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.

SDR CALA2026031214514Skin · dentedFUSELAGE EXTERNAL SKIN DENTED BS 1016+3 AND BELLOW STRINGER 13L INSTALLED A REPAIR, BS 1016, STRINGER 13L IAW SRM 51-40-02-0G-0 AND SRM 53-80-01-2R-6 FIGURE 202 DETAIL A.Feb 28, 2026 · N14735 · Boeing 737724SDR DALA2026030401480Skin · crackedCRACK INDICATIONS WERE NOTED AT THE NR 4 & 5 HOLES OF THE FUSELAGE SKIN AT THE FORWARD ENTRY DOOR (L1) CUT OUT AFT LWR CORNER DURING NDT INSP. REPAIR IS REQUIRED PRIOR TO FURTHER FLIGHT. AMOC TO AD 24-05-03 MAY BE REQUIRED. CORRECTIVE ACTION: CRACK INDICATIONSFeb 28, 2026 · N179DN · Boeing 767332SDR DALA2026030301450Doubler · corroded(LOG 1471327) DOUBLER REPAIR BETWEEN BS 967 AND BS 1006, S-23L AND S-26L / CORROSION. DOUBLER REPAIR BETWEEN BS 967 AND BS 1006, S-23L AND S-26L PER ERA 632146-14.Feb 27, 2026 · N952DZ · Boeing 7379GPERSDR TSAA2026030270001Skin · crackedWHILE ACCOMPLISHING SERVICE CHECK, CRACK WAS FOUND. CRACK IS APPROXIMATELY 1 5/8 INCHES LONG, 7 ¼ INCHES AFT OF STA 727D (727D +7 ¼), 12 INCHES FWD OF STA 727E (727E -12), 7 ½ BELOW S-20R, 3 ¾ INCHES AFT OF THE WING-TO-BODY FAIRING, 10 ¾ INCHES ABOVE THE EXISTFeb 27, 2026 · N360WA · Boeing 737300SDR R61A2026022700051Skin · gougedWHILE IN HEAVY CHECK - GOUGE IN SKIN NEAR AT FR. 16 NEAR STGR 21L-22L. CUT OUT DAMAGE, FABRICATED AND INSTALLED PERMANENT REPAIR AT SKIN NEAR AT FR. 16 NEAR STGR 21L-22L REF. EMB SRM 53-10-01/AD01.Feb 27, 2026 · N217JQ · Emb ERJ170200LRSDR REXA2026080601501Skin · crackedSECONDARY NRC FROM NRC 00115: AFTER STIFFENETR REMOVAL, CRACK WAS FOUND ON SKIN OF ACCESS PANEL 171CL. SKIN OF ACCESS PANEL 171CL WAS REPAIRED PER REO 670-53-82-430 REV:--Feb 26, 2026 · N297PQ · Cndair CL6002D24SDR SWIA2026022675945Skin · corrodedINTERNAL SKIN AFT OF BS 280 BETWEEN STR 19L - 20L CORRODED. REMOVED, FABRICATED NEW REPLACEMENT SEALING DOUBLER, AND INSTALLED THE NEW DOUBLER IAW DWG BA670-31051, REV NC, DWG BA670-31057, REV -L AND SRM 51-42-06-001-001-A01. CHECKED GOOD.Feb 26, 2026 · N732SK · Cndair CL6002C10SDR SWIA2026022675573Skin · damagedPERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED BETWEEN FS 581 - FS 597 AND STRG 24R - STRG 25R DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM (FILED CLOSED)PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED BETWEEFeb 26, 2026 · N790SK · Cndair CL6002C11SDR SWIA2026022675572Skin · damagedPERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED BETWEEN FS 1000 - FS 1015 AND STRG 25R - STRG 26R DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM (FILED CLOSED)PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED BETWFeb 26, 2026 · N790SK · Cndair CL6002C11SDR