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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR SWAA2025010978781Doubler · crackedEGPR SURROUND DOUBLER IS CRACKED BS233 WL175 8' ABOVE S-24R MARKED<[01] TRIMMED; FABRICATED PARTS AND REPAIRED THE EGPR SURROUND DOUBLER BS233 WL175 8' ABOVE S-24R IAW SRM 53-10-15-2R-4 REPAIR 4 PARG 4(B-M) AND SRM 51-40-02-0G-0SDR DALA2025010600128Skin · dentedSHIP 672 DTE, ER/A 493505-14AD REV B REQUIRES STAGE 3 DTA APPROVAL AND AM OCS TO AD 2020-01-18, 2019-07-04, AND 2018-18-07. FUSELAGE / SKIN / STA 1716, BETWEEN STR 20R & S-21R / DENT. CORRECTIVE ACTION: REF ERA 493505-14ADSDR JJBA20241223053Skin · dentedFF2, DENT FOUND ON SKIN UNDER EXTERNAL POWER RECEPTACLE ACCESS PANEL BTW FR 6-7 ON LH SIDE. FF2, ON SKIN UNDER EXTERNAL POWER RECEPTACLE ACCESS PANEL BTW FR 6-7 ON LH SIDE, DENT FOUND OUT OF LIMMIT. FF2, SKIN UNDER EXTERNAL POWER RECEPTACLE ACCESS PANEL BTW FRSDR GTIA2024121938606Skin Panel · damagedPENETRATION DAMAGE FOUND ON CROWN SKIN @ FRAME 50-51 STRINGER 1L. RAF-01 3597812-01.--SDR GTIA2024121938605Skin · corrodedBURN MARK & CORROSION FOUND ON CROWN SKIN AT FRAME 52-53 AND STRINGERS 3R-3L. RAF-01 3553178-01.--SDR CALA2024121803105Skin · damagedSKIN, R2 DOOR CUTOUT REPAIR - INTERIM REPAIR TO THE FUSELAGE SKIN R2 DOOR CUTOUT TOOLING DAMAGE AT FORWARD LOWER CORNER NEAR BS 962, S17R WAS ACCOMPLISHED PER EC/RA 5331-03138 - PART 1 AT GYR. WORK ACCOMPLISHED PER ECRA 5331-03138 MAJOR REPAIR TO LP NON-ROUTSDR WRXR20241217003Skin · dentedDURING ROUTINE OPERATIONS AT (CVG), MAINTENANCE NOTED THAT THE RH, AFT STRUCTURE (P/N WA670-30632-3) HAS (1 EA.) LIGHTNING STRIKE. POST BLEND, THE DAMAGE HAS BEEN MEASURED AT 0.0015” DEEP (REO 670-53-84-167). COMPLIED WITH EA 23-C7-53-1115; PERFORM A DETAILED SDR SWIA20250311216Skin · gougedFWD FUSELAGE LOWER SKIN GOUGED AS MARKED BETWEEN FRAMES 21-22 STRINGER 27L. (C-CHECK RO 1/9/2025) CUT AWAY DAMAGE ON FWD FUSELAGE LOWER SKIN BETWEEN FRAMES 21-22 STRINGER 27L. FABRICATED AND INSTALLED DOUBLER REPAIR PER ETD. REF: ETD2024-170-033341 RESDR VNAA202501210011Skin · wornWEAR ON INTERNAL FUSELAGE SKIN, SETTLEMENT AREA OF AVIONICS COMPARTMENT DOOR. (E/E). WEAR ON INTERNAL FUSELAGE SKIN, SETTLEMENT AREA OF AVIONICS COMPARTMENT DOOR. (E/E). WAS REPAIRED PER REO 690-53-21-032 REV. ••SDR SWAA2025012078304Support Angle · crackedCRACK ANGLE - SUPPORT BS 867 AND STRINGER 26L AFT CARGO COMPARTMENT 2024-763321<[01] REPLACED ANGLE - SUPPORT BS 867 AND STRINGER 26L AFT CARGO COMPARTMENT