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 SWAA2024120272231Panel · crackedPANEL 193D HAS 5.5' GROOVE .5' WIDE WITH CRACK IN FACESHEET<[01] C/W EA 24-153-03309.SDR DALA2024120211341Door · damaged(LOG 6430406) BELT LOADER HIT AIRCRAFT HARD RIGHT SIDE FORWARD CARGO DOOR BREAKS SET JET BRIDGE ON. REPAIRED LOWER LOBE DAMAGE PER ERA 622437-14 REV ORIG AND ERA 622437-14/ PRI'S "O"-"6" AND NRC #001,002,003, 004.SDR DALA2024120211330Skin · defective(LOG 0681481) WHILE ACCOMPLISHING DVI IAW CC 2330-2031 FOUND SUSPECTED CROWN INNER SKIN DEFECT AT STA 727C+16.5", LBL 12 COMMON TO VIASAT RADOME DOUBLER. ACCOMPLISHED SKIN REPAIR STA 727C+16.5" LBL 12 COMMON TO VIASAT RADOME DOUBLER IAW ERA 622502-14.SDR UIEA2024112601116Bear Strap · crackedLH FWD DOOR, AFT LOWER CORNER WITH CRACK INDICATION AT SECOND LOWER HOLE ON BEAR STRAP APPROX. 10 O'CLOCK.(<P>CRACK WAS REPAIRED IAW EA 6753A937. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024112501114Skin · scratchedTRAFFIC ALERT & COLLISION AVOIDANCE SYS HEALTH CHECK, ON TCAS UPPER ANTENNA WITH SCRATCHES ON FUSELAGE SKIN(<P>THE TCAS UPPER ANTENNA DOUBLER WAS BLEND OUT AND INSPECTION WERE PERFORMED IAW TRE 6753708. NO FURTHER DEFECTS NOTED.</P>)SDR SWI2025F00355Skin · damagedMULTIPLE LIGHTNING STRIKES ALONG LH, LOWER EXTERNAL AIRCRAFT SKIN BETWEEN FS 202.00 - 581.00. MARKED AND NUMBERED (12EA) (C-CHECK RO 3/14/2025) REPAIRED DAMAGE ALONG LH, LOWER EXTERNAL AIRCRAFT SKIN BETWEEN FS 202.00 - 581.00 REF. MHIRJ REO 670-53-00-7SDR SWIA2025031701126Skin · dentedDENT AT FS 220.00 ON EXTERNAL AIRCRAFT SKIN BETWEEN STGR 23R - 24R. MARKED. (C-CHECK RO 3/14/2025) REPAIRED DENT AT FS 220.00 ON EXTERNAL AIRCRAFT SKIN BETWEEN STGR 23R - 24R PER REO 670-53-11-2067 REV -- DATER 2024-12-27. COMPLIED WITH SKYWEST TASK CARSDR DALA2025011500350Skin · damagedLIGHTNING STRIKE ON THE FUSELAGE AT THE RH WINDOW PANEL, STA 484 TO 503. ACCOMPLISH ER/A 622755-14 SECTION II INSPECTION WITHIN EVERY 24 MONTHS UNTIL ACCOMPLISHMENT OF SECTION III PERMANENT REPAIR NO LATER THAN 48,400 TOTAL CYCLES. ASSOCIATED ER/A 00-622755 ADSDR ASAA2024112654855Skin · corrodedEXTERIOR SKIN AROUND BELLY DRAIN BS.500+19.35 SHOWS SIGNS OF CORROSION. GROUNDED - YES. REMOVED DRAIN PLUG IAW B737 SRM 51-40-02: STRIPPED PAINT IAW B737 SRM 51-21-11-150-801. BLENDED CORROSION ORIG. THICKNESS 0.080, REMOVED 0.001 , 0.079 REMAINS FOUND TO BE WSDR SWAA2024121872131Stringer Clip · crackedCRACKED STRINGER CLIP AT PAX CABIN BS727E S-5L. MARKED<[01] REMOVED AND REPLACED STRINGER CLIP AT BS727E S-5L PER SRM 51-40-02-0G-0 AND BOEING DWG 146A1112 REV.