SWIA2026022675571Skin · damagedPERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO LH FWD FUSLEAGE SKIN LOCATED BETWEEN FS 394 - FS 409 AND STRG 13L - STRG 14L DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM (FILED CLOSED)PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO LH FWD FUSLEAGE SKIN Feb 26, 2026 · N790SK · Cndair CL6002C11SDR SWIA2026022675570Skin · damagedPERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO RH FWD FUSLEAGE SKIN LOCATED BETWEEN FS 394 - FS 409 AND STRG 13R - STRG 14R DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM (FILED CLOSED)PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO RH FWD FUSLEAGE SKINFeb 26, 2026 · N790SK · Cndair CL6002C11SDR SWIA2026022675569Skin · damagedPERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO UPPER FUSLEAGE SKIN LOCATED BETWEEN FS 830.40 - FS 847 AND STRG 1L - STRG 0 DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM (FILED CLOSED)PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO UPPER FUSLEAGE SKIN LOFeb 26, 2026 · N790SK · Cndair CL6002C11SDR CALA2026030514369Skin Panel · damagedLEFT SKIN BTW BS 654+88 - 654+110, S29L-30L CREASED. THERE ARE NO ALLOWABLE LIMITS FOR THE CREASE IAW SRM 53-00-01-1A-1, PERFORMED A REPAIR IAW ECRA 5330-07699, PART 1 INTERIM REPAIR WITHOUT ANY DEVIATION.Feb 26, 2026 · N69059 · Boeing 767424ERSDR DALA2026030401479Skin · crackedCRACK INDICATIONS WERE NOTED AT THE NR 5 HOLE OF THE FUSELAGE SKIN AT THE FORWARD SERVICE DOOR (R1) CUT OUT AFT LWR CORNER DURING NDT INSP. REPAIR IS REQUIRED PRIOR TO FURTHER FLIGHT. AMOC TO AD 24-05-03 MAY BE REQUIRED. REPAIRED THE R1 DOOR AFT LOWER CORNERFeb 26, 2026 · N179DN · Boeing 767332SDR MASA20260303004Skin · dentedDURING C1, C3 SCHEDULED MAINTENANCE INSPECTIONS OF FWD FUSELAGE SKINS, MULTIPLE DENTS FOUND O RH SIDE (QTY 9). THE DAMAGES ARE OUTSIDE THE ALLOWABLE LIMITS DEFINED IN ERJ175 SRM 53-10-01, AD02. AS PER ETD2026-170-003152 DISPOSITION-001 THE 9 DENTS WHERE FOUNDFeb 26, 2026 · N85340 · Emb ERJ170200LRSDR DALA2026030201421Skin · crackedCRACK ON FUSELAGE SKIN STA Y = 1087 LONG 13 LH-14LH SIDE. REPAIR AND PRI 631743-14 (1469678)Feb 26, 2026 · N952AT · Boeing 717200SDR N6WA2026022702Skin · gougedFUSELAGE SKIN GOUGED AT FS977.00 AT STGR27. REPAIRED FUSELAGE SKIN AT FS977.00 AT STGR27 IAW GOJET EO-C550-53MR-119-OFeb 26, 2026 · N523GJ · Cndair CL6002C11SDR REXA2026080601523Skin · corrodedAFTER REMOVAL INTERNAL PRODUCTION DOUBLER, CORROSION ON FUSELAGE INNER SKIN, BETWEEN FS= 295 TO FS= 310 AND STGR 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT WAS FOUND CORROSION ON FUSELAGE INNER SKIN, BETWEEN FS= 295 TO FS= 310 AND STGR 26LH TO 26RH AT