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 I5EA2019052100017Skin · crackedDISCREPANCY: FOUND CRACK AT LT FUSELAGE STA. 460 BETWEEN STRINGERS 8L AND 9L. CORRECTIVE ACTION: ACCOMPLISHED REPAIR AT LT FUSELAGE STA 460 BETWEEN STRINGERS 8L AND 9L PER AD 2009-01-02 AND SB 737-25-1544 INSTRUCTIONS.SDR I5EA20190512Skin · crackedDISCREPANCY: FOUND CRACK AT LT FUSELAGE STA. 500F BETWEEN STRINGERS 8L AND 9L. CORRECTIVE ACTION: ACCOMPLISHED REPAIR AT LT FUSELAGE STA. 500F BETWEEN STRINGERS 8L AND 9L PER AD 2009-01-02 AND SB 737-25-1544 INSTRUCTIONS.SDR I5EA20190511Skin · crackedDISCREPANCY: FOUND CRACK AT LT FUSELAGE STATION. 360 BETWEEN STRINGERS 8L AND 9L. CORRECTIVE ACTION: ACCOMPLISHED REPAIR AT LT FUSELAGE STATION. 360 BETWEEN STRINGERS 8L AND 9L PER AD 2009-01-02 AND SB 737-25-1544 INSTRUCTIONS.SDR I5EA2019052100001Skin · damagedDISCREPANCY: FOUND DAMAGE AT RT FUSELAGE STA. 400 BETWEEN STRINGERS 8R AND 9R. CORRECTIVE ACTION: ACCOMPLISHED REPAIR AT RT FUSELAGE STA. 400 BETWEEN STRINGERS 8R AND 9R AS PER AD 2009-01-02 AND SB 737-25-1544 INSTRUCTIONS.SDR SWAA2022030981672Scuff Plate · crackedFCB FWD AND AFT SCUFF PLATES ARE CRACKED / RECEIVED NEWS PARTS WITH P/N 654A0004-337 FWD SIDE P/N 654A0004-338 AFT SIDE LOCATED AND DRILLED CORNER SCUFF PLATES IAW SRM 51-40-05; FWD AND AFT CORNER SCUFF PLATE WILL BE ISNTALLED WITH CARD #753-646-62-01. 59202U SDR SWAA2022030981673Scuff Plate · crackedACB FWD AND AFT SCUFF PLATE ARE CRACKED / RECIVED FWD AND AFT SCUFF PLATE; ACB AND LOCATED AND DRILLED IAW SRM 51-40-05-0G-0 WILL BE INSTALL WITH CARD# 753-721-00-01 59205U 27MAY19SDR SWAA2022030902343Scuff Plate · crackedAFT CARGO BAY FWD SCUFF PLATE IS CRACKED / REMOVED AND REPLACED AFT CARGO BAY FWD SCUFF PLATE IAW AMM TASK 53-11-02-020-801 AND AMM TASK 53-11-02-420-801.SDR SWAA2022030902344Scuff Plate · crackedAFT CARGO BAY AFT SCUFF PLATE IS CRACKED / REPLACED AFT CARGO BAY AFT SCUFF PLATE. LOCATED AND DRILLED NEW AFT CARGO BAY AFT SCUFF PLATE PER REF AMM 53-11-02-020-801 AND AMM 53-11-02-420-801.SDR SWAA2022030904372Skin · out of toleranceDTIP - DOUBLER REPAIR FOUND ON LOWER EXTERNAL FUSELAGE SKIN AT BODY STATION 185; LBL 5; REPAIR DEVIATIONS REGARDING FASTENER TYPE; SPACING; AND REPAIR DOUBLER LOCATION REQUIRE INSTALLATION OF NEW REPAIR PER AAR EA 190305. / REMOVED EXISTING REPAIR ON EXTERNAL SDR V0XR20190613AV2Skin · corrodedAVIONICS BAY DOOR SEAL INTERFACE/DOOR CUTOUT HAS LIGHT CORROSION WITH SMALL NICKS AROUND ENTIRE CIRCUMFERENCE ON INNER SKIN REPAIRED REO 690-53-21-032 (RECOMMENDED MOD IS69053210009 TO BE INCORPORATED) REPEAT INSPECTION 13,100 FLIGHT CYCLESSDR REXA2019060414780Doubler · corrodedCORROSION ON INTERNAL PRODUCTION DOUBLER IN STA. FS= 295 TO FS= 310 BETWEEN STGR 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT. THE PRODUCTION DOUBLER WAS REPLACED PER CRJ-900 S.R.M. 51-42-06-001-001-A01 PAR. 6.SDR CALA2019051700774Doubler · crackedREF. N/R: 99834615 EXT PWR RECEPTACLE DOUBLER CRACKED AT FWD MID SECTION. DATA WAS TRANSCRIBED FROM PAPER DOCUMENT N/R 99834615 WORK ACCOMPLISHED. REMOVED AND REPLACED THE EXTERNAL POWER RECEPTACLE CUTOUT DOUBLER AS PER SRM 51-40-02 & 53-10-15 (FOR DETAILS SEESDR DALA2019051503042Skin · cracked(LOG 1074319) DURING INSPECTION FOUND CRACKED EXTERNAL SKIN NATS AIRPHONE ANTENNA NR 2 AT LOWER FUSELAGE. REPLACED AIRPHONE ANTENNA 2 BY COVER PLATE ON AFT LOWER FUSELAGE AS PER ERA 12-090911-14 REV. C.SDR FXGA201905141940Skin · corrodedCORRODED FUSELAGE SKIN AT F/STA 150 STRINGER 33L. CORROSION WAS FOUND 2 INCHES FORWARD OF AN EXISTING REPAIR MADE PER OVERHAUL MANUAL FIGURE 12-22. REMOVE EXISTING REPAIR AND CUT-OUT CORRODED AREA. EXTEND REPAIR PER OVERHAUL MANUAL FIGURE 12-22 TO COVER NEWSDR R61A201906110598Skin · dented2 DENTS FWD OF FRAME11, ABOVE STRINGER 18L, L=20MM W=10MM D=-.015" BELOW STRINGER 18L, L=21MM W=11MM D=.020". REMOVED AND REPLACED THE SHEAR TIE AT FRAME 12 BETWEEN STRINGER 19L - 20L. RECONTOURED DENTS AT FRAME 12, STRINGER 19L -20L, AND FR 11, STRINGER 18LSDR SWAA2019061133529Skin · damagedSKIN CREASED BETWEEN BS. 380 TO BS. 400, BETWEEN 1" ABOVE STR. 24L TO 1" BELOW STR. 23L. / REPAIRED SKIN IAW EA.SDR ABXA20190513031Skin · crackedCRACK IN SKIN AT FUSELAGE STATION 757 BETWEEN STRINGERS 35R AND 36R. THE SKIN WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR ABXA20190513023Skin · corrodedCORROSION ON THE FUSELAGE SKIN AT STRINGERS 38L AND 39L AT FUSELAGE STATION 420. THE SKIN WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR P5CA2019051400069Skin · damagedREPAIR- SKIN MODIFICATION PER SB 747-53A2487.(<P>1. REPAIR DAMAGED AREA IAW EI NO. T2019A53M-1979 REV. 2. 2. JOB COMPLETED AND COND CHK NORMAL.</P>)SDR P5CA2019051400071Skin Panel · crackedREPAIR- SHARP DENTS WITH CRACK ON RH SIDE SKIN PANEL BETWEEN STA 2690.85 AND 2701.51(<P>1. ACCOMPLISHED REPAIR AREA I.A.W. EI NO. T2019A53M-2495 REV. 1. </P><P>2. JOB COMPLETED AND COND CHK NORMAL.