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 DALA2019021100904Skin · dentedDURING INSPECTION FOUND LARGE DENT MEASURING 13.5" BY 11" BY A DEPTH OF 0.375 WITH A 0.75" LONG MINOR GOUGE AS SEEN IN FIGURE 12. THE SUBJECT DENT IS LOCATED BETWEEN STA 492-500B AND STR 21R-23R. UNDERLYING STR 22R IS BENT. REPAIRED PER PRI 575226-14 REV 4. REFeb 10, 2019 · N384DA · Boeing 737832SDR ASOA2019021593015Skin · crackedDURING SCHEDULED MAINTNENACE CHECKS FOUND SKIN DAMAGE AT THE #2 RADIO ALTIMETER BASE BETWEEN FRAMES 68-69 AND STRINGERS 21L-21R. THE DAMAGE IS IN THE FORM OF CRACKING AROUND THE FASTNER HOLES USED TO SECURE THE #2 RADIO ALTIMETER. MAINTENANCE REPAIRED I/A/W SRFeb 9, 2019 · N14188 · Emb EMB145XRSDR JJBA2019021209004Skin · damagedPER ETD 2018-145-121259 A PERMANENT REPAIR REQUIRED OF THE REAR FUSELAGE II - LOWER SKIN AREA UNDER DATA PLATE WITHIN 500 FC. REMOVED DAMAGED AREA. PERFORMED FLUORESCENT PENTRANT INSPECTION OF CUT-OUT. NO CRACKS DETECTED. FABRICATED REPAIR DOUBLER AND FILLER. Feb 9, 2019 · N12175 · Emb EMB145XRSDR DALA201902110870Access Panel · corrodedINITIAL INSPECTION: CORROSION ON AFT LAVATORY ACCESS PANEL BTW STA Y 1309 -1322 AND BTW LOG 20LH -21LH FUS. CORROSION LEVEL 2. AFT LAVATORY ACCESS PANEL,SKIN AND INTERNAL DOUBLER WERE REPAIRED PER ER/A 473500-14 REV. A SECTION II AND ETI-88-19-009 REV.3. PERFOFeb 9, 2019 · N973DL · Doug MD88SDR DALA2019021109868Skin · crackedFIVE CRACKS WERE FOUND ON LOWER AFT CORNER EXTERNAL SKIN AT FORWARD CARGO DOOR JAMB STA Y= 422. ON LOWER AFT CORNER EXTERNAL SKIN AT FORWARD CARGO DOOR JAMB STA Y= 422 WAS REPAIRED PER ER/A 575330-14AD REV.ORIGINAL (SECTION I PERMANENT REPAIR) AND ETI-88-19-01Feb 8, 2019 · N905DL · Doug MD88SDR ABXR2019020500286Skin · corrodedSKIN CORRODED.Feb 8, 2019 · N743AX · Boeing 767232SDR SWAA2022030326198Panel · corrodedNOSE WHEEL WELL PANEL 114AC HAS CORROSION / RECEAVED PANEL 7320265/NEW FOR TRACKING ONLY TO BE INSTALLED ON NRC T892801Feb 7, 2019 · N279WN · Boeing 7377H4SDR SWAA2022030326199Panel · corrodedNOSE WHEEL WELL PANEL 113AC HAS CORROSION / RECEAVED NEW PANEL 7320265 FOR TRACKING ONLY TO BE INSTALL ON NRC T892801Feb 7, 2019 · N279WN · Boeing 7377H4SDR SWAA2022030326200Panel · corrodedNOSE WHEEL WELL PANEL 114BW HAS CORROSION / RECEAVED NEW PANEL 7320579/NEW FOR TRACKING ONLY TO BE INSTALLED ON NRC T892801Feb 7, 2019 · N279WN · Boeing 7377H4SDR SWAA2022030326201Panel · corrodedNOSE WHEEL WELL PANEL 113BW HAS CORROSION / RECEAVED NEW PANEL 7320579/NEW FOR TRACKING ONLY TO BE INSTALLED ON NRC T892801Feb 7, 2019 · N279WN · Boeing 7377H4SDR IPXA2019022759426Skin · corrodedINSPECTION TYPE:3CEXTERIOR FUSELAGE SKIN HAS CORROSION BETWEEN STA. 2140-2163 AND LONG. 33L-35L.REPAIRED CPORRODED FUSELAGE SKIN BETWEEN STA. 2140-2163 AND BETWEEN LONG. 33L-35L IAW SRM 53-70-01 REPAIR 3 FIG. 201. (MAJOR)Feb 7, 