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 IPXA2019060542873Skin · corrodedINSPECTION TYPE: SEG3 LOWER SKIN CORRODED OUT OF MANUFACTURERS LIMITS. LOWER SKIN REPLACED BY FABRICATING NEW SKIN PER EO M-2550-11648-0.SDR IPXA2019060542872Skin · corrodedINSPECTION TYPE:SEG3LOWER SKIN CORRODED OUT OF MANUFACTURERS LIMITS.LOWER SKIN REPLACED BY FABRICATING A NEW SKIN PER EO M-2550-11648-0SDR IPXA2019060542871Skin · corrodedINSPECTION TYPE: SEG3 LOWER SKIN CORRODED OUT OF MANUFACTURERS LIMITS. LOWER SKIN REPLACED BY FABRICATING NEW SKIN PER EO M-2550-11648-0SDR IPXA2019060542870Skin · corrodedINSPECTION TYPE: SEG3 LOWER SKIN CORRODEDD OUT OF MANUFACTURERS LIMITS. LOWER SKIN REPLACED BY FABRICATING NEW SKIN PER EO M-2550-11648-0SDR IPXA2019060542869Skin · corrodedINSPECTION TYPE:SEG3 LOWER SKIN CORRODED OUT OF MANUFACTURERS LIMITS. LOWER SKIN REPLACED BY FABRICATING NEW SKIN PER EO M-2550-11648-0SDR IPXA2019060542866Skin · corrodedINSPECTION TYPE:SEG3 LOWER SKIN CORRODED OUT OF MANFACTURES LIMITS LOWER SKIN REPLACED BY FABRICATING A NEW SKIN PER EO M-2550-11648-0SDR SWAA2022031078667Scuff Plate · crackedFWD CARGO BAY; FWD CORNER SCUFF PLATE IS CRACKED / FWD CARGO BAY; FWD CORNER SCUFF PLATE REPAIRED PER EA 1-A53-2076. REV 11SDR SWAA2022031078668Scuff Plate · crackedAFT CARGO BAY; FWD CORNER SCUFF PLATE IS CRACKED / AFT CARGO BAY; FWD CORNER SCUFF PLATE REPAIRED PER EA 1-A53-2076; REV 11.SDR SWAA2022031079036Skin · out of toleranceFOUND DIAMETER OF HOLE 7L AT STR-3L TO BE OUT OF LIMITS I.A.W. CUSTOMER CARD 12107-53. HOLE DIA: O.324 IN.. LIMITS: 0.312-0.3130 IN. / REAMED HOLE 7L AT STR 3L STA 1016 TO .328 IAW CUSTOMER CARD 12107-53 STEP 20A. HOLE 7L FOUND TO BE IN TOLERANCE IAW CUSTOMER SDR SWAA2022031079037Skin · out of toleranceFOUND DIAMETER OF HOLE 8L AT STR-3L TO BE OUT OF LIM ITS I.A.W. CUSTOMER CARD 12107-53. HOLE DIA: O.321 I N.. LIMITS: 0.312-0.3130 IN. / REAMED HOLE 8L AT STR 3L STA 1016 TO .328 IAW CUSTOMER CARD 12107-53 STEP 20C. HOLE 8L AT STR 3L STA 1016 FOUND TO BE IN TOSDR SWAA2022031079039Skin · out of toleranceFOUND DIAMETER OF HOLE 7R AT STR-3R TO BE OUT OF LIMITS I.A.W. CUSTOMER CARD 12107-53. HOLE DIA: O.326IN.. LIMITS: 0.312-0.3130 IN. / REAMED HOLE 7R AT STR 3R STA 1016 TO .328 IAW CUSTOMER CARD 12107-53 STEP 25A. HOLE 7R FOUND TO BE IN TOLERANCE IAW CUSTOMER CSDR SWIA2019080146111Skin · chafedFUSELAGE EXTERIOR SKIN HAS SEVERAL CHAFES/SCRATCHES AT APU EXHAUST OPENING AFT END. REPAIRED IAW REO.SDR