</P>)SDR ASOA201905134016Skin · dentedIAH - DURING MAINTENANCE INSPECTION A DENT IN THE SKIN WAS DISCOVERED AT FRAME 63 STRINGER 21R-20R ON A RIVET LINE. MAINTENANCE CUT OUT THE DAMAGED SKIN AND PERFORMED A FILLER / DOUBLER REPAIR. OPERATIONAL/ PRESSURIZATION CHECKSWERE PERFORMED WITHOUT DEFECT ANSDR CALA2019051300766Doubler · crackedREF. N/R: 99834615 EXT PWR RECEPTACLE DOUBLER CRACKED AT FWD MID SECTION. DATA WAS TRANSCRIBED FROM PAPER DOCUMENT N/R 99834615 WORK ACCOMPLISHED REMOVED AND REPLACED THE EXTERNAL POWER RECEPTACLE CUTOUT DOUBLER AS PER SRM 51-40-02 & 53-10-15 (FOR DETAILS SEE SDR REXA2019061720869Skin · damagedINITIAL INSPECTION: LIGHTNING STRIKES (3EA) ON EXTERNAL FUSELAGE SKIN, FS253.5, FS259.5 AND FS261 OVER STGR 27. (FUS)
LIGHTNING STRIKES (3EA) ON EXTERNAL FUSELAGE SKIN, FS253.5, FS259.5 AND FS261 OVER STGR 27 WERE REPAIRED PER CRJ 900 SRM 53-00-00-201-003-A03SDR CA190521012Skin · corroded(CAN) RH SKIN BLENDED TO REMOVE CORROSION AT APU EXHAUST HEAT SHIELD LOCATIONS. (TC# 20190521012)SDR CALA2019051300754Skin · crackedLT FRAME 35 STRINGER 30 HOLE 2 IS CRACKED IN SIDE SHELL LAYER AT 5:00 OUTBOARD LOOKING INBOARD A3NB-53-3-6315 PER NON ROUTINE 9296254 INTERIM REPAIR ACCOMPLISHED PER ECRA 5331-02382 PART 1. A PERMANENT REPAIR NEEDS TO BE ACCOMPLISHED PER PART 3 OF ECRA 5331-02SDR WVER2019051119Doubler · corrodedPERFORMED A MAJOR REPAIR BY REMOVING TCAS ANTENNA DOUBLER AND STRINGER 27 FORWARD SECTION AT FS 295 TO FS 310. INSTALLING A NEW SERVICABLE TCAS DOUBLER P/N SH670-32364-7 AND THE SAME SERVICABLE STRINGER 27 FORWARD SECTION IAW SRM 51-40-11-001-001-A01, 51-47-06SDR WVER2019051017Skin Panel · chafedFUSELAGE LOWER SKIN PANEL BETWEEN 910 TO 927 HAS SEVERAL CHAFES AT STIRINGER 27. REPAIRED FUSELAGE LOWER SKIN PANEL IAW REO 670-53-00-290 REV. E.SDR SWAA2022030946798Skin · corrodedINVESTIGATING DEFECT NO N203097; CORROSION WAS FOUND ON EXTERNAL FUSELAGE SKIN BS 989-994 LBL 8.5 AT FASTENER LOCATIONS 4EA(INSIDE BS 986-1006 BETWEEN STR2R-2L AS DOCUMENT ED ON N203097/ SA-M 326 A1234592) / REPAIRED EXTERNAL SKIN; FUSELAGE BS 986-1006 BETWEENSDR CA191121005Doubler · corroded(CAN) SER - DISPOSITION FOR CORROSION DAMAGE, BOTTOM SKIN, WASTE ACCESS DOUBLER OPERATOR REPORTED CORROSION DAMAGE ON REAR BARREL BOTTOM SKIN, WASTE ACCESS DOUBLER P/N C01342310-103 REF. CORROSION WAS BLENDED (TC# 20191121005)SDR SWAA2019060433258Skin · damagedSKIN DAMAGED AT BS. 1010, 1" BELOW STR. 14L. / REPAIRED SKIN DAMAGE IAW EA & ER.SDR SWAA2019052332940Skin · crackedAFT PRESSURE BULKHEAD WEB OUTER SKIN CRACKED AT BS. 1016, STR. 7R INNER MOST FASTENER ADJACENT TO CENTER PLUG. REPAIRED SKIN IAW EA.SDR