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 VNAA20251004022Skin · damagedPREVIOUS REWORK (3EA) BTW STGR 20R TO 18R AND FS 385, FS 427, FS 453 AT EXTERNAL FUSELAGE . EA) BTW STGR 20R TO 18R AND FS 453 AT EXTERNAL FUSELAGE WAS REPLACED PER CRJ900 SRM 53-00-00-201-003-A03Aug 28, 2024 · N550NN · Bombdr CL6002D15SDR VNAA20251004021Skin · damagedPREVIOUS REWORK (2EA) BTW STGR 22L TO 20L AND FS 596, FS 606 AT EXTERNAL FUSELAGE. PREVIOUS REWORK (2EA) BTW STGR 22L TO 20L AND FS 596, FS 606 AT EXTERNAL FUSELAGE WERE EVALUATED PER CRJ900 SRM 53-31-01-101-003-A04 AND REPAIRED PER REO 690-53-31-1071 REV.-.Aug 28, 2024 · N550NN · Bombdr CL6002D15SDR VNAA20251004020Skin · damagedPREVIOUS REWORK (4EA) BTW STGR 18L TO 17L AND FS 517, FS 563. FS 575, FS 638 AT EXTERNAL FUSELAGE FASTENERS (2 EAS) BTW STGR 18L TO 17L AND FS 563. FS 575 AT EXTERNAL FUSELAGE WERE REPLACED PER CRJ900 SRM 53-00-00-201-003-A03, PREVIOUS REWORK BTW STGR 18L TOAug 28, 2024 · N550NN · Bombdr CL6002D15SDR VNAA20251004019Skin · damagedPREVIOUS REWORK (2EA) BTW STGR 19L TO 17L AND FS 477.40 AT FWD FUSELAGE. PREVIUS REWORK (2EA) BTW STGR 19L TO 17L AND FS 477.40 AT FWD FUSELAGE WERE REPAIRED PER REO 690-53-00-636 REV - -Aug 28, 2024 · N550NN · Bombdr CL6002D15SDR VNAA20251004018Skin · crackedPREVIOUS REWORK (2EA) BTW STGR 21L TO 20L AND FS 280 TO FS 326 AT FWD FUSELAGE. REWORK BTW STGR 21L TO 20L AND FS 326 AT FWD FUSELAGE WAS REPAIRED PER REO 690-53-21-2030 REV - , AND REWORK BTW STGR 21L TO 20L AND FS 326 AT FWD FUSELAGE WAS REPAIRED WITH NRAug 28, 2024 · N550NN · Bombdr CL6002D15SDR VNAA20251004017Skin · damagedPREVIOUS REWORK (1EA) IN STGR 23L AND FS 211 AT FWD FUSELAGE. LIGHTNING STRIKE DAMAGE TO FUSELAGE SKIN BTW FS202.75 - FS280.00 AND BTW STR20L-STR23L WERE REPAIRED PER REO 670-53-11-2059 REV - -Aug 28, 2024 · N550NN · Bombdr CL6002D15SDR COEA2024121007921Skin Panel · dentedWO 256296 NR 3 HEAVY CHECK COE/MAJOR REPAIR: R/H EXTERNAL SKIN AND INTERNAL STRINGER 6R ARE DENTED BETWEEN FRAMES 20-22. CORRECTIVE ACTION: REPAIRED PER SRAS ES_00246484_01...24451 ISSUE A.Aug 28, 2024 · N921FX · Aerosp ATR42300SDR SWIA2024110828Doubler · gougedAFT LOWER SKIN DOUBLER REPAIR HAS SEVERAL GOUGES FROM WING TO BODY FAIRING (C-CHECK RO 11-6/2024) REMOVED AND REPLACED EXISTING DOUBLER REPAIR AT AFT LOWER SKIN WING TO BODY FAIRING REF REO 670-53-00-290, REV -F, DATED 2019/04/26. PRESSURE LEAK CHECK GOAug 28, 2024 · N755EV · Cndair CL6002C10SDR