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 FDEA2020082191965Skin · dentedDENT EXTERNAL SKIN FR24 PLUS 12INCH STR51R LOWER FUSELAGE PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN FR 24 PLUS 12 INCH STR 51R LOWER FUSELAGE TITLE: FUSELAGE, PLATES AND SKIN: SKIN BETWEEN FR 24-FR 25, S51R, DENT, PERMANENT REPAIR EA # 6-5330-T0355526 "MSDR SWAA2020081006552Skin · dentedDENT ON FUSELAGE SKIN BS1006+3.3' .7' BELOW STR 15R / REPAIRED PER EA 20-153-01276 REV IR AND ATS ER 20-02937 REV IRSDR SWAA2020081006551Skin · dentedFUSELAGE SKIN HAS DENT BS 1006+2' 2.5' BELOW 15R / DAMAGE REPAIRED/INSPECTED AND EVALUATED PER EA 20-153-01276 REV IR AND ATS ER 20-02937 REV IR. REFER TO NRC U188806 FOR TRACKINGSDR SWAA2020080599239Skin · corrodedCORROSION ON FUSELAGE LOWER SKIN BS 1088 RBL 5 TO LBL5 JUST FORWARD WL 210 OF APU DOOR. REMOVED CORROSION IN TWO AREA'S 4'X7' AND 0.50'X7 MAX BLEND OF .005' IN BOTH AREA'S ORIGINAL THICKNESS 0.080'. AS PER EA 20-153-01244 REV IR AND ATS ER. 20-02917 REV IR THSDR 120B2020070900048Skin Panel · gougedGOUGE FOUND ON FUSELAGE SKIN BEHIND SLIDE PANEL 196ER.SDR SWAA2021042798664Skin · dentedFUSELAGE SKIN HAS DENT AT STA 1080 BETWEEN STR 24R AND 25R OUT OF LIMIT NOT SMOOTH. [CARD G582333]. REMOVED FASTERNERS; REMOVED DAMAGER; PERFORMED HFEC;ROTATORY AND (INSURANCE CUT AROUND THE CUTOUT)NO CRACK FOUND ; ROUGHNESS TEST;INSTALLED REPAIR PAINT; INSTALSDR SWAA2021042798663Skin · dentedDENT ON FUSELAGE AT STA 1054 STR 17L FOUND OUT OF LIMITS LESS THAN 10' FROM CUTOUT. [CARD G363535] REMOVED RIVET; CUTED DAMAGE PERFORMED HFEC; ROTO; DVI; COUNTER SINK; INSURENCE CUT INSPECTION ON AREAS; FABRICATED DOUBLER REPAIR PARTS AS PER REF. B737700 SRM 5SDR SWAA2020081006387Skin · dentedDENT ON FUSELAGE SKIN BS360+14' ABOVE STR 17L REF C029807; V474383; V474384 AND V474416 / REPAIRED AS PER EA 20-153-01105 REV IR AND ATS ER 20-02866 REV IRSDR SWAA2020072199869Skin · dentedFOUND DENT AT FUSELAGE SKIN STA 905+10' AND STR 22R / EVALUATED DENT FOUND OUT OF LIMITS. CUT OUT DAMAGE. DIMENSION 4' X 2 3/4' AT FUSELAGE SKIN BETWEEN BS 911 AND BS 923 STR 22R. REMOVED FASTENERS ON DAMAGE AREA. PERFORMED HFEC, ROTARY INSP, PERFORMED SDR SWAA2020072001339Skin · cracked0.5 INCH CRACK INDICATION AT CHEM-MILL POCKET AT BS 608 ON STRINGER 4L. INDICATION DETECTED WITH PART 6; 53-30-25 AND VERIFIED WITH PART 6; 53-30-09 AND PART 4; 53-30-07 IAW SA-M 326 A1131762, A1131764, AND A1131768. REPAIRED THE CRACK IN SKIN AT BS 608 STSDR 120B2020070800039Skin · corrodedSMALL AREA OF CORROSION ON THE FUSELAGE EXTERNAL SKIN UNDER RT FWD UPPER WING FILLET PANEL (192CR).SDR SWIA202082051854Plate · corrodedAVIONICS BAY ANTENNA MOUNTING PLATE LOCATED BETWEEN FS 295.00 TO 310.00, ON STGR 27 HAS CORROSION ON VARIOUS AREAS. REMOVED AND REPLACED THE TCAS DOUBLER REFERENCING DWG, AND SRM. CSDR SWAA2020081006550Skin · dentedDENT