MAIN AVIOFeb 25, 2026 · N297PQ · Cndair CL6002D24SDR IXXA20260420003Skin · crackedAD2024-05-03, SB 767-53A0301 REV 2. CRACK FOUND AT FORWARD SERVICE DOOR CUTOUT AFT LOWER CORNER BETWEEN STA 340 - STA 332 1' HOLE ABOVE S-20R. REF XTREME AVIATION NRC 341Feb 25, 2026 · N255CM · Boeing 767223SDR SWAA2026032774494Doubler · crackedEGPR SURROUND DOUBLER IS CRACKED BS233 WL175 8' ABOVE S-24R . TRIMMED OUT THE DAMAGED, FABRICATED REPAIR PARTS AND INSTALLED ALL REPAIR PARTS AT THE EGPR SURROUND DOUBLER AT BS233 WL175 8' ABOVE S-24R IAW SRM 53-10-15-2R-4, REPAIR 4, PARG 4(B-M).Feb 25, 2026 · N923WN · Boeing 7377H4SDR CALA2026031714621Skin · dentedSECTION 46 AT LOWER SKIN BETWEEN STA 1439 / STA1461 AND STR 38R HAS DENT & CREASE CREATED THE SFR AND IT IS NECESSARY TO QC CHECK AND APPROVAL THE SFR THE SFR #3048 WAS REVIEWED BY QC. DENT/CREASE IN THE FUSELAGE SKIN BETWEEN STA 1439/1461 AND STGR - 38R WAS RFeb 25, 2026 · N76062 · Boeing 767424ERSDR CALA2026030514329Skin · damagedACFT DAMAGE TO LT SIDE SECTION 41. BETWEEN BS 312 - 360, STRINGERS 21L & 22L. ACCOPLISHED SECTION A , STEOS 1 ,2 AND 3 DVI. NO DEFECTES FOUND. REMOVED DAMAGED SKIN BETWEEN BS 312 -360, S21L & S22L REF SECTION A STEP 7, A-B REF AVO 7548-26-02-25-01 REV A. Feb 25, 2026 · N37548 · Boeing 7379SDR DALA2026030201423Skin · damagedFUSELAGE / SKIN / STA 229.00 AND STA 256.00, BETWEEN L-15R & L-16R / LIGHTNING STRIKES. REPAIRED PER ER/A 619580-14AD. (1467470)Feb 25, 2026 · N717JL · Boeing 717200SDR DALA2026022501339Skin · dentedFUESLAGE EXTERNAL SKIN DENT REPAIR AT APPROX 2 FEET IN FRONT OF 1L DOOR LOWER FWD EDGE. CORRECTED PER A330 SRM 53-11-11-205-039. (1466513)Feb 25, 2026 · N406DX · Airbus A330941SDR SWIA2026022476884Skin · crackedSKIN CRACKED AT BS 235, STR 26R AT AFT CORNER OF NLG CUTOUT. REPAIRED THE SKIN RADIUS AT BS 235 IAW REO 601R-53-11-048, REV -D. & REO 601R-53-11-4076, REV--, SRM 51-42-06, SRM 51-25-01, & AMM 32-22-05.Feb 24, 2026 · N207PS · Cndair CL6002B19SDR COEA2026070711803Skin · dentedDURING HEAVY CHECK, LT STATIC PORT AREA SKIN DENTED. REPAIRED IAW SRAS 00026106-01 ISSUE A, DATED 6/11/2026.Feb 24, 2026 · N803FX · Aerosp ATR72212SDR COEA2026062503803Skin · dentedEXTERNAL FUSELAGE CROWN SKIN IS DENTED BETWEEN FRAMES 28D-29 STRINGERS 2-3R. REPAIRED PER SRM 530000-300-803-A01 REV. 121.Feb 24, 2026 · N803FX · Aerosp ATR72212SDR SWIA2026022475926Skin · chafedEXTERNAL SKIN REPAIR CHAFED FS975 BL0. REPAIRED CHAFED DAMAGE ON EXTERNAL SKIN PREVIOUS REPAIR COVER PLATE AT FS 975 & BL 00 IAW REO 670-53-00-815 REV -. DIMENSION OF BLEND: L=1.500" W=1.115" THICKNESS FOUND= 0.043".COMPLIED WITH SKY CARD 51-900-1002-SKY SFeb 24, 2026 · N732SK · Cndair CL6002C10SDR