NACA2024082800005Skin · corrodedFUSELAGE RH SKIN EXTERIOR SURFACE CORROSION AT STA 188 AND WL 170 -220. CORROSION REMOVED IAW EO 767-53-0059 EARN N399CM-0019Aug 28, 2024 · N399CM · Boeing 767323SDR NACA2024082800004Skin · crackedOPEN HOLE HFEC INSPECTION FOUND 01 EA CRACK AT THE BOTTOM HOLE OF FORWARD SERVICE DOOR(R1) CUTOUT AFT LOWER CORNER FUSELAGE SKIN.AND THE CRACK LENGTH IS ABOUT 0.3 INCH LONG AS MARKED. REPAIRED IAW SRMAug 28, 2024 · N399CM · Boeing 767323SDR NACA2024082800003Skin · corrodedFUSELAGE SKIN EXTERIOR SURFACE CORROSION AT STA 188 TO 212 AND S-19L TO S-16L. EO 767-53-0059 BOEING RDRSJX-NAC-24-0105-11B. STAG EARN 0012 &0013Aug 28, 2024 · N399CM · Boeing 767323SDR IXXA20241003010Skin Panel · crackedFUSELAGE BS 180935 LH SIDE SKIN ABOVE HORIZ STAB, LOWER FWD HOLE SHOWS CRACK INDICATION NOTED AT 1 O'CLOCK POSITION AT BASE OF COUNTERSINK. HAECO WO 320008 NON ROUTINE 40582Aug 28, 2024 · N491AZ · Boeing 767323SDR HNAA2024100100924Plate · corrodedE052973 LAV POTABLE WATER FILL/DRAIN EXTERNAL REINFORCEMENT PLATE HAS CORROSION. REMOVED AND INSTALLED NEW LAV POTABLE WATER FILL/DRAIN EXTERNAL REINFORCEMENT PLATE IAW EMB 145 SRM 51-40-02.Aug 28, 2024 · N696AE · Emb EMB145LRSDR R61A2024091900408Doubler · corrodedWATER/WASTE DOOR EXTERNAL CUTOUT INNER FLANGE IS CORRODED AS MARKED NEAR BONDING WIRE. REMOVED AND REPLACED WASTE/WATER INNER FLANGE INTERNAL WASTE BOX DOUBLER AND REINSTALLED WASTE BOX AND SHEAR CLIPS REFER SRM 51-40-08Aug 28, 2024 · N131HQ · Emb ERJ170200LRSDR R61A2024091900407Doubler · dentedREAR FUSELAGE LOWER SKIN PANEL EXTERNAL SIDE HAS 1EA PROTRUDING DENT AT FR 98-99, STGR 29L-29R. PERFORMED REPAIR DOUBLER ON REAR FUSELAGE FR98-99 STGR 29L-29R LOWER SKIN PANEL EXTERNAL SIDE REF SRM 53-30-01/REPAIR 12PAug 28, 2024 · N131HQ · Emb ERJ170200LRSDR DALA2024082908565Doubler · mislocatedSHIP 3311 A330 / FUSELAGE SKIN / MISLOCATION OF DOUBLERS AT FR62-FR63, STGR4LH TO 4RH PER AA 4430-01016. ER/A 616527-14 REV. CORRECTIVE ACTION: COMPLIED WITH. (0526902)Aug 28, 2024 · N811NW · Airbus A330323SDR DALA2024082908549Skin · gougedAIRCRAFT 1029, SKIN PANEL BETWEEN FR51 TO FR52 STR 32L TO 43L HAS NUMEROUS GOUGES. CORRECTIVE ACTION: EVALUATED AREA IAW A321 SRM 53-41-11-283 DAMAGE FOUND WITHIN ALLOWABLE LIMITS, EXPECEPT ON SPOT AT FR 51 STR 38L OUT OF LIMITS REPAIRED IAW A321 SRM 53-00-11-Aug 28, 2024 · N129DN · Airbus A321211SDR DALA2024082908548Skin · ground damageAIRCRAFT 3062, INCURRED