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 CALA2023031500753Skin · dentedDENT ON FUSELAGE SKIN BTW FR1-2 L/H LAP JOINT. AS NOTED ON LTPR 5001217873-0010.Mar 14, 2023 · N848UA · Airbus A319131SDR CALA2023031500745Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND RBL 54.60 IS CRACKED. ADDING VERBIAGE TO PREVIOUS ENTRY SUPPORT TASK NSA EMX NR 00070Mar 14, 2023 · N38257 · Boeing 7378SDR SWIA2023050100002Unknown · dented*DENTS IN BOTTOM DOUBLER BELOW AND AFT OF GROUND AIR CONDITIONING CONNECTION PNL 172BR (MARKED) (C-CHECK RO 4/26/2023) REPAIRED DAMAGED AREA COMMON TO LOWER FUSELAGE SKIN APPROXIMATELY BETWEEN FS574 & FS621 AND STRG26L TO STRG20R IAW REO 601R-53-61-799Mar 13, 2023 · N905EV · Cndair CL6002B19SDR HNAA2023041200114Unknown · unknownRH VERTICAL DRAG ANGLE HAS 2 POSSIBLE CRACKS BETEEN FRAMES 76 AND 77. REPAIRED IAW EO1-53-23-0087Mar 13, 2023 · N692AE · Emb EMB145LRSDR YENA2023031600249Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION CLIP AT FR31 BTW STR43L AND STR44 IN FWD CARGO COMPARTMENT REF. MPD TASK 532180-01; (RESOLVED ON W/O: 1212223 TASKCARD: NR-00023 ) REMOVED AND REPLACED CLIP LOC. FR31 BTW STR43L AND STR44 IN FWD CARGO COMPARTMENTS IAW A320 Mar 13, 2023 · N646JB · Airbus A320232SDR YENA2023031600248Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION CLIP AT FR32 BTW STR43R AND STR44 IN FWD CARGO COMPARTMENT REF MPD TASK 532180-01; (RESOLVED ON W/O: 1212223 TASKCARD: NR-00024 ) REMOVED AND REPLACED CLIP LOC. FR32 BTW STR43R AND STR44 IN FWD CARGO COMPARTMENTS IAW A320 SRMar 13, 2023 · N646JB · Airbus A320232SDR YENA2023031600247Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION CLIP AT FR33 BTW STR42R AND STR43R IN FWD CARGO COMPARTMENT REF MPD TASK 532180-01; (RESOLVED ON W/O: 1212223 TASKCARD: NR-00025 ) REMOVED AND REPLACED CLIP LOC. FR33 BTW STR42R AND STR43R IN FWD CARGO COMPARTMENTS IAW A320 Mar 13, 2023 · N646JB · Airbus A320232SDR YENA2023031600246Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION CLIP AT FR33 STR43L AND STR 43R IN FWD CARGO COMPARTMENT REF MPD TASK 532180-01; (RESOLVED ON W/O: 1212223 TASKCARD: NR-00026 ) REMOVED AND REPLACED CLIP LOC. FR33 BTW STR43L AND STR43R IN FWD CARGO COMPARTMENTS IAW A320 SRMMar 13, 2023 · N646JB · Airbus A320232SDR YENA2023031600245Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION STRINGER 42R AT FR32 PLUS 1 INCH IN FWD CARGO COMPARTMENT REF. MPD TASK 532180-01; (RESOLVED ON W/O: 1212223 TASKCARD: NR-00027 ) PERFORMED PERMANENT REPAIR LOC. STR42R AT FR32 PLUS 1INCH IN FWD CARGO COMPARTMENT IAW A320 SRMar 13, 2023 · N646JB · Airbus A320232SDR