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 AALA202311066648Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING LOCATED AT BS 540 AND RBL 32.40. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1.SDR AALA202311064999Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING LOCATED AT BS 540 AND RBL 6.14. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1.SDR AALA202311066047Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING LOCATED AT BS 540 AND LBL 32.40. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1.SDR AALA202311060533Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING LOCATED AT BS 540 AND LBL 40.87. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1.SDR AALA202311062727Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING LOCATED AT BS 540 AND LBL 54.60. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1.SDR YENA2023101101234Unknown · unknownDURING HEAVY MAINTENANCE: REPLACE FRAME FOOT 43 LH DUE TO CRACK OUT OF LIMITS IN PASSENGER CABIN; REF AEROMAN NR 2023-483107 WO: 2023 276/1, REMOVED AND REPLACED FITTING FRAME AND FRAME FOOT LOC FRAME 43 LH SIDE BTW STRINGER 18 AND 24 PASSENGER CABIN I.A.W A32SDR YENA2023101101233Unknown · unknownDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 66 LH, DOOR STOP 7, UPPER INB HOLE AT AFT GA LLEY AREA (1 EA) (CRACK DIRECTION AT 1 AND 7 O CLOCK, D= 0.100 IN); (RESOLVED ON W/O: 1242939 TASKCARD: NR-00014) REF. AEROMAN N/R 2023- 482974 WO 2023 276/1, PERFSDR YENA2023101101231Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 RH, DOOR STOP 6, LOWER INB HOLE AT AFT GA LLEY AREA (1 EA) (CRACK DIRECTION AT 8 O CLOCK,D= 0.120 IN); (RESOLVED ON W/O: 1242939 TASKCARD: NR-00027) FUR-A320-53-00897 REF AEROMAN N/R 2023-482976, PERFORMESDR SWAA2023102407782Panel · delaminatedPANEL 191D IS DELAMINATED 25' AFT OF THE T/E TOOL SIDE SHOULD READ: PANEL 191D IS DELAMINATED 25' FWD OF THE T/E TOOL SIDE<[01] PANEL 191D DELAMINATION 25' AFT OF THE T/E TOOL SIDE WAS REPAIRED IAW SRM 51-70-05-2R-2 & FINISH RESTORED REFERENCE PARA 4 L.;[02] VSDR AALA202310166963Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING LOCATED AT BS 540 AND LBL 15.04. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1.SDR AALA202310160259Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING LOCATED AT BS 540 AND LBL 32.40. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1.SDR DALA2023101008327Unknown · unknownDURING WALK-AROUND ON SERVICE CHECK, CORROSION FOUND ON WASTE BOX DOUBLER. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 014-0001:0514-2001/004 00017 REPAIRED PER PRI 612578-14 REV 0, 1, 2, AND ER/A 612578-14 REV ORIGINASDR 2A6R2023100566802Unknown · unknownDURING A 1000 HOUR AIRFRAME INSPECTION FOUND L/H KEEL BEAM CAP P/N L533M1009203 AND R/H KEEL BEAM CAP P/N L533M1010203 CORRODED AT THE END OF THE CAP ON BOTH SIDES. THE CORROSION IS THROUGH THE FULL THICKNESS OF THE CAP. PERFORMING A REPAIR AS PER AIRBUS REPAISDR JGVR20231005001Unknown · unknownREPAIRED CORRODED AREAS OF THE FUSELAGE NOSE SKIN AROUND THE RH NOSE AVIONICS DOOR LATCH CUTOUTS, BY MECHANICALLY BLENDING AREAS, PERFORMING NDT, AND