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 SWAA2022072524870Shield · corrodedCORROSION ON AFT CARGO BAY FWD DOOR SHIELD AT RBL 22 BS 767+3; BS 767+7; BS 767+15. / [01] CORROSION ON SHIELD WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.;[02] VERIFIED CORRECTIVE ACTION ITEM 1;[03] REMOVED AFT CARGO BAY FWD DOOR SHIELJul 1, 2022 · N8641B · Boeing 7378H4SDR DALA2022070504619None · none(LOG 2301942) DURING INSPECTION FOUND DENT ON FUSELAGE SKN BELOW CAPTAINS WINDOW. DENT ON FUSELAGE SKN BELOW CAPTAINS WINDOW WAS REPAIRED PER ER/A 600277-14 REV. ORIGINAL AND PRI 600277-14 REV. 0.Jul 1, 2022 · N801DZ · Boeing 737SDR SWAA2022072724552Baffle · crackedFWD CARGO COMP. LEFT SIDE BAFFLE IS CRACK AT FWD END BETWEEN STA 500A AND 500B LBL-24. / [01] REMOVED FWD CARGO LT.SIDE BAFFLE AT STA 500A AND 500B LBL 24 IN REF SRM 51-40-02-0G-0;[02] VERIFIED STEP 1;[03] PEROFRMED HFEC ROTO INSP ON FASTENER OPEN HOLES; IAW BJun 30, 2022 · N7732A · Boeing 7377BDSDR SWAA2022072734896Baffle · crackedFWD CARGO COMP. LEFT SIDE BAFFLE IS CRACK AT FWD END BETWEEN STA 500A AND 500B LBL-24. / [01] REMOVED FWD CARGO LT.SIDE BAFFLE AT STA 500A AND 500B LBL 24 IN REF SRM 51-40-02-0G-0;[02] VERIFIED STEP 1;[03] PEROFRMED HFEC ROTO INSP ON FASTENER OPEN HOLES; IAW BJun 30, 2022 · N7732A · Boeing 7377BDSDR SWAA2022072724554Channel · crackedFWD CARGO COMP. RIGHT/Z-CHANNEL HAS A CRACK BETWEEN STA 500C-STA 500D RBL-24. / [01] LOCATED AND DRILLED NEW FWD CARGO RT. SIDE 'Z' CHANNEL IN REF SRM 51-40-05-0G-0;[02] VERIFIED STEP # 1;[03] TREATED AND PRIMED FWD CARGO RT. Z CHANNEL AS PER SRM 51-20-01-0G-0Jun 30, 2022 · N7732A · Boeing 7377BDSDR FDEA202206301621Skin · unknownAGING AIRCRAFT - EXISTING REPAIR DOUBLER FOUND ON FUSELAGE SKIN AT STATION 392 LONGERON 25 RIGHT HAND. EXISTING REPAIR DOUBLER ON FUSELAGE SKIN AT STATION 392 LONGERON 25 RIGHT HAND EVALUATED AND FOUND REPAIRED IN ACCORDANCE WITH SRM 53-00-01-2R REPAIR 7 FJun 30, 2022 · N593FE · Doug MD11SDR FDEA202206301746Skin · unknownAIRCRAFT REPAIR ASSESSMENT:EXISTING EXTERNAL DOUBLER REPAIR FOUND ON FUSELAGE SKIN AT FR85,BTW STGR41L-44L. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: A300/A310 RPR IDENT&SUPPLEMENTAL MX REQ(SMR) TRK, INSPECTION OF EXISTING REPAIR DETEJun 30, 2022 · N721FD · Airbus A300*SDR DALA2022070104601None · none(LOG 2300979) DURING INSPECTION DENT DAMAGE WAS FOUND ON FUSELAGE SKIN AT STATION 224.8 AND S-21L. MAINTENANCE REPAIRED DAMAGE PER ERA 600277-14.Jun 30, 2022 · N801DZ · Boeing 737SDR