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 SWAA2020031642497Skin · dentedFUSELAGE SKIN HAS A DENT BS 992+4, 1" BELOW STR 14L, DENT MEASURES: L=.8", W=.6", Y=.003" W/Y=200 DAMAGE REPAIRED/INSPECTED & EVALUATED PER EA 1-753-36715 REV IR (ATS ER 20-01888 REV IR) INSTALLED DENT DOT PER MPM 52.03.01.02 PARAGRAPH 2.C.(1)(B) NO FUSDR SWAA2020031642496Skin · dentedFUSELAGE SKIN HAS A DENT BS 1006+3.7, 2.9" BELOW STR 14L, DENT MEASURES: L=2.3", W=1.9", Y=.004" W/Y=475 REPAIR ACCOMPLISHED ON ER NO 20-01888 REV IR & EA NO 1-753-36715 REV IR FACT AS A RESULT OF POST REPAIR INSPECTIONSDR SWAA2020031202394Skin · not reported(SKYLINE DTIP) FUSELAGE SKIN REPAIR AT BS 1025, S-15L TO S-17AL REQUIRES ADDITIONAL REWORK. (REF ESR: 20-01837) FUSELAGE SKIN REPAIR AT BS 1025, S-15L TO S-17AL WAS REPAIRED IAW ATS ER 20-01871 REV IR DATED 28FEB2020 AND EA 1-753-36639 REV IRSDR REXA2020030200249Coaming · worn"INITIAL INSPECTION: WEAR SEVERAL PLACES AROUND AFT BAGGAGE-BAY DOOR CUT OUT CARGO-2 TCI: 53-30-204
""(LOWER COAMING) AFT BAGGAGE-BAY DOOR CUT OUT CARGO-2 WAS REPLACED PERCRJ-900 SRM 51-41-02-001-001-A01 SDR FDEA202002200358Skin · damagedWHILE ACCOMPLISHING E.O. #G-5310-EO332629 D P5 FOUND EXISTING UNDERWING LONGERON FASTENER HOLE AT LEFT HAND STATION 1014 AND STRINGER 36 LEFT OVERSIZED TO 0.403" INSTEAD OF 0.371" AS PER DRAWING 675W0002 SHEET 8. WORK ACCOMPLISHED AS PER EA G-5310-T0352363SDR FDEA202002200357Skin · crackedDURING ACCOMPLISHMENT OF HIGH FREQUENCY EDDY CURRENT INSPECTION ON LEFT HAND SIDE FUSELAGE SKIN COMMON TO UNDERWING LONGERON, FOUND 02 CRACK INDICATION AROUND FASTENER HOLES AT STATION 1024 AND STATION 1032, STRINGER 37 LEFT, APPROXIMATE 0.8" AND 1" IN LSDR ABXR2020022700013Skin · crackedUPPER L/H FUSELAGE STA 1654.5 BETWEEN STRINGERS 4L-5L EXTERNAL SKIN IS CRACKED.REPAIRED L/H FUSELAGE SKIN STA: 1654.5 I.A.W. B767 SRM 53-80-01-2R-4 REPAIR 4.SDR SWAA2020022641717Doubler · corrodedDOUBLER ATTACHED TO FORWARD LOWER INTERCOSTAL ATTACH POINT ON LAV PAN AT BS. 849 JUST ABOVE STRINGER 25 LEFT. / R&R DOUBLER IAW SRM AND DWG.SDR DALA2020022101309Skin · corrodedCORROSION ON FUSELAJE SKIN STA=864 AND STR- 28R TO STR- 29R. SUMMARY OF NRC 00198: CORROSION (LEVEL 2) ON FUSELAJE SKIN STA= 864 AND STR- 28R TO STR- 29R WAS REPAIRED PER ETI-90-20-009 REV. ORIGINAL AND ER/A 585513-14 REV. ORIGINAL SECTION I. ACCORDING TO ER/ASDR SWAA2021082019396Skin · corrodedCORROSION ON FUSELAGE SKIN AROUND DRAIN VALVE BS 480+18; 6.5' BELOW STR 28L / BLENDED CORROSION ON FUSELAGE SKIN AROUND DRAIN VALVE BS 480+18 6.5' BELOW STR 28 L/H INSPECTED & EVALUATED PER EA 1-753-36709 REV IR & ATS ER 20-01892 REV IR THIS EA THE DAMAGE IS ASDR SWAA2021082019397Skin · corrodedCORROSION ON FUSELAGE SKIN AROUND DRAIN VALVE BS 500A+3; 6.5' BELOW STR 28L / BLENDED CORROSION ON FUSELAGE SKIN AROUND DRAIN VALVE BS 500A+3 6.5' BELOW STR 28 L/H INSPECTED & EVALUATED PER EA 1-753-36709 REV IR & ATS ER 20-01892. REV IR AS PER THIS EA THE DAMSDR SWIA2020040649941Skin · gouged3 EA. GOUGES ON FUSELAGE SKIN, (2 FWD. AND 1 AFT), OF F.S 985.00 AT STRG. 27 (MRK€™D) (C-CHECK) RO 4/3/2020 COMPLIED WITH REO. REPAIR OF 3 EA. GOUGES ON FUSELAGE SKIN, F.S 985.00 AT STRG. 27 LEAK CHECK GOOD COMPLIED WITH SKYWEST TASK CARDSDR SWAA2020032331169Skin · gougedFUSELAGE SKIN HAS A GOUGE BS 400+2.4; STR 27R / FUSELAGE SKIN GOUGE BS 400+2.4; STR 27R REPAIRED IAW ATS ER 20-01914; REV IR; DATED 10-MAR-2020 AND PER EA NO: 1-753-36694 REV IR 55981U 11MAR20SDR SWAA2020031642495Skin · gougedFUSELAGE SKIN HAS A GOUGE BS 400+2.4, STR 27R FUSELAGE SKIN GOUGE BS 400+2.4, STR 27R REPAIRED IAW ATS ER 20-01914, REV IR, DATED 10-MAR-2020 AND PER EA NO: 1-753-36694 REV IR 55981U 11MAR20SDR DALA2020022591380Skin · corrodedWASTE SYSTEM VACUUM BLOWER FWD OUTLET AREA SKIN FOUND CORROSION. REPAIRED DOUBLER AND TRIPLER PER SRM 53-60-01. (LP 1495819)SDR SWAA2020022441626Doubler · crackedEXTERNAL POWER RECEPTACLE SURROUND DOUBLER DAMAGE WITH .375"CRACK NOTED 4" UP FROM AFT LOWER CORNER JUST BELOW INITIAL RUBBING STRIP. / REPAIRED DOUBLER PER SRM.SDR V0XD202002190012Tripler · gougedEXTERNAL FUSELAGE SKIN REPAIR, TRIPPLER AT F.S. 977.00 GOUGED. CORRECTIVE ACTION TO BE ACCOMPLISHED ON W/O 80799 W/C 1167.SDR SWAA2020032442812Skin · dentedFOUND A DENT ON FUSELAGE SKIN SECTION 43 STA 360+2.2" AND 2" ABOVE STR 5L DOT 107-018 FUSELAGE SKIN SECTION 43 STA 360+2.2" AND 2" ABOVE STR 5L REPAIRED PER AAR RES WI 2015746-6 REV IR AND EA NO 1-753-36736 REV IR FACT AS A RESULT OF POST REPAIR INSPECSDR SWAA2020032442682Skin · dentedFOUND A DENT ON FUSELAGE SKIN SECTION 43 STA 360+2.5" AND 2" BELOW STR 5L DOT 107-018 REPAIR ACCOMPLISHED PER EA 1-753-36736 REV IR (AAR RES WI NO 20105746-6 REV IR). REFER TO NRC W141014 FOR TRACKING.SDR SWAA2020032442681Skin · dentedFOUND DENT ON FUSELAGE SKIN SECTION 43 STA 360 + 2.5" AND OVER STR 17L DOT 107- / 015 INSTALLED REPAIR AT FUSELAGE STA 360-391, BETWEEN STR 16L & STR 18L REF AAR / RES-WI #2015746-2 REV I.R AND SOUTHWEST EA NO: 1-753-36647 REV IRSDR IPXA2020030952892Finger Doubler · corrodedINSPECTION TYPE:2CCENTER CARGO BETWEEN STA. 1721 TO 1741 AND L51 R/H TO L51 L/H HAS CORRODED FINGER DOUBLER.REMOVED, FABRICATED AND REPLACED FINGER DOUBLER BETWEEN STA 1721 TO 1741 AND L 51R TO 51L IAW DWG AGA7809 AND SRM 51-35-01. (MINOR)SDR IPXA2020030252613Skin · crackedINSPECTION TYPE:C12CRACK ON FUSELAGE SKIN (P/N : 148T3131-6) NEAR STA 1654 , S-13ARREPAIR I.A.W 767-300F SRM 53-80-01-2R-7 REV.76.01SDR 2020F00250Beam · corrodedAIRBORNE/PEMCO NON-ROUTINE 2387N736 DISCREPANCY: FWD CARGO COMPARTMENT, OUTER CORD OF LWR SILL FASTENER LOCATION CORRODED AT FS 610, STRINGERS S-32R. PEMCO ENG. SVC. REQUEST NO.: RES 14415: FWD LWR CARGO DOOR BEAM HAS CORROSION ON UPPER AND LWR FLANGES. REQUESSDR CALA2020022400469Skin · dentedTHE LOWER FUSELAGE HAS A DENT AT THE 6 O CLOCK POSITION BELOW THE FORWARD CARGO DOOR S-29L TO 29R (BETWEEN STA 580 - 600) DOT 48-003 REF AAR N/R 9733007 EVALUATED DENT AT LOWER FUSELAGE SKIN BETWEEN STA 580 & STA 600 S-29L TO S-29R DENT MEASURES L=2.300" W=1.6SDR UIEA202002210286Skin · corrodedSKIN AT LOWER LOBE CIRCUMFERENTIAL SPLICE LOCATION AT STA 1720 TO STA 1741 S45L 3 EA AREA FOUND CORROSION INDICATION.(<P>FUSELAGE SKIN BETWEEN STA 1720 TO STA 1740 STR 45L CORROSION AREAS REPAIRED IAW RI 53-00-13922 REV A.</P>)SDR DALA2020022091297Pressure Plate · crackedA CRACK DOES NOT EXCEED THE AUTHORIZED REPAIR AREA WAS FOUND AT THE PR ESSURE PLATE AREA BETWEEN FR 35LH AND FR36LH, PERFORMED REPAIR ON INTERNAL STRUCTURE BETWEEN FR 35 TO FRAME 36 LH SIDE ON PRESSURE PANEL ON OPEN HOLES AS PER WORK CARD 5311-01171- 04A-DE, SSDR GTIA2020021985023Skin · gougedGOUGE FOUND ON SKIN PANEL FR43 LH STR Y+1650.0. DAMAGE L 24-30MM X W 12.15MM X D 1.32MM, ORIGINAL STRUCTURE THICKNESS 5MM. RAF01 2516705-02 OPENED. REF LTPR NRI 5000976522-0010.-REVIEWED NR#5000976522-0010 AND HAS BEEN ACCOMPLISHED. REFER TO EO5331-2013 REV 00SDR GTIA2020021985022Skin · damagedBURN MARK FOUND ON SKIN PANEL AT FR 27-28, STR 6RH. RAF-01 2516706-01 OPENED. REF LTPR NRI 5000963029-0010.-REVIEWED LTPR NR#5000963029-0010 AND SPIRIT TC NR-00003 AND HAS BEEN ACCOMPLISHED. PERFORMED CONVERSION OF TEMP REPAIR INTO PERMANENT AS PER AIB POSSIERSDR DALA2020021901241Skin · corrodedAWR HIDDEN CORROSION IN REF NRC 895. DURING REMOTION OF VAPOR BARRIER WAS FOUND CORROSION ON CENTER WING UPPER SKIN STA 943- 962 BTW X=-44 TO X=-60 AT WING BOX AREA MRB 57-331-02 (CPAX) SUMMARY; OF NRC 01179: CORROSION LEVEL 1; CORROSION ON CENTER WING UPPER SSDR DALA2020021901240Skin · corrodedINITIAL INSPECTION: CORROSION ON CENTER WING UPPER SKIN STA 992 BTW X=44 AT WING BOX AREA MRB 57-331-02 (CPAX) SUMMARY OF NRC 00891. CORROSION LEVEL 1. CORROSION ON CENTER WING UPPER SKIN STA 992 BTW X=44 AT WING BOX AREA WAS REMOVED PER MD-90 SRM 51-10-03 PARSDR DALA2020021901239Skin · corrodedINITIAL INSPECTION: CORROSION ON CENTER WING UPPER SKIN STA 902 TO 924 BTW X=44 TO X=60 AT WING BOX AREA MRB 57-331-02 (CPAX) SUMMARY. OF NRC 0888. CORROSION LEVEL I. CORROSION ON CENTER WING UPPER SKIN STA 902 TO 924 BTW X=44 TO X=60 AT WING BOX AREA WAS REMOSDR