REPORTING FOR REPAIR DISPOSITION. FABRICATED AND INSTALLED REPAIR DOUBLERS IN ACCORDANCE WITH FIELD REPAIR.SDR JJBA20231011008Unknown · unknownAT RF1, FRAME 68, LH SIDE SHEAR CLIP BTW STR 6L-9L FOUND CRACKED. AR RF1, FRAME 68, LH SIDE SHEAR CLIP BTW STR 6L-9L REPLACED.SDR SWAA2023102406717Panel · debondedPANEL 192E OUTER SKIN IS DISBONDED. (MARKED)<[01] REPAIRED DISBONDED OUTER SKIN ON PANEL 192E IAW SRM 51-70-05-2R-2.;[02] VERIFIED CORRECTIVE ACTION ITEM 1 COMPLETED.SDR DALA2023100408191Unknown · unknownSHIP 674 WING CENTER BOX / UPPER SKIN AND STRINGER 14 / BSTA 960 AND BETWEEN LBL 70.50 & LBL 45.57 / CORROSION. CORRECTIVE ACTION: REF ERA 597544-14. (2999918)SDR DALA2023100408186Unknown · unknownSHIP 186 OPEN HOLE HFEC INSPECTION FOUND 01 EA CRACK IN THE REMOVED CHORD AT LOWER FORWARD FASTENER, AS MARKED. CORRECTIVE ACTION: ACCOMPLISHED THE REPAIR FOR FORWARD OUTER CHORD AT RH BS 1809.5 REF TO JOB CARD NO:5310-01376-0805 (2998993)SDR DALA2023100408185Unknown · unknownSHIP 186 INSPECTION FOUND 01 EA CRACK IN THE FORWARD OUTER CHORD AT LOWER FORWARD FASTENER OF "AREA 1"; IT IS VERIFIED WITH OPEN HOLE HFEC INSPECTION. CORRECTIVE ACTION: ACCOMPLISHED THE REPAIR FOR THE FORWARD OUTER CHORD AT RH BS 1809.5 REF TO JOB CARD NO:531SDR IPXA2023100651868Unknown · delaminatedACCESS Z100 PANEL 143DF DELAMINATED AND HYD CONTAMINATION DOT 049 PNL RACK, CARD NO 298481. FABBED PANEL 143DF FROM 5024N400001SS-G BATCH # 4055277 PER SREO A300-5320-57698-A, REVIEWEDSDR IPXA2023100652030Access Panel · delaminatedACCESS Z100 PANEL 147AF DELAMINATED DOT 049. CARD NO 298489 FABBED PANEL 147AF FROM 5024N400001SS-G BATCH # 4055277 PER SREO A300-5320-57698-A. REVIEWEDSDR YENA2023100301180Not Reported · not reportedDURING HEAVY MAINTENANCE: CRACK INDICATION ON WINDSHEILD CENTER POST LOWER ATTACHMENT INTERNAL AREA RH SIDE, UPPER TENSION BOLT, CRACK LENGTH IS 0.125 INCH APPROX IN COCKPIT (1 EA); (RESOLVED ON W/O: 1257978 TASKCARD: NR-00037 ) REFERENCE AEROMAN W.O. 2023 2SDR SROM2023100200023Unknown · crackedCRACK DAMAGE TO UPPER CHANNEL OF RH WING TO FUSELAGE (ARMPIT) FAIRING SUPPORT STRUCTURE AT STA X400 AND Z173.0.SDR SWAA2023100406149Panel · delaminated193B PANEL HAS A CAVITY IN THE PANEL LAYERS AROUND FASTENER HOLE #16 THAT APPEARS TO EXTEND MORE THAN HALF WAY THROUGH THE THICKNESS OF THE PANEL AND FASTENER HOLE #18 HAS DELAMINATION. 193B PANEL HAS A CAVITY IN THE PANEL LAYERS AROUND FASTENER HOLE #16 THAT SDR DALA2023100408174Unknown · unknownSHIP 3101 AIRFRAME VIBRATION WITH HISTORY. CORRECTIVE ACTION: MTC IN PROGESS. (4555546)SDR DALA2023100308089Unknown · unknownCORROSION ON FRAME CLIP STA Y=832 BTW STRG 28L/27L AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00349: CORROSION LEVEL 2. FRAME CLIP STA Y=832 BTW STRG 28L/27L AT AFT CARGO COMPARMENT WAS REPAIRED PER B717 SRM 53-00-06-2R PROCEDURE 2 REPAIR 2 AND DWG 9912243 REV JSSDR IPXA2023103094868Unknown · unknownFOUND PUNCTURE ON FUSELAGE PANEL LEFT SIDE WING TO BODY PANEL***SM39/LMX6*** INSTALLED PANEL IAW AMM 53-53-07SDR DALA2023100308084Unknown · unknownCORROSION ON CUSP WEB STA Y=965 X=-56 AT CPAX. SUMMARY OF NRC 00669: CORROSION LEVEL 2. CUSP WEB STA Y=965 X=-56 AT CPAX WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4. (LP #2993211)SDR AALA202310023798Shear Angle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING LOCATED AT BS 540 AND RBL 40.87. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1.SDR AALA202310025659Shear Angle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING LOCATED AT BS 540 AND RBL 54.60. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1.SDR 29GA2023092900001Access Door · obstructedTHE PILOT ON 403 AT 2200 Z SENT ACARS MESSAGE SAYING THAT HE HAD A RAPID DE-COMPRESSION DURING CLIMB OUT OF MCO WHEN PASSING THE 11,000 FEET AND HE IS DECLARING EMERGENCY RETURNING TO MCO. WHEN LANDED IN MCO OUR MX TEAM MET THE PILOT J. ORTIZ (6517) AND RIGHTSDR DALA2023092908005Unknown · unknownCRACK ON UPPER FITTING AT AFT CABIN COMPARTMENT IN LONGERON 2L AT STA 1116. SUMMARY OF NRC 00224: UPPER FITTING AT AFT CABIN COMPARTMENT IN LONGERON 2L AT STA 1116 WAS REPAIRED PER B717 SRM 53-00-05-2R REPAIR 2 FIG 201 SHEET 2. (LP #2992175)SDR QMLA2023092820080Unknown · unserviceableDURING INSPECTION OF TAIL CONE IN ACCORDANCE WITH 32-5302-EO-2990 CRACKS WERE DISCOVERED AT STA 6616, SERVICE ENGINEERING WAS NOTIFIED, PICTURES AND DIMENSIONS FOR THE DAMAGE WERE EMAILED IN. AWAITING A REPAIR PROCEEDURE FROM SERVICE ENGINEERINGSDR I5EA2023092700020Unknown · corrodedFORWARD CARGO FLOOR HAS CORROSION ON FRAME AT STA. 500A BETWEEN STRINGERS 26L AND 27L. CUT OUT DAMAGED SECTION OF FRAME AND INSTALLED REPAIR IAW B737-300 SRM 53-00-07 REPAIR 10 FIG 201.SDR YENA2023092901159Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION ON DOUBLER OF PREVIOUS REPAIR ON CENTER RH LONGITUDINAL BEAM FR13/FR14 AND Y270 AT RH FLOOR STRUCTURE REF TOMX W.O. 239JB/ 2301 / E190 / B8 CHECK NR00163; REPLACED RH LONGITUDINAL BEAM BTW FR13/FR14 AND Y720 AT RH FLOOR STRUSDR YENA2023092901155Unknown · unknownDURING HEAVY MAINTENANCE: INITIAL INSPECTION(CPCP): CORROSION ON CTR RH BEAM BTW FR 86-89 AND Y=250 AT FLOOR STRUCTURE (W2); (RESOLVED ON W/O: 1229824 TASKCARD: NR-00010 ) SUMMARY: CORROSION ON CTR RH BEAM BTW FR84-89 AND Y=250RH AT FLOOR STRUCTURE (W2) WAS RESDR YENA2023092901154Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION ON SHEAR CLIP OVER FR 82 BTW STRG 28/27 LH AT AFT CARGO COMPARTMENT; (RESOLVED ON W/O: 1229824 TASKCARD: NR-00011 ) REMOVED AND REPLACED SHEAR CLIP OVER FR 82 BTW STRG 28/27 LH AT AFT CARGO COMPARTMENT. PER EMB-190 SRM 51-12SDR YENA2023092901153Unknown · unknownDURING HEAVY MAINTENANCE: INITIAL INSPECTION: (CPCP FINDING) CORROSION ON SHEAR CLIP OVER FR 83 BTW STRG 20-19R AT AFT CARGO COMPARTMENT; (RESOLVED ON W/O: 1229824 TASKCARD: NR-00012 ) CORROSION ON SHEAR CLIP OVER FR83 BTW STRG 20-19R AT AFT CARGO COMPARTMENT SDR YENA2023092901152Unknown · unknownDURING HEAVY MAINTENANCE: INITIAL INSPECTION: ( CPCP FINDING): CORROSION ON SEAT TRACK BEAM BTW FR 12-13 AND Y=270RH AT FWD FLOOR STRUCTURE (W1); (RESOLVED ON W/O: 1229824 TASKCARD: NR-00013 ) CORROSION ON SEAT TRACK BEAM BTW FR12-13 AND Y=270RH, AT FWD FLOOR SDR YENA2023092901151Unknown · unknownDURING HEAVY MAINTENANCE: INITIAL