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 U2RA202502050009Skin · damagedDURING INSPECTION OF DATUM AIRCRAFT, ON SECTION 41 FUSELAGE SKIN, BETWEEN STA 488 AND STA 520 AND BETWEEN STR-22L AND STR-25L, WAS FOUND WITH BLEND OUT AND DENT DAMAGE.SDR CALA2025020400275Skin · damagedFUSELAGE SKIN AT FR34 STRG 43 HAS A REWORK AREA THAT IS OUT OF L IMITS CATECORY C.SDR 2025FA0000078Skin · failed insp9V-SFN IS CURRENTLY IN THE HANGAR FOR C CHECK. DURING THE ACCOMPLISHMENT OF THE ADSI IB744530224, INSPECTION ON THE SECTION 46 CROWN SKIN UNDER DORSAL FAIRING, FOUND TEFLON COATING AT DORSAL FIN FAIRING SEAT AREA WORN.SDR VNAA20250329009Skin · corrodedCORROSION ON DRAIN HOLES ON FS946 BTW STGR 26L-26R AT AFT FUSELAGE. CORROSION ON DRAIN HOLES ON FS946 BTW STGR 26L-26R AT AFT FUSELAGE WAS REMOVED PER CRJ-700 SRM 51-21-06-001-001-A01 AND REPAIRED PER REO 670-53-51-340 REV- -.SDR SWAA2025030491037Access Panel · crackedCRACK ACCESS PANEL 191D AT LOWER FUSELAGE 2025-93279<[01] REPAIRED ACCESS PANEL 191D AT LOWER FUSELAGE IAW B737-700 SRM 51-70-05-2R-2 REPAIR 2. REFER TO INDIVIDUALS SIGNOFFS BELOW.;[02] TASK COMPLETEDSDR DALA2025013000732Skin · wrinkledAIRCRAFT 3017, AC SKIN IS WRINKLED AT AFT TAIL JACK PAD AREA. CORRECTIVE ACTION: REPAIR INSTRUCTIONAL STEPS ARE COMPLETED AND MATCH FINAL - FUSELAGE / TAIL CONE / STR 31L - STR 31RH AND FR 72 - FR 75 / BUCKLE ER/A 623583-14 REV. ORIG. SECTION I PERMANENT REPAISDR CALA2025012900234Skin · crackedFWD SERVICE DOOR AFTER CUTOUT - IT WAS FOUND A SKIN AND BEARSTRAP CRACK INDICATION IN THE MARKED HOLE AT 1 AND 7 ON''CLOCK POSITION. ( ORIGINATING DOCUMENT NR 2395993)SDR DALA2025012900689Doubler · corrodedCORROSION ON DOUBLER REPAIR, BTW PROJECTION LONGS 26/27RH AT AFT CARGO DOOR, FWD JAMB C2. SUMMARY OF NRC 00010: CORROSION LEVEL 2. DOUBLER REPAIR BTW PROJECTION LONGS 26/27RH AT AFT CARGO DOOR, FWD JAMB C2 WAS MANUFACTURED AND REPLACED PER B717-200 SRM 53-20-1SDR VNAA20250329001Repair · wornWEAR ON PREVIOUS REPAIR DOUBLER, LOCATED BTW FS985 TO FS969 AND STGR 26L TO 26R. PREVIOUS REPAIR DOUBLER, LOCATED BTW FS985 TO FS969 AND STGR 26L TO 26R WAS REPAIRED PER REO 670-53-00-290 REV.