DALA2020021801200Skin · corrodedINITIAL INSPECTION: CORROSION ON CENTER WING UPPER SKIN STA 902 TO 924 BTW X=-44 TO X=-60 AT WING BOX AREA MRB 57-331-02 (CPAX) SUMMARY; OF NRC 00884, CORROSION LEVEL 1 , CORROSION ON CENTER WING UPPER SKIN STA 902 TO 924 BTW X=-44 TO X=-60 AT WING BOX AREA WASDR DALA2020021801199Skin · corrodedINITIAL INSPECTION: CORROSION ON CENTER WING UPPER SKIN STA 924 TO 943 BTW X=-44 TO X=-60 AT WING BOX AREA MRB 57-331-02 (CPAX) SUMMARY; OF NRC 00885, CORROSION LEVEL 1; CORROSION ON CENTER WING UPPER SKIN STA 924 TO 943 BTW X=-44 TO X=-60 AT WING BOX AREA WASSDR DALA2020021801198Skin · corrodedINITIAL INSPECTION: CORROSION ON CENTER WING UPPER SKIN STA 924 TO 943 BTW X=44 TO X=60 AT WING BOX AREA MRB 57-331-02 (CPAX) SUMMARY ; OF NRC 889, CORROSION LEVEL 1 ; CORROSION ON CENTER WING UPPER SKIN STA 924 TO 943 BTW X=44 TO X=60 AT WING BOX AREA WAS ATTSDR DALA2020021801197Skin · corrodedINITIAL INSPECTION: CORROSION ON CENTER WING UPPER SKIN STA 943 TO 962 BTW X=44 TO X=60 AT WING BOX AREA MRB 57-331-02 (CPAX) SUMMARY ;OF NRC 00890, CORROSION LEVEL 1 : CORROSION ON CENTER WING UPPER SKIN STA 943 TO 962 BTW X=44 TO X=60 AT WING BOX AREA WAS ATSDR DALA2020021801196Skin · corrodedINITIAL INSPECTION: CORROSION ON CENTER WING UPPER SKIN STA 883 TO 902 BTW X=44 TO X=60 AT WING BOX AREA MRB 57-331-02 (CPAX) SUMMARY OF THE NRC 00887: CORROSION WAS ATTENDED PER MD-90 SRM 51-10-03 PAR 26 (A) VOL. II ETI-90-20-008 REV. 1 AND ER/A 585247 -14 RESDR DALA2020021801195Skin · corrodedINITIAL INSPECTION: CORROSION ON CENTER WING UPPER SKIN STA 962 TO 984 BTW X=-44 TO X=-60 AT WING BOX AREA MRB 57-331-02 (CPAX) SUMMARY OF THE NRC 00886: CORROSION WAS ATTENDED PER MD-90 SRM 51-10-03 PAR 26 VOL. II AND ETI-90-20-007 REV. ORIG AND ER/A 585124-1SDR SWIA2020032749417Skin · chafed*EXTERNAL SKIN HAS FOUR CHAFES ALONG STGR27 BETWEEN FS969.00 €“ FS977.00. (MARKED) (C-CHECK) RO 3/25/2020 REPAIRED EXTERNAL SKIN ALONG STGR27 BETWEEN FS969 - FS977 REF REO. COMPLIED WITH TASK CARD STRUCTURAL MAJOR REPAIR (**RII**). LEAK CHECK GOODSDR AALA202002189022Skin · corrodedAIRCRAFT WAS GROUNDED: CORROSION AND CRACK ON AFT FUSELAGE SKIN PANEL AT THE LAVATORY EXHAUST PORT CUT OUT BETWEEN FR 69 AND FR 70 BETWEEN S31R AND S32R. REPAIRED SKIN PER SRM 53-41-11-300-004.**SUPPLEMENTAL REPORT TO CORRECT SECTION 3 TOTAL TIMES AND CYCLES.SDR 2020FA0000187Skin · corrodedAIRBORNE/PEMCO NON-ROUTINE 2387N1106 DISCREPANCY: (722109) CORROSION ON SKIN, INTERNAL SIDE STA. 1263-1285 STR. 36-37 R/H CORRECTIVE ACTION: REMOVED & REPLACED DAMAGED SHEAR TIE @ STA 1285, BETWEEN S37R-S36R IAW B767 SRM 51-40-02. REPAIR DOUBLER & TRIPLER FROSDR CALA2020022400461Skin · corrodedFWD LAVATORY