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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR 2A6R2023072068101Unknown · unknownDURING AN 800 HOUR AIRFRAME INSPECTION, FOUND A CRACK IN THE TOP FLANGE OF FRAME ONE. THE CRACK IS LOCATED ON THE FWD BOTTOM LBL 195 ON RIB P/N B531K1341-205 BENEATH THE CENTER CONSOLE MOUNT AND WAS MEASURED TO BE 1.4 INCH IN LENGTH.SDR EVCA202307190001Firewall · crackedAFT ENGINE FIREWALL IS CRACKED APPROX. 2.0 INCHES ON RH SIDE.SDR MK1Y20230719002Unknown · unknownSTA 933 ABOVE STR 19R INNER CHORD FRAME: DURING CONVERSION AT IAI FACILITIES, MTX FOUND CORROSION ON INNER CHORD FRAME AT STA 933 ABOVE STR 19R. THE CORROSION WAS REMOVED PER SRM PRACTICES. J/C MF02920R0217-01 WAS REISED AND FURTHER INSPECTIONS WERE PERFORMEDSDR MK1Y20230719001Unknown · unknownSTA 871.5 ABOVE STR 19R INNER CHORD FRAME: DURING CONVERSION AT IAI FACILITIES, MTX FOUND CORROSION ON INNER CHORD FRAME AT STA 871.5 ABOVE STR 19R. THE CORROSION WAS REMOVED PER SRM PRACTICES. J/C MF02920R0218-01 WAS REISED AND FURTHERSDR IPXA2023080393790Unknown · crackedINSPECTION TYPE:3CCENTER WING LOWER AUX L/H STRINGER 52 SPLICES REPAIR C AND Z HAS A CRACKED AT STA XCW=64.REMOVED, FABRICATED AND REPLACED CRACKED SPLICES REPAIR AT THE CENTER WING LOWER AUX L/H STRINGER 52 IAW SRM 57-10-03 FIG 201 REPAIR 1. (MAJOR)SDR AALA202307191576Tape · peelingAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED RETURNED TO CLT. WHILE CLIMBING THRU 5000 FEET, THE FLIGHT CREW HEARD A BANG FOLLOWED BY THE SOUND OF AIR RUSHING ABOVE. THE FLIGHT CREW THOUGHT THYE HAD HIT SOMETHING AND SUBSEQUENTLY SDR DALA2023071905857Unknown · unknownSHIP 3353 DURING HCK AT SAL AND DURING ACCOMPLISHMENT OF EM 5330-01152, SE VERAL FASTENERS COMMON TO THE FR 84, 85, 86, AND 87 REINFORCEMEN T ANGLES COULD NOT BE INSTALLED PER THE EM. CORRECTIVE ACTION: REF ER/A 610508-14AD. (2872401)SDR DALA2023071905856Unknown · unknownSHIP 3353 DURING HCK AT SAL AND DURING ACCOMPLISHMENT OF EM 5330-01152, SE VERAL FASTENERS COMMON TO THE LH FR 84,85, 86, AND 87 FRAME REIN FORCEMENTS COUND NOT BE INSTALLED PER THE EM. CORRECTIVE ACTION: REF ER/A 610507-14AD. (2872375)SDR SWIA20230717Unknown · crackedLEFT SIDE ABOVE AFT CARGO DOOR AT FS 605.0 STR 9.0 JUST ABOVE AND BELOW FRAME FLANGE IS CRACKED A RIVET HOLE LOCATION. INSIDE FUSELAGE.COMPLIED WITH ALL STEPS 1-7. REMOVED DAMAGED AREA, FABRICATED, AND INSTALLED ALL REPAIR ITEMS ON FS605 FRAME, STGR 9L REF RESDR SWAA2023081779391Unknown · crackedMAIN CABIN INNER CHORD CRACKED AT AT FASTENER HEAD STA 294.5+8' LBL 55'<[01] REMOVED AND REPLACED NEW INNER CHORD AT FWD MAIN