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 SWAA2024010312903Access Panel · delaminatedDELAMINATED ACCESS PANEL 193B WING TO BODY FAIRING EXTERNAL SKIN AFT LEFT CORNER AT LOWER FUSELAGE 2023-652045<[01] TOOL USED CALIPER P/N: 700-113-10; S/N 0033174; DUE DATE: 12-MAR-24.;[02] HOT BONDER P/N HCS9200B-AV; S/N 18196127; DUE DATE: 22-JAN-24.;[03] TOOct 20, 2023 · N461WN · Boeing 7377H4SDR HNAA2023112100436Unknown · unknownE004302 PREVIOUSLY BLENDED AREA BTW FR 28-29 STGR 5R FOUND TO HAVE REMAINING LIGHTNING STRIKE DAMAGE. CUTOUT DAMAGE, AND PERFORMED DOUBLER REPAIR OF PREVIOUSLY BLENDED AREA BTW FR 28-29 STGR 5R FOUND TO HAVE REMAINING LIGHTNING STRIKE DAMAGE IAW EDT2023-145-Oct 20, 2023 · N654AE · Emb EMB145LRSDR HNAA2023112100435Unknown · unknownE004296 PREVIOUSLY BLENDED AREA AT FR 27 STGR 5R FOUND TO HAVE REMAINING LIGHTNING STRIKE DAMAGE. : CUT OUT DAMAGE, AND PERFORMED DOUBLER REPAIR ON PREVIOUSLY BLENDED AREA FOUND TO HAVE REMAINING LIGHTNING STRIKE DAMAGE AT FR 27 STGR 5R IAW ETD2023-145-02670Oct 20, 2023 · N654AE · Emb EMB145LRSDR HNAA2023112100434Unknown · unknownE004294 PREVIOUSLY BLENDED AREA AT FR 26 STGR 5R FOUND TO HAVE REMAINING LIGHTNING STRIKE DAMAGE. CUT OUT DAMAGE, AND PERFORMED DOUBLER REPAIR ON PREVIOUSLY BLENDED AREA FOUND TO HAVE REMAINING LIGHTNING STRIKE DAMAGE AT FR 26 STGR 5R IAW ETD2023-145-026709 Oct 20, 2023 · N654AE · Emb EMB145LRSDR DALA2023110509107Unknown · unknownSHIP 1807 DAMAGE PREVIOUSLY EVALUATED BY DELTA UNDER LOG 8209111. SCRATCH ON LH FUSELAGE SKIN AT STA 1538 AND STGR 35. CORRECTIVE ACTION: PERMANENT REPAIR ON LH FUSELAGE SKIN BETWEEN STA 1540 AND STGR 35 LH WAS PERFORMED PER ER/A 612712-14AD (0046915)Oct 20, 2023 · N831MH · Boeing 767432ERSDR DALA2023102408748Unknown · unknown(LOG 0026558) DENTS LOCATED APPROXIMATELY 6.6" BELOW THE FWD EDGE OF THE AFT CARGO DOOR IMMEDIATELY FORWARD OF STA 807 BETWEEN STR 25-R AND STR 27-R. DENTS REPAIRED PER ERA 602847-14.Oct 20, 2023 · N3745B · Boeing 737832SDR DALA2023102408722Unknown · unknownSHIP 1807 ERA 612712-14AD ISSUED FOR SKIN REPAIR TO STA 1540, STRINGERS 34 L - 37L, FOLLOW ON ACTION IS REQUIRED. CORRECTIVE ACTION: ACCOMPLISH ERA 612712-14AD SECTION II AT 30000 TOTAL FLIGHT CYCL ES ON THE AIRFRAME, THEN EVERY 3000 FLIGHT CYCLES THERAFTER ASOct 20, 2023 · N831MH · Boeing 767432ERSDR DALA2023102308703Unknown · unknownELONGATED AND CRACKED HOLES ON FUSELAGE SKIN AT STA Y=1178 PROJECTION OF SPAR 14L IN REF NRC 00086. SUMMARY OF NRC 00123: DAMAGE IN HOLES ON FUSELAGE SKIN AT STA Y=1178 PROJECTION OF SPAR 14L WAS REPAIRED PER B717-200 SRM 53-03- 01-2R REPAIR I. PAR. 6 J. FIG. Oct 20, 2023 · N979AT · Boeing 717200SDR SWIA2024032601019Skin · damagedDAMAGE ON LT SIDE OF FUSELAGE BETWEEN FS 349 AND FS 364 AND BETWEEN STRG 16L AND STGR 14L AND ON STRGR 15L. DAMAGE MEASURES 6" IN DIAMETER 3" BELOW STGR 14L AND 6.5" FWD OF FS 364.0. DAMAGE MEASURES .125" DEEP AT DEEPEST POINT WITH 2 SHEARED RIVETS ON STGR 15LOct 19, 2023 · N744SK · Cndair CL6002C10SDR SWAA2023113012456Gusset · crackedCRACK GUSSET LOCATED BS500I AND STR19R AT FWD CARGO COMPARTMENT 2023-650013<[01] REPLACED GUSSET AND FASTENERS LOCATED BS500I AND STR19R AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02 SRM 51-10-02 Ï¿½TEM 9; AND DRAWING # 143A7902 REV : B<BR>SEE INDIVIDUAL Oct 19, 2023 · N8604K · Boeing 7378H4SDR HNAA2023112100451Unknown · unknownE003942 EXTERNAL SKIN, THERE ARE 2 PREVIOUS LIGHTNING STRIKE BLENDS AT FR24-25, ON STGR 20L-21L. CUT OUT 2 PREVIOUS LIGHTNING STRIKE BLENDS, AND PERFORMED DOUBLER REPAIR AT CENTER FUSELAGE II, EXTERNAL SKIN, AT FR24-25, ON STGR 20L-21L IAW ETD2023-145-026517Oct 19, 2023 · N654AE · Emb EMB145LRSDR ASAA2023101945851Skin · dentedREEVALUATE 1 EACH DENT AT RH FWD FUSELAGE FWD OF FWD CARGO DOOR CUTOUT BETWEEN FR 24 AND FR24A AND BETWEEN STR 31 AND STR 32 GROUNDED - YES. EVALUATED DENT LENGTH .400, WIDTH .300 DEPTH .005, NEAREST STIFTNER 1.0 D/A=.005 LOCATED BETWEEN FR24 AND FR24A AND BETOct 19, 2023 · N844VA · Airbus A320214SDR GTIA2023101937548Skin Panel · dentedDENT EXTERNAL SKIN BETWEEN FR 68-FR 69 AND STR 32 R/H TO STR 33 R/H. DAMAGE MAPPING MEASUREMENTS. LENGTH 3.495 INCHES, WIDTH 1.857 INCHES AND DEPTH 0.037 INCHES. RAF-01 3347941-01 GENERATED-PERMANENT REPAIR PERFORMED OF THE FUSELAGE SKING BETWEEN FR 68-FR 69 AOct 19, 2023 · N618NK · Airbus A320232SDR VNAA20231019002Skin · gougedTHE FUSELAGE SKIN IS GOUGED ON THE UPPER EDGE ABOVE THE AFT BAGGAGE BAY DOOR, APPROXIMATELY 1" LONG AND .013" DEEP. REPAIRED IAW EA 23-C9-53-1436 REV IR DATED 10/6/2023.Oct 19, 2023 · N610NN · Cndair CL6002D24SDR FDEA202310191778Skin · crackedSKIN CRACKED AT UPPER AFT CORNER OF #3 AIR CONDITIONING COMPARTMENT DOOR CUTOUT. REPAIRED IN REF. TO ENGINEERING AUTHORIZATION: #1-5330-T0376720; PART 1. TITLE: FUSELAGE - NO. 3 RH AIR CONDITIONING DOOR JAMB SKIN FOUND WITH CRACK IN UPPER AFT CORNER-OMISSIOOct 19, 2023 · N607FE · Doug MD11FSDR SWAA2023113011987Access Panel · delaminatedDELAMINATED