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 COEA2023011016807Skin · corrodedHEAVY CHECK COE/MAJOR REPAIR: EXTERIOR UPPER FUSELAGE FRAMES 16-17 UNDER T2CAS GPS ANTENNA SKIN HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPAIRED PER SRAS ES_00204435_02...19921 ISSUE A, DATED 1/2/2023.SDR AALA202212203596Skin · corrodedAIRCRAFT WAS GROUNDED: CORROSION EXTERNAL SKIN BETWEEN FR 69 AND FR 70, BETWEEN S2L AND S2R. MAINTENANCE REPAIRED SKIN PANEL PER EA 340258.SDR SWAA2022110265666Doubler · crackedSUPPLEMENTAL INFORMATION: EGPR DOUBLER LOWER FORWAD FLANGE IS CRACKED AND REQUIRES PERMANENT REPAIR / [01] PAINT STRIP REPAIR AREA I.A.W MM51-21-11-701;[02] REMOVED EXTERNAL POWER RECEPTACLE ACCESS DOOR I.A.W MM 52-49-02-000-801;[03] REMOVED FASTENER TO GAIN ASDR DALA2022102907012Skin · damagedWHILE ON THE LINE IN ATL MAINTENANCE REPORTED IMPACT DAMAGE TO THE FWD CARGO DOOR SURROUND SKIN AND UNDERLYING FR 20A. THE DAMAGE IS LOCATED BETWEEN S-37R AND S-40R. THE SKIN DAMAGE MEASURES 5.5 IN THE CIRCUMFERENTIAL DIRECTION AND APPROX. 2.125 FWD-AFT POSSDR 2022F00430Skin · debondedFUSELAGE SKIN DISBONDED BETWEEN BS 908-916, AT UPPER ROW OF FASTENERS OF THE S-10L LAP SEAMSDR SWAA2022111765343Gusset · crackedFWD CARGO COMP STA 500D S-19L GUSSET APPEARED CRACKED / [01] CRACK CONFIRMED IAW NDTM PART 6; 51-00-00 PROCEDURE 23. CRACK LENGTH : 0.75'<BR>[NORTEC 600 ; B/C 172389 ; CALIB.DUE- 3/23];[02] REMOVED AND REPLACED ONE GUSSET AT STA. 500D STRINGER 19L REF.SRM 51-4SDR SWAA2022111465420Angle · corrodedRIGHT TRANSITION ANGLE; STA. 500A THRU 500I CORRODED, FOUND OUT OF LIMITS. LOCATED AND DRILLED NEW IAW SRM 51-40-02. REPLACED THE RH SIDE TRANSITION ANGLE IAW SRM 51-40-02.SDR SWAA2022111465419Shield · corrodedRIGHT SHIELD, RBL 21 BS 492-500A HAS CORROSION. SHIELD REMOVED AND REPLACED WITH NEW IAW SRM 51-40-02.SDR AALA202211032847Skin · crackedAIRCRAFT IN BASE MAINTENANCE: FOUND CRACKED UPPER SKIN AT BTU CUTOUT ON AFT CARGO COMPARTMENT BALL MAT PANEL 151SF. ACCOMPLISHED PERMANENT REPAIR AT UPPER SKIN BTU CUTOUT ON AFT CARGO COMPARTMENT PANEL 151SF PER B777-200 SRM 53-00-53-2R-6.SDR DALA2022102807001Skin · corrodedON WALK AROUND FOUND LWR BELLY SKIN CORROSION JUST FWD OF APU BOTTLE ACCESS DOOR BODY STATION 1867.7. REPLACED SKIN STRAP ON BUFF N/R # 1 REF B757 DWG.SDR CALA2022102802981Floor Support · corroded(A3NB-53-3-6222) MAIN CABIN AFT FLOOR SUPPORT STRUCTURE AT FR 66 POST-Y1732 HAS CORROSION DOT 126-68SDR UIEA2022092101012Doubler · crackedFUSELAGE RHS STA 2521 - TWO CRACKS FOUND ALONG RADIUS OF UPPER LOBE DOUBLER AT FUSELAGE AND VERTICAL STAB, ATTACH FITTING AREA(<P>CRACK AREA REPAIRED AS PER ATLAS AIR EO 4453A224 REV 8 PART 2 STEP 5.