CABIN LBL 55 SRM 51-40-02-0G-0 AND DWG :141A8110;[02] (RII) VERIFIED STEP 1;[03] COMPLETEDSDR SWAA2023072879406Angle · crackedCRACK FOUND ON CENTER TANK UPPER ATTACH ANGLE AT STA 663 RBL 45 ( WL 193 )<[01] REMOVED THE REPAIR THAT WAS ORIGINALLY INSTALLED PER NRC G098319. INSTALLED A NEW REPAIR PER EA 23-157-02220 [SRM 57-10-10-2R-3 (REPAIR 3 ALTERNATE 2) AND SRM 57-10-10-2R-6 (REPAIRSDR YENA2023071900835Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FRAME 68 RH SIDE AT LEVEL STR. 22R IN LOWER HOLE INBD. SIDE OF THE DOOR STOP FITTING Ñ1 CRACK DIRECTION 8 AND 12 O CLOCK; (RESOLVED ON W/O: 1227112 TASKCARD: NR-00012 ) REF AEROMAN NR 2023-393765 WO 2023 228SDR YENA2023071900834Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FRAME 68 LH SIDE AT LEVEL STR. 22L IN LOWER HOLE INBD. SIDE OF THE DOOR STOP FITTING Ñ 1 CRACK DIRECTION 12 AND 5 O'CLOCK AFT GALLEY AREA; (RESOLVED ON W/O: 1227112 TASKCARD: NR-00013 ) REF AEROMAN NR 2023-39SDR YENA2023071900833Unknown · unknownDURING HEAVY MAINTENANCE: CRACK SHEAR PLATE LOC BTW FR69 TO FR 70 AT LEVEL STRG 23L AT AFT GALLEY AREA; (RESOLVED ON W/O: 1227112 TASKCARD: NR-00019 ) REF AEROMAN WO 2023-228/1, NR 2023-393830; REMOVED AND REPLACED SHEAR PLATE LOC. BTW FR69 TO FR70 AT LEVEL STSDR YENA2023071900832Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION LOWER SILL LOC BTW FR 66 TO FR 68 AT LEVEL STR23L AT AFT GALLEY AREA (REPAIR AREA)CPCP RELATED ITEMS MPD RELATED TASK 534195/01; (RESOLVED ON W/O: 1227112 TASKCARD: NR-00023 ) REF AEROMAN WO 2023-22/1, WO 2023-393831; PERFSDR YENA2023071900831Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION LOWER SILL BTW FR60 AND FR62 IN BULK CARGO COMPARTMENT (CPCP RELATED REFER TO MPD TASK 534107-01); REF AEROMAN WO 202-228/1, NR 2023-393838; PERFORMED REPAIR ON LOWER SILL BTW FR60 AND FR62 IN BULK CARGO COMPARTMENT IAW A320SDR CALA2023071902274Unknown · corrodedPOSSIBLE CORROSION ON LH INNER CHORD BTW STA. 992.5 TO STA 947.5 (REF. AAR NR 99977302). REMOVED AND INSTALLED NEW LH INNER CHORD BTW STA 992.5 TO STA QC A78 V768499). 947.5 IAW B737-700 SRM 51-40-02-0G-0, SRM 51-40-05-0G-0, SRM 51-40-08-0G-0, DRAWING #147A850SDR QR9R2023071700002Rail · unserviceableAFTER SHUTDOWN, WHILE SECURING AIRCRAFT, THE L/H SLIDING DOOR CAME OFF THE TRACK WHILE IT WAS BEING CLOSED. REPLACED L/H SLIDING DOOR CENTER CAR RAIL IAW 53-31-01, 4-2.SDR DALA2023071805807Unknown · unknown(LOG 2867629) AFT CARGO COMPARTMENT DOOR CUTOUT SURROUND STRUCTURE LOWER BILGE AREA UNDER SCUFF PLATE IS HEAVILY CORRODED. REMOVED AND REPLACED SILL LOWER CHORD AND WEB IAW B737 SRM 51-40-02 AND B737 SRM 51-40-05.SDR UIEA2023071860709Unknown · unknownAPU COMPARTMENT L/H STA 2664 WL 305 FRAME FOUND CRACKED.