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 FDEA202401120081Skin · dentedDURING BIRD STRIKE INSPECTION FOUND DENTS LOCATED FWD OF CAPTAINS WINDHIELD AFT OF RADOME. REPLACED FUSELAGE SKIN PANEL 141T3830-18 REF E.A. H-5330-T0377384 REV. C PT2 AND SRM STANDARD PRACTICES. SEE JPF FOR WORK ACCOMPLISHED,SDR JJBA20240117022Skin · chafedRF1 EXT, CHAFFING FOUND ON LH SKIN INSIDE PYLON AREA BTW FR 67-68 AND BTW STR 7L-8L. SKIN REPAIRED WITH A DOUBLERSDR AALA202401173211Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN EXTERNAL LOWER FUSELAGE SKIN BETWEEN STA 2195.75 AND STA 2221.65, BETWEEN S41L AND S43L. REPAIRED SKIN PER SRM 53-00-01-2R REPAIR 7.SDR CALA2024032100804Skin · buckledRAMP REPORTS DAMAGE TO THE TAIL STAND AREASDR SWAA2024020943436Access Panel · crackedACCESS PNL. # 323AR HAS PANEL LWR. POSITIONING METAL CLIP IS CRACKED . PANEL ATTACHED METAL CLIP IS CRACKED.<[01] REMOVED AND REPLACED RETAINER ON ACCESS PANEL 323AR. AS PER SRM 51-40-02-0G AND DWG 172A6122;[02] VERIFIED STEP # 1SDR VNAA202401210021Skin · nickedSEVERAL NICKS ON FUSELAGE SKIN BTW STA. 1000 TO STA 1051.30 AND STGR 23RH TO STGR 27RH. REPAIR WAS PERFORMED PER REO 690-53-61-1324 REV - -SDR R61A2024011800001Rivet · misinstalledCF 1 REPAIR AT FR 23, BTWN STR 14L-17L FOUND INCORRECTLY INSTALLED. REPAIRED IAW ETD2024-000742. MAJOR.SDR DALA2024011400562Unknown · unknownSHIP 3251, INSPECTIONS HAVE BEEN ADDED VIA SEPARATE LOG PAGE 0751012. CLOSED LOG AND REMOVED MONITOR INSP.) DTE DURING ACCOMPLISHMENT OF AA 2330-01179-02H, FUSELAGE SKIN WAS GOUGED DURING REMOVAL OF PCS TIMING ANTENNA COVER PLATE (PN 21299). DURING CURRENT CHSDR DALA2024011200522Unknown · unknownSHIP 3010 DURING LIGHTING STRIKE INSP FOUND DAMAGE AT APPROX STATION 3850 FR 2 @ 8:30 POS. CORRECTIVE ACTION: COMPLIED WITH ERA 614971-14. (0148893)SDR DALA2024011100495Unknown · unknownSHIP 3010 DURING LIGHTNING STRIKE INSP FOUND DAMAGE AT APPROX STA 4762 FR6. CORRECTIVE ACTION: REPAIRED PER A321 SRM 53-11-11-300-041. CONTINUE ON MON. (0148164)SDR DALA2024011100494Unknown · unknownSHIP 3010 DURING LIGHTNING STRIKE INSP FOUND DAMAGE AT APPROX STA. 4330 FR5 @ 8:30 POS. CORRECTIVE ACTION: REMOVED DAMAGE BY DRILLING 5/32"(.159") HOLE REF A321 SRM 53-11- 11-300-034. WIP 491375. PERFORMED ROTATING PROBE TO NEW HOLE PER A321 NTM 51-10-01. NO DSDR DALA2024011100493Unknown · unknownSHIP 3010 A321 / FUSELAGE SKIN LIGHTNING STRIKE / BLEND / RH FR2 / JUST BE LOW RHS STRGR LAP JOINT. CORRECTIVE ACTION: COMPLIED WITH ERA 614971-14. CONTINUE ON MON. (0148437)SDR DALA2024011100480Unknown · unknownLIGHTNING STRIKE DAMAGE IMMEDIATELY AFT OF RADOME 12 O CLOCK POSITION, AT APPROXIMATELY FR1 STGR 2L. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR PER A321NEO SRM 53-11-11-300-034. (7817765)SDR DALA2024011100479Unknown · unknownLIGHTNING STRIKE DAMAGE ON RH FUSELAGE AT APPROX FR6 AND STGR 27. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR PER A321NEO SRM 53-11-11-300-034. OK FOR SVC. (7817763)SDR DALA2024011100478Unknown · unknownLIGHTNING STRIKE DAMAGE ON RH SIDE FUSELAGE AT APPROX FR11 AND STRG 30. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR PER A321NEO SRM 53-11-11-300-034. (7817762)SDR DALA2024011100477Unknown · unknownLIGHTNING STRIKE DAMAGE ON 1R DOOR KICK PLATE AT APPROX FR20 AND STGR 23. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR PER A321NEO SRM 53-11-11-300-034. OK FOR SERVICE. (7817761)SDR DALA2024011100476Unknown · unknownLIGHTNING STRIKE DAMAGE ON RH SIDE FUSELAGE AT APPROX FR24 AND STRGR 20. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR PER A321NEO SRM 53-11-11-300-034. (7817760)SDR DALA2024011100475Unknown · unknownLIGHTNING STRIKE DAMAGE ON RIGHT SIDE FUSELAGE AT APPROXIMATELY FR28 AND STR 24. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR PER A321NEO SRM 53-11-11-300-034. (7817759)SDR SWIA20240418109Access Door · missingCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA77925-690-53-61-1075 838SK MXCODEID61849-PR - DURING POST FLIGHT INSPECTION, FOUND LOW PRESSURE AIR HOOK UP COVER MISSING AND SAFETY WIRE BROKE. COMPLIED WITH TEMPORARY REPAIR OF GOUGE DAMAGE TO LOWER FUSELAGE SKIN BETSDR HNAA2024021900073Rivet · loose53-2049 LOOSE RIVET ON LH SIDE SKIN AT FR80 BTW STR6L-7L. REPAIRED IAW EO1-53-24-0053SDR IPXA2024020952990Skin · corrodedMAIN CABIN CTR WING BOX R/H SIDE SURFACE HAS CORROSION AT STRINGER 15 AND 27.5 INCH FROM CL. (114-02) ORIGINAL MATERIAL THICKNESS OF CENTER WING UPPER FWD & CENTER SKIN AT BLENDED SMOOTH AREAS BETWEEN STA X=-27 & X=-31 ABOVE STRG 15 LOCATION IS 0.159" THICK I.SDR VNAA20240214003Skin · dentedINITIAL INSPECTION: SEVERAL DENTS ON FUSELAGE SKIN, SETTLEMNT AREA OF LEFT AND RIGTH VENTRAL FIN FAIRING BTW FS 1126.00 TO REAR SPAR DATUM STABILIZER 67.5% SEVERAL DENTS ON FUSELAGE SKIN, SETTLEMNT AREA OF LEFT AND RIGTH VENTRAL FIN FAIRING BTW FS 1126.00 TO RSDR IPXA2024020952961Skin · corrodedMAIN CABIN CTR WING BOX R/H SIDE SURFACE HAS CORROSION AT STRINGER 15 BETWEEN STA 1219-1239 (114-01) ACCOMPLISHED EA 011-5730-01-B0145 I/R AND EO-89278-REQ1 ATTACHED TO FAULT T3F18E003Q6BGSDR VNAA202401210020Doubler · corrodedCORROSION ON INNER SKIN OF PRODUCTION DOUBLER STA 295 TO STA 310 BTW STGR 26LH TO STGR 26RH. DUE EXCESSIVE CORROSION ON INNER SKIN OF PRODUCTION DOUBLER STA 295 TO STA 310 BTW STGR 26LH TO STGR 26RH WAS REPLACED PER CRJ-900 SRM 53-00-00-101-001-A01 AND SRM 5SDR DALA2024011100484Unknown · unknownSHIP 3137 ELONGATED HOLES IN FUSELAGE CROWN SKIN AT VIASAT AREA. CORRECTIVE ACTION: RERPAIRED PER ER/A 00-605207. (0147416)SDR DALA2024011000461Skin · dentedSHIP 6717 PROTUDING DENT FOUND ON R/H SIDE OF FUSELAGE AT STA 199.09 PLUS (18IN) BETWEEN STRINGER 18R & 19R. CORRECTIVE ACTION: ACCOMPLISHED REPAIR BS 199.09+18 STR 18R-19R I.A.W DELTA ER/A # 614777-14 REV O. (0146952)SDR LR7A2024010903356Skin · damagedDURING SCHEDULED B-3 CHECK UNDER JOB CARD HB5301, FOUND RH FUSELAGE SKIN NICKED AT FS790.0E, WL176, RBL81. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 1001057895.SDR LR7A2024010903355Skin · dentedDURING SCHEDULED B-3 CHECK UNDER JOB CARD HB5301, FOUND LH EXTERIOR FUSELAGE SKIN DENTED AT FS389, WL219, LBL83. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 1001057890.SDR LR7A2024010903354Skin · gougedDURING SCHEDULED B-3 CHECK UNDER JOB CARD HB5301, FOUND FUSELAGE SKIN GOUGED AT FS762.0E, WL146, LBL65. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 1001065386.SDR LR7A2024010903346Skin · gougedDURING SCHEDULED B-3 CHECK UNDER JOB CARD HB5301, FOUND FUSELAGE BELLY SKIN GOUGED AT FS759.0E, RBL44, WL133. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 1001059426.SDR LR7A2024010903345Skin · gougedDURING SCHEDULED B-3 CHECK UNDER JOB CARD HB5301, FOUND FUSELAGE BELLY SKIN GOUGED AT FS777.0E, RBL30, WL126. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 1001059425.SDR LR7A2024010903344Skin · gougedDURING SCHEDULED B-3 CHECK UNDER JOB CARD HB5301, FOUND FUSELAGE BELLY SKIN GOUGED AT FS249, LBL6 WL126. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 1001059388.SDR LR7A2024010903341Skin · gougedDURING SCHEDULED B-3 CHECK UNDER JOB CARD HB5301, FOUND FUSELAGE BELLY SKIN GOUGED AT FS257, LBL15, WL126. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 1001057983.SDR LR7A2024010903340Skin · gougedDURING SCHEDULED B-3 CHECK UNDER JOB CARD HB5301, FOUND FUSELAGE BELLY SKIN GOUGED AT FS248, RBL19, WL127. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 1001057942.SDR LR7A2024010903339Skin · gougedDURING SCHEDULED B-3 CHECK UNDER JOB CARD HB5301, FOUND FUSELAGE BELLY SKIN GOUGED AT FS357, LBL6, WL126. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 1001057928.SDR DALA2024010900386Unknown · unknownSHIP 1603 AGING AIRCRAFT INSPECTION ITEM- PREVIOUS DOUBLER REPAIR - NUT LOOSE ON FASTENER BELOW S-28R BETWEEN STA 1395 AND STA 1417, AFT OF AFT CARGO DOOR. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER ERA 614744-14. (0146259)SDR HNAA2024021900071Skin · corroded53-2019 CORROSION STR21L BTW SKIN JUNCTION 3 AND FR24. REPAIRED IAW EO1-53-24-0056SDR V0XR20240116AV1Skin · corrodedREAR FUSELAGE I SKIN DAMAGED FORWARD OF THE CARGO DOOR AT FRAME 61 AND STRINGER 17L. THE DAMAGE IS ALONG THE RIVETS AND LOOKS LIKE A CRACKED PUNCTURE. AFTER FURTHER INSPECTION, THE CORROSION GOES COMPLETELY THROUGH. REPAIRED IAW EMBRAER ETD2021-145-000003 REV.SDR DALA2024010900387Unknown · unknownSHIP 1603 ERA 614744-14 SECTION I ISSUED FOR REPAIR AT STA 1395, STR 26R-2 9R. FOLLOW ON ACTION IS REQUIRED. CORRECTIVE ACTION: ACCOMPLISH ERA 614744-14 SECTION II EVERY 12K CYCLES AFTER SECTI ON I. (0145745)SDR CALA2024030700650Skin · damagedGASH CAUSED BY TOWBARLESS TRACTOR PENETRATED FUSELAGE SKIN AT STATION 471 FROM STR.39L TO 37R. IN ADDITION SRATCHES AT