</P>)SDR UIEA2022092101013Doubler · crackedFUSELAGE LHS STA 2521 - CRACK FOUND ALONG RADIUS OF UPPER LOBE DOUBLER AT FUSELAGE AND VERTICAL STAB, ATTACH FITTING AREA(<P>CRACK AREA REPAIRED AS PER ATLAS AIR EO 4453A224 REV 8 PART 2 STEP 4</P>)SDR UIEA2022092101014Skin · cracked1EA CRACK FOUND ON SKIN AT LH BS980 DRAG FITTING AT STR 38 CRACK APPROX 0.125" INCH LENGTH, RUNNING TO AFT DIRECTION(<P>SKIN REPAIRED AS PER SRM 53-20-01-2R-2 REPAIR 2 FIG 201 AND ATLAS AIR EO 4453A499 REV 13 PART 3</P>)SDR UIEA2022092801052Skin · corrodedAFT CARGO COMPT STA 1680 - STA 1700 S50L - S51L INTERNAL SKIN FOUND SURFACE CORROSION(<P>CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 WITHIN SRM 53-00-01 ALLOWABLE DAMAGE 2 FIG 101 LIMITS </P>)SDR UIEA2022092801053Skin · corrodedAFT CARGO COMPT STA 1720 - STA 1740 S50R - S51R INTERNAL SKIN FOUND SURFACE CORROSION(<P>CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND 51-20-01 WITHIN SRM 53-00-01 ALLOWABLE DAMAGE 2 FIG 101 LIMITS </P>)SDR UIEA2022092801054Skin · corrodedAFT CARGO COMPT STA 1720 - STA 1740 S51L - S51R INTERNAL SKIN FOUND SURFACE CORROSION(<P>CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND 51-20-01 WITHIN SRM 53-00-01 ALLOWABLE DAMAGE 2 FIG 101 LIMITS</P>)SDR UIEA2022092801055Skin · corrodedAFT CARGO COMPT STA 1680 - STA 1700 S50R - S51R INTERNAL SKIN FOUND SURFACE CORROSION(<P>CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND 51-20-01 WITHIN SRM 53-00-01 ALLOWABLE DAMAGE 2 FIG 101 LIMITS </P>)SDR DALA2023061204738Unknown · unknown(LOG 2468572) LION AIR, THE PREVIOUS OPERATOR FOR AC 3954, FOUND 2 DENTS ON THE FWD LH FUSELAGE SKIN STA 312 - 328 AND STR 22L - 24L. DURING H-CHECK INSPECTION FOUND SEVERAL DISCREPANT FASTENERS OVER AND UNDERSHOT COMMON TO EXISTING DOUBLER REPAIR ACCOMPLISHEDSDR SWAA2022111464963Angle · corrodedFWD CARGO STA. 500G-500I CORROSION AROUND NUT-PLATE HOLES ON LEFT SUPPORT CHANNEL/TRANSITION ANGLE. REMOVED LIGHT SURFACE CORROSION; FOUND WITH IN LIMITS; TREATED AND PRIMED PER SRM 53-00-53-1A-2.SDR A6WA202210268356Skin · damagedLOWER CENTER WING PLANK HAS CHAFFED IN 2 EA AREAS FROM FAIRING PANEL 193AB ****AIRCRAFT REMOVED FROM SERVICE**** REPLACED L/H LOWER CENTER WING PLANK REF REO 601R-57-21-880 REV D DATED 2017-03-06SDR EE4Y2022102616490Skin · dentedDURING THE ACCOMPLISHMENT OF THE INSPECTIONS AS PER ETD2014-190-068050 REV A, WAS FOUND DENT #5,BEYOND LIMITS AS PER SRM 53-21-01 AD 52. SINCE DENT #5 IS CLOSE TO DENTS #6, #8 AND BLEND OUT #7, CUSTOMER DEVELOPED A REPAIR LAYOUT FOR YOUR EVALUATION AND APPROVASDR EE4Y2022102616488Skin · dentedDURING THE ACCOMPLISHMENT OF THE INSPECTIONS AS PER ETD2016-190-031302, WAS FOUND OILCAN DAMAGE LOCATED AT FR 04 AND BETWEEN STRINGER 11R AND 12R. SINCE THE MENTIONED DAMAGE IS LOCATED CLOSE TO THE INTEGRATED PITOT STATIC / AOA SENSOR 4 AND INSIDE THE RVSM ARESDR 1E1R2022102600417Skin · damagedWHILE REMOVING THE DOUBLER AND TRIPLER FROM INTERNAL SKIN BETWEEN FRAMES 49 AND 50, AT STRINGER L1 AND L2, 5EA. FASTENER HOLES WERE FOUND TO BE ELONGATED.SDR Y2PA2022102522071Skin · crackedDISCREPANCY: DURING C-CHECK IN KDHN, COMMERCIAL JET FOUND A PLUGGED HOLE AT STATION 315 L16L CORRECTIVE ACTION: COMMERCIAL JET IN KDHN PERFORMED A HFEC INSPECTION OF THE AREA AND FOUND THE HOLE TO BE CRACKED. THEY TRIMMED OUT THE DAMAGE AREA IAW FIG 3 