YENA2023031600244Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION CLIP AT FR34 BTW STR43R AND STR44 IN FWD CARGO COMPARTMENT REF. MPD TASK 532180-01; (RESOLVED ON W/O: 1212223 TASKCARD: NR-00028 ) REMOVED AND REPLACED CLIP LOC. FR34 BTW STR43R AND STR44 IN FWD CARGO COMPARTMENTS IAW A320 SMar 13, 2023 · N646JB · Airbus A320232SDR YENA2023031600243Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16RH SIDE INTERCOSTAL FITTING ON HOLE 3 AT DOOR STOP POSITION 7 CRACK DIRECTION IS 9 O'CLOCK AT FWD GALLEY AREA (1EA); REF: ARM W/O 2-33 12/1 N/R 2023-98134 REMOVED AND REPLACED NEW INTERCOSTAL FITTING AND FMar 13, 2023 · N646JB · Airbus A320232SDR CALA2023031500744Beam · corrodedCABIN - STA 325 LBL 20-36 FLOOR SUPPORT FOUND CORRODED TRANSFER REF. NON-ROUTINE HX NRC WO.1458070 AND ORIGINATED BY EMP NO. V897979 CABIN STA 325 LBL 20-36 FLOOR SUPPORT REPAIRED AS PER EC/RA 5310-08126 REV-. ATTACHED FORM 44-0008 ITEM 1 TO ITEM 36 ACCOMPLISHMar 13, 2023 · N76062 · Boeing 767*SDR CALA2023031500742Floor Support · corroded(B737-53-3-0711) RBL +10 FLOORBEAM SUPPORT HAS SURFACE CORROSION STA 328-294 FLOORBEAM SUPPORTS CORROSION OUT OF LIMITS REF SRM 53-10-51-A PA RA 4B. REPLACED WITH NEW SUPPORTS REF SRM 51-40-02. DATA WAS TRA NSCRIBED FROM PAPER DOC AERSALE WO 3826 NR 24738 WORKMar 13, 2023 · N14214 · Boeing 7378SDR CALA2023031500736Unknown · corroded(B737-53-3-0711) L1 DOOR THRESHOLD STA 344 TO 320 HAS SURFACE CORROSION L1 DOOR THRESHOLD STA 344 TO 320 REMOVED AND REPLACED FOR NEW ON E IAW B737-800 SRM 51-40-02-0G-0 PAR 4.B. AND 7.A. DATA WAS TRAN SCRIBED FROM PAPER DOC AERSALE WO 3826 NR 24706 WORK ACP BMar 13, 2023 · N14214 · Boeing 7378SDR CALA2023031500735Unknown · crackedWING CENTER SECTION UPPER SURFACE HORIZONTAL PRESSURE WEB STA 665 RBL 40 CRACKED REF AAR N/R 974984 ACCOMPLISHED HORIZONTAL PRESSURE DECK WEB REPAIR BETWEEN STA 663 TO STA 675 FROM RBL38 TO EBL60 PER REF B737 SRM 53-40-51-2R-2 FIG 202 DETAIL A WORK ACCOMPLISHEMar 13, 2023 · N25705 · Boeing 737*SDR A6WA202303138499Bulkhead · crackedE17/003/453 - FS621 PRESS BULKHD WEB MOD ********AIRCRAFT REMOVED FROM SERVICE********** COMPLIED WITH 601R-53-1240 REV D DATED 10-31-2016, REPAIR AND MODIFICATION TO F.S.621.00 PRESSURE BULKHEAD WEB.Mar 13, 2023 · N436AW · Cndair CL6002B19SDR A6WA202303138497Support · crackedWHILE REMOVING FS 621 LINTEL SUPPORT, FOUND 1EA "BUILD UP" LEG, P/N: 601R35212-103 TO BE CRACKED. ********AIRCRAFT REMOVED FROM SERVICE********** LOCATED AND DRILLED 1EA NEW "BUILD UP" LEG, P/N: 601R35212-103 FOR FS 621 LINTEL SUPPORT IAW CRJ 200 SRM 51-40-11.Mar 13, 2023 · N436AW · Cndair CL6002B19SDR SWAA2023041115151Angle · corrodedCORROSION INNER CHORD LOCATED AT LEVEL STR 17L BS 303.9 LBL 55 WL 208.1 AT FWD GALLEY AREA 2023-180925<[01] TOOL USED ULTRASONIC THICKNESS INSTRUMENT P/N 45MG S/N 130064101 DUE DATE 12-OCT-23;[02] REPLACED INNER CHORD LOCATED AT LEVEL STR 17L BS 303.9 LBL 55 WMar 12, 2023 · N280WN · Boeing 7377H4SDR DALA2023031401869None · noneFOUND CRACK ON FS973.0 WHILE WORKING ON AS REDATED WORKCARD 5352 -01038-01A CRACK IS LOCATED AT LH FRAME, IS 12 INCHES LONG AND IS CRACKING OUTBOARD. THIS TASK IS AD RELATED. ACCOMPLISHMENT WORK CARD 5352-0138-08A. (RD471692) REMOVED AND REPLACED FRAME WITH SEMar 12, 2023 · N301DU · Bombdr BD1001A10SDR ASAA2023031142536Intercostal · wornMAIN CABIN AFT WET AREA R/H SIDE AREA, INTERCOSTAL HAS 2 EACH WEAR MARKS AT THE UPPER FLANGE LOWER SURFACE BETWEEN BS 1006 AND BS 1016 APPROX. RBL-17. MARKED GROUNDED - YES. REMOVED DAMAGE, ORIGINAL THICKNESS 0.063. REMOVED 0.008 REMAINING THICKNESS 0.055. FOUMar 11, 2023 · N586AS · Boeing 737890SDR A6WA202303118518Angle · crackedSTIFFENER ANGLE P/N 601R36008-51 LOCATED ON AFT SIDE OF FS621 PRESSURE BULKHEAD BETWEEN LBL36 AND STR 16B AT WL 79 IS CRACKED ON INBOARD END. *********AIRCRAFT REMOVED FROM SERVICE********** REPLACED STIFFENER ANGLE P/N 601R36008-51 AT AFT SIDE OF F.S. 621 BULMar 11, 2023 · N442AW · Cndair CL6002B19SDR IPXA2023031691889Stiffener · crackedINSPECTION TYPE:C6*MAJOR REPAIR* CRACK ON THE STIFFENER (P/N: 141T5146-65) OF THE FLOOR BEAM ASSEMBLY AT STA 246, LBL 40.REPAIR I.A.W 767-300F SRM 53-10-51-2R-4 REV 85.01.Mar 11, 2023 · N344UP · Boeing 76734AFSDR A6WA202303118494Angle · corrodedPAX DOOR LOWER SILL ANGLE CORRODED. *******AIRCRAFT REMOVED FROM SERVICE******** REMOVED AND REPLACED PAX DOOR LOWER SILL ANGLE (P/N 601R31527-221S) IAW CRJ 200 SRM 51-41-06, 51-42-13, 51-42-21.Mar 11, 2023 · N436AW · Cndair CL6002B19SDR CALA2023031300713Fitting · crackedSUPPORT TASK - AD022-06-07 EA5380-01113 REV B FUS RH STA2370 STR12R STRINGER END FTG FOUND CRACKED. TRANSFER REF NON - ROUTINE WO.1540428 AND ORIG BY V897008 RH BS2370 PIVOT BULKHEAD FWD CHORD ATT STRINGER END FTG STR 12R REPLACED AS PER SRM51-10-02 AND INSTALMar 11, 2023 · N774UA · Boeing 777222SDR CALA2023031300712Skin · noneREF LOGPAGE 6161264 FOUND AREA TO BE REWORKED AS LIGHTNING DAMAGE NOT AS A DENT AS ORIGINAL DESCRIPTION ON BS 395 STRINGER 20 L/H (REF. AAR NR 99958964).Mar 11, 2023 · N26215 · Boeing 7378SDR VNAA202303110004Skin · dentedL/H EXTERNAL FUSELAGE SKIN HAS MULTIPLE DENTS BETWEEN FS 193.00 AND FS 202.75 AFT OF TRU BAY DOOR. REMOVED AND REPLACED THE LH EXTERNAL FUSELAGE SKIN BETWEEN FS 193.00 AND FS 202.75 AFT OF TRU BAY DOOR IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-40-11-001-001-AMar 11, 2023 · N572NN · Bombdr CL6002D15SDR SWAA2023041814661Strap · corrodedCORROSION ON AFT PAX CABIN FLOOR STRUCTURE TENSION STRAP FROM STA 1016 TO 1016+10; LBL 3; WL 208.1.