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.

SDR DALA2023042803341Unknown · unknownSHIP 3402 DURING C CHECK IN MSP, MAINTENANCE WAS ACCOMPLISHING A PERMANENT REPAIR TO A DENT ON THE FUSELAGE PER LP 6618724. THE SKIN IS P/N F53275116200. IT IS MADE FROM 0.110 THICK 6013HDT/6156 T4 HT TO -T62 CLAD SHEET. LOCALLY, THE AREA IS 0.063 THICK. PERApr 15, 2023 · N402DX · Airbus A330941SDR DALA2023041703042Unknown · unknownSHIP 3401 FOUND GOUGE ON EMPENNAGE SKIN APPROX 11" AFT OF FRAME 80 BETWEEN STRINGER 48R AND 49R. CORRECTIVE ACTION: REPAIRED PER PRI 607734-14 REV O, REV 1, REV2 AND ER/A 607734-14 REV O. OK FOR SERVICE. (2721067)Apr 15, 2023 · N401DZ · Airbus A330941SDR DALA2023041703034Unknown · unknownSHIP 1702 LIGHTNING STRIKE DAMAGE AT STA 325 BETWEEN STR 28-29R. CORRECTIVE ACTION: SUPPLEMENTING LOG. 10 X MAGNIFIED INSPECTION REQUIRED EVERY 1,500 FLIGHT CYCLES. PERMANENT REPAIR REQUIRED IN 6,000 CYCLES PER B767-300 SRM 53-00-01-2R-8. (2721572)Apr 15, 2023 · N172DZ · Boeing 767332SDR DALA2023041703023Unknown · unknown(LOG 2720387) WHILE LAYOVER IN ATL, MTC REPORTED DENTS LOCATED AT SECTION 46, THE DENTS ARE LOCATED APPROXIMATELY 2.0 FWD FROM STA 888 BETWEEN STR 27L AND 27R. REPAIRED DAMAGE PER ERA 607906-14.Apr 15, 2023 · N808DN · Boeing 737932ERSDR IXXA20230415001Skin · corrodedFOUND PAINT DAMAGE OUT OF LIMITS AT STR.39R STA. 1486Apr 15, 2023 · N739AX · Boeing 767SDR SWAA2023041827588Radome · delaminatedFOUND HOLE IN CENTER OF RADOME WITH HONEYCOMB MISSING.<[01] DELAMINATION MEASUREMENT IS 1.0? L BY 0.90 H.;[02] COMPLIED WITH EA; TASK CARD # 23-153-01233Apr 14, 2023 · N561WN · Boeing 73773VSDR DALA2023041703041Unknown · unknownSHIP 3401 (DTE)DAMAGE TOLERANCE EVALUATION DUE WITHIN 6 MONTHS PER ER/A 607734-14. CORRECTIVE ACTION: COMPLIED WITH INSP. (2719618)Apr 14, 2023 · N401DZ · Airbus A330941SDR DALA2023042703275Unknown · unknownSHIP 3351 DURING ACCOMPLISHMENT OF THE MOCK-UP FOR EM 5330-01152 MTC HAS REPORTED SEVERAL DEVIATIONS THAT REQUIRED ADDITIONAL OR ALTERNATE INSTRUCTIONS TO THE EXISTING WORK STEPS TO BE ABLE TO ACCOMPLISH THEM. CORRECTIVE ACTION: REF VA 101000. (2717632)Apr 13, 2023 · N851NW · Airbus A330223SDR DALA2023042703274Unknown · unknownSHIP 3356 DURING ACCOMPLISHMENT OF THE MOCK-UP FOR EM 5330-01152 MTC HAS REPORTED SEVERAL DEVIATIONS THAT REQUIRED ADDITIONAL OR ALTERNATE INSTRUCTIONS TO THE EXISTING WORK STEPS TO BE ABLE TO ACCOMPLISH THEM. CORRECTIVE ACTION: REF VA 101000. (2717709)Apr 13, 2023 · N856NW · Airbus A330223SDR DALA2023041603008Skin · corroded(LOG 2717867) DURING INSPECTION FOUND CORROSION ON UPPER FUSELAGE EXTERIOR SKIN UNDER ADF 2 ANTENNA STA 727+9-727B STR 1-2R. REPAIRED CORROSION ON UPPER FUSELAGE EXTERIOR SKIN UNDER ADF2 ANTENNA STA 727-727B, STR 1-2R I.A.W ER/A 607358-14.Apr 13, 2023 · N931DQ · Boeing 7379GPERSDR SWAA2023041726251Doubler · crackedEXTERNAL POWER DOOR SURROUND STRUCTURE HAS A CRACK ON THE DOUBLER IN ZONE 1.