2019 · N255UP · Doug MD11FSDR DALA2019020900897Skin · dentedDURING CURRENT H CHECK AT AEM, 2 DENTS WERE FOUND ON THE FUSELAGE SKIN P/N 143A3212-8 (MATERIAL 2024-T3 CLAD SHEET) BETWEEN BSTA 360 AND BSTA 380 & S-17L TO S-18L. MAINTENANCE REPAIRED DAMAGE PER ERA 574683-14.Feb 7, 2019 · N3745B · Boeing 737832SDR CALA2019020800224Skin · crackedR/H FR 16 DOUBLE JOGGLE AT DOOR STOP FITTING 7, FASTENER HOLE 8 HAS CRACK INDICATION REF. NTM FIGURE 53-11-53-991-001-A REPAIRED FASTENER HOLE 8 IN UPPER DOUBLE JOGGLE AREA AT FR 16 R/ H IAW ECRA 5311-02075. ACCOMPLISH THE INITIAL INSPECTION REQUIRE MENTS AT TFeb 7, 2019 · N829UA · Airbus A319131SDR AALA201902089009Doubler · corrodedCORROSION ON THE AFT ATG 4 ANTENNA MOUNTING AREA EXTERNAL SKIN DOUBLER BETWEEN FRAMES 56 AND 57, STRINGERS 41L AND 43L. REPAIRED THE SKIN DOUBLER IAW EA 289074.Feb 7, 2019 · N190UW · Airbus A321211SDR JGVR20190207001Skin · corrodedFOUND CORROSION AROUND THE RH FORWARD NOSE DOOR (AVIONICS ACCESS DOOR) ON THE FUSELAGE SKIN, REPAIRED BY BLENDING, NDT AND INSTALLING REPAIR DOUBLERS.Feb 7, 2019 · N609QS · Cessna 560XLSDR NACA2019021960030Skin · crackedSUBSURFACE CRACK AT BS400, EXISTING REPAIR ABOVE STR19R. REMOVED EXISTING REPAIR & REPLACED WITH NEW REPAIR DOUBLER IAW SRM 53-00-01 FIG. 201.Feb 6, 2019 · N361NC · Boeing 737301SDR NACA2019021960029Skin · crackedSUBSURFACE CRACK AT BS 500+3-BS500+8.5 BELOW STR17R. REPAIRED FUSELAGE CRACK IAW SRM 53-00-01 REPAIR 31 FIG. 201.Feb 6, 2019 · N361NC · Boeing 737301SDR NACA201902192028Skin · crackedSUBSURFACE CRACK AT BS420+3 AT STR26L. REPAIRED FUSELAGE CRACK IAW 53-00-01 REPAIR 31 FIG. 201Feb 6, 2019 · N361NC · Boeing 737301SDR DALA2019020700861Skin Panel · crackedDURING INSPECTION FOUND 1/2 CRACK ON GROUND SVC PANEL FUSELAGE SKIN. INSTALLED CATEGORY "A" PERMANENT REPAIR PER SRM 53-10-15 REPAIR 4.Feb 6, 2019 · N302DQ · Boeing 737732SDR SWAA2022030206616Scuff Plate · crackedFWD CARGO FWD CORNER THRESHOLD IS CRACKED / REMOVED AND REPLACED PER AMM.53-11-02Feb 5, 2019 · N220WN · Boeing 7377H4SDR SWAA2022030264099Scuff Plate · crackedFWD CARGO BAY FWD CORNER THRESHOLD IS CRACKED. / REPAIRED FWD CARGO BAY. FWD CORNER THRESHOLD IAW EA# 1-A53-2076 REV.11Feb 5, 2019 · N558WN · Boeing 73773VSDR SWAA2022030270970Scuff Plate · crackedFWD CARGO FWD CORNER SCUFF PLATE IS CRACKED / REPAIRED PER RO # RA15S6. INSTALLED ON TASK CARD 753-140-00-01Y.Feb 5, 2019 · N955WN · Boeing 7377H4SDR IPXA2019021879095Pad · gougedINSPECTION TYPE:4CJACK PAD IS GOUGED IN 3EA LOCATIONS.REMOVED DOUBLER AT JACK PAD AND REMOVED DOUBLER FORWARD OF JACK PAD, EXTERNAL CUTOUT AND INCORPORATED THE TWO REPAIRS,FABRICATED FILLERS, DOUBLER AND INSTALLED IAW A300-600 SRM 53-10-12, PAR.13, FIG.210.Feb 5, 2019 · N136UP · Airbus A300F4622RSDR ASOA201902055033Skin · dentedFWD RIGHT SIDE FUSELAGE SKIN HAS A DENT AT APPROXIMATELY