ABXA201906074113Skin · damagedDAMAGE IN THE SKIN AT THE FORWARD LOWER CARGO DOOR FRAME AT FUSELAGE STATION 539, STRINGER 30R. THE DAMAGE IS MEASURED 3.5" BY 0.5". THE SKIN WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR IPXA201906052806Skin · dentedINSPECTION TYPE:SEG3 - LH FUSELAGE NOSE SECTION SKIN AT STA 239, W.L. 210 REMOVED FASTNERS COMON TO DENT, ROTO PROBED HOLES REPLACED FASTNERS, RESTORED FINISHES PER E0 B757-5330-72670-ASDR DALA2023062805199Unknown · unknownSHIP 685 FUSELAGE / SKIN, STRAP AND FRAME CHORD / BS 480, S-28L TO 28R / OVERSIZED HOLES. CORRECTIVE ACTION: REF ERA 531971-14. (1105050)SDR IPXA2019062143566Skin · gougedEXTERIOR FUSELAGE SKIN JUST AFT OF POWER RECEPTACLE GOUGED. MARKED IN REDFOUND GOUGE TO BE OUT OF LIMITS IAW A300-600 SRM 53-10-12. ORIG MAT'L THK .071" REMOVED .039"; REMAINING .032" REPAIR IAW SRM 51-40-50 AND 53-10-12, FIGURE 207, SHT 3.SDR QXEA2019061200246Doubler · corrodedLAV SERVICE PORT INTERNAL DOUBLER CORRODED. REPLACED LAV SERVICE PORT INTERNAL DOUBLER IAW SRM 51-42-05 AND 51-40-15. REPAIRED FRAME FLANGE COMMON TO THE SKIN AT FSX4.1 ON RH SIDE BETWEEN STR 24 AND STR 25 IAW SRM 53-00-00 REPAIR #18 .9 NDT CARRIED OUT IAW NDTSDR SWAA2022031033258Skin · corroded***CORROSION*** FUSELAGE OUTER SKIN AROUND TAIL JACK POINT WL214 STA1084 RBL12 / REPAIRED CORROSION ON FUSELAGE OUTER SKIN BS 1084; WL 214; RBL 12 PER SWA EA 1-753-35116 REV IR AND ATS ER 19-03648 REV IR.SDR SWAA2022031033254Skin · corroded***CORROSION*** SKIN AROUND WASTE TANK VENT WL 181 STA917 STR 21L-22L / CORROSION ON SKIN AROUND WASTE TANK VENT BS 917 STR 21L-22L FOUND TO BE OUT OF LIMITS PER SRM 53-00-01-1A-1. REPAIRED BLEND DAMAGE PER ER-19-03609 REV 1R AND EA 1-753-35067 REV 1RSDR SWAA2019070234383Skin · corrodedFUSELAGE SKIN AROUND WATER SERVICE DOOR CORRODED BETWEEN BS. 910 TO BS. 924, STR. 26R. REPAIRED SKIN PER ER AND EA.SDR SWAA2019062133975Skin · corrodedFUSELAGE OUTER SKIN AROUND DRAIN CORRODED AT BS. 967+5, LBL 8. REPAIRED SKIN IAW ER AND EA.SDR CALA2019060400880Skin · corrodedCORROSION FOUND I NSIDE SKIN AT FR 20 STR 28,29 RIGHT. REPAIRED CORROSION ON SKIN AT FR20 STR 28-29 RIGHT IAW ECRA 5331 -02395. THIS A PERMANINENT REPAIR NO FURTHER ACTION REQUIRED.SDR SWAA2022030902684Scuff Plate · crackedAFT CARGO COMPARTMENT DOOR CUT-OUT AFT CORNER THRESHOLD CRACKED. / AFT CARGO DOOR AFT CORNER THRESHOLD REPAIRED ON BACKSHOP WORK ORDER 39556-1600-0002 IAW EA 1-A53-2076 REV 11.SDR SWAA2019070334493Skin · damagedFUSELAGE