ON FUSELAGE SKIN BS360+12' 3' BELOW STR 5L / REPAIRED PER EA 20-153-01291 REV IR AND ATS ER 20-02933 REV IRSDR SWAA2020072300270Skin · dentedDENT ON FUSELAGE SKIN LOCATED STA 907+8.0' AND 2.0' BELOW STR 20 RT . / REPAIRED DENT ON FUSLAGE SKIN LOCATED AT STA 907+8.0' AND 2.0' BELOW STR 20RT REF B737-700 SRM 53-00-01-2R-3 REPAIR 3. THIS IS A CATEGORY 'B' REPAIR TABLE 204 - REPAIR EXTENDED BEYOND STRISDR SWIA2020090952318Skin · crackedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA53539-670-53-21-1660, MXCODEID49248-PR. CRACK LOCATED AT FS389 STR19 LT ON CENTER ROW OF LAP OF OUTER SKIN AREA, REPAIRED IAW SRM. THE REPAIR COMPLETED 10/18/2006 DOESN'T FOLLOW SRM REQUIREMENTS. THE SUBJECT CONDITISDR U2RA202009090605Skin · damagedA DENT WITH A NICK WAS NOTED ON THE FUSELAGE SKIN LOCATED APPROXIMATELY BODY STATION 444.5 AT STRINGER S-44L. ACCOMPLISHED REPAIR IN ACCORDANCE WITH BOEING SERVICE REQUEST 4-4843050665 AND ITS ASSOCIATED MESSAGES.SDR SWAA2020081097974Skin · corrodedMULTIPLE AREAS OF CORROSION FOUND ON CROWN SKIN; BS 947-1006; STR-2L TO STR-2R (UNDER DORSAL FIN) / REPAIRED CORROSION DAMAGE ON CROWN SKIN; BS947-1006 STR 2L TO 2R (UNDER DORSAL FIN) PER ER 20-02856 REV IR AND EA 20-153-01127 REV IRSDR IPXA2020072087915Tripler · gougedINSPECTION TYPE:2C, EXTERIOR FUSELAGE REPAIR TRIPLER GOUGED AT FWD CARGO DOOR CUTOUT LOWER AFT CORNER.REPAIRED GOUGED EXTERIOR FUSELAGE SKIN EXISTING REPAIR AT FWD LOWER CARGO DOOR CUTOUT AFT JAMB AT STA. 1002 IAW VT-SAA EA 011-5330-01-A8413 REV. IR AND UPS ESDR HNAA2020072000200Skin · corrodedHEAVY CHECK - EXTERIOR SKIN CORRODED BTW FR 66-67 STR 21L-21R...ACCOMPLISHED REPAIR OF EXTERIOR SKIN CORROSION BTW FR 66-67 STGR 21L-21R IAW ETD# ETD2020-145-020488.SDR U2RA2020070840002Skin · dentedDURING ACCOMPLISHMENT OF INSPECTIONS REQUIRED BY TASK CARD 53-804-01-01, A DENT WAS NOTED ON LOWER FUSELAGE EXTERNAL SKIN, AFT CARGO CUTOUT AFT EDGE , BODY STATION 1920, BETWEEN STRINGERS S-36R S-37R. DENT WAS REPAIRED IN ACCORDANCE WITH FLIGHT VEHICLES CONSUSDR SWIA2020082151912Skin · corrodedCORROSION ON VARIOUS AREAS BETWEEN FS559.00+80 €“ FS559.00+112, STGR 26L €“ STGR 26R (C-CHECK) RO 8/18/2020 REPAIRED FUSELAGE SKIN BETWEEN FS559+80 AND FS559+112 AND BETWEEN STR26L AND STR26R PER REO AND CRJ200SRM. COMPLETED SKYWEST TASK CARD.SDR SWAA2020072302034Skin · dentedAFT UPPER CORNER OF CARGO DOOR CUTOUT SKIN DENTED.SDR P5CA2020070700249Skin · gougedGOUGE DAMAGE ON FUSELAGE SKIN OUTER SURFACE AT STA 481, BETWEEN S-45L AND S-46L. REPAIRED THE DAMAGED AREA IAW EI NR T2020A53M-1666 REV 2. JOB COMPLETED AND CONDITION CHECK NORMAL.SDR U2RA2020090170001Skin · crackedDURING ACCOMPLISHMENT OF SB 747-53A2305, SKIN CRACKING WAS DISCOVERED NEAR THE LEFT AND RIGHT HAND AFT CORNERS OF THE NOSE WHEEL WELL. ACCOMPLISHED REPAIRS AS OUTLINED IN SERVICE REQUEST 4-4818744620 AND ITS ASSOCIATED