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.

SDR DALA2024120911558Skin · scratchedSHIP 3134 SCRATCH EXTERNAL SKIN LOCATED AT FR 61 BTW STR 27R TO STR 28R AT LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH ER/A 622662-14. (0700219)Dec 8, 2024 · N334NB · Airbus A319114SDR R61A2024120800581Skin · mechanic errorDURING HEAVY CHECK FWD FUSELAGE LOWER SKIN AT FR14 AND STR23L/H FOUND TWO HOLES PREVIOUS DAMAGE AT INNER DOUBLER OF EXTERNAL POWER RECEPTACLE. FWD FUSELAGE LOWER SKIN AT FR14 STR23 L/H HAS BEEN REPAIR IAW ETD 2024-170-031549REV.ADec 8, 2024 · N743YX · Emb ERJ170200LRSDR AALA202502251298Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON AFT LOWER FASTENER HOLE OF FR35 LH AND STR30 CRACK DIRECTION 5 AND 11 OCLOCK . CRACK MEASURE IS L=0.160 INCH. MAINTENANCE PERFORMED TIME LIMITED REPAIR (INSTALLED FILLER) ON HOLE H2 LOC.AT FR35 ON AFT LOWDec 7, 2024 · N773XF · Airbus A319112SDR VNAA20250127017Skin · bulgedPROTUBERANCE ON EXTERNAL SKIN RH SIDE BTW FS202.75 TO FS 210.00 AND STRG 13A TO STRG 12A AT FORWARD FUSELAGE. PROTUBERANCE ON EXTERNAL SKIN RH SIDE BTW FS202.75 TO FS 210.00 AND STRG 13A TO STRG 12A AT FORWARD FUSELAGE WAS EVALUATED PER CRJ700 SRM 53-00-01-Dec 7, 2024 · N519AE · Cndair CL6002C10SDR JR2R20241207777Skin · corrodedFORWARD CARGO CUT-OUT, FUSELAGE SKIN IN AREA COVERED BY AFT SCUFF PLATE HAS TWO AREAS OF SURFACE CORROSION AT ATTACH SCREW HOLESDec 7, 2024 · N86316 · Emb ERJ170200LRSDR DALA2025122309388Skin · not reportedFUSELAGE SKIN, BS 500 - 520, S27L TO S28R, ATG4 WIFI ANTENNA INSTALLATION PROXIMITY TO REPAIR DOUBLER. REF ERA 515287-14. (0696329)Dec 6, 2024 · N697DL · Boeing 757232SDR AALA202502284384Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON EXTERNAL FUSELAGE SKIN PANEL BETWEEN FR 69 AND FR 70 AT S2L. REPAIRED SKIN PANEL PER EA 361152.Dec 6, 2024 · N167US · Airbus A321211SDR AALA202502262965Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON UPPER FUSELAGE EXTERNAL SKIN PANEL AT FR 70 BETWEEN S1L AND S2L. REPAIRED SKIN PANEL PER EA 361152.Dec 6, 2024 · N167US · Airbus A321211SDR AALA202502260209Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON UPPER FUSELAGE EXTERNAL SKIN PANEL AT FR 70 BETWEEN S1R AND S2R. REPAIRED SKIN PANEL PER EA 361152.Dec 6, 2024 · N167US · Airbus A321211SDR VNAA20250127015Access Panel · corrodedCORROSION ON SETTLEMENT AREA OF ACCESS PANEL 195AB CORROSION ON SETTLEMENT AREA OF ACCESS PANEL 195AB WAS EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-82-55-101-002-A02 AND WAS REPLACED PER CRJ700 SRM 51-42-13-001-001-A01Dec 6, 2024 · N519AE · Cndair CL6002C10SDR VNAA20250127013Skin · dentedDESCRIPTION: DENT ON FUSELAGE SKIN BTW FS 1069.75 TO FS 1088.20 AND BTW STGR 17RH-16RH AT REAR FUSELAGE. DENT ON FUSELAGE SKIN BTW FS 1069.75 TO FS 1088.20 AND BTW STGR 17RH-16RH AT REAR FUSELAGE WAS REPAIRED PER REO 