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 CALA2019092301625Skin · gougedFUSELAGE EXT SKIN GOUGES AND DENT AT FR 21 STR 17L 18L PER NR LP 9292413. REPAIRED DAMAGED SKIN AT LT FR21 STR 17, 18L IAW ECRA 5311-02248 NO FURTHER ACTION REQUIRED.SDR COEA2019112927804Skin · dentedWO 197234 NR 77 HEAVY CHECK HATS/MAJOR REPAIR: DENT ON R/H FUSELAGE FORWARD OF FRAME 16. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0103933_01...15060 ISSUE C, DATED 10/31/2019.SDR DALA2019092205582Doubler · wornSHIP 6811 INITIAL INSPECTION: WORN ON PREVIOUS REPAIR DOUBLER STA:1280 BTW STGR:12R - 10R AT PAX CABIN. CORRECTIVE ACTION: SUMMARY OF NRC 00598 PREVIOUS REPAIR DOUBLER STA:1280 BTW STGR:12R - 10R AT PAX CABIN.(CPAX) WAS REPLACED PER B757-200 SRM AND SUPPLEMENTSDR DALA2019092105486Skin · dented(AIRCRAFT 6714, L/P 1280728) DENT ON EXTERNAL FUSELAGE SKIN STA 1473 APPROX BTW S-27R (FUS). DENT ON EXTERNAL FUSELAGE SKIN STA 1473 APPROX BTW S-27R WAS REPAIRED PER ER/A 581527-14 REV ORIGINAL AND ETI-57-19-101 REV 2. MAINTENANCE REQUERIMENTS WERE VERIFIED ASDR DALA2019092105484Skin · dented(AIRCRAFT 6714, L/P 1280610) FROM MON 36, LOG 2167125: TWO ADJACENT DENTS CLOSE TO MON DENT LOG # 2167125 AND .800" CLOSE TO PREVIOUS DOUBLER REPAIR STA 619 TO 626 BTW ST 16L AND ST18L. FUS. SUMMARY OF NRC S/N 00515 LT FUSELAGE SKIN FROM STA 590 TO STA 660 BTWSDR CALA2019092301619Skin · dentedFWD OF THE F/H LATERAL AVIONICS COMPARTMENT DOOR (13") FUSELAGE SKIN IS CREASED FR11-12 STR 35-36R ON REF 9292408. CUT OUT DAMAGED AREA AND INSTALLED REINFORCING REPAIR DOUBLER AT FR 11-12, STR 35R-36R IAW SRM 53-11-11-300-041. PERFORMED HFEC AT CUTOUT IAW NTMSDR SWAA2022032160256Skin · corrodedEVIDENCE OF CORROSION UNDER LOWER ATC ANTENNA ON FUSELAGE SKIN. STATION 354 BL 0. / REMOVED CORROSION, BLENDED SKIN AND REAPPLIED PROTECTIVE FINISH IAW EA 1-753-35640.SDR JJBA20190919005Skin · dentedFUSELAGE CF1 14" AFT OF MAIN CABIN DOOR HAS DENT/GOUGE IN AREA OF PREVIOUS DENT. PERMANENT REPAIR IS DUE WITHIN 50 CYCLES.SDR KCSA201909191226Skin · corrodedEVIDENCE OF CORROSION FUSELAGE EXTERNAL STRINGER 34 L STA 657 - 670.SDR KCSA201909191225Skin · corrodedEVIDENCE OF CORROSION FUSELAGE EXTERNAL STRINGER 33 L STA 658 - 676.SDR JGVR20190919002Skin · corrodedREPAIRED CORRODED AREAS OF THE LT AND RT FORWARD FUSELAGE SKINS, LOCATED UNDER AND ADJACENT TO THE FORWARD CHIN FAIRINGS, BY R&R THE FORWARD CHIN FAIRINGS FOR ACCESS, BLENDING, PERFORMING NDT, FABRICATING AND INSTALLING DOUBLERS AND FILLERS AS REQUIRED IN ACCOSDR SWAA2022032139358Skin · corroded***CORROSION*** CORROSION ON FUSELAGE CROWN SKIN AND ALONG FASTENER ROWS BETWEEN BS907 AND BS1017; LBL12.5 TO RBL12.5 / REMOVED CORROSION OF FUSELAGE CROWN SKIN BETWEEN BS 907 AND BS 1017; LBL 12.5 TO RBL 12.5 PER EA 1-753-35686 REV. IR AND ER 19-04884 REV.IR.SDR FDEA201909182754Skin · corrodedUPPER