JASC 5330

Service difficulty reports · 79,312

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.

SDR EE4Y2025100623289Skin · damagedDURING THE STRUCTURAL INSPECTION, IT WAS FOUND ON FORWARD FUSELAGE, AT FR18+18MM AND STGR-26R+85MM, EXTERNAL SKIN WITH A LIGHTNING STRIKE DAMAGE. EVALUATED THOUGH DAMAGE AND FOUND OUT OF LIMITS IAW ERJ190, PART II SRM 53-10-01, AD53, PARAGRAPH 4.B.(3): THE DISOct 6, 2025 · N688DR · Emb ERJ190200LRSDR EE4Y2025100623288Skin · damagedDURING THE MAINTENANCE ACTIVITIES AN EXISTING BLEND OUT WAS FOUND, IT IS LOCATED ON REAR FUSELAGE AT FR94+240MM, BTWN STRG 23R-25R. EVALUATED BLEND OUT WITH CLAD LAYER PENETRATED AND FOUND OUT LIMITS PER ERJ190 PART II SRM 53-30-01, AD 51, FIGURE 104, SHEET 4 Oct 6, 2025 · Emb ERJ190200LRSDR EE4Y2025100623287Skin · scratchedDURING THE STRUCTURAL INSPECTION IT WAS FOUND ON FORWARD FUSELAGE, RH-LATERAL SEAT TRACK FROM FR19 TO FR20 OTBD CROWN AREA WITH SCRATCH. EVALUATED BLEND OUT AREAS AND FOUND OUT OF LIMITS PER ERJ190, PART II SRM 53-10-10, AD51, PARAGRAPH 4.B. (NO DAMAGES AREA AOct 6, 2025 · N688DR · Emb ERJ190200LRSDR IPXA2025111395107Skin · corrodedSECTION 48 CORRODED FUSELAGE SKIN BET. STA.1885.20 TO 1918.90 LH SIDE JUST ABOVE THE APU LH DOOR FWD HINGE AS MARKED (059-07). ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-95725-REQ1 AND VT-SAA EA 757-5330-01-B0581 REV IR. REVIEWEDOct 5, 2025 · N456UP · Boeing 75724APFSDR CALA2025101309986Skin · damagedFUSELAGE SKIN AT BS 177 - 196.50, STR 17R -24R DAMAGED. INTERIM REPAIR PERFORMED AT FUSELAGE SKIN STA 177 - 196.50, STR 17R - 24R IAW ECRA 5310-08695.Oct 5, 2025 · N33284 · Boeing 737824SDR ABXA20251005256Skin · damaged"DURING AIRCRAFT N764CK C4-CHECK IN OSCODA MICHIGAN (OSC), KALITTA MAINTENANCE DISCOVERED FUSELAGE SKIN CORROSION UNDER STRINGER S-38L AT STA 1395 WHILE PERFORMING A STRINGER SPLICE. THE CORROSION WAS BLENDED IAW B767-300 SRM AND FOUND TO BE OUT OF LIMITS AND Oct 5, 2025 · N764CK · Boeing 7673P6SDR ABXA20251005251Skin · corrodedWHILE 764CK WAS UNDERGOING C 4 -CHECK IN OSC, CORROSION WAS FOUND ON THE INNER SURFACE OF THE INNER SKIN AT STA 1177 ALONG THE S-36L LAP JOINT.  SEE FIGURE 1.  THE CORROSION WAS REMOVED BY BLENDING AND THE BLEND WAS BEYOND THE ALLOWABLE LIMIT GIVEN IN B767 SRMOct 5, 2025 · N764CK · Boeing 7673P6SDR IXXA20251005006Skin · dentedDENT IN FUSELAGE SKIN BETWEEN 1562 AND 1582,STR 15L - 16L.Oct 5, 2025 · N395CM · Boeing 767323SDR IXXA20251005005Skin · dentedRIGHT FUSELAGE SKIN DENTED AT STA 1582-1605 STR 16R.Oct 5, 2025 · N395CM · Boeing 767323SDR VNAA202601170001Skin · dentedSEVERAL DENTS ON EXTERNAL FUSELAGE SKIN BTW FS 1015.00 TO FS 1031.00 BTW STGR 20 LH TO STGR 23 LH. SEVERAL DENTS