<[01] REMOVED AND CONTOURED DAMAGE AS NEEDED. NO DAMAGE TO PREVIOUSLY INSTALLED DOUBLER. REMOVED AND REPLACED FILLER. ALL WORK DONE PER SRM 53-10-15-2R-4 REPAIR 4. THIS IS A PERMANENT Apr 12, 2023 · N460WN · Boeing 7377H4SDR DALA2023041402973Unknown · unknownSHIP 3354 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR INTERNAL STRUCTURE MODIFICATION DOUBLER AT FR84, STR5AR IN UPPER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH PRI 606202-14 REV. 0, VALIDATED ER/A 606202-14 REV. ORIGINAL MATCHES PRI 606202-14 REV.0. (27168Apr 12, 2023 · N854NW · Airbus A330223SDR DALA2023041402972Unknown · unknownSHIP 3354 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR INTERNAL STRUCTURE MODIFICATION DOUBLER AT FR84, STR2AR IN UPPER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH PRI 606202-14 REV. 0, VALIDATED ER/A 606202-14 REV. ORIGINAL MATCHES PRI 606202-14 REV. 0. (2716Apr 12, 2023 · N854NW · Airbus A330223SDR DALA2023041402967Unknown · unknownSHIP 3354 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR SKIN LOCATED LOWER LH SIDE STRINGER BTW FR11 TO FR12 AT LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH PRI 607246-14 PRI REV. 0, PRI REV. 1 VALIDATED ERA 607246-14 REV. ORIGINAL MATCHES. (2716534)Apr 12, 2023 · N854NW · Airbus A330223SDR YENA2023041300385Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION TRAILING EDGE UPPER SKIN LOWER SURFACE OVERHANG AREA BTW RIB 15 AND RIB 16 ON RH WING; (RESOLVED ON W/O: 1200126 TASKCARD: NR-00037 ) REF AEM NR 2023-68586 FOR ALL WORK ACCOMPLISHED, REPAIR MULTI-SITE CORROSION SPOTS FOUND OApr 12, 2023 · N529JB · Airbus A320232SDR DALA2023041302958Unknown · unknownSHIP 3354 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR INTERNAL STRUCTURE DOUBL ER AT FR86, STR2BL IN UPPER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH PRI 606202-14 REV. 0, VALIDATED ER/A 606202-14 REV. EXISTING MODIFICATIOINSTALLED AS PER EM 5330-01151-05B. Apr 12, 2023 · N854NW · Airbus A330223SDR DALA2023041302956Unknown · unknownSHIP 3354 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR INTERNAL STRUCTURE DOUBLER AT FR86,STR2BR IN UPPER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH PRI 606202-14 REV. 0, VALIDATED ER/A 606202-14, EXISTING MODIFICATION INSTALLED AS PER EM 5330-01151-05B. MODIApr 12, 2023 · N854NW · Airbus A330223SDR DALA2023041302955Unknown · unknownSHIP 3354 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR INTERNAL STRUCTURE MODIFICATION DOUBLER AT FR84, STR 2AL. CORRECTIVE ACTION: COMPLIED WITH PRI 606202-14, VALIDATED ER/A 606202-14 MATCHES PRI 606202-14. EXISTING MODIFICATIONINSTALLED AS PER EM 5330-0115Apr 12, 2023 · N854NW · Airbus A330223SDR DALA2023041302954Unknown · unknownSHIP 3354 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR INTERNAL STRUCTURE MODIFICATION DOUBLER AT FR84,STR5AL IN UPPER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH PRI 606202-14, VALIDATED ER/A 606202-14 MATCHES PRI 606202-14 EXITING MODIFICATION INSTALLED AS PApr 12, 2023 · N854NW · Airbus A330223SDR DALA2023041302953Unknown · unknownSHIP 3354 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR SKIN LOCATED ON EXTERNAL SKIN FR 11 TO FR 11A APPROX 13 INCH FROM STR 30 ON RH SIDE. CORRECTIVE