OF EO17SDR SWAA2022103165135Retainer · looseR/H HORIZONTAL STAB LOWER FWD SLIDING SEAL UPPER RETAINER LOOSE / [01] RE-SECURED SLIDER SEAL RETAINER IAW AMM 53-31-31SDR CALA2022102702959Cleat · corrodedFWD CARGO PIT R/H FR27 BETWEEN STRINGER 42R-43R HAS CORROSION AT CLEAT (A3NB-53-3-6105) GENERATED BY V919150 AT HAECO LCQ PER NR 9294246 (44246) REMOVED AND REPLACED CLEAT FWD CARGO PIT R/H FR27 BETWEEN STRING ERS 42R-43R WITH P/N 5323039820101 IAW A319 SRM 51SDR CALA2022102702952Skin · crackedRHS FR 16 DOUBLE JOGGLE HOLES #8 CRACKED AT 2 O?CLOCK POSITION AND #D CRACKED AT 3 O?CLOCK POSITION. UMULATES 33,077 TOTAL AIRCRAFT FLIGHT CYCLES, PERFORM INSPECTION F THE LATEST REVISION OF EC 5311-02907. THERE AFTER REPEAT INSPE K PERFORMED BY VTMAE EMPLOYEESDR DALA2022102506947Skin · dentedAIRCRAFT 3352, DURING SERVICE CHECK IN MSP, MAINTENANCE FOUND A DENT ON THE FUSELAGE SKIN BETWEEN FR 3132 AND STR 26LH-28LH. MAINTENACE IN PROGRESS PER ER/A 603230-14. LP 2466966.SDR SWIA202266929Skin · corrodedVHF ANTENNA CUT OUT AT F.S. 455.8 STGR 0 AFT O/B DOME NUTPLATE HAS A HOLE CORRODED. COMPLIED WITH REO 601R-53-41-3091 REV-. MAJOR REPAIR.SDR CALA2022102702947Pressure Blkhd · crackedCRACK INDICATION ON FR36LH PRESSURE PANEL IN OPEN FASTENER HOLES A AND B COMMON TO LONGITUDINAL BEAM Y1292, CONTACT PLANNING TO ASSIGN AND ACCOMPLISH EA 5330-05216 OP2 BEFORE NEXT FLIGHT IN FWD CARGO COMPARTMENT (2 EA). ED PART 1 INTERIM REPAIR ON AEROMAN NR#2SDR UIEA2022102101158None · nonePRESSURIZATION LEAKAGE EVIDENCE ON EXTERNAL DOUBLERS INSTALLED IN UPPER FUSELAGE SKIN SURFACE AT BODY STA 434 / STA 654+22(<P>SEALANT WAS REPLACED AROUND OF EXTERNAL DOUBLERS <SPAN>INSTALLED IN UPPER FUSELAGE SKIN SURFACE AT BODY STA 434 / STA 654+22</SPAN></PSDR IPXA2022102587489Skin · misrepairedTEMP BLIND FASTENER INSTALLED FUSELAGE 8" FWD OR STA 676 - 1 INCH O/B OF S39LREPAIRED IAW E.O. B767-5330-85085-B ON NRC 684229SDR IPXA2022102487432Skin · misinstalledINSPECTION TYPE:N/ATEMP BLIND FASTENER INSTALLED FUSELAGE 8 INCH FWD OR STA 676 - 1 INCH O/B OF S39LFABRICATED REPAIR DOUBLER IAW UPS E.O.B767-5330-85085-A ON NRC 684228SDR ASAA2022102340500Skin · deformedFOUND DEFORMATION AROUND PREVIOUS REPAIR HOLES OF FUSELAGE SKIN. BS 480-500. GROUNDED - YES. PERFORMED FUSELAGE SKIN REPAIR PER ENGINEERING INSTRUCTIONS. REF 900ER-53EA-24872.SDR SWAA2022102563402Scuff Plate · crackedFWD CARGO DOOR CENTER SCUFF PLATE IS CRACKED AT OUTER EDGE 3' AFT OF FWD EDGE OF OF PLATE IN DENTED AREA. HFEC VERIFIED PER NDT PART 6; 51-00-00 PROC. 14 AND FPI PER SOPM 20-20-02. DURING ACCOMPLISHMENT 53-30-15-1A-2-A00074-INSP (DENTS - HFEC INSPECTION) - FWDSDR DALA2022102506939Skin · dentedSHIP 655 DENT ON FUSELAGE SKIN STA 740 BTW S-25R AND S-26R ARE OUT OF LIMITS. CORRECTIVE ACTION: SUMMARY OF NRC 00674: DENT ON FUSELAGE SKIN STA 740 BTW S-25R AND S-26R WAS REPAIRED PER ER/A 603151-14 REV ORIGINAL AND PRI 603151-14 REV, 1. (2462622)SDR CALA2022102402915None · crackedDURING ROTO INSP OF LH FRAME FOOT AT FR43 CRACK