-FSDR SWIA20250228128Skin · corrodedCF III INTERNAL SIDE FUSELAGE SKIN CORROSION ON SHEAR CLIPS AT FR 88 STRINGER 27R/28R. (C-CHECK RO 2/27/2025) REMOVED AND REPLACEDSHEAR CLIPS AT FR 88 STRINGER 27R/28R REF SRM 51-40-08. NO CHANGE IN WEIGHT CAUSED BY REPAIRS.SDR 2025FA0000114Skin · corrodedDURING AN INSPECTION FOUND CORROSION AROUND FASTENER HOLES ON THE LOWER FUSELAGE AFT SECTION AT FS 779 LH STRINGER 21L AND AT FS 779 AT THE CHIN FAIRING FASTENER HOLE.SDR AALA202501295799Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT SIDE OF FUSELAGE SKIN AT AFT LAVATORY SERVICE PANEL FROM STA 847 TO STA 867, FROM S24L TO S25L. ACCOMPLISHED REPAIR PER SRM 51-40-05 AND EA 361206.SDR 2025FA0000060Skin Panel · corrodedDURING REMOVAL OF PANEL 163AC, FOUND PANEL TO BE CORRODED. PERFORMED AN EDDY CURRENT INSPECTION ON A BLENDED AREA LOCATED ON PANEL 163AC, FOR THE PRESENCE OF CRACKS AND CORROSION, IAW THE CESSNA 560XL NDTM, PART 6, 20-00-02. NO CRACKS OR CORROSION NOTED AT THESDR SWIA202507210027Repair · gougedTHE DOUBLER REPAIR ON THE EXTERIOR JUST AFT OF FS977 BETWEEN STR26L AND STR26R HAS MULTIPLE GOUGES (C-CHECK RO 07/18/2025) REMOVED DAMAGED DOUBLER AND INSTALLED REPAIR PARTS. REF REO# 670-53-00-290 REV:-F DATE: 2019/04/26. LEAK CHECK GOOD . COMPLIED WITH TSDR ASAA2025012756002Skin · corrodedEXTERIOR SKIN BS.887 TO BS.1016 STR.23L UPPER LAP SHOWS SIGNS OF CORROSION 17 AREA. (MARKED IN RED). GROUNDED - YES. REMOVED CORROSION 17(EA) ON ZONE B. DAMAGE AREAS FROM STA 887-STA 1016 STR 23L UPPER LAP ORG MAT THICK 0.063, REMOVED 0.004 REMAINING 0.059 FOUSDR CALA2025020200254Skin · dentedLOWER FUSE HAS 2EA DENTS AT APPROX 43-STR38R FR27 A3NB-05-3-6003SDR CALA2025013000245Skin · damagedFUSELAGE SKIN FR61 STR42R HAS SET MARK AT RIVET (A3NB-05-3-6003) PER HAECO LCQ NON ROUTINE 9298879/32879 INSPECTION IAW SRI 53-41-11-205-048 BY 20500 FC OR 41000 FH WITH 4600 FH. ORIGINAL DISCREPANCY FOUND ON LCQ NR 9298879. 4600 FH. ORIGINAL DISCREPANCY FOUNSDR SWIA202502280126Skin · damagedFWD. LOWER CORNER OF PAX DOOR SURROUNDING STRUCTURE SKIN PANEL IS DAMAGED (C-CHECK RO 2/26/2025) REMOVED AND INSTALLED SKIN SPLICE PERMANENT REPAIR TO FWD LOWER CORNER OF PAX DOOR SURROUND STRUCTURE REF-CRJ-900 SRM 51-42-06-001-001 A01, SRM 51-42-21-001SDR SWIA202504040125Skin · scratchedVHF ANTENNA NUMBER 2 SKIN HAS SURFACE SCRATCHES (C-CHECK RO 04/04/2025)BLEND IS OUT OF LIMITS REF CRJ700 SRM 53-21-01-101-006-A01 AND RECEIVED REO 670-53-21-2564 REV -- 2025-02-16, FOUND ACCEPTABLE TO ENGINEERING , AND PERFORMED OPERATIONAL TEST OF THE VHF SYSSDR SWAA2025021889628Bear Strap · crackedCRACK INDICATION ON BEAR STRAP FORWARD GALLEY DOOR BS 291-BS 294.5 BETWEEN S-8R AND S-9R .CRACK LENGTH 0.500 IN.APPROX. AT PASSENGER CABIN 2025-91754<[01] TOOL USED ON STEP#6: EDDY CURRENT EQUIPMENT; P/N: NORTEC 600D; S/N:240524311; CAL DUE DATE:13-NOV-25;[02]SDR QXEA2025021800035Doubler · corrodedDOUBLER