ACTION: COMPLIED WITH PRI 606202-14, VALIDATED ER/A 606202-14 MATCHES PRI 606202-14. EXISTING REPAIR INSTALLApr 12, 2023 · N854NW · Airbus A330223SDR DALA2023041302952Unknown · unknownSHIP 3354 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR INTERNAL STRUCTURE MODIFICATION DOUBLER AT FRAME 86 STRINGER 2BL IN UPPER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH PRI 606202-14, VALIDATED ER/A 606202-14 MATCHES PRI 606202-14. EXISTING MODIFICATION INApr 12, 2023 · N854NW · Airbus A330223SDR DALA2023041302951Unknown · unknownSHIP 3354 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR INTERNAL STRUCTURE MODIFICATION DOUBLER AT FRAME 86 ,STR2BR IN UPPER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH PRI 606202-14. VALIDATED ER/A 606202-14 MATCHES PRI 606202-14. EXISTING MODIFICATION INSTALLApr 12, 2023 · N854NW · Airbus A330223SDR DALA2023041302950Unknown · unknownSHIP 3354 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN FR 13 AND 32 INCHES ABOVE LAP JOINT AT LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH PRI 606202-14 VALIDATED ER/A 606202-14 MATCHES PRI 606202-14. EXISTING REPAIR INSTALLED PERA330 SRM 53Apr 12, 2023 · N854NW · Airbus A330223SDR DALA2023041302949Unknown · unknownSHIP 3354 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR INTERNAL STRUCTURE MODIFICATION DOUBLER AT FRAME 86 , STR 5AL IN UPPER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH PRI 606202-14, VALIDATED ER/A 606202-14 MATCHES PRI 606202-14. (2716235)Apr 12, 2023 · N854NW · Airbus A330223SDR DALA2023041302948Unknown · unknownSHIP 3354 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR INTERNAL STRUCTURE DOUBLER AT FR84 AT LEVEL OF STRG 2AR ON UPPER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH PRI 606202-14, VALIDATED ER/A 606202-14 MATCHES PRI 606202-14. EXISTING MODIFICATION INSTALLED AApr 12, 2023 · N854NW · Airbus A330223SDR DALA2023041302947Unknown · unknownSHIP 3354 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR SKIN AT FR 10 AND 7 INCH ES FROM CENTER LINE ON UPPER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH PRI 606202-14, VALIDATED ER/A 606202-14 MATCHES PRI 606202-14. EXITING REPAIR INSTALLED PER A330 SRM 53-11-Apr 12, 2023 · N854NW · Airbus A330223SDR DALA2023041302946Unknown · unknownSHIP 3354 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR PASSENGER CREW DOOR L4 EXTERNAL SKIN AFT LOWER CORNER AREA IN PASSENGER CABIN. CORRECTIVE ACTION: COMPLIED WITH PRI 606202-14, VALIDATED ER/A 606202-14 MATCHES PRI 606202-14. EXISTING REPAIRINSTALLED PER Apr 12, 2023 · N854NW · Airbus A330223SDR DALA2023041302945Unknown · unknownSHIP 3354 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR INTERNAL STRUCTURE MODIFICATION DOUBLER FR86, STR5AR IN UPPER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH PRI 606202-14. VALIDATED ER/A 606202-14 MATCHES PRI 606202-14. EXISTING MODIFICATION INSTALLED AS PApr 12, 2023 · N854NW · Airbus A330223SDR DALA2023041302944Unknown · unknownSHIP 3354 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR SKIN AT FR27 TO