670-51-00-085 REV - A AND PER REO 670-53Dec 6, 2024 · N519AE · Cndair CL6002C10SDR REXA2025012300084Skin · crackedCRACK IN LH FWD FUSELAGE SKIN LOCATED IN WL 79.5 AND F.S. 189.5 AT AFT LOWER CORNER OF CUTOUT ACCESS PANEL 211AL LH FWD FUSELAGE SKIN LOCATED IN WL 79.5 AND F.S. 189.5 AT AFT LOWER CORNER OF CUTOUT ACCESS PANEL 211AL WAS REPAIRED PER REO 670-53-11-2068 REV --Dec 6, 2024 · N317CA · Cndair CL6002C10SDR BLUA202412190001Skin · corrodedDURING 12, 24, 48 & 96 MONTH INSPECTIONS, CORROSION WAS DISCOVERED IN THE CABIN FLOOR LOWER SKIN AT SEVERAL LOCATIONS. FROM FS 157.00 TO FS 366.56. REPAIRS WERE MADE IN ACCORDANCE WITH TEXTRON AVIATION FIELD REPAIR # FR-560-5027-14050. DOUBLERS WERE INSTALLED Dec 6, 2024 · N560ML · Cessna 560XLSDR GTIA2025050638903Skin Panel · puncturedPENETRATION DAMAGE FOUND AT FRAME 5 SKIN PANEL, STRINGER BELOW Z508. RAF-01 # 3277238-01 CREATED.-PERFORMED PERMANENT REPAIR LH FUSELAGE SKIN PANEL FR4 - FR6 Z-339 PER SPIRIT EA 5311-24114 W/O 336903Dec 5, 2024 · N948NK · Airbus A320271NSDR SWIA202503241205Skin · gougedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA75762-670-53-21-2207 N772SK MXCODEID60308-PR - TEMPORARY DISPOSITION FOR BLENDED GOUGE AND DENT DAMAGE TO THE FUSELAGE UPPER SKIN AT FS349.00 AND BETWEEN STR 4L -STR 5L. COMPLIED WITH REINSPECT PER REO 670-53-21-2207.Dec 5, 2024 · N772SK · Cndair CL6002C10SDR CALA2024121103061Skin · damagedFOUND DAMAGE AT FUSELAGE EXTERNAL SKIN BTW STA 500D AND STA 500E BTW STR 19R AND STR 20R REF TO LOG#3085861 (REF AAR NR 100002760 9) REPAIRED AREA AT FUSELAGE EXTERNAL SKIN BTW STA 500D AND STA 500. ESFR NO. 1037866 E, BTW STR19R AND STR20R REF TO LOG PAGE NO.Dec 5, 2024 · N69847 · Boeing 737924ERSDR DALA2024120911563Skin · scratchedSHIP 3134 SCRATCHES FOUND ON EXTERNAL SKIN AT FR61 AND FR62 AND STR 27RH AND STR 28R SCRATCH AT FR61. CORRECTIVE ACTION: REPAIRED PER ER/A 622662-14. (0695292)Dec 5, 2024 · N334NB · Airbus A319114SDR EE4Y2024120521407Skin · damagedPERFORMED REPLACEMENT OF PERMANENT REPAIR INSTALLED AT FR01+65MM STR 20L+130MM, (FWD FUSELAGE) AS PER COOPESA´S EO COO-EO-2024-21042-R00 REV 00, SINCE EXISTING REPAIR WAS FOUND WITHOUT MATERIAL TRACEABILITY RECORDS, THE REPAIR WAS FOLLOWED BY THE EMBRAER DISPODec 5, 2024 · N203JB · Emb ERJ190100IGWSDR EE4Y2024120521405Skin · corrodedCORROSION WAS IDENTIFIED ON THE FUSELAGE SKIN LOCATED IN CENTER FUSELAGE II AT FR73+275MM, STGR-28L. THE AFFECTED AREA HAS BEEN REVIEWED, AND THE DAMAGE WAS FOUND OUT THE ALLOWABLE DAMAGE LIMITS AS PER ERJ SRM PART II, 53-22-01, AD51, PAR. 5A (2), TABLE 102. Dec 5, 2024 · N230JB · Emb ERJ190100IGWSDR SWI2025F00083Skin · damagedSEVERAL PILOT HOLES IN NEW SKIN P/N 170-61801-013 DO NOT LINE UP WITH EXISTING HOLES IN ACFT. (FILED CLOSED) REPAIRED ALL MISALIGNED HOLES PER ETD2024-170-032450 REV.: A. - THIS REPAIR IS CONSIDERED TEMPORARY AS IT WILL REQUIRE A DETAILED STRUCTURAL ANADec 4, 2024 · N127SY · Emb ERJ170200LRSDR VNAA20250127005Skin · dentedDENT DAMAGE TO FUSELAGE SKIN IN RVSM AREA AT FS202.75 AND BETWEEN STRINGER 15R AND 16R DENT DAMAGE TO FUSELAGE SKIN IN RVSM AREA AT FS202.75 AND BETWEEN STRINGER 15R AND 16R WAS REPAIRED PER REO 670-53-11-2072 REV.