R61A201905090502Strap · corroded*** WHILE AIRCRAFT WAS IN FOR HEAVY CHECK *** MAINTENANCE REPORTED LEVEL 2 CORROSION ON SEVERAL AREAS ON AFT BELLY FAIRING ATTACHMENT FLANGE STRAP BETWEEN FR74 TO FR76 AND STRG 22R - 28R. MAINTENANCE REMOVED AND REPLACED THE AFT BELLY FAIRING ATTACHMENT FLANGESDR ASOA201905094017Skin · corrodedIAH - DURING MAINTENANCE INSPECTION THE BELLY SKIN WAS FOUND TO BE CORRODED UNDER THE AFT RADIO ALTIMETER BASE. MAINTENANCE REMOVED THE CORROSION, CUT OUT THE DAMAGED SKIN AND PERFORMED A FILLER / DOUBLER REPAIR IN ACCORDANCE WITH TECHNICAL DISPOSITION ETD2019SDR DALA2019051302974Doubler · dented(AIRCRAFT 682, L/P 1066806) TOOL MARKS ON PREVIOS REPAIR DOUBLER SKIN STA 1500 TO 1520 BTW LONGERON 28RH/L (FUS). CORRECTIVE ACTION: SUMMARY OF NRC 00111: DENTS AT EXISTING REPAIR BTW BS 1500-1520 AND S-28L TO S-28R WERE EVALUATED PER ETI-57-19-060 REV: 1 AND SDR DALA2019051302973Doubler · dented(AIRCRAFT 682, L/P 1066795) TOOL MARKS ON PREVIOS REPAIR DOUBLER SKIN STA 1500 TO 1520 BTW LONGERON 28R/L (FUS). SUMMARY OF NRC 00111: DENTS AT EXISTING REPAIR BTW BS 1500-1520 AND S-28L TO S-28R WERE EVALUATED PER ETI-57-19-060 REV: 1 AND ER/A 515024-14 REV: SDR CALA2019051300746Skin · crackedREF NR LP 9130407 SUPPORT TASK EA 5380-01178 RT FUSELAGE BS1654 TO BS 1674 STR 13A FOUND CRACK AT SKIN APPROX 3/4" IN LENGTH FUSELAGE BS1654 TO BS 1674 STR 13A CRACKED AREA REPAIR CARRIED OUT AS PER SRM 53-80-01 REPAIR 7 FORM 44.0008 ITEM 1-20 ATTACHED DIP RAISDR CALA2019051300745Skin · crackedREF. N/R: 99835371 AS PER T/C EA 5310-05878 REV F OP001 IF CRACKS ARE FOUND ON THE RT SIDE STA 540 NBETWEEN STR S-22R AND S-23R INSTALL A SKIN REPAIR IAW OP-05 OF EA 5310-05878 REVF OP005 REPAIR FRAME 540 RT SIDE BETWEEN STR 22R AND 23R PER EA 5310-05878 REV FSDR 7C7A2019050910504Skin Panel · dented2 DENTS ON LEFT HAND FUSELAGE BETWEEN STATION X277-X285 ABOVE AND BELOW STRINGER 11P. RD 8-53-16128 WAS ISSUED AND PROVIDES PREMANENT ALLOWANCE FOR MULTIPLE DENT DAMAGE TO THE LEFT HAND SIDE FUSELAGE SKIN PANELS(P/N 85320281 AND 85320313) BETWEEN X270.50 - X29SDR SWAA2022030929787Scuff Plate · crackedAFT CARGO BAY AFT CORNER THRESHOLD IS CRACKED. / REPAIRED PER EA 1-A53-2076 REV 11SDR SWAA2022030903876Scuff Plate · crackedR1 DOOR SCUFF PLATE FOUND CRACKED / REMOVED R1 DOOR SCUFF PLATE IAW AMM 53-11-01-000-801 LEAD33 09MAY19. OK TO INSTALL INSP391 09MAY19 INSTALLED R1 DOOR SCUFF PLATE IAW AMM 53-11-01-420-801SDR SWAA2019061133528Skin · crackedFASTENER HOLE OF T CORD CRACKED BETWEEN