R61A2026032700065Skin · dentedTWO DENTS FR9-11 STGR 14L-16L. REMOVED AND REPLACED FWD FUSELAGE SKIN FR 9-11 AND STGR 14L-16L REF EMB SRM 51-40-08.Feb 24, 2026 · N239JQ · Emb ERJ170200LRSDR DALA2026030201418Skin · corrodedCORROSION ON SKIN STA 737 X: -15 TO -30 APROX AT FUSELAGE. REPAIR INSTRUCTIONS AND PRI 631685-14 (1466288)Feb 24, 2026 · N949AT · Boeing 717200SDR DALA2026030201417Skin · crackedCRACK ON FUSELAGE SKIN STA Y =1037 LONG 13 LH-14LH SIDE. REPAIRED PER PRI 631741-14 (1466248)Feb 24, 2026 · N952AT · Boeing 717200SDR DALA2026022501347Skin · corrodedFUSELAGE EXTERNAL SKIN & INTERNAL SKIN DOUBLER AT THE WASTE SERVICE PANEL CUTOUT, BS 1540 - 1560, S27 - 29R CORRODED. REPAIRED IAW ERA 632028-14. (1465593)Feb 24, 2026 · N582NW · Boeing 757351SDR DALA2026022501344Skin · dentedDENT ON EXTERNAL SKIN LOCATED AT FR 3 & 19 INCHES BELOW RH STRINGER, LOWER FUSELAGE. PERFORMED PERMANENT REPAIR ON THE SKIN IAW SRM 53-11-11-300-041, STEP 2.A, FIGURE 001.Feb 24, 2026 · N377NW · Airbus A320211SDR SWIA2026022376138Skin · corrodedEXTERIOR SKIN CORRODED IN SEVERAL AREAS FS559+80 TO FS559+112 STRINGER 26L TO 26R. PERFORMED REPAIR BY BLENDING CORROSION IAW REO 601R-53-51-734 REV-A DATED 2026-04-23.Feb 23, 2026 · N457SW · Cndair CL6002B19SDR DALA2026022401326Skin · bulgedLOWER FUSELAGE FR66, STR39L POTABLE WATER SERVICE PANEL FWD LOWER CORNER WITH BULGED SKIN AND SOLID RIVETS WITH CORROSION. CORRECTIVE ACTION: REPLACED POTABLE WATER SERVICE PANEL INTERNAL REINFORCEMENT DOUBLER P/N D5348011420800 PER SRM 51-72-11-911-001 AND 51Feb 23, 2026 · N331NB · Airbus A319114SDR DALA2026022401325Skin · bulgedLOWER FUSELAGE FR66 BETWEEN STR 38R-39R (WASTE) TOILET SERVICE PANEL AFT LOWER CORNER WITH BULGED SKIN. CORRECTIVE ACTION: REPLACED (WASTE) TOILET SERVICE PANEL INTERNAL REINFORCEMENT DOUBLER P/N D5348011521201 PER SRM 51-72-11-911-001 AND 51-42-11- 801-PARG 2Feb 23, 2026 · N331NB · Airbus A319114SDR SWIA2026022275553Skin · gougedFORWARD FUSELAGE SKIN GOUGED BETWEEN FR 10-11 STGR 13L-14L (C-CHECK RO 03/18/2026)PERFORMED THROUGH DAMAGE REPAIR ON FWD FUSELAGE SKIN AT FR 10-11, STGR 13L-14L. REF. SRM 53-10-01/AD03. SEE CONTINUE CARD FOR WORK PERFORMED. NO CHANGE TO WEIGHT AND BALANCE.Feb 22, 2026 · N400SY · Emb ERJ170200LRSDR DALA2026022301296Skin · damagedTOOLING DAMAGE ON AFT SIDE OF C23, P'4 - P'5 AT UPPER OTBD HOLE. CORRECTED IAW ERA 632216-14, REV. ORIGINAL. (1462480)Feb 22, 2026 · N858NW · Airbus A330223SDR CALA2026050816072Skin · ground damageAIRCRAFT STRUCK BY WATER SERVICING TRUCK. AFT OF WATER SERVICING DOOR. LOCATION OF DAMAGE IS AFT OF THE LAV VACUME WASTE ACCESS PANEL, UNDER BULK CARGO LAV WASTE TANKS. WASTE TANK RINSE LINE FITTING