SKIN CREASED AT BS. 827+5, BETWEEN STR. 24L TO STR. 25L. REPAIRED SKIN IAW ER AND EA.SDR SWAA2019070334408Skin · dentedFUSELAGE SKIN DENTED AT BS. 440+5, BETWEEN STR 26R TO STR. 28R. REPAIRED SKIN PER ER AND EA.SDR IPXA2019063043916Doubler · dentedINSPECTION TYPE:12Y AFT FUSELAGE SKIN, DENT/BLEND ON REPAIR DOUBLER BETWEEN FRAME 84 & 86 AND STR. 43R.REPAIRED SAID AREA IAW EA 300-5319-01-A7811 REV. I/R AND EO A300-5330-73062-A. (MINOR)SDR DALA2019060423394Skin · dentedFUSELAGE SKIN DENTED BETWEEN FR14-15 STR 34-35RT AND BETWEEN FR15-16 STR 36-37RT, COMPLIED WITH PRI 547049-14 REVISION 1 AND ER/A 547049-14 REVISION H.SDR UIEA20190604378Skin · gougedGOUGE ON AIRCRAFT SKIN AT STA 1229, S 27 RBL AND S 26 RBL.(<P>PERFORMED INSPECTION OF DAMAGE, FOUND TO BE WITHIN LIMITS IAW SRM 53-00-01. DENT GOUGE REMOVED IAW SRM 51-10-02. NO FURTHER DEFECTS NOTED. </P><P>LP 1074740 - M5: HFEC NDT INSPECTION REQUIRED. TRANSSDR Q2SA201906041421Skin · crackedAIRCRAFT GROUNDED. CPCP ITEM LEVEL 2 CORROSION FINDING. DURING LOWER FUSELAGE EXTERNAL INSPECTION ON W/C D-53-836-0101, FOUND CRACK IN SKIN 4 AND 7/8" LONG FROM STA 940 TO 945 RIGHT SIDE OF FUSELAGE BETWEEN STRINGERS S-23R AND S-24R. ENGINEERING ORDER 3753A2SDR DALA2021041402197Doubler · dentedSHIP 658 2 DENTS REPORTED ON DOUBLER REPAIR OF 553127-14 REV ORIGINAL AT STA 620 ABOVE STRINGER 16L, DENT #1 LOCATED 0.56, AFT OF THE FRAME AND 0.87, ABOVE THE STRINGER. DENT #2 LOCATED 0.75, AFT OF THE FRAME AND 2.56, ABOVE THE STRINGER. CORRECTIVE ACTION: SUSDR DALA2019062403771Skin · damagedDAMAGE SIX FEET FORWARD OF 2L DOOR AT THE FLOOR LINE. REMOVED SEATS 16A THROUGH 16C TO ACCESS AND REM SIDEWALL PANELS FOR VISUAL INSPECTION OF SUSPECTED DAMAGE AREA REPLACED SIDEWALL PANELS AND SEATS 16A THRU 16C PER AMM 2520 NO INTERNAL DAMAGE NOTED C/W RI SDR Q2SA2019060531422Skin · scratchedAIRCRAFT GROUNDED. SCRATCH APPROX 24" LONG @ FUSELAGE STATION 1874-1895 SECTION 47 FROM STR 49L TO 46R. DAMAGE REPAIRED AS PER BOEING MESSAGE TLS-SOF-19-0015-02B.SDR P5CA2019060400097Skin · corrodedM/D STA 1238 STR 9L-10L SKIN INNER SURFACE FOUND CORROSION. (<P>CABIN <SPAN>STA 1238 STR 9L-10L SKIN INNER SURFACE CORROSION AREAS SMOOTHED IAW SRM 51-10-02 AND REPROTECTED IAW SRM 51-20-01, AND CHECKED WITHIN SRM 53-00-01 ALLOWABLE DAMAGE 1 FIG 101 LIMIT. </SSDR P5CA2019060400098Skin · corrodedM/D STA 1238 STR 10R-11R SKIN INNER SURFACE FOUND CORROSION.