DALA2022070604708None · noneSUPPLEMENTAL INFORMATION SHIP 3308 UPON ARRIVAL IN ATL, MTC FOUND A V-SHAPED GOUGE ON THE NOSE FWD FUSELAGE RH SKIN. JUST FWD OF FR13 AND ABOVE STR 30. ONE LEG OF THE GOUGED AREA MEASURES 2.50 INCHES IN LENGTH WHILE THE OTHER IS 5.00 INCHES IN LENGTH WITH MAXIJun 29, 2022 · N808NW · Airbus A330323SDR ASAA2022062939285Shear Plate · corrodedMAIN CABIN R/H AT FR69 ON LATERAL SHEAR PLATE HAS CORROSION ON TOP SURFACE GROUNDED - YES. REMOVED & REPLACED SHEAR PLATE AT FRAME 69 (RIGHT HAND SIDE) REFERENCE A320 SRM 51-42-11 & AIRBUS DRAWING D53474180. P/N D534711242030 PO 1030042.1Jun 29, 2022 · N364VA · Airbus A320214SDR DALA2022070604715None · noneMON, 30 L/L, 8116638;DENT;ABOVE L1 FWD EDGE; 3090;LARGE DENT / CREASE JUST ABOVE FWD EDGE OF L1 DOOR ON UPPER FUSELAGE SKIN FOA. REPAIRED DENT ON EXTERIOR FUSELAGE SKIN AT FR11 APPROX. 30" ABOVE L3 COCKPIT WINDOW IAW A321 SRM 53-11-11-300-041. REPAIR IS CAT B.Jun 29, 2022 · N390DN · Airbus A321211SDR DALA2022070104612None · noneSHIP 3316 ERA 598076-14 SECTION II ACCOMPLISHED IN MSP. FOLLOW ON ACTION I S REQUIRED. CORRECTIVE ACTION: ERA 598076-14 SECTION II REPAIR IS TIME LIMITED TO 6 MONTHS. FUR THER DTE (DAMAGE TOLERANCE EVALUATION) IS REQUIRE FOR AIRCRAFT T O FLY BEYOND THIS LIMIT.Jun 29, 2022 · N816NW · Airbus A330323SDR IPXA2022062983615Skin · damagedINSPECTION TYPE:SEG4RIGHT SIDE LOWER FUSELAGE LIGHTNING STRIKE DAMAGED REPAIR AT STA 700 AND S-24 R PERMANENT REPAIRREMOVE TEMPORARY REPAIR DOUBLER PER SRM 51-40-02, FABRICATED AND INSTALLED NEW DOUBLER ON MATERIAL 2024-T3 .071" PER 53-00-01-2R-29Jun 29, 2022 · N413UP · Boeing 75724APFSDR MK1Y20220629008Frame · crackedDURING MAINTENENCE INSPECTION FOUND CRACK ON THE FRAME INNER CHORD AT STA 632, STR 13R TO STR 14RJun 29, 2022 · N279CJ · Boeing 767306SDR MK1Y20220629007Frame · dentedDURING MAINTENENCE INSPECTION FOUND DENT ON LARGE CARGO DOOR SURROUND STRUCTURE, AFT FRAME WEB, STA 618 BETWEEN STR 29R AND STR 30R.Jun 29, 2022 · N279CJ · Boeing 767306SDR MK1Y20220629001Skin · damagedDURING MAINTENENCE INSPECTION FOUND IMPACT DAMAGE THAT CAUSE TORN SKIN ON FUSELAGE AT STA 1926, BL 0 TO RBL 5.Jun 29, 2022 · N279CJ · Boeing 767306SDR DALA2022091306081None · noneER/A 596427-14 HAS BEEN REVISED TO 'A'. FOLLOW ON ACTION IS REQU IRED. PERFORM SECTION II WITHIN 2400FC OF SECTION I (FROM 3820FC TOTAL ). SECTION II IS TBD PENDING FURTHER DAMAGE TOLERANCE ANALYSIS ( DTA ) OR SKIN PANEL CHANGE. ASSOCIATED ER/A 14-596427 ADDEDJun 28, 2022 · N362DN · Airbus