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.
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 DALA2022112907604Longeron Fitting · crackedSHIP 198 HFEC INSPECTION FOUND 01 EA CRACK AT LH LOWER UNDER-WING LONGERON FITTING AS MARKED AND REPLACEMENT IS REQUIED IN ACCORDANCE THE W/C 5711-01042-03. CORRECTIVE ACTION: ACCOMPLISHED LONGERON FITTING MOD AT LH LWR UNDER WING REF TO JOB CARD 5711-01042-03SDR DALA2022112907603Not Reported · crackedSHIP 198 HFEC INSPECTION FOUND 01EA CRACK OF THE REMOVED FWD OUTER CHORD AT NINTH FASTENER HOLE OF COUNT FORM TOP, IT IS ABOUT 25MM LONG AND DIRECTION IS 7 O'CLOCK. CORRECTIVE ACTION: ACCOMPLISHED RH SIDE FWD OUTER CHORD PERMANENT REPAIR REFER TO AMDS WORKCARDSDR DALA2022112907602Not Reported · crackedSHIP 198 HFEC INSPECTION FOUND 01EA CRACK OF THE REMOVED FWD OUTER CHORD AT FORWARD SIDE FASTENER OF DOWN MOST ROW, IT IS ABOUT 5MM LONG AND DIRECTION IS 1 O'CLOCK. ACCOMPLISHED RH SIDE FWD OUTER CHORD PERMANENT REPAIR REFER TO AMDS WORKCARD 5310-01376-0805 (SDR DALA2022112907601Structure · crackedSHIP 198 HFEC INSPECTION FOUND 01 EA CRACK AT FORWARD OUTER CHORD INTERNAL SURFACE.IT IS AROUND THE FORWARD FASTENER IN CIRCLE NOTE 5 AREA AS PER STEP 4 .ACCOMPLISH SECTION 08(RH) PRIOR TO FURTHER FLIGHT. CORRECTIVE ACTION: ACCOMPLISHED RH SIDE FWD OUTER CHORDSDR DALA2022112907600Structure · crackedSHIP 198 HFEC INSPECTION FOUND 01 EA CRACK AT FORWARD OUTER CHORD INTERNAL SURFACE.IT IS AROUND THE FIFTH FASTENER COUNT FROM TOP IN CIRCLE NOTE 3 AREA AS PER STEP 2 .ACCOMPLISH SECTION 08(RH) PRIOR TO FURTHER FLIGHT. CORRECTIVE ACTION: ACCOMPLISHED RH SIDE FWSDR CALA2022112803237None · noneCARGO SPILL IN AFT PIT, APPEARS TO BE GRAVEL THROUGHOUT ENTIRE AFT CARGO PIT. PERFORMED IMMEDIATE CLEANUP.WITHIN 7DAYS,ACCOMPLISH EC/RA2011-01000,CARGO COMPARTMENT IN DEPTH SPILL CLEANUP ADD EMP:U339805 PER ECRA 2011-01000 WITHIN 7 DAYS ACCOMPLISH IN DEPTH CLESDR YENA2022112901164Not Reported · corrodedDURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE III / FR80 & STGR 27R-28R / CORROSION. TEMPORARY REPAIR. (CONSIDERED AS A MAJOR REPAIR)SDR YENA2022120501210Access Door · handler errorFLT# 1802, FLL-JFK. 