<[01] NO ALLOWABLE DAMAGE LIMITS FOUND IN SRM FOR THIS ITEM. THE STRUCTURAL ITEMS THAT DO NOT HAVE ENTRIES ARE CALLED REPAIRABLE BY REPLACEMENT PER SRM 51-10-02 Mar 10, 2023 · N281WN · Boeing 7377H4SDR SWAA2023041815577Rail · corrodedAFT CARGO BAY - RAIL HAS CORROSION BS 767+5 LBL 7.75; LBL 12; RBL 3.<[01] VERIFIED APLICABILITY SRM 53-60-53-0I-2 FOR IDENTIFICATION AND SRM 53-00-53-1A-2 FOR ALLOWABLE DAMAGE;[02] COMPLETED STEPS 1-3.<BR><BR>OK TO APPLY CHEMICAL CONVERSION COATING AND PRIMER.Mar 10, 2023 · N281WN · Boeing 7377H4SDR CALA2023031300710Fitting · crackedSUPPORT TASK - AD2022-06-07 EA5380-01113 REV B FUS RH STA2370 STR32R STRINGER END FTG FOUND CRACKED. TRANSFER REF NON - ROUTINE WO.1540453 AND ORIG BY V897008 RH BS2370 BULKHEAD FWD CHORD ATT STRINGER END FTG STR 32R REPLACED AS PER SRM51-10-02 AND INSTALLED AMar 10, 2023 · N774UA · Boeing 777222SDR CALA2023031300709Door Sill · corrodedDOOR SURROUND STRUCTURE SILL ANGEL WITH CORROSION ON L1 (REF. AAR NR 99959066).Mar 10, 2023 · N26215 · Boeing 7378SDR A6WA202303108485Unknown · corrodedMULTIPLE SPOTS OF CORROSION NOTED ON R/H PRESSURE FLOOR SILL PANEL BETWEEN FS 409+128 AND FS559 ****AIRCRAFT REMOVED FROM SERVICE***** REPAIRED R/H PRESSURE FLOOR SILL REF REO 601R-53-41-666 REV C DATED 2012-11-06 AND REO 601R-53-41-3127 REV A DATED 2023-03-08Mar 10, 2023 · N415AW · Cndair CL6002B19SDR A6WA202303108486Floor Support · crackedANGLE BRACKET SECURING FS 621 BULKHEAD TO L/H FLOOR SILL MISSING RIVETS ****AIRCRAFT REMOVED FROM SERVICE******* REPLACED FLOOR SUPPORT ANGLE REF REO 601R-53-61-117 REV E DATED 2018-01-15Mar 10, 2023 · N415AW · Cndair CL6002B19SDR EE4Y2023100317405Unknown · unknownDURING THE ALLEGIANT EO # 53-120-003 ALLEGIANT EO INSTRUCTIONS ACCOMPLISHMENT WHICH IS RELATED WITH AD 2018-14-09 THERE WERE FOUND TWO (2 EA) FASTENER HOLES WITH CRACK INDICATION ON CROSSBEAM SPLICING AT FR 16 LHS (H8) AND AT FR 20 LHS (H26). WORK PERFORMEDMar 10, 2023 · N223NV · Airbus A320214SDR EE4Y2023100317404Unknown · unknownDURING THE ALLEGIANT EO # 53-120-003 ALLEGIANT EO INSTRUCTIONS ACCOMPLISHMENT WHICH IS RELATED WITH AD 2018-14-09 THERE WERE FOUND TWO (2 EA) FASTENER HOLES WITH CRACK INDICATION ON CROSSBEAM SPLICING AT FR 16 LHS (H8) AND AT FR 20 LHS (H26). WORK PERFORMEDMar 10, 2023 · N223NV · Airbus