A321213SDR SWIA2022081666285Skin · gougedEXTERNAL FUSELAGE BETWEEN FS969.00 TO FS985.00 AT STGR27 IS GOUGED (WHERE AFT TO BODY FAIRING IS LOCATED) (C-CHECK RO 8/14/2022) PERFORMED REPAIRS TO EXTERNAL FUSELAGE FS969.00 TO FS985.00. @ STGR27 IAW REO 670-53-00-695, REV: --, 2022-07-05, REO 670-53Jun 28, 2022 · N608SK · Cndair CL6002C10SDR DALA2022063004585None · noneSHIP 177 ERA 600267-14 ISSUED FOR REPAIR TO STA 1550-1563, STRINGER 24-25 L FORWARD VACUUMOUTLET NOZZLE. FOLLOW ON ACTION IS REQUIRED, CORRECTIVE ACTION: ACCOMPLISH ERA 600267-14 SECTION II INSPECTIONS AT OR BEFORE 30, 000 TOTAL FLIGHT CYCLES, THEN EVERY 3000 Jun 28, 2022 · N177DN · Boeing 767332SDR A6WA202206288198Nut Plate · elongatedTEMPORARY REPAIR TO THE ELONGATED NUT PLATE HOLE IN FUSELAGE STRUCTURE AT STRINGER 19R BETWEEN FS409+80 - FS409+96. ****AIRCRAFT REMOVED FROM SERVICE *** REPAIRED FUSELAGE SKIN NUT PLATE HOLE AT STRINGER 19R BETWEEN FS409+80 TO FS409+96 REF REO 601R-53-31-128 Jun 28, 2022 · N451AW · Cndair CL6002B19SDR A6WA202206288197Panel · dentedFS605.00+1 STRINGER 23L+3 INWARD DENT C/T EXTERIOR SIDE OF SKIN PANEL. ***AIRCRAFT REMOVED FROM SERVICE **** DRESSED BACK DENT AS PER INSTRUCTIONS OUTLINED IN REO 601R-53-61-7829 REV DATED 2022-05-17.Jun 28, 2022 · N451AW · Cndair CL6002B19SDR IPXA2022062883598Support · crackedINSPECTION TYPE:CEXTERNAL LOWER FUSELAGE RH AIRCON BAY AFT PANEL SUPPORT BRACKET CRACKED.INTSALLED SUPPORT BRACKET IAW-SRM 51-40-21.Jun 28, 2022 · N153UP · Airbus A300*SDR FDEA202206271567Finger Doubler · noneEXISTING REPAIR DOUBLER FOUND ON EXTERIOR FUSELAGE SKIN AT STATION 675 LONGERON 50 RIGHT HAND. EXISTING REPAIR DOUBLER ON EXTERIOR FUSELAGE SKIN AT STATION 675 LONGERON 50 RIGHT HAND EVALUATED AND FOUND REPAIRED IN ACCORDANCE WITH SRM 53-00-01-2R REPAIR Jun 27, 2022 · N593FE · Doug MD11FSDR IPXA2022071884267Stiffener · crackedINSPECTION TYPE:3CAFT CARGO AT STA 1841 AND RBL 36 VERTICAL STIFFENER IS CRACKED.REMOVED,FABRICATED, REPLACED VERTICAL STIFFENER IAW SRM 51-31-01 AND 51-33-01 (MINOR)Jun 27, 2022 · N290UP · Doug MD11FSDR SWAA2022071223311Panel · crackedCRACKED PANEL BREAK STA 540; BL0-RBL 25; WL 208. / [01] REPLACED CRACKED PANEL BREAK STA 540; BL0-RBL 25; WL 208 PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; REF IPC 53-42-11-66.;[02] VERIFIED CORRECTIVE ACTIONS STEP 1.Jun 27, 2022 · N8695D · Boeing 7378H4SDR SWAA2022071223312Panel · crackedCRACKED PANEL BREAK STA 540; BL0-LBL 25; WL 208. / [01] REPLACED CRACKED PANEL BREAK STA 