'AIRCRAFT SUSTAINED DAMAGE FWD OF THS ACCESS DOOR-SKIN PUNCTURE; IMPACT DAMAGE REPAIRED IAW TASK CARD A22-971-01 "FUSELAGE/AFT FUSELAGE/FR 69-70 & STR 40RH AND 41RH/SKIN PUNCTURE-TIME LIMITED REPAIR" AND NON ROUTINE ITEMS NR00002 THRU NR00SDR EVCA11232022Stiffener · crackedLEFT HAND VERTICAL TUNNEL STIFFENER IS CRACKED ON UPPER ENDSDR DALA2022122308335Unknown · unknownBS 1340 TO STA 1380 AND STR S-3L TO STR S-3R. IDTV DEMOD HOLES CRACKED. CORRECTIVE ACTION: REF ERA 603941-14.SDR DALA2022112807566Unknown · crackedSHIP 659 DTE, ER/A 590590-14 REV. A; FUSELAGE / MAIN FRAME / OPENING FRAME / LOWER MAIN SILL / CHORD / STA.1360 TO 1440, S-26R TO S- 28R / CRACK & CORROSION. CORRECTIVE ACTION: REF ERA 590590-14 REV A. (2508077)SDR CALA2022112303209Not Reported · crackedPERFORM EA 5310-04554 REV B OP 005 REF. AAR N/R:9662903 ACCOMPLISHED EA 5310-04554 REV."B" OP-005, SHORT CRACK ON OR STOP DRILLED CRACKS,CONFIGURATION "B" ON JOB CARD SEQ#1431.SDR CALA2022112103192Screw · missingPDA 3 FOUND A SCRREW MISSING FROM PANEL 195LL. SIZE IS SMALLER THAN 15 SQUARE INCHES. INSTALLED A NEW SCRREW. CORRECTION OF PANEL#, CORRECT PANEL# IS 197LL.SDR FXGA202211172230None · noneFUSELAGE SKIN GOUGED AT F/STA 463, STR 21L. TO REPAIR A DEEP GOUGE ON FUSELAGE SKIN. PERFORM SKIN REPAIR PER AEI EO 20455.SDR YENA2022111001105None · noneDURING HEAVY MAINTENANCE: CORROSION LOWER SILL LOCATED ON FR 68 STR 23L AT AFT GALLEY AREA; PERFORMED PERMANENT REPAIR ON LOWER SILL LOCATED ON FR68 STR 23L AT THE AFT GALLEY AREA IAM A321 SRM 53-41-14-300-001 STEP 2. A FIGURE 001.ALL WORK ACCOMPLISHED BY AEROSDR CALA2022110903092Unknown · vibrationINTERMITTENT STRONG VIBRATION IN TAIL OF AIRCRAFT LANDING. FLUSHED TOILETS WITH NO EFFECT. DID NOT NOTICE ANY DIFFERANCE IN CABIN PRESSURE. DEBRIEFED CREW. VIBRATION WAS FIRST FELT BY THE CABIN CREW IN THE CREW REST AREA, THEN IT WAS FELT IN THE AFT GALLEY ANDSDR DALA2023080906497Unknown · unknownSHIP 3115 CRACKS FOUND IN LHS CONTINUITY FITTING AND RHS FRONT WINDSHIELD FRAME AT LWR CENTER POST. CORRECTIVE ACTION: REPAIRED PER 602799-14AD. (2487495)SDR YENA2022111101114None · noneFLT#1075, PVD-MCO. 'LEVEL 3 FUME NOTED ON DECENT THROUGH 20,000 IN FWD AND AFT GALLEYS; PERFORMED GVI OF APU NO LEAKS NOTED. PERFORMED LEVEL A DECONTAMINATION. COMPLIED WITH INFORMATION NOTICE 2017-T015, SECTION A, ISOLATED FAULT TO TYPE 10 (A), 1, C PER TSM 0SDR SIMA20221107002None · noneHIGH SPEED REJECTED TAKEOFF AT APPROXIMATELY 90 KIAS. BRK OVERHEAT EICAS MSG FOLLOWED QRH PROCEDURE. RIGHT OB BRAKE RAN HOTTEST (450 DEGREES CELSIUS) ALL BRAKES TEMPORARILY IN AMBER. MEDIUM BRAKING WAS APPLIED DURING REJECT-C/A-DEFERRED PER AMM REF AMM 05-50-1SDR SIMA20221107001None · noneSMELL IN CABIN AFTER TAKEOFF, CLIMB,AND LANDING PERFORM F C F CLIMBING TO CRUISE ALTITUDE FOR FOR 30 MIN COLD SOAK AND RETURN TO LAND , FA2 STATED SHE SMELLED BURNING SMELLED DURING TAKE OFF ROLL AND IMMEDIATELY ON LANDING THEN SMELL DISAPPERED.REF TO LGP 4716SDR CALA2022110703074Fastener · missingMISSING FASTENERS, INSTALLED NEW FASTENERS.SDR YENA2022110701094None · noneFLT#1280, FLL-DCA. 