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 DALA2023060204428Unknown · unknownAIRCRAFT 1804, FOUND RIVET NOT FLUSH WITH FUSELAGE LOWER SURFACE AT 4 INCH AFT OF STA 1307 AND ON S-35L. CARRIED OUT DVI FOUND CORROSION ON THE STRINGER AT STGR 35L STA 1311 AFTER REMOVED THE RIVET NOT FLUSH WITH FUSELAGE LOWER SURFACE AT 4 INCH AFT OF STA 130SDR SWAA2023070571838Doubler · crackedEXISTING REPAIR DOUBLER INSTALLED BS455 TO BS480 STR2L TO 3R REF: T209160; REPAIR-53EA-01161 AND FAULT TTG8Q0039LWC<[01] REQUEST NDI TO FOR CRACK FREE CONDITION AT THE CHEM-MILL STEPS WITHIN THE REPAIR AREA IAW WIP1; AND SERVICE BULLETIN 737-53-1310; FIGURE 24SDR SWAA2023061354967Panel · crackedPANEL 122YAC SHOWS SEVERAL CRACKS AT FWD CARGO COMPARTMENT<[01] RECEIVED NEW FWD CARGO COMP PANEL 122YAC. PART:453A1220-9; PO#:1792296. PANEL WILL BE INSTALL IN TTG8Q00JDU3C PER AMM 25-52-00-200-803;[02] VERIFIED STEP 1SDR YENA2023060600580Unknown · unknownDURING HEAVY MAINTENANCE: CPCP FOUND, CORROSION ON SEAT TRACK BEAM BTW FR 84 AND Y:340 LH AT CABIN FLOOR STRUCTURE. (W2); REF TOMEX WO 2196, NR 00084, CORROSION ON SEAT TRACK BEAM BTW FR 84 AND Y: 340 LH AT CABIN FLOOR STRUCTURE WSS REMOVED AND EVALUATED OUT OSDR YENA2023060600579Unknown · unknownDURING HEAVY MAINTENANCE: CPCP FINDING, CORROSION ON FRAME 80- BTW STGR 28R/27R AT AFT CARGO DOOR CUTOUT STRUCTURE; REF TOMEX NR 00102, CORROSION ON FRAME 80 BTW STGR 28R/27R AT AFT CARGO DOOR CUTOUT STRUCTURE WAS REMOVED AND EVALUATED OUT OF LIMITS OT=0.118 SDR DALA2023060504517Unknown · unknownSHIP 660 DTA MONITOR INSPECTION LOG REF ERA 608341-14. CORRECTIVE ACTION: REF ERA 608341-14. (2794909)SDR N6WA2023060501Skin · dentedDENT IN FUSELAGE SKIN AT FS250-FS265 STRG 14L. REPAIRED IAW WITH STS EA 72-2023-144 AND GOJET EO C550-53MR-007.SDR CALA2023060201739Skin · missingPDA 1 FOUND 1/2 PANEL 193CL MISSING ON ARRIVAL. THREE PANELS FOUND MISSING. RT SIDE SHOWN FOR COMPARISON CORRECTION: LANDING GEAR PANELS ADDRESSED ON CDL WRITEUP LP 4370202. REMOVED REMAINING UPPER HALF OF PANEL(PICTURED NEXT TO INSTALLED NUTPLATES WERE INSTASDR K11A2023060100210Skin · unknownCRACK IN FUSELAGE SKIN COMING FROM UNDER EXISTING REPAIR AT STA 727D-727E / STR 23R-25R REPAIRED IAW B737-400 SRM 53-00-01 FIG 201, DETAIL X, XISDR ASAA2023053043471Skin · delaminatedFLOOR PANEL 141A5810-235 INSERTS CORRODED. GROUNDED - YES. REPAIRED FLOOR PANEL 141A5810-235 IAW B737-900ER SRM 53-00-50-2R-0.SDR CALA2023053101725Skin · corrodedCORROSION LOWER SURFACE RIGHT WING CENTER BS 785.9 BTW KEEL BEAM AND BL 62 AT LOWER FUSELAGE (4 EA). REFER