540; BL0-LBL 25; WL 208 PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; REF IPC 53-42-11-66.;[02] VERIFIED CORRECTIVE ACTIONS STEP 1.Jun 27, 2022 · N8695D · Boeing 7378H4SDR IPXA2022070983992Stiffener · crackedINSPECTION TYPE:3CAFT CARGO UNDER FLOOR PANEL 187AF AT STA 1841 AND LBL26 HAS A STIFFENER THAT IS CRACKED.REMOVED, FABRICATED, REPLACED THE STIFFENER IAW SRM 51-33-01 AND 51-31-01 (MINOR)Jun 27, 2022 · N290UP · Doug MD11FSDR IPXA2022070583819Support Angle · crackedINSPECTION TYPE:3CFWD CARGO COMPARTMENT SIDEWALL SUPPORT ANGLE CRACK AT LH SIDE STA.919.REMOVED,FABRICATED AND REPLACED CRACK SUPPORT ANGLE IAW SRM 51-35-01 AND 51-31-01 (MINOR).Jun 27, 2022 · N290UP · Doug MD11FSDR SWAA2022062922821Skin · buckledDENT / BUCKLE ON RH FUSELAGE SKIN BELOW REGISTRATION NUMBER LETTER W & PAX WINDOW STA 876-887 STGR 9R-10R / [01] EVALUATED DIAGONAL BUCKLE / DENT RH FUSELAGE SKIN SECTION 46 ZONE 2 PRIMARY STRUCTURE IAW SRM 51-090-07 & SRM 53-00-01-1A-1. DENT HAS MINIMAL MOVEMJun 26, 2022 · N274WN · Boeing 7377H4SDR DALA2022062804507Skin · corrodedSHIP 178 AFT CARGO COMPARTMENT SKIN CORROSION AT STA1197+10 AND S-36R. CORRECTIVE ACTION: CORROSION REMOVED AND ACCOMPLISHED AS PER PRI 599942-14. (2294464)Jun 26, 2022 · N178DN · Boeing 767332SDR FDEA202206251804None · cracked1EA CRACK INDICATION WAS FOUND AT RIGHT SIDE FR54 STGR44 FASTENER HOLE. ACCOMPLISHED THE WORK BY REAMING THE HOLE THIS IS CATE.B REPAIR I.A.W EA NO:6-5330- T0369235 P1, SEQ NO:000909, TITLE:FUSELAGE-PLATES & SKINS-RH JUNCTION BETWEEN LATERAL SKIN PANEL AND Jun 25, 2022 · N721FD · Airbus A300*SDR SWAA2022070122804Plate · crackedDURING ACCOMPLISHMENT OF 22-153-01522-WIP1[TTG8Q00D7FVA]; OVERSIZED REPAIR FASTENER HOLE LOCATED AT BS 922; S-27R FOUND TO HAVE VISIBLE INTERNAL EDGE DAMAGE AND HFEC HOLE PROBE CRACK INDICATION. / [01] REPAIRED FASTENER HOLE PER EA 22-153-01522.;[02] REPAIRED Jun 25, 2022 · N492WN · Boeing 7377H4SDR FDEA202206241785None · noneTHE LH LOWER FUSELAGE SKIN WAS FOUND DENT FR67 STGR35 ACCOMPLISHED THE CATE.B DOUBLER REPAIR TO THE LH FUSELAGE SKIN I.A.W A300-600 SRM 53- 10-12-201 PARA.5 PAGE.343-346 FIG.224(SHEET-4) & 53-17-12-001 PAGE.42-43 & SRI:53-10-12-201 IIR:53-10-12-2-004-00 PARJun 24, 2022 · N721FD · Airbus A300*SDR Y2PA2022062422034Skin Panel · crackedDISCREPANCY: WHILE AT C-CHECK AT COMMERCIAL JET IN KDHN THE AREA OF THE AFT FUSELAGE STATION 1401 AND LONG 1L, THE REPAIR DOUBLER AND SKIN ON THE FUSELAGE CROWN AREA WAS FOUND CRACKED CORRECTIVE ACTION: COMMERCIAL JET