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 EE4Y2020090711597Skin · dentedDURING ROUTINE MAINTENANCE AT THE COOPESA MAINTENANCE FACILITY IN SAN JOSE, COSTA RICA (SJO), THE FUSELAGE SKIN BETWEEN STA 498 AND STA 502 AND BETWEEN S-21R AND S-25R WAS FOUND TO HAVE 3 EA. DENTS. REPAIRED PER ENGINEERING AUTHORIZATION Nº 72-2020-179 AND DOCSDR EE4Y2020090711595Skin · dentedDURING MAINTENANCE VISIT, A DENT WAS NOTED ON THE FUSELAGE SKIN AT STA. 345.5, ABOVE STR. 20R. THE DENT WAS OUT OF LIMITS PER 737-400 SRM. THE DAMAGE WAS REPAIRED PER ENGINEERING AUTHORIZATION Nº 20-2020-028 AND DOCUMENTED UNDER JOB: A1J170 NRI 1-32.SDR EE4Y2020090711586Skin · crackedDURING SCHEDULED MAINTENANCE AT COOPESA FACILITY IN SAN JOSE, COSTA RICA (SJO), THE FUSELAGE SKIN BETWEEN STA 827 AND STA 847 AND BETWEEN STGR-1 AND STGR-2L UNDER THE ELT ANTENNA WAS FOUND WITH OIL CANNING AND CRACK DAMAGE. THE DAMAGE WAS REPAIRED PER ENGINEESDR SWIA202053469Skin · chafedLOWER WING PLANK HAS MINOR CHAFING DAMAGE FROM FUSELAGE FAIRING AT AT BOTH LBL 45 AND RBL 45 AT APPROXIMATELY FS 513. C-CHECK RO 10/18/2020. REPAIRED IAW REO. NO MEASUREABLE WEIGHT CHANGES. MAJOR REPAIR TASK CARD & FORM M337 COMPLETED AND ATTACHED. REFER SDR SWAA2020091115145Skin · cracked1 EACH CRACK FOUND FUSELAGE CROWN SKIN FS 767 2 RIGHT OF STRINGER 1R AND 11' AFT FS 767 AND CRACK IS 0.75' LONG. REPAIRED PER EA 20-153-01667 INTERIM REPAIR SEE 943.SDR SWIA2020091152460Skin · damagedTWO DAMAGED AREAS TO FUSELAGE SKIN AFT OF L1 DOOR AT FR21L AND BETWEEN STR 14L AND 15L. FIRST DAMAGE IS A PUNCTURE 16CM LONG WITH A DENT 24CM L X 17CM H X 1.5CM D. SECOND DAMAGE IS A GOUGE 3MM L X 7MM W X 3MM D, REFERENCE CP2180429-1. FILED CLOSED. COMPLIESDR IPXA2020090855878Stringer · corrodedFUSELAGE SKIN CUTOUT FOR STRINGER REPAIRS STA 1430-1445 STRINGER 30. REPAIRED IAW B757-5310-77770-A.SDR SWIA2020090852316Skin · dentedTRANSFER FROM EAML 484780: FOUND 3 DENTS TO MEASURE: NR 1: 2.25" LONG BY .085" DEEP. NR 2 IS 1.125" LONG BY .053" DEEP. NR 3 1.25" LONG BY .046" DEEP FROM FR 21 TO FR 22 AT STRINGER 15L. THIS HAS BEEN DETERMINED TO BE MAJOR REPAIR, FORM M-337 WILL BE REQUIREDSDR SWAA2021041314397Skin · dentedTRANSFERRED FROM CARD V262886=FUSELAGE EXTERNAL SKIN DENT AT STA. 1006 + 3.5'; 2.5' BELOW STR. 16R HAS ADDITIONAL GOUGE DAMAGE NOTED IN DENTED AREA. / FUSELAGE EXTERNAL SKIN DENT AT BS 1006+3.5' BELOW STRINGER 16R REPAIRED IAW EA 20-153-01763 REV IR AND ATS ERSDR SWAA2020092814393Skin · corrodedCORROSION ON EXTERNAL FUSELAGE SKIN UNDER ADF NR 1 ANTENNA BS678-BS707 S-1 TO S-2R WL306. REPAIRED CORROSION ON FUSELAGE SKIN UNDER ADF NR 1 ANTENNA AT BS 678 - BS 707 S-1 TO S-2R WL 306, PER ER 20-03231 