CARGO COMPT UNDER FLOOR NEAR STA 1270 AT RBL 105 STRUCTURE EXFOLIATED REPAIRED CORROSION FOUND AT UPPER CARGO COMP UNDER FLOOR AREA NEAR STATION 1270 RBL105 REF E.A 1-5730-T0350234 P1. TITLED "WING-PLATES AND SKINS-CENTER WING- UPPER SKIN-REWORK" ALSDR DALA2019091805417Skin · corrodedCORROSION LEVEL: 2. CORROSION EXTERNAL SKIN LOC. FR 65+10 STR 31R STR 32R AT LOWER FUSELAGE (1 EA) SSI 534108 AND WORK CARD 5100-3201. PERFORMED PERMANENT REPAIR LOC BTW FR 65 TO FR 66 AND STR 31R TO STR 33R AS PER SRM 53-00-11-300-033, ER/A 581054-14AD REVISISDR ABXA20190918148Splice Plate · corrodedCORROSION ON THE UPPER SURFACE OF THE FUSELAGE SKIN CIRCUMFERENTIAL SPLICE PLATE AT FUSELAGE STATION 434, STRINGERS 39L AND 39R. THE SPLICE PLATE WAS REPLACED. THE AIRPLANE WAS GROUNDED.SDR ABXA20190918143Plug · corrodedCORROSION ON LEFT SIDE WINDOW PLUG AT FUSELAGE STATION 845. THE WINDOW PLUG WAS REPLACED. THE AIRPLANE WAS GROUNDED.SDR FDEA2019102472735Skin · dentedUPPER FUSELAGE RHS, APPROX STA 1761 LONGERON NO. 9, SKIN DENTED, MARKED. REMOVED DENT AND REPAIRED AREA REF SRM 53-00-01-2R FIG. 201 SHEETS 2 AND 3, AND SRM51-31-01.SDR FDEA2019091972263Skin · crackedFRAME 40 TO CENTER WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION, RIGHT HAND, LOWER FASTENER HOLE FOUND CRACK SIGNAL REPAIRED THE FRAME 40 TO CENTER WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION, RIGHT HAND, LOWER FASTENER HOLE CRACK PER EA 6SDR FDEA2019091972262Skin · crackedFRAME 40 TO CENTER WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION, RIGHT HAND, MIDDLE FASTENER HOLE FOUND CRACK SIGNAL REPAIRED THE FRAME 40 TO CENTER WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION, RIGHT HAND, MIDDLE FASTENER HOLE CRACK PER EASDR DALA2019091905420Skin · dented(AIRCRAFT 6811, L/P 1275433) DENTS ON EXTERNAL FUSELAGE SKIN BTW STA 616-620 STRINGER 15-16L (AFT OF PREVIOUS REPAIR DOUBLER) (FUS). REPAIRED PER ER/A 581358-14 REV ORIGINAL AND ETI-57-19-116 REV ORIGINAL. HFEC INSPECTION WAS ACCOMPLISHED ON DENTS ON EXTERNAL SDR HEER20190917266Skin · corrodedFORWARD SHELL ASSEMBLY WAS FOUND TO BE CORRODED (TWO PLACES AT EXISTING INSERTS). THE REPAIR DOCUMENTATION WILL BE SUBMITTED FOR FAA APPROVAL. THE FORWARD SHELL ASSEMBLY WILL THEN BE REPAIRED IN ACCORDANCE WITH THE FAA-APPROVED REPAIR DATA.SDR SIMA20190916001Skin · dentedSUPPLEMENTAL FUSELAGE DENTED BETWEEN FR1 AND FR3. C/A-REPLACED RT FF1 SKIN PANEL IAW SRM 51-40-02 AND 51-21-01.SDR SWIA2019101846545Skin · chafedFUSELAGE SKIN AROUND APU EXHAUST IS CHAFED AT TWO LOCATIONS BETWEEN F.S. 654.20 TO F.S. 672.20. CHAFES ARE APPROX 0.125 LONG, 0.125 WIDE AND 0.015 DEEP. (C-CHECK) RO: 10/16/2019 REMOVED DAMAGE @ FS 654 - FS 672.20 AROUND APU EXH IAW REO.SDR DALA2019091705377Skin · damagedLOWER FUSELAGE, LT SIDE SKIN CREASED ALONGAFT SIDE OF FR 17 BETWEEN STR 23L -24L. ALSO