(<P>APU COMPARTMENT L/H STA 2664 WL 305 FRAME P/N: 65B02757-13 CRACK AREA REPAIRED IAW RI-53-82-16342 REV A. NO FURTHER DEFECTS NOTED.</P>)SDR IPXA2023081693929Bracket · brokenINSPECTION TYPE:1CBROKEN CENTER SUPPORT BRACKET AT C54 R/H.REMOVED, FABRICATED AND REPLACED IAW SRM 51-40-21.SDR YENA2023071800820Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION LOWER SIL LOC. BTW FR66-FR68 STR 23L AT AFT GALLEY AREA (CPCP MPD 534195-01); (RESOLVED ON W/O: 1222084 TASKCARD: NR-00021 ) REMOVED & REPLACED LOWER SIL LOC. BTW FR66- FR68 AT STR 23L AT AFT GALLEY AREA IAW A320 SRM 5-42-11SDR YENA2023071800819Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION LOWER SIL LOC. BTW FR 66- FR68 AT STR 23R AT AFT GALLEY AREA. (CPCP MPD 534195-01); (RESOLVED ON W/O: 1222084 TASKCARD: NR-00022 ) PERFORMED PERMANENT REPAIR ON LOWER SIL BTW FR 37 PLUS 12.5 INCHES THRU FR 68 AT LEVEL OF STRSDR YENA2023071800803Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION INTERNAL STRUCTURE WEB LOC. BTW FR 69 AND FR 70 AT LEVEL STR 23L AT AFT GALLEY AREA (CPCP-RELATED MPD TASK 534195-01); REMOVED AND REPLACED STRUCTURE WEB LOC. BTW FR69 AND FR70 AT LEVEL OF STR 23L AT AFT GALLEY AREA IAW A320SDR YENA2023071800801Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION LOWER SIL LOC. BTW FR 66- FR68 AT STR 23R AT AFT GALLEY AREA. (CPCP MPD 534195-01); PERFORMED PERMANENT REPAIR ON LOWER SIL BTW FR 37 PLUS 12.5 INCHES THRU FR 68 AT LEVEL OF STR 23R SIDE. IAW A320 SRM 53-41-14-300-001 PAR 2ASDR 2023FA0000369Unknown · unknownDURING THE ACCOMPLISHMENT OF ADSI IB744530258 – SHEAR TIE AT STA 1000 LBL 57.50 CENTER TANK TOP FOUND CRACKED AT STANDOFF FASTENER HOLES. INSPECTION TASK RELATED TO AD 2015-13-06, SB 747-53A2860.SDR AALA202309057412Fork · wornAIRCRAFT IN BASE MAINTENANCE: AFT AVIONIC COMPARTMENT RACK 80VU LEFT HAND LOWER LATERAL FITTING WORN BETWEEN FR 23 AND FR 24 AT Y1263. REPLACED FORK END PER EA 346411.SDR AALA202309058800Fork · wornAIRCRAFT IN BASE MAINTENANCE: AFT AVIONIC COMPARTMENT RACK 80VU RIGHT HAND LOWER LATERAL FITTING WORN BETWEEN FR 23 AND FR 24 AT -Y1263. REPLACED FORK END PER EA 346411.SDR SWAA2023081678302Access Panel · bulgedLOWER MID KEEL BEAM ACCESS PANEL # 192F HAS FASTENER HOLES BULGING/CRACKED<[01] ALL STEPS COMPLETED;[02] SUMMARY=PREPARED DAMAGED AREA FOR REPAIR (FASTENER HOLES) AT PANEL #192F AS PER B737 SRM 51-70-04-2R-9.