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 SWIA2020072751423Doubler · chafedAPPROX. F.S 969 LOWER FUSELAGE DOUBLER HAS TWO CHAFES AT STGR 27. PERFORMED DOUBLER REPAIR AT APPROX. F.S 969 STRINGER 27 REF. REO . COMPLIED WITH TASK CARD. PRESSURE CHECK GOOD.SDR SWAA2020070792668Skin · corrodedCORROSION ON EXTERNAL FUSELAGE SKIN AT BS 907 - 1006, WL 306, LBL 10 - RBL 10. REPAIRED THE SKIN IAW ER 20-02767, REV IR, AND EA 20-153-00965, REV IR.SDR ASOA202006147038Skin · corrodedTYS A/C IS HERE FOR A REPAIR OF A DOUBLER AT FRAME 4 AND STRINGERS 9L TO 11L DUE TO MORE DAMAGE FOUND. MAINTENANCE CUT OUT THE DAMAGE AREAS, FABRICATED FILLERS AND A NEW DOUBLER, INSTALLED REPAIR PARTS IAW ETD 2020-145-019642. ALLODINED,PRIMED AND PAINTED IAW SDR SWIA2020072251371Skin · dentedDENT IN AIRCRAFT SKIN BS 603, STR 18L. REPAIRED THE DENT WITH GOUGE IAW REO.SDR YENA2020061820367Skin · nickedDURING HEAVY MAINTENANCE, NICK EXTERNAL SKIN BTW FR25-FR26 AT STR 42L-43L; (REF ARM W/O 2020 112/1 N/R 2020-187902). PERFORMED PERMANENT MAJOR REPAIR IAW A320 SRM 53-00-11-300-029 FIG 001 SHEET 1 AND THIS REPAIR IS CLASSIFIED AS CATEGORY B WITH INSPECTION THRESDR AALA202006159023Doubler · corrodedAIRCRAFT IN RON VISIT: LOWER AFT FUSELAGE DOUBLER PLATE CORRODED NEAR AFT CARGO DOOR SELECTOR VALVE. REMOVED AND REPLACED DOUBLER, FILLER AND U-CHANNEL IAW GOGO DRAWING P15511, P18146 AND SRM 51-42-11.SDR DALA2020061202468Skin · corrodedCORROSION DAMAGE COMMON TO THE FUSELAGE SKIN UNDERLYING THE NR 2 TFTS AIRPHONE ANTENNA AT STA 500A+12 AND BL 0. PERFORMED AND COMPLIED WITH ALL INSTRUCTION STEPS IAW PRI ERA 586973-14 REV-3.SDR SWIA2020072951492Skin · dentedPOSSIBLE DENTS AND DISTORTIONS ON EXTERNAL SKIN JUST AFT OF PAX DOOR APPROX. FROM FS364.00 AND FS394.00 BET STGR 23L TO STGR 17R (C-CHECK) RO 7/25/2020 --DENTS ARE "OUT OF LIMITS" DUE TO SUBSEQUENT LOCATION OVER STR21L & STR22L, NO DAMAGE ALLOWED REF CRJ7SDR SWIA2020072751417Skin · scratched* R/H SIDE EXTERNAL FUSELAGE ARE VARIOUS SMALL SCRATCHES JUST AFT AND BELOW A/C SERVICE CONNECTION FS 1031.0 (C-CHECK) RO 7/23/2020 BLENDED VARIOUS SCRATCHES ON RH SIDE EXTERNAL FUSELAGE SKIN JUST AFT AND BELOW A/C CONNECTION AT FS 1031.0. REF CRJ 700 SRMSDR SWAA2020070992109Web · corrodedCORROSION ON SUBTHRESHOLD WEB AT FWD CARGO BAY BS440 - BS493 RBL28 WL156. REMOVED AND INSTALLED NEW SUBTHRESHOLD WEB AT FWD CARGO BAY BS 440-BS 493 RBL 28 WL 156 ITEM 7530597 IAW SRM 53-30-15-01-1; SRM 53-30-15-1A-1; SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; DWG SDR CALA2020062051016Skin · dentedDENT WITH SCRAPED PAINT REPORTED AND CONFIRMED APPROX.3 FEET FWD OF MAIN CABIN DOOR OPENING AND LOCATED APPROX. 6 FEET ABOVE REF L/P 7961636 AND EC/RA #5330-06441. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLER PER EC/RA#5331-02679 ,PART 1. INITIATED DIP TO "ACCOSDR AALA2020061529008Doubler · corrodedAIRCRAFT IN MOD VISIT: DURING FUSELAGE INSPECTION INSPECTION FOUND THE AFT LOWER GOGO ANTENNA BASE DOUBLER WITH CORROSION. CORROSION WAS REMOVED AND REMAINING THICKNESS WAS OUT-OF-LIMITS. THE GOGO ANTENNA DOUBLER WAS REPLACED.