TO AEROMAN NON ROUTINE 2023-239484 MEASURES ON REWORKED AREAS ARE: P1 L: 2.392 IN W: 0.996 IN P2 INCH IAW NDT MANUAL PART 4, 51-00-10. NOMINAL THICKNESSSDR AALA202308149979Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON BULK CARGO COMPARTMENT INTERNAL REINFORCEMENT SKIN PANEL BETWEEN FR 65 AND FR 66, BETWEEN S33R AND S40R. REPLACED REINFORCEMENT SKIN PANEL PER SRM 51-42-11.SDR R61A2023063000363Skin Panel · dentedBIRD STRIKE ON FWD FUSELAGE BETWEE FRA 3 TO FRA 5 AND STR 2L TO 12L. REPAIRED IAW ETD2023-170-014336 AND EMB 170/175 SRM 51-40-02 AND51-43-02. ALSO REF VP-023072-2023 N/R 8 THRU 19 AND 36 THRU 40 FOR WORK ACCOMPLISHED.SDR DALA2023060104419Unknown · unknownSHIP 683 UPPER FORWARD FUSELAGE HAS DEFORMED/WRINKLED SKIN IN TWO PLACES. LOCATED RIGHT SIDE ABOVE THE "A" IN DELTA AND BETWEEN THE FIRST AND SECOND WINDOW. MARKED/CIRCLED IN RED. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0283:2020-2373/SDR FDEA202305270985Skin · corrodedH AFT FUSELAGE, APPROX STA 2140-2164, BOTTOM EDGE OF FAIRING AJC7897-1, HAS SURFACE CORROSION. REPAIRED LH AFT FUSELAGE BOTTOM EDGE AT APRROX STA 2140-2164, REF SRM 53-70-01 2R REPAIR 3 FIG 201 SHEET 1-5, MD-11 SRM 51-33-01-0G, DAC DWG AJC7059. "MAJOR SDR DALA2023053004252Skin · crackedCRACK AT FUSELAGE SKIN STA 1087 BETWEEN LONG 13/14 RH. (FUS). SUMMARY OF NRC 00300: FUSELAGE SKIN STA 1087 BETWEEN LONG 13/14 RH WAS REPAIRED PER PRI 608247-14 REV 1 AND ER/A 608247-14 REV. ORIGINAL. ACCOMPLISH SECTION II: REPETITIVE INSPECTION WITHIN EVERY 24SDR CALA2023052901681Skin · deformedR/H FUSELAGE STA 259.5 STR 20R LEADING EDGE OF SKIN DOUBLER REPAIR IS BENT/ CONTOUR IS DEFORMED. 43 AND BS 277, S-18R AND S-23R IN ACCORDANCE WITH PART 2 OF ECRA CYCLES. NOTE TO PLANNING: THIS ECRA IS BEING EVAL. FOR DAMAGE TO INSPECTION CRITERIA WILL BE INCLUSDR JJBA20230703028Unknown · unknownCF1 EXTERNAL SKIN, DENT FOUND BTWN FRAME 15-16 AND BELOW STR 11R SKIN REPIRED WITH A DOUBLER.SDR VNAA202306230020Skin · nickedSEVERAL NICKS ON FUSELAGE SKIN AT STA 1015 TO STA 1047 BTW STGR 21RH TO STGR 27. NICKS ON FUSELAGE SKIN AT STA 1015 TO STA 1047 BTW STGR 21RH TO STGR 27 WERE REPAIRED PER EA 23-C9-53-0742 REV. IR SECTION III PERMANENT REPAIR. AND PER EA 23-C9-53-0743 REV A. SDR SWAA2023062155560Shim · out of toleranceAAI: REF: NRC: G049597: EXISTING SEAT TRACK REPAIR SHIM HAS FASTENER HOLE WITH ZERO EDGE AT FWD SIDE OF THE REPAIR; STA 727B; LBL 45.5 2023-334567<[01] PERFORMED PERMANENT REPAIR LOCATED FLOOR BEAM UPPER CHORD AT BS 727B AND LBL 45.5. IAW B737-700 SRM 53-40-51SDR CALA2023052901695Skin · damagedDOOR SURROUND STRUCTURE SKIN DAMAGED FWD CARGO DOOR REAR SIDE APPROX 13 INCH ABOVE THE BOTTOM. REF ECRA 5330-07090 QC TO ACCOMPLISH A RECHECK WITHIN 3 CYCLES PER GMM 06-35-05. CARRIED BY ELB ACCOMPLISHED REEVAL OF BLENDED AREA. VERIFIED NO CRACKS AND WITHIN LISDR DALA2023052604240Unknown · unknownSHIP 3351 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED FR19 TO FR20 BTW STR 49R TO STR51R AT LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH ER/A 608134-14. EXISTING REPAIR INSTALLED PER A330 SRM 53-21-11 PARA. 5.C FIGURE 204, WHICH IS SDR DALA2023052604217Unknown · unknownSHIP 3351 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED FR 0 TO FR1 LH SIDE STRINGER AT LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH ER/A 608134-14. EXISTING REPAIR INSTALLED PER DELTA ER/A 504502-14. (2784584)SDR FDEA202305250940Skin · unknownDURING AGING AIRCRAFT INSPECTION, FOUND EXISTING REPAIR LOCATED ON FUSELAGE EXTERNAL SKIN, STA 1570 TO STA 1585, S3L TO S5L, REQUIRES EVALUATION FOR B757-200SF LOADING COMPLIED WITH FEDEX E.A. F-5330-T0374381-P1, TITLE: FUSELAGE - PLATES AND SKINS - BS 157SDR FDEA202305250938Skin · unknownDURING AGING AIRCRAFT INSPECTION, FOUND EXISTING REPAIR LOCATED ON FUSELAGE EXTERNAL SKIN, STA 1495 TO STA 1522, S3L TO S5L REQUIRES EVALUATION FOR B757-200SF LOADING COMPLIED WITH FEDEX E.A. F-5330-T0374384-P1, TITLE: FUSELAGE - PLATES AND SKINS - BS 1495SDR CALA2023052601663Skin · damagedREFERENCE L/P 4677633. FOR INTERIM SKIN REPAIR AT STATION 500H-540 STR 26L-26R. REQUIRES 2ND DTA DIP NOTE TO PLANNING: THIS EC/RA IS BEING EVALUATED FOR DAMAGE SUPPLEMENTAL INSPECTIONS. THE INSPECTION CRITERIA WILL BE TOLERANCE. UNDER 14CFR 26.43(D) WHICH WILLSDR CALA2023052601656Skin · corrodedSKIN AT EXTERNAL A/C CONNECTION CORRODED AND PULLING THROUGH FASTENERS. SEE ATTACHED IMAGES FUSELAGE SKIN REPAIR IN ACCORDANCE WITH PART 2 OF EC/RA 5330-07087 ON OR BEFORE 20 MAY 2025 PERFORMED INTERIM REPAIR PER EC/RA 5330-07087 AT STA 500H-540 LOWER SKIN. PLSDR DALA2023052504155Unknown · unknownSHIP 3407 STAGE II DTE LIMIT. CORRECTIVE ACTION: REF ER/A 588875-14. (2782951)SDR V0XD20230524001Skin Panel · crackedLEFT HAND WINDSHIELD OUTBOARD POST SKIN IS CRACKED AT UPPER SIDE. CORRECTIVE ACTION: REPAIRED L/H WINDSHIELD OUTBOARD POST SKIN IAW EMB SB 145-53-0079 REV. 1 DATED 07NOV 2012. SEE AVAMAX W.O. 81054 W.C. 2189SDR CALA2023052601667Skin · corrodedSKIN AT EXTERNAL A/C CONNECTION CORRODED AND PULLING THROUGH FASTENERS. SEE ATTACHED IMAGES FUSELAGE SKIN REPAIR IN ACCORDANCE WITH PART 2 OF EC/RA 