I.A.W. B737-800 SRM 51-40-02 AND DWG 149A8102 SHEET 19 REV. A AND DWG 149A8104 SHEET 1 REV. B;[02] CORRESDR SWIA20250110216Skin · gougedFWD FUSELAGE LOWER SKIN GOUGED AS MARKED BETWEEN FRAMES 21-22 STRINGER 27L. (C-CHECK RO 1/9/2025) CUT AWAY DAMAGE ON FWD FUSELAGE LOWER SKIN BETWEEN FRAMES 21-22 STRINGER 27L. FABRICATED AND INSTALLED DOUBLER REPAIR PER ETD. REF: ETD2024-170-033341 RESDR DALA2024122011880Skin · damagedREF STEP #7 OF AA WORK CARD 4430-01018-02D, FOUND SEVEN HOLES ELONGATED AND ONE WITH TOOLING DAMAGE NEXT TO HOLE. COMPLIED WITH ER/A622841-14 REV ORIGINAL AND VERIFIED THAT IT MATCHES PRI 622841-14 REV ORIGINAL, REV 1, REV 2, REV 3, REV 4 AND REV 5. (LP# 071SDR WRXR20241216003Skin · gougedGOUGES ON FAIRING 196AR AND FIXED FAIRING SH670-36302-6. CLEANED AND EVALUATED DAMAGE IAW CRJ700 SRM 53-3-52-32-101-001-A01. SMOOTH AND BLENDED DAMAGED AREA IAW CRJ700 SRM 51-12-00-001-001-A01. REMOVED AND REPLACED 5EA. FASTENERS IAW CRJ700 SRM 51-42-00-001-00SDR WRXR20241216002Skin · gougedGOUGES ON FAIRING 195AL AND FIXED FAIRING SH670-36302-5. CLEANED AND EVALUATED PANEL 195AL IAW CRJ700 SRM 53-82-83-101-001-A01. DAMAGE FOUND TO BE MORE THAN THE 4” MAXIMUM LENGTH AND HAS WORN PAST THE COPPER MESH DOWN TO BARE COMPOSITE. SMOOTH AND BLENDED DAMASDR SWI2025F00224Skin · corrodedTHE EXTERIOR SKIN AROUND APU EXHAUST HAS FRETTING CORROSION WHERE THE APU EXHAUST SHIELD IS INSTALLED. (C-CHECK RO 2/27/2025) PERFORMED REPAIR OF EXTERIOR SKIN AROUND APU EXHAUST FRETTING CORROSION WHERE THE APU EXHAUST SHIELD IS INSTALLED REF REO 601RSDR SWI2025F00223Skin · scratchedSEVERAL SCRATCHES ON EXTERNAL SKIN UNDER FOOTPRINT OF FWD DRAIN MAST (C-CHECK RO 2/26/2025) REMOVED SEVERAL SCRATCHES ON EXTERNAL SKIN UNDER FOOTPRINT OF FWD DRAIN MAST AND PERFORMED REO 690-53-21-1854 REV -- DATE:2024-12-23. AND COMPLIED WITH TASK SDR ASAA2024121555099Doubler · crackedEGPR SURROUND DOUBLER IS CRACKED AT LOWER HINGE PAD FWD RIVET. GROUNDED - YES. REMOVED DAMAGE & REPAIRED SURROUND DOUBLER IAW B737-700 SRM 53-10-15-2R-4.SDR AALA202412189558Skin Panel · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN SKIN PANEL SURROUNDING AFT LAVATORY VENT LOCATED AT FR 70 FROM S31R TO S32R. ACCOMPLISHED SKIN REPAIR PER SRM 53-41-11 AND EA 360393.SDR JR2R20241216859Panel · dented351GL HAS DENT ON FWD SIDE OF PANELSDR N6WA2024121508Skin · dentedSMALL DENT ON RH FUSELAGE UNDER RH ENINE FS1088.2-FS1098.2 BETWEEN STGR 21R -22R. PERFORMED DOUBLER PATCH REPAIR ON RH FUSELAGE UNDER ENGINE