DENTED AREA FWD & AFT OF FR 17 BETWEEN STR 23L & 24L . COMPLIED WITH ERA 581352-14 REV 0. A /C O/K FOR SERVICE. (LP# 1274315, 6234745)SDR DALA2019091705376Skin · damagedLOWER FUSELAGE, LT SIDE, SKIN CREASED ALONG AFT SIDE OF FR 17 BETWEEN STR 23L - 24L. ALSO DENTED AREAS ARE FWD & AFT OF FR 17 BETWEEN STR 23L -24L. ACCOMPLISHED PRI 581352-14AD REV 2 AWAITING FINAL EA 430466 REV ORIG ACCOMPLISHED RII 708436 {QC1976}. COMPLIED SDR IPXA2019091646824Skin Panel · gougedINSPECTION TYPE:SPV REF# DI# 680932; LEFT FUSELAGE DENT AND GOUGE DAMAGE AT STA 557, BELOW S19 ***PERMANENT REPAIR***REPAIRED PER EO NR B757-5330-73707-P1.SDR DALA2019091605344Skin · dented(LOG 5995782) DURING INSPECTION FOUND FUSELAGE/AFT CARGO DOOR CUTOUT/FWS SIDE/SKIN DENT. FABRICATED REPAIR PARTS PER SRM 53-00-01 REPAIR 23. INSTALLED REPAIR PER SRM. INSTALLED CATEGORY B REPAIR PER SRM 53-00-01 REPAIR 23.SDR RAIA2019100891409Skin · gougedAFT FUSELAGE EXTERIOR SKIN IS GOUGED AT FR 67 & STR 7 L/H SIDE INSIDE PYLON ACCESS PANEL 414DB....REPAIRED AFT FUSELAGE EXTERIOR SKIN GOUGE AT FR 67 & STR 7 LH.SDR JJBA20190914004Skin Panel · not reportedPERMANENT REPAIR OF FORWARD RH FUSELAGE SKIN PANEL 120-22656-048 REQUIRED WITHIN 3000 FLIGHT CYCLES. MADE PERMANENT REPAIR OF FORWARD RH FUSELAGE SKIN PANEL 120-22656-048.SDR CALA2019091701551Skin · crackedB767-06-3-7140 EMP - RT STAB TO BODY CUTOUT FWD SKIN CRACKED. (REF NR LP 9130454). EMP RT STAB TO BODY CUTOUT FWD SKIN BETWEEN STA 1725 - STA 1740 AND STR 15R - STR 22R REPAIRED AS PER SRM 53-80-01 REPAIR 3 FIG 201.SDR R61A2019100311051Rivet · abnormalMAINTENANCE FOUND A PROTRUDING RIVET AT REAR FUSELAGE LOWER EXTERNAL SKIN BETWEEN FRAMES 96-97, STRINGERS 21R TO 23R. THE RIVET WAS REMOVED AND REPLACED IAW SRM 53-30-01, ALLOWABLE DAMAGE 03, PARA 6 (A).SDR R61A201910031049Skin · corrodedMAJOR - REAR FUSELAGE LOWER EXTERNAL SKIN FR97-98 STR29L-28R, DATA PLATE AREA CORROSION FOUND. ACCOMPLISHED PERMANENT REPAIR ON REAR FUSELAGE SKIN FR97-98 STGR29L-28R IAW ETD2019-170-130281. A/C REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.SDR FDEA201909132356Skin Panel · corrodedFUSELAGE SKIN HAS EVIDENCE OF CORROSION ON INNER SURFACE AT APU INLET DOOR PANEL FORWARD ATTACHMENT AREA CORROSION FOUND TO BE OUTSIDE LIMITS ,SKIN PANEL REPLACED IAW BOEING DWG # 148N3105 AND SRM 51-40-02.SDR C77A2019091300007Doubler · corrodedDURING BASIC CHECK, CORROSION DAMAGE WAS DISCOVERED DURING INSPECTION ON THE CENTER FUSELAGE III WASTE BOX SKIN DOUBLER, P/N 170-66931-001, ALONG THE INNER EDGES OF THE DOUBLER (REFERENCE PHOTO 1 FOR DETAILS). THE CORROSION DAMAGE WAS BLENDED WITH THE DEEPESTSDR C77A2019091300002Skin Panel · dentedBEFORE A FLIGHT OUT OF BIS, A DENT WAS DISCOVERED ON THE FWD FUSELAGE SKIN OF AIRCRAFT, P/N 170-03387-003, BETWEEN S-17L-18L AND CROSSING OVER FR11. ENGINEERING ORIGINALLY RECEIVED