-ADec 4, 2024 · N519AE · Cndair CL6002C10SDR VNAA20250127002Skin · dentedDENTS ON AFT LOWER FUSELAGE SKIN BTW FS1162.00-55.63% REAR SPAR DATUM AND BTW STR22L-STR22R. DENTS ON AFT LOWER FUSELAGE SKIN BTW FS1162.00-55.63% REAR SPAR DATUM AND BTW STR22L-STR22R WERE REPAIRED PER REO 670-53-71-095 REV. - - AND EA A1-670-53-00054 REV CDec 4, 2024 · N519AE · Cndair CL6002C10SDR SWIA2025012400004Skin · dentedEXTERNAL FUSELAGE JUST OUTSIDE OF FWD JACK PAD.DENT IS VISIBLE,IN BETWEEN STR26L AND STR 27 (C-CHECK RO 1/23/2025) DRESS-BACK DENT PER REO 670-51-00-085 REV -A DATE 2017-08-23. FOUND OUT OF LIMITS. REPAIRED EXTERNAL FUSELAGE JUST OUTSIDE OF FWD JACK PADDec 4, 2024 · N170PQ · Cndair CL6002D24SDR R61A2024121700587Skin · damagedMAJOR REPAIR: REAR FUSELAGE LOWER SKIN HAS THROUGH DAMAGE NEAR WIFI ANTENNA MOD. REPAIRED IAW 170EA-53-30-007MR, ETD2024-170-900614, ETD2024-170-900620, ETD2024-170-900621, ETD2024-170-900639, ETD2024-170-032298.Dec 4, 2024 · N760YX · Emb ERJ170200LRSDR SWIA2025022841203Skin · chafedCHAFE ON EXTERNAL SKIN BELLY DOUBLER AT STR.27 BETWEEN APROX. FS.913.00 AND FS.927.00 (MARKED). (C-CHECK RO 2/26/2025) REPAIRED EXTERNAL SKIN BELLY DOUBLER AT STGR27 BETWEEN FS913-FS927 REF-CRJ-900 MHIRJ REO 690-53-00-586 REV -- DATE 2025-01-13. LEAK CHDec 3, 2024 · N809SK · Cndair CL6002D24SDR SWIA2024121364Skin · damagedLH FWD FUSELAGE BIRD STRIKE FOR DAMAGE REF SRM 53-10-01/AD02. APPEARS TO FALL IN THE "NO DAMAGE ALLOWED" AREA WITH CORNER OF DAMAGE BEGINNING AT TOP FORWARD CORNER OF LOWER RSVM AREA. DAMAGE IS 7.5" WIDE BETWEEN FR1 AND FR2 AND 11" TALL STARTING FROM STGR 18Dec 3, 2024 · N85377 · Emb ERJ170200LLSDR SWIA2024120901358Skin · damagedTRANSFER FROM EAML 1484481 : REF EAML 1484455 GVI OF THE LH FWD FUSELAGE BIRD STRIKE FOR DAMAGE REF SRM 53-10-01/AD02. DAMAGE SHOWN IN PICTURES APPEARS TO FALL IN THE "NO DAMAGE ALLOWED" AREA WITH CORNER OF DAMAGE BEGINNING AT TOP FORWARD CORNER OF LOWER RSVMDec 3, 2024 · N85377 · Emb ERJ170200LLSDR IPXA2024120509872Skin · damagedDAMAGE AREA ON FUSELAGE SKIN AFT OF AFT PIT DOOR MISSING TOPCOAT. APPLIED PRIMER AS REQUIRED. PROTECTIVE COATING WILL NEED TO BE APPLIED WHEN GROUND TIME PERMITS REF B747-8 SRM 51-20-01. APPLIED TOPCOAT AT REQ'D PER B747-8 SRM 51-20-01.Dec 3, 2024 · N631UP · Boeing 7478FSDR AALA202503037918Skin Panel · scratchedAIRCRAFT IN BASE MAINTENANCE: SCRATCH ON INTERNAL SKIN LOCATED BTW FR56 TO FR57 AND BTW STRG42L TO STRG43L IN AFT CARGO COMPARTMENT ,SCRATCH MEASURES ARE L=2.825 INCH W=0.071 INCH. MAINTENANCE PERFORMED TIME