'DURING TOP OF DESCENT A STRONG ELECTRIC TYPE SMELL PICK UP ON ALL AIRCRAFT. ESPECIALLY STRONGER ROWS 17 AND 18 PER INFLIGHT; ACCOMPLISHED AMM 05-50-00-810-831-A INSPECTION TO IDENTIFY THE CAUSE OF THE CABIN ODOR REPORTED. FOUND A HINT OF SMSDR SIMA20221105002None · noneHIGH SPEED - 166 KTS FOR 2 SEC FLAPS FULL WS ESCAPE/ GO AROUND-C/A-C/W FLAP/SLAT EXTENDED SPEED EXCEEDANCE W/C 05-50-07-200-801. SPEED EXCEEDANCE WAS FOUND TO BE BELOW THE THRESHOLD VALUE AND TIME WAS BELOW 10 SECONDS. NO FURTHER ACTION REQUIRED PER W/C. NO DESDR JJBA20221107005None · noneDAMAGE FOUND ON LH SIDE SKIN BTW FR 61-64 AND BTW STR 17L-18L. REPAIR DOUBLER ON LH REAR FUSE 1 SKIN, BTW FR 61-63 AND BTW STR 16L-18LSDR TAMF20221104029None · noneDURING THE AIRCRAFT UNLOADING PROCEDURE, A GOUGE WAS FOUND ON FRAME 20 RH SIDE OF THE FWD CARGO DOOR CUT OUT.
IN ACCORDANCE WITH AIRBUS STRUCTURAL REPAIR MANUAL TASK MANUAL 53-21-11-283-006A TEMPORARY REPAIR WAS PERFORMED.SDR YENA2022110201084None · noneFLT#1558, BOG-FLL .' INFLIGHT COMPLAINED ABOUT DIRTY SOCKS SMELL AT 18K TILL LANDING. THE FLIGHT CREW DIDN'T EXPERIENCE IT; INSPECTED A/C AND FOUND THE LEVEL TO BE LEVEL A. PERFORM TSM 05-50-00-810-831-A AND IDENTIFIED THE SOURCE OF ODOR TO BE APU. PERFORMED ESDR WX0A2022110274304None · noneNRC 0000-0004:THIS NRC IS RAISED TO COMPLY WITH ALLEGIANT M313 DIGITAL FORM COMPLIANCE, REFER 5000-0038 CORROSION FOUND ON LH WING UPPER SKIN UPPER SURFACE AT RIB 8 REAR SPAR AREA. / PROCESS FORM M313 ACCOMPLISHED, M313 ATTACHED.CORROSION REMOVED AS PE SRM 51-SDR WX0A2022110274303None · noneNRC 0000-0003: THIS NRC IS RAISED TO COMPLY WITH ALLEGIANT M313 DIGITAL FORM COMPLIANCE, REFER 6000-0029 R/H WING T/E AT RIB 7, CORROSION FOUND ON UPPER SKIN LOWER SURFACE / PROCESS FOR M313 CARD ACCOMPLISHED, M313 ATTACHED.CORROSION REMOVED AS PER SRM 51-74-0SDR WX0A1900010074302None · noneNRC 5000-0026: 193-26. CORROSION FOUND ON LH WING UPPER SKIN LOWER SURFACE AT TRAILING EDGE AREA BETWEEN RIB 7-9/ L/H WING UPPER SKIN LOWER SURFACE AT TRAILING EDGE AREA BTW RIB 7-9 CORROSION REMOVED AT BLEND AREA (A-C-D) AND REPAIRED AS PER TD/70525679/055/20SDR WX0A1900010074301None · noneNRC 5000-0038: 193-32. CORROSION FOUND ON LH WING UPPER SKIN UPPER SURFACE AT RIB 8 REAR SPAR AREA. / LH WING UPPER SKIN UPPER SURFACE AT RIB 8 REAR SPAR AREA, CORROSION REMOVED AT BLEND AREA B