(<P>CABIN <SPAN>STA 1238 STR 10R-11R SKIN INNER SURFACE CORROSION AREAS SMOOTHED IAW 51-10-02 AND REPROTECTED IAW SRM 51-20-01, AND CHECKED WITHIN SRM 53-00-01 ALLOWABLE DAMAGE 1 FIG 101 LIMIT. </SPANSDR P5CA2019060400099Skin · corrodedM/D STA 1238 STR 8R-9R SKIN INNER SURFACE FOUND CORROSION.(<P>CABIN STA <SPAN>1238 STR 8R-9R SKIN INNER SURFACE</SPAN><SPAN> CORROSION AREAS SMOOTHED IAW SRM 51-10-02 AND REPROTECTED IAW SRM 51-20-01, AND CHECKED WITHIN SRM 53-00-01 ALLOWABLE DAMAGE 1 FIG 101 SDR P5CA2019060400100Skin · corrodedM/D STA 1244 STR 2R-3R SKIN INNER SURFACE FOUND CORROSION.(<P>CABIN <SPAN>STA 1244 STR 2R-3R SKIN INNER SURFACE<STRONG> </STRONG>CORROSION AREAS SMOOTHED IAW SRM 51-10-02 AND REPROTECTED IAW SRM 51-20-01, AND CHECKED WITHIN SRM 53-00-01 ALLOWABLE DAMAGE 1 FIG SDR P5CA2019060400101Skin · corrodedM/D STA 1244 STR 0-1R SKIN INNER SURFACE FOUND CORROSION.(<P>CABIN <SPAN>STA 1244 STR 0-1R SKIN INNER SURFACE CORROSION AREAS SMOOTHED IAW SRM 51-10-02 AND REPROTECTED SRM 51-20-01, AND CHECKED WITHIN SRM 53-00-01 ALLOWABLE DAMAGE 1 FIG 101 LIMIT. </SPAN></P>)SDR P5CA2019060400102Skin · corrodedM/D STA 1483 STR 18L-19L SKIN INNER SURFACE FOUND CORROSION.(<P>CABIN STA 1483 STR 18L-19L SKIN INNER SURFACE CORROSION AREAS SMOOTHED IAW SRM 51-10-02 AND REPROTECTED IAW SRM 51-20-01, AND CHECKED WITHIN SRM 53-00-01 ALLOWABLE DAMAGE 1 FIG 101 LIMIT. </P>)SDR P5CA2019060400103Skin · corrodedM/D STA 1483 STR 17L-18L SKIN INNER SURFACE FOUND CORROSION. (<P>CABIN <SPAN>STA 1483 STR 17L-18L SKIN INNER SURFACE CORROSION AREAS SMOOTHED IAW SRM 51-10-02 AND REPROTECTED IAW SRM 51-20-01, AND CHECKED WITHIN SRM 53-00-01 ALLOWABLE DAMAGE 1 FIG 101 LIMIT. <SDR P5CA2019060400104Skin · corrodedM/D STA 1483 STR 13L-14L SKIN INNER SURFACE FOUND CORROSION.(<P>CABIN <SPAN>STA 1483 STR 13L-14L SKIN INNER SURFACE CORROSION AREAS SMOOTHED IAW SRM 51-10-02 AND REPROTECTED IAW SRM 51-20-01, AND CHECKED WITHIN SRM 53-00-01 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.</SSDR P5CA2019060400105Skin · corrodedM/D STA 1238 STR 8L-9L SKIN INNER SURFACE FOUND CORROSION.(<P>CABIN <SPAN>STA 1238 STR 8L-9L SKIN INNER SURFACE CORROSION AREAS SMOOTHED IAW SRM 51-10-02 AND REPROTECTED IAW SRM 51-20-01, AND CHECKED WITHIN SRM 53-00-01 ALLOWABLE DAMAGE 1 FIG 101 LIMIT. </SPANSDR P5CA2019060400106Skin · corrodedM/D STA 1238 STR 10L-11L SKIN INNER SURFACE FOUND CORROSION.