LIMITED REPAIR LOCATED ON EXTERNAL SKIN LOCATED BTW Dec 2, 2024 · N122US · Airbus A320214SDR NACA2024120200006Skin · corrodedFOUND M/D INNER SKIN CORROSION AT BS 1197+132 TO 1219 S-13R TO S-14R. ACCOMPLISH EO 767-53-0065Dec 2, 2024 · N379CX · Boeing 767323SDR NACA2024120200005Skin · crackedFORWARD R/H SERVICE DOOR CUTOUT AFT LOWER CORNER FASTENER HOLE CRACK. ACCOMPLISHED EO 767-53-0064.Dec 2, 2024 · N379CX · Boeing 767323SDR SWAA2024120673598Skin · crackedCRACK INDICATION AT FASTENER LOCATED AT BS 539 STR 3R +3 CRACK INDICATION AT FASTENER LOCATED AT BS 539 STR 3R +3. SEE ATTACHMENTS FOR PIC<[01] REPAIRED HOLE CRACK INDICATION BY OVERSIZING OVER EA 24-153-03342 WIP 2Dec 2, 2024 · N8652B · Boeing 7378H4SDR DALA2024120311406Skin · arced(LOG 0689631) LIGHTNING STRIKE ON FUSELAGE SKIN AT STA-400+6 BETWEEN STR-27R AND STR-27L. REPAIRED LIGHTNING STRIKE ON FUSELAGE SKIN AT STA 400+6 BETWEEN STR 27R-27L IAW B737 SRM 53-00-01-2R-38.Dec 2, 2024 · N853DN · Boeing 737932ERSDR DALA2024120311405Skin · arced(LOG 0689626) LIGHTNING STRIKES ON FUSELAGE SKIN AT STA-360+6 BETWEEN STR-27R AND STR-27L. REPAIRED LIGHTNING STRIKE ON FUSELAGE SKIN AT STA 360+6 BETWEEN STR 27R-27L IAW B737 SRM 53-00-01-2R-38Dec 2, 2024 · N853DN · Boeing 737932ERSDR 2024FA0000937Skin · corrodedCORROSION FOUND AT BL 0.00 AFT OF AFT FUSELAGE FARING WHERE BELLY FAIRINGS JOIN TOGETHER.Dec 2, 2024 · N387QS · Cessna 680SOVSDR CALA2024120303007Skin · crackedPERFORMED INTERIM REPAIR TO LH WING OUTBD LOWER SKIN PANEL CRACK BETWEEN WSTA 564.5 - 591.5 AT S-9L REFER TO EC/RA 5725-01152. REQUIREMENTS PER PART 2 OF EC/RA 5725-01152 ON OR BEFORE 25 MAY 2026. DIP TO BE INITIATED A DTA DIP TO STATE: ON THE LH WING LOWER SKDec 2, 2024 · N24202 · Boeing 737824SDR DALA2024120211320Skin · scratchedSHIP 3134 SCRATCH EXTERNAL SKIN LOCATED AT FR 62 BTW STR 27R TO STR 28R AT LOWER FUSELAGE. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON EXTERNAL SKIN LOCATED AT FR 62 BTW STR 27R TO STR 28R AT LOWER FUSELAGE AS PER A319 SRM 53-41-11-300-109. (0688236)Dec 2, 2024 · N334NB · Airbus A319114SDR DALA2024120311431Stringer · abnormalSHIP 5642 LIGHTNING STRIKE - FS 600 STGR 10L. CORRECTIVE ACTION: REPAIRED DAMAGED IAW PRI 622743-14 REV4. (0686725)Dec 1, 2024 · N542US · Boeing 757251SDR CALA2024122303147Skin · crackedDOOR 1LH - CRACK INDICATIONS FOUND FASTENER HOLES OF FORWARD SERVICE DOOR CUTOUT AFT LOWER CORNER FUSELAGE SKIN AND BEAR STRAP. CORRECT LOCATION THIS LOG PAGE DOOR 1RH. ACCOMPLISH INSPECTIONS 5330-07388 ON OR BEFORE THE AIRCRAFT REACHES 37,500 TOTAL FLIGHT REQNov 30, 2024 · N667UA · Boeing 767322SDR CALA2024121603091Skin · crackedDOOR 1LH - CRACK INDICATIONS FOUND FASTENER HOLES OF FORWARD ENTRY DOOR CUTOUT AFT LOWER CORNER FUSELAGE SKIN AND BEAR STRAP.Nov 30, 2024 · N667UA · Boeing 767322SDR DALA2024120311434Skin · abnormalSHIP 5642 DTE LOGPAGE FOR