FWD OF R1 DOOR IS CORRODED. REMOVED AND REPLACED DOUBLER AT FWD OF R1 DOOR IAW SRM 51-40-08.SDR IPXA2025012887953Panel · dentedFOUND ON WAI DENT RH LOWER FUSELAGE FWD OF FWD LOWER CARGO DOOR OPERATING SWITCH PANEL DEFERED PER EO-92626-REQ1. OPENSDR DALA2025012700647Skin · ground damageSHIP 3410 FUSELAGE / REAR / SKIN BETWEEN FR68 - FR69 AND STGR49RH / GROUND IMPACT DAMAGE. CORRECTIVE ACTION: COMPLIED WITH ERA 619702-14 REV D SECTION III. (0777045)SDR CALA2025012700214Skin · gougedMAIN CABIN CROWN AREA STA 291.5 STRAP BETWEEN STR 4R-5R GOUGE REF AAR N/R 9937217 REMOVED,FABRICATED AND INSTALLED NEW STRAP AT STA 291.5 BETWEEN STR 4R-5R IAW B737-800 SRM 51-40-02-0G-0 AND DWG 141A8330.SDR AALA202504243737Skin Panel · noneAIRCRAFT IN BASE MAINTENANCE: PREVIOUS REPAIR FOUND 12" X 9.5" ON REAR FUSELAGE SKIN BETWEEN FR 62 TO FR63 AND STR 39R TO STR 43R. MAINTENANCE ACCOMPLISHED TIME LIMITED REPAIR ON REAR FUSELAGE SKIN BETWEEN FR 62 TO FR63 AND STR 39R TO STR 43R IAW EA 362801.SDR AALA202504240038Skin Panel · noneAIRCRAFT IN BASE MAINTENANCE: EXESTING REPAIR FOUND 8" X 8", FR 62 TO FR63 AND STR 41L TO 42L. MAINTENANCE ACCOMPLISHED TIME LIMITED REPAIR ON REAR FUSELAGE SKIN BETWEEN FR 62 TO FR63 AND STR 40LH TO STR 43LH IAW EA 362800 FOR MON REFER TO NCN 5030926.SDR CALA2025020200252Skin · gougedACFT L/H AFT FUSELAGE EXTERIOR HAS GOUGE IN LOCATION ZONE 160 ST A 28296 FR 60 BETWEEN STR 37-38 LEFT PER HAECO LCQ NON ROUTINE 9 296795/40795 GENERATED BY V901665 WITH INSPECTION REQUIREMENTS PER SRI 53-41-11-205-146. REPAIR IS FROM REPAIR EMBODIMENT WITH INTSDR DALA2025012300569Skin · buckledAIRCRAFT 3014, FR74 BUCKLED BETWEEN STR 31R AND 31L. CORRECTIVE ACTION: REPLACED PER AIRBUS REPAIR DRAWING R535-70010-000 REV P.SDR SWAA2025012388706Skin · crackedGROUND SERVICE DOOR SURROUND HAS CRACK AT BOTTOM<[01] INSPECTION C/W SURFACE INSPECTION OF CUT OUT PER NDT PART 6 51-00-00 PROCEDURE 4 NO DEFECTS NOTED;[02] REPAIRED GROUND SERVICE DOOR SURROUND PER SRM 53-10-15-2R-4;[03] INSPECTION C/W REPAIRED GROUND SERVICESDR BAGA2025012300003Skin · corrodedFORWARD SERVICE DOOR (R1) LOWER SKIN UNDERNEATH SCUFF PLATES FOUND CORROSION AROUND ATTACHMENT HOLES. ACCOMPLISHED REPAIR. (HEAVY CHECK)SDR DALA2025100807325Access Panel · out of limitsELONGATED HOLES (11 EA) WERE FOUND ON ACCESS PANEL OF LIGHT ASSY MB LOWER ARE OUT OF LIMITS PER DWG 5925039 REV. F. HOLES OUT OF LIMITS WERE REPAIRED PER ER/A 623283-14 REV. (0773037)SDR ASAA2025012256514Skin · corrodedEXTERIOR SKIN UPPER LAPSEAM BS.727E+13 TO BS.887 