REV IR ON SWA EA 20-153-01795 REV IR.SDR DALA2020090903015Skin · corrodedSHIP 3165, CORROSION INTERNAL STRUCTURE INTERNAL SKIN LOCATED BETWEEN FR30 TO FR34 AND BETWEEN STRG 41L TO STRG 41R IN FWD CARGO COMPARTMENT. CORRECTVE ACTION: PERFORMED PERMANENT REPAIR, AS PER ER/A NR 587500-14 REVISION ORIGINAL AND PRI NR 587500-14 REVISIOSDR YENA2020090800450Skin · damagedDURING HEAVY MAINTENANCE, PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN BETWEEN FR 96 TO FR 97 AT STGR 23R LOWER FUSELAGE. PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN BETWEEN FR96 TO FR97 AT LEVEL STGR 23R LOWER FUSELAGE, IAW E190 SRM 53-30-01, REPAIR 63, ITEM SDR YENA2020090800449Skin · dentedDURING HEAVY MAINTENANCE DENT EXTERNAL SKIN FR 96 TO FR 97 AT LEVEL STR23L LOWER FUSELAGE. PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN BETWEEN FR96 TO FR97 AT LEVEL STGR 23L LOWER FUSELAGE, IAW E190 SRM 53-30-01, REPAIR 63, ITEM 5. DETAILED VISUAL INSPECTIOSDR DALA2020090752969Skin · damagedCORROSION LEVEL: 2 FOUND DURING INITIAL INSPECTIO ON INTERNAL FUSELAGE SKIN FROM FS 1340 TO 1360 BTW S-29L AND S-30 (AFT ATG ANTENNA)(SM). REPLACED FILLER(INTERNAL DOUBLER),EXTERNAL DOUBLER AND STIFFENER PER SRM.SDR SWIA202053478Skin · dentedADM NR N922EV-6861. THE DENT IS ON THE LT SIDE OF THE FUSELAGE AT FS 262.00 AND APPROXIMATELY 35 INCHES DOWN FROM WL 73.50. THE DAMAGE IS A DENT WITH A LENGTH OF 0.975 INCHES AND A WIDTH OF 0.446 INCHES. THE DEPTH OF THE DENT IS 0.012 INCHES. PLOT, MAP, ANSDR DALA2022122008265Skin · dentedFOUND DENT LEFT SIDE 25 INCHES AFT OF AFT LEFT PASSENGER SERVICE DOOR 2.5" WIDE 2.5" TALL .075 DEEP BETWEEN FRAME FR 79 AND 78 BELOW STGR 19L. PER ENGINEERS REQUEST PERFORMED HFEC ON DENT PER ANDTP TASK BD500-A-J51-10-05-00AAA-353A-A NO INDICATIONS NOTED (QC20SDR SWIA202053398Skin · corrodedCORROSION ON OUTER SIDE OF SKIN IN MULTIPLE AREAS FS 597.00 TO FS 693.00, ALONG THE ATTACH POINT OF THE WING TO BODY FAIRINGS, MARKED. C-CHECK RO 10/16/2020. REMOVED CORROSION ON OUTER SIDE OF SKIN IN MULTIPLE AREAS FROM FS 597-FS 693 FROM 4 EA SKIN COMPONENSDR SWAA2020101213496Bear Strap · crackedCRACK FORWARD GALLEY DOOR (RI) BEAR STRAP INTERNAL ARE LOCATED AT BS 291.5 TO BS 294.5 BETWEEN STR 8R AND STR 9R AT PASSENGER CABIN. REPAIRED FORWARD BELLY DOOR INTERNAL AREA AT BS 291.5 AND BETWEEN STR 7R AND STR 9R, IAW EA N. 20-153-01918 REVISION IR AND EASDR SWAA2021042713498Skin · dentedDENT ON FUSELAGE SKIN BS 251+5; 5' ABOVE STR 17L (EXISTING DENT T874699 WITH EVIDENCE OF FURTHER DAMAGE) / CUT OUT DAMAGE AREA AND INSTALLED REPAIR AT FUSELAGE SKIN STA. 251.6 TO 259.5 AND BETWEEN STR15L AND STR.18L REF. AAR RES-WI # 2016200-8 REV IR AND EA. NSDR