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 HNAA2024072600577Skin · dented53-2013 DENT ON FUSE SKIN AT FR21 STR16L. REPAIRED IAW EO1-53-24-0353May 23, 2024 · N637AE · Emb EMB145LRSDR AALA202405240210Doubler · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT PHONE ANTENNA INTERNAL DOUBLER PLATE BETWEEN FR 63 AND FR 64, BETWEEN S41R AND S42R. REPLACED DOUBLER PLATE PER EA 354103.May 23, 2024 · N757UW · Airbus A319112SDR FDEA202405230721Doubler · chafedLOWER FORWARD CARGO COMPARTMENT DOOR CUT OUT FORWARD JAMB LOWER EDGE DOUBLER FOUND WITH CHAFE, LONGERON 38R - LONGERON 42R AT STATION 895. LOWER FORWARD CARGO COMPARTMENT DOOR CUTOUT FORWARD JAMB LOWER EDGE DOUBLER LONGERON 38R - LONGERON 42R AT STATION 89May 23, 2024 · N615FE · Doug MD11FSDR FDEA202405230720Skin · chafedLOWER FORWARD CARGO COMPARTMENT DOOR CUT OUT AFT JAMB LOWER EDGE DOUBLER FOUND WITH CHAFE, STATION 1002.3,LONGERON 39-42 RIGHT HAND SIDE. LOWER FORWARD CARGO COMPARTMENT DOOR CUTOUT AFT JAMB LOWER EDGE DOUBLER WORK ACCOMPLISHED AS PER EA # 1-5330-T0308423CMay 23, 2024 · N615FE · Doug MD11FSDR SWI2024F111101Skin · gougedGOUGE DAMAGE LOCATED ON FS1144.00 AT STR9 (R/H) (C-CHECK RO 8/22/2024) REPAIRED DAMAGE ON FS1144.00 AT STR9 (R/H) IAW REO 670-53-61-2296 REV-- DATE 2024-08-07, CRJ700 SRM 53-61-06, 51-40-11, 51-21-11, 51-25-06, 51-25-16, 51-42-06, AMM 29-11-11, 20-70-00May 22, 2024 · N754SK · Cndair CL6002C10SDR SWIA2024080500607Repair · gougedGOUGE ON EXISTING REPAIR DOUBLER AT FS977 AT STR27 (C-CHECK RO 7/24/2024) REMOVED AND REPLACED EXISTING REPAIR DOUBLER AT FS 977 AT STR27 IAW REO 670-53-00-290 REV-F DATE 2019-04-26 AND SRM 51-23-03. LEAK CHECK GOOD.May 22, 2024 · N716EV · Cndair CL6002C10SDR COEA2024072609917Skin · dentedWO 254917 NR 200105 HEAVY CHECK COE/MAJOR REPAIR DISCREPANCY: R/H EXTERNAL FUSELAGE BETWEEN FRAMES 19-20 AT STRINGER 11R HAS A DENT. CORRECTIVE ACTION: REPAIRED PER SRAS ES_00240251_01...23669 ISSUE A, DATED 6/28/2024.May 22, 2024 · N917FX · Aerosp ATR42300SDR HNAA2024070500508Skin · gougedE038958 CARGO FR-70 BETWEEN STGRS 12R/13R IS GOUGED AT PREVIOUS REPAIR. REPAIRED CARGO FR 70 BTW STR 12R-13R GOUGE AT PREVIOUS REPAIR IAW EO1-53-24-0394 AND ETD2018-145-123916 REV A.May 22, 2024 · N649PP · Emb EMB145LRSDR SWAA2024052388704Doubler · crackedEXTERNAL POWER DOOR FRAME DOUBLER LOOSE/BROKEN<[01] PERFORMED EA 24-153-01378May 22, 2024 · N8327A · Boeing 7378H4SDR DALA2024052205414Skin · dentedDENT ON FUSELAGE SKIN STA 205, 1" ABOVE LONGERON 17L WITH DIMENSIONS AS A FOLLOW D (WIDTH)=1.300, X (DEPTH)=0.110, D/X=11.81 IS OUT OF LIMITS PER B717 SRM 53-01-01-1A, PROCEDURE 3 ALLOWABLE DAMAGE 3 PAR 4. C CONDITION 1B. SUMMARY OF NRC 00388: PREVIOUS REPAIR May 22, 2024 · N974AT · Boeing 717200SDR MK1Y2024052200383Skin · damagedSMALL HOLE AND DEFORMED SKIN FOUND ON