STR.23L HAS 9 AREAS THAT SHOW SIGNS OF CORROSION. (MARKED IN RED). GROUNDED - YES. ACCOMPLISHED ASA EA 800-53EA-28299 REV:00 REV. DATE 3/10/2025. TITLE SECTION 46 LH FUSELAGE SKIN, BETWEEN STA 727E+13 AND STA.88SDR UIEA2025012000091Skin · crackedFORWARD ENTRY DOOR CUTOUT AFT LOWER CORNER WITH TWO CRACK INDICATIONS AT HOLE 2 ON SKIN, POSITION 11 O´CLOCK AND 5 O'CLOCK, SEE N.D.T. INSPECTION REPORT.(<P>TWO CRACK INDICATIONS AT HOLE 2 ON SKIN, POSITION 11 O´CLOCK AND 5 O'CLOCK, WERE REPAIRED IAW SRM 53-SDR UIEA2025012000092Skin · crackedFUSELAGE - SECTION 41 - SERVICE DOOR CUTOUT AFT LOWER CORNER WITH A CRACK INDICATION AT HOLE 2 ON SKIN AND BEAR STRAP, POSITION 2 O´CLOCK, SEE N.D.T. INSPECTION REPORT.(<P>CRACK ON RH FUSELAGE, R1 DOOR CUTOUT, AFT LOWER CORNER ON SKIN WAS REPAIRED IAW SRM 53-SDR SWI2025F01029Skin · dentedEVALUATE PROTRUDING DENT ON EXTERNAL FUSELAGE SKIN BETWEEN FS 295.00 - 310.00, STGR 25L - 26L (C-CHECK RO 07/18/2025)REPAIRED PROTRUDING DENT ON EXTERNAL FUSELAGE SKIN BETWEEN FS 295.00 - 310.00, STGR 25L - 26L REF REO 670-53-21-2591 REV -- DATED 2025-03-22 SDR SWI2025F01028Skin · damagedNICKS AND DENTS ON AIRCRAFT EXTERNAL SKIN BETWEEN FS 1000.00 - 1051.00, STGR 27 - 21R (C-CHECK RO 07/18/2025)REPAIRED NICKS AND DENTS ON AIRCRAFT EXTERNAL SKIN BETWEEN FS 1000.00 - 1051.00, STGR 27 - 21R IAW REO 670-53-61-2490, REV-- , DATE.2025-04-17. COMPLISDR SWIA202507210021Skin · dentedEVALUATE DENT ON EXTERNAL FUSELAGE SKIN AT FS 409.00 BETWEEN STGR 21R - 22R (C-CHECK RO 07/18/2025)EVALUATED DENT, AFTER A VISUAL INSPECTION, 1 LIGHTING STRIKE WAS FOUND. REPAIRED LIGHTNING STRIKE ON EXTERNAL FUSELAGE SKIN AT FS 409.00 BETWEEN STGR 21R - 22R SDR SWI2025F00427Repair · gougedAFT LOWER EXTERNAL SKIN REPAIR DOUBLER GOUGED FS969-FS985 (C-CHECK RO 04/04/2025)COMPLIED WITH ALL STEPS OF REO # 670-53-00-290 REV - F DATED 2019/04/26 AND PERFORMED PRESSURIZATION OF THE AIR CONDITIONING DISTRIBUTION SYSTEM WITH THE APU REF. CRJ-700 AMM 21-5SDR IPXA2025021901241Skin · crackedCRACK - SKIN , STA 2658 BETWEEN S-11R AND S-12R (REPAIR). REPAIR DAMAGE AREA I.A.W UPS EO-92808-REQ1 REV.1 AND SRM 53-80-01-2R-4 REV.102 EGAT WORK SHEET NO.50052.SDR IPXA2025021901235Skin · crackedCRACK - SKIN , STA 2658 BETWEEN S-11L AND S-12L (REPAIR). REPAIR DAMAGE AREA I.A.W UPS EO-92807-REQ1 REV.1 AND SRM 53-80-01-2R-4 REV.102 EGAT WORK SHEET NO.50053. JOB COMPLETED.SDR CALA2025012400192Skin · damagedFR 21 STR42 HAS ILLEGAL LIGHTNING STRIKE REPAIR 2 EA HI-LOCKS WI TH NO SPACING A3NB-05-3-6003.SDR DALA2025012300543Skin · buckledAIRCRAFT 3017, FR73 BUCKLED BETWEEN STR 31R AND 31L. CORRECTIVE ACTION: REPLACED PER AIRBUS REPAIR DRAWING R535-70010-000 REV P. ADDITIONAL INFORMATION 019-0007:1212-6055/022 00032. (LP 0772065)SDR GTIA2025011638683Skin Panel · corrodedFWD CARGO COMPT PROFILE PANEL HOLE CORROEDED FRAME 28 STR 37R RAF 01 3371750-01 GENERATED SDR CREATED-REPAIRED FWD CARGO COMPT FASTENR HOLE AT FRAME 28 STR 37A IAW SRM 51-44-11 RDAF AIRBUS 81515054/003 2024#A FOUND TO BE CAT A REPAIR, NO FURTHER ACTION REQUIRESDR ASAA2025012056708Skin · corrodedCORROSION ON SKIN AT STR 4L AND STA727C SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY B MAJOR REPAIR TO FUSELAGE SKIN PANELS 146A3131-9 AND BETEEEN STA 727C STRG 4L IAW EA 800-53EA-28407 REV00 (SUBMITTED EAR UNDER MIG-5 N/R SA042461) SRXR430X.SDR FDEA202501200107Skin · corrodedAFT FUSELAGE STATION 2140 RIGHT HAND PANEL #347DF CUTOUT SURFACE CORROSION. SURFACE CORROSION AT AFT FUSELAGE - STATION 2140 RIGHT HAND PANEL #347DF CUTOUT PER MD-11 SRM 53-70-01-2R FIGURE 201, REPAIR 3. REPAIR CARRIED OUT PER MD-11 SRM 53-70- 01-2R FIGURSDR DALA2025012400607Skin · ground damage(LOG 0771210) DUE TO A BELT LOADER INCIDENT, IMPACT DAMAGE WAS SUSTAINED AT THE FORWARD CARGO DOOR SURROUND AT BS 440, S-24R. DAMAGE REPAIRED PER ERA 623606-14.SDR DALA2025012100470Doubler · wornWEAR ON REPAIR DOUBLER BTW STA Y=954 L24R TO L27R AT EXTERNAL FUSELAGE. SUMMARY OF NRC 00011: PREVIOUS REPAIR DOUBLER BTW STA Y=954 L24R TO L27R AT EXTERNAL FUSELAGE WAS REPLACED PER PRI 562383-14 REV 3 AND ERA 562383-14 REV B SECTION III: PERMANENT REPAIR. PESDR ASAA2025011955356Skin · corrodedLH FUSELAGE SEC 44 BUTT JOINT STA 727 FROM STGR 1L TO STGR 4L HAS SIGNS OF CORROSION SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY B MINOR REPAIR TO FUSELAGE SKIN PANEL 144A3111-18 AT STA 727 BUTT JOINT BETWEEN STGR 1L-4L IAW EA 800-53EA-28139 REV 00 SRXR430SDR ASAA2025011955354Skin · corrodedRH FUSELAGE SKIN SEC 44 BUTT JOINT AT STA 727 STGR 2R HAS SIGNS OF CORROSION SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY B MINOR REPAIR TO FUSELAGE SKIN PANEL 144A3111-18 AT STA 727 BETWEEN STGR 2R-3R IAW EA 800-53EA-28131 REV 00 SRXR430X.SDR ASAA2025011955351Skin · corrodedL/H SEC 43 LAP SEAM STA 500D STR 14L HAS SIGNS OF CORROSION SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY A REPAIR ON FUSELAGE SKIN P/N 143A3212-20 AT STGR 14L LAP JOINT BTW STA 500D AND STA 500E IAW EA#800-53EA-28115 REV 00 SRXR430X.
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