ACCESS PANEL 191D AT LOWER FUSELAGE 2023-649973<[01] TOOL USED CALIPER P/N: 500-196-30; S/N B22072476; DUE DATE: 14-JUL-24.;[02] TOOL USED: THERMOGRAPHY CAMERA P/N: FLIR-T530; S/N: 79316001; DUE DATE: 23-JAN-24.;[03] TOOL USED: HOTBONDER PN: HCS920Oct 18, 2023 · N8604K · Boeing 7378H4SDR SWIA20231157018Unknown · dentedDENT DAMAGE FOUND TO RH SIDE OF THE FUSELAGE, BELOW THE FORWARD EDGE OF THE RH ENGINE, AND IN THE PRESSURE VESSEL. THE DENT IS LOCATED ON THE FUSELAGE BETWEEN FS574.00 AND FS589.00 AND BETWEEN WL 97.50 AND WL 79.50. DENT MEASURES 15€? IN WIDTH BY 12 13/16€Oct 18, 2023 · N929EV · Cndair CL6002B19SDR DALA2023110509106Unknown · unknownSHIP 1807 DAMAGE PREVIOUSLY EVALUATED BY DELTA UNDER LOG 8209109. DENT ON LH FUSELAGE SKIN AT STA1499 AND 1.500" ABOVE STGR 31. CORRECTIVE ACTION: PERMANENT REPAIR ON LH FUSELAGE SKIN AT STA1499 AD 1.500" ABOVE STGR 31, WAS PERFORMED PER ER/A 612802-14 (004490Oct 18, 2023 · N831MH · Boeing 767432ERSDR DALA2023101908635Unknown · unknownSHIP 0693 MULTIPLE DEEP SCRATCHES AND DENTED SKIN AFT OF AND BELOW AFT LEFT CABIN DOOR FOUND DURING WALKAROUND. CORRECTIVE ACTION: REF ERA 612890-14. (4509838)Oct 18, 2023 · N693DL · Boeing 757232SDR DALA2023101908631Unknown · unknownSHIP 0693 FUSELAGE SKIN / STA 1681 - STA 1701 / STR 18L - STR 19L / DENT. CORRECTIVE ACTION: REF ERA 612890-14. (0023352)Oct 18, 2023 · N693DL · Boeing 757232SDR DALA2023101908630Unknown · unknownSHIP 0668 IN REF TO: NRC 00210: AFTER REMOVE CORROSION AREA WAS FOUND AREA OUT LIMITS, STA 760 AND 780 BTW S-19R AND S-18R OF FUSELAGE SKIN. CORRECTIVE ACTION: SUMMARY OF NRC 00502: EXTERNAL FUSELAGE SKIN ON STA 760/780 BTW S-19R AND S-18R WAS REPAIRED PER ER/Oct 18, 2023 · N668DN · Boeing 757232SDR DALA2023101908629Unknown · unknownSHIP 0668 FUSELAGE / EXTERNAL SKIN / BTW STA 760 & STA 780 / BTW S18R & S19R / CORROSION. CORRECTIVE ACTION: REF ERA 612228-14. (0023603)Oct 18, 2023 · N668DN · Boeing 757232SDR DALA2023101908628Unknown · unknownSHIP 0668 DTE, 612228-14AD FUSELAGE SKIN CORROSION. CORRECTIVE ACTION: REF ERA 612228-14AD. (0023592)Oct 18, 2023 · N668DN · Boeing 757232SDR SWAA2023110111611Skin · corrodedDOT A24-3 EXTERNAL FUSELAGE SKIN CORRODED AROUND VACUUM WASTE EXHAUST PORT BETWEEN STRINGERS 22L AND 23L SATION 917.