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 AALA202406067389Skin · crackedAIRCRAFT WAS GROUNDED: AT WALK AROUND FOUND ELECTRICAL GROUND POWER CUTOUT BOTTOM SIDEIS CRACKED OUT. REPAIRED ELECTRICAL GROUND POWER CUTOUT. PER SRM 53-10-15.SDR JR2R20240604108Skin · corrodedFUSELAGE SKIN CORRODED UNDER FWD CARGO SCUFF PLATESDR VNAA202407090005Skin · damagedIN REF. TRFKE00BFL7B:REO 690-53-00-532.1500FH PERM REPAIR - TEMPORARY REPAIR FOR LIGHTNING STRIKE DAMAGE TO FUSELAGE SKINS BTW FS379.00-FS437.00 & STR25L-STR27 AND FS897.00- FS913.00 & STR2L-STR3L WITHIN 1500FH ACCOMPLISH APERMANENT REPAIR IAW APPROVED PROCEDUSDR R61A2024060700248Skin · damagedGOUGE AND DENT ON LEFT SIDE OF AC BELOW CAPT WINDOW(JETWAY DAMAGE). REPAIRED IAW ETD2024-170-015344 REV B. RETURNED TO SERVICE 6/7/2024SDR UIEA2024052800464Skin · damagedEXTERNAL FUSELAGE STA 844 STR18R+5" SKIN PANEL WITH SCRATCH.(<P>PERFORMED BLEND OUT REPAIR AND FOUND STRUCTURALLY ACCEPTABLE TO BOEING IAW COOPESA EO N°: COO-EO-2024-20121-R00 DATED MAY/08/2024 AND BOEING MESSAGE COO-TLS-24-0107-0413 DATED MAY/08/24. DOCUMENTSDR SIMA20240602005Skin · corrodedNRTC # E041258 -FUSELAGE INTERNAL SKIN CORRODED BETWEEN FR 75/76 STGRS 28R/29R. (MAJOR REPAIR) (LEVEL 2 CORROSION) PERFORMED REPAIR TO FUSELAGE INTERNAL SKIN BETWEEN FR 75/76 AND STR 28R/29R IAW ERS-EJ-53MR-5004SDR SIMA20240602006Doubler · corrodedNRTC # E041256-FUSELAGE INTERNAL SKIN CORRODED BETWEEN FR 76/77 STGRS 28R/29R. (MAJOR REPAIR) (LEVEL 2 CORROSION) PERFORMED REPAIR TO FUSELAGE INTERNAL SKIN BETWEEN FR 76/77 STGRS 28R/29R IAW ERS-EJ-53MR-5006SDR DALA2024060305747Skin · damagedSHIP 3122 LIGHTNING STRIKE DAMAGE TO SKIN 2.25" FWD OF FRAME 4 AND 12" ABOVE LOWER SKIN LAP SPLICE. CORRECTIVE ACTION: DRILLED AND REMOVED DAMAGE IAW A319 SRM 53-11-11-300-034. (0373471).SDR DALA2024060305746Skin · damagedSHIP 3122 LIGHTNING STRIKE DAMAGE TO SKIN 4" FWD OF FRAME 8 AND 10" ABOVE LOWER SKIN LAP SPLICE. CORRECTIVE ACTION: DRILLED AND REMOVED DAMAGE IAW A319 SRM 53-11-11-300-034. (0373480)SDR U2RA2024081500040Skin · damagedFOUND RIVET HOLES ELOGATED ON SKIN 2700 LH SIDE AFTER MEASURMENT RIVET HOLES DIAMETER BETWEEN .280 INCH UP TO .320 INCHSDR U2RA2024081500030Skin · corrodedRT SIDE FUSELAGE INNER WINDOW BELT CORROSION AT STA 1000 STR 15-STR 23SDR U2RA2024081500029Skin · damagedFOUND RIVET HOLES ELOGATED ON SKIN RH SIDE AFTER MEASURMENT RIVET HOLES DIAMETER IS BETWEEN .280 TO .320 INCHSDR SWIA20240716601Skin · puncturedTRANSFER FROM EAML 1359085 : TRANSFERRED FROM CAMP 28294575. PUNTURE DAMAGE OF 4' BETWEEN FS265.00 AND FS280.00 AND STR25L AND STR26R. PERFORMED TEMP REPAIR PER REO 670-53-11--1957 IN PREPARATION FOR FERRY FLIGHT. PERMANENT REPAIR REQUIRED. THIS HAS BEEN DETESDR VNAA202407110001Skin · corrodedINITIAL INSPECTION: CORROSION ON DOOR CUT-OUT INNER SKIN AT E/E MAIN COMPARTMENT. DOOR CUT-OUTINNER SKIN AT E/E MAIN COMPARTMENT WAS REPAIRED PER REO 690-53-21-032 REV--.SDR