IN KDHN, REMOVED EXISTING DOUBLER, PERJun 24, 2022 · N835US · Doug MD88SDR LR7A2022062403127Skin · corrodedDURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5314, FOUND THE BELLY SKIN CORRODED AT FS277.0E, LBL12-RBL9, WL126. / REPAIRED IAW LOCKHEED SMP583 SRM, FIG. 51-140-12. NR# 1000686326.Jun 24, 2022 · N402LC · Lkheed 382GSDR SWAA2022081122222Baffle · crackedCRACK ON FWD CARGO BAY BAFFLE TO FRAME ATTACH ANGLE AT LBL 24 BS 500B+19. / [01] REMOVED ANGLE IAW SRM 51-40-02-0G-0;[02] RECEIVED NEW CLIP P/N:143A7502U159 ; LOT:1494686-4 AND LOCATED AND DRILLED AT FCB LBL 24 BS 500B+19' IAW SRM 51-40-05 . REQUEST OK TO INSTJun 23, 2022 · N951WN · Boeing 7377H4SDR SWAA2022081122220Baffle · crackedCRACK ON FWD CARGO BAY BAFFLE TO FRAME ATTACH ANGLE AT LBL 24 BS 400+1. / [01] REMOVED ANGLE IAW SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW ANGLE P/N 143AU155 IAW SRM 51-40-05-0G-0. REQ. OK TO INSTALL;[03] VERIFIED CORRECTIVE ACTION #2<BR>OK TO INSTALL GIVJun 23, 2022 · N951WN · Boeing 7377H4SDR SWAA2022081122221Tie Clip · crackedCRACK ON FWD CARGO BAY BAFFLE TO FRAME ATTACH ANGLE AT LBL 24 BS 500A+19. / [01] REMOVED ANGLE IAW SRM 51-40-02-0G-0;[02] RECEIVED NEW CLIP P/N:143A7502U159 ; LOT:1494686-4 AND LOCATED AND DRILLED AT FCB LBL 24 BS 500A+19' IAW SRM 51-40-05 . REQUEST OK TO INSTJun 23, 2022 · N951WN · Boeing 7377H4SDR SWAA2022080922225Gusset · crackedCRACK ON FWD CARGO BAY GUSSET AT BS 500D R/H STRINGER 19. / [01] REMOVED GUSSET AT FCB BS 500D R/H STR 19 IAW SRM 51-40-02.;[02] NO FOUND ALLOWABLE DAMAGE LIMITS ON SRM ; GUSSET MUST BE REPLACED IAW SRM 51-10-02 PARAGRAPH 9;[03] LOCATED AND DRILLED DRILLED NEWJun 23, 2022 · N951WN · Boeing 7377H4SDR SWAA2022080922224Gusset · crackedCRACK ON FWD CARGO BAY GUSSET AT BS 500D L/H STRINGER 19. / [01] REMOVED GUSSET AT FCB BS 500D L/H STR 19 IAW SRM 51-40-02;[02] NOT FOUND ALLOWABLE DAMAGE LIMITS ON SRM ; GUSSET MUST BE REPLACED IAW SRM 51-10-02 PARAGRAPH 9;[03] LOCATED AND DRILLED NEW GUSSET Jun 23, 2022 · N951WN · Boeing 7377H4SDR SWAA2022072735017Skin · corrodedFUSELAGE SKIN HAS PIT BS 195 3' BELOW S-24R. / [01] APPLIED PAINT STRIPPER ON AREAS TO ACCESS AT FUSELAGE SKIN STA 195 3' BELOW STR 24R AS PER REF B737-700 AMM 51-21-11-150-810;[02] REMOVED FASTENER 1 EACH TO ACCESS TO REMOVE DAMAGE ON AREAS AS PER REF B737-70Jun 23, 2022 · N478WN · Boeing 7377H4SDR IPXA2022070583821Stiffener · crackedINSPECTION TYPE:3CRH MLG W/W AFT O/B WEB 3RD STIFFENER CRACK AT LWR END.REMOVED AND REPALCED CRACKED