JASC 5330
Service difficulty reports · 79,293
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 AALA202602063870Skin · gougedAIRCRAFT IN BASE MAINTENANCE: GOUGE ON FUSELAGE SKIN BETWEEN BS 276.5 AND BS 303 AND STR 25R AND STR 26R. ACCOMPLISHED A PERMANENT REPAIR ON FUSELAGE SKIN. PER B787-8 SRM B787-A-53-10-01-09A-664A-A FIG 5SHT 1.SDR JJBA20260127078Skin · damagedTOP FUSELAGE SKIN DENTED AT PREVIOUS RIVET PLUG BTW FR 22-22A, STR 2 - 1R. TOP FUSE SKIN WAS REPAIRED.SDR SWAA2026012262980Skin · crackedEXTERNAL POWER DOOR LOWER CUTOUT CRACKED AT FASTENER. PERFORMED HFEC AROUND CRACK CUTOUT PER PART 6 51-00-00 P23. CUT OUT DAMAGED AREA IAW SRM 53-10-15-2R, FABRICATED AND INSTALLED REPAIR IAW SRM 53-10-15-2R-4, REPAIR 4. ; INSTALLED REPAIR IAW SRM 53-10-1SDR DALA2026012200479Skin · corrodedSKIN CORRODED, LEFT AFT FUSELAGE AT LAV EXHAUST VENT. WHILE IN ATL FOR C-CHECK, MAINTENANCE REMOVED CORROSION ON AFT LAVATORY EXHAUST VENT CUTOUT IAW SRM 53-70-01-2R, REPAIR 3, AND ER/A 631684-14. (LP 1411210)SDR AALA202604068191Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION INTERNAL SKIN LOCATED BTW FR59 AND FR60 AT LEVEL STGR 43L IN BULK CARGO COMPARTMENT. THE MEASURE ARE: L=0.400 INCHES W=0.175 INCH D=0.002 INCHES.SDR DALA2026012100440Skin · crackedHFEC INSPECTION CARRIED OUT ON THE LT FUSELAGE SKIN ,SECTION 48, FOUND TWO CRACKS IN STRINGER 13, BS 1654 - 1678, THE LENGTH OF CRACK IS 0.19 IN AND 0.15 INCH, THE FUSELAGE SKIN CRACK AREA WAS REPAIRED AS PER B767-400 SRM 53-80-01 (1408646)SDR SWIA2026011875735Skin · corrodedDEEP CORROSION PIT FOUND BEHIND RH FUSELAGE HINGE FITTING OF REAR NOSE LANDING GEAR DOOR. WET INSTALLED ALL REPAIR PARTS AT STR 26R & NLG BAY WEB FWD OF FS.235 & RBL 6 WITH NEW FASTENERS PER REO 601R-53-11-4054 REV --. LEAK CHECK GOOD. COMPLIED WITH TASK CARDSDR SWAA2026021862663Tie Clip · crackedCRACKED TIE CLIP, BS 277, S10R IN THE PAX CABIN. REPLACED THE TIE CLIP IAW SRM 51-10-02-0G-0, ITEM 9, DWG 141A1110, SHEET 18, REV -, & DWG 141A8380, SHEET 33, REV -.SDR ASAA2026011863956Skin · corrodedEXTERIOR FUSELAGE SKIN SHOWED SIGNS OF CORROSION AROUND TOILET VENT ABOVE LAV SERVICING PANEL. GROUNDED - YES. ACCOMPLISHED REPAIR 3, SECTION 47 FUSELAGE SKIN REPAIR AT BS 917, BTWN S21-22L. INSTALLED A DOUBLER, TRIPLER, FILLER & RESTORED PROTECTIVE FINISHESSDR YENA2026012100050Skin · corrodedDURING HEAVY MAINTENANCE: FUSELAGE / REAR FUSELAGE / FR 65-66 & STR31R / INNER SKIN / CORROSION DAMAGE - TIME LIMITED REPAIR; REFERENCES: /1/ AEROMAN EA 53-0077-25 REV. 1 (COVER + PARTS 1-3) /2/ AIRBUS RDAF 81680476/005/2025 ISSUE B /3/ AIRBUS TD/81680476/037/SDR YENA2026012100048Skin · corrodedDURING HEAVY MAINTENANCE: FUSELAGE / REAR FUSELAGE / LOWER SKIN PANEL / FR64-FR65 BETWEEN STGR43L-STGR44 / CORROSION AND ELONGATED HOLE - TIME LIMITED REPAIR; REFERENCES: /1/ AEM EA 53-0094-25 (COVER + PARTS 1-4) /2/ AIRBUS DOSSIER 81702291 /3/ AIRBUS RDAF 817SDR YENA2026012100046Skin · damagedDURING HEAVY MAINTENANCE: FUSELAGE / REAR FUSELAGE / EXTERNAL SKIN / BTW FR 82-83 AND STGR 3-5LH / DENT DAMAGE – PERMANENT REPAIR; REFERENCES: /1/ AEROMAN EA 53-0095-25 (COVER + PART 1-2) /2/ RDAF 81703158/002/2025#A /3/ AIRBUS DOSSIER 81695068 /4/ A321NEO SRSDR DALA2026012000421Skin · dentedFUSELAGE DENT BETWEEN BS 620 - 640, STRINGERS 15L-17L. REMOVED SKIN SECTION WHERE DAMAGE WAS LOCATED IAW SRM 53-30 -01-2R-2. PERFORMED HFEC OF CUTOUT & BHEC OF OPEN FASTENER HOLES, NO DEFECTS NOTED IAW SRM 53-30-01-2R-2. PERFORMED DVI OF STRUCTURE AROUND CUTSDR 2026FA0000036Skin · abnormalDUE TO EXISTING EXTERNAL REPAIR IN FUSELAGE SKIN, SHOP CANNOT INSTALL SHEAR TIE, P/N 95292-257 IN ACCORDANCE WITH DWG REQUIREMENTS.SDR 2026FA0000033Skin · mechanic errorDURING INSTALLATION OF SHEAR TIE PER DWG 371-53-00-C4157 VIEWS 5C8-1 AND 1B5, THE SHOP MISTAKENLY DAMAGED THE COUNTERSINK OF ONE FASTENER HOLE COMMON TO THE FUSELAGE SKIN AT BS 1241, BETWEEN STR 27R AND 28R.SDR 2026FA0000031Doubler · corrodedDURING INSTALLATION OF DOUBLER PER DWG 371-53-11-C3164, CORROSION WAS DETECTED ON THE OUTER FLANGE OF FRAME BS 390 BETWEEN STR 19R AND 20R.SDR SWIA2026011775651Skin · corrodedUPON REMOVAL OF AFT DRAIN MAST, FOUND CORROSION ON EXTERNAL SKIN BETWEEN BS 1031 - BS 1047 AND STR 27 - STR 26R. COMPLIED WITH REO 670-53-61-2664 REV -.SDR SWIA2026021375239Skin · crackedHFEC CONFIRMED CRACK RT LOWER SKIN JUST FORWARD OF RT LANDING GEAR WHEEL WELL CUT OUT AT RIB 3. PERFORMED CRACK REPAIR AT RIB 3 JUST FORWARD OF LANDING GEAR CUTOUT ON RIGHT WING LOWER SKIN IAW ETD2026-170-001158. REPAIR PARTS WEIGHED LESS THAN 2.5 LBS, NO WEISDR DALA2026012200499Skin · gougedFUSELAGE SKIN STA 148.55 LONGERON 19L TO 20L GOUGE DAMAGE. C/W ERA 626451-14 (1406347)SDR SWIA2026011675709Skin · corrodedFUSELAGE EXTERNAL SKIN AT AFT LAV SERVICING POINT IS CORRODED BETWEEN FS559+80 AND FS559+112 BETWEEN STGR20R AND STGR24R. REPAIRED EXTERNAL SKIN AT AFT LAV SERVICING POINT BETWEEN FS559+80 AND FS559+112 BETWEEN STGR20R AND STGR24R IAW MHIRJ REO 601R-53-51-729SDR SWIA2026041775706Doubler · corrodedFUSELAGE EXTERNAL SKIN DOUBLER AT THE LAV SERVICING POINT IS CORRODED. REPAIRED EXTERNAL SKIN DOUBLER AT LAV SERVICING POINT IAW REO 601R-53-51-729 REV--. COMPLETED TASK CARD 51-900-1003-SKY.SDR DALA2026012200492Skin · crackedCRACK INTERNAL SKIN ON TOP FWD EDGE AT FWD ENTRY DOOR. INTERNAL SKIN ON TOP FWD EDGE AT FWD ENTRY DOOR WAS REPAIRED PER B717-200 S.R.M. 52-10-02 (1404734)SDR DALA2026011600385Skin · not reportedERA 536961-14, MONITOR INSPECTION LOG REPAIR TO C1 DOOR CUTOUT, LOWER FWD CORNER. REF ERA 536961-14AD. (1404006)SDR SWIA2026011575598Skin · chafedRIGHT WING HAS CHAFING ON LOWER WING PLANK AT RBL 45 FROM CONTACT WITH BELLY FAIRING 193AB. REPAIRED THE