ON EXTERNAL FUSELAGE SKIN BTW FS 1015.00 TO FS 1031.00 BTW STGR 20 LH TO STGR 23 LH WERE REPAIRED PER REO 670-51-00-085 REV - A AND REO 690-53-61Oct 4, 2025 · N645NN · Cndair CL6002D24SDR CALA2025103010756Skin · damagedAFTER FURTHER EVALUATION, LIGHTNING STRIKE FOUND TO BE OUT LIMI TS REQUIRE REPAIR ON FUSELAGE SKIN BTW STA 380 TO STA 400 AND S- -5R TO S-6R. PERFORMED REPAIR ON FUSELAGE SKIN BTW STA 380 TO STA 400 AND S- -5R TO S-6R IAW SRM 53-00-01-2R-3, THIS REPAIR IS A Oct 4, 2025 · N61898 · Boeing 737924ERSDR YENA2025100301008Skin · damagedDURING HEAVY MAINTENANCE: FUSELAGE / AFT FUSELAGE / WASTE PANEL SURROUND SKIN DOUBLER AT FR75-76 AND STR31LH-36LH / CORROSION - TEMPORARY REPAIR; REFERENCES: /1/ AIRBUS REO-500-53-61-2180 REV -- /2/ AIRBUS CRC 00195904 /3/ AVIANOR REPORT JB-3132-C01-3035 REV 1Oct 4, 2025 · N3132J · Airbus BD5001A11SDR CALA2025100609665Skin · corrodedFOUND CORROSION ON LEFT OF CENTER VHF ANTENNA AND CRACKS UNDER VHF ANTENNA ON FUSELAGE SKIN.Oct 4, 2025 · N75853 · Boeing 757324SDR CALA2025100609657Skin · nickedRIGHT FUSELAGE SKIN, AFT STATIC PORT HAS SMALL NICKS. SDR ENTRY WORKED PER UAL ECRA 5360-02034 SDR2033 ATTACHED FORM 44-0008Oct 4, 2025 · N14118 · Boeing 757224SDR JJBA20251010039Skin · corrodedRFI EXT, SKIN UNDER ANTENNA BTW FR 70-68 AND STR 21R-21L FOUND CORRODED. REPAIR DOUBLER ON RFI LOWER SKIN, BTW FR 68-69 AND BTW 21L-21ROct 3, 2025 · N16149 · Emb EMB145XRSDR DALA2025101007390Skin · damagedPERFORM ER/A 628645-14 REV. ORIGINAL SECTION III ON EXTERNAL SKIN FR 3 AND 10.5 INCH ABOVE STATIC PORT RVSM AREA REFERENCE TO LOG PAGE 1153824. PERFORMED REPAIR ON UPPER SKIN BETWEEN FR2 TO FR4 RH SIDE AND 10.5 INCH ABOVE STATIC PORT RVSM AREA AS PER A320 SRMOct 3, 2025 · N373NW · Airbus A320212SDR CALA2025100709751Skin · ground damageAIRCRAFT AFT FUSALAGE CONTACTED LAV TRUCK AT LAV SVC HATCH. MULTIPLES DENTS AREAS AROUND LAV SERVICE DOOR ON THE STRINGERS THAT REQUIRED OPEN UP FOR FURTHER INSPECTION FOR DAMAGE. REF. SRM 53-00-01-1A-1. SEE ATTACHED PHOTOS FOR LOCATION OF DAMAGE. SKIN AND Oct 3, 2025 · N222UA · Boeing 777222SDR DALA2025100607258Skin · dentedSHIP 5801 DENTS OVER FLANGE OF FRAME BTW S-27L TO 26L AND STA 1500 AT AFTER CARGO COMPARTMENT (C2). CORRECTIVE ACTION: SUMMARY OF NRC 00510. FRAME BTW S-27L TO 26L AND STA 1500 AT AFTER CARGO COMPARTMENT (C2) WAS REPAIRED PER PRI 629266-14 REV. 2 AND ER/A 6292Oct 3, 2025 · N581NW · Boeing 757351SDR DALA2025100607236Skin · corrodedDURING H CHECK AT TECHOPS MX (QRO), WHILE ACCOMPLISHMENT OF TASK CARD 5300-2422, THE FUSELAGE SKIN WAS FOUND CORRODED AT LOWER FORWARD CORNER OF CUT OUT LAVATORY SERVICE ACCESS DOOR BETWEEN BSTA 847 AND BSTA 867 AND BETWEEN S-23L AND