<BR>APPLIED REPAIR IN DAMAGED AREA (FASTENER HOLES) SDR HNAA2023080700289Unknown · unknownE986166 EXTERNAL FUSELAGE REPAIR FRAME 7-8 STR 13L-15L HAS NO DTI INFO. : RECEIVED PIEDMONT EO1-05-23-0186 FOR EXISTING EXTERNAL FUSELAGE REPAIR AT FR 7-8 AND BTW STR 13L-15L. EO ACCEPTS REPAIRED AREA AS IS AND HAS INSTRUCTIONS FOR DTISDR DALA2023071405722Unknown · unknownSHIP 3248 NEED TO COMPLY WITH ER/A 605147-14AD REV A SECTION III. (CRACK). CORRECTIVE ACTION: COMPLIED WITH ER/A 605147AD REV A SECTION III. (2865054)SDR CALA2023071402253Profile · cracked(A3NB-52-4-6032) LH EMERGENCY ESCAPE HATCH AFT LOAD TRANSMITTING PROFIL IS CRACKED BETWEEN FASTENERS. DOT NO. 17-39. W/C:58438 REMOVED LH EMERGENCY HATCH LOAD TRANSMITTING PROFIL IAW SRM 51-4 2-11 2 EA INSTALLED NRU FWD LOAD TRANSMITTING PROFIL AND SHEET 2 EA SDR FDEA202307121743Fitting · failedCORROSION FOUND IN THE RIB 5 FITTING. REPAIRED PER AIRBUS REPAIR INSTRUCTIONS R57240425SDR SWAA2023081677573Channel · corrodedAFT CARGO COMPARTMENT RIGHT SIDE; FLOOR STRUCTURE 'Z CHANEL' AROUND HOLES HAS EVIDENCE CORROSION BETWEEN STA 727J TO STA 747.<[01] RH Z CHANNEL SECTION TO BE REPLACED FROM STA 727F TO 767 FOR WORK ACCOMPLISHED REFERENCE TASKCARD: TTG8Q00M5XGH;[02] RH Z CHANNELSDR SWAA2023081677985Access Panel · bulgedLOWER FUSELAGE FWD KEEL BEAM ACCESS PANEL # 192E HAS BULGING/CRACKED FASTENER HOLES<[01] PREPARED DAMAGED AREA FOR REPAIR FASTENER HOLES AS MARKET ON PANEL #192E AS PER B737 SRM 51-70-04-2R-9. APPLIED REPAIR IN DAMAGED AREA (FASTENER HOLES) AS PER B737 SRM 51-SDR DALA2023071405731Unknown · unknownSHIP 3326 WINGS/CENTER/FR 40 BLKHD/HOLE #260 LH,RH/INSPECTIONS. CORRECTIVE ACTION: REF ER/A 604565-14AD. (2863124)SDR CALA2023071402240Profile · crackedRH EMERGENCY ESCAPE HATCH AFT LOAD TRANSMITTING PROFIL IS CRACKED BETWEEN FASTENERS. DOT NO. 17-40. W/C:58439 REMOVED RH EMERGENCY ESCAPE HATCH AFT LOAD TRANSMITTING PROFIL IAW SRM 51-42-11. INSTALLED NEW TRANSMITTING PROFIL 2EA IAW SRM 51-42-11. TREATED AND PSDR DALA2023071305709Unknown · unknownSHIP 0676 CORROSION AT BEAM STA 1681. CORRECTIVE ACTION: SUMMARY OF NRC 000692. BEAM STA 1681 WAS REPAIRED PER B757-200 SRM 53-60. (2862210)SDR DALA2023071305704Unknown · unknownSHIP 0687 CORROSION ON PREVIOUS REPAIRED DOBLER BTW STA 1500 TO STA 1520, S-29L TO S-28L AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00100 DOUBLER WAS REPLACED PER DWG AFP42-0040-00 AND B757-200 SRM 51-40. (2861704)SDR FXGA202307122336Unknown · unknownDAMAGE TO FLOOR STRUCTURE F/S 1148 BL RIGHT 45 WL 208. REPAIR OF DAMAGE FLOOR STRUCTURE AT F/S1148 BL RIGHT 45 WL 208. FABRICATE REPLACEMENT PARTS AND INSTALL PER SRM.SDR SWAA2023072177057Unknown · corrodedAFT CARGO COMPARTMENT; FWD L/H #3 CAPSTRIP HAS CORROSION ON LOWER SURFACE