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 SWI2023F00288Unknown · gougedLOWER FUSELAGE SKIN AT TCAS ANTENNA LOCATION BETWEEN FS295.00 AND FS310.00 HAS NUMEROUS GOUGES (C-CHECK RO 8/31/2023) REMOVED AND INSTALLED REPAIR FILLER AND EXTERNAL DOUBLER REF. REO 670-53-21-2298 REV. -- DATED 2023-07-03. FILLET SEALED OUTER DOUBLERJun 23, 2023 · N738SK · Cndair CL6002C10SDR SWI2023F00146Unknown · damagedFUSELAGE SKIN SPLICE @ FS 755 BETWEEN STR20L AND STR20R, PN 601R210303-1 IS DAMAGED AND REQUIRES REPLACEMENT. (FILED CLOSED)FUSELAGE SKIN SPLICE @ FS 755 BETWEEN STR20L AND STR20R, PN 601R210303-1 REMOVED. FABRICATED NEW SKIN SPLICE SAME AS ORIGINAL PN 601R210Jun 23, 2023 · N449SW · Cndair CL6002B19SDR SWI2023F00139Unknown · damagedFUSELAGE SKIN SPLICE @ FS 755 BETWEEN STR20L AND STR20R, PN 601R210303-1 IS DAMAGED AND REQUIRES REPLACEMENT. (FILED OPEN)FUSELAGE SKIN SPLICE @ FS 755 BETWEEN STR20L AND STR20R, PN 601R210303-1 REMOVED. FABRICATED NEW SKIN SPLICE SAME AS ORIGINAL PN 601R21030Jun 23, 2023 · N449SW · Cndair CL6002B19SDR DALA2023062905221Unknown · unknownFUSELAGE LWR SKIN / BETWEEN Y-175 AND STR 41R, FR20 AND FR21 / GOUGE DAMAGE. DTE ERA 604884-14 REV A MONITOR LOG REQUIRES STAGE 3 DTA APPROVAL BY 66000 CYCLES AFTER SECTION I REPAIR. DAMAGE TOLERANCE AND FATIGUE REVIEW. ASSOCIATED ER/A 00-604884 ADDED FOR AC 1Jun 23, 2023 · N102DN · Airbus A321211SDR DALA2023062605114Unknown · unknown(LOG 2830670) LOCATED PREVIOUS BLENDOUT AT FUSELAGE SKIN STA 500A-500B, STR 22-21R. REPAIRED PREVIOUS BLENDOUT AREA OF FUSELAGE SKIN STA 500A-500B, STR 22-21R PER DELTA ERA 609136-14 REV ORIGINAL.Jun 23, 2023 · N937DM · Boeing 7379SDR 2023FA0000337Shield · chafedINNER STINGER SKIN DAMAGE TO L/H SKIN P/N 6912640-20 AND R/H SKIN 6912640-24, REF ENGINEERING MEMO DQ40101M1.Jun 23, 2023 · N662QS · Cessna 680ASDR SWI2023F00301Unknown · crackedWHILE PREPARING TO REMOVE FWD LATCH BEARING PAD C-CHANNEL ON JOB 71019591 OP 250 CAMP #26779522, FOUND CRACK IN INNER SKIN UNDER ADJACENT ZED- STIFFENER. (C-CHECK RO 8/31/2023) COMPLIED WITH REO #670-54-21-1562 REV (--) 2023-07-03 STEPS 1-16. WET-INSJun 22, 2023 · N738SK · Cndair CL6002C10SDR AALA202308143940Access Door · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LOWER FUSELAGE ACCESS DOOR 312AR INTERNAL STRUCTURE. REPLACED ACCESS DOOR PER AMM 52-41-16-400-001-A.Jun 22, 2023 · N712US · Airbus A319112SDR Y2PA2023080823043Skin Panel · dentedDURING A TAIL-STRIKE INSPECTION IN KYIP, C.A.S. MAINTENANCE FOUND THE APB WEB DENTED AND CRACKED, L=20” W=58” DEPTH=0.050” AT F.S 1334-1338. MAINTENANCE IN KYIP PERFORMED THE DAMAGE CUTOUT OF THE APB SKIN, MAINTENANCE PERFORMED A HFEC INSPECTION AND VERIFIEDJun 22, 2023 · N834US · Doug MD88SDR Y2PA2023080823040Skin · damagedDURING A TAIL-STRIKE INSPECTION IN KYIP, MAINTENANCE FOUND THE SKIN IS GROUND OFF BETWEEN F.S. 1331-1338, BETWEEN L29L AND L29R. MAINTENANCE