RT WING LOWER WING PLANK AT RBL 45 IAW REO 601R-57-21-880, REV D.SDR AALA202603182672Skin Panel · corrodedENGINEERING REVIEWED THIS EVENT AND DETERMINED THE CORRECT LEVEL WAS LEVEL 1 NOT LEVEL 2. SECTION 7 CORROSION LEVEL FIELD WAS CORRECTED ACCORDINGLY. AIRCRAFT IN BASE MAINTENANCE: CORROSION AROUND RIVET INTERNAL SKIN LOC. BTW FR33 TO FR 34 AND BTW ST R 41R TO SDR ASAA2026011564730Skin · corrodedSTA 520 TO STA 540 STR-27L TO STR-27R SKIN CORRODED. GROUNDED - YES. REMOVED CORROSION FOUN DTO HAVE 100% MATERIAL LOSS OUT OF LIMITS IAW B737-700 SRM 53-00-01-1A-5 REAPIRED IAW ASA EA# 700-53EA-29869. W= 6.50 O= .080 R= 0.00 L= 7.50 D= .080SDR HNAA2026021600131Skin · gougedFUSLAGE SKIN IS GOUGED INSIDE PANEL 414DB ON L/H PYLON BETWEEN FR 67-68 AND STGR 7L-8L. REPAIRED FUSELAGE SKIN INSIDE PANEL 414DB ON L/H PYLON BETWEEN FR 67-68 AND STGR 7L-8L IAW EMB145 ETD2026-145-001016 REV "B" AND EO1-53-26-0050SDR AALA202601212672Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION AROUND RIVET INTERNAL SKIN BTW FR33 - FR 34 AND STR 41R - STR41L FWD CARGO COMPARTMENT. MAINTENANCE REWORKED FASTNER HOLSES IAW EA 370487.SDR DALA2026011600368Skin · corroded(LOG 1403707) WHILE IN ATL FOR C-CHECK, MAINTENANCE REMOVED CORROSION ON AFT LAVATORY EXHAUST VENT CUTOUT PER SRM 53-70-01-2R REPAIR 3. MAINTENANCE REPAIRED DAMAGE PER SRM 53-70-01-2R REPAIR 3 AND ERA 631684-14.SDR AALA202601152236Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FUSELAGE SKIN, AT ELECTRICAL GROUND POWER RECEPTACLE DOOR LOWER CUTOUT SURROUND DOUBLER BETWEEN BS 224.8 AND BS 235.8, BETWEEN S21R AND S22R. REPAIRED SKIN PER SRM 53-10-15-2R-4.SDR AALA202601158362Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FUSELAGE SKIN, AT ELECTRICAL GROUND POWER RECEPTACLE DOOR LOWER CUTOUT SURROUND DOUBLER AT BS 224, S20R. REPAIRED SKIN PER SRM 53-10-15-2R-4.SDR REXA2026011500003Skin · crackedA CRACK WAS FOUND ON LEFT HYDRAULIC BAY SKIN AT TRU DOOR CORNER IAW EA CRJ953-19108. REPLACED SKIN PER APPLICABLE SRM AND DRAWINGS. SKIN WAS DEEMED FCBS AND WAS DOCUMENTED AS A MAJOR REPAIR.SDR JR2R20260115233Skin · chafedAFT LOWER FUSELAGE AT MID AVIONICS BAY DOOR SURROUND STRUCTURE UPPER FWD CORNER SKIN DOUBLER IS CHAFED. REPAIRED PER ETD.SDR JR2R20260115232Skin · chafedAFT LOWER FUSELAGE AT MID AVIONICS BAY DOOR SURROUND STRUCTURE UPPER AFT CORNER SKIN DOUBLER IS CHAFED. REPAIRED PER ETD.SDR JR2R20260115029Skin · corrodedAFT CARGO SCUFF PLATE AREA EXTERNAL SKIN IS CORRODED IN MULTIPLE AREAS. REPAIRED PER ETD.SDR JR2R20260115021Skin · corrodedFWD CARGO SCUFF PLATE AREA EXTERNAL SKIN IS CORRODED IN MULTIPLE AREAS. REPAIRED PER ETD.SDR JR2R20260115753Skin · dentedDENT AT LOWER AFT FUSELAGE SKIN FR 89 - 90 STR 26L-27L. REPAIRED PER ETD.SDR EE4Y2026150123769Skin · corrodedCORROSION DAMAGE AFFECTING THE CENTER FUSELAGE II SKIN INNER FACE,LOCATED IN THE S29L LOCATION, AT FR73+235MM. VERIFIED BLEND OUT WITH CLAD LAYERPENETRATED AND FOUND OUT OF LIMITS IAW PART II SRM 53-22-01, AD51, PARAG. 