-.;[02] VERIFIED CORRECTIVE ACTION ITEMS AND TASK CARD COMPLETED.SDR DALA2024120211329Skin · damaged(LOG 0680085) FUSELAGE CROWN SKIN / FS727C PLUS 16.2, S-3L TO S-2L / DAMAGED SKIN AT VIASAT MOD FITTING DOUBLER. REPAIRED PER ERA 622502-14.SDR LR7A2024112603648Skin · crackedDURING SCHEDULED C-10 CHECK UNDER JOB CARD HC5321, FOUND FUSELAGE SKIN CRACKED AT FS685, LBL72, WL156. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-10. NR# 0466.SDR LR7A2024112603646Skin · corrodedDURING SCHEDULED C-10 CHECK UNDER JOB CARD HC5321, FOUND FUSELAGE SKIN CORRODED AT FS637, LBL51, WL140.5. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0462.SDR LR7A2024112603621Skin · dentedDURING SCHEDULED C-10 CHECK UNDER JOB CARD HC5321, FOUND FUSELAGE SKIN DENTED BETWEEN FS289.0E TO FS300.0E, RBL22-28, WL280. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 190.SDR DALA2024112711259Skin · mechanic errorEXTERNAL SURFACE OF FUSELAGE SKIN COMMON TO VHF ANTENA MATING SURFACE WAS FOUND MISDRILLED, LOCATED Y=917 L-30/L-29L IN REF NRC 12. SUMMARY OF NRC 00169: FUSELAGE SKIN COMMON TO ANTENA MATING SURFACE WAS FOUND MISDRILLED, LOCATED Y=917 L-30/L-29L WAS REPAIRED SDR DALA2024112711254Skin · damagedSHIP 3302 DURING INSPECTION FOUND BURN MARK AT EXTERNAL FUSE SKIN FR1 AND FR2 BELOW STGR 32RH 13 INCHES. CORRECTIVE ACTION: DRILLED OUT AND REPAIRED PER A330 SRM 53-11-11-300-018. (0679181)SDR DALA2024112611234Doubler · mechanic errorSHIP 3421 DURING VIASAT INSTALLATION. MISDRILLED TO DOUBLER #1 BETWEEN FR60 AND FR61 AND S-2L AND S-1L. CORRECTIVE ACTION: REPAIRED PER ERA 622492-14 REV ORIGINAL. (0678621)SDR SWIA2024121601366Skin · corrodedDURING REMOVAL OF WASTE ACCESS DOOR FOUND CORROSION PRESENT ON THE WASTE BOX DOUBLER AREA COVERED BY THE WASTE ACCESS DOOR HINGE. (C-CHECK RO 12/13/2024) REMOVED AND REPLACED WASTE BOX DOUBLER WITH NEW REF. ERJ175 SRM 51-40-08. DOUBLER REPLACED WITH OEMSDR IPXA2024112588764Skin · damagedFUSELAGE SKIN DAMAGE 41€? FWD OF AFT CARGO DOOR NEEDS DEFERRED PER EO-92145-1 REQUEST TO HAVE FUSELAGE REPAIR DEFERRED PER EO-92145-1. OPENSDR ASAA2024112454666Skin · corrodedWASTE TANK VACUUM BLOWER OUTLET SKIN REPAIR CORRODED. GROUNDED - YES. REMOVED AND REPLACED TRIPLER AT WASTE TANK VACUUM BLOWER OUTLET IAW BOEING 737-800 SRM 53-70-01-2R-3 W 3" O .071 R .060 L 3" D .011.SDR SWI2025F00315Skin · damagedTRANSFER FROM EAML 1476473 : REF AML 1472665: BIRDSTRIKE DAMAGE NOTED ON FUSELAGE SKIN (DWG: 601R33010, AL ALY ALCD 2024-T42, 0.063€? PAD UP THK., 0.038€? CHEM. MILL. THK., REF. DENT: 11.50€? L X 2.50€? W X 0.100€? D €¢ 7-OFF PULLED