MESSAGES.SDR SWAA2020072101188Skin · dentedDENT FOUND ON EXTERIOR FUSELAGE SKIN AT STA 360+16.5; 4' ABOVE STR 23L. EXTERIOR FUSELAGE SKIN DENT AT BS 360+16.5; 4' ABOVE STR 23L MEASURED 5.5' X 3.9' X .010 W/Y=390. FOUND TO BE OUT OF LIMITS DUE TO DAMAGE WITHIN DENT PER SRM 53-00-01-1A-1. REMOVED DAMAGSDR ABXA20200721141Skin · corrodedSTA 1080 STR 30L. BLEND OUT FUSELAGE SKIN INTERNAL. AIRCRAFT WAS GROUNDED.SDR DALA2020070402541Skin · dentedERA 581352-14 REVISED TO REV 'A'. SECTION I ISSUED FOR DENT DMG TO FWD FUSELAGE LOWER SKIN, FR17 S-23L TO S-24L. DAMAGE TOLERANCE STAGE II RECEIVED.SDR MK1Y20200702006Skin · dentedDURING MAINTENENCE INSPECTION A DENT WAS FOUND AT STA 1562 TO STA 1582, STR 17R TO STR 19R.SDR SWIA2020081151716Skin · nickedLOWER SKIN AT FWD AND AFT CARGO DOOR CUTOUT HAVE A FEW SMALL NICKS. COMPLIED WITH REPAIR OF LOWER SKIN AT FWD AND AFT CARGO DOOR CUT OUT IAW REO.SDR SWAA2020072101540Skin · dentedDENT FOUND ON EXTERIOR FUSELAGE SKIN BS 1040+6.6, 2 INCHES ABOVE STRINGER 15L. MEASURES 3.6'L X 3.3'W X .088'D W/Y=37. AND OUT OF LIMITS DUE TO DAMAGE WITHIN DENT IAW SRM 53-00-01-1A-1, TABLE 102. REPAIRED THE FUSELAGE SKIN IAW EC 20-153-01137 & ER 20-02873SDR MK1Y20200701002Skin · corrodedFOUND EXISTING CORROSION ON CENTER WING UPPER SKIN, STA 950, RBL 90.SDR FDEA202006301434Skin · crackedSUSPECTED CRACK L/H NUMBER 2 PACK UPPER AFT CORNER CRACK WAS REPAIRED IN REF TO SRM 53-50-00 FIG 3A AND EA .8-5350-T0354952SDR SWAA2020072000515Skin · dentedDENT DAMAGE AT STA 380; 4' ABOVE S-17L IS OUT OF LIMITS PER SRM 53-00-01-1A-1 AND REQUIRES REPAIR. REFERENCE N/R T791830; AND T791961. / FACT AS A RESULT OF POST REPAIR INSPECTIONSDR SWAA2020072000531Skin · dentedDENT DAMAGE AT STA 907 +17'; AT STR-19L IS OUT OF LIMITS PER SRM 53-00-01-1A-1 DUE TO A CREASE AT THE STRINGER. REFERENCE LOG BOOK PAGE 0735870. / FACT AS A RESULT OF POST REPAIR INSPECTIONSDR IXXA20200720025Skin · crackedAIRCRAFT GROUNDED FOR HEAVY MAINTENANCE SCHEDULED VISIT. IN COMPLIANCE OF TASK CARD 53-872-00-01, EXTERNAL FUSELAGE SKIN CRACKED AT THE LOWER AFT CORNER OF THE R1 DOOR CUTOUT. CRACK IN R1 DOOR LOWER AFT CORNER FOUND TO BE OUT LIMITS. REPAIRS ACCOMPLISHED IN ACSDR FDEA2020070601443Skin · dentedFUSELAGE EXTERNAL SKIN RT SIDE FWD OF FRAME 26, BETWEEN STRINGERS 38R-39R SKIN DENTED AND SCRATCHED. ACCOMPLISHED REPAIR DOUBLER ON FUSELAGE EXTERNAL SKIN RT SIDE FWD OF FRAME 26, BETWEEN STRINGERS 38R-39R IAW SRM 53-10-12, FIG 225 SHEET 1.SDR FDEA2020070201434Skin · crackedSUSPECTED CRACK LT NUMBER2 PAC EXHAUST, UPPER AFT CORNER CRACK WAS REPAIRED IN REF TO SRM 53-50-00 FIG 3A AND EA 8-5350-T0354952.SDR UIEA2020070201477Skin · deformedDEFORMATION ON FUSELAGE SKIN NEAR STA 620, S-25L TO S-26L. REPAIRED THE DEFORMATION FUSELAGE SKIN IAW EI NO T2020A53M-1669 REV 2. JOB COMPLETED AND CONDITION CHECK NORMAL.SDR SWIA2020082551978Skin · dentedTHE