***SUPPLEMENTAL ACTION SECTION 3 ASDR KCSA202006111080Skin · corrodedLOWER FUSELAGE SKIN, BS 1740 CORRODED.SDR SWIA2020072751416Skin · dentedDENT ON FUSELAGE SKIN FWD OF FS 265.00 BETWEEN STGR 24R - 25R (C-CHECK) RO 7/23/2020 REPAIRED FUSELAGE SKIN DENT FWD OF F.S 265 BETWEEN STGR 24R - 25R REF. MHIRJ REO. PRESSURE CHECK GOOD. COMPLIED WITH TASK CARD.SDR IPXA2020062977045Skin · corrodedINSPECTION TYPE:2CCENTER WING BOX UPPER SKIN AT STRINGER 9 & XCW -101 HAS CORROSION.REPAIRED CENTER WING BOX UPPER SKIN CORROSION AT STRINGER 9 & XCW -101 IAW VT-SAA EA 011-5730-01-A8360 REV. IR AND UPS EO MD11-5730-76994-A. (MAJOR)SDR IPXA2020062967017Skin · corrodedINSPECTION TYPE:2CCENTER WING BOX UPPER SKIN AT STRINGER 3 AND XCW 101 HAS CORROSION.REPAIRED CENTER WING BOX UPPER SKIN CORROSION AT STRINGER 3 AND XCW 101 IAW VT-SAA EA 011-5730-01-A8361 REV IR AND UPS EO MD11-5730-77002-A. (MINOR)SDR MASA20200610037Skin · dentedDURING A C-CHECK, A GOUGE WAS FOUND ON THE LOWER SKIN BS 913+4 REPAIRED I/A/W REO 670-53-00-290.SDR MASA20200610036Skin · dentedDURING A C-CHECK, THE FUSELAGE SKIN BS 410 STRINGER 20L WAS FOUND DENTED. REPAIRED WITH NON FLUSH EXTERNAL LAP JOINT.SDR MASA20200610035Doubler · corroded(C-CHECK) REMOVED AND REPLACED TCAS ANTENNA DOUBLER FS295-FS310 AT STGR 27SDR SWIA2020080751679Skin · corrodedEVALUATE EVIDENCE OF CORROSION ON EXTERIOR FUSELAGE BETWEEN FS 980 AND FS 988 AND BETWEEN STGR 26L AND STGR 26R. REPAIRED FUSELAGE SKIN BETWEEB FS 977 - 985 BETWEEN STGRS 26L - 26R, BY RERPLACING THE EXISTING DOUBLERS WITH NEW IAW REO. ALL CHECKED GOOD.SDR SWIA2020072251364Skin · dented6 EA. DENT LOCATED @ APPROX. FS605 BELOW WL 783.50 (MARKED). PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PRACTICES. ALL DENTS REPAIRED WITHIN ALLOWABLE LIMITS REF REO, ALL STEPS COMPLIED WITHSDR SWIA2020071451334Skin · corrodedEXTERNAL SKIN IS CORRODED AT APPROX FS559+96-559+112, STR26L-26R. (C-CHECK) RO 7/10/2020 BLENDED CORROSION, REF SRM 51-21-06. FOUND TO BE OUT OF LIMITS. NO ALLOWABLE DAMAGE IN DISCREPANT AREA. SUBMITTED TO ENGINEERING AND RECIEVED DISPOSITION OF REO. COMPSDR SWIA2020071451333Skin · corrodedEXTERNAL SKIN IS CORRODED AT APPROX FS559+44, STR25L-25R. (C-CHECK) RO 7/10/2020 BLENDED CORROSION ON EXTERNAL SKIN AT FS 559+44 BETWEEN STR 25L-25R REF SRM. BLENDED AREA FOUND TO BE OUT OF LIMITS REF SRM. REPAIRED EXTERNAL SKIN AT FS 559+44 BETWEEN STR 25LSDR SWIA2020071451296Skin · corrodedEXTERNAL SKIN IS CORRODED AT APPROX FS559+34, STR26L. (C-CHECK) RO 7/10/2020 BLENDED CORROSION, REF SRM 51-21-06. FOUND REMAINING MATERIAL TO BE OUT OF LIMITS, REF SRM. SUBMITTED TO ENGINEERING, WHO APPROVED A DISPOSTION FOR BLENDED CORROSION DAMAGE TO FUSESDR SWAA2020062991198Skin · corrodedCORROSION FOUND ON THE EXTERNAL SKIN AROUND FASTENER HEADS, BS 990-1001, STRINGER 2L. REPAIRED THE SKIN IAW EA 20-153-00844, REV IR, AND ER 20-02425, REV IR.SDR SWAA2020062991199Skin · corrodedCORROSION