STA. 513 FROM STR. 39R TO 40L FUSELAGE REPAIR WAS PERFORMED BY BOEING. AIRCRAFT RETURNED TO UAL-RE-2400413. FAA 8100-9 DTD. 03/04/2024. ECRASDR SWIA20240202107Skin · dentedFORWARD FUSELAGE EXTERNAL SKIN IS DENTED BETWEEN FRAMES 9 - 10 AND STRINGER 18L - 20L. (C-CHECK RO 2/2/2024) PERFORMED EXTERNAL FILLER AND DOUBLER REPAIR AT FR 9-10 STGR 18-20L. REF ETD2024-170-000738. WEIGHT ADDED FOR DOUBLER REPAIR IS 370G. THIS DOES NOTSDR VNAA202401220009Skin · dentedDENT ON EXTERNAL FUSELAGE SKIN BTW FS 169.00 TO FS 173.00 BTW STGR 19 LH TO STGR 23 LH, WL 87.90. DENT ON EXTERNAL FUSELAGE SKIN BTW FS 169.00 TO FS 173.00 BTW STGR 19 LH TO STGR 23 LH, WL 87.90. WAS REPAIRED PER. REO 690-53-11-1660 REV -- AND REO 670-51-00-SDR IPXA2024011019213Unknown · unknownFWD LOWER CARGO DOOR CUT OUT, AFT EDGE SKIN PREVIOUS BLENDOUT DAMAGE. BLENDED OUT DAMAGE TO PREVIOUS CUTOUT, NEW DIMENSIONS ARE 10.00 INCH VERTICAL X .350 DEEP. APPLIED PRIMER AND PAINT AS REQ. REF. SRM 53-00-15-2R-8 REPAIR 8 AND AMM 51-22-00.SDR DALA2024010900353Not Reported · not reportedSHIP 3310 DURING CURRENT H CHECK, WHILE EXECUTION OF JC 5310-01461-03 IN ORDER TO PERFORM A330-SB-53-3273 REV 2 AND OVERSIZED HOLE WAS FOUND (G4) BETWEEN FR53.6 AND FR53.7 AT STGR5LH. CORRECTIVE ACTION: REF ER/A 514675-14AD. (0144774)SDR IPXA2024010819213Unknown · unknownFWD LOWER CARGO DOOR CUT OUT, AFT EDGE SKIN PREVIOUS BLENDOUT DAMAGE.SDR IPXA2024021902794Skin · dented*SUPPLEMENTAL SDR* FAULT- SECTION 46 FUSELAGE SKIN REPAIR DOUBLE ONE DENT , STA1920-1940, S-31~S32R.(EVALUATE) 1.MEASURE DENT DIMENSION LENGTH:2.4", WIDTH:1.35", DEPTH:0.034, A/Y:39.7 AND PERFORMED EO-89159-REQ1 REV.1. 2.JOB COMPLETED.REVIEWEDSDR IPXA2024012908224Skin · damaged*** SUPPLEMENTAL SDR *** FAULT- TWO SCRATCHES 0N THE RIGHT SIDE FUSELAGE SKIN AT STA 320, S-14R. DOT 8-001 AFTER FURTHER EVALUATION NO DAMAGE WAS FOUND. ONLY TOP COAT WAS AFFECTED. CLEANED AREA PER SOPM 20-30-03. NO MATERIAL LOST. VERIFIED WITH TR T17807 + TR8SDR CALA2024012200165Skin · damagedDUE TO THE AUTOMATIC DIRECTION FINDER (ADF) AREA STILL HAVE MARKS, GROOVES/SCRATCHES, THIS CAUSED ERROUNEOUS RESULT ON NDT INSPECTION. REWORK THE AREA AS PER APPLICABLE PROCEDURES. MORE DETAILS PICTURES ATTACHED. CLASSIFIED AS MAJOR REPAIR . . NECESSARY TO ACCSDR CALA2024011700127Skin · crackedSUPPORT TASK - EA 5310-07557 OP 002 - 1EA CRACK FOUND ON LH UNDERWING LONGERON FTG FX SKIN FASTENER HOLE, CRACK RUNNING TO AFT DIRECTION APPROX 0.125" IN DEPTH STARTING FROM I/B EDGE TRANSFER REF NON - ROUTINE WO.2622006 AND ORIG BY V924734 RON DOUBLER INSTALLSDR DALA2024010800311Unknown · unknownSHIP 3310 CRACK INDICATION FROM 14I HOLE LOCATED AT RH STRG 15A LEVEL AT UPPER FUSELAGE. CRACK DIRECTION IS 11 OCLOCK AND CRACK DEPTH IS 0.083 INCH. FOR AD MANDATED DOCUMENTS AN AMOC MAY BE REQUIRED. REFERENCE EM 5310-01461 AND AIRBUS SB A330-53-3273 REV 02. C
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