FUSELAGE UPPER SKIN, L/H SIDE, BETWEEN STA 1890 AND STA 1898May 22, 2024 · N437CM · Boeing 767330SDR MK1Y2024052200382Skin · damagedFOUND MULTIPLE NICKS, SCRATCHES AND BLEND OUTS ON FUSELAGE EXTERNAL SKIN, BETWEEN STA 1351 AND STA 1373, BETWEEN STR 21R AND STR 23R.May 22, 2024 · N437CM · Boeing 767330SDR MK1Y2024052200381Skin · damagedFOUND MULTIPLE NICKS, GOUGES AND SCRATCHES ON FUSELAGE SKIN AT SEC 45, BETWEEN STA 1395 AND STA 1417, BETWEEN STR 28L AND STR 33L.May 22, 2024 · N437CM · Boeing 767330SDR MK1Y2024052200377Skin · damagedFOUND SEVERAL BLEND OUTS ON FUSELAGE SKIN BETWEEN STA 287 AND STA 303, BETWEEN STR 35L AND STR 57L.May 22, 2024 · N437CM · Boeing 767330SDR MK1Y2024052200376Skin · damagedFOUND SEVERAL BLEND OUTS ON FUSELAGE SKIN BETWEEN STA 610 AND STA 632, BETWEEN STR 21R AND STA 26R.May 22, 2024 · N437CM · Boeing 767330SDR DALA2024052305481Skin · damagedAIRCRAFT 3903, LIGHTNING STRIKE DAMAGE TO THE FUSELAGE SKIN (P/N: 141A3810-36) JUST AFT OF THE STA 178 PRESSURE BULKHEAD AND BETWEEN RBL 20 AND RBL 30. CORRECTIVE ACTION: OVERSIZE/REAMED THE SUBJECT HOLE TO REMOVE THE DISCHARGE DAMAGE, COMMON TO THE SKIN ONLY May 21, 2024 · N903DN · Boeing 737990ERSDR DALA2024052305437Skin · damagedAIRCRAFT 3903, LIGHTNING STRIKE AFT OF STA 178 BETWEEN RBL 20 AND RBL 30. CORRECTIVE ACTION: REMOVED FASTENER NEXT TO LIGHTING STRIKE PER B737 SRM 51-40-00. REMOVED 13 RIVETS TO ALLOW FOR SKIN SEPARATION REMOVED DAMAGE WITH A .875" CUTOUT PER STEP 2. OF PRI 61May 21, 2024 · N903DN · Boeing 737990ERSDR JJBA20240522051Skin · crackedRH EXTERNAL FUSELAGE, BTW FRAME 77-80 AND BTW STR 3R-9R, CRACKS (6X) FOUND AROUND FASTENERS. 4 BUSHINGS REPAIRS AND A REPAIR DOUBLER ON RH REAR FUSELAGE II SKIN, BTW FR 77 & 79 AND BTW STR 3R-7RMay 21, 2024 · N21197 · Emb EMB145XRSDR JR2R202405212137Skin · corrodedFUSELAGE SKIN UNDER FWD CARGO DOOR CUT-OUT COOORDED IN MULTIPLE PLACES. REPAIREDMay 21, 2024 · N89342 · Emb ERJ170200LRSDR SWIA20240520Skin · crackedLEFT SIDE JUST BELOW TRU BAY VERY AFT CORNER IS A VISIBLE CRACK.(MARKED) (C-CHECK RO 8/22/2024) REMOVED AND INSTALLED NEW L/H TRU NOSE SKIN REF-CRJ700 SRM 51-42-06-001-001 A01 REV 38 DATE JUL-25-2020,DWG CC670-33040 REV.-G, REO 670-53-11-1983 REV -- DATMay 20, 2024 · N758SK · Cndair CL6002C10SDR SCNA20240702260Access Panel · wornPERFORMED PERMANENT CATEGORY A REPAIR ON CENTER SECTION LOWER CHORD I/B FLANGE FROM STA 543.250" TO STA 565.250" RBL 40" I/A/W SUN COUNTRY A. ENGINEERING AUTHORIZATION 53-0204 REV. 00, AND SRM 57-10-13-2R-3 REPAIR 3 TABLE 201 FIGURE 201 AND 202. NOTE: ALSO REMay 20, 2024 · N8011A · Boeing 7378SDR CALA2024052401588Skin · crackedDURING NDT PROCEDURE AS PER PART 6, 51-00-16. IT WAS FOUND A CRACK HOLE AT STA 340 AND STGR 20R ON THE FORWARD SERVICE DOOR CUTOUT AFT LOWER CORNER. GENERATE UPDATE TO ATTACH