AALA202409045536Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK FOUND AT THE NOSE FORWARD FUSELAGE LEFT HAND LATERAL FORWARD SKIN PANEL EXTERNAL SURFACE RADIATING FROM FASTENER HOLE BETWEEN FR 13 AND FR 14, S10L AND BETWEEN AT Z+780 AND Z+950. REPAIRED SKIN PANEL PER EA 355027. SEE AALA2SDR JJBA20240805006Skin · damagedFOUND HOLE THROUGH AIRCRAFT 0.15748 IN. IN DIAMETER 2.5 IN AFT OF FRAME 23, AND 1 IN BELOW STRINGER 3L. REPAIRED OPEN HOLE THROUGH FUSELAGE SKIN 2.5" OFF OF FRAME 23 AND 1" BELOW STR 3LSDR VNAA202407100004Skin · dentedDENT BTW FS310.00 TO FS319.70 AND STGR27 TO STGR26 RH SIDE AT EXTERNAL FUSELAGE SKIN. DENT BTW FS310.00 TO FS319.70 AND STGR27 TO STGR26 RH SIDE AT EXTERNAL FUSELAGE SKIN WAS REPAIRED PER REO 670-51-00-085 REV-A AND PER REO 690-53-21-1784 REV--SDR YENA2024060500836Doubler · corrodedDURING HEAVY MAINTENANCE: TOILET WASTED DOUBLER CORRODED; REF TO AVIONAR JOB # A000049102-1023, WASTE ACCESS DOUBLER BTW FR 75/76 AND BTW 31L AND 36L REPAIRED I.A.W A224-634-11 AND AIRBUS REO 500-53-61-1231,TEMPORARY DISPOSITION, DVI TO BE CARRIED OUT AT INTERSDR YENA2024060500830Skin · corrodedDURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE / BOTTOM SKIN / BTWN FR57-58 & STR 36L-36R / CORROSION DAMAGE - TIME LIMITED REPAIR. (CONSIDERED AS A MAJOR REPAIR)SDR YENA2024060500829Doubler · corrodedDURING HEAVY MAINTENANCE: FUSELAGE / REAR BARREL / FR 75-76 AND STGR 32-36LH / WASTE ACCESS PANEL CUTOUT DOUBLER / CORROSION - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)SDR YENA2024060500828Doubler · corrodedDURING HEAVY MAINTENANCE: FUSELAGE / REAR BARREL / FR 75-76 AND STGR 32-36LH / WASTE ACCESS PANEL CUTOUT DOUBLER / CORROSION - TEMPORARY REPAIR. (CONSIDERED AS A MAJOR REPAIR)SDR N6WA2024060301Skin · damagedDENT/HOLE IN RIGHT SIDE FUSLAGE UNDER 4TH WINDOW. MAJOR REPAIR COMPLIED WITH REPAIR IAW REO 670-53-21-2404.SDR DALA2024060305749Skin · dentedDAMAGE FOUND- EXTERNAL DENT LEFT FWD FUSELAGE. 4 INCH X 3 INCH ABOVE STRG 29L AND AFT OF FR30A. TWO PANELS FWD CARGO OPENED FOR MTC(975849) REMOVED PAINT FROM EXTERNAL DENT FOR INSPECTION PER ENGINEERING REQUEST(249846) C/W HFEC OF DAMAGED AREA PER A220 ANDTP SDR DALA2024060205728Skin · dentedAIRCRAFT 6814, LOCATED DENT APROX STA 640, BTWN STR 25-26L. CORRECTIVE ACTION: REPAIRED FUSELAGE SKIN DENT AT STA 640 BETWEEN STRINGER 25-26L PER DELTA ERA 618020-14 REV. ORIGINAL. (LP 0369744)SDR F27A2024080600574Skin · corrodedCORROSION WAS FOUND UNDER THE AIRCRAFT DATA PLATE. CORROSION WAS REMOVED AND BLENDED. NDT FOUND SKIN AT .021IN. INSTALLED DOUBLER OF .040IN AND REINSTALLED DATA PLATE. WORK WAS PERFORMED BY TECHNICAIR GRAND RAPIDS MI ON THEIR WORK ORDER S66-24-66992.SDR SWIA2024082600529Skin · damagedADM# N187PQ-7903. FOUND LIGHTNING STRIKE DAMAGE AT FS752.5 ON STRINGER 9R. LIGHTNING STRIKE DAMAGE TO SKIN ON UPPER SKIN PANNEL AT THE BOTTOM EDGE TO THE SIDE SKIN PANEL BLENDED. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATESDR HNAA2024072600582Skin · dented53-2054 RF1 EXTERNAL LH LWR SKIN HAS DENT AT BTW FR65-66 BTW STR20-21L. REPAIRED IAW SRM 53-31-01SDR VNAA202407100005Skin · nickedINITIAL INSPECTION: SEVERAL NICKS BTW FS1000.00 TO FS1051.30 AND STGR#27 TO STGR#24RH SIDE AFT FUSELAGE. SEVERAL NICKS BTW FS1000.00 TO FS1051.30 AND STGR#27 TO STGR#24RH SIDE AFT FUSELAGE WERE REPAIRED PER REO 690-53-61-1410 REV -SDR SWAA2024062891371Doubler · corrodedCORROSION ON EXTERNAL SKIN EXISTING DOUBLER LOCATED AFT POSITION BONDING JUMPER ATTACH ON WIFI RADOME AREA BTW BS 727B TO BS 767 AND BTW STR 4L TO STR 4R AT UPPER FUSELAGE. PERFORMED PERMANENT REPAIR ON FUSELAGE - SKIN PANEL - ROW 44 WIFI STC EXTERNAL DOUBLERSDR WX0A2024061932083Skin · damaged(AIRCRAFT NOT GROUNDED) (DISCREPANCY DISCOVERED DURING AIRCRAFT HEAVY MX VISIT) NRC 2000-0005: (S/M)34240-01 REAR FUSELAGE SKIN, AT L2 DOOR CUTOUT, UPPER FWD CORNER FOUND DAMAGED. / REAR FUSELAGE SKIN L2 DOOR CUTOUT UPPER FWD CORNER PERMANENTLY REPAIRED PER AISDR DALA2024053005681Skin · dentedSHIP 6814 FUSELAGE SECTION 43, EXTERNAL SKIN AT BS 640, STR 25L-26L DENTED. DTA MONITOR INSP REF ERA 618020-14. CORRECTIVE ACTION: REF ERA 618020-14. (0366488)SDR DALA2024053005658Skin · dented(LOG 0367414) WHILE ON THE LINE IN LAX, MAINTENANCE OBSERVED A DENT AND GOUGE COMMON TO THE FUSELAGE SKIN (P/N 143A3212). THE DAMAGE AREA IS APPROXIMATELY 2.0" FROM THE BOTTOM ROW OF THE S14L LAP SPLICE AND 4.75 FORWARD OF STA380. MAINTENANCE REPAIRED DAMAGE SDR SWIA2024F00638Plate · corrodedAFT ATG ANTENNA RETAINING PLATE ASSY HAS CORROSION ROUND FWD COAX CABLE HOLE (C-CHECK RO 8/4/2024) REMOVED AND INSTALLED NEW AFT ATG ANTENNA DOUBLER PN P16492 REF. CRJ700 SRM 51-42-20-001-001-A01 AND GOGO DRAWING P13112-20110 REV H DATED 5/04/2011. COMSDR ASAA2024052850113Skin · crackedLH HORIZ LWR SKIN IS CRACKED AT STA 97 JUST FWD OF REAR SPAR. GROUNDED - YES. REMOVED CRACKED SKIN DAMAGE BY CUTOUT & INSTALLED FILLER & REPAIR DOUBLER IAW B737-800 SRM 55-10-01-2R-11 CAT B REPAIR.SDR DALA2024053005668Skin · corrodedSHIP 3219 DISC: ER/A 607913-14 HAS BEEN REVISED TO 'B'. FOLLOW ON ACTION IS REQU IRED. C/A: NOSE FWD FUSELAGE/ LOWER CENTER SKIN PANEL AND REINFORCEMENT /CORRODED. PERFORM SECTION II EVERY 16000FC AFTER SECTION I. ASSOCIATED ER/A 14-607913 ADDED FOR AC 3219. (SDR DALA2024052905610Skin · dentedSHIP 6806 IN REF TO MON 0953076, FOUND 2 DENTS ABOUT 5 FEET AFT OF C1. DOOR. CORRECTIVE ACTION: SUMMARY OF NRC 00203. AREA WAS REPAIRED PER B757-200 S.R.M. 53- 00-01-2R REPAIR 29. (0363644)SDR DALA2024053005675Skin · dentedSHIP 6806 IN REF TO MON 0953076, FOUND 2 DENTS ABOUT 5 FEET AFT OF C1. DOOR. CORRECTIVE ACTION: SUMMARY OF NRC 00203. AREA WAS REPAIRED PER B757-200 S.R.M. 53- 00-01-2R REPAIR 29. (0363621)SDR AALA202405309256Skin · gougedAIRCRAFT WAS GROUNDED: FOUND GOUGE AFT OF RIGHT HAND AFT SERVICE DOOR BETWEEN BS 1000 TO 1016 AND STR 11R TO 12R. ACCOMPLISHED PERMINENT SKIN REPAIR. NO FURTHER DAMAGE NOTED. PER