FR28 BTW STR38R TO STR39R AT LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH PRI 606202-14, VALIDATED ER/A606202-14 MATCHES PRI 606202-14 EXISTING REPAIR INSTALLED PER A330 SRM 53-21-11-3Apr 12, 2023 · N854NW · Airbus A330223SDR DALA2023041302943Unknown · unknownSHIP 3354 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR SKIN AT FR30 TO FR31 BTW 27L TO STR28L AT LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH PRI 606202-14, VALIDATED ER/A 606202-14 MATCHES PRI 606202-14. EXITING REPAIR INSTALLED PER A330 SRM 53-21-11-300Apr 12, 2023 · N854NW · Airbus A330223SDR DALA2023041302929Unknown · unknownSHIP 3230 FUSELAGE SKIN FR15-FR16 SPLICE REPAIR DUE TO BIRD STRIKE. CORRECTIVE ACTION: COMPLIED WITH ERA 605603-14 REV ORIG. (2716420)Apr 12, 2023 · N330NW · Airbus A320211SDR DALA2023041302907Unknown · unknownCRACKS ON EXTERNAL FUSELAGE SKIN STA Y=1076 AND BTW L13-RH TO L14-RH. SUMMARY OF NRC 00041: EXTERNAL FUSELAGE SKIN STA Y=1076 AND BTW L13-RH TO L14-RH WAS REPAIRED PER PRI 607016-14 REV 1 AND ER/A 607016-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. (LP #271666Apr 12, 2023 · N891AT · Boeing 717200SDR DALA2023041302905Unknown · unknownCRACKS ON EXTERNAL FUSELAGE SKIN STA Y=1087 AND BTW L13-RH TO L14-RH. SUMMARY OF NRC 00042: EXTERNAL FUSELAGE SKIN STA Y=1087 AND BTW L13-RH TO L14-RH WAS REPAIRED PER PRI 607016-14 REV 1 AND ER/A 607016-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. (LP #271652Apr 12, 2023 · N891AT · Boeing 717200SDR DALA2023041202875Unknown · unknownSHIP 3354 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR INTERNAL STRUCTURE DOUBLER FR84 AT LEVEL OF STR2AL ON UPPER FUSELAGE. CORRECTIVE ACTION: REF ER/A 606202-14. (2715825)Apr 12, 2023 · N854NW · Airbus A330223SDR DALA2025013000728Skin · crackedFUSELAGE SKIN Y=1037, L13R TO L14R HAS CRACK REPAIR & INSPECTIONS. ACCOMPLISH ER/A 606978-14 REV A SECTION II INSPECTION WITHIN EVERY 15,000 CYCLES AFTER ACCOMPLISHMENT OF SECTION I REPAIR. ASSOCIATED ER/A 00-606978 ADDED FOR AC 9551. (LP #0786135)Apr 11, 2023 · N891AT · Boeing 717200SDR DALA2023051903991Unknown · unknownER/A 607628-14 ISSUED FOR LIGHTNING STRIKE DAMAGE ON THE FWD-MID FUSELAGE SKIN (FR35-FR38, STR-8L TO STR-9L). ASSOCIATED ER/A 00-607628 ADDED FOR AC 8117. (LP# 2715274)Apr 11, 2023 · N117DU · Airbus BD5001A10SDR DALA2023041202872Unknown · unknownSHIP 3354 DURING HCK, MULTIPLE LIGHTNING STRIKES WERE FOUND ON EXISTING DOUBLER INSTALLED PER ERA 503083-14, REV A. THE INSTALLED REPAIR WAS REMOVED AND NEW REPAIR INSTALLED. CORRECTIVE ACTION: REF ERA 607246-14. (2714778)Apr 11, 2023 · N854NW · Airbus A330223SDR DALA2023041202871Unknown · unknownSHIP 3354 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR SKIN LOCATED LOWER LH SI DE STRINGER BTW FR11 TO FR12 AT LOWER FUSELAGE. CORRECTIVE ACTION: REF ER/A 607246-14. (2715280)Apr 11, 2023 · N854NW · Airbus A330223SDR EE4Y2023041117589Skin · damagedDURING THE STRUCTURAL INSPECTION, IT WAS FOUND A BLEND OUT EXCEEDED 50 PERCENT OF THE SKIN THICKNESS. ALLIANCE INTENDS TO PERFORM A REPAIR FOLLOWING SRM II 53-22-01 