MS20426AD4 FASTESDR SWIA202501270094Skin · damagedTRANSFER FROM EAML 1476473 : REF AML 1472665: BIRDSTRIKE DAMAGE NOTED ON FUSELAGE SKIN (DWG: 601R33010, AL ALY ALCD 2024-T42, 0.063€? PAD UP THK., 0.038€? CHEM. MILL. THK., REF. DENT: 11.50€? L X 2.50€? W X 0.100€? D €¢ 7-OFF PULLED MS20426AD4 FASTESDR TSAA2024112600026Skin · corrodedCORROSION AT LH SIDE FUSELAGE EXTERNAL SKIN AT STA 1088, S-5L~S-6L. CORROSION REMOVED LEVEL 1 AT 1088, S-5L~S-6L FROM PN 65-46882-1 ORIGINAL THICKNESS 0.064" REMOVED 0.002" AND REMAINING THICKNESS IS 0.062 AND IS WITHIN LIMITS PER SRM 53-00-01 ALLOWABLE DAMASDR TSAA2024112600025Skin · corrodedCORROSION AT LH SIDE FUSELAGE EXTERNAL SKIN AT STA 1088, S-2L~S-4L. CORROSION REMOVED LEVEL 1 AT STA 1088, S-2L~S-4L FROM PN 65-46882-1 ORIGINAL THICKNESS 0.071" REMOVED 0.001" AND REMAINING THICKNESS IS 0.070 AND IS WITHIN LIMITS PER SRM 53-00-01 ALLOWABLE DSDR TSAA2024112600024Skin · corrodedCORROSION AT RH SIDE FUSELAGE EXTERNAL SKIN AT STA 1028~1042, S-9R. CORROSION REMOVED LEVEL 1 AT STA 1028-1042, S-9R FROM PN 65-46882-1 ORIGINAL THICKNESS 0.0064" REMOVED 0.002" AND REMAINING THICKNESS IS 0.062 AND IS WITHIN LIMITS PER SRM 53-00-01 ALLOWABLE SDR TSAA2024112600016Skin · corrodedSURFACE CORROSION ON FUSELAGE EXTERIOR SKIN AT BS947+6" S25L+3". SURFACE CORROSION ON FUSELAGE EXTERIOR SKIN AT BS947+6" S25L+3" WAS REMOVED LEVEL 1, P/N 65-45776-11 ORIGINAL THICKNESS WAS 0.063" AND AFTER REMOVING 0.003" REMAINED 0.06" AND IS WITHIN LIMIT SDR TSAA2024112600011Skin · corrodedSURFACE CORROSION ON FUSELAGE EXTERIOR SKIN AT BS907 S23R. CORROSION REMOVE LEVEL 1 AT BS907 S23R, FROM PN 65C35778-21, ORIGINAL THICRNESS 0.071" REMOVED 0.007" AND REMAINING THICRNESS IS 0.064" AND IS WITHIN LIMITS PER IAW B737-300 SRM 52-30-01 IDENTIFICATIOSDR TSAA2024112600010Skin · corrodedSURFACE CORROSION ON FUSELAGE EXTERIOR SKIN AT BS907 S17R+4". CORROSION REMOVE LEVEL 1 AT BS907 S17R+4", FROM PN 65C35768-21, ORIGINAL THICRNESS 0.071" REMOVED 0.007" AND REMAINING THICRNESS IS 0.064" AND IS WITHIN LIMITS PER IAW B737-300 SRM 52-30-01 IDENTIFSDR FDEA202411231726Skin · damagedUPPER FUSELAGE SKIN BETWEEN STA 412/434 AND STG 8/9 RH WITH LIGHTNING STRIKE. UPPER FUSELAGE SKIN BETWEEN STA 412/434 AND STG 8/9 DAMAGE WAS REPAIRED I.A.W. E.A. #: H-5330-T0381396 RELEASE DATE: NOV 23, 2024 THE FIRST INSPECTION TO BE REALISED ON 30,000 CYCSDR DALA2024112511165Skin · dentedDENTS AND NICKS WERE FOUND ON THE EXTERNAL SKIN FLUSH REPAIR STA Y 237 AND BTW LONGERON 17L/18L. ALSO WRONG INSTALLED FASTENERS ON INTERNAL DOUBLERS BTW STA Y218/256 AND BTW LONGERONS 