AARD 11-20-00.SDR DALA2024052905604Skin · damagedLIGHTNING STRIKE DAMAGE TO SKIN FOUND ON FRAME 3, Z-137-7R. CORRECTIVE ACTION: REPAIRED DAMAGE PER A330 SRM 53-11-11-205-203. (0362130)SDR UIEA2024052800462Skin · damagedLIGHTNING STRIKE - SKIN, NOSE CARGO DOOR FREIGHTER L/H EXTERNAL SKIN, STA 140~ STA 160, WL 205 2 EA, STA 179 S-24AL 1 EA(<P>1. PERFORMED EI T2024A52M-1254 SEQUENCE A. REV 0, W/S 40409 (SRM 53-00-01-2R-9 REV 42) AND DWG 65B20288 SH 1 REV A 2. ACCOMPLISHED EI T2SDR VNAA202407020014Skin · corrodedCORROSION ON CIRCUMFERENTIAL JOINT AT FS 280.00 BTW STGR 25RH TO STGR 25 LH. CORROSION ON CIRCUMFERENTIAL JOINT AT FS 280.00 BTW STGR 25RH TO STGR 26 LH WAS REPAIRED PER REO 690-53-21-1782 REV -- AND BAY BTW STGR 25LH TO STGR 26LH WAS CLEANED PER CRJ900 SRM SDR YENA2024052900794Skin · dentedDURING HEAVY MAINTENANCE: INITIAL FINDING. DENT ON RH FUSELAGE SKIN BETWEEN FR2 AND FR3 AT 14" BELOW OF STGR RH SIDE; (RESOLVED ON W/O: 1283758 TASKCARD: NR-00001) FUR CREATED # FUR-A320-53-01269, REF MEXICANA WO1310910, 1283758, NRC 00228, : DENT ON RH FUSELASDR YENA2024052900793Skin · dentedDURING HEAVY MAINTENANCE: INITIAL FINDING. DENT ON LH FUSELAGE SKIN AT FR23 AND 1.5" ABOVE STRG 22; (RESOLVED ON W/O: 1283758 TASKCARD: NR-00004) REF MEXICANA WO 1310910, 1283758, NRC 00230. DENT ON LH FUSELAGE SKIN AT FR 23 AND 1.5" ABOVE ON STGR 22 WAS REPAISDR YENA2024052900791Skin · dentedDURING HEAVY MAINTENANCE: INITIAL FINDING. DENT ON LH FUSELAGE SKIN AT FR 23 AND 1.5" ABOVE STGR 22; REF WO # 1283758 NR # 00230 DENT ON LH FUSELAGE SKIN AT FR23 AND 1.5" ABOVE ON STGR 22 WAS EVALUATED & FOUND OUT OF LIMITS I.A.W A320 S.- R.M. 53-11-11-283-0SDR AALA202405289644Skin Panel · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FUSELAGE SKIN PANEL AT FR 14 AND S6R. MAINTENANCE REPAIRED SKIN PANEL PER SRM 53-11-11-300-054.SDR CALA2024060301686Skin · crackedDURING NDT PROCEDURE AS PER PART 6, 51-00-16. IT WAS FOUND A CRACK INDICATION ON THE HOLE OF SERVICE DOOR AFT LOWER SKIN CUT OUT AT STA 340 AND STGR 19R ON FIRST LAYER. SEE THE PICTURES. ACCOMPLISHED REPAIR AT RH DOOR #1 AS PER SRM 53-10-01-2R-1.SDR SWAA2024070989552Doubler · crackedEXTERNAL POWER RECEPTACLE ACCESS DOOR CUTOUT SKIN DOUBLER HAS A CRACK AT LOWER SIDE (AT FASTENER)<[01] REMOVED AND DISCARDED DAMAGED EGPR DOUBLER; LOCATED; DRILLED AND INSTALLED NEW EXTERNAL GROUND POWER RECEPTACLE DOUBLER AS PER B737-700 SRM 51-40-02-0G-0 ANDSDR QXEA2024052800143Skin · dentedDENT ON LH FORWARD FUSELAGE EXTERNAL SKIN BETWEEN FR11-FR12 AND STRINGERS 14L AND 15L. REPLACED LH FORWARD FUSELAGE EXTERNAL SKIN BETWEEN FR11-FR12 AND STRINGERS 14L AND 15L REF SRM 51-40-08.SDR HNAA2024072600579Skin · dented53-2017 CTR FUSE II DENT ON LWR AIRCRAFT SKIN AT FR26 STR20L. REPAIRED IAW EO1-53-24-0408SDR HNAA2024072600578Skin · damaged53-2015 DAMAGE FOUND ON FUSE SKIN AT SKIN JOINT ON FR23 STR18R. REPAIRED IAW EO 1-53-24-0350
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