A320214SDR EE4Y2023100317403Unknown · unknownDURING THE ALLEGIANT WORK ORDER 00458714-91 INSPECTION INSTRUCTIONS ACCOMPLISHMENT RELATED TO AD2022-08-08 WERE FOUND HOLES AT FR16 RH SIDE WITH DIAMETERS THAT IS MORE THAN OR EQUAL TO THE MINIMUM STARTING HOLE DIAMETER. ADDITIONALLY, WERE FOUND TWO HOLES WITMar 10, 2023 · N216NV · Airbus A320214SDR EE4Y2023031017394Beam · corrodedDURING TH ESTRUCTURE INSPECTION WAS FOUND AT UPPER FUSELAGE FORWARD PAX CABIN AT FR 16, Y503.2 LONGITUDINAL BEAM WITH CORROSION. DUE TO THIS FACT LONGITUDINAL BEAM P/N: D5311282720200 FROM FR 12 TO FR 16 Y503.2 WAS REPLACED IAW A319 SRM 51-72-11-911-001. THE RMar 10, 2023 · N338NV · Airbus A319111SDR EE4Y2023031017393None · corrodedDURING TH ESTRUCTURE INSPECTION WAS AT UPPER FUSELAGE AFT PASSENGER CREW DOOR CUTOUT BETWEEN FR 66 AND FR 68 AT STRG 23R SILL BEAM WITH CORROSION. DUE TO THIS FACT SILL BEAM P/N D5348004320701 WAS REPLACED IAW A319 SRM 51-72-11-911-001 PARAGRAPH 2B. THE REPLACMar 10, 2023 · N338NV · Airbus A319111SDR EE4Y2023031017392Beam · corrodedDURING TH ESTRUCTURE INSPECTION WAS AT UPPER FUSELAGE AFT PAX CABIN AT FR 68+80MM Y160.5 LONGITUDINAL BEAM WITH CORROSION. DUE TO THIS FACT LONGITUDINAL BEAM FROM FR 68 TO FR 70 Y160.5 WAS REPLACED IAW A319 SRM 51-72-11-911-001. THE REPLACE WAS HANDLED UNDER CMar 10, 2023 · N338NV · Airbus A319111SDR EE4Y2023031017413Beam · corrodedDURING THE INSPECTION PER ALLEGIANT TASK IT WAS FOUND AT THE PAX CABIN, AFT PASSENGER LH SIDE AT FR68 DORR SILL BEAM WITH CORROSION. THE REPORTED DAMAGED PART WAS REPAIRED I/A/W THE A319 SRM 53-41-14-300-001, FIGURE 001, REPAIR PRINCIPLE 5. SEE COOPESA WORK ORMar 10, 2023 · N319NV · Airbus A319111SDR EE4Y2023031017412Beam · corrodedDURING THE INSPECTION PER ALLEGIANT TASK IT WAS FOUND AT THE PAX CABIN, AFT PASSENGER RH SIDE AT FR68 AROUND GIRT BAR A FITTING WITH CORROSION. THE REPORTED DAMAGED PART WAS REPAIRED I/A/W THE A319 SRM 53-41-14-300-001, FIGURE 001, REPAIR PRINCIPLE 5. SEE COOPMar 10, 2023 · N319NV · Airbus A319111SDR EE4Y2023031017391Beam · corrodedDURING TH ESTRUCTURE INSPECTION WAS FOUND IN THE UPPER FUSELAGE AFT PAX CABIN AT FR 68 Y765 LONGITUDINAL BEAM WITH CORROSION. DUE TO THIS FACT LONGITUDINAL BEAM P/N D5472192200000 WAS REPLACED IAW A319 SRM 51-72-11-911-001 PARAGRAPH 2 . THE REPAIR WAS HANDLED Mar 10, 2023 · N338NV · Airbus A319111SDR EE4Y2023031017411Skin Panel · nickedDURING A VISUAL INSPECTION AS PER ALLEGIANT TASK IT WAS FOUND THE LOWER FUSELAGE SKIN WITH A NICK AT FR26+385MM BETWEEN STR42L AND STR43L. THE REPORTED DAMAGED AREA WAS REPAIRED I/A/W A320 SRM 53-21-11-300-076 