FS1088.2- FS10982 BETWEEN STGR21R-22R IAW GOJET EO C500-53MR -038-0.SDR SWAA2025012877088Plate · crackedCRACK ON CORRUGATED PLATE LOCATED AT LEVEL IRSS 212 TRAILING EDGE AT LT WING 2024-758889<[01] REPLACED CORRUGATED PLATE LOCATED AT LEVEL IRSS 212 TRAILING EDGE AT LT WING I.A.W B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 TOOK MEASURES OF CRACK L= 1.160? TOOLSDR SWAA2024121776621Skin · crackedDURING ACCOMPLISHMENT OF 5331-I-16838-NG [TTG8Q00VM3PM]; FOUND INDICATION OF POSSIBLE CRACK AT FUSELAGE SKIN LAP SPLICE LOWER SKIN AT S-14R STA 787+6.5'. PERFORMED EA 24-153-03454 REF TTG8Q00XLL2C FOR MAINTENANCE ACCOMPLISHED.SDR SWAA2024121776620Skin · crackedDURING ACCOMPLISHMENT OF 5331-I-16838-NG [TTG8Q00VM3PM]; FOUND INDICATION OF POSSIBLE CRACK AT FUSELAGE SKIN LAP SPLICE LOWER SKIN AT S-14R STA 787+5'. PERFORMED EA 24-153-03454 FOR REPAIR.SDR DALA2024121611754Skin · not reportedSHIP 6704 REPAIR TO FUSELAGE SKIN AT STA 600-650, S-14L-19L REQUIRES MODIFICATION PER SECTION II OF ERA 510972-14AD REV A. CORRECTIVE ACTION: REF ERA 510572-14AD. (0708742)SDR SWIA202503111212Skin · corrodedCORROSION ON EXTERNAL SKIN AT TCAS ANTENNA LANDING BETWEEN FS295 TO FS310.00 STR27 (C-CHECK RO 2/18/2025) FABRICATED 1- DOUBLER 2- FILLER WITH MATERIAL 2024T3 .063" AND INSTALLED REPAIR ON EXTERNAL SKIN AT TCAS ANTENA LANDING BETWEEN FS 295.00 AND FS 3SDR AALA202503051673Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON CENTER WING UPPER SKIN PANEL, UPPER SURFACE AT FR 42, BETWEEN RIB 1 AND +Y1292.SDR AALA202502254316Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND INTERNAL SURFACE AROUND RIVET ON FR35 AT LEVEL STR30 LH SIDE, CRACK DIRECTION 9 OCLOCK.CRACK MEASURE IS L=0.236 INCH. MAINTENANCE PERFORMED TIME LIMITED REPAIR (INSTALLED BUSHING)ON HOLE W1 LOCATED INTERNAL SDR SWIA202502191212Skin · corrodedCORROSION ON EXTERNAL SKIN AT TCAS ANTENNA LANDING BETWEEN FS295 TO FS310.00 STR27 (C-CHECK RO 2/18/2025) FABRICATED 1- DOUBLER 2- FILLER WITH MATERIAL 2024T3 .063" AND INSTALLED REPAIR ON EXTERNAL SKIN AT TCAS ANTENA LANDING BETWEEN FS 295.00 AND FS 3SDR DALA2024121311703Skin · dentedDAMAGE T: ELONGATE HOLES, PROTRUDING DENTS, AND GOUGES ON FUSELAGE SKIN STA Y 1037 BTW LONG 7R-13R. SUMMARY OF NRC 00627: ELONGATED HOLES, PROTRUDING DENTS, AND GOUGES ON FUSELAGE SKIN STA Y 1037 BTW LONG 7R-13R WERE REPAIRED PER PRI 622118-14 REV 3 AND ER/A 6SDR SWIA2025040401211Skin · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA62022-670-53-61-1716 N707SK