IN KYIP REMOVED AND CUT OUT DAMAGED SKIN BETWEEN F.S. 1331-1338, L29L- L29R, MAINTENANCE PERFORMED A HFEC INSPECTIONJun 22, 2023 · N834US · Doug MD88SDR Y2PA2023080823038Skin · dentedDURING A TAIL-STRIKE INSPECTION IN KYIP, C.A.S. MAINTENANCE FOUND THE SKIN GROUND DOWN AND DENTED BETWEEN L29L-L29R AT F.S. 1338-1363. MAINTENANCE IN KYIP PERFORMED CUTOUT OF DAMAGED AREA, MAINTENANCE PERFORMED A HFEC INSPECTION OF THE AREA AND VERIFIED NOJun 22, 2023 · N834US · Doug MD88SDR Y2PA2023080823037Skin · pilot errorDURING A TAIL-STRIKE INSPECTION IN KYIP, C.A.S. MAINTENANCE FOUND A DRAG MARK ON THE FUSELAGE SKIN AT APPROXIMATELY F.S. 1322 L30, AND THE SKIN GOUGED BETWEEN F.S. 1334 TO 1338, L29L – L29R. MAINTENANCE IN KYIP PERFORMED A HFEC INSPECTION OF THE DAMAGE AREA AJun 22, 2023 · N834US · Doug MD88SDR DALA2023062305080Unknown · unknownREPAIR DOUBLER LOCATED AT THE AFT CARGO DOOR-AFT FRAME (FS 994 AND STR 26R) IS DAMAGED ON THE EXTERIOR SURFACE. SUMMARY OF NRC 00477: REPAIR DOUBLER LOCATED AT THE AFT CARGO DOOR AFT-FRAME (FS 994 AND STR 26R) WAS REPLACED PER B717-200 SRM 53-20-15-2R PRODECURJun 22, 2023 · N919AT · Boeing 717200SDR VNAA202307290002Doubler · chafedREPAIR DOUBLER CHAFED FS 982.00 STR 27Jun 21, 2023 · N502AE · Cndair CL6002C10SDR DALA2023062205073Unknown · unknownSHIP 663 DTE, ERA 609687-14, MONITOR INSPECTION LOG REPAIR TO FUSELAGE SKIN BETWEEN BS 650-661 AND STRINGERS 25L-27L. CORRECTIVE ACTION: REF ERA 609687-14. (2827876)Jun 21, 2023 · N663DN · Boeing 757232SDR REXA2022062200391Skin · corroded"MINOR CORROSION AROUND FASTENERS ON FWD CARGO DOOR SURROUNDING STRUCTURE AT FS 517.00 AND 565.00 STGR 26L REMOVED .004"" MATERIAL MAX. FROM A NOMINAL THICKNESS OF .080"" ON FWD CARGO DOOR SURROUND CLOSING SKIN P/N SH690-33778-7, BETWEEN STR 24L AND STR 25L, FJun 21, 2023 · N181PQ · Cndair CL6002D24SDR DALA2023062105026Unknown · unknownCORROSION AROUND SETTLEMENT AREA OF VOR/LOC ANTENNA PANELS UPPER LH (2L), LOWER LH (1L), UPPER RH (2R), AND LOWER RH (1R). SUMMARY IN REF NRC 00403: LEVEL CORROSION 2. SETTLEMENT AREA OF VOR/LOC ANTENNA PANELS UPPER LH (2L), LOWER LH (1L), UPPER RH (2R), AND LJun 21, 2023 · N919AT · Boeing 717200SDR DALA2023062605106Unknown · unknown(LOG 2826389) DURING INSTALLATIONS, CORROSION WAS FOUND ON THE EXTERNAL SURFACE OF THE FUSELAGE CROWN UPPER SKIN (PN 146A3101-38), UNDER #2 ADF ANTENNA BETWEEN APPROX. BS 727+18 AND BS 727A+16, STR S-1 AND S-2R, AROUND NUTPLATE FASTENER HOLES. MAINTENANCE REPAJun 20, 2023 · N939DG · Boeing 7379SDR DALA2023062605105Unknown · unknown(LOG 2826336) CORROSION FOUND UNDER THE #1 ADF ANTENNA BETWEEN BS 679 TO 701, S-1 TO S-2R. REPAIRED CORROSION PER ERA 609547-14.Jun 20, 2023 · N939DG · Boeing 7379SDR DALA2023062605104Unknown · unknown(LOG 2825815) DURING MAINTENANCE INSPECTIONS, A DEEP DENT WAS FOUND COMMON TO THE FUSELAGE SKIN AT APPROX. BS 497, S-25L. REPAIRED DAMAGE