B3SDR IXXA2022012008Tear Strap · corrodedTEAR STRAP CORRODED BEYOND LIMITSJan 20, 2022 · N762CX · Boeing 767232SDR 2022FA0000037None · noneLEFT FUSELAGE BOND ASSEMBLY P/N: 7411391-1 CHAFED. ACCOMPLISHED MINOR REPAIR TO LEFT FUSELAGE BOND ASSEMBLY P/N: 7411391-1 IAW TEXTRON AVIATION ENGINEERING MEMO DQ33187M1 DATED 1/19/22.Jan 20, 2022 · N690QS · Cessna 680ASDR IXXA2022012007Stringer · corrodedSTRINGER CORRODED BEYOND LIMITSJan 20, 2022 · N762CX · Boeing 767232SDR IXXA2022012006Stringer · corrodedSTRINGER CORRODED BEYOND LIMITSJan 20, 2022 · N762CX · Boeing 767232SDR IXXA2022012005Frame · corrodedCORROSION ON FRAME BEYOND LIMITSJan 20, 2022 · N762CX · Boeing 767232SDR IXXA2022012004Skin · crackedFUSELAGE SKIN CRACKEDJan 20, 2022 · N762CX · Boeing 767232SDR IXXA2022012003Stringer · corrodedSTRINGER CORRODED BEYOND LIMITSJan 20, 2022 · N762CX · Boeing 767232SDR IXXA2022012001Channel · corrodedCHANNEL CORRODED BEYOND LIMITSJan 20, 2022 · N762CX · Boeing 767232SDR SWIA202265006None · cracked* CO-PILOT'S WINDSHIELD SIDE POST, LOWER AFT FITTING IS CRACKED, MARKED. (C-CHECK RO 3/14/2022) REMOVED AND RELACED CO-PILOT'S WINDSHIELD SIDE POST, LOWER AFT FITTING.REF CRJ 200 SRM 51-42-21-00 / DWG 601R33007 REV U. TO SEE ALL ADDITIONAL STEP SEE CONJan 19, 2022 · N886AS · Cndair CL6002B19SDR R61A2022020500115Shear Tie · corrodedCORRODED SHEAR CLIP, FR 87, STGR 27R-28R, AFT OF DRAIN FITTINGS. REMOVED AND REPLACED SHEAR CLIP AFT OF DRAIN FITTING BETWEEN FR 87 STGR 27R-28R. REF EMB SRM 51-40-08.Jan 19, 2022 · N867RW · Emb ERJ170200LRSDR R61A2022020500114Shear Tie · corrodedCORRODED SHEAR CLIP, FR 82, STGR 28L-29L. REMOVED AND REPLACED SHEAR CLIP AT FR 82 BETWEEN STGR 28L-29L. REF EMB SRM 51-40-08.Jan 19, 2022 · N867RW · Emb ERJ170200LRSDR R61A2022020500101Seat Track · corrodedDURING HEAVY CHECK MAINTENANCE FOUND CORROSION FOUND ON CFI LH IB CABIN SEAT TRACK BETWEEN FR23 AND FR34. REMOVED AND REPLACED SEAT TRACK ON CFI LH IB BETWEEN FR23 AND FR34IAW EMB 170 SRM 51-41-02, 51-43-03, 51-43-04 AND ETD2022-170-002456.Jan 19, 2022 · N631RW · Emb ERJ170100SESDR R61A2022020300095Beam · corrodedAFT SERVICE DOOR LOWER BEAM HAS CORROSION AROUND BOTH FWD AND AFT GIRT BAR FITTINGS. REMOVED AND REPLACED AFT SERVICE DOOR LOWER BEAM REF. SRM 51-40-08Jan 19, 2022 · N227JQ · Emb ERJ170200LRSDR CALA2022012000190Plate · crackedLH PRESSURE PNL FRAME 36 HOLES 2,3,4,5,6,7,9,10,15,20,21,22,23,2 4,26,27 AND 28 ARE CRACKED IN THE PRESSURE PNL AD2018-06-04 GEN BY V061633 AT HAECO LCQ PER NR 9290732 (28732). ACP REPAIR INSTRUCTIONS PER REO L-23537 REV IR WITH NO DEVIATION 63,512 TOTAL A/C FJan 19, 2022 · N481UA · Airbus A320232SDR CALA2022012000189Plate · crackedRH PRESSURE PNL FRAME 36 HOLES 4,6,7,8,9,13,14,16,17,18,20,22,25 AND 26 ARE CRACKED IN THE PRESSURE PANEL AD2018-06-04 GEN BY V0 61633 ACCOMPLISHED REPAIR INSTRUCTIONS ON RH FR36 PRESSURE