SERVICE PANEL IS BULGING AT RIGHT AFT CORNER AND ALSO HAS A RIVET HEAD PULLING THROUGH. REMOVED FWD LAVATORY SERVICE PANEL AFT R/H CORNER HAS CORROSION,BURNISHED CORROSION REF SRM 51-10-10. SKIN IS .080 THICK REF SRM 53-10-10 . NEED TO VERIFY HOW SDR CALA2020022400463Skin · dentedREAR FUSELAGE UPPER EXTERNAL SURFACE FOUND 1EA DENT MARK AT FR82 -83 STRINGER 2R-3R REF NON-ROUTINE NO.9400060 - ORIGINATED BY EMP V916780,SPEC NO.A3NB-05-3-6062. REAR FUSE UPPER EXT SURFACE AT FR82-FR83 STR 2R-3R REPAIRED PER SRM 53-51-11-300-010. THIS IS A CSDR HNAA2020021800069Skin · dentedDMT 40 - ACCOMPLISH PERMANENT REPAIR OF DENT IN LH FORWARD FUSELAGE NEAR ACCESS DOOR 123BL BETWEEN FR 8 AND 9,SL18L-19L COMPLETE: ACCOMPLISHED PERMANENT REPAIR OF DENT IN LH FORWARD FUSELAGE NEAR ACCESS DOOR 123BL BETWEEN FR 8 AND 9, SL18L-19L IAW PIEDMONT ESDR C77A202002170005Skin · dentedDURING BASIC CHECK AT EAMS, DENT DAMAGE WAS DISCOVERED ON THE P/N 170-61701-013 REAR FUSELAGE LOWER SKIN AT THREE LOCATIONS IN TWO BAYS BETWEEN FR94/FR95 AND S-21L/S-23L. REFERENCE ETD2020-170-005177-A FIGURE 1 FOR DAMAGE DETAILS. THE DAMAGE IS NOT ALLOWABLE PSDR AALA202002189021Doubler · crackedAIRCRAFT WAS NOT GROUNDED: CRACKED FUSELAGE SKIN DOUBLER AT THE EXTERNAL GROUND POWER DOOR CUT OUT WHERE THE DOOR LATCH CONTACTS. REPAIRED SKIN DOUBLER PER EA 303418.SDR IPXA2020021765179Skin · damagedINSPECTION TYPE:N/AINTERIM REPAIR TO FUSELAGE SKIN R/H SIDE OF THE A/C AFT OF FR2, REF EO A300-5330-60265-AREPAIRED PER EO A300-5330-60265-BSDR SWIA2020033049504Skin · dentedADM #1293. FS 625.25 AND STR 15.75R RIGHT SIDE OF AIRCRAFT BELLOW ENGINE. FOUND TO BE A DENTED SCRATCH MEASURES 2.55 INCHES LONG AND .011 INCHES DEEP. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACSDR R61A202002190193Doubler · corrodedWHILE IN HEAVY CHECK FOUND FORWARD CARGO, CORRODED FASTENERS BETWEEN FR21-FR22, STGR28R- 27R. REMOVED CORROSION ON THE DOUBLER BY BLENDING. MAX. MATERIAL REMOVED WAS 0.003" FROM AN ORIGINAL OF 0.050". THERE ARE NO LIMITS AVAILABLE ON THE DOUBLER. REF SRM 51-10SDR DALA2020021761183Skin · crackedINITIAL INSPECTION: CRACK ON FUSELAGE SKIN STA Y=1494 BTW LONG 2 -3 LH (FUS) LOG-PAGE UPDATED SUMMARY OF NRC 00591: SKIN STA Y=1494 BTW LONG 2-3 LH WAS REPAIRED PER ER/A 585379-14 REV. ORIG AND ETI-90-20-002 REV. 1 PERFORM A GENERAL VISUAL INSPECTION PER ER/A SDR DALA2020021761182Skin · corrodedINITIAL INSPECTION: CORROSION ON PREVIOUS REPAIR FRAME STA 1364 BTW LONGS 29RH AND 28RH AT AFT CARGO COMPARTMENT MRB 53-302-07 ( CCT) SUMMARY OF NRC 00555. CORROSION LEVEL 2 PREVIOUS REPAIR FRAME STA 1364 BTW LONGS 29RH AND 28RH AT AFT CARGO COMPARTMENT WAS RE
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