SWIA202053085Skin · corrodedBELLY SKIN FS 559+96 BETWEEN STGRS 23R/24R AS VIEWED FROM OUTSIDE AND BELOW WASTE DRAIN VALVE ASSEMBLY RIVETS/SKIN CORRODED, AS MARKED. C-CHECK RO 10/4/2020. REPAIRED BELLY SKIN FS 559+96 BETWEEN STGRS 23R/24R AS VIEWED FROM OUTSIDE AND BELOW WASTE DRAIN VALSDR SWIA202053084Skin · corrodedBELLY SKIN BETWEEN FS 559+80/559+112 AND STGRS 25L/26R SKIN/RIVETS CORRODED, AS MARKED. VISIBLE FROM OUTSIDE/BOTTOM. C-CHECK RO 10/4/2020. REPAIRED BELLY SKIN BETWEEN FS 559+80/559+112 AND STGRS 25L/26R SKIN/RIVETS CORROSION, REF REO. LEAK CHECK GOOD.SDR SWAA2020091514951Skin · dentedREF DEFECT NO 0823623 FUSELAGE SKIN HAS A DENT WITH SCRATCH AT STA 1016+5 AND BELOW STR 14L. EVALUATED DENT ON FUSELAGE SKIN AT STA 1016 + 5' AND BELOW STR 1RL, DENT MEASURES (L: 2.5' / W: 1.8 / Y: .096 / W/Y: 18.75) OUT OF LIMITS, IAW SRM 53-00-01-1A-1. HFESDR MASA20200907061Skin · puncturedPUNCTURE IN THE FUSELAGE AFT OF THE MAIN PAX DOOR BETWEEN FR 21-22 AND STR 14L-15L.SDR UIEA2020090431924Skin · corrodedSTA 1730 STR 43L FUSELAGE SKIN FOUND 1EA CORROSION INDICATION APPROX 1.75" X 1. FUS-STA 1720-1740 STR42L-44L, FUSELAGE SKIN DAMAGED AREAS REPAIRED IAW SRM 53-00-01-2R-1 REPAIR 1 DETAIL 1. THIS REPAIR IS A PERMANENT REPAIR AND CATEGORY B REPAIR.SDR MK1Y20200831001Skin · dentedFOUND DENT DAMAGE ON THE BOTTOM SKIN AT STA 1906-1915 BELOW RT LONGERON, APPROX 10.5" FROM APU DOOR CUTOUT.SDR SWAA2020090313013Doubler · crackedEXTERNAL GROUND POWER DOOR AFT LATCH RUBBING BLOCK DOUBLER HAS 2 EA CRACKS AT LOWER RIVET. MOD / INSTALLED TIME LIMITED REPAIR PER EA 20-153-01603. SEE ATTACHED SA-M 326 FOR WORK IN PROGRESS DETAILS PERMANENT ACTION REQUIRED: PERMANENT REPAIR OF THIS ITEM WILSDR SWIA202053210Skin · corrodedLOWER FUSELAGE SKIN AT TCAS ANTENNA LOCATION CORRODED AROUND HOLE CUT-OUT. C-CHECK RO 10/9/2020. BLENDED OUT CORROSION AND EVALUATED LOWER FUSELAGE SKIN AT TCAS ANTENNA LOCATION HOLD CUT-OUT AND FOUND TO BE OUT OF LIMITS, REF CRJ-900 SRM AND CRJ-900. REPAIRSDR SIMA2020083129005Skin · deformedSKIN DEFORMATION LOCATED AT FRAME 23 STRINGERS 16R ? 17R.-C/A-SKIN DEFORMATION LOCATED AT FRAME 23 STRINGERS 16R ? 17R. FOUND STRINGER 17R AT FR 23 TO BE BENT. PERFORMED STRINGER REPAIR IAW EMB 145 SRM 53-00-03-RE.SDR SWIA202053302Skin · dentedADM N494CA-6376 SKIN DEVIATION, RIGHT SIDE, AFT OF RADOME BETWEEN STRINGERS 15-16 AT STA 173. EVALUATION AND REPAIR AS REQUIRED. C-CHECK RO 10/13/2020. DENT NR 1 ON RT SKIN AT APPROXIMATELY FS 170.5 AND WL 86.5 MEASURES .70" WIDTH BY 2.0" LENGTH AND .010" DSDR SWIA202053044Skin · chafedCENTER WING LOWER PLANK CHAFED UNDER PANEL 193AB AT APPROXIMATE RBL 45. C-CHECK RO 10/4/2020. REPAIRED CHAFING