INSPECTION (CPCP FINDING): CORROSIONON LH CNTR BEAM BTW FR 86-89 & Y=250LH AT FLOOR STRUCTURE (W2); CORROSION ON LH CNTR BEAM BTW FR86-FR 89 AND Y=250LH AT FLOOR STRUCTURE (W2) WAS REMOVED AND EVALUATED OUT OF LIMITS PER EMB 1SDR YENA2023092901150Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION ON SHEAR CLIP OVER FR 79 BTW STRG 25/24 LH AT AFT CARGO COMPARTMENT; (RESOLVED ON W/O: 1229824 TASKCARD: NR-00016 ) REMOVED AND REPLACED SHEAR CLIP PER EMB-190 SRM 51-41-02 AND 51-41-01. REWF TOMX NR 00223 REF TOMX W.O. 239JSDR YENA2023092901149Unknown · unknownDURING HEAVY MAINTENANCE: INITIAL INSPECTION (CPCP FINDING): CORROSION ON SHEAR CLIP OVER FR 86 BTW STRG 27-28R AT AFT CARGO COMPARTMENT; (RESOLVED ON W/O: 1229824 TASKCARD: NR-00017 ) CORROSION ON SHEARCLIP OVER FR 86 BTW STRG 27-28RH AT AFT CARGO COMPARTMENTSDR YENA2023092901148Unknown · unknownDURING HEAVY MAINTENANCE: INITIAL INSPECTION(CPCP FINDING): CORROSION ON DOUBLER OF PREVIOUS REPAIR ON CENTER LH LONGITUDINAL BEAM BTW FR 19 & Y=230 AT FLOOR STRUCTURE (W1); DOUBLER OF PREVIOUS REPAIR ON CENTER LH LONGITUDINAL BEAM BTW FR 19 & Y=230LH AT FWD FSDR CALA2023092902911Panel · corroded(B737-53-3-0785) AFT CARGO COMPARTMENT WAST TANK WHERE RINS FITTING HEATER TERMOSTAT ATTACHE TO IT THE PANAL IS CORRODED.SDR YENA2023092801143Unknown · unknownDURING HEAVY MAINTENANCE: INITIAL INSPECTION (CPCP FINDING): CORROSION ON SHEAR CLIP OVER FR 86 BTW STRG 27-28R AT AFT CARGO COMPARTMENT; "CORROSION ON SHEARCLIP OVER FR 86 BTW STRG 27-28RH AT AFT CARGO COMPARTMENT WAS REMOVED AND EVALUATED (O.T)=0.050"" & (R.SDR YENA2023092801142Unknown · unknownDURING HEAVY MAINTENANCE: INITIAL INSPECTION (CPCP FINDINGS): CORROSION ON LH CNTR BEAM BTW FR 86-FR 89 & Y=250LH AT FLOOR STRUCTURE (W2); "CORROSION ON LH CNTR BEAM BTW FR86-FR 89 AND Y=250LH AT FLOOR STRUCTURE (W2) WAS REMOVED AND EVALUATED OUT OF LIMITS PERSDR YENA2023092801141Unknown · unknownDURING HEAVY MAINTENANCE: INITIAL INSPECTION: ( CPCP FINDING): CORROSION ON SEAT TRACK BEAM BTW FR 12-13 AND Y=270RH AT FWD FLOOR STRUCTURE (W1); "CORROSION ON SEAT TRACK BEAM BTW FR12-13 AND Y=270RH, AT FWD FLOOR STRUCTURE (W1) WAS REMOVED PER EMB 190 SRM51-1SDR YENA2023092801140Unknown · unknownDURING HEAVY MAINTENANCE: INITIAL INSPECTION(CPCP): CORROSION ON CTR RH BEAM BTW FR 86-89 AND Y=250 AT FLOOR STRUCTURE (W2); "SUMMARY: CORROSION ON CTR RH BEAM BTW FR84-89 AND Y=250RH AT FLOOR STRUCTURE (W2) WAS REMOVED AND EVALUATED OUT OF LIMITS PER EMB 190 SDR YENA2023092801139Unknown · unknownDURING HEAVY MAINTENANCE: INITIAL INSPECTION(CPCP FINDING): CORROSION ON DOUBLER OF PREVIOUS REPAIR ON CENTER LH LONGITUDINAL BEAM BTW FR 19 & Y=230 AT FLOOR STRUCTURE (W1); "DOUBLER OF PREVIOUS REPAIR ON CENTER LH LONGITUDINAL BEAM BTW FR 19 & Y=230LH AT FWD SDR YENA2023092801137Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION ON SHEAR CLIP OVER FR 82 BTW STRG 28/27 LH AT AFT CARGO COMPARTMENT; REMOVED AND REPLACED SHEAR CLIP OVER FR 82 BTW STRG 28/27 LH AT AFT CARGO COMPARTMENT. PER EMB-190 SRM 51-12-01, 51-10-03, 51-75-16, 51-41-01 AND 51-41-02.
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