RH FUSELAGE SKIN HAS 3 DENTS BETWEEN FS 409 AND FS 421 AND BETWEEN STR 16R AND STR 17R. REPAIRED RH FUSELAGE SKIN 3 EA. DENTS BETWEEN FS 409 AND FS 421 AND BETWEEN STR 16R AND STR 17R AS PER REO.SDR SWIA2020082551977Skin · dented* THE RH FUSELAGE SKIN HAS 1 DENT BETWEEN FS 394 AND FS 409 AND BETWEEN STR 16R AND STR 17R. (MARKED WITH BLACK GREASE PENCIL) (C-CHECK 8/23/2020)REPAIRED DENT ON RH FUSELAGE SKIN BETWEEN FS 394 AND 409 AND BETWEEN STR 16R AND 17R AS PER MHIRJ REO.SDR SWIA2020082551976Skin · dentedTHE RH FUSELAGE SKIN HAS 1 DENT BETWEEN FS 409 AND FS 421 AND BETWEEN STR 15R AND STR 16R. REPAIRED RH FUSELAGE SKIN DENT BETWEEN FS 409 AND FS 421 AND BETWEEN STR 15R AND STR 16R AS PER REO.SDR SWIA2020082551975Skin · dentedTHE RH FUSELAGE SKIN HAS 1 DENT BETWEEN FS 394 AND FS 409 AND BETWEEN STR 15R AND STR 16R. REPAIRED DENT AREA REF COMPLIED WITH REOSDR SWIA2020082551974Skin · dentedTHE RH FUSELAGE SKIN HAS 1 DENT BETWEEN FS 349 AND FS 364 AND BETWEEN STR 15R AND STR 16R. COMPLIED WITH REO DISPOSITION FOR DENT DAMAGE TO FUSELAGE SKIN BETWEEN FS 349-364AND STR 15R-16R.SDR SWIA20208251973Skin · dented* THE LH SIDE FUSELAGE SKIN PANEL BETWEEN FS 169 AND FS 173, JUST FWD OF THE TRU ACCESS DOOR, HAS 2 DENTS NEXT TO ONE ANOTHER. REPAIRED DENT LOCATED AT LH SIDE FUSELAGE SKIN PANEL FS 169-FS 173 JUST FWD OF THE TRU ACCESS DOOR. REF REO.SDR SWAA2020072797551Skin · corrodedCORROSION ON CROWN SKIN EXTERNAL SURFACE IN MULTIPLE AREAS FROM APPROXIMATELY BS 887- BS 996 STR 3L - STR 3R / REPAIRED DAMAGE ON CROWN SKIN EXTERNAL SURFACE IN MULTIPLE AREAS FROM APPROXIMATELY BS887-996; STR3L- STR3R PER ER# 20-02823 REV IR AND EA # 20-153-0SDR MASA20200630047Doubler · corroded(C-CHECK) LOWER ANTENNA FS301 STR 27R CORRODED. R&R TCAS LOWER ANTENNA DOUBLER AT FS301 STR 27.SDR SWIA2020082551972Skin · dentedOVAL SHAPED DENT THAT IS 2 IN LONG BY 1 INCH WIDE LOCATED AT APPROX. FS 1162, STRINGER 23L. MAP EVALUATE AND REPAIR AS REQUIRED. IF FOUND WITHIN LIMITS, ELIMINATE DENT USING AIRCRAFT STANDARD PRACTICES/PROCEDURES. REPAIRED OVAL SHAPED DENT AT APPROX FS1162 SSDR DALA2020070202528Bear Strap · crackedAPPROX 1.5" CRACK DETECTED IN BEARSTRAP WHILE C/W FORECAST L1 DOOR CUTOUT INSP. C/W REPAIR W/C PER W/C.SDR UIEA2020063051290Skin · corrodedAFT FUSELAGE RT WASTE SYSTEM OVERBOARD VENT SKIN FOUND CORRODED, BS 2090, STRINGERS 35R-36R, SURFACE CORROSION REMOVED AND PROTECTED IAW SRM 51-10-02, AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-01-1A-1 ALLOWABLE DAMAGE 1, FIG 101 LIMITS.SDR FDEA2020071071371Skin · chafedFORWARD CARGO COMPARTMENT DOOR CUTOUT STATION 1009 LONGERON 40 RIGHT HAND TO LONGERON 41 RIGHT HAND FOUND CHAFFING. FORWARD CARGO COMPARTMENT DOOR CUTOUT REPAIR CARRIED OUT AT STATION 1009 LONGERON 40 RIGHT HAND TO 41 RIGHT HAND AS PER MD-11 SRM 53-00-15-2
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