5330-07087 ON OR BEFORE 20 MAY 2025 PERFORMED INTERIM REPAIR PER EC/RA 5330-07087 AT STA 500H-540 LOWER SKIN. PLSDR DALA2023052504156Unknown · unknownSHIP 3351 DURING HCK AT AEROMAN (SAL) AND ACCOMPLISHMENT OF EM 5330-01152, SEVERAL FASTENERS AT FR 84R, 85R, 86R, AND 87R REINFORCEMENT AN GLES COULD NOT BE INSTALLED. CORRECTIVE ACTION: REF ER/A 609094-14AD. (2782735)SDR SWAA2023061451440Baffle · crackedFOUND BAFFLE CRACKED AT FWD. CARGO S-26L; BETWEEN STA. 500A - 500B.<[01] REMOVED DAMAGED BAFFLE; RECEIVED & REPAIRED NEW BAFFLE FOR ACCESS TO ROUTE WIRE BUNDLE; INSTALLED NEW REPAIRED BAFFLE AT FWD. CARGO S-26L. BETWEEN STA. 500A - 500B; AS PER DWG. 143A7505; SDR CALA2023052401635Skin · dentedUNDOCUMENTED DENT DISCOVERED AT BS 1480 + 19 BETWEEN S24R-S25R. DIMENSIONS: 5.00"L X 2.65"W X .125"D AND IS .5" FROM BS 1500 & S24R. PER SRM 53-00-01 ALLOWABLE DAMAGE 1 FIGURE 101 DETAIL III. DENT OUT OF LIMITS. UE DIP FOR INSPECTION REQUIREMENTS TABLE 206/REPSDR DALA2023052404133Unknown · unknownSHIP 3351 DURING HCK AT AEROMAN (SAL) AND ACCOMPLISHMENT OF EM 5330-01152, SEVERAL FASTENERS AT FR84L, FR85L, FR 86L, AND FR 87L REINFORCE MENT ANGLES COULD NOT BE INSTALLD PER EM. DELTA ERA 608932-14AD WAS WRITTEN TO ALLOW FASTENER INSTALLATION. CORRECTIVE ACSDR DALA2023052304103Unknown · unknownCORROSION ON SKIN STA Y=214 BTW STR 28R AND STR 29R AT (E/E). SUMMARY OF NRC 00458: CORROSION LEVEL 2. SKIN STA Y=214 BTW STR 28R AND STR 29R WAS REPAIRED PER ER/A 608703-14 REV. ORIGINAL SECTION I: PERMANENT REPAIR TIME CONTROLLED ITEMS, ACCOMPLISH SECTION IISDR SIMA20230522002Skin · dentedDENT/PROTRUSION BETWEEN FR 23-24, STGR 24L-25L(MAJOR REPAIR)-C/A-PERFORMED PERMANENT REPAIR TO DENT/PROTRUSION BETWEEN FR 23-24, STGR 24L-25L IAW ERS-EJ-53MR-4780.SDR CALA2023052401633Skin · damagedACFT DAMAGE BY CATERING TRUCK TO AREA BELOW L2 DOOR APPROXIMATELY 22 INCHES BELOW THE GOLD STRIPE, DAMAGE IS APPROXIMATELY 2.75 INCHES BY 7 INCHES. SKIN IS SCRAPED AND APPEARS THERE COULD BY SOME STRINGER DAMAGE AS WELL AS A POSSIBLE PUNCTURE. IMAGES ADDED. PISDR CALA2023052401628Skin · damagedREF LOG PAGE 3179948, FUSELAGE SKIN REPAIR AT STA 787 BETWEEN ST R 22R AND 23R FWD OF AFT PIT DOOR- INTERIM REPAIR APPROVAL FOR DAMAGE TOLERANCE REQUIREMENTS. ANALYSIS {DTA}. REMOVE THE AIRCRAFT FROM SERVICE ON OR BEFORE APPROVAL FOR DAMAGE TOLERANCE REQUIREMESDR IPXA2023052393303Skin · crackedINSPECTION TYPE:CRH WING ROOT AT PANEL 611AB HAS A CRACK ON THE SKIN ON THE NUTPLATE SIDEREPAIRED AREA IAW SRM 53-15-63SDR VNAA202305220010Skin · crackedSEVERAL NICKS ON LOWER SKIN OF