<[01] REMOVED CORROSION AND EXAMINED AREA WITH 10X MAGNIFIER I.A.W SRM 53-70-01-0L-1. NO DEFECTS FOUND.;[02] REMOVED CORROSION ; VISUALLY INSPECOct 17, 2023 · N773SA · Boeing 7377H4SDR DALA2023101808589Unknown · unknownLIGHTNING STRIKE ON EXTERNAL SKIN. 13" AFT OF FR35.3 AT STR 38R. REPAIRED LIGHTNING STRIKE ON EXTERNAL SKIN 13" AFT OF FR35.3 AT STR 38R PER A321 SRM 53-21-11-300-026. INSPECTION THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT: 60,000FC/120,000FH WHICHEVER IS ACHOct 17, 2023 · N330DX · Airbus A321211SDR DALA2023101808588Unknown · unknownDENT ON EXTERNAL FUSELAGE SKIN FR 70+9.5", 2.5" BELOW STR 24L. C/W ER/A 612633-14 REV ORIGINAL. (LP# 0021986)Oct 17, 2023 · N330DX · Airbus A321211SDR ASAA2023101646294Skin · corrodedFOUND CORROSION UNDER AFT DRAIN MAST GROUNDED - YES. REMOVED DAMAGE ORIG .063, MATERIAL LOSS .006, REMAINING .057 FOUND TO BE OUT OF LIMITS THIS IS AN EXCLUDED AREA, REF A320 SRM 53-41-11-283-065 REMOVED DAMAGE, HFEC , DVI NO DEFECTS NOTED. FABRICATED, LOCATEDOct 16, 2023 · N637VA · Airbus A320214SDR R61A2023110500607Access Panel · corrodedDURING HEAVY CHECK MAINTENANCE FOUND CFIII CORROSION FOUND ON INTERCOSTAL AT WASTE ACCESS DOOR PANEL. CORRODED WASTE DOOR INTERCOSTAL REPLACED IAW EMB 175 SRM 51-41-02.Oct 16, 2023 · N740YX · Emb ERJ170200LRSDR JJBA20231019034Unknown · unknownCRACKS SUSPECTED (13X) ON LH SKIN AROUND FASTENERS BTW FR 77-80 BTW STR 3L-9L. AFTER NDT INSPECTION, 11 CRACKS FOUND. SKIN REPAIRED WITH 11 BUSHINGSOct 16, 2023 · N16178 · Emb EMB145XRSDR JJBA20231019031Unknown · unknownCRACKS SUSPECTED (8X) ON RH SKIN AROUND FASTENERS BTW FR 77-80 BTW STR 3R-9R. SKIN REPAIRED WITH 16 BUSHINGS AND 1 REPAIR DOUBLEROct 16, 2023 · N16178 · Emb EMB145XRSDR JJBA20231018025Unknown · unknownRF1 EXT, CRACK FOUND BY NDT INSPECTION ON RH TOP SKIN AT FR 75 BTW STR 1R-3R. SKIN REPAIRED WITH A DOUBLEROct 16, 2023 · N16178 · Emb EMB145XRSDR EE4Y2023101618632Skin Panel · damagedDURING INSPECTION TASK 532180-01-2-001 TWO BURN MARKS ON FASTENER HEAD AND ONE BURN MARKON FASTENER HEAD AND ADJACENT SKIN ON STGR40LH 230MM FWD FR25 WERE FOUND. THE DAMAGES WERE REPAIRED FOLLOW THE REPAIR INSTRUCTIONS IAW A320 SRM TASK 53-21-11-300-012 FIGUREOct 16, 2023 · N281NV · Airbus A320214SDR EE4Y2023101618631Skin Panel · damagedDURING INSPECTION TASK 532180-01-2-001 TWO BURN MARKS ON FASTENER HEAD AND ONE BURN MARK ON FASTENER HEAD AND ADJACENT SKIN ON STGR43LH BETWEEN FR26 WERE FOUND. THE DAMAGES WERE REPAIRED FOLLOW THE REPAIR INSTRUCTIONS IAW A320 SRM TASK 53-21-11-300-012 FIGURE Oct 16, 2023 · N281NV · Airbus A320214SDR SWAA2023110110960Skin · corrodedLOWER EXTERNAL FUSELAGE STA.450 LBL 12'; CORROSION FOUND AROUND RADIO