REPAIR 63 GUIDELINES; HOWEVER, THE DAMAGED AREA IS LOCATED IN A NON-ALLOWED REPAIR AREA AS PERApr 11, 2023 · N934QQ · Emb ERJ190100IGWSDR EE4Y2023041117586Skin · damagedDURING THE STRUCTURAL INSPECTION, IT WAS FOUND AN EXISTING REPAIR WITHOUT RECORDS IN THE FUSELAGE SKIN, LOCATED BETWEEN FRAMES 83-84 AND BETWEEN STRINGERS 13L-16L. WAS REPAIRED FOLOWING EMB REPAIR INSTRUCTIONS UNDER ETD2023-190-003976 REV / AND COOPESA EO# COOApr 11, 2023 · N934QQ · Emb ERJ190100IGWSDR SWAA2023051825558Shield · corrodedR/H FLOOR TO SIDEWALL SHIELD CORROSION; BS500+2; +6; +10; +14; RBL24; WL156; R/H FLOOR TO SIDEWALL SHIELD CORROSION BS500+2 +6 +10 +14 RBL24 WL156<[01] REMOVED CORROSION FROM 6 SPOTS ON PART 143A8126Y36. THE DEEPEST SPOT IS 1.00 X 1.50 DEPTH 0.015. ORDINAL THIApr 10, 2023 · N958WN · Boeing 7377H4SDR SWAA2023051725559Support Angle · corrodedR/H FLOOR TO SIDEWALL SUPPORT ANGLE CORROSION; BS500A +2; 6; 10; BS500B+10; +14; BS500C +7; +10; RBL24; WL156<[01] VERIFIED APPLICABILITY IAW SRM 53-30-53-01-2 AND SRM 53-00-53-1A-2;[02] REMOVED CORRSION AT<BR><BR>BS 500A+2 0.005'(OUT OF LIMIT) - THE DEEPEST DApr 10, 2023 · N958WN · Boeing 7377H4SDR DALA2023051703934Unknown · unknownSHIP 3230 SRM REPAIR FOLLOW-ON INSPECTION REQUIRED FOR BUSHING REPAIR OF FUSELAGE SKIN PER ER/A 607816-14 AT FR11, RHS, ABOVE W/S UPPER SILL. CORRECTIVE ACTION: COMPLIED WITH. (2713274)Apr 10, 2023 · N330NW · Airbus A320211SDR SWIA2023042800009Unknown · noneLIGHTNING STRIKE DAMAGE ON SKIN BETWEEN FR02 AND FR03 AND BETWEEN STR28L AND STR26L. (C-CHECK RO 4/27/2023) PERFORMED THROUGH HOLE REPAIR BY DRILLING AND INSTALLING SOLD RIVET ON LIGHTNING STRIKE DAMAGE REF. ETD2023-170-009369.Apr 9, 2023 · N194SY · Emb ERJ170200LRSDR UIEA2023040500314Unknown · unknownLOWER HALF FUSELAGE, EXTERNAL SKIN. LIGHTNING STRIKE ON RIVET HEAD BELLOW 11" FROM STG 21 LH AT STA172.5(<P>LOWER HALF FUSELAGE, EXTERNAL SKIN FROM STG 21 LH AT STA172.5 RIVET WAS REMOVED AND REPLACED. AREA WAS INSPECTED AND NOT FOUND DAMAGE NOTED SRM 51-40-02Apr 9, 2023 · N662GT · Boeing 76731ASDR DALA2023040902731Unknown · unknownSHIP 3082 STRINGER 44 DOUBLER BETWEEN FR28 AND FR31 DAMAGED. CORRECTIVE ACTION: INSTALLED NEW DOUBLER PER A321 SRM 51-44. (2710933)Apr 9, 2023 · N382DN · Airbus A321211SDR DALA2023040902727Unknown · unknownSHIP 3082 FUSELAGE SKIN DAMAGE APPROX FR29 TO FR31 S44 TO S41L. CORRECTIVE ACTION: REPLACED SKIN PER A321 SRM 51-42. (2710922)Apr 9, 2023 · N382DN · Airbus A321211SDR FDEA202304070588Skin · damagedR/H EXTERIOR FUSELAGE SKIN DOUBLER HAS 2EA DENTS BETWEEN BS 540 AND BS 560 AND STRINGER S-22R AND STRINGER S23R REPAIRED PER FEDEX EA # F-5330-165083-P3Apr 7, 2023 · N938FD · Boeing 757200SDR DALA2023041002752Unknown · unknownSHIP 3230 FORWARD FUSELAGE UPPER FO BIRD STRIKE DAMAGE SITE #3 FR9. CORRECTIVE ACTION: COMPLIED WITH MAJOR REPAIR (2708839)Apr 7, 2023 · N330NW · Airbus A320211SDR IXXA2024041705Skin · crackedR/H FUSELAGE SKIN AT R1 DOOR LOWER CORNER CUTOUT CRACK INDICATION STA 335, STR 20RApr 6, 2023 · N389AZ · Boeing 767319
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