ON CENTER WING LOWER PLANK UNDER PANEL 193AB AT APPROXIMATE RBL 45, IAW REO AND CRJ200 SRM.SDR SWIA202053043Skin · corrodedCORROSION ON EXTERNAL FUSELAGE SKIN AT NUTPLATE LOCATIONS FOR PANEL 192BB BETWEEN STR 20L AND STR 27. C-CHECK RO 10/4/2020. REMOVED CORRSION ON EXT FUSELAGE SKIN AT NUTPLATE LOCATION FOR PANEL 191BB STGR 27 AND 20L. REMAINING MATERIAL THICKNESS FOUND TO BE SDR A6WA202009237294Skin · dentedDENT AT FS 679.8 & S22R-1 THAT MEASURES .8" L X .8" W X .006" D WITH A W/D=133 AND IS LESS THAN 1" FROM S22R. DENT IS NOT WITHIN ALLOWABLE LIMITS, REF CRJ 200 SRM 53-00-31 FIG 103 SH 3 AND SH 4. AIRCRAFT REMOVED FROM SERVICE. CUT DAMAGE AREA OUT 1.5" X 1.2"SDR A6WA202009217291Skin · dentedDENT AT FS 660.9 & S22R-2", DENT MEASURED AT .5" L X .5" W X .005" D WITH A W/D=100 ADDITIONAL DENT IDENTIFIED ON AERSALE W/O 002862 CARD NO 453-900-501-N0002 FOUND AT FS 657.80 & S22R+2" THAT MEASURES .7"L X .7"W X .009"D WITH A W/D=77. BOTH DENTS ARE NOT WISDR IPXA2020091436174Doubler · wornINSPECTION TYPE: 2C TAIL CONE INTERNAL DOUBLER AT FWD LOWER END HAS DEEP CHAFE WEAR FROM LBL-40 TO RBL-40 Y=2163. REPAIRED CHAFED INNER DOUBLER AND REPLACED 2 EA SPLICE ANGLES ON TAIL CONE AT Y=2163 BETWEEN LBL-40 AND RBL-40, IAW EA 011-5350-01-A8544 AND EO MSDR FDEA202008282050Skin · gougedFUSELAGE, FWD LOWER FUSELAGE SKIN AT STATION 773 STRINGER 36 LT FOUND WITH EXISTING BLEND OUT WITH GOUGE MARK. FWD LOWER FUSELAGE SKIN AT STATION 773 STRINGER 36 LT EXISTING BLEND OUT WITH GOUGE MARK, EVALUATED AND FOUND EXCEED LIMIT PER B767 SRM 53-00-01-1SDR KCSA202008281139Skin · crackedCRACK IN SKIN ON LT OF EMPENNAGE APPROXIMATELY STA 2656SDR Y2PA2020090220019Skin · crackedDISCREPANCY: DURING C-CHECK AT KDHN, FOUND ON THE UPPER MAIN CARGO DOOR FS313L TO 332L ABOVE WINDOW FRAME, SKIN IS CRACKED ALONG RIVET ROW. CORRECTIVE ACTION: COMMERCIAL JET STOP DRILLED CRACK AND VERIFIED CRACK CONTAINMENT VIA NDT. FABRICATED, DRILLED, DEBURSDR DALA2020083182889Skin · crackedWHILE ACCOMPLISHING THE SKIN AND BEARSTRAP INSPECTION, BEARSTRAP WAS FOUND CRACKED AT L1 DOOR STA 338. REPAIRED PER ERA 587520-14AD.SDR IPXA2020082879550Skin · dentedINSPECTION TYPE:SEG NEW DENT DISCOVERED AT STA 525 BELLOW STRINGER 27L ON FUSELAGE EXTERIOR SKIN. MARKED IN RED, REPAIRED IAW B757-200SRM 53-00-01-2R-29 ZONE A.SDR SWAA2021081612935Skin · corroded***CORROSION*** ON EXTERNAL FUSELAGE SKIN BS677 - BS707 S-1 - TO S-2R WL306. MARKED / REPAIRED EXTERNAL FUSELAGE SKIN BS 677 - BS 707 STR S-1 TO S-2R WL 306 IAW SWA EA 20-153-01779 REV IR AND ATS ER 20-03207 REV IRSDR SWIA202052876Skin · dentedRT FUSELAGE EXTERIOR DENT FOUND JUST AFT OF FS 280, APPROX STGR 26, FLAGGED. C-CHECK RO 