AND REPAIRED AND AS PER TD/70525679/055/2022#C AND AIRBUS REPAIR ISDR WX0A1900010074300None · noneNRC 5000-0025: 193-22. CORROSION FOUND ON LH WING UPPER SKIN LOWER SURFACE AT TRAILING EDGE AREA RIB 22./LH WING UPPER SKIN LOWER SURFACE AT TRAILING EDGE AREA RIB 22, CORROSION REMOVED AT BLEND AREA NO.1 AND REPAIRED AND AS PER TD/70525679/055/2022#C AND AIRSDR WX0A1900010074295None · noneREF WO465856-1 TC53-140-003, NOTED TOOLING MARK ON THE LH KEEL BEAM MLG DOOR FWD HINGE FITTING AFT LUG AFT FACE AT 3 O'CLOCK POSITION, MEASURING 0.200-IN L X 0.100-IN W X 0.015-IN D./REMOVED AND REPLACED LH MLG DOOR LOWER FWG HINGE FITTING IAW AIRBUS REPAIR INSDR UIEA2022103001177None · noneDURING AFT CGO COMPT INSPECTION, FOUND PREVIOUS TRIMMED AREA ON THE FLOOR WEB ORIGINAL HOLE AT FS 1910 RBL 44".(<P>AFT CGO COMPT STA 1910 RBL 44" DAMAGED AREA TRIMMED OFF AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 AND EO 4453C264</P>)SDR YENA2022110101081None · noneDURING HEAVY MAINTENANCE: CORROSION ON WEB BTW FR 87 AND Y= +300 / Y=-1200; REF TOMX WO: N354JB/2047 NR-00229 - CORROSION ON SHEAR PANEL CENTRAL AND LH SIDE BTW FR87 AND Y= +300 / Y=-1200 WAS REMOVED AND EVALUATED OUT LIMITS PER EMB 190 SRM 51-12-01, SRM 51-10SDR YENA2022110101080None · noneDURING HEAVY MAINTENANCE: CORROSION ON FLOOR STRUCTURE WEB (UPPER AND LOWER SURFACE) BTW FR 12-16 AND Y=-1090 TO Y=-1270 (LH SIDE); REF. TOMX WO: N354JB/2047 NR-00259 - CORROSION ON FLOOR STRUCTURE WEB (UPPER AND LOWER SURFACE) BTW FR 12-16 AND Y=-1090 TO Y=-1SDR YENA2022110101079None · noneDURING HEAVY MAINTENANCE: CORROSION ON FLOOR SUPPORT UPPER SURFACE BTW FR 15-16 AND Y=-1110 TO Y=-1170 (LH SIDE); REF. TOMX WO: N354JB/2047 NR-00260-: CORROSION ON FLOOR SUPPORT BTW FR 15-16 AND Y=-1110 TO Y=-1170 (LH SIDE) WAS REMOVED AND EVALUATED OUT OF LIMSDR YENA2022110101077None · noneDURING HEAVY MAINTENANCE: SEVERAL CORROSIONS ON FLOOR STRUCTURE WEB UPPER BTW FR 15-16 AND Y=.-320 TO Y=-930 LH SIDE; REF TOMX WO 2047 NR 00262. REMOVED AND REPLACED DOUBLE UPPER SURFACE BTW FR 15-16 Y=-320 TO Y=-930 LH SIDE REF SRM 51-41-02 AND 51-42-02.SDR YENA2022110101076None · noneDURING HEAVY MAINTENANCE: SEVERAL CORROSIONS ON TRANSVERSAL BEAM OF FLOOR STRUCTURE ON FR 17 BTW Y=-290 TO Y=290; REPAIRED TRANSVERSAL BEAM FLOOR STRUCTURE REF EMB 190 SRM 53-00-10 REPAIR 53. REF TOMX WO 2047 NR00264.SDR YENA2022110101066None · noneDURING HEAVY MAINTENANCE: REF TOMX WO 2047 NR 00253. CORROSIONS ON FLOOR STRUCTURE LONGITUDINAL BEAM BTW FR 12-19 AND Y=240 TO Y=300 RH SIDE; REMOVED AND