FS234 BETWEEN STRINGERS 14R AND 15R. REPAIRED DAMAGE IAW EA 45-2019-003.Feb 5, 2019 · N876AS · Cndair CL6002B19SDR DALA2019020600807Doubler · corrodedINITIAL INSPECTION: CORROSION ON REPAIR DOUBLER SPLICE BTW L30 TO LL29R AND STA 593 TO 579 AT MID CARGO COMPARTMENT. DOUBLER SPLICE BTW L30 TO LL29R AND STA 593 TO 579 AT MID CARGO COMPARTMENT WAS REPLACED PER DC9 / MD80 SRM 53-14-2 FIG.3. (LP0933052)Feb 5, 2019 · N905DL · Doug MD88SDR ABXR2019020500262Skin · corrodedFUSELAGE SKIN CORRODED.Feb 5, 2019 · N743AX · Boeing 767232SDR ABXR2019020500260Skin · corrodedFUSE SKIN CORRODED.Feb 5, 2019 · N743AX · Boeing 767232SDR FXGA201902041918Skin · corrodedCORROSION AT RT WING ILLUMINATION LIGHT. TO REPAIR A CORRODED SKIN BETWEEN F/STA 720B AND 720C AND LONGERON S-14R AND S-16R. REPAIR CORRODED SKIN PER SRM 53-30-3 FIGURE 22. SEE PAGE 2 FOR RE-INSPECTION REQUIREMENTS.Feb 4, 2019 · N794AJ · Boeing 727227SDR SWAA2019032030861Skin · corrodedEXTERNAL SKIN CORRODED AT BS 886, BETWEEN STR 25R TO STR 24R. REPAIRED SKIN IAW ER AND EA.Feb 4, 2019 · N566WN · Boeing 7377CTSDR JJBA2019021304005Skin · dentedFUSELAGE DENTED BETWEEN FR 73 AND FR 74, STR 18R - 21R MARKED WITH GREEN DOT. COMPLIED WITH ETD 2019-145-012414 FOR PERMANENT ACCEPTANCE/REPAIR OF DENT/DAMAGE ON FUSELAGE SKIN BETWEEN FR 73 AND 74 AND STR 18R AND 21R. THIS REPAIR DOES NOT ADVERSELY AFFECT A FAFeb 4, 2019 · N33182 · Emb EMB145XRSDR FDEA2019020740263Skin · damagedBETWEEN STRINGER 38R AND 39R AT STATION 603 PREVIOUS DAMAGE WAS BLENDED OUT. REMOVED PAINT FROM SUSPECT AREA . THIS AREA REQUIRES NDT TO MEASURE FOR MATERIAL REMAINING THICKNESS PER. E.A. H-5330-T0345021. C/W SKIN THICKNESS CHECK OF BLENDED AREA IAW B76Feb 4, 2019 · N113FE · Boeing 7673S2FSDR DALA2019020500804Skin · gougedGOUGES AND NICKS ON FUSELAGE SKIN FROM STA Y1109 TO Y1129 BTW LONGERONS 12L-14L (FUS). FUSELAGE SKIN FROM STA Y1109 TO Y1129 BTW LONGERONS 12L-14L WAS REPAIRED PER ER/A 575178-14 REV ORIG AND ETI-17-19-017 REV 3.Feb 4, 2019 · N949AT · Boeing 717200SDR ABXR2019020400192Skin · corrodedFUSELAGE SKIN CORRODEDFeb 4, 2019 · N743AX · Boeing 767232SDR ABXR2019020400188Skin · corrodedSKIN CORRODEDFeb 4, 2019 · N743AX · Boeing 767232SDR ABXR2019020400182Skin · corrodedSKIN CORRODED.Feb 4, 2019 · N743AX · Boeing 767232SDR ABXR2019020400164Skin · corrodedSKIN CORRODED.Feb 4, 2019 · N743AX · Boeing 767232SDR SWAA2022030270907Scuff Plate · crackedAFT CARGO DOOR CUTOUT; LOWER FORWARD CORNER SCUFF PLATE IS CRACKED AND DAMAGED. / R/R AFT CARGO DOOR CUTOUT; LOWER FORWARD CORNER SCUFF PLATE PER E.A 1-A53-2076Feb 3, 2019 · N955WN · Boeing 7377H4SDR SWAA2022030270908Scuff Plate · crackedAFT CARGO DOOR CUTOUT; LOWER AFT CORNER SCUFF PLATE IS CRACKED AND DAMAGED. / R/R AFT CARGO DOOR CUTOUT; LOWER AFT CORNER SCUFF PLATE PER E.A 1-A53-2076Feb 3, 2019 · N955WN · Boeing 7377H4SDR