PER ERA 609404-14.Jun 20, 2023 · N939DG · Boeing 7379SDR DALA2023062205078Unknown · unknown(LOG 2826334) LOWER CHORD AT UPPER HORIZONTAL BEAM CRACKED AT STRINGER 5A BETWEEN BS 1138 AND BS 1156 AT UPPER SIDE OF OPENING FOR HORIZONTAL STABILIZER. REPAIRED DAMAGE PER ERA 609790-14 REV ORIGINAL.Jun 20, 2023 · N939DG · Boeing 7379SDR DALA2023062205077Unknown · unknown(LOG 2826298) SKIN DENT DAMAGE BS500+18 BELOW STR 25L. REPAIRED IAW ER/A 609404-14 REV ORIGINAL.Jun 20, 2023 · N939DG · Boeing 7379SDR DALA2023062105042Unknown · unknown(LOG 2826403) LH FUSELAGE TO VERTICAL STAB CLOSURE ANGLE IS CHAFED. REMOVED AND REPLACED LH FUSELAGE TO VERTICAL STAB CLOSURE ANGLE IAW 737-800 SRM 51-40-02-OG.Jun 20, 2023 · N378DA · Boeing 737832SDR DALA2023062005003Unknown · unknownTOOL MARKS ON CUSP WEB STA Y=255 AND LBL=46 APROX AT PAX CABIN (W1). SUMMARY OF NRC 00430: CUSP WEB STA Y=255 AND LBL=46 WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIG.219. (LP #2825205)Jun 20, 2023 · N957AT · Boeing 717200SDR SWAA2023071760757Skin · corrodedSPOTTY SKIN CORROSION; BS1050 -1088; BETWEEN SKATE ANGLE AND AFT LEFT VERTICAL FIN FWD SUPPORT ANGLE<[01] SEVERAL AREAS OF CORROSION ON THE ANGLE AT BS 1036 FROM STR2R-STR2L FOUND TO BE OUT OF LIMITS DUE TO NO SRM ALLOWABLE DAMAGE IAW SRM 51-10-02 PAR 9C;[02] Jun 19, 2023 · N417WN · Boeing 7377H4SDR FDEA202306181056Skin · damagedFOUND DAMAGE TO THE A/C SKIN ON THE LH SIDE, BEHIND THE STATIC PORT/RVSM CONTROLLED AREA, AND BELOW THE OUTFLOW VALVE. INSTALLED ALL REPAIR PART ON AIRCRAFT IAW SRM 53-00-01-2R.Jun 18, 2023 · N574FE · Doug MD11FSDR AALA202308076936Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT INTERNAL FUSELAGE SKIN BETWEEN FR 56 AND FR 57, BETWEEN S42L AND S43L. REPAIRED SKIN PER EA 346076 AND SRM 53-00-11-300-013.Jun 17, 2023 · N673AW · Airbus A320232SDR SWAA2023071260273Bear Strap · wornFWD ENTRY DOORWAY BEAR STRAP HAS WEAR FROM DOOR FRAME CONTACT IN CLOSED POSITION. LOCATED APPROX. 2' FWD OF AFT LOWER LATCH FITTING; 1.2' LONG AND .037' AT DEEPEST POINT. MRKD<[01] REMOVED FASTENERS TO FACILITATE DAMAGE REMOVAL. BLENDED DAMAGE TO 20 TO 1RATIO Jun 17, 2023 · N8615E · Boeing 7378H4SDR CALA2023061901925Skin · scratchedSCRATCH AT AFT FUSELAGE SECTION 48AFT BETWEEN STA 2064.5 TO 2105.5 STRINGERS BETWEEN S23R TO S28R AREA L 46" X W 1/2" X Y0,056" APPROX. L 46? X W 1/2? MAX. A 3? SECTION OF THE SCRATCH HAS DAMAGES IDENTIFIED AND NO VISIBLE MOISTURE. CLEANED SURFACE AND FIBER DAJun 17, 2023 · N29977 · Boeing 7879SDR FDEA202306171045Skin · burnedEXTERIOR FUSELAGE SKIN HAS LIGHTNING STRIKE DAMAGE AT STA 1547 BETWEEN S23R & S24R EVALUATED LIGHTNING STRIKE @ STA 1547 BETWEEN S23R & S24R MATL LOSS .010 MATL REMAINING .030 ORIGINAL MATL .040 FOUND TO BE OUT OF LIMITS PER BAC DWG 146N3430 REV - & B757 SRJun 17, 2023 · N934FD · Boeing 757200SDR AALA202306190997Skin · wornAIRCRAFT IN BASE MAINTENANCE: FUSELAGE SKIN FOR EXTERNAL POWER DOOR CUTOUT HAS WEAR DAMAGE AT LOWER AREA, LOCATED FROM BS 224 TO BS 235 AT S19R. REPAIRED SKIN PER SRM 53-10-15-2R-4.Jun 17, 2023 · N909AN · Boeing 737823SDR DALA2023061804946Unknown · unknownAIRCRAFT 3353, CORROSION FLOOR BEAM YC1 LOCATED FR72 TO FR73 AT AFT GALLEY AREA (SSI 534159-01-2). CORRECTIVE ACTION: REPLACED FLOOR BEAM YC1 AND FASTENERS LOC BETWEEN FR73 AND FR74 ON AFT GALLEY AREA. (LP 2821357)Jun 17, 2023 · N853NW · Airbus A330223SDR DALA2023061804945Unknown · unknownAIRCRAFT 3353, CORROSION FLOOR BEAM YC FR73 TO FR74 AT AFT GALLEY AREA (SSI 534159-01-2). CORRECTIVE ACTION: REPLACED FLOOR BEAM YC, COUPLING (2 E/A) AND FASTENERS LOC BETWEEN FR73 AND FR74 ON AFT GALLEY AREA. (LP 2821351)Jun 17, 2023 · N853NW · Airbus A330223SDR CALA2023061901912Skin · damagedB767-06-3-7083 - FUSELAGE SKIN HAS LIGHTNING STRIKE AT BS654+44-BS654+66 BTW S22R / S23R TRANSFER REF HXWO 1839295 AND ORIGINATED BY EMP V896888 FUSELAGE SKIN AT STA654+44 TO STA654+66 BETWEEN STR22R-23R WORK ACCOMPLISHED BY MECHANIC V897549 INSPECTED BY V8963Jun 16, 2023 · N649UA · Boeing 767322SDR CALA2023061901910Skin · crackedCRACK INDICATION FOUND ON FUSELAGE SKIN AT BS 1629 PLUS 4 INCHES AND 0.250 INCHES BELOW STR 14R. CRACK LENGTH = 0.600 INCHES APPR OX. REFER TO AEROMAN NON ROUTINE 2023-318032. PO.2022 12424400101, ALUMINIUM SHEET 7075-T6 0.050 INCH PO WHICHEVER COMES LAST. REPJun 16, 2023 · N672UA · Boeing 767322SDR DALA2023061904989Unknown · unknownSHIP 3123 PULLED EXTERNAL SKIN FASTENERS LOCATED BETWEEN FR24 TO FR35 AND FROM STR32L TO STR18L AT LOWER FUSELAGE. CORRRECTIVE ACTION: REPAIRED PER A319 SRM 53-21-11. (2820168)Jun 16, 2023 · N323NB · Airbus A319114SDR DALA2023061904988Unknown · unknownSHIP 3123 PULLED EXTERNAL SKIN FASTENERS LOCATED BETWEEN FR12 TO FR24 AND FROM STR18R TO STR28R ON UPPER FUSELAGE. CORRECTIVE ACTION: REPAIRED PER A319 SRM 51-73-11-801. (2819818)Jun 16, 2023 · N323NB · Airbus A319114SDR DALA2023061904960Unknown · unknownLIGHTING STRIKE FOUND AT STA 106 AT LBL 5 AWAY FROM FASTENER DRILLED OUT DAMAGE TO .311 PER B717 SRM 53-02-01-2R REPAIR 1. BHEC INSPECTED OPEN HOLE PER B717 SRM 53-02-01-2R REPAIR 1 WITH NO DEFECTS NOTED. FABRICATED, LOCATED. AND DRILLED REPAIR DOUBLER IAW B71Jun 16, 2023 · N993AT · Boeing 717200SDR DALA2023061604903Unknown · unknownLIGHTING STRIKE FOUND AT STA 1189 AT RBL 2 AT A FASTENER. LIGHTING STRIKE STA 1189 FOUND TO BE OUT OF LIMITS PER B717 SRM 53-01-01-A1 PROCEDURE 2. CUTOUT DAMAGE, FABRICATED, LOCATED, AND DRILLED REPAIR DOUBLER AND FILLER IAW B717 SRM 53-00-00-2R-2. TREATED ANDJun 16, 2023 · N993AT · Boeing 717200SDR SWAA2023081459502Gusset · crackedFWD CARGO COMPARTMENT R/H SIDE WALL GUSSET CRACKED @ S-19R STA 500D<[01] REMOVED AND REPLACED R/H SIDE GUSSET AT STA 500D STR 19R PER B737-700 SRM 51-40-02-0G-0 AND DRAWING 143A7902;[02] VERIFIED 1.;[03] VERIFIED REMOVAL OF RH