JASC 5330
Service difficulty reports · 79,329
Reports filed under 5330 · Fuselage Main, Plate/Skin, 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 = '5330' 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 = '5330' 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 2025FA0000161Support Bracket · corrodedFUSELAGE FAIRING SUPPORT AND STRAP HAVE CORROSION PRESENT IN MULTIPLE LOCATIONS OF VARYING THICKNESSES.SDR SWIA2025030777185Skin · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE RA95454-601R-53-11-3962 MXCODEID106127-PR - TEMPORARY DISPOSITION FOR DENT DAMAGE ON FUSELAGE SKIN PANEL FWD OF BS 280 AND ABOVE STR 6L. SUBJECT CONDITION IS ACCEPTABLE FOR 500 FH FROM TIME OF INCORPORATION OF REO 601R-53SDR SWIA2025030777173Skin · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE RA73304-601R-53-11-3730 455SW MXCODEID59029-PR - DENT ON RT FUSELAGE NOSE SKIN AT FS21000 BETWEEN STR 12R AND 13R COMPLIED WITH TEMPORARY DISPOSTION PER REO 601R-53-11-3730 REV -- DATED 2021-10-03 PERMANENT REPAIR DUE WITSDR SWIA2025030775541Skin · dentedBIRD STRIKE ON FINAL APPROACH AT 400 AGL, STRUCK NOSE BELOW FO WINDSCREEN.. DENT FOUND UNDER FO WINDSHIELD RT FUSELAGE SKIN PANEL BTWN BS 185 - 193, BL 0 - RBL 6.10. REPIARED THE DENT BETWEEN BS 185 - 193, IAW SRM 51-42-06, & DWG 600-33010, REV AD, SHEET 1.SDR SWIA202509020004Skin · dentedPROTRUDING DENT ON SKIN OVER FRAME FS333.00 BETWEEN STGR21 & 22L. REMOVED AND INSTALLED NEW FABED BUTT STRAP AT FS333 BETWEEN STGR18L AND STGR21L REF-SRM 51-42-21-001-001 A01, SRM 51-42-06-001-001 A01, DWG SH670-32420 REV E. LEAK CHECK PASSED.COMPLIED WITH TSDR AALA202503191795Skin · gougedAIRCRAFT IN BASE MAINTENANCE: FORWARD CARGO DOOR CUTOUT EDGE SKIN HAS 2 EA GOUGES AT BS 501 BETWEEN STR 38R AND STR 39R. PERFORMED 2 EA BLEND-OUTS AT FORWARD CARGO DOOR CUT-OUT EDGE SKIN. PER B777-300 SRM 53-00-01-1A-1.SDR DALA2025031001809Skin · damagedSHIP 3326 FUSELAGE DAMAGE BETWEEN FRAME 26.1 AND 27 AND STRINGER 51L AND 54R. CORRECTIVE ACTION: REPAIRED PER ERA 624933-14. OK FOR SERVICE. (7119648)SDR VNAA202503070041Skin · corrodedCORROSION ON SKIN PANEL IN STA. FS= 295 TO FS= 310 BETWEEN STGR 24RH TO 25RH AT MAIN AVIONICS COMPARTMENT. CORROSION ON SKIN PANEL IN STA. FS= 295 TO FS= 310 BETWEEN STGR 24RH TO 25RH AT MAIN AVIONICS COMPARTMENT WAS REPAIRED PER REO 690-53-21-1884 REV - .SDR VNAA202503070039Skin · dentedDENT ON EXTERNAL SKIN BTW FS 437.00 TO FS 453.00 AND STGR 16RH TO 17RH AT FWD FUSELAGE. DENT ON EXTERNAL SKIN BTW FS 437.00 TO FS 453.00 AND STGR 16RH TO 17RH AT FWD FUSELAGE WAS EVALUATED WITHIN LIMITS PER CRJ-900 SRM 53-00-01-101-001-A01.SDR VNAA202503070013Skin · corrodedCORROSION ON SKIN PANEL BTW FS 280.00 TO FS 295.00 STGR 25RH TO STGR 24 RH. CORROSION ON SKIN PANEL BTW FS 280.00 TO FS 295.00 STGR 25RH TO STGR 24 RH WAS REPAIRED PER REO 690-53-21-1884 REV - -.SDR EE4Y2025030721920Skin · damagedDURING THE MAINTENANCE INSPECTION TWO LIGHTNING STRIKE WAS FOUND AT (THROUGH DAMAGES 1) FR 20+42MM, STR 27LH+26MM AND (THROUGH DAMAGES 2) AT FR 20+22MM, STR 27LH+70MM, THE DAMAGES WERE CORRECTED IN ACCORDANCE WITH THE REPAIR INSTRUCTIONS OUTLINED IN ETD2025-19SDR VNAA202503070005Skin · damagedLIGHTNING STRIKE DAMAGE TO LOWER BELLY PANEL SKIN BTWN FS250.00-FS265.00 & STR25R-STR26R). REPAIRED PER REO 690-53-11-1937 REV --PERMANENT REPAIR.SDR VNAA202503070004Skin · gougedFUSELAGE SKIN MULTIPLE BLENDED GOUGE BTWN FS1015.00 - FS1051.30. FUSELAGE SKIN MULTIPLE BLENDED GOUGE BTWN FS1015.00 - FS1051.30 WERE REPAIRED PER REO 690-53-61-1505 REV --PERMANENT DISPOSITION.SDR VNAA202503070002Skin · crackedPERM REPAIR BEFORE 19,970.55 FH - SKIN LWR BELLY PANEL WITHIN 4,663.83 FH (BEFORE 23,204.37 FH) REPLACE THE DISCREPANT ITEM IN ACCORDANCE WITH APPROVED PROCEDURES. SKIN LWR BELLY PANEL WAS REPAIRED PER REO 670-53-11-2098 REV. - -SDR VNA2025F00006Skin · crackedPERM REPAIR BEFORE 19,970.55 FH - SKIN LWR BELLY PANEL WITHIN 4,663.83 FH (BEFORE 23,204.37 FH) REPLACE THE DISCREPANT ITEM IN ACCORDANCE WITH APPROVED PROCEDURES. SKIN LWR BELLY PANEL WAS REPAIRED PER REO 670-53-11-2098 REV. -.SDR EE4Y2025030721917Skin Panel · misrepairedDURING THE MAINTENANCE INSPECTION, IT WAS FOUND AT THE FORWARD FUSELAGE SKIN, FROM FR18+155MM TO FR19+60MM, BETWEEN STR-26LH AND STR-27LH+170MM, AN EXISTING DOUBLER THAT DOES NOT COMPLY WITH ETD2017-190-024715 DATED MARCH 20, 2017, GUIDELINES. THE ISSUE WAS COSDR EE4Y2025030721912Skin Panel · corrodedDURING THE MAINTENANCE INSPECTION, CORROSION WAS FOUND ON THE INNER SURFACE OF THE FUSELAGE SKIN AT FR82, BETWEEN STRG-27R AND STRG-28R. THE DAMAGE WAS CORRECTED IN ACCORDANCE WITH THE REPAIR INSTRUCTIONS OUTLINED IN ETD2025-190-900569 AND THE COOPESA ENGINEERSDR FDEA202503070335Skin · crackedFUSELAGE- LOWER FUSELAGE #1 AIRCON RAM AIR EXHAUST AFT UPPER CORNER AT LEFT HAND SIDE APPROXIMATE STATION 586 FOUND CRACKED. CRACKED SKIN AT LOWER FUSELAGE #1 AIRCON RAM AIR EXHAUST AFT UPPER CORNER AT LEFT HAND SIDE APPROXIMATE STATION 586 REPAIRED AS PERSDR VNAA202504130011Skin Panel · dentedDENT ON FWD FUSELAGE SKIN ON STGR 22 LH BTW FS 349.00 TO FS 364.00. DENT ON FWD FUSELAGE SKIN ON STGR 22 LH BTW FS 349.00 TO FS 364.00. WAS REPAIRED PER 690-53-21-1907 REV. --. UNTIL A TRANSPORT CANADA ACCEPTED NDTM TECHNIQUE HAS BEEN MADE AVALIABLE, THE