RELIEF IN THE FORM OF ETD2017-170-039578, WHICH PROVIDED A 250FC FLYBY PROVIDEDSDR C77A2020011100007Skin · corrodedDURING BASIC CHECK AT EAMS, CORROSION DAMAGE WAS FOUND TO THE CENTER FUSELAGE III SKIN FORWARD OF THE WASTE DOOR AT FRAME 88 (P/N 170-91883-005). REFERENCE ETD2019-170-120787, FIGURE 1 FOR DETAILS. EAMS REQUESTED AND RECEIVED PERMANENT REPAIRS FOR THE DAMAGE ISDR SWAA2019101637916Doubler · corrodedAFT CARGO COMPARTMENT SPOT CORRODED BETWEEN BS. 727E TO BS. 747, STR. 25R. / REPAIRED DOUBLER IAW SRM AND DWG.SDR SWAA2019101437781Skin · dentedFOUND DENT ON EXTERIOR FUSELAGE SKIN AT STA. 827+6, 3.5" ABOVE STR. 27R TO 2.5" BELOW STR. 27R. / REPAIRED SKIN IAW ER AND EA.SDR SWAA2019101437780Skin · dentedFOUND DENT ON EXTERIOR FUSELAGE SKIN AT STA. 792+6, 1.0" BELOW STR. 27R. REPAIRED SKIN PER ER AND EA.SDR SWAA2019101437779Skin · dentedFOUND DENT ON EXTERIOR FUSELAGE SKIN AT STA. 792+11.2 5.4" ABOVE STR. 27R. REPAIRED SKIN PER ER AND EA.SDR SWAA2019101437775Skin · dentedFOUND DENT ON EXTERIOR FUSELAGE SKIN AT STA. 1006+1.7 4.0" ABOVE STR. 23R. / REPAIRED SKIN IAW SWA EA AND ER.SDR SWAA2019101437773Skin · dentedFOUND DENT ON EXTERIOR FUSELAGE SKIN AT STA. 732+6, 3.0" ABOVE STR. 26R. REPAIRED SKIN PER ER AND EA.SDR SWAA2019101437772Skin · dentedFOUND DENT ON EXTERIOR FUSELAGE SKIN AT STA. 792+8, 3.0" ABOVE STR. 27R. REPAIRED FUSELAGE SKIN IAW ER AND EA.SDR RAIA201909110001Skin · crackedMOUNTING PLATE FOR RADIO ALTIMETER #2 FWD ANTENNA ON AFT FUSELAGE IS SEPARATING FROM THE AIRCRAFT. CORROSION FOUND BETWEEN MOUNTING PLATE AND SKIN OF FUSELAGE. NO CORROSION FOUND ON THE FUSELAGE ONLY MOUNTING PLATE. AFTER CLEANING CRACKS WERE FOUND ON THE FUSESDR KCSA201909111218Skin · corrodedFUSELAGE SKIN INNNER SURFACE HAS EVIDENCE OF CORROSION AT STA 654+11 S-33L.SDR KCSA201909111217Skin · corrodedFUSELAGE SKIN INNNER SURFACE HAS EVIDENCE OF CORROSION AT STA 654+11 S-34L.SDR IPXA2019100217446Skin · crackedINSPECTION TYPE:4CFWD. FUSELAGE SKIN IS CRACKED AT STA. Y=563, L48L BETWEEN X=24 AND X=44.REPAIRED EXTERIOR FUSELAGE SKIN AT STA. Y=563, L48L AND BETWEEN X=24 AND X=44 IAW VT-SAA EA 011-5330-01-A7902 REV. I/R AND UPS EO MD11-5330-74106-A. (MAJOR)SDR FDEA201909102196Skin · crackedMAIN DECK R3 DOOR AFT JAMB LOWER WEB BOX AT STATION 1305.25 TO STATION 1315.42 LONGERON 26 RIGHT TO LONGERON 27 RIGHT FOUND CRACKED. MAIN DECK RIGHT 3 DOOR AFT JAMB LOWER WEB BOX AT STATION 1305.25 TO STATION 1315.42 BETWEEN LONGERON 26 RIGHT TO LONGERON 27 RSDR AALA201909169064Buttstrap · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FUSELAGE SKIN BUTT JOINT SPLICE STRAP AT FR 64 BETWEEN S43R AND S44. REPAIRED STRAP PER EA 297338.SDR RAIA201909100001Skin · crackedFUSLAGE SKIN UNDER AFT DRAIN MAST CRACKED AND HAS HOLE. REPAIR INFORMATION ATTACHED TO SUPPLIMENTAL E-MAIL SENT TO 9-AMC-AFS-SDR@FAA.GOV.
Back to JASC 5330