MXCODEID52967-PR - AFT FUSELAGE OUTSIDE SKINR/H SIDE BETWEEN FS 1015.00 AND FS 1051.30 AND BETWEEN STR 27R AND STR 23R THERE ARE VARIOUS DENTS AND GOUGES AND NICKS. REPAIRED AFT FUSELAGE OSDR SWIA202503061211Skin · crackedLH TRU DOOR CUT OUT, THE LOWER AFT CORNER OF THE FUSELAGE SKIN HAS POSSIBLE CRACK IN THE RADIUS (MARKED) (C-CHECK RO 3/5/2025) VERIFIED SUSPECTED CRACK ON THE LEFT-HAND TRU DOOR CUT-OUT. REPAIRED REF. REO 670-53-11-2076 REV. -- DATE: 2025-01-23. COMPLISDR SWIA202501241211Doubler · corrodedTHE AFT ATG ANTENNA DOUBLER AT MATING SURFACE ON EXTERIOR HAS FRETTING CORROSION. (C-CHECK RO 1/23/2025) REMOVED AND REPLACED INSTALLED NEW AFT ATG ANTENNA EXTERNAL DOUBLER FS 1031.00 - FS 1051.30, STGR24R - STGR27 REF AIRCELL DOCUMENT NUMBER D12942-20SDR SWAA2025010775977Doubler · crackedCRACK LOCATED ON EGPR SURROUND DOUBLER 2024-763604<[01] STEP 6. EDDY CURRENT EQUIPMENT USED P/N: NORTEC 600D; S/N: 210138103 AND DUE DATE: 10-JUN-25;[02] PERFORMED PERMANENT REPAIR LOCATED EXTERNAL GROUND ELECTRICAL POWER RECEPTACLE SURROUND DOUBLER BTW BS 227SDR DALA2024121211681Skin · corroded(LOG 0705260) CORROSION WAS FOUND IN SETTLENMENT AREA AFTER REMOVE PASSENGER TELEPHONE ANTENNA BTW STA 500 AND STA 500A. FUSELAGE SKIN BTW STA 500 AND STA 500A WAS REPAIRED PER ER/A 622737-14 REV.ORIGINAL AND PRI 622737-14 REV.4SDR DALA2024121211664Skin · crackedCRACK AND WEAR AT SKIN CUTOUT STA Y 994 AT LONGERON 25R AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00774: CRACK AND WEAR AT SKIN CUTOUT STA Y 994 AT LONGERON 25R AT AFT CARGO COMPARMENT WAS REPAIRED PER B717-200 SRM 53-20-15-2R, PROCEDURE 12, REPAIR 12, FIG 201. SDR KCSA202412111123Skin · crackedNLG W/W RH CORNER @ APPROX STA 390 BETWEEN RS44 & RS45 - CRACKED ( APPROX 2 IN. LONG)SDR KCSA202412111122Skin · corrodedEVIDENCE OF CORROSION IN FWD CARGO BILGE AREA AROUND LAV SERVICE DRAIN PLATE APPROX BS 582-598 RBL 1-12SDR SWIA2025022841210Skin · chafedEXTERNAL SKIN AROUND THE TCAS ANTENNA MOUNT HOLES HAS CHAFING DAMAGE. (C-CHECK RO 2/26/2025) REMOVED CHAFE ON EXTERNAL SKIN AROUND THE TCAS ANTENNA MOUNT HOLES AND COMPLIED WITH ALL STEPS OF REO 690-53-21-1856 REV-- DATE:2024-12-24COMPLIED WITH TASK 51SDR SWI2025F00236Skin · scratchedEXTERNAL SKIN AROUND THE AREA OF TCAS ANTENNA SEALANT HAS MULTIPLE AREAS OF SCRATCHES. (C-CHECK RO 2/26/2025) REMOVED MULTIPLE AREAS OF SCRATCHES ON EXTERNAL SKIN AROUND THE AREA OF TCAS ANTENNA AND PERFORMED REO 690-53-21-1856 REV-- DATE:2024-12-24. SDR CALA2024121603096Skin · damagedFWD CARGO DOOR EDGE DAMAGE. DAMAGE IS ON THE OUTER SKIN AND SEAL RETAINER. ALSO THERE IS NO DAMAGED AREA, INTERIM REPAIRED, SEALED AND TAPED WITH ALUMINUM WITHIN #1 FLIGHT CYCLE. DAMAGE ON THE DOOR STRUCTURE. FOIL. LEAK TEST PASSED. SEAL DEPRESSOR WAS NOT DAMSDR VNAA2024121311101Skin · damaged#3 VHF ANTENNA MOUNTING AREA UNDER ANTENNA FUSELAGE SKIN IS DAMAGED. / C/W INTELSAT EA9596-REVB FUSELAGE / FS 629-645 / SCRATCHES UNDER VHF-3 ANTENNA, DELTA ENGINEERING 8100-9 # ST04797NY-011. IAW EA9596-REVC INSTRUCTIONS.SDR DALA2024121111631Skin · mechanic errorSHIP 3411 MISDRILLED AT VIASAT #2 FITTING LOCATION BETWEEN FR60 AND 61, STRINGER P'1 AND P'2. CORRECTIVE ACTION: REPAIRED PER ER/A 622812-14 REV ORIGINAL. (0702416)SDR 2024FA0000952Skin · crackedCRACK FOUND IN ROOF FS388, LWS43. WL225. APPROX 1" LONG.SDR 2024FA0000951Skin · crackedCRACKS FOUND IN ROOF SKIN IN TWO LOCATIONS. ONE CRACK APPROXIMATELY 2.5" LONG AT FS388, LWS43, WL225. ANOTHER CRACK APPROXIMATELY 2.75" LONG FOUND AT FS388, RWS43, WL225.SDR 2024FA0000950Skin · crackedA CRACK MEASURING APPROXIMATELY 3/4" LONG WAS DISCOVERED ON THE ROOF SKIN LOCATED AT FS388, LWS43, WL225 APPROXIMATELY.SDR SWIA20240113209Skin · dentedADM# N208SY-8348- DENT FOUND NEAR MAIN CABIN DOOR. ON BOTTOM, LEFT SIDE OF FWD LEFT HAND PASSENGER DOOR. DENT DAMAGE TO FUSELAGE SKIN LOCATED BETWEEN FR12 & FR13 AND BETWEEN STGR 16L & STGR 15L. EVALUATE DENT RECONTOUR AND REMOVE EVIDENCE IF POSSIBLE. (C-SDR SWIA202501020009Skin · dentedADM# N208SY-8348- DENT FOUND NEAR MAIN CABIN DOOR. ON BOTTOM, LEFT SIDE OF FWD LEFT HAND PASSENGER DOOR. DENT DAMAGE TO FUSELAGE SKIN LOCATED BETWEEN FR12 & FR13 AND BETWEEN STGR 16L & STGR 15L. EVALUATE DENT RECONTOUR AND REMOVE EVIDENCE IF POSSIBLE. (C-SDR AALA202412110729Skin · crackedAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND SIDE OF FUSELAGE EXTERNAL POWER PANEL LOWER CUTOUT SKIN IS BENT WITH CRACK. LOCATED BETWEEN STA 229 AND STA 235.8 AND BETWEEN S21R AND S22R. ACCOMPLISHED DOUBLER REPAIR PER SRM 53-10-15-2R-4.SDR GTIA2024121038592Skin · corrodedCORROSION ON EXTERNAL SURFACE OF CROWN SKIN AT FRAME 51 - FRAME 54 - STRINGER 2L TO 2R.-PERFORMED PERMANENT REPAIR ON THE CROWN SKIN BETWEEN FR 51-FR54 + 52L-52R REF SPIRIT WO 335980 EA 5341-24115 REV 00, RAF-01 3427128-01, THALES EA 3515 REV 1R WITH 8110-3 APSDR 2024FA0000953Skin · crackedCRACK DISCOVERED IN ROOF SKIN, FS388, RWS43, WL225, APPROX 1.78 INCHES LONG.
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