SIDE GUSSET ON STEP #1;[04] CERTIJun 15, 2023 · N444WN · Boeing 7377H4SDR SWAA2023081459501Gusset · crackedFWD CARGO COMPARTMENT L/H SIDE WALL GUSSET CRACKED @ S-19L STA 500D<[01] COMPLETED INSTALLATION FWD CARGO COMP. LEFT SIDE GUSSET ASSY STA 500D STR 19L PER B737-700 SRM 51-40-02-0G-0 AND DRAWING 143A7902. (PERFORMED BY. E.G # 1184)Jun 15, 2023 · N444WN · Boeing 7377H4SDR SWAA2023071059771Stringer · crackedCRACK STRINGER 26L ON BS 540 AT FWD CARGO COMPARTMENT 2023-378952<[01] TOOL USED P/N 45MG; S/N 221860711; DUE DATE 07/NOV/23;[02] TOOL USED: EDDY CURRENT EQUIPMENT; PN: NORTEC 600D; SN: 200048001; DUE DATE: 01-MAY-24;[03] TOOLS USED: TEMPERATURE CONTROLLER: P/Jun 15, 2023 · N298WN · Boeing 7377H4SDR SWAA2023071059079Gusset · crackedCRACK GUSSET LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT 2023-378927<[01] REPLACED GUSSET LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT IAW B737-700 SRM: 51-10-02 ITEM 9 AND 51-40-02.;[02] CORRECTED STEP 1 REPLACED GUSSET LOCATED BS500D AND STR19L FWD CAJun 14, 2023 · N298WN · Boeing 7377H4SDR SWAA2023071059078Gusset · crackedCRACK GUSSET LOCATED BS500D AND STR19R FWD CARGO COMPARTMENT 2023-378928<[01] REPLACED GUSSET AND FASTENERS LOCATED BS500D AND STR19R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 DWG 143A7902 SHEET 209 REV. -. SEE INDIVIDUAL SIGN OFFJun 14, 2023 · N298WN · Boeing 7377H4SDR IXXA2023071002Skin · crackedR1 DOOR CUTOUT AFT LOWER CORNER CRACKEDJun 14, 2023 · N409AZ · Boeing 7673P6SDR IXXA2023071001Skin · crackedL1 DOOR CUTOUT AFT LOWER CORNER CRACKEDJun 14, 2023 · N409AZ · Boeing 7673P6SDR DALA2023092107765Unknown · unknownSHIP 3323 FOUND 1X LIGHTNING STRIKE ON RIVET FR11 BETWEEN STRINGER 43/44. CORRECTIVE ACTION: PERFORMED TERMINATING ACTION ON RIVET AT FR 11 BETWEEN STRINGERS 43-44(LT), BY REMOVED HI-LOC, CLEANED UP HOLE DAMAGE, INSTALLED NEW HI LOC, IAW A330 SRM 51-42-11 AND Jun 13, 2023 · N823NW · Airbus A330302SDR DALA2023092107764Unknown · unknownSHIP 3323 FOUND LIGHTNING STRIKE ON RIVET FR12A BETWEEN STRINGER43/44. CORRECTIVE ACTION: REMOVED RIVET. OVERSIZED HOLE TO REMOVE DAMAGE PER A330-SRM 53-11-11. PERFORMED HFEC OPEN HOLE INSPECTION. NO CRACK INDICATION. INSTALLED SOLID RIVET PER A330-SRM 53-11-1Jun 13, 2023 · N823NW · Airbus A330302SDR JJBA20230705005Unknown · unknownCORROSION SUSPECTED ON REAR FUSELAGE I LH LATERAL SKIN INNER SURFACE BTW FRAME 60 & 61 AT STR 19L. SPLICE REPAIR ON LH REAR FUSE 1 STRINGER 19L, BTW FR 60-62Jun 13, 2023 · N14177 · Emb EMB145XRSDR VNAA202306230013Skin · dentedSEVERAL DENTS ON FUSELAGE SKIN (18 LH AND 13 RH), SETTLEMNT AREA OF LEFT AND RIGTH VENTRAL FIN FAIRING BTW FS 1069.75 TO REAR SPAR DATUM STABILIZER 67.5%, BTW STGR 22LH TO STGR 21LH. SEVERAL DENTS ON FUSELAGE SKIN (18 LH AND 13 RH), SETTLEMNT AREA OF LEFT AJun 12, 2023 · N551NN · Cndair CL6002D24
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