AFT CARGO COMPARTMENT FWD L/H #3 CAPSTRIP HAS CORROSION ON LOWER SURFACE<[01] REMOVED AND INSTALLED NEW CAP STRIP P/N 453A2611-10 A TAG A194733 IAW SRM 51-40-02;[02] VERIFIED ITEM 1<BR>CSDR DALA2023071305705Unknown · unknownSHIP 0667 CORROSION ON PREVIOUS REPAIR DOUBLERS ON WEB BTW STA 1711-1720 IN 13LBL, 10LBL AND 23LBL AND BTW STA 1681-1700 RBL 50 AT CABIN FLOOR STRUCTURE W4. CORRECTIVE ACTION: NEW DOUBLERS ON WEB BTW STA 1711-1720 IN 13LBL, 10LBL, AND 23LBL AND BTW STA 1681-17SDR REXA2022071200490Fitting · damagedWHILE PERFORMING SB 670BA-53-044 REVISION G DATED JUL 05/2022 PART B FOUND LH STR12 FITTING PN CC670-33563-001SB CANNOT BE INSTALLED IN ACCORDANCE WITH SERVICE BULLETIN INSTRUCTIONS DUE TO LOW EDGE DISTANCE AT FASTENER GOING THROUGH FITTING AND BULKHEAD AND THSDR IPXA2023071972719Unknown · unknown*SDR FILED OPEN* *MAJOR REPAIR* FAULT: DENT FOUND ON RH STA 1260 LOWER FRAME REVIEWED.SDR UIEA2023070400682Unknown · unknownCORROSION DAMAGE ON THE SECTION 43, SHEAR PANEL, BETWEEN STA 566 / STA 610 AND RBL 73.80 / RBL 88.50(<P>REWORKED AREA ON THE SECTION 43, SHEAR PANEL, BETWEEN STA 566 / STA 610 AND RBL 73.80 / RBL 88.50 PER MXA EO TRE6753606 - FVCI REF. 23109-3 (APPROVED BY FAASDR UIEA2023070400683Unknown · unknownCORROSION DAMAGE ON THE SECTION 41, SHEAR PANEL, BETWEEN STA 368 / STA 390 AND LBL 54.75 / LBL 76.80(<P>REWORKED AREA ON THE SECTION 41, SHEAR PANEL, BETWEEN STA 368 / STA 390 AND LBL 54.75 / LBL 76.80 PER MXA EO TRE6753605 - FVCI REF. 23109-2 (APPROVED BY FAASDR UIEA2023070400684Unknown · unknownCORROSION DAMAGE ON THE SECTION 41, SHEAR PANEL, BETWEEN STA 368 / STA 390 AND LBL 76.80 / LBL 88.50(<P>REWORKED AREA ON THE SECTION 41, SHEAR PANEL, BETWEEN STA 368 / STA 390 AND LBL 76.80 / LBL 88.50 PER MXA EO TRE6753604 - FVCI REF. 23109-1 (APPROVED BY FAASDR UIEA2023070400685Unknown · unknownCORROSION DAMAGE ON THE SECTION 41, SHEAR PANEL, BETWEEN STA 266.5 / STA 287.5 AND LBL 54.75 / RBL 54(<P>REWORKED AREA ON THE SECTION 41, SHEAR PANEL, BETWEEN STA 266.5 / STA 287.5 AND LBL 54.75 / RBL 54 PER MXA EOS TRE6753607 (FVCI REF. 23109-4), TRE6753608 (SDR DALA2023071005541Unknown · unknownSHIP 0676 CORROSION AT WEB S17L BTWN STA 960 AND STA 980 AND PAX CABIN IN REF NRC 00491. CORRECTIVE ACTION: SUMMARY OF NRC 00703: WEB S17L BTWN STA 960 AND STA 980 AND PAX CABIN WAS REPLACED PER B757-200 SRM (2858047)SDR HNAA2023080700288Unknown · unknownE985348 STRINGER 6R CRACKED BEHIND FRAME 13 R/H SIDE OF COCKPIT. EMOVED AND REPLACED STRINGER 6R BEHIND FRAME 13 R/H SIDE OF COCKPIT IAW EMB145 SRM 51-40-02.
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