AIRSDR ASAA2025030656676Skin · corrodedAT DRAIN MAST ON THE RIGHT-HAND SIDE HAS CORROSION SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY "A" REPAIR ON FUSELAGE SKIN P/N 147A3400-4 BY AFT DRAIN MAST ON THE RIGHT-HAND SIDE AT STA 986.5 TO STA 1006 AND STR 24L TO 25L. IAW 800-53EA-28423 REV00 SRXR430SDR ASAA2025030656675Skin · corrodedCORROSION ON FASTENERS FWD OF OUTFLOW VALVE BETWEEN STA 986 AND STA 967 SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY "A" REPAIR ON FUSELAGE SKIN P/N 147A3400-4 BETWEEN STA 967 AND STA 986 AT AND STR 25R TO 27R. IAW EA800-53EA-28423 REV00 SRXR430X.SDR CALA2025031302754Skin · gougedFWD CARGO COMP FLOOR STRUCTURE GOUGE IN SKIN APROX 6 INCHES FWD OF FWD OF FR 26 BETWEEN STR 41L AND STR 42L. GENERATED BY V89904 5 ON HAECO LCQ NR 9290788 / 38788. ESFR COMPLETEDSDR AALA202503078982Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LOWER FUSELAGE SKIN AROUND POTABLE WATER TANK DRAIN AT BS 957, FROM S26L TO S27L. REPAIRED SKIN PER EA 362240.SDR ASAA2025030656412Skin · corrodedCORROSION AT HOT DRAIN MAST BETWEEN STA 986.5 AND STA 1016 JUST BELOW STGR 23L IN 3 PLACES SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY A MINOR REPAIR ON FUSELAGE SKIN P/N 147A3400-4 AT STGR 23L BETWEEN STA 986.5 AND STA 1016 AT HOT DRAIN MAST IAW EA 800-53SDR ASAA2025030656410Skin Panel · corrodedCORROSION ON FUSELAGE SKIN BETWEEN STA 500C TO STA 500E FROM STGR 27L TO STGR 28L SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY A MINOR REPAIR ON FUSELAGE SKIN P/N 143A3232-28 BETWEEN STA 500C TO STA 500E FROM STGR 27L TO STGR 28L IAW EA#800-53EA-28278 REV 0SDR SWIA202503200005Doubler · corrodedPOST REMOVAL-WASTE BOX DOUBLER CORRODED AT THE 2 FORWARD CORNER CUTOUTS (C-CHECK RO 03/19/2024)REMOVED AND REPLACED WASTE BOX DOUBLERREF EMB SRM 51-40-08. SEE CONTINUATION CARD FOR WORK ACCOMPLISHED O.E.M. PART INSTALLED NO CHANGE TO WEIGHT AND BALANCESDR CALA2025031302752Skin · gougedFWD CARGO COMP FLOOR STRUCTURE GOUGE IN SKIN APROX 6 INCHES FWD OF FR 26 BETWEEN STR 43L AND STR 44L.SDR DALA2025031001841Skin · gouged(LOG 0842164) WHILE ON THE LINE IN SFO, MTC DISCOVERED GOUGE DAMAGE DIRECTLY AFT OF THE FWD CARGO DOOR. REPAIRED DAMAGE PER ERA 614995-14.SDR DALA2025031001840Skin · dented(LOG 0842820) DURING HEAVY MAINTENANCE VISIT AT MEXICANA MRO FACILITIES (MEX), A DENT + GOUGE DAMAGE HAS BEEN FOUND ON THE FUSELAGE SKIN, BETWEEN STA 360 / STA 380 AND STRINGERS S-17L / S-18L. REPAIRED DAMAGE PER ERA 597051-14.SDR DALA2025031001834Doubler · gouged(LOG 0842515) FWD CARGO DOOR CUTOUT, AFT EDGE DOUBLER IS GOUGED. REMOVED AND REPLACED DAMAGED DOUBLER IAW B737-900 SRM 