BS. 180 TO BS. 188, BETWEEN LBL 1 TO LBL 8. / REPAIRED SKIN PER EA.SDR FDEA201905071010Skin · damagedMDIS 608 53-30 8313 05MAY19 MEM OPEN U FOUND RIVETS PULLING THRU THE SKIN ON THE AFT RT SIDE OF FUSELAGE, APPROX 18 INCHES BELOW THE AFT CARGO DOOR FRAME, FROM CENTER OF DOOR FRAME GOING AFT. MARKED WITH GREEN TAPE. BETWEEN STA. 1721 AND STA. 1781 PSDR A6WA2019050846595Skin · dentedREF LP 326168 / 1 - FUSELAGE AFT OF F.S.755.00 ON BOTTOM SIDE OF FUSELAGE DAMAGED. APPROXIMATELY 28 INCHES BY 9 INCHES OF DENTED / WRINKLED SKIN. TWO STRINGERS DAMAGED ON INSIDE OF FUSELAGE APPROXIMATELY 1 INCH FROM F.S.755.00.SDR HEER20190507882Skin · puncturedFORWARD SHELL ASSEMBLY INNER SKIN WAS FOUND TO BE DAMAGED - PUNCTURED UNDER THE EXISTING RT PASSENGER DOOR STRUT INSTALLATION. THE REPAIR DOCUMENTATION WILL BE SUBMITTED FOR FAA APPROVAL. THE FORWARD SHELL ASSEMBLY WILL THEN BE REPAIRED IN ACCORDANCE WITH THSDR SWAA2022030998354Scuff Plate · crackedFWD CARGO DOOR; FWD CORNER THRESHOLD SCUFF PLATE IS CRACKED. / REPLACED DAMAGED THRESHOLD CORNER FROM STOCK ORD#7530028-BHR PER SRM 51-10-02.SDR CA190521029Skin · corroded(CAN) WE HAVE FOUND CORROSION AND BLENDED OUT THE CORROSION ON THE SUBJECT AIRCRAFT AS FOLLOWS CORROSION A: FS559+56 BETWEEN STRG 26RH AND STRG 26LH. CORROSION B: FS559+74 BETWEEN STRG 26RH AND STRG 26LH. CORROSION C: FS559+112 BETWEEN STRG 26RH AND STRG 26LSDR SWAA2022030971669Scuff Plate · crackedFORWARD CARGO BAY FORWARD CORNER SCUFF PLATE CRACKED. / LOCATED & DRILLED NEW FWD CORNER SCUFFPLATE OF FWD CARGO BAY DOOR CUTOUT PN 7530406 PO #710525/1 IAW SRM 51-40-05-0G-0. REFERENCE CUSTOMER CARD #753-140-00-01Y FOR REMOVAL & INSTALLATION OF SCUFF PLATE. 5SDR CALA2019050700707Skin · scratchedMOVE TEAM REPORTS A/C FUSE SKIN SCRATCHED DMG 4 INCH LONG AT BS 368 AT STRINGER S-16L, JUST AFT OF 1LH MED. REF SRM 53-00-01 ALLOWABLE DAMAGE LIMITS FIGURES103 AND 7, THE A REA SKIN THICKNESS IS .071 WITH MAX LIMIT BETWEEN 10 AND 15%. IN ITIAL MEASUREMENT IS ASDR IPXA2019050541765Skin Panel · gougedINSPECTION TYPE:N/A FUSELAGE TAIL SECTION DENT & GOUGE REPAIR AT S-45 BETWEEN FR 83-84. REPAIRED FUSELAGE TAIL SKIN IAW EO A300-5330-71842-C.SDR CALA2019051300001Skin · corrodedBULK CARGO STA 1540 STR 37L AREA INTERIOR SKIN FOUND CORROSION. REPAIRED IAW ECRA 5331-02373PART 1 ITERIM REPAIR AT NRC TJE518820 INSP 156019. REPAIR IS CONSIDERED PERMANENT AS LONG AS REINSPECTION REQUIREMENTS OF PART 2 ARE COMPLIED WITH. ACCOMPLISH THE INSPE
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