ASSEMBLY - REMOVAL IAW AMM DMC-B787-A-38-32-14, FOR CLOSEST Feb 21, 2026 · N16009 · Boeing 78710SDR SWIA2026031175506Skin · dentedAFT FUSELAGE SKIN, BS 700 BTWN STRINGERS 20L-24L DENTED. ACOMPLISHED WHIT REO 601R-53-61-8482, FOR REPAIR ON AFT FUSELAGE SKIN.Feb 21, 2026 · N913EV · Cndair CL6002B19SDR CALA2026022614068Skin · gougedGOUGE ON FUSELAGE SKIN BS 727E, STRINGER 19R. MAJOR REPAIR. ACCOMPLISHED A DOUBLER REPAIR ON THE SKIN BS 727E, STR 19R IAW SRM 53-00-01-2R-1, REPAIR 1, FIG 201.Feb 21, 2026 · N57439 · Boeing 737924ERSDR HNAA2026032600243Skin · crackedREAR FUSELAGE EXTERNAL SKIN HAS POSSIBLE CRACK AROUND RIVET AT FR 78 BETWEEN STGR 4L / 5L. PERFORMED CUTOUT OF CRACK AROUND RIVET ON REAR FUS EXTERNAL SKIN AT FR 78 AND BTW STR 4L-5L AND PERFORMED PERMANENT REPAIR OF SKIN AT FR 78 AND BTW STR 4L-5L IAW PIEDMOFeb 20, 2026 · N699AE · Emb EMB145LRSDR AALA202603182915Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION FOUND ON SKIN DOUBLER UNDER ETWLU ANTENA @ FR42-FR43, STR 1R TO STR 1L. MAINTENANCE REPLACED SKIN DOUBLER IAW SRM 51-42-11-801 AND DWG SI17-016-01 SHEET 9, DETAIL H.Feb 20, 2026 · N8027D · Airbus A319115SDR CALA2026031314561Skin · corrodedFOUND CORROSION AFT OF AFT CARGO BAY SKIN PANEL AT LAV VENT DUCT BASE BETWEEN BS 907 & 927, S-21L & S-22L. FABRICATED AND INSTALLED REPAIR PARTS AT LT FUSELAGE SKIN BETWEEN BS 907 & 927 BETWEEN S-21L & S-22L IAW SRM 51-40-02-0G-0 AND SRM 53-70-01-2R-3.Feb 20, 2026 · N35236 · Boeing 737824SDR DALA2026022301304Skin · damagedFORWARD SIDE OF FRAME 61 & P2, TOOLING DAMAGE ON FUSELAGE SKIN. REPAIRED IAW ERA 632216-14, REV ORIG. (1460345)Feb 20, 2026 · N858NW · Airbus A330223SDR DALA2026022301303Skin · damagedAFT SIDE OF C 23 HAD TOOLING DAMAGE. CORRECTED IAW ERA 632216-14, REV ORIG. (1460306)Feb 20, 2026 · N858NW · Airbus A330223SDR DALA2026022301302Skin · damagedTOOLING DAMAGE (VARIOUS)- BETWEEN FR 61 & 62, STRINGER 2L & 2R. REPAIRED IAW ERA 632216-14, REV ORIG. (1460232)Feb 20, 2026 · N858NW · Airbus A330223SDR DALA2026022301301Skin · damagedTOOLING DAMAGE, TWO EACH. BETWEEN FR 60 & FR 61, STRINGERS 1 & 2R. REPAIRED IAW ERA 632216-14, REV. ORIG. (1460225)Feb 20, 2026 · N858NW · Airbus A330223SDR DALA2026022001246Skin · damagedSHIP 3358 FORWARD SIDE OF FRAME 60 @ P'1 TOOLING DAMAGE ON FUSELAGE SKIN. CORRECTIVE ACTION: REPAIRED PER ERA 632216-14 REV. ORIG. (1459015)Feb 19, 2026 · N858NW · Airbus A330223SDR DALA2026022001245Skin · damagedSHIP 3358 JUST OUTBOARD OF P'2 TOOLING DAMAGE ON FUSELAGE SKIN AND ADJACENT CLIP. CORRECTIVE ACTION: REPAIRED PER ERA 632216-14 REV. ORIG. (1459013)Feb 19, 2026 · N858NW · Airbus A330223
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