INDICATION WAS NOTED ON FASTER HOLE. REAPIR BEFORE NEXT FLIGHTSDR CALA2022102402912None · noneJETBRIDGE SCRATCHED PAINT NEXT TO DOOR 1L METAL SHOWING REF FIGURE 103 SECTION B, AC CAN BE OPERATED FOR 50 FLT HOURS PER SRM LIMITS. INSPECTED DAMAGE PER SRM 53-00-01-1A-1. LOCATION OF DAMAGE STA 360 AC LEFT, BELOW STRINGER 7L. CLEANED AREA. SCRACHES FOUND. DSDR CALA2022102402913None · corrodedBULK CARGO BET FR57 -5 STRINGER 37R IS CORRODEDSDR CALA2022102402914None · crackedDURING ROTO INSP OF RH FRAME FOOT AT FR43 CRACK INDICATION WAS NOTED OF FASTENER HOLE. REPAIR BEFORE NEXT FLIGHTSDR ABXA2023050986Skin · misrepairedDURING AIRCRAFT C-CHECK AT AIRBORNE (TAMPA), MISDRILLED WAS REPORTED COMMON TO FUSELAGE UPPER SKIN P/N 143T3111-1 LOCATED AT STA 705 AND S-1R. THE FINAL HOLE SIZE IS 0.323”. THEREFORE FOUND OUT OF LIMITS IAW 767-200 SRM 53-00-01 ALLOWABLE DAMAGE. FLIGHT VEHICLSDR SWAA2022112262958Skin · crackedCRACK EXTERNAL SKIN SERVICE DOOR CUT OUT LOCATED BS 294.5 MORE 3 INCHES AND BETWEEN STR8R TO STR9R FWD GALLEY AND LAV . REPLACED STUB FRAME LOCATED AT BS294.5 MORE 3 INCHES AND BETWEEN STR8R TO STR9R FWD GALLEY AND LAV IAW SRM 51-10-02 ITEM 9 AND DWG-141A837SDR SWAA2022111462916Skin · chafedCHAFING DAMAGE ON INNER FUSELAGE SKIN AT FWD CARGO BAY BS400+13 RBL3. MARKED. / [01] VERIFIED SRM 53-00-01-1A-5 ALLOWABLE DAMAGE 5 IS APPLICABLE FOR THIS EVALUATION.;[02] REMOVED DAMAGE BETWEEN STA 402 - 407; RLB 2 - RBL 4 IAW SRM 53-00-01-1A-5;[03] VERIFIED CSDR GTIA2022102436735Skin · damagedBURNT MARK FOUND AT FR 68-69 STRINGER 44. RAF 294913001. OPEN SDR ITEM.-VERIFIED LHT NR# 5001186184-0010. REPAIR WAS PERFORMED AS PER SRM 53-41-11-300-054 REV 33. REPAIR IS CATEGORY A AS PER SRM 53-41-42-205-053 REV 33. DEFECT MAPPED IN TRAXSDR DALA2022102406854None · noneSHIP 655 DTE, ER/A 602866-14; FUSELAGE / SKIN / STA. 1424 / BTW S27R & S29R / DENT. CORRECTIVE ACTION: REF ERA 602866-14.SDR DALA2022102406853None · noneSHIP 655 DENT ON FUSELAGE SKIN STA 1424 BTW S-27R AND S-29R ARE OUT OF LIMITS IN REFERENCE TO LOG 2690860. CORRECTIVE ACTION: SUMMARY OF NRC 00673: DENT ON FUSELAGE SKIN STA 1424 BTW S-27R AND S-29R WAS REPAIRED PER ER/A 602866-14 REV ORIGINAL AND PRI 602866-1SDR HKGA20221021001Skin · corrodedDURING THE HEAVY CHECK MAINTENANCE VISIT CORROSION WAS FOUND UNDER THE RIGHT HAND STRAKE AT THE AFT FUSELAGE SECTION BETWEEN FS 17088 TO 17103.64 AT STRINGERS 16R A PERMANENT REPAIR WAS INSTALLED IAW EMB120 ETD2022-120-029431 REV A.SDR DALA2022102506943Skin · unknownSHIP 655 ER/A 475076-14AD REV. D; B757 FUSELAGE / SKIN / STA. 590- 661 / STR 14L-19L / SPLICE. CORRECTIVE ACTION: REF ERA 475076-14 REV D. (2461099)SDR UIEA2022100801101Threshold Web · corroded***CORROSION***FWD CARGO DOOR THRESHOLD WEB, CORROSION STA. 460+3-460+10, RBL 28, WL 157 (REMOVED DAMAGED THRESHOLD WEB AND INSTALLED REPLACEMENT THRESHOLD WEB PN# 654A0003-58 @STA 440 TO 492 FWD CARGO DOOR THRESHOLD PER DWG# 143A8330 AND SRM 51-40-02-0G-0)
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