ALTIMETER CABLE ACCESS HOLE<[01] REMOVED CORROSION LOWER EXTERNAL FUSELAGE SKIN IAW SRM 51-10-02 ITEM 15;[02] VISUAL INSPECTED AREA WITH 10X MAGNIFYNG GLASS IAW SRM 51-10-02 ITEM 15;[03] STEOct 14, 2023 · N773SA · Boeing 7377H4SDR SWAA2023101710942Beam · crackedINNER SKIN CRACKED AFT SIDE 20.5 INCHES FROM BOTTOM. REMOVED FRAME PER SRM 51-40-02 2.P/N 141A6120-6 AND IT SHOULD BE P/N 141A6121-7. LOCATED NEW BEAM PER SRM 51-40-05. 3. INSTALLED NEW BEAM P/N 141A6121-7 PER SRM 51-40-02. 4. INSPECTED WORK ABOVE 5.C/WOct 14, 2023 · N245WN · Boeing 7377H4SDR AALA202310179767Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: COSSOROIN ON FUSELAGE SKIN AROUND AFT LAVATORY VENT AT BS 917, FROM S21L TO S 22L. REPAIRED SKIN PER SRM 53-70-01-2R-3.Oct 14, 2023 · N931AN · Boeing 737823SDR EE4Y2023101418623Skin Panel · corrodedDURING THE STRUCTURAL INSPECTION PER ALLEGIANT WORK CARD 05-000-002, AFT LAVATORY VENT OUTLETSKIN EXTERNAL EXISTING REPAIR IAW A320 SRM 53-41-11-300-004 WITH CORROSION WAS FOUND. DUE THE DAMAGE IS BEYOND SRM LIMITS AIRBUS WAS CONTACTED REQUESTING REPAIR INSTRUOct 14, 2023 · N335NV · Airbus A319111SDR I5EA2023101400001Unknown · unknownCRACK ON FUSELAGE STA 727+6 STR 10R. REPAIRED FUSELAGE SKIN AT STA 727+6 STR 10R IAW BOEING MESSAGE SFW-SFW 23-0162-07B.Oct 14, 2023 · N545CC · Boeing 73748ESDR 2023F00313Skin · dentedCUTOUT OIL CANNED AREA (1.25" DIAMETER) ON L/H AFT FUSELAGE SKIN EXTERIOR BETWEEN FS 967 AND FS 986.5 AND STR 24L AND STR 25L IAW AERO DESIGN SERVICES EO #ADS-N467TW-01 REVISION IR DATED 02/OCT/2023. ACCOMPLISHED HFEC NDT INSPECTION AROUND CUTOUT AREA WITH NO Oct 13, 2023 · N467TW · Boeing 737200SDR VNAA202311290021Skin · corrodedCORROSION ON DOOR SILL BTW FS517.00 TO FS565.00 AT SURROUND STRUCTURE FWD CARGO DOOR. CORROSION ON DOOR SILL BTW FS517.00 TO FS565.00 AT SURROUND STRUCTURE FWD CARGO DOOR WAS REMOVED PER EA 23-C9-53-1536 REV. IROct 12, 2023 · N556NN · Cndair CL6002D24SDR VNAA202311290017Skin · dentedSEVERAL DENTS (2EAS) ON FUSELAGE SKIN SETTLEMENT AREA OF VENTRAL FIN FAIRING LH. SEVERAL DENTS (2EAS) ON FUSELAGE SKIN SETTLEMENT AREA OF VENTRAL FIN FAIRING LH WERE REPAIRED PER EA 23-C9-53-1542 REV. IROct 12, 2023 · N556NN · Cndair CL6002D24SDR VNAA20231125003Skin · scratchedSCRATCH BTW FS230.00 TO FS234.00 AND STGR#21 TO STGR#20 LH SIDE FWD FUSELAGE. SCRATCH BTW FS230.00 TO FS234.00 AND STGR#21 TO STGR#20 LH SIDE FWD FUSELAGE WAS REPAIRED PER EA 23-C9-53-1555 REV.IR SECTION III - PERMANENT REPAIROct 12, 