IMAGES FROM THE DAMAGED HOLE AND CHANGE THE ATTRIBUTES TO MAJOR REPAIR AND SDR.May 20, 2024 · N655UA · Boeing 767322SDR CALA2024052401584Skin · corrodedDURING ACCOMPLISHMENT OF NR:1896678 WAS FOUND CORROSION IN THE INTERNAL FUSELAGE SKIN PANEL LOCATED BTW STA. 1562/1582 AND STGR 24/25 LH SIDE. FOR REFERENCE SEE: SRM 53-60-01-0I-1.May 20, 2024 · N655UA · Boeing 767322SDR SWIA2024052300020Skin · dentedPERFORM REWORK ON DENTED AREA ON LH SIDE OF FWD FUSELAGE BETWEEN FR 21 - FR 22 AND STGR16 -SGTR 17 IN REFERENCE TO ERJ175 SRM 51-75-00. (FILED CLOSED)PERFORMED REWORK ON DENTED AREA ON LH SIDE OF FWD FUSELAGE BETWEEN FR 21 - FR 22 AND STGR16 -SGTR 17 IN REFEREMay 20, 2024 · N282SY · Emb ERJ170200LLSDR CALA2024052201556Skin · damagedDURING INSPECTION AT 321BL; 322AL & 323AL LH UPPER SKIN B.L 0.0 AT SEC 48 BS 1582 TO BS 1654; WAS FOUND SKIN WITH SCRATCHES AND NICK. NECESSARY EVALUATION PROCESS. SEE IMAGES FOR FUTHER DETAILS. 7245 PART 1.A AND PART 1.B. THIS REPAIR IS A CATEGORY ''''B'''' RMay 20, 2024 · N655UA · Boeing 767322SDR DALA2024052105410Skin · damagedAIRCRAFT 3903, ERA 618146-14 REV ORIG REPAIR TO FUSELAGE SKIN LIGHTNING STRIKE AT STA190 RBL 10 HAS FOLLOW ON ACTIONS. CORRECTIVE ACTION: DAMAGE TOLERANCE ANALYSIS (DTA)STAGE III ADDITIONAL APPROVAL REQUIRED TO OPERATE BEYOND 24 MONTHS FROM SECTION I INSTALL. May 20, 2024 · N903DN · Boeing 737990ERSDR DALA2024052105379Skin · crackedCRACK ON FUSELAGE SKIN LOCATED Y=1022 AND Y=1076 ON LONGERON L-14R. SUMMARY OF NRC 00164: FUSELAGE SKIN LOCATED Y=1022 AND Y=1076 ON LONGERON L-14R WAS REPAIRED PER ER/A 617295-14 REV O, SECTION I: PERMANENT REPAIR. PERFORM SECTION II: REPETITIVE INSPECTIONS WMay 20, 2024 · N974AT · Boeing 717200SDR DALA2024052105378Skin · crackedCRACK ON FUSELAGE SKIN LOCATED Y=1087 BETWEEN L-13 AND LONGERON L-14R. SUMMARY OF NRC 00165: FUSELAGE SKIN LOCATED Y=1087 BETWEEN L-13 AND LONGERON L-14R WAS REPAIRED PER ER/A 617295-14 REV O, SECTION I: PERMANENT REPAIR. PERFORM SECTION II: REPETITIVE INSPECTMay 20, 2024 · N974AT · Boeing 717200SDR DALA2026030301463Skin · damagedFOUND LIGHTNING STRIKE IN BETWEEN FR 21 AND FR 22 24" LEFT OF RADIO ALT. H.I.T. DIMENSION 66MM/11MM "363 SQMM". INSPECTED LIGHTNING STRIKE AND CRITERIA MEETS A350 ASR 53-00-61-01001-661A-A. REPAIR CARRIED OUT AS PER ASR A350-53-11-61-09002- -664A-A REV 78. (LPMay 19, 2024 · N574DZ · Airbus A350941SDR SWAA2024062587817Gusset · crackedFWD CARGO COMP STA 500D STR 19R GUSSET CRACK. REMOVED AND REPLACED GUSSET AT FWD CARGO COMP STA 500D STR 19R AS PER SRM 51-40-02-0G-0 & DWG 143A9481.May 19, 2024 · N464WN · Boeing 7377H4SDR DALA2024052205424Skin · damagedAIRCRAFT 5004, AIRCRAFT 5004, UPON ARRIVAL INTO SEA, THE A/C EXPERIENCED HEAT DAMAGE DUE TO ELECTRICAL ARCING NEAR THE POWER RECEPTACLE DOOR. FUSELAGE SKIN BETWEEN FRAMES 6 