PANEL PER R ON OR BEFORE 69,512 TOTAL AIRCRAFT FLIGHT CYCLES OR 146,671 Jan 19, 2022 · N481UA · Airbus A320232SDR FDEA202201190098Floor Panel · wornMAIN DECK FLOOR PANEL #221BF STA 297 TO 440 FOUND WORN FABRICATED MENTIONED PANEL PER FEDEX SRX-25-005 REF. ENGINEERING DESPOSITION OF RFTA NO:02841-0205. MAJOR REPAIRJan 19, 2022 · N920FD · Boeing 757200SDR FDEA202201190096Floor Panel · wornMAIN DECK FLOOR PANEL #222 MAF STA 297 TO 440 FOUND WORN FABRICATED MENTIONED PANEL PER FEDEX SRZ 25-005 REF. ENGEENIRING DISPOSITION OF RFTA NO: 02841-0205. MAJOR REPAIRJan 19, 2022 · N920FD · Boeing 757200SDR IXXA2022011908Seat Track · corrodedSEAT TRACK REPAIREDJan 19, 2022 · N762CX · Boeing 767232SDR IXXA2022011907Stringer · corrodedSTRINGER CORRODED BEYOND LIMITS.Jan 19, 2022 · N762CX · Boeing 767232SDR IXXA2022011906Shear Tie · corrodedSHEAR TIE CORRODED BEYOND LIMITSJan 19, 2022 · N762CX · Boeing 767232SDR IXXA2022011905Channel · corrodedCHANNEL CORRODED BEYOND LIMITSJan 19, 2022 · N762CX · Boeing 767232SDR IXXA2022011904Frame · corrodedCORRODED FRAME WEB OUT OF LIMITSJan 19, 2022 · N762CX · Boeing 767232SDR IXXA2022011902Stringer · corrodedSTRINGER CORRODE BEYOND LIMITS.Jan 19, 2022 · N762CX · Boeing 767232SDR IXXA2022011901Stringer · corrodedSTRINGER CORRODED BEYOND LIMITS.Jan 19, 2022 · N762CX · Boeing 767232SDR SWIA202265212None · damaged*SERVICE DOOR HAS SEVERAL AREAS OF CHAFF DAMAGE ON EXTERIOR SKIN AROUND DOOR HANDLE (MARKED) (C-CHECK RO 3-25-22) REMOVED DAMAGE AT SERVICE DOOR ON EXTERIOR SKIN AROUND DOOR HANDLE PER REF CRJ200 SRM 51-12-00. FOUND OUT OF LIMITS. RECEIVED AND COMPLIED WJan 18, 2022 · N875AS · Cndair CL6002B19SDR SWIA202264888None · corrodedA-BAY TCAS OMNIDIRECTIONAL ANTENNA DOUBLER CORRODED (C-CHECK RO 3/11/2022) REPLACED A-BAY TCAS OMNIDIRECTIONAL WITH NEW ANTENNA DOUBLER.REF CRJ700 SRM 51-42-06-001-001-A01,SRM 51-42-21-001-001-A01. DWG:SH670-30023 REV G. LEAK CHECK GOOD. COMPLIED WITH TJan 18, 2022 · N732SK · Cndair CL6002C10SDR IXXA20220217003Skin · dentedPROTRUDING DENT AT BS 392 AND ABOVE STRINGER 32LJan 18, 2022 · N479AZ · Boeing 767323SDR R61A2022020500111Filler · corrodedCORROSION - RH CROSSBEAM FR17. REMOVED CORROSION AND PERFORMED PERMANENT REPAIR ON RH CROSSBEAM FR 17. REF EMB SRM 53-00-10/REPAIR 03P.Jan 18, 2022 · N867RW · Emb ERJ170200LRSDR R61A2022020500110Filler · corrodedCORROSION AND TOOLING MARKS - RH CROSSBEAM FR14. REMOVED DAMAGE SECTION BY CUT-OUT, FABRICATED AND INSTALLED REPAIR PARTS FOR CROSSBEAM FRAME 14 REFER SRM 53-00-10/REPAIR 03P.Jan 18, 2022 · N867RW · Emb ERJ170200LRSDR SWIA202264156None · corroded*LOWER SILL JUST FWD OF THE AFT CARGO DOOR ENTRANCE HAS CORROSION AT APPROX. FS.985 TO FS.1000 (MARKED) (C CHECK RO 02-03-22) REPLACED AND MODIFIED LH LOWER SILL FROM APPROX. F.S 985 TO F.S 1000 REF. REO 670-53-61-2048 REV -- DATED 2022-01-22 . COMPLIED WIJan 18, 2022 · N710SK · Cndair CL600*SDR R61A2022020500108Seat Track · corrodedLEVEL 2 CORROSION FOUND ON CFII RH OUTBD CABIN SEAT TRACK. SEAT TRACK WAS REPLACED IAW 51-41-01Jan 18, 2022 · N631RW · Emb ERJ170100SESDR FDEA202201180077Doubler · failedDURING PERFORMING EA T G-5710-T0366180 A P2 STEP 11.C.