REPLACED LONGITUDINAL BEAM REF SRM 51-41-01,51-41-02,51-43-01 AND 51-43-04.SDR YENA2022110101064None · noneDURING HEAVY MAINTENANCE: CORROSION ON FLOOR SUPPORT (UPPER SURFACE) BTW FR 12-13 AND Y=350 TO Y=410 RH SIDE; REF TOXM WO 2047 NR 00252. REMOVED AND REPLACE FLOOR SUPPORT IAW EMB 190 SRM 51-41-01 AND 51-43-01. BTW FR 12-13 AND Y=350 TO Y=410 RH SIDE.SDR YENA2022110101049None · noneDURING HEAVY MAINTENANCE: FUSELAGE/ FR35 FWD FACE-TO-PRESSURE BULKHEAD ATTACHMENT AT LEVEL OF STGR30 LH - CRACK ON FASTENER HOLE/ DTA. (CONSIDERED A MAJOR REPAIR)SDR SWIA202266677None · damagedLT SIDE OF FUSELAGE, AFT OF MAIN CABIN DOOR, BELOW PAX WINDOW AT 1A, HAS DAMAGE THAT NEEDS TO BE EVALUATED (FILED CLOSED) COMPLIED WITH PERMANENT REPAIR ON LH FUSLAGE SKIN BETWEEN FS364.00 - FS374.00 AND STR13L -STR14L IN REFERENCE TO REO 601R-53-21-3576 RSDR YENA2022103101046None · noneFLT#2427, FLL- MBJ. (AIRCRAFT PERFORMED AN AIR TURN BACK TO FLL) 'SIMILAR TO THE PREVIOUS LOGBOOK ENTRY ON CLIMB AT 11000 AT 300 KTS, NOTICEABLE VIBRATION NO ENG VIBRATION WAS NOTED. AT FL 80 RECEIVED A CALL FROM FROM FA IN REAR GAELLEY NOTING STRONG VIBRATIOSDR COEA2023011015807Fitting · crackedWO 239777 NR 100050 HEAVY CHECK COE/MAJOR REPAIR: L/H MAIN GEAR TRUNNION FITTING HAS A CRACK ON THE UPPER SURFACE AT THE UPPER FASTENER FOR THE FAIRING SUPPORT. CORRECTIVE ACTION: REPAIRED L/H TRUNNION IAW ATR72 SRM 535700-300-802-A01.SDR UIEA2022092000997None · noneM/D STA 460 LBL 95 - 98 FLOOR BEAM UPPER CAP FOUND CORROSION(<P>FLOOR BEAM UPPER CAP CORROSION AREA REPAIRED AS PER RI NO.RI-53-10-15897 REV.A</P>)SDR UIEA2022092000999None · noneM/D STA 1197 TO 1198 RBL 116 FLOOR SUPPORT FOUND CRACKED(<P>FLOOR SUPPORT CRACK AREA REPAIRED AS PER RI NO: RI-53-40-15879 REV.A</P>)SDR UIEA2022092101004None · noneAFT CARGO BILGE SKIN FOUND CORROSION AT BS 1487 RBL 6 BILGE LONGERON MOUNT BOLT AREA(<P>CORROSION AREA REPAIRED AS PER RI NO: RI-53-61-15881 REV.B</P>)SDR UIEA2022092101006None · noneBULK CGO COMPT FLOOR INTERCOSTAL I/B AND O/B FLANGE FOUND CRACKED AT RBL 7.625 STA 2080(<P>FLOOR INTERCOSTAL I/B AND O/B FLANGE REPAIRED AS PER RI NO: RI-53-61-15877 REV.A</P>)SDR UIEA2022092101008None · noneFWD CGO COMPT STA 740 RBL 12" FRAME WEB UPPER AREA FOUND PUNCTURE(<P>FRAME WEB PUNCTURE AREA REPAIRED AS PER RI NO: RI-53-20-15878 REV.A</P>)SDR UIEA2022092101009None · noneFWD CGO COMPT STA 570-600 RBL 38-56 BALL MAT PANEL FOUND DAMAGED(<P>BALL MAT SKIN REPAIRED AS PER SRM 53-00-53-2R-2 REPAIR 2 FIG 201</P>)
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