AFT FUSELAGE BTW FS 977.00 TO 1051.3 AND STG 21 RH TO STR 27. NICKS ON LOWER SKIN OF AFT FUSELAGE BTW FS 977.00 TO 1051.3 AND STG 21 RH TO STR 27 WERE REPAIRED PER EA EA 23-C9-53-0562-IR ; EA 23-C9-53-0565-IR ;EA 23-C9-53-0566-ISDR VNAA202305220009Skin · crackedWEAR MARK ON EXTERNAL FUSELAGE SKING BTW FS897-FS913 AND BTW STGR 26L-27. WEAR ON EXTERNAL FUSELAGE SKIN BTW FS897 TO FS913 AND STGR 26L TO STGR 27 WAS REPAIRED PER EA 23-C9-53-0554 REV. IRSDR AALA202305309860Skin · corrodedAIRCRAFT IN BASE MAINTENANCE; CORROSION ON AFT LAVATORY VENT FUSLEAGE SKIN LOCATED AT BS 917, FROM S21L TO S22L, AT LBL 43. REPAIRED SKIN PER EA 345067.SDR UIEA2023052300506Unknown · unknownCORROSION - FOUND FUSELAGE SKIN CORROSION STA 1700 - STA 1720, S46L - S47L(<P>1) ACCOMPLISH EI T2023A53M-1148 REV 0. 2) ACCOMPLISH EI T2023A53M-1148 REV 1. 3) JOB COMPLETED AND CONDITION CHECK NORMAL</P>)SDR UIEA2023052300504Unknown · unknownLIGHTNING STRIKE - FOUND FUSELAGE SKIN SURFACE HAVE LIGHTNING STRIKE AT STA 680 S42L(<P>1) ACCOMPLISH EI T2023A53M-1111 REV 0. 2) ACCOMPLISH EI T2023A53M-1111 REV 1. 3) JOB COMPLETED AND CONDITION CHECK NORMAL</P>)SDR UIEA2023052300503Unknown · unknownLIGHTNING STRIKE - FOUND FUSELAGE SKIN SURFACE HAVE LIGHTNING STRIKE AT STA 460 BETWEEN S40L AND 241L(<P>1) ACCOMPLISH EI T2023A53M-1119 REV 0. 2) ACCOMPLISH EI T2023A53M-1119 REV 1. 3) JOB COMPLETED AND CONDITION CHECK NORMAL</P>)SDR FDEA202305200962Skin · dented1EA DENT ON FUSELAGE SKIN, AT FR98~99, STGR2L~3L CUT OUT THE DAMAGED DENT, FABRICATED THE REPAIR DOUBLER AND INSTALLED WITH BLIND RIVETS, SEALANT I.A.W A300-600F SRM 53-19-12-201, PARA.6, FIG.202, PAGE.213~218, THIS REPAIR IS CLASSIFIED AS A MAJOR CATEGORYSDR AALA202305256940Skin · wornAIRCRAFT IN BASE MAINTENANCE: WORN FASTENER HOLE IN SKIN LOCATED AT BS 520, S17L, AND LBL 70. REPAIRED SKIN PER EA 344545 AND SRM 53-00-01-2R REPAIR 1.SDR CALA2023052201599Skin · corrodedFUSELAGE SKIN IN SECTION 47 AT STA 917, BTW S-21L AND S-22L WITH CORROSION ON REPAIR TRIPLER (VENT CUTOUT) (REF: AAR NR 99968798) MAJOR REPAIRSDR DALA2023052304108Unknown · unknownSHIP 3305 DTA ER/A 603846-14 REV A MONITOR INSPECTION LOG REFERENCE REQUIRES 3RD STAGE DTA APPROVAL ON OR BEFORE 1ST OF 82300 CYC OR 219700 HRS AFTER SECT I. CORRECTIVE ACTION: REF ER/A 603846-14. (2774517)SDR DALA2023052304107Unknown · unknownSHIP 3317 BELOW WING SCAN LIGHT LT SIDE AT STR 28L & FR 30 PERM REPAIR C/W PEPER RI 605363-14. CORRECTIVE ACTION: REF ER/A 605363-14 AND SRM 53-21-11-300-017. (2775149)
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