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 DALA2024010800310Unknown · unknownSHIP 3310 CRACK INDICATION FROM 14F HOLE LOCATED AT RH STRG 15A LEVEL AT UPPER FUSELAGE. CRACK DIRECTION IS 9 OCLOCK AND CRACK DEPTH IS 0.078 INCH. COERRECTIVE ACTION: ACCOMPLISHED REAMED HOLE 14F TO NEXT OVERSIZE LOCATE ON EXTERNAL SKIN AT RH STR15A LEVEL AT SDR IPXA2024010802794Unknown · unknownSECTION 46 FUSELAGE SKIN REPAIR DOUBLE ONE DENT , STA1920-1940, S-31~S32R.(EVALUATE) PERFORMED NDT/ET FOR DENT AREA, I.A.W.747 NDT MANUAL PART 6, 51-00-00 PROCEDURE 23 REV:175 RESULT:NO CRACK INDICATION WAS FOUND.SDR IPXA2024010808224Unknown · unknownOPEN. TWO SCRATCHES 0N THE RIGHT SIDE FUSELAGE SKIN AT STA 320, S-14R. DOT 8-001 APPROVEDSDR VNAA20240212003Skin · damagedPERM REPAIR - LOWER FUSELAGE SKIN MULTIPLE LIGHTNING STRIKES WITHIN 746.25 FHS FROM REV.-- (STARTING AT 19,934.42 FH), REPAIR, OR REPLACE THE DISCREPANT ITEM IN ACCORDANCE WITH APPROVED PROCEDURES IN REF TRFKE00BDQWC:EA A1-690-53-00002. LIGHTNINGS STRIKES LOCSDR VNAA20240212002Skin · damagedPERM REPAIR BEFORE 20,720.22 FH - LIGHTNING STRIKE STR24R-STR25R AT FS 235.00 THE SUBJECT CONDITION IS STRUCTURALLY ACCEPTABLE FOR 900 FLIGHT HOURS FROM THE TIME OF INCORPORATION OF THIS REO AT REV IN REF TRFKE00BD723:690-53-11-1621. PERM REPAIR BEFORE 20,720.SDR CALA2024011000078Skin · corrodedGEN ITEM: 63-5310-1-2630 CABIN LEFT SIDE AT STATION 1111 S-16L HAS CORROSION ON THE SKIN UNDER THE STRINGER, JUST BELOW LOWER FORWARD CORNER SECTION OF WINDOW, MARKED WITH STREAMER REPAIRED AIW REA 47585REA01. SEE PARTIAL WORK SHEET NO 14 1-4 FOR ALL WORK ACCOSDR CALA2024011000076Skin · corrodedGEN ITEM: 63-5310-1-2507 B767-53-3-7058 CORROSION ON INTERNAL FUSELAGE SKIN STA 1560 STRINGER 39L-39R AROUND THE TOILET SERVICE PANEL. REPAIRED THE AREA STA 1562-1582 IAW EC/RA 5300-0349, REA 47585FA B04, EC/RA 5360-01749, REA 47585FAB03. REF NON-ROUTINE 16563SDR DALA2024010900376Unknown · unknownSHIP 1603 FOUND A PUNCTURE ON RH FUSELAGE SKIN AT 20INCHES UPPER FROM ACCESS DOOR 312AR AND BETWEEN STA1678-STA1702. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER ERA 614690-14. (0140370)SDR IPXA2024010887820Skin · gougedIMPACT OF TAIL STEADY DUE INCLEMENT WEATHER CONDITIONS HAS CREATED A GOUGE L 1.25'' X W 0.15'' X D 0.03'' ON SKIN 18 (148U3260). DETAILED AREA ASSESSMENT C/O IAW SRM 53-00-01-1A-1 REV 41 AND AREA REPAIRED IAW DETAIL II NO FURTHER DAMAGE FOUND.SDR IPXA2024010588458Skin · damagedAIRCRAFT SKIN DAMAGE STA 2550 DUE TO TAIL STAND GROUND EQUIPMENT, REF T3F18E003PD3V PERFORMED GROUND HANDLING EQUIPMENT HITS AIRPLANE CONDITIONAL INSPECTION C/O IAW AMM 05-51-59/201 REV 43. FOUND DAMAGE ON STA 2550, SECTION 48. DAMAGE REPORTED ON BARCODES; T3FSDR IPXA2024010587860Skin · gougedIMPACT OF TAIL STEADY DUE INCLEMENT WEATHER CONDITIONS HAS CREATED A GOUGE L 0.75'' X W 0.15'' X D 