STIFFENER IAW SRM 51-35-01 AND 51-31-01 (MINOR).Jun 22, 2022 · N290UP · Doug MD11FSDR DALA2022062704473Fastener · damagedSHIP 679 PROTUBERANCE AROUND REPAIR FASTENER, STA. 441 BTW. S-25R TO S-26R AT OUTER FUSELAGE. CORRECTIVE ACTION: SUMMARY OF NRC 00050. AREA WAS REPAIRED PER PRI 600108-14 REV 2 AND ER/A 600108-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. (2289142)Jun 22, 2022 · N679DA · Boeing 757232SDR IPXA2022070583850Skin · corrodedINSPECTION TYPE:C20APU COMPARTMENT HAS CORROSION ON INTERIOR SKIN L/H SIDE AT LOWER WEB ABOVE CLAMSHELL DOOR, AFT OF FWD HINGE (2 SPOTS) DOT 46-06WORKED PER RCD 271218, 757-200PF REV 114.00 CHAPTER 51-70-10-2R-4 PER SRM 53-80-01-2R, FIG 201Jun 21, 2022 · N413UP · Boeing 75724APFSDR IPXA2022070583831Skin · corrodedINSPECTION TYPE:CK20APU COMPARTMENT HAS CORROSION ON INTERIOR SKIN LH LOWER WEB AREA ABOVE CLAMSHELL DOOR, AFT OF AFT HINGE. DOT 46-06WORKED PER RCD 271220. 757-200PF REV 114.0 CHAPTER 51-70-10-2R-4 PER SRM 53-80-01-2R, FIG 201Jun 21, 2022 · N413UP · Boeing 75724APFSDR IPXA2022080100360Panel · corrodedFAULT - CORROSION - SUPPORT, RH AIR CONDITION COMPARTMENT ACCESS DOOR, MIDDLE SUPPORT. (REPLACE) TASK COMPLETEDJun 20, 2022 · N572UP · Boeing 74744AFSDR R61A2022070700426Skin · dentedRH FWD FUSELAGE DAMAGED BELOW RH LOWER SMART PROBE. REPAIRED DAMAGE IAW EMB ETD2022-170-021284. ALSO REF VP-025972-2022 N/R 1,9,10,11,22,23 FOR REPAIR.Jun 20, 2022 · N443YX · Emb ERJ170200LRSDR CALA2022062201547Skin · gougedAFT FUSELAGE SKIN, REPAIR DOUBLER AND SKIN LAP, AT S14L JUST FORWARD OF STA 1720, ARE GOUGED. AIRCRAFT FLIGHT CYCLES BUT BEFORE 44,000 TOTAL AIRCRAFT FLIGHT CYCLES....REF ORIGINAL L/P# 980227 AND HANGAR N/R# 674756 PLANNING TO CONTACT ENGINEERING FOR EC/RA 533Jun 20, 2022 · N17126 · Boeing 757200SDR SWAA2022092220224Skin · defectiveANOMALY ON EXTERNAL FUSELAGE SKIN BS970 - BS887 S-4R TO S-6R. MARKED. BS887 - BS960 S-6R TO S-8R. MARKED. BS887 - BS947 S-8R TO S-11R. MARKED. BS887 - BS928 S-11R TO S-13R. MARKED. BS887 - BS908 S-13R TO S-14R. MARKED. / [01] PERFORMED CLAD PENETRATION TEST INJun 18, 2022 · N8656B · Boeing 7378H4SDR SWAA2022092220225Skin · defectiveANOMALY ON EXTERNAL FUSELAGE SKIN BS858 - BS887 S-4R - S-10R. MARKED. / [01] PERFORMED CLAD PENETRATION TEST IN SEVERAL LOCATIONS ON SKIN PANEL BS 858 TO 887 S-4R TO S-10R LISTED BELOW PER SRM51-10-07-0G-0 PARA. 5D-E<BR><BR>1) BS 867+5.5' 3.5' BELOW STR 9R<BR>Jun 18, 2022 · N8656B · Boeing 7378H4
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