53-00-01-2R-25 AND PRI ER/A 614995-145 JOB COMPLETE RECEIVED FINAL ERA 614995-14 REV A ALL STEPS MATCH PRI 614995 REV 0 JOB COMPLETE.SDR CALA2025031002650Skin · corrodedLEFT WING UNDER WING TO BODY FAIRING FUS SPOT EXFOLIATED CORR. BELOW ATTACHED ANGLE S-22L STA 540 REF AAR N/R 9939235SDR AALA202503062494Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FUSELAGE SKIN AT EXTERNAL POWER DOOR LOWER CUTOUT FROM BS 224.8 TO BS 235.8, FROM S22R TO S23R. ACCOMPLISHED REPAIR PER SRM 53-10-15-2R-4.SDR SWI2025F01615Skin · damagedDAMAGE FOUND ON FUSELAGE AFT OF GROUND AIR CONNECTION DOOR DUE TO CONNECTION COVER SMACKING SIDE OF FUSELAGE DURING FLIGHT. COMPLIED WITH TEMPORARY REPAIR REO 690-53-61-1044 REV-A DATED 2021-11-07. PERMANENT REPAIR DUE WITHIN 4750 FLT HRS BY 35218.3 TAT, (C-SDR AALA202506193303Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON FASTENER HOLE (AFT-LOWER POSITION) LOCATED ON FR35 AT LEVEL OF STR30L, LOWER FUSELAGE. CRACK DEPTH = 0.118 INCHES, CRACK POSITION: 4 OCLOCK LOOKING FROM OUTSIDE ON LOWER FUSELAGE. MAINTENANCE TIME LIMITEDSDR AALA202506132780Skin Panel · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON FASTENER HOLE (AFT/LOWER POSITION) LOCATED O N FR35 AT LEVEL OF STR30R, LOWER FUSELAGE HOLE IDENTIFIED AS HOLE #2 CRACK DIMENSION IS D=0.115 IN. MAINTENANCE PERFORMED TIME LIMITED REPAIR INSTRUCTIONS (INSDR IPXA2025042860851Skin · crackedCRACK FOUND IN HOLE A ON LH FR47 HORIZONTAL JUNCTION. AREA. INSTALLED NEW FASTENER P/N: EN6114V10-42 BATCH#:0004380268 AND NUT P/N: ASNA2531-10 BATCH#: 0004377544 AND SEALANT P/N:04-001-0169 BACTH: 0004310740 IAW A300-600 SRM 51-40-21 AND E.A.#: 300-5710-27-ASDR SWAA2025041101710Skin · debondedPANEL 194CR OUTER SKIN IS DISBONDED. (MARKED)<[01] 194CR PANEL OUTER SKIN DAMAGE HAS BEEN REPAIRED PER [SRM 51-70-05-2R-2-A00733 (REPAIR 2 - REPAIR OF DAMAGE THAT IS MORE THAN 0.50 INCH (12.70 MM) IN DIAMETER TO ONE SKIN AND THE HONEYCOMB CORE - AIRFRAME - PERSDR IPXA2025041060873Skin · crackedCRACK FOUND IN HOLE E ON LH FR47 HORIZONTAL JUNCTION. AREA MARKED IN BLACK. INSTALLED NEW FASTENER P/N: EN6114T9-30 BATCH#:0003918575 AND NUT P/N: ASNA2531-9 BATCH#: 0004014715 AND SEALANT P/N:04-001-0169 BACTH: 0004310740 IAW A300-600 SRM 51-23-10 AND E.A.#SDR R61A2025032300156Doubler · corrodedDURING HEAVY CHECK MAINTENANCE FOUND LEVEL 2 CORROSION ON ANTENNA DOUBLER FWD FUSELAGE FWD OF FWD CARGO. REPLACED DOUBLER IAW SRM 51-41-02SDR ASAA2025030456607Skin · puncturedFUSELAGE SKIN STA 950 STR 23R-24R HAS PUNCTURE. GROUNDED - YES. CUT OUT PUNCTURE AND REMOVED DAMAGED SHEAR TIE AT STA 947.5 STR 23R-24R IAW B737-800 SRM 51-10-02, SRM 51-40-02. REPAIRED