S-25L. MAINTENANCE REPAIREOct 3, 2025 · N3768 · Boeing 737832SDR CALA2025100609651Skin · damagedLH FUSELAGE AFT STATIC PORT ELEV FEEL COMPUTER HAS EVIDENCE OF SMALL NICKS. WORKED PER UAL ECRA# 5360-02032 NR# 133444 SDR# 2031 ADD EMP:V940985Oct 3, 2025 · N14118 · Boeing 757224SDR JR2R20251003165Skin · dentedEXTERNAL SKIN HAS A DENT BETWEEN FR19-FR20 AT STR17R-STR18R. REPAIRED PER ETD.Oct 3, 2025 · N84307 · Emb ERJ170200LRSDR SWAA2025110520667Skin · corrodedCORROSION INTERNAL SKIN LOCATED BTW STA 727D TO STA 727E BTW STR 27L TO STR 27R AND WL 148.5 AT AFT CARGO. GAINED ACCESS LOCATED BTW STA 727D TO STA 727E BTW STR 27L TO STR 27R AND WL 148.5 THE CORROSION FOUND ON VHF COMMUNICATION ANTENNA #2 ONLY AT LOWER FUSOct 2, 2025 · N8620H · Boeing 7378H4SDR IPXA2025103060968Skin · corrodedAFT LOWER FUSELAGE FROM STA 1480 TO STA 1500, S-27R TO S-28R, HAS PROTUBERANT DENT, FLL-018, ATA 53. REINSTALLED RH FLOOR PANEL AT AFT CARGO COMP STA 1440 TO STA 1520 IAW B757-200PF SRM 51-40-02-0G-0. ACCOMPLISHED REPAIR PER B757-200PF SRM 53-00-03-2R REPAIR 1Oct 2, 2025 · N459UP · Boeing 75724APFSDR CALA2025102910692Skin · wornFUSELAGE INTERIOR SKIN CHAFED, FORWARD OF L1 DOOR IN TORQUE TUBE AREA. REMOVED AND REPLACED L1 DOOR MIDDLE HINGE GAP COVER IAW DWG 141A3112 REV A, DWG 141A3110 REV-, AND SRM 51-40-02 RESTORED PROTECTIVE FINISH IAW AMM 51-21-73.Oct 2, 2025 · N26226 · Boeing 737824SDR IPXA2025102661012Skin · corrodedAFT LOWER FUSELAGE FROM BS 1560 - 1580, S29R, HAS PROTRUDING DENT, FLL-018, ACCOMPLISH REPAIR PER SRM 53-00-01-2R REPAIR 28 REV. 124 REQUIREMENTS.Oct 2, 2025 · N459UP · Boeing 75724APFSDR IPXA2025101558814Skin · damagedMAJOR REPAIR, SKIN DOUBLER BS 700 - 720, STRINGERS 1R & 2R IS BENT AND DEFORMED, . ACCOMPLISHED REPAIR PER EO-95379-REQ1 AND VT-SAA EA 757-5330-01-B0577, REV. IR.Oct 2, 2025 · N425UP · Boeing 75724APFSDR CALA2025101309943Skin · damagedDAMAGE FOUND TO SKIN BETWEEN STRINGERS 25L AND 26L AROUND STATION 400.REMOVED EXISTING FASTENERS AROUND DAMAGED SKIN AREA, TRIMMED OUT DAMAGED SKIN PER SRM 51-10-02. REF IMAGE ATTACHED FOR DIMENSIONS, SUMMITED TO ESC-MCO FOR REPAIR INSTRUCTION. VERIFY MATERIALOct 2, 2025 · N17719 · Boeing 737724SDR JJBA20251008035Skin · crackedAT REAR FUSE, CRACK FOUND ON LH TOP SKIN AT FR 75 BTW STR 2L-3L. REPAIR DOUBLER ON LH REAR FUSE I UPPER SKIN, AT FR 75 AND AT STR 2LOct 2, 2025 · N16149 · Emb EMB145XRSDR CALA2025100609641Skin · dentedAFT FUSELAGE EXTERNAL SKIN RIGHT ABOVE AFT CARGO DOOR CUTOUT UPR EDGE FWD HINGE THERE IS A DENT. WORKED PER UAL ECRA# 5360-02023 SFR# 2014 NR#: 133462Oct 2, 2025 · N14118 · Boeing 757224SDR AALA202510044149Skin · corrodedAIRCRAFT WAS GROUNDED: CORROSION ON FUSELAGE SKIN AROUND