0.03'' ON SKIN 17 (148U3240). DETAILED AREA ASSESSMENT C/O IAW SRM 53-00-01-1A-1 REV 41 AND AREA REPAIRED IAW DETAIL II NO FURTHER DAMAGE FOUND.SDR VNAA202402280001Skin · scratchedSEVERAL SCRATCH ON EXTERNAL REAR FUSELAGE SKIN AREA BTW FS985.00 - FS1000.00 AND STGR 14 - STGR 16. FUSELAGE SKIN AREA BTW FS985.00 - FS1000.00 AND STGR 14 - STGR 16 WAS REPAIRED PER REO 690-53-61-1346 REV - -SDR DALA2024022302546Skin · damagedSHIP 3411 FOA DAMAGE ON FWD CARGO DOOR CUTOUT FWD LWR FR20-FR20A AT STRG 39RH. CORRECTIVE ACTION: REPAIRED PER A330 SRM 51-11-11. (4879145)SDR VNAA202401210019Skin · dentedSEVERAL DENTS ON FUSELAGE SKIN, SETTLEMENT AREA OF RIGHT VENTRAL FIN FAIRING BTW FS 1069.75 TO REAR SPAR DATUM STABILIZER 67.5%, BTW STGR 22RH TO STGR 21RH. SEVERAL DENTS ON FUSELAGE SKIN, SETTLEMENT AREA OF RIGHT VENTRAL FIN FAIRING BTW FS 1069.75 TO REASDR VNAA202401210018Skin · dentedSEVERAL DENTS ON FUSELAGE SKIN, SETTLEMENT AREA OF LEFT VENTRAL FIN FAIRING BTW FS 1069.75 TO REAR SPAR DATUM STABILIZER 67.5%, BTW STGR 22LH TO STGR 21LH. SEVERAL DENTS ON FUSELAGE SKIN, SETTLEMENT AREA OF LEFT VENTRAL FIN FAIRING BTW FS 1069.75 TO REAR SPSDR DALA2024010900384Unknown · unknownSHIP 1603 ERA 614690-14 SECTION I ISSUED FOR SKIN REPAIR TO STA 1678-1702, S 23R TO S25R FUSELAGE SKIN. CORRECTIVE ACTION: ACCOMPLISH ERA 614690-14 SECTION II AT/BEFORE 37500 TOTAL FLIG HT CYCLES, THEN EVERY 12000 CYCLES THEREAFTER. (0139526)SDR AALA202401082050Skin · noneAIRCRAFT IN BASE MAINTENANCE: EXISTING FUSELAGE SKIN REPAIR AT STA 2370 FROM S45L TO S45R. ACCOMPLISHED DOUBLER REPAIR PER EA 350221.SDR R61A2024010400777Skin · gougedWHILE IN HEAVY CHECK - DENT/GOUGE ABOVE THE PILOT'S SIDE WINDOW FRAME 11 AND 12. STRINGER 05L AND 06L. PERFORMED DOUBLER REPAIR ABOVE THE PILOT'S SIDE WINDOW LOCATED BETWEEN FRAME 11 AND 12 AND STRINGERS 05L AND 06L REF EMB SRM 53-10-01/REPAIR 12P, EMB SRM 51SDR JR2R20240104445Skin · corrodedAFT WASTE WATER SERVICE PANE DOOR CUTOUT CORRODEDSDR DALA2024010400135Unknown · unknownSHIP 3120 CRACK IN THE FWD FACE OF FR35, LH SIDE. CORRECTIVE ACTION: REPAIRED AREA PER ERA 613454-14AD. (0138769)SDR DALA2024010400134Unknown · unknownSHIP 3120 CRACK IN THE FWD FACE OF FR35, LH SIDE. CORRECTIVE ACTION: REPAIRED HOLE #W1 LH AND HOLE #2 LH PER ERA 613454-14AD. (0138754)SDR DALA2026072304311Skin · damagedERA 604661-14 REV B (MTC DISCOVERED THREE (3) SCRIBE LINES ON THE FUSELAGE CROWN SKIN BETWEEN BS 727A 727B AND S-1 S-2R). - INSPECT AREA. REFER ERA 604661-14AD. (0138007) AIRCRAFT WAS GROUNDEDSDR SWAA2024020837381Skin · crackedR1-DOOR CUTOUT SKIN FWD STA 312 4' BELOW STR 8R APPEARED CRACK AROUND FASTENER<[01] INSTALLED REPAIR AT R1 DOOR CUTOUT BEARSTRAP SKIN REF SRM 53-10-01 ATR-6 4.N. AND FIGURE 202;[02] REFER TO EA 24-153-00239; BARCODE: TTG8Q00R6BKP;[03] 'DAMAGE REPAIRED PER 737-SDR HNAA2024012500034Rivet · pulled3 PULLED