SKIN, FABRICATED NEW SHEAR TIE AND INSTALLED IAW ASA EA 800-53EA-28409 ANDSDR SWAA2025031202214Skin · delaminatedFUSELAGE TAILCONE HAS A DELAMINATION ON INNER SURFACE AT BS 1156+32'; AT 11 O'CLOCK POSITION. <[01] 04 - REPAIRED PER [SRM 51-70-05-2R-1-A00732 (REPAIR 1 - REPAIR OF DAMAGE TO ONE SKIN OF A HONEYCOMB PANEL - AIRFRAME - PERMANENT)]; [02] TASK CARD COMPLETED.SDR CALA2025030402577Skin · damagedEVIDENCE #1 OF LIGHTNING STRIKE FOUND AT STA 424 BTW ST 3 AND 4. (CORRECTION OF PREVIOUS UPDATE) EVIDENCE #1 OF LIGHTNING STRIKE FOUND AT STA 420 BTW R/H ST 3 AND 4. REMOVED DAMAGED RIVET AS PER SRM 53-00-01-2R-41 REPAIR 41. UP TO PARAGRAPH 4A. PERFORMED SDR DALA2025030401663Skin · dentedSHIP 3312 FUSELAGE EXTERNAL SKIN FOUND DENT AT FR25A, BETWEEN STRINGER S-41R AND S-42R. CORRECTIVE ACTION: COMPLIED WITH ERA 624355-14 REV ORIGINAL. (0839642)SDR SWIA2025090900303Skin · dentedADM# N896SK-5148 DENT JUST AFT OF NLG FUSELAGE CUTOUT, SLIGHTLY TO THE RIGHT OF THE CENTERLINE OF THE AIRPLANE. 2 INCH X .75 INCH X.090 DEPTH. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PRACTISDR SWIA202507170303Skin · dentedDENT DAMAGE ON LH HYDRAULIC BAY SKIN PANEL BETWEEN FS169.00 - FS173.00 AND STR21L - STR23L. THE SUBJECT CONDITION IS STRUCTURALLY ACCEPTABLE FOR 1250 FLIGHT HOURS FROM TIME OF INCORPORATION OF THIS REO AT REV €Œ--€?., PART NUMBER: - , SERIAL NUMBER: 15069,SDR LR7A2025030303736Skin · crackedDURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5304, FOUND RH WHEEL WELL SKIN CRACKED AT UPPER MIXING CHAMBER MOUNTING SCREW HOLE, FS494, RBL61, WL260. / REPAIRED IAW LAC MEA 382-53-24-210. NR# 0527.SDR LR7A2025030303720Skin · damagedDURING SCHEDULED C-14 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RH AFT FUSELAGE SKIN DAMAGED AT FS737-FS803, WL144-WL174, RBL61-RBL80. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0288.SDR LR7A2025030303715Skin · chippedDURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5321, FOUND AFT FUSELAGE SKIN CHIPPED AT FS908, LBL61, WL208. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 0136.SDR IPXA2025032621567Access Panel · corrodedCORROSION - BRACE, R/H AIR CONDITION ACCESS PNL NO.192ER STA 1059.9 RBL 57.7.FOUND CHAFE DAMAGE THRU CHAFE PLATE 100% MATERIAL LOSS, REMOVED CHAFE PLATE AS REQUIRED IAW SRM 53-19-12 PARA 5.INSPECTED AND VERIFIED RECEIVING MATERIAL FOR LEFT LOWER HORIZ. STAB.INSDR IPXA2025031726547Skin · gougedMAJOR REPAIR, ACCESS DOOR 119BL REAR CUT OUT FUSELAGE, OUTER SKIN HAS (2EA) GOUGES. DOT 72-024 ACCOMPLISHED PER UPS EO: EO-93125-REQI AND VT MAE EA 757-5330-27-A3841
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