LAVATORY VENT LOCATED AT BS 917, FROM S21L TO S22L. ACCOMPLISHED DOUBLER REPAIR TO SKIN PER SRM 53-70-01-2R-3.Oct 2, 2025 · N864NN · Boeing 737823SDR DALA2025100307225Skin · dentedAFT FUSELAGE TOP SURFACE JUST RIGHT OF RUDDER CENTER HAS A DENT. ASSESSED DENT PER A319 SRM 53-51-11-283-024. (1230717).Oct 2, 2025 · N324NB · Airbus A319114SDR DALA2025100307216Skin · corrodedCORROSION INTERNAL SKIN LOCATED BTW FR 67 TO FR 68 AND BTW STR 30L TO STR 31L IN AFT CARGO COMPARTMENT. COMPLIED WITH ER/A 628904-14. (1230844).Oct 2, 2025 · N352NB · Airbus A319114SDR SWIA2025100401Skin · dentedONE DENTED AREA ON RT TOP FUSELAGE SKIN, DWG 601R33010. AND ONE DEFORMED AREA ON BS 241.60 FRAME. BETWEEN BS 233.276 - 241.60 BETWEEN BL 0.0 - RBL11.16. REF REO 601R-53-11-4021. REPAIRED DENTED AREA ON RT TOP FUSELAGE SKIN IAW REO 601R-53-11-4022, REV-. COOct 1, 2025 · N916EV · Cndair CL6002B19SDR SWIA2025102900001Doubler · corrodedWASTE SERVICE DOOR CUTOUT INTERNAL DOUBLER CORRODED AT HINGE POINT AREA (C-CHECK RO 10/28/2025)REMOVED AND REPLACED WASTE SERVICE DOOR CUTOUT INTERNAL DOUBLER, REF EMB SRM 51-40-08Oct 1, 2025 · N262SY · Emb ERJ170200LLSDR CALA2025101309987Skin · corrodedLAVATORY TOILET SERVICE AT LWR EXTERNAL FUSELAGE SURFACE STRUCTURE WITH BULDGING SKIN AROUND FASTENERS. INSTALLED REPAIR AT FUSELAGE LOWER SKIN STA 827 - 887, STR 22L - 26L IN ACCORDANCE WITH AAR-MIA ESR-WI 2023803-19-12777 REV. IR,Oct 1, 2025 · N33284 · Boeing 737824SDR AALA202510131540Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION TO FUSELAGE LOWER SKIN AROUND DRAIN HOLE AT BS 727J, S27R. REPAIRED SKIN PER SRM 53-60-01-2 -R-4.Oct 1, 2025 · N943NN · Boeing 737823SDR AALA202510131080Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION TO FUSELAGE LOWER SKIN AROUND DRAIN HOLE AT BS 727L, BL 0. REPAIRED SKIN PER SRM 53-60-01-2 -R-4 AND EA 368857.Oct 1, 2025 · N943NN · Boeing 737823SDR AALA202510107928Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION TO FUSELAGE SKIN PANEL AROUND ACCESSORY ACCESS DOOR 312AR CUTOUT AT FR 71 BETWEEN S27R AND S28R. ACCOMPLISHED DOUBLER REPAIR PER EA 368590.Oct 1, 2025 · N428AA · Airbus A321253NXSDR FDEA2025100911865Skin · dentedFUSELAGE: RAMP REPORTED DENT 24 INCH FORWARD OF BULK CARGO DOOR AT AFT FUSELAGE ON SKIN BETWEEN STATION 1887 - STATION 1902 LONGERON 40LEFT - LONGERON 41LEFT, REQUIRED TO PERFORM TERMINATING REPAIR, (REFERANCE: WRI: 53304011). DENT AT 24 INCH FORWARD OF BUOct 1, 2025 · N574FE · Doug MD11FSDR DALA2025100207187Skin · corrodedCORROSION SPOTS FOUND ON FUSELAGE SKIN, INTERNAL SIDE BETWEEN STRGR 31L - STRGR 32L AND FR67 - FR69. COMPLIED WITH ER/A 628904-14. (1229384).Oct 1, 2025 · N352NB · Airbus A319114SDR DALA2025100207181Skin · damagedSHIP 3321 / FUSELAGE / SKIN / AFT OF FR 61 / BETWEEN P2 AND P3 / NEEDS PERMANENT REPAIR. CORRECTIVE ACTION: PERMANENT REPAIR PER ERA 629144-14. (1228894)Oct 1, 2025 · N821NW · Airbus A330323SDR DALA2025100207180Skin · crackedSHIP 3321 VIASAT / AFT ANTENNA STAND-OFF DOUBLER / FUSELAGE SKIN / FR 64/ CRACKS AND DOUBLE DRILLED FASTENER HOLES. CORRECTIVE ACTION: REPAIRED PER ERA 629146-14. (1228744)Oct 1, 2025 · N821NW · Airbus A330323SDR DALA2025100207174Skin · damagedSHIP 3321 FUSELAGE / SKIN / FR 62 - FR 63 / P'1 - P'2 / VIASAT MOD / MISLOCATED FASTENER HOLES. CORRECTIVE ACTION: REPAIRED PER ERA 629016-14. (1228573)Oct 1, 2025 · N821NW · Airbus A330323SDR N6WA2025093002Skin · damagedRH FUSELAGE SKIN DAMAGED BETWEEN FS364.00 TO FS409.00. REPAIRED IAW GOJET EO C550-53MR-095-O AND AWATS EO 25-CRJ5-53-303Sep 30, 2025 · N522GJ · Cndair CL6002C11SDR N6WA2025093001Skin · damagedR/H SIDE FUSELAGE SKIN DAMAGED BETWEEN FS333.00 TO FS364.00. REPAIRED IAW GOJET EO C550-53RM-096-O AND AWATS EO 25-CJR5-53-304Sep 30, 2025 · N522GJ · Cndair CL6002C11SDR CALA2025100709753Skin · corrodedAFT LAV SERVICE PANEL COUTOUT AFT LOWER CORNER SKIN IS BULGING AND RIVETS PULLING THROUGH. AFT LAV SVC PNL CORROSION. PERFORMED REPAIR TO THE FUSELAGE SKIN P/N'S 146A3231-4,146A3201- 7 AND INTERNAL DOUBLER BETWEEN STA 807-887 AND S19L - S24R IAW EC/RA 5360-0Sep 30, 2025 · N38727 · Boeing 737724SDR N6WA2025100104Skin · gougedEXTERNAL SKIN HAS A GOUGE BETWEEN FS969.00-FS985.00 AT STRINGER 27. PERFORMED DOUBLER TRIPPLER REPAIR BETWEEN FS969.00-985.00 AT STGR27 IAW GOJET EO-C550-53MR-092-OSep 30, 2025 · N506GJ · Cndair CL6002C11SDR CALA2025102610516Skin · damagedDURING AAI INSPECTION NO RECORDS OR INSPECTION REQUIREMENTS WERE FOUND FOR THE EXTERNAL DOUBLER REPAIR ON THE FUSELAGE BETWEEN STA 727G - 727H AT STR 21L. REMOVED EXISTING DOUBLER ON FUSELAGE SKIN BETWEEN STA727G TO 727H AT STR 21L. FABRICATED AND INSTALLED NSep 29, 2025 · N17233 · Boeing 737824SDR SWIA2025100600929Skin · dentedDUE TO BIRD STRIKE, FOUND DENT ON FWD FUSELAGE LOWER LH SIDE SKIN. THE DENT IS LOCATED BETWEEN FR01 AND FR02, AND BETWEEN STGR 25L AND STGR 26L. IT MEASURES 3.3 INCHES LONG, 2.75 INCHES WIDE, AND 0.077 INCHES DEEP. THERE IS A CREASE AND OIL CANNING PRESENT. (Sep 29, 2025 · N171SY · Emb ERJ170200LRSDR SWIA202509300029Skin · dentedDUE TO BIRD STRIKE, FOUND DENT ON FWD FUSELAGE LOWER LH SIDE SKIN. THE DENT IS LOCATED BETWEEN FR01 AND FR02, AND BETWEEN STGR 25L AND STGR 26L. IT MEASURES 3.3 INCHES LONG, 2.75 INCHES WIDE, AND 0.077 INCHES DEEP. THERE IS A CREASE AND OIL CANNING PRESENT. (Sep 29, 2025 · N171SY · Emb ERJ170200LR
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