DAMAGE FROM CONTACT WITH GSE EQUIPMENT WHILE OVERNIGHT IN MIA. THE FUSELAGE SKIN IS DENTED AND GOUGED BETWEEN FR 30 AND FR 33 AND BETWEEN STRINGERS 26L AND 27L. DAMAGE CONSISTS OF FOUR (4) DENTS AND TWO (2) GOUGES. CORRECTIVE ACTION: COAug 28, 2024 · N362DN · Airbus A321213SDR YENA2024082901181Skin · dentedDURING HEAVY MAINTENANCE: DENT ON EXTERNAL SKIN BTW FR 28 AND FR 29 STRG 37L-38L; (RESOLVED ON W/O: 1313885 TASKCARD: NR-00052) PERFORMED PERMANENT REPAIR LOC. ON EXTERNAL SKIN BTW FR 28 AND FR 29 STRG 37L-38L IAW A320 SRM 53-21-11-300-093, THIS REPAIR IS CLASAug 28, 2024 · N706JB · Airbus A320232SDR YENA2024082901179Skin · damagedDURING HEAVY MAINTENANCE, TAIL CONE, FR 80-84 BOTH RT & LT SIDES, APU AIR INTAKE DUCT, THIS PERMANENT REPAIR HAS BEEN APPROVED VIA REF /3/RDAF AND IS CLASSIFIED AS MAJOR.(E/C: A24-1107-01)Aug 28, 2024 · N706JB · Airbus A320232SDR FDEA202408281181Skin · damagedEXTERIOR FUSELAGE, ZONE 100, LIGHTNING STRIKE AT F.S. 654+110 TO 654+115, S37R. MEASURED ORIGINAL THICKNESS AT .085 AND REMAINING AT .067 FOR A DIFFERENCE OF .018 REMOVED, PER 767 NDTM PART 4 51- 00-10 PROCEDURE 2. BLEND FOUND TO BE OUT OF LIMITS EXCEEDS 15Aug 28, 2024 · N287FE · Boeing 7673S2FSDR JR2R202408287061Doubler · corrodedANTENNA CUTOUT DOUBLER AND 2 INTERCOSTALS CORRODEDAug 28, 2024 · N86309 · Emb ERJ170200LRSDR SWI2024F01187Skin · corrodedINNER CLOSING SKIN HAS CORROSION IN MULTIPLE AREAS FS536.00 - 578.00 STGR25L. (MARKED IN RED) (C-CHECK RO 11-6/2024) REMOVED CORROSION FROM INNER CLOSING SKIN IN MULTIPLE AREAS FS536.00 - 578.00 STGR25L PER CRJ700 SRM 51-21-06-001-001-A01 AND FOUND TO BAug 27, 2024 · N755EV · Cndair CL6002C10SDR NACA2024082700002Skin · crackedOPEN HOLE HFEC INSPECTION FOUND 02 EA CRACKS AT TWO BOTTOM HOLES OF FORWARD ENTRY DOOR(L1) CUTOUT AFT LOWER CORNER FUSELAGE SKIN.AND THE CRACK LENGTH IS ABOUT 0.1 INCH AND 0.3 INCH LONG AS MARKED. REPAIRED IAW SRMAug 27, 2024 · N399CM · Boeing 767323SDR NACA2024082700001Skin · crackedWHILE PERFORMING A DVI FOR AN UNRELATED EO, FOUND A 7/8 INCH FUSELAGE SKIN CRACK BELOW STR 22L AND BS 7278+2 3/8, CONFIRMED WITH EDDY CURRENT. ACCOMPLISHED EO 737-53-0360, REFERENCE ATTACHED PROJECT WORKSHEET.Aug 27, 2024 · N403YK · Boeing 737436SDR CALA2024090302357Skin · crackedEC/RA NO.: 5311-02101 REV. - CRACK INDICATION IN HOLE NO. 2 AT 6 O''CLOCK POSITION IN THE AFT SKIN LAYER AT FRAME 35 AND 10 CM FO RWARD STGR 30 LH, ON HAECO LCQ NR 9298721, PER PART 