5A (2),TABLE 102, FIG. 104 SHEET 2. THE CSDR SWIA2026011475657Skin · corrodedUPON REMOVAL OF RAD ALT ANTENNA (E19) , FOUND CORROSION ON INTERNAL SKIN BETWEEN FS 1031 - FS 1047. CUT AWAY IDENTIFIED AREA OF FUSELAGE SKIN, FABRICATED NEW DOUBLER AND INSTALLED AT FS 1031-FS1047 UNDER RAD ALT ANTENNA BETWEEN STGR27 AND 26L IAW REO 670-53-6SDR SWAA2026012061084Skin Panel · debondedSKIN PANEL 193CL LOWER FWD CORNER OUTER SKIN HAS A DEBONDED DENT. SKIN PANEL 193CL LOWER FWD CORNER OUTER SKIN WITH A DISBONDED DENT WAS REPAIRED IAW SRM 51-70-05-2R-2.SDR CALA2026011913049Skin · corrodedFUSELAGE SKIN INTERNAL BETWEEN BS 879 - 900 BLIGE CENTER LINE HAS CORROSION (EXFOLIATED). REPAIR ACCOMPLISHED IAW ECRA 5330-07683. MAJOR REPAIR. PERFORMED A REPAIR IAW VT MAE 757-5330-13-A4231, ATTACHED TO EC/RA AS FIGURE 1 THROUGH 35 WITH NO DEVIATIONS IAW SDR DALA2026011600377Skin · crackedREFERENCE ER/A 617297-14 - FUSELAGE / SKIN / STA 1037, L-14L / CRACKS. CORRECTIVE ACTION: REPAIRED PER ER/A 14-617297. (1401870)SDR FDEA202601140039Skin Panel · damagedLIGHTNING STRIKE ON UPPER SKIN BTWN B STA 903.5 - 933 AND S-1R AND S-2R. THE LIGHTNING STRIKE AT UPPER SKIN BETWEEN STA 903.5 - 933 AND STG-1R AND STG-2R. WAS REPAIRED IAW SRM 53-00-01-2R REPAIR 1 REV 93 AUG 15/2025SDR DALA2026011400334Skin · damagedFUSELAGE SKIN AND STRINGER 3R AT FR 61, FR 62 DAMAGED HOLES AND TOOLING DAMAGE. REPAIRED PER ERA 627795-14 REV A. (1400862)SDR DALA2026062303733Skin · corrodedERA 620866 REVISED TO REV A. SECTION I ISSUED FOR CORROSION TO AFT FUSELAGE SKIN SURROUND WASTE SERVICE CUTOUT. FOLLOW ON ACTION REQUIRED. ACCOMPLISH SECTION IV WITHIN 2 FC OF LOG PAGE CREATION. SECTION II REQUIRED EVERY 1000 FH THEREAFTER UNTIL SECTION III. SSDR SWIA2026030975461Doubler · corrodedANTENNA DOUBLER IS CORRODED FS310.00 - 319.00 STGR27. (C-CHECK RO 03/07/2026)INSTALLED NEW TCAS ANTENNA CHANNEL P/N SH670-32364-7, AT FS310-FS319, STGR 27, REF. CRJ700 SRM 51-42-20-001-001-A01, CRJ700 SRM 51-42-06-001-001-A01 AND DWG SH670-30023 REV G, COMPLSDR DALA2026011600374Skin · crackedCRACK ON SKIN FUSELAGE BTW L15R, BS 037 AT AFT FUSELAGE AREA. DAMAGED FUSELAGE AREA WAS REPAIRED PER PRI 631355-14 REV. (1399353)SDR JJBA20260114033Mount · corrodedRADIO ALTIMETER #2 FORWARD MOUNT HAS CORROSION. REMOVED AND REPLACED RAT #2 EXTERNAL ANTENNA MOUNT AND NEW RAT #2 INTERNAL ANTENNA MOUNT.SDR DALA2026011400335Skin · damagedFUSELAGE SKIN AND STRINGER 3R AT FR 61, FR 62 DAMAGED HOLES AND TOOLING DAMAGE. CORRECTED PER ERA 627795-14 REV A. (1400731)SDR AALA202601141129Skin · dentedAIRCRAFT IN BASE MAINTENANCE, DENT TO FUSELAGE SKIN AT BS 215, S17L. REPAIRED SKIN IAW SRM 53-10-01-2R-8.
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