16/18 AT FUSELAGE. SUMMARY OF NRC 00343: PREVIOUS REPAIR ON STA Y 237 AND BTSDR SWI2025F00372Doubler · crackedPASSENGER DOOR AFT PULL IN CAM DOUBLER CRACKED. CAMP 29201392. (C-CHECK RO 3/14/2025) REMOVED AND REPLACED PASSENGER DOOR AFT PULL IN CAM DOUBLER REF. DRWG 601R31702 REV. N, CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01. COMPLIESDR CALA2024112902987Skin · damagedEVIDENCE OF LIGHTNING DAMAGE FOUND AT STATION 460 STRINGER S-10L NOTED: PREVIOUS UPDATE WAS DONE BY INSPECTION. REMOVED LIGHTNING STRIKE DAMAGE AT STATION 460 STRINGER S-10L BY INSPECTION REQUIRED FOR HFEC ON BLENDOUT OF LIGHTNING STRIKE AFTER HFEC DAMAGE REMASDR CALA2024112902986Skin · damagedEVIDENCE OF LIGHTNING DAMAGE FOUND AT STATION 500E STRINGER S-3R DAMAGE IS APPROX .25 FROM RIVET AND REQ REPAIR SEE PHOTO FOR DIMENSION AND LOCATION OF DAMAGE. INNER DIMENSIONAL PHOTO AND LOCATION SENT DESCRIPTION AND DIMENSIONS TO ENGINEERING FOR REPAIR. PER SDR CALA2024112701320Skin · dentedFOUND REPAIR SKIN DOUBLER DENTED APPROXIMATELY 6 FT FWD OF DOOR #2L. DENTED DOUBLER IS LIFTING AFT UPPER AND LOWER CORNERS OF DOUBLER AND DRAWING SKIN INTO DENT AT AFT SIDE OF DOUBLER. PERFORMED GVI OF AREA APPROX. 24" SURROUNDING DAMAGED FUSELAGE SKIN AND DSDR SWIA2024112500022Skin · dentedTRANSFER FROM EAML 1476546 : REF AML#1476032: UPON INSPECTION, FOUND A DENT ON THE LH SIDE OF FWD FUSELAGE SKIN BETWEEN FR 6 AND FR 7, STGR 17L AND STGR 18L MEASURING 3.20 INWIDE BY 4.33 IN LONG AND MAX. DEPTH OF 0.77 MM. (FLIGHT 3954 - FILED CLOSED) AFTSDR FDEA202411221721Skin · damagedUPPER FUSELAGE SKIN BETWEEN STA 347/368 AND STG 9/10 RH WITH LIGTINING STRIKE DAMAGE ON UPPER FUSELAGE SKIN BETWEEN STA 347/368 AND STGR 9/10 RH WAS REPAIRED I.A.W. SRM 53-00-01-2R REPAIR 29 REV 90 AUG 15, 2024. THE FIRST INSPECTION TO BE REALISED ON 30,00SDR ABXA20241122232Bear Strap · corrodedDURING N744AX C-CHECK AT AIRBORNE (TAMPA), THE LH BULK CARGO DOOR SURROUND STRUCTURE, BEAR STRAP P/N 146T8220-1 BETWEEN STA 1395-1417 AND STR 33L HAS CORROSION. THE DAMAGE WAS REMOVED BY BLEND-OUT PROCESS. THE ORIGINAL THICKNESS IS 0.160 INCHES AND THE REMAINISDR DALA2024112211152Skin · crackedSHIP 1601 FUSELAGE SKIN CRACK AT STA 1726 AND S-7R. CORRECTIVE ACTION: FUSELAGE SKIN AND CHORD STRAP CRACK AT STA1726, S-7R. TRIMED OUT THE DAMAGE PARTS AND PERFORMED REPAIR AS PER PRI:622403-14 (0671872)SDR IXXA20241122001Skin · crackedL-1 DOOR CUTOUT AFT LOWER CORNER IS CRACKED AT FASTENER HOLE IN BEAR STRAPSDR ASAA2024112156683Skin · damagedRAMP REPORTS DAMAGE TO FWD SIDE OF AFT CARGO DOOR CUTOUT. GROUNDED - YES. ACCOMPLISHED CATEGORY C MINOR TIME LIMITED REPAIR PER EA#800-53EA-27899 REV 02 ON 11/26/2024. WITHIN 500 FLIGHT CYCLES FROM 18085 TOTAL FLIGHT CYCLES OR 3 MONTHS FROM 23 NOV 2024, WHICHESDR CALA2024121603078Skin · pulled(SUPPORT TASK) FUSELAGE SKIN BETWEEN STA 360 TO 380 STR 25 L/H FASTENERS ARE PULLING THROUGH THE SKIN. PERFORMED REPAIR AT FUSELAGE SKIN BETWEEN STA 360 TO STA 380 STR EDGE IAW B737 SRM 53-00-03-2R-1 FIG 205, SRM 51-40-02, SRM 25L AND REMOVED AND REINSTALLED SDR FDEA202411211783Skin · damagedAIRCRAFT REPAIR ASSESSMENT: EXISTING DOUBLER REPAIR FOUND ON FUSELAGE SKIN BTW FR31~32, S-49R~52R COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 1SDR IPXA2024112509095Skin · ground damageOUTER FUSELAGE SKIN DAMAGE FROM GROUND EQUIPMENT, GOUGE, 41€? FORWARD OF AFT CARGO DOOR, GOUGE OVER 1€? LONG. INSTALLED REPAIR IAW EO-92145-PRELIM2SDR DALA2024112211154Skin · crackedSHIP 1601 DURING CCK AT STAG, A CRACK WAS NOTED ON THE FUSELAGE SKIN AT STA 1726, S-7R. CORRECTIVE ACTION: ACCOMPLISH ER/A 622403-14AD SECTION II (0671228)SDR DALA2024112211149Skin · not reportedSHIP 5652 FUSELAGE / SKIN AT FWD ATG4 ANTENNA / FS 508-520 BETWEEN S-28R & S 28L / EXTENSION OF DOUBLER DTE REQUIRED IN 12 MONTHS ACCORDING TO ERA 547524-14 REV C. CORRECTIVE ACTION: REFER TO ERA 547524-14 REV C. (671605)SDR DALA2024112211140Skin · damagedSHIP 3146 EXTERNAL SKIN SURFACE BTW FR47 AND FR70 FROM STR-23 LH/RH DAMAGE. CORRECTIVE ACTION: COMPLIED WITH ERA 622361-14AD REV 0. (0671453)SDR 2A6R2024112171301Skin · crackedCRACK DAMAGE WAS DISCOVERED ON THE CENTER TAIL CONE SKIN (PN: L533M1022262) MEASURING APPROXIMATELY 0.60”. ADDITIONAL DAMAGE REQUIRING REPAIR IN THIS AREA DUE TO A DOUBLE DRILLED FASTENER HOLE WAS DISCOVERED ON THE RH ENGINE DECK (PN: L533M1018346) AND ON THESDR SWI2025F00383Skin · corrodedCORROSION NOTED ON INTERNAL SKIN AROUND AFT DRAIN MAST SUPPLY LINES BETWEEN FS1031-FS1051 (MARKED) (C-CHECK RO 3/14/2025) REPAIRED THE SKIN AROUND AFT DRAIN MAST SUPPLY LINES PER REO 670-53-61-2430 REV-- DATED 2024-12-26, ALL STEPS COMPLIED WITH. COMPLSDR R61A2024120700570Skin · damagedDAMAGE RH RADOME AND RVSM SKIN AREA ON RH SIDE. REMOVED AND REPLACED RADOME AND LWR SKIN FR1-6 STGR 20R-20L. IAW EMB SRM 51-40-08SDR CALA2024112701321Skin · damagedINSPECT (GENERAL VISUAL) LAVATORY SERVICE PANEL(S) FOR, BUT NOT LIMITED TO: {B737-38-3-0129} - FASTENERS PULLING THRU LAV PANEL FRAME STRUCTURE LOCKING FOR MX FERRY FLIGHT 2 SEPARATE AREAS OF BULGING METAL AT LOWER FWD AND AFT CORNERS OF LAV DOOR REPAIR. FWD
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