SWIA20190405697Skin · chafedTHE FUSELAGE SKIN IS CHAFED BELOW THE AFT LAVATORY WATER SERVICING PORT AT APPROX. FS 559.00+96 ON THE RH SIDE. (C-CHECK) RO: 03/29/2019 BLENDED CHAFE BELOW THE AFT LAV WATER SERVICE PORT AT APPROX FS 559.00+94 BETWEEN STGR 21R TO STGR 22R IAW SRM AND REO.Feb 3, 2019 · N506CA · Cndair CL6002B19SDR ASOA201902035030Skin · dentedFORWARD RT SIDE FUSELAGE SKIN HAS A DENT AT APPROX FS260 BETWEEN STRINGERS 16R AND 17R. REPAIRED DAMAGE IAW EA 45-2019-002 DATED 2019-01-22.Feb 3, 2019 · N876AS · Cndair CL6002B19SDR UIEA2019020503105Skin · dentedSHARP DENT ON FUSELAGE SKIN PANEL NEAR STA 540. BETWEEN S-33R AND S-34R.(<P>1.REPAIR DENT AREA I.A.W. EI NO.T2019A53M-150 REV.1.</P>)Feb 3, 2019 · N412MC · Boeing 74747UFSDR UIEA2019020503119Doubler · corrodedCORROSION-DOUBLER,LOWER FUSELAGE,STA 979 FORM ACCESS PNL NO.192 FFR.(<P>1.RMV CORROSION DOUBLER I.A.W. SRM 51-40-02-0G-0 REV.84 2.INSTL NEW DOUBLER I.A.W. BOEING DWG NO.140110999 SH.30 REV.- & 14244780 SH.12 REV.F & 417112400 SH2 REV.-& 65B04118 SH.2 REV.P &14Feb 3, 2019 · N412MC · Boeing 74747UFSDR ABXR2019020300113Skin · corrodedSKIN CORRODED.Feb 3, 2019 · N743AX · Boeing 767232SDR ABXR2019020300106Skin · corrodedSKIN CORRODED.Feb 3, 2019 · N743AX · Boeing 767232SDR SWAA2022030245242Scuff Plate · crackedAFT CARGO THRESHOLD SCUFF PLATE IS CRACKED. / REMOVED CRACKED THRESHOLD SCUFF PLATE AFT CARGO AND REPLACED WITH NEW PART P/N 146A8342-7 IAW IPC 53-13-00-05A; AMM 53-11-02-020-801 AND AMM 53-11-02-420-801 ATAG# WN2730Feb 2, 2019 · N8609A · Boeing 7378H4SDR SWAA2022030166281Skin · corroded***CORROSION*** FUSELAGE CROWN EXTERNAL SKIN; BS 978 TO BS 1002; IN STR 1 FASTENER HOLES / FUSELAGE CROWN SKIN AT BS 978 TO BS 1002; STR 1 WAS REPAIRED IAW ATS ER 19-01789 REV IR DATED 20FEB19 AND EA 1-753-34224 REV IRFeb 2, 2019 · N565WN · Boeing 73776QSDR SWIA20190405696Skin · dentedTWO DENTS FWD OF WINDOW #3 ON THE LEFT SIDE OF THE FUSELAGE APPROX. JUST ABOVE THE FLOOR LINE. (C-CHECK) RO: 03/29/2019 REPAIRED DENTS IAW REO.Feb 2, 2019 · N506CA · Cndair CL6002B19SDR A6WA2019020546357Skin · damagedFOUND CHAFING DAMAGE TO OUTER SKIN OF PREVIOUS REPAIR PER GREO 601R-53-61-1285EFeb 2, 2019 · N463AW · Cndair CL6002B19SDR DALA2019020430710Doubler · corrodedDURING INSPECTION OF A REPAIRED AREA AT FUSELAGE SKIN STA 851; L29L-29R, SOME CORROSION WAS FOUND. NRC 00225: REPAIR DOUBLER WAS REPLACED PER ER/A 540245-14 REV. ORIGINAL. ASSOCIATED ER/A 14-540245 ADDED FOR AC 9509. (LP #0929471)Feb 2, 2019 · N950AT · Boeing 717200SDR DALA2019020200708Access Panel · corrodedCORROSION ON LAVATORY SERVICE ACCESS INNER PANE AT FUSELAGE. (FUS). NRC 00059: LAVATORY SERVICE ACCESS INNER PANE AT FUSELAGE WAS REPLACED PER B717-200 SRM 51-41-02 AND 51-41-05. (LP #0928367)Feb 2, 2019 · N950AT · Boeing 717200
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