(5), 01EA ZLJ-8(BACB30NY8K*) COUNTERSUNK FASTENER AT STA998 STGR35 RHS FOUND TOO CLOSE TO EDGE OF MACHINED STEP OF DOUBLER P/N 143W2314Y406, AND WILL RESULT IN KNIFE EDGE WITH MACHINED STEP ON AFT EDGJan 18, 2022 · N843FD · Boeing 777FHTSDR FDEA202201180076Doubler · failedDURING PERFORMING EA T G-5710-T0366180 A P1 STEP 11.C.(5), 01EA ZLJ-8(BACB30NY8K*) COUNTERSUNK FASTENER AT STA998 STGR35 LHS FOUND TOO CLOSE TO EDGE OF MACHINED STEP OF DOUBLER P/N 143W2314Y405, AND WILL RESULT IN KNIFE EDGE WITH MACHINED STEP ON AFT EDGJan 18, 2022 · N843FD · Boeing 777FHTSDR R61A2022020100078Shear Panel · corrodedWHILE AC WAS IN FOR HVY CK FOUND CORROSION FOUND ON FWD FUSE FLOOR STRUCTURE SHEAR WEB BTWN FR 12-14 OTBD RH SIDE. MX REPLACED SHEAR WEB PN 170-05663-003 IAW SRM 51-41-02, 5143-04.SEE AAR NRC# 1000-0174 FOR DETAILS OF WORK PERFORMED. AC REMAINS IN YQG FOR COMJan 18, 2022 · N631RW · Emb ERJ170100SESDR R61A2022012900072Seat Track · corrodedWHILE AC WAS IN FOR HVY CK, CORROSION FOUND ON FWD FUSE RH INBD CABIN SEAT TRACK BTWN FR 12 AND FR20. MX REPLACED SEAT TRACK PN 170-03263-001 IAW SRM 51-41-01, 51-41-02, 51-43-03. FOR DETAILS OF WORK PERFORMED. AC REMAINS IN YQG FOR COMPLETIONJan 18, 2022 · N631RW · Emb ERJ170100SESDR R61A2022012700065Stringer · damagedWHILE PERFORMING DRILL UP ON STGR 29R FR 77-78. MIS-LOCATED SPLICE FASTENER HOLE IN STGR 29R. PERFORMED STRINGER SPLICE REPAIR STGR 29R FR 77/78 REF ETD2022-170-000112-BJan 18, 2022 · N127HQ · Emb ERJ170200LRSDR CALA2022011800184Keelbeam · elongatedWHILE ACCOMPLISHING INSPECTIONS PER FCD 5330-05575D OF THE RH FUSELAGE KEEL BEAM MLG ATTACHMENT STRUCTURE, PRODUCTION REPORTED ALL HOLES OUT OF LIMITS AND ELONGATED. -06891 (SEE FIGURE 1 - 17 OF EC/RA 5311-02712 FOR LOCATIONS). ACCOMPLISH A PERMANENT REPAIR PEJan 18, 2022 · N837UA · Airbus A319131SDR CALA2022011800183Stringer Splice · corrodedFWD CARGO STRINER SPLICE STR41L FR30-FR31 CORRODED GENERATED BY V079881 ON HAECO LCQ NR 9292493/30493. ORGINAL LP 7776370 REMOVED & REPLACED STRINGER SPLICE ON STG 41L BETWEEN FR 30-31 I AW A320 SRM 51-72-11 ADD EMP:V061765Jan 18, 2022 · N435UA · Airbus A320232SDR CALA2022011800175Rib · elongatedWHILE ACCOMPLISHING FCD 5330-05575 LH HOLES, FOUND ALL HOLES OUT OF SIDE LIMITS AND ELONGATED WITH VISUAL DAMAGE (NO DOT)Jan 18, 2022 · N837UA · Airbus A319131SDR CALA2022011800174Rib · elongatedWHILE ACCOMPLISHING FCD 5330-05575 RH HOLES, FOUND ALL HOLES OUT OF SIDE LIMITS AND ELONGATED WITH VISUAL DAMAGE EXCEPT HOLES #R 13 AND #R19.Jan 18, 2022 · N837UA · Airbus A319131
Back to JASC 5300