RIVETS HAVE CORROSION AT FR67 STR20R. R&R'D PANEL IAW EO1-53-24-0043SDR HNAA2024012500033Rivet · pulled2 PULLED RIVETS HAVE CORROSSION AT FR68 STR21L. R&R'D PANEL IAW EO1-53-24-0043SDR DALA2024010500168None · noneSHIP 3242 DISC: PERFORM ERA 614433-14AD. C/A: PERFORMED ER/A 614433-14AD REV: ORIGINAL AS PER PRI REV 0 OF ER/ A 614433-14AD REV: ORIGINAL JOB COMPLETE. (LP: 0138264)SDR UATA202401043521Skin · crackedWHILE INSPECTING THE AIRFRAME PER AD2022-17-06, AOT C212-53-0001 AND SB212-53-0055, A CRACK OF 0.719" WAS FOUND ON THE FUSELAGE SKIN IN THE AREA OUTLINED TO BE INSPECTED BY THE AOT. THE OEM HAS BEEN CONTACTED, THE SITUATION REPORTED, AND A REPAIR SCHEME REQUESSDR IPXA2024011945274Skin · damagedLIGHTNING STRIKE RH EXTERNAL SKIN AT STA.367 AND BETWEEN STR RBL 12 AND STR RBL 13. DOT 69-007 ACCOMPLISH REPAIR PER 757-200PF SRM REV 118 CH 53-00-01-2R-29SDR SWAA2024012537083Skin · delaminatedPANEL 193AR HAS A DELAMINATION ON THE INNER SURFACE SKIN (MARKED)<[01] DELAMINATION ON INNER SURFACE SKIN OF PANEL 193AR WAS REPAIRED IAW SRM 51-70-05-2R-2.;[02] VERIFIED CORRECTIVE ACTION #1SDR AALA202401227943Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON CENTER WING SECTION LOWER FUSELAGE SKIN AT BS 540, S22L. REPAIRED SKIN PER EA 350543 AND SRM 51-40-02.SDR CALA2024010500044Skin · crackedDURING 4C CHECK IN HAECO HKG WHILE ACCOMPLISHING EA5380-01178 OP1 STEP 3.2R 1EA CRACK FOUND AT BS 1654.5 AFTER 4.5? STR 13AL APPROX 7/8? IN LENGTH. ENCE 5.215 IAW SRM 53-80-01-2R-7 REPAIR 7 FIG 201. T NING AT 37500 FLIGHT CYCLES AFTER AIRPLANE DELIVERY, REPEATSDR CALA2024010500041Skin · damagedPSEVERAL PREVIOUS REWORK ON FUS SURF FR 24-30 STRG 41-43 R/H A3NB-53-4-6123, ZONE 100 SEQ#726 PSEVERAL PREVIOUS REWORK WERE FOUND ON FUSELAGE SKIN FR 24-30 STGR 41-43 R/H A3NB-53-4-6123, ZONE 100 SEQ#726 M 53-21-11-283-018 REV. 147. PERFORMED PERMANENT REPAIR SDR CALA2024010500037Skin · unknownPSEVERAL PREVIOUS REWORK WERE FOUND ON FUSELAGE SKIN FR 24-30 STGR 41-43 R/H A3NB-53-4-6123, ZONE 100 SEQ#726 RM 53-21-11-283-018 REV. 147. PERFORMED PERMANENT REPAIR DOUBLER ON THRESHOLD AT 60,000FC / 120,000FH FROM THE TIME OF ADL/REPAIR -21-11-205-060 REV 1SDR IPXA2024010339386Skin · unknown*SDR FILED OPEN* FAULT - DENT, FUSELAGE EXTERNAL SKIN, STA 1654.5 ~ STA 1678, S-25R TO S-26R (EVALUATE) OK TO WORKSDR DALA2024010300086Unknown · unknownSHIP 3120 CORROSION WAS FOUND AFFECTING UPPER PLATE BOX BETWEEN FR42-43 RHS. CORRECTIVE ACTION: REPAIRED PER ERA 613864-14. (0137224)SDR DALA2024010300075Unknown · unknownSHIP 3015 REPAIR DOUBLER AT FWD ATG4 ANTENNA AREA, BETWEEN FR25 & FR26 NEEDS INSP. CORRECTIVE ACION: COMPLIED WITH ERA 604474-14AD. (0137106)SDR DALA2024010200056Unknown · unknownSHIP 3312 FUSELAGE SKIN CHAFED AT UPPER CUTOUT OF L2 DOOR. CORRECTIVE ACTION: REPAIRED PER PRI 614652-14 AND ERA 614652-14. (0135899)SDR DALA2024010200016Unknown · unknownAIRCRAFT 1603, SUSPECT CORROSION FOUND IN FWD CARGO LOWER AREA AT STA 478 TO STA 500 AND BETWEEN S-36R AND S-37R. CORRECTIVE ACTION: THE DAMAGED DOUBLER IN FWD CARGO LOWER AREA AT STA487 TO STA500 AND BETWEEN S-36R AND S-37R. REMOVED AND REPLACED THE INTERNAL SDR IPXA2024012433335Skin · debonded**SUPPLEMENTAL SDR**FAULT - DISBOND - SKIN, EXTERNAL LOWER SIDE SURFACE OF L/H AFTER WING TO BODY ACCESS PNL NO.197KL. (REPAIR) REVIEWEDSDR IPXA2024010333335Unknown · unknown*SDR FILED OPEN* FAULT - DISBOND - SKIN, EXTERNAL LOWER SIDE SURFACE OF L/H AFTER WING TO BODY ACCESS PNL NO.197KL. (REPAIR) OK TO WORKSDR IPXA2024010333266Skin · unknownMAJOR REPAIR* FAULT- CRACK, FUSELAGE EXTERNAL SKIN, STA1654 STA1678 S-13AR (REPAIR) ACCOMPLISHED REPAIR I.A.W SRM 53-80-01-2R-7 REV.88 REVIEW COMPLETESDR DALA2024010300090Unknown · unknownSHIP 3317 UPON ARRIVAL IN CDG, MTC NOTED TWO DENTS WITH SCRATCH DAMAGE TO THE FUSELAGE SKIN (P/N: F5347928020200) LOCATED BELOW THE AFT SERVICE (4L) DOOR. THE UPPER DENT MEASURES 1.0" X 0.5" AND THE LOWER DENT MEASURES 1.75" X 1.5". THE MAXIMUM DENT DEPTH IS 0SDR DALA2024010200023Unknown · unknown(LOG 0134439) LIGHTNING STRIKE DAMAGE TO FUSELAGE SKIN STA 218 STR 24L. C/W FUSELAGE SKIN REPAIR ER/A 614698-14 REV ORIG.SDR DALA2024010200020Unknown · unknown(LOG (0134163) LIGHTNING STRIKE DAMAGE TO FUSELAGE SKIN STA 500C STR 23L. CW ERA 614705-14 REV ORIG.SDR DALA2024010200008Unknown · unknownDURING WALK AROUND FOUND CORROSION AROUND EXHAUST VENT. REMOVED AFT CARGO BULKHEAD PANELS TO FOM. REMOVED ELBOW TUBE FOR FOM. REMOVED EXISTING FASTENERS IN SKIN, TRIMMED OUT DAMAGED SKIN, REF A320 SRM 53-41-11-300-004. COMPLETED HFEC ON CUTOUT REF NTM 51-SDR REXA2024030700240Skin · corrodedMULTIPLE SPOTS OF CORROSION FOUND ON CLOSING SKIN AROUND FWD CARGO DOOR. REPAIRED IAW ENDEAVOR EA CRJ953-15863SDR R61A2024010500780Skin · dentedDENT FOUND ON REAR FUSELAGE BETWEEN FR 92- FR 93, AND BETWEEN STR 5R- STR 6R. DENT ON REAR FUSELAGE BETWEEN FR92-93 AND STR 5R-6R WAS FOUND TO BE WITHIN LIMITS IAW SRM 53-30-01 AD02. SEE AWS AND NDT REPORT TWO40472-1 FOR DETAILS. NO CRACKS FOUND. DENT DIMENSISDR JR2R20231230599Doubler · corrodedWASTE CUTOUT INSIDE OF FUSLAGE CORRODEDSDR SWI2024031100200Skin · chafedCHAFFING ON LOWER FUSELAGE SKIN AT FS974 (MARKED, CHAFFING FROM SUPPORT STRAP ON PANEL 196DR). (C-CHECK RO 3/10/2024) REPAIRED CHAFING ON LOWER FUSELAGE SKIN AT FS974 IAW ALL STEPS OF REO 670-53-00-718 REV -- DATED 2024-01-26 AND REO 670-53-00-290 REV-F, DSDR ASAA2023122948173Skin · dentedR/H REAR FUSELAGE FR 74 2 OFF DENTS REAR OF PANEL 313AR DENTED FROM INSIDE. GROUNDED - YES. EVALUATED DENT 1 5.8" AFT OF FR 73, 2.1" DOWN OF STGR 27 RH. DIA<0.1 DENT IS .033/1.5<0.1 FOUND TO BE WITHIN LIMITS IAW A320 SRM 53-51-11-283-004 AND 53-00-11-283-005.
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