9/27/2020. REPAIRED RT FUSELAGE EXTERIOR DENT FOUND JUST AFT OF FS 280, APPROX STGR 2, REF BOMBARDIER MHIRJ REO.SDR FDEA202008262032Skin · damagedFUSELAGE, FORWARD LOWER FUSELAGE SKIN AT STATION 478, STRINGER 35 LEFT FOUND WITH EXISTING BLEND OUT. FWD LOWER FUSELAGE SKIN AT STATION 478 STRINGER 35 LEFT EXISTING BLEND OUT AREA. REPAIRED AS PER E.A NR: H-5330-T0356108 PART 1 TITLE: FUSELAGE-PLATES & SKISDR FDEA202008262030Skin · damagedFUSELAGE, FWD LOWER FUSELAGE AT STATION 325, STRINGER 34 LT FOUND WITH EXISTING BLENDOUT. FWD LOWER FUSELAGE SKIN AT STATION 325 STRINGER 34 LT EXISTING BLENDOUT EXCEED LIMIT AS PER B767 SRM 53-00-01-1A ALLOWABLE DAMAGE 1 FIGURE 101 DETAIL II. DAMAGED SKINSDR FDEA202008262027Skin · damagedFUSELAGE - RIGHT HAND LOWER FUSELAGE AT STATION 390, BETWEEN STRINGER 29 RIGHT TO 30 RIGHT FOUND WITH EXISTING BLEND OUT. RIGHT HAND LOWER FUSELAGE SKIN AT STATION 390 BETWEEN STRINGER 29 RIGHT - STRINGER 30 RIGHT EXISTING BLEND OUT EXCEED LIMIT PER B767 SSDR SWAA2020082711794Doubler · damagedEXTERNAL GROUND POWER RECEPTICAL DOOR SURROUND DOUBLER DAMAGED. REPAIRED PER SRM 53-10-15-2R-4. SEE ATTACHED SAM 326 FOR WORK IN PROGRESS DETAILSSDR SWIA202053260Skin · corrodedFUSELAGE EXTERNAL SKIN UNDER FWD WING TO FUSELAGE FAIRINGS THE SKIN IS CORRODED FROM FS 409.00+64 TO FS 409.00+96 BETWEEN STRG 26R TO 18L. C-CHECK RO 10/13/2020. COMPLIED WITH PERMANENT REPAIR TO FUESLAGE EXTERNAL SKIN UNDER FWD WING TO FUSELAGE FAIRINGS FROSDR SWIA202053259Skin · corrodedFUSELAGE EXTERNAL SKIN UNDER THE FWD WING TO FUSELAGE FAIRINGS THE SKIN IS CORRODED BETWEEN FS 409.00+64 TO FS 409.00+96 AND BETWEEN STRG 18R TO 25R. C-CHECK RO 10/13/2020. COMPLIED WITH PERMANENT REPAIR, IAW MHIRJ REO AT RIGHT HAND FUSELAGE LOWER SKIN COMMOSDR SWIA202053039Skin · crackedLT SIDE FUSELAGE SKIN HAS SUSPECTED CRACK AT AFT LATCH LOWER CORNER FOR PANEL 211AL AND LOWER EDGE OF SKIN BELOW LATCH. C-CHECK RO 10/4/2020. REMOVED AND REPLACED LT SIDE FUSELAGE SKIN PANEL 211AL SURROUND FRAME WITH NEW SERVICEABLE P/N 600-33052-145, REF MHSDR HNAA2020092400268Skin · damagedMULTIPLE RIVETS ON FR 77 BETWEEN STR 3L-9L HAVE POSSIBLE CRACKS (6 TOTAL). PERFORMED DYE PENETRANT INSPECTION, IAW EASI NDTM 3. RELEVANT INDICATION NOTED SKIN CRACK ENDS, MARKED, RADIOMETER EASI 0452. COMPLETE: CUTOUT DAMAGED AREA ON FR 77 BETWEEN STR. 4L-9SDR HNAA2020092400265Skin · damagedMULTIPLE RIVETS ON FR 78 BETWEEN STR 5R-7R HAVE POSSIBLE CRACKS (3 TOTAL). PERFORMED DYE PENETRANT INSPECTION, IAW EASI NDTM 1. RELEVANT INDICATION NOTED SKIN CRACK ENDS MARKED RADIOMETER EASI 0452. COMPLETE: CUTOUT DAMAGED AREA ON FR 78 BETWEEN STR 5R-6R.
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