(<P>CABIN <SPAN>STA 1238 STR 10L-11L SKIN INNER SURFACE</SPAN><SPAN> CORROSION AREAS SMOOTHED IAW SRM 51-10-02 AND REPROTECTED IAW SRM 51-20-01, AND CHECKED WITHIN SRM 53-00-01 ALLOWABLE DAMAGE 1 FIGSDR P5CA2019060400109Skin · corrodedM/D STA 1003 STR 12R-13R SKIN INNER SURFACE FOUND CORROSION.(<P>CABIN <SPAN>STA 1003 STR 12R-13R SKIN INNER SURFACE CORROSION AREAS SMOOTHED IAW SRM 51-10-02 AND REPROTECTED IAW SRM 51-20-01 AND CHECKED WITHIN SRM 53-00-01 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.</SSDR P5CA2019060400110Skin · corrodedM/D STA 1003 STR 9R-10R SKIN INNER SURFACE FOUND CORROSION(<P>CABIN STA 1003 STR 9R-10R SKIN INNER SURFACE CORROSION AREAS SMOOTHED IAW 51-10-02 AND REPROTECTED IAW 51-20-01 AND CHECKED WITHIN SRM 53-00-01 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.<BR /></P>)SDR P5CA2019060400111Skin · corrodedM/D STA 1003 STR 12L-13L SKIN INNER SURFACE FOUND CORROSION(<P>CABIN STA 1003 STR 12L-13L SKIN INNER SURFACE CORROSION AREAS SMOOTHED IAW SRM 51-10-02 AND REPROTECTED IAW SRM 51-20-01 AND CHECKED WITH SRM 53-00-01 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.<BR /></P>)SDR P5CA2019060400112Skin · corrodedM/D STA 1003 STR 9L-10L SKIN INNER SURFACE FOUND CORROSION.(<P>CABIN STA 1003 STR 9L-10L SKIN INNER SURFACE CORROSION AREAS SMOOTHED IAW SRM 51-10-02 AND REPROTECTED IAW SRM 51-20-01 AND CHECKED WITH SRM 53-00-01 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.<BR /></P>)SDR P5CA2019060400113Skin · corrodedM/D STA 1003 STR 10L-11L SKIN INNER SURFACE FOUND CORROSION.(<P>CABIN STA 1003 STR 10L-11L SKIN INNER SURFACE CORROSION AREAS SMOOTHED IAW SRM 51-10-02 AND REPROTECTED IAW SRM 51-20-01 AND CHECKED WITHIN SRM 53-00-01 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.<BR /></P>SDR P5CA2019060400116Skin · corrodedM/D STA 1003 STR 14R-15R SKIN INNER SURFACE FOUND CORROSION.(<P>CABIN STA 1003 STR 14R-15R SKIN INNER SURFACE CORROSION AREAS SMOOTHED IAW SRM 51-10-02 AND REPROTECTED IAW SRM 51-20-01 AND CHECKED WITHIN SRM 53-00-01 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.<BR /></P>SDR P5CA2019060400117Skin · corrodedM/D STA 1003 STR 7R-8R SKIN INNER SURFACE FOUND CORROSION.(<P>CABIN STA 1003 STR 7R-8R SKIN INNER SURFACE CORROSION AREAS SMOOTHED IAW SRM 51-10-02 AND REPROTECTED IAW SRM 51-20-01 AND CHECKED WITHIN SRM 53-00-01 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.<BR /></P>)SDR FDEA2019060311202Skin · corrodedFOUR RIVETS PULLED THRU SKIN AT FUSELAGE STATION APPROX. FS1581.BETWEEN 50 AND 51R. REPAIRED DAMAGE IAW SRM 53-00-06-2R.
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