THRU 8 AROUND GROUND POWER PANEL INCURRED HEAT DAMAGE FROM ELECTRICAL FIRE. CORRECTIVE May 19, 2024 · N504DZ · Airbus A321271NXSDR DALA2024052005368Skin · damagedSHIP 3331 DAMAGE FOUND ON ARRIVAL: FWD SIDE OF AFT CARGO DOOR SURROUNDING SKIN. CORRECTIVE ACTION: COMPLIED WITH A330 SRM 53-41-11-283-001. CONTINUE IN SERVICE. (5273513)May 19, 2024 · N831NW · Airbus A330302SDR DALA2024052005366Skin · damagedSHIP 3331 FWD SKIN AFT CARGO DOOR CUT OUT DAMAGE. CORRECTIVE ACTION: COMPLIED WITH ERA 61815121-14. CONTINUE. (5273514)May 19, 2024 · N831NW · Airbus A330302SDR DALA2024052005365Skin · damagedSHIP 3331 DAMAGE FOUND ON ARRIVAL: FWD SIDE OF AFT CARGO DOOR SURROUNDING SKIN. CORRECTIVE ACTION: COMPLIED WITH ERA 618151-14 REV 3 AND ERA 618151-14 REV ORG. (0350128)May 19, 2024 · N831NW · Airbus A330302SDR SWIA2024080500018Skin · gougedMULTIPLE GOUGES IN THE EXTERNAL FUSELAGE SKIN AT FS1031.0 AND STR22RH JUST AFT OF THE EXTERNAL GROUND AIR SOURCE PANEL GOUGES ARE LOCATED IN ORANGE FLAGGED BOXED AREA (C-CHECK RO 7/24/2024) REPAIRED DAMAGE ON EXTERNAL SKIN AT FS1031.0 AND STR22RH JUSTMay 18, 2024 · N716EV · Cndair CL6002C10SDR JR2R20240518603Skin · dentedDENT ON FUSELAGE SKIN NEAR RH ICE DET AT FR4 AND STR10R. REPAIRMay 18, 2024 · N85340 · Emb ERJ170200LRSDR SWIA20240517Skin · scratchedFOUND SCRATCHES/CHAFING ON FUSELAGE SKIN DORSAL FIN 321AT TRANS#28248712 (C-CHECK RO 8/22/2024) REMOVED DAMAGE ON FUSELAGE SKIN UNDER DORSAL FIN 321AT REF REO 670-53-00-731 REV -- DATED 2024-07-13. ALL CHECKS GOOD. COMPLIED WITH TASK CARD 51-900-1002-SKMay 17, 2024 · N758SK · Cndair CL6002C10SDR COEA2024072605917Skin · corrodedWO 254917 NR 200071 HEAVY CHECK COE/MAJOR REPAIR DISCREPANCY: INTERNAL FUSELAGE ABOVE STRINGER 6R BETWEEN FRAMES 20-21 HAS LEVEL 2 CORROSION UNDER INSULATION STANDOFF. CORRECTIVE ACTION: REPAIR PER ATR42 SRM 530000-300-803-A01.May 17, 2024 · N917FX · Aerosp ATR42300SDR HNAA2024070500501Skin · crackedE037054 EXTERIOR FUSELAGE RH DV WINDOW CUTOUT AFT UPPER CORNER IS CRACKED. REPAIRED CRACKED EXTERIOR FUSELAGE RH DV WINDOW CUTOUT AFT UPPER CORNER IAW PIEDMONT EO1-53-24-0335 AND EMB 145 ETD2024-145-013969May 17, 2024 · N649PP · Emb EMB145LRSDR SWAA2024062487257Bear Strap · crackedR-1 DOOR CUTOUT SKIN STA 312 4' BELOW STR 8R CRACK AROUND FASTENER HOLE<[01] ACCOMPLISHED R1 DOOR SKIN BEAR STRAP REPAIR BETWEEN STA 291-328 STR 7R-10R REF SRM 51-40-05-0G-0 AND SRM 53-10-01-2R-6;[02] 'DAMAGE REPAIRED PER 737-700 SRM 53-10-01-2R-6 (REPAIR 6) FMay 17, 2024 · N464WN · Boeing 7377H4SDR R61A2024061000249Doubler · corrodedINTERNAL DOUBLER FOR WASTE SERVICE DOOR CUTOUT CORRODED AT LOWER IB CORNER. REMOVED AND REPLACED WASTE BOX INTERNAL DOUBLER BETWEEN FRAMES 88-89 AND RESTORED SURFACE PROTECTION TO REWORKED AREA REFER SRM 51-40-08, 51-23-06 AND CPM 51-25-00.May 17, 2024 · N127HQ · Emb ERJ170200LRSDR DALA2024052005350Skin · damagedSHIP 3102 LIGHTNING STRIKE FOUND ON FASTENER ON FR 14 AT 2 O-CLOCK. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON AFFECTED HOLE LOC. FR14 AND AT 11 INCH BELOW OF UPPER STRG LH SIDE AS PER A319 SRM 53-11-11-300-035. (0347535)May 17, 2024 · N302NB · Airbus A319114SDR DALA2024051905324Skin · corrodedAIRCRAFT 3723, DURING ROUTINE INSPECTIONS, CORROSION DAMAGE WAS FOUND ON THE FUSELAGE SKIN (P/N 141A3521-11) AT APPROX. BS 357, ABOVE STR 28L. ADDITIONALLY, CORROSION DAMAGE WAS FOUND ON THE SPLICE STRAP (PN 141A3523-14) AT BS 360, ABOVE STR 28L, ADJACENT TO TMay 17, 2024 · N393DA · Boeing 737832SDR JR2R20240517222Skin · corrodedFUSELAGE SKIN BELOW THE FWD CARGO DOOR CUT-OUT CORRODED IN MULTIPLE LOCATIONS. REPAIREDMay 17, 2024 · N85340 · Emb ERJ170200LRSDR EE4Y2024051720187Skin Panel · dentedDURING ACCOMPLISHMENT OF THE ALLEGIANT TASK 51-000-001 , DENT ON UPPER EXTERNAL REAR FUSELAGE AT FR 78+315MM BETWEEN STGR 2R - 3R WAS FOUND.THE PERMANENT REPAIR REPAIR WAS PERFORMED IAW A320 SRM 53-51-11-300-002 PARAG 2 A FIG 001 SHEET 001 REV 148 DTD 02-01-20May 17, 2024 · N205NV · Airbus A320214SDR DALA2024051705298Doubler · damagedMISSING MATERIAL IN ONE HOLE WAS FOUND AT INNER DOUBLER. SUMMARY OF NRC 00583: AREA WAS REPAIRED PER ER/A 617844-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-617844 ADDED FOR AC 9560. (LP #0346414)May 17, 2024 · N983AT · Boeing 717200SDR ASAA2024051651594Doubler · corrodedINTERNAL DOUBLER INSIDE CUTOUT FOR SERVICE DOOR 312AR IS CORRODED GROUNDED - YES. REMOVED CORROSION ON 5EA. AREAS ON INTERNAL DOUBLER AROUND DOOR 312AR CUTOUT-FOUND AREA TO BE OUT OF LIMITS, NO LIMITS FOUND IN SRM. ORIGINAL THICKNESS .055", REMOVED .028", REMAMay 16, 2024 · N854VA · Airbus A320214SDR IPXA2024062810799Skin · damagedMDC DOOR AFT MIDDLE FUSELAGE SKIN WITH DAMAGE REMOVED NEGLIGIBLE SURFACE DISCREPANCY BY HAND WITH SCOTCH BRITE THAT WAS NOTED IN PAINT SURFACE ONLY IAW SRM 51-73-11 AND NO MATERIAL LOSS WAS NOTED. OK TO TREAT AND PRIME. RESTORED SURFACE PROTECTION IAW SRM 51-2May 16, 2024 · N127UP · Airbus A300F4622RSDR SWAA2024062486573Doubler · crackedFOUND POWER RECEPTACLE DOUBLER CRACKED AT STA 235.8 ZONE 1<[01] VERIFIED WORKMANSHIP AND CONFORMITY.;[02] REMOVED AND REPLACE EGPR INNER DOUBLER AT STA 219.8-STA 244 STGR 19R-STGR 24R AS PER SRM 51-40-02-0G-0 AND DWG #'S 141A3702 AND 141A0640.;[03] VERIFIED STMay 16, 2024 · N464WN · Boeing 7377H4SDR DALA2024052105374Skin · damagedSHIP 190 ER/A 566238-14AD REV A ISSUES FOR REPAIR TO CENTER UPPER NG SKIN AT STA 955 LBL 85. CORRECTIVE ACTION: DTE, ER/A 566238-14AD REV A. DTA REQUIRED NO LATER THAN 12MAY25. DAMAGE TOLERANCE ANALYSIS REQUIRED. (0346059)May 16, 2024 · N190DN · Boeing 767332
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