PARAGRAPH 2A, FIGURE 001. SEE COOPESA WORK ORDER AMar 10, 2023 · N217NV · Airbus A320214SDR EE4Y2023031017390Frame · noneDURING TH ESTRUCTURE INSPECTION WAS FOUND IN THECCKPIT WINSHIEL SIDE POST FR 4LH UPPER ATTACHMENT FITTING AND FRAME SECTION WITH DOUBLE HOLE. DUE TO THIS FACT FITTING P/N D5311086620200 AND FRAME P/N D53111068202200 WERE REPLACED. THE REPAIR WAS HANDLED UNDER Mar 10, 2023 · N338NV · Airbus A319111SDR EE4Y2023100317400Skin Panel · corrodedDESCRIPTION: DURING THE STRUCTURAL INSPECTION PER ALLEGIANT WORK CARD 200003-01-1-001_P1-OP-UP/0 PROCESS, COO FOUND AT EMPENNAGE, DORSAL FIN AREA WITH CORROSION BETWEEN THE SKIN AND CONNECTOR 7113VC. CORRECTIVE ACTION REPAIRED FUSELAGE SKIN SECTION FROM FMar 10, 2023 · N338NV · Airbus A319111SDR EE4Y2023031017409Skin Panel · dentedDURING THE ACCOMPLISHMENT ALLEGIANT TASK , IT WAS FOUND REAR LOWER FUSELAGE SKIN AT FR69+300MM BETWEEN STRINGERS 43R AND 44 WITH DENT. THE DAMAGED AREA WAS REPAIRED PER SRM 53-41-11-300-016 PARAGRAPH 2A, FIGURE 002. SEE COOPESA WORK ORDER A1M140, 1-29 FOR FURTMar 10, 2023 · N237NV · Airbus A320214SDR 2023FA0000123Link · abnormalABNORMAL INDICATION WAS DISCOVERED DURING ULTRASONIC TEST NDT 71-23-103 PART 4.Mar 10, 2023 · Cndair CL6002B19SDR EE4Y2023031017416Floorbeam · corrodedDURING THE CORROSION TASK INSPECTION IT WAS FOUND AT UPPER FUSELAGE, AFT ENTRY CABIN, WET AREA AT FR68, -Y1292, THE FLOOR BEAM WITH CORROSION. THE DAMAGED PART WAS REPLACED BY A NEWONE PER SRM 51-72-11-911-001 AND AIRBUS DRAWING D53472780. SEE COOPESA WORK ORDMar 10, 2023 · N229NV · Airbus A320214SDR EE4Y2023031017414Beam · corrodedDURING THE INSPECTION PER ALLEGIANT TASK IT WAS FOUND CORROSION AT THE AFT PASSENGER DOOR SILL AT FR68 LH SIDE. A PERMANENT REPAIR WAS PERFORMED AS PER A319 SRM 53-41-14-300-001 REPAIR PRINCIPLE 8 FIGURE 001. SEE COOPESA WORK ORDER A1M148, 2-25 FOR DETAILS.Mar 10, 2023 · N319NV · Airbus A319111SDR ASAA2023030942526Support · corrodedR/H TRANSITION PANEL STA 500C TO 500E HAS CORROSION. GROUNDED - YES. CORROSION FOUND TO BE BEYOND LIMITS IAW B737-800 SRM 53-00-53-1A-2 FIG 103 CUTOUT DAMAGED SECTION AND PERFORMED SIDEPLATE REPAIR IAW B737-800 SRM 53-00-53-2R-5W- .4 O- .040 R- 0 L- .5 D- .040Mar 9, 2023 · N536AS · Boeing 737890SDR A6WA202303098517Unknown · unknownON FWD SIDE OF FS 621 BULKHEAD ABOVE AFT BAGGAGE BAY DOOR FOR LINTEL REPAIR ACCESS FOUND RIV-NUT TO BE FREE SPINNING *********AIRCRAFT REMOVED FROM SERVICE*********** COMPLIED WITH MHIRJ REO 601R-53-61-7980 REV-- DATED 2023-03-10.Mar 9, 2023 · N436AW · Cndair CL6002B19
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