FOUND ON THE EXTERNAL SKIN AROUND FASTENER HEADS, BS 990 - 998, STRINGER 2R. REPAIRED SKIN IAW EA 20-153-00844, REV IR, AND ER 20-02725, REV IR.SDR MASA20200608033Skin · dented(C-CHECK)FUSELAGE SKIN LH STA 661+90.00 AND FS661+98.40 BETWEEN STGR 10L AND STGR 11L HAS DENT/BLEND.SDR FDEA202006081152Skin · dentedFUSELAGE SKIN AT STA 1581, STRINGER 49R HAS DENT DAMAGE. REPAIRED FUSELAGE SKIN (DOUBLER REPAIR) USING SRM 53-20-00 AS A REFERENCE.SDR FDEA2020062571140Skin · crackedDURING HIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT ON EXTERNAL SURFACE OF FUSELAGE WITHIN A 2 INCH RADIUS OF ALL HOLES COMMON TO THE RIGHT HAND UNDERWING LONGERON AND FUSELAGE SKIN, FOUND 03 EACH CRACKS ON THE SKIN APPROXIMATELY 1.5Ï¿½ AT STATION 10SDR FDEA2020062571139Skin · crackedDURING HIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT ON EXTERNAL SURFACE OF FUSELAGE WITHIN A 2 INCH RADIUS OF ALL HOLES COMMON TO THE LEFT HAND UNDERWING LONGERON AND FUSELAGE SKIN, FOUND 03 EACH CRACKS ON THE SKIN APPROXIMATELY 0.5Ï¿½ AT STATION 1SDR FDEA2020060871140Skin · crackedDURING HIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT ON EXTERNAL SURFACE OF FUSELAGE WITHIN A 2 INCH RADIUS OF ALL HOLES COMMON TO THE RIGHT HAND UNDERWING LONGERON AND FUSELAGE SKIN, FOUND 03 EACH CRACKS ON THE SKIN APPROXIMATELY 1.5 AT STATION 1027 STRISDR FDEA2020060871139Skin · crackedDURING HIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT ON EXTERNAL SURFACE OF FUSELAGE WITHIN A 2 INCH RADIUS OF ALL HOLES COMMON TO THE LEFT HAND UNDERWING LONGERON AND FUSELAGE SKIN. FOUND 03 EACH CRACKS ON THE SKIN APPROXIMATELY 0.5 AT STATION 1027 STRINSDR SWAA2020061090389Skin · damagedFUSELAGE SKIN DAMAGE AT BS 794.6 ABOVE STR 24L FOUND TO BE OUT OF LIMITS. REPAIRED SKIN PER SRM 53-00-01-2R-3 REPAIR 3.SDR UIEA2020061091252Skin · corrodedCORROSION FOUND ON THE INNER FUSELAGE SKIN, AFT CARGO COMPARTMENT BS 1680, STRINGERS 50L TO 51R. REPAIRED THE DAMAGED AREA IAW EI T2020A53M-1426, REV 3.SDR UIEA2020060101254Skin · crackedA CRACK WAS FOUND ON THE FUSELAGE SKIN UNDER THE DRAG SPLICE FITTING NEAR BS 980 STRINGER 38R. REPAIRED THE DAMAGED AREA IAW SRM 53-20-01-2R-2, REPAIR 2, REV 88, AND EI T2020A53M-1510, REV 2, AND EI T2020A53M-1419, REV 1, ATTACHED TO W/O 4641182.SDR UIEA2020061091255Skin · crackedCRACK ON SKIN PANEL UNDER THE DRAG SPLICE FITTING AT STA 980 S-38L. REPAIRED DAMAGED AREA IAW SRM 53-20-01-2R-2, REPAIR 2 REV 88, EI T2020A51M-1482 REV 1, AND T2020A53M-1419 REV 1. CONDITION CHECKED NORMAL.SDR UIEA2020061001264Skin · corrodedCORROSION FOUND ON THE UPPER SURFACE OF THE FUSELAGE SKIN PANEL AT BS 1720, BL 0. REPAIRED THE DAMAGED AREA IAW EI T2020A53M-1455, REV 2.SDR DALA2022032802033None · none(LOG 1564168) DURING INSPECTION FOUND SKIN DAMAGE BELOW L-1 DOOR AT FS 314 AND STR 19L. REMOVE EXISTING FASTENERS AND CUT OUT DAMAGE FABRICATED DRILLED DEBURRED CHEM COATED AND PRIMED. INSTALLED REPAIR AND FILLET SEALED EDGES. CATEGORY B REPAIR INSP REQUIREMENSDR IPXA2020062656972Cap · crackedINSPECTION TYPE:2C RT UNDER WING CANTED PANEL CAP IS CRACKED AT STA 1236.8 AND Z= -100. REPAIRED CRACKED RT UNDER WING CANTED PANEL CAP AT STA 1236.8 AND Z= -100 IAW EO MD11-5310-76799-A. (MAJOR)SDR IPXA2020061256417Strap · crackedINSPECTION TYPE:C11 CRACK ON FUSELAGE SKIN AND CHORD STRAP NEAR STA 1725.5. REPAIR IAW SRID:4-4801590830, EO B767-5330-76807-A AND EO B767-5330-24301-F.SDR IPXA2020061156416Skin · crackedINSPECTION TYPE:C11 CRACK ON FUSELAGE SKIN AND CHORD STRAP NEAR STA 1725.5. REPAIR IAW SRID:4-4801590830, EO B767-5330-76807-A AND UPS EO B767-5330-24301-F.SDR DALA2023053104374Unknown · unknownSHIP 6705 REPAIR TO FUSELAGE SKIN AT STA 320 AND S-18R REQUIRES SECTION IV REPETITIVE C-CHECK INTERNAL AND EXTERNAL DVI INSPECTIONS. THE REPAIR IS ACCOMPLISHED PER ERA 380491-14. CORRECTIVE ACTION: REF ERA 380491-14. (1563806)SDR SWAA2020061892094Skin · dentedHAS A DENT EXTERNAL SKIN LOC. BS 259.5 TO BS 268.25 AND BETWEEN S-16L TO S-17L AT UPPER FUSELAGE / REPAIRED FUSELAGE SKIN BTW BSTA 259.5 AND BSTA 277 S-15L AND S-18L IAW EA #20-153-00758 REV IR AND EA #53-0487-20 REV.0SDR SWAA2021081689548Doubler · crackedPOWER ACCESS ON FUSELAGE BELOW LOWER HINGE CRACKED / REMOVED AND INSTALLED NEW INTERNAL DOUBLER AT EXTERNAL POWER ON FUSELAGE STA 243.70 TO STA 219.80 WL 180.0 TO WL 190.0; REF B737-700 SRM 51-42-02-0G-0; DRAWING NO 141A0640 SRM 53-10-15-1R-5 REPAIR 5; AMM 24-SDR SWAA2020062389395Skin · corrodedUPPER FUSELAGE SKIN EXTERIOR HAS AREAS OF CORROSION AROUND FASTENERS AND BETWEEN BAYS APPROXIMATELY BS 887- BS 1006 STR 3L TO STR 3R. CORROSION ON UPPER FUSELAGE EXTERIOR SKIN AROUND FASTENERS AND BETWEEN BAY APPROXIMATELY BS 887-1006 STR 3L TO STR 3R REPAIRSDR SWAA2020062293576Skin · dentedFUSELAGE SKIN HAS A DENT AT BS 312+2'; 2' BELOW S-2L. DENT MEASURES AT L=1.1'; W=0.9'; Y=.015'; W/Y=60. FUSELAGE SKIN DENT AT BS 312+2' BELOW STR 2L WAS REPAIRED IAW EA 20-153-00851 REV IR DATED 06/19/2020 & ATS ER 20-02734 REV IR DATED 06/19/2020.SDR 2A6D20200603001Deck Plate · elongatedHAS AN ELONGATED HOLE ON THE RT SIDE OF THE TRANSMISSION DECK THAT IS UTILIZED IN THE AFT AC EVAPORATOR PN EC130-6204-2 INSTALLATION DWG EC130-622 AS THE MOST INBOARD AFT HOLE UTILIZING AN AN3-4A BOLT. AT THE HOLES WIDEST POINT IT MEASURES AT .35 BY .26. THESDR SWIA2020072751414Skin · dentedRH SIDE FUSELAGE BETWEEN FS 985 AND FS1000 IN BETWEEN STGR12 AND 13 HAS A SCRATCH/GOUGE MEASURING 6 IN X 1.3 IN AND A MAX DEPTH OF .007 IN. COMPLIED WITH TEMPORARY REPAIR PER REO 670-53-61-1475 REV A. PERMANENT REPAIR DUE WITHIN 6700 FH FROM ORIGINAL ISSUE OF SDR IPXA2020070357261Skin · corrodedINSPECTION TYPE:3C RT AFT FUSELAGE SKIN BETWEEN STA 1986 - 2164 LONGERON 33R TO LONGERON 35R BETWEEN HORIZONTAL STAB FAIRING HAS CORROSION. REPAIRED CORRODED SKIN ON AFT FUSELAGE BETWEEN STA 2140 - 2164 LONG 33R AND LONG 35R IAW SRM 53-70-01 REPAIR 3 FIG 201.SDR KCSA202006021077Doubler · corrodedCORROSION ON POTABLE WATER OVER FLOW VALVE DOUBLER.
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