2A OF THE LATEST REVISION OF ECRA 5331-03113 ON OR COMES FIRST. PERFORM REPEAAug 27, 2024 · N830UA · Airbus A319131SDR CALA2024082900508Skin · corrodedFOUND CORROSION ON EXT. SKIN LOCATED UNDERNEATH LAVATORY SERVICE PAN. SEE L/P 9032982.ADDED PICS.ADDED MORE PICS. REMOVED CORROSION FROM SKIN AROUND EXTERIOR LAV PAN OPENING. LOCATION IS FROM STA. 847 TO STA 867 AND BETWEEN STR. 24L AND STR. 25L. FWD BLENDAug 27, 2024 · N14237 · Boeing 737824SDR SWAA2024100730584Bear Strap · crackedCRACK INDICATION ON BEAR STRAP FORWARD GALLEY DOOR BS 290-296 BETWEEN S-8R AND S-9R AT PASSENGER CABIN.CRACK LENGTH 4.125 IN. 2024-533434<[01] TOOL USED ON STEP 7 AND 8 ET EQUIPMENT: P/N: NORTEC 600D; S/N: 220272512; CAL DUE DATE: 08-JAN-25;[02] STEP 9. EDDY CAug 26, 2024 · N266WN · Boeing 7377H4SDR CALA2024091602431Skin · dentedRH AFT FUSELAGE AT FRAME 63 & STR 31R, HAS A DENT. MPLISH INSPECTION REQUIREMENTS PER PART 2 OF LATEST REVISION OF AIRCRAFT FLIGHT CYCLES (FH NOT RELEVANT). ACCOMPLISH REPEAT INS EC/RA 5341-01466 ON OR BEFORE THE AIRCRAFT REACHING 39,907 TOTAL PECTIONS EVERY 6Aug 26, 2024 · N435UA · Airbus A320232SDR HNAA2024091200818Doubler · mechanic error53-2524 - TOOL MARK ON REAR FUSELAGE UPPER SKIN AT FRAME 75 AND LH STR #2. REPAIRED IAW SRM 53-31-01 & EO1-53-24-0515.Aug 26, 2024 · N686AE · Emb EMB145LRSDR SWAA2024090331577Skin · perforatedREPLACE NOSE RADOME DUE TO FOUND PERFORATED SKIN 2024-454693<[01] REPLACED NOSE RADOME IAW B737-700 AMM 53-52-00-000-801 AND AMM 53-52-00-400-801 <BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] TASK COMPLETED <BR>REPLACED NOSE RADOME IAW B737-700 AMM 53-52-00-000-801 AAug 26, 2024 · N487WN · Boeing 7377H4SDR IPXA2024082764213Skin · damagedCREW ENTRY DOOR CUTOUT, INTERNAL LINNING HAS MATERIAL LOSE. DOT 28-01. (RO-28)Aug 26, 2024 · N402UP · Boeing 75724APFSDR HNAA2024100100889Skin · corrodedE052290 AFT FUSELAGE 1, ON THE LOWER EDGE OF THE CARGO DOOR CUT OUT THERE IS CORROSION. AT FR 65-66, STGR 16L-17L. REMOVED AND REPLACED AFT FUSELAGE1 CARGO DOOR CUTOUT LOWER CENTER SILL IAW EMB145 SRM 51-40-02.Aug 25, 2024 · N696AE · Emb EMB145LRSDR SCNA20240920320Skin · damagedWORK ORDER A1P190 JOB 2 ITEM 70: PERFORMED FUSELAGE SKIN REPAIR BETWEEN STA 440 AND STA480, S-4R AND S-6R DUE TO LIGHTNING STRIKE IAW COOPESA EO# C00-EO-2024-20839 R01 DATED 9/07/2024.Aug 25, 2024 · N819SY · Boeing 73786NSDR SCNA20240920319Skin · damagedWORK ORDER A1P190 JOB 2: UPPER FUSELAGE, EXTERNAL