ERA 622743-14AD REV ORIGINAL B757-200 / FUSELAGE / SKIN / STA 600 / STR 10L / LIGHTNING STRIKE. CORRECTIVE ACTION: REF ERA 622743-14AD. (0686587)Nov 30, 2024 · N542US · Boeing 757251SDR AALA202412019240Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FUSELAGE SKIN INTERNAL SIDE, LOCATED BETWEEN STA 1874 AND STA 1895, BETWEEN S39L AND S40L, IN AFT CARGO CARGO COMPARTMENT. ACCOMPLISHED DOUBLER REPAIR PER EA 359906.Nov 30, 2024 · N791AN · Boeing 777223SDR KCSA202411301120Skin · corrodedCORROSION ON FUSELAGE SKIN INTERIOR APPROX BS 1490 RBL 40 BETWEEN STR 4R AND 5RNov 30, 2024 · N715CK · Boeing 7474B5FSDR CALA2024121603087Skin · damagedIT WAS FOUND OLD SCRIBE LINE ON FUSELAGE SKIN RH SIDE AT STA 1165 TO 1175 BETWEEN STR19 TO STR20 AS PER SRM 53-00-00-0G-0. PERFORMED REWORK AS PER ECRA 5330-07323. ON IS AN INTERIM SOLUTION WITH INSPECTION REQUIREMENTS. ACCOMPLI EC/RA 5360-01910 ON OR BEFORE TNov 29, 2024 · N69059 · Boeing 767424ERSDR DALA2024120211372Doubler · corrodedCORROSION ON DOUBLER BELOW TEE FITTING STA 1053 LONGERON 30 AT AFT BULKHEAD. SUMMARY OF NRC 00563: CORROSION LEVEL 2. DOUBLER BELOW TEE FITTING STA 1053 LONGERON 30 AT AFT BULKHEAD WAS REPLACED PER B717 SRM 53-20-08-0I PROCEDURE 2 AND 51-41-05-0G. (LP #0684614Nov 29, 2024 · N979AT · Boeing 717200SDR DALA2024120211352Skin · dentedSHIP 689 IN REFERENCE TO NRC 00023. DENT BTW STA 440 TO STA 460 AND S-27L TO S-28L AT EXTERNAL FUSELAGE SKIN. CORRECTIVE ACTION: SUMMARY OF NRC 00251: DENT ON FUSELAGE SKIN BTW STA 440 TO 460 AND S-27L TO S-28L WAS REPAIRED PER ER/A 622587-14 REV. ORIGINAL SECNov 29, 2024 · N689DL · Boeing 757232SDR SIMA20241128001Skin · puncturedREAR FUSELAGE SKIN HAS PUNCTURE BETWEEN FR 98-99, STRINGERS 2R-3R (MAJOR REPAIR) ACCOMPLISHED ERS-EJ-53MR-5097 FUSELAGE SKIN BETWEEN FR 98-99 AND STR 2R-3R PUNCTURED-PERMANENT REPAIRNov 28, 2024 · N762DT · Emb ERJ170100STDSDR CALA2025010900066Skin · dentedEXTERIOR FUSELAGE SKIN DENTED BETWEEN STA 787-807 STR 24L- STR 25L. DENT FOUND TO BE OUT OF LIMITS PER B737 SRM 53-00-01-1A-5. REPAIRED FUSELAGE SKIN IAW B737-800 SRM 53-00-01-2R-1.Nov 27, 2024 · N14230 · Boeing 737824SDR VNAA20250102001Doubler · corrodedCORROSION ON INTERNAL PRODUCTION DOUBLER IN STA. FS= 295 TO FS= 310 BETWEEN STGR 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT. CORROSION ON INTERNAL PRODUCTION DOUBLER IN STA. FS= 295 TO FS= 310 BETWEEN STGR 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT. (E/E) WAS Nov 27, 2024 · N590NN · Cndair CL6002D24SDR DALA2024120311422Drain Mast · corrodedCORROSION FOUND ON FUSELAGE AT MATING SURFACE OF AFT HEATED DRAIN MAST. CEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0462:3833-2001/004 00521 REPAIRED PER ER/A 622287-14 PRI REV 0, ER/A 595615-14 REV B PRI REV 1, REVNov 27, 2024 · N102DU · Airbus BD5001A10
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