2023 · N557NN · Cndair CL6002D24SDR DALA2023103008886Unknown · unknownSHIP 1807 EXTERNAL SKIN WITH PROTUDING DENT BETWEEN STA 1329 AND 1351 &S- 35L AND S34L. CORRECTIVE ACTION: EXTERNAL SKIN, STA 1329 AND 1351, STGR 35L AND 34L WAS REPAIRED I.A.W B767-400 SRM 53-00-01-2R- 29. ALSO INTERVAL INSPECTION 9.000 FC EXTERNAL DETAIL INSOct 12, 2023 · N831MH · Boeing 767432ERSDR AALA202310244025Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON BILGE AREA SKIN INNER SURFACE, FROM STA 807 TO STA 827, S27R TO S26R. REPAIRED SKIN PER EA 348767.Oct 12, 2023 · N304RB · Boeing 737823SDR AALA202310249522Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON BILGE AREA SKIN INNER SURFACE, FROM STA 847 TO STA 867, S27R TO S26R. REPAIRED SKIN PER EA 348767.Oct 12, 2023 · N304RB · Boeing 737823SDR DALA2023101308425Unknown · unknownSHIP 3157 NICK EXTERNAL SKIN LOCATED BTW FR 2 TO FR 3 AND 8 INCH BELOW OF LH S IDE STRINGER AT LOWER FUSELAGE. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN LOCATED BTW FR2 TO FR3 AND 8 INCHBELOW OF LH SIDE STRINGER AT LOWER FUSELAGE AS PER A3Oct 12, 2023 · N357NB · Airbus A319114SDR SWIA20231227011Unknown · crackedFORWARD EQUIPMENT COMPARTMENT, L/H SIDE, FLOOR WEB IS CRACKED AT FS193, MARKED. (C-CHECK RO 12/23/2023) CRACK CONFIRMED OUT OF LIMIT PER REO 670-53-11-509 REV E DATED 2018-02-08. COMPLIED WITH REO 670-53-11-1899 REV-- DATED 2023-11-02. CUT AWAY DAMAGE WEBOct 11, 2023 · N743SK · Cndair CL6002C10SDR VNAA202311280010Skin · corrodedCORROSION ON INTERNAL SKIN CUT OUT, DOOR SURROUND STRUCTURE, MAIN AVIONIC COMPARTMENT. CORROSION ON INTERNAL SKIN CUT OUT, DOOR SURROUND STRUCTURE, MAIN AVIONIC COMPARTMENT WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND WAS REPAIRED PER REO 690-53-21-032Oct 11, 2023 · N556NN · Cndair CL6002D24SDR VNAA202311280008Skin · nickedSEVERAL NICKS BTW FS225.00 TO FS 265.00 AND BTW STGR#25 LH TO STGR#25 RH EXTERNAL FUSELAGE. NICKS BTW FS225.00 TO FS 265.00 AND BTW STGR#25 LH TO STGR#25 RH EXTERNAL FUSELAGE WERE BLENDED OUT PER REO 690-53-11-1627 REV. --Oct 11, 2023 · N556NN · Cndair CL6002D24SDR SWAA2023103109837Doubler · crackedEXTERNAL GROUND POWER DOOR CUTOUT LOWER DOUBLER SKIN CRACKED; MISSING A PIECE OF SKIN<[01] ACCOMPLISH EXTERNAL GROUND POWER DOOR CUTOUT LOWER DOUBLER SKIN REPAIR AS PER SRM 53-10-15-2R-4 AND BOEING DRAWING#141A8701.;[02] VERIFIED STEP 1;[03] ACCOMPLISHED EXTEROct 11, 2023 · N8622A · Boeing 7378H4
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