SKIN SECTION AT STA 500+3 AND 1.5 INCH BELOW STR-4R SKIN LAP JOINT WITH LIGHTNING STRIKE. PERFORMED FUSELAGE SKIN BLEND REPAIRS DUE TO LIGHTNING STRIKE DAMAGES AT THREE LOCATIONS BETWEEN STA 460 AND 500A, S-Aug 25, 2024 · N819SY · Boeing 73786NSDR SCNA20240920318Skin · damagedWORK ORDER A1P190 JOB 2 ITEM 71: UPPER FUESLAGE, EXTERNAL SKIN SECTION AT STA 481 AND 1.750 INCH BELOW STR-4R SKIN WITH LIGHTNING STRIKE. - - - WORK PERFORMED: PERFORMED FUSELAGE SKIN BLEND REPAIRS DUE TO LIGHTNING STRIKE. DAMAGES AT THREE LOCATIONS BETWEENSTAAug 25, 2024 · N819SY · Boeing 73786NSDR SCNA20240920317Skin · damagedWORK ORDER A1P190 JOB 2 ITEM 73: UPPER FUSELAGE, EXTERNAL SKIN SECTION AT STA 500 + 12 AND 1.5 INCH BELOW STR-4R SKIN LAP JOINT WITH LIGHTNING STRIKE. - - WORK PERFORMED: PERFORMED FUSELAGE SKIN BLEND REPAIRS DUE TO LIGHTNING STRIKE DAMAGES AT THREE LOCATIONS Aug 25, 2024 · N819SY · Boeing 73786NSDR SCNA20240920316Skin · damagedUPPER FUSELAGE EXTERNAL SKIN SECTION AT STA 203 AND WL243 SKIN WITH LIGHTNING STRIKE (RHS) - - WORK PERFORMED: PERFORMED FUSELAGE SKIN FREEZE PLUG REPAIR BETWEEN STA200 AND STA210, WL240 AND WL250, RBL30 AND RBL40 (DETAIL A) IAW COOPESA EO# C00-EO-2024-20832-RAug 25, 2024 · N819SY · Boeing 73786NSDR SCNA20240920315Skin · damagedUPPER FUSELAGE, EXTERNAL SKIN SECTION AT STA 233 AND WL 265 (RBL 40) SKIN WITH LIGHTNING STRIKE. - - WORK PERFORMED: PERFORMED FUSELAGE SKIN FREEZE PLUG REPAIR BETWEEN STA 230 AND STA 250, WL260 AND WL270, RBL30 AND RBL40 (DETAIL B) IAW COOPESA EO #000-EO-2024Aug 25, 2024 · N819SY · Boeing 73786NSDR CALA2024090302343Skin · corrodedCORROSION UNDER AND AROUND WITH FASTENER HEADS PULLING THROUGH AFT LAX SERVICE PAN / FUSELAGE SKIN LOWER SIDE AT STA 1560 10110 REPIRED PER AMES DOCUMENT 47627REA01 AND UNITED DOCUMENT EC/RA 5 300-03133 ESFR 1037086 REF NR 173733-0100-0041Aug 25, 2024 · N73860 · Boeing 75733NSDR FDEA202408251171Skin · damagedEXTERIOR FUSELAGE, ZONE 100, LIGHTNING STRIKE AT F.S. 541 BETWEEN S39R AND S39L. EXTERIOR FUSELAGE, ZONE 100, LIGHTNING STRIKE AT F.S. 541 BETWEEN S39R AND S39L, FUSELAGE SKIN DOUBLER REPAIR PERFORMED IAW SRM 53-00-01-2R REPAIR 10. MAJOR REPAIR.Aug 25, 2024 · N287FE · Boeing 7673S2FSDR IPXA2024082635620Skin · corrodedEVIDENCE OF 2 PULLED RIVETS AND CORROSION FORWARD OF VHF ANTENNA AT 6 O CLOCK POSITION UNDER AFT CARGO. RESTORED FINISHES PER AMM 51-21-10.Aug 24, 2024 · N470UP · Boeing 75724APFSDR FDEA202408241170Skin · ground damageDURING TOWING OF THE AIRCRAFT INTO THE HANGAR 8.2, TAIL LH SIDE OF FUSELAGE STA 1768.80 TO STA 1787.45 STRINGER 20L MADE CONTACT WITH THE TAIL STAND. ACCMPLISHED REPAIR IAW EA 757-5380-16-A3665 SECTION 48 - FUSELAGE STA 1768 TO STA 1787.5 S-19L TO S-20L LAAug 24, 2024 · N785FD · Boeing 757222SDR R61A2024091000396Doubler · corrodedWHILE IN HEAVY CHECK - FUSELAGE SKIN WASTE BOX DOUBLER HAS CORROSION FRAME 88-89 STRINGER 25R-28R, DISCOVERED DURING POST REMOVAL INSPECTION OF WASTE SERVICING PANEL REMOVAL. REMOVED AND REPLACED WASTE BOX INTERNAL DOUBLER BETWEEN FR 88-89 STGR 25R-28R. REF Aug 23, 2024 · N105HQ · Emb ERJ170200LRSDR VNAA20251005014Skin · damagedCRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.62% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DATUM. RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.62% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DATUAug 22, 2024 · N550NN · Bombdr CL6002D15SDR VNAA20251005013Skin · crackedDISCREPANCY: CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.62% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DATUM. LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.62% STGR DATUM TO STGR DATUM TO 67.5% REAug 22, 2024 · N550NN · Bombdr CL6002D15SDR SWIA2024091600822Panel · puncturedPANEL 151 BZ FOUND WITH PUNCTURE IN ONE SPOT. (C-CHECK RO 9/15/2024) PANEL 151 BZ HAS BEEN REPAIRED REF EO# CL600-2D24-21-L08161, REV.IR, DATED 8/25/24. COMPLIED WITH 51-900-1002-SKY. SEE CONTINUATION SHEET FOR DETAILS.Aug 22, 2024 · N693CA · Cndair CL6002D24SDR DALA2024082308412Skin · damagedAIRCRAFT 9550, LIGHTNING STRIKES ON SKIN STA Y=256, 229 AND BTW RH LONGERONS 15/16 AT EXTERNAL FUSELAGE. CORRECTIVE ACTION: SKIN STA Y=256, 229 AND BTW RH LONGERONS 15/16 AT EXTERNAL FUSELAGE WAS REPAIRED PER. PRI 619580-14 REV. 4 AND ER/A 619580-14AD REV. ORIAug 22, 2024 · N717JL · Boeing 717200SDR NACA2024082100002Skin · scratchedFOUND RH LOWER AFT FUSELAGE SCRATCH AT STA1351 - STA1373 & S-28R TO S-29R. CORROSION REMOVED IAW SRMAug 21, 2024 · N399CM · Boeing 767323SDR SWIA202409270002Skin · dentedADM #N613CZ-7545 - REAR FUSELAGE BETWEEN FR 98 - 99 AND BETWEEN STRINGER 23L - 25L. DENT MEASURING L= .530" X W = .530" X H .004 W/H = 132. PLEASE EVALUATE DENT AND RECONTOUR TO ORIGINAL FORM. (C-CHECK RO 9/26/2024) AFTER FURTHER EVALUATION ON REAR Aug 21, 2024 · N613CZ · Emb ERJ170200LR
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