JASC 5730

Service difficulty reports · 27,262

Reports filed under 5730 · Wing, 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 = '5730'
  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.

SDR SWIA2019050345821Skin · damagedRT WING PLANK MOST AFT FASTENER HOLE ON END OF STRAP OVERSIZED. (C-CHECK) RO: 05/02/2019 COMPLIED WITH REPAIR OF RT WING PLANK MOST AFT FASTENER HOLE ON END OF STRAP OVERSIZED IAW REO.Apr 18, 2019 · N953SW · Cndair CL6002B19SDR DALA2019042402626Skin · damagedRH LOWER WING SKIN STRINGER L-6.5 FOUND FASTENER CODE B LOCATION NO.2 HOLE DIAMETER:0.3920" GREATER THAN 0.3185". C/W ERA 576702-14.Apr 18, 2019 · N154DL · Boeing 7673P6SDR DALA2019042292575Skin · crackedDURING NDT INSPECTION, A CRACK WAS FOUND AT FASTENER HOLE NR 3 ON THE LT WING UPPER SKIN, ABOVE PYLON FWD ATTACHMENT AREA. FASTENER HOLE NR 3 WAS REPAIRED IAW ETI-57-19-037 REV. 6, AND ER/A 577350-14 AD REV ORIG.Apr 18, 2019 · N554NW · Boeing 757251SDR FDEA201904267822Spar Cap · crackedRH WING TE REAR SPAR LOWER CAP SILL AT APPROX STA XORS 415 FOUND CRACK CRACKED SILL REMOVED AS PER SRM 51-31-01-0G AND REPLACED SILL AT RIGHT HAND WING TRAILING EDGE REAR SPAR LOWER CAP AT APPROXIMATE XORS 415 AS PER SRM 51-34-01-0G. REPAIR CLASSIFIED AS MApr 17, 2019 · N619FE · Doug MD11FSDR SWAA2022030704047Panel · delaminatedPANEL 521KB CUTOUT CORNERS ARE DELAMINATED / PANEL 521KB CUTOUT CORNERS DELAMINATIONS WERE REPAIRED IAW SRM 51-70-05-2R-6 56144U 04/17/2019.Apr 16, 2019 · N212WN · Boeing 7377H4SDR CA190416009Skin · cracked(CAN) FOUND LOWER HALF OF 62061-04 WING SKIN ASSEMBLY ON THE RIGHT HAND WING (DIMPLED STIFFENER THAT REINFORCES WING WALK AREA) CRACKED AT THE ENDS OF TWO DIMPLED STIFFENERS 7` AFT OF MAIN SPAR ON EITHER SIDE OF RIB P/N 66597-01 (STA 36.22). OWNER HAS REQUESApr 16, 2019 · Piper PA28181SDR FDEA2019041650794Skin · chafedLEFT WING DROOP LEADING EDGE UPPER SKIN OUTBOARD EDGE FOUND CHAFING MARK AT STATION XDLE 329.774 REPAIR CARRY OUT AT LEFT HAND WING DROOP LEADING EDGE UPPER SKIN OUTBOARD EDGE AT XDLE 329.774 AS PER SRM 57-40-01-2R FIGURE 202 REPAIR 15. REPAIR CLASSIFIED Apr 15, 2019 · N619FE · Doug MD11FSDR PCSA201904260014Skin · corrodedLEVEL 3 CORROSION FOUND AT RH WING LOWER SKIN - WS 826 TO WS 835Apr 14, 2019 · N316CM · Boeing 767338SDR R61A201904120452Tip Cap · cracked*** WHILE AIRCRAFT WAS IN FOR HEAVY CHECK *** MAINTENANCE REPORTED A CRACK ON THE FRONT SPAR LOWER AND UPPER SECTION OF THE RT WINGTIP. (CRACK LENGTH: LOWER AREA: 2.3" UPPER AREA: 0.5") MAINTENANCE REMOVED & REPLACED THE RT WINGTIP ASSY IAW AMM 57-30-00 & 57-3Apr 12, 2019 · N443YX · Emb ERJ170200LRSDR R61A201904120451Tip Cap · cracked*** WHILE AIRCRAFT WAS IN FOR HEAVY CHECK *** MAINTENANCE REPORTED A CRACK ON THE FRONT SPAR LOWER SECTION OF THE LT WINGTIP. MAINTENANCE REMOVED & REPLACED THE LT WINGTIP ASSY IAW AMM 57-30-00 & 57-30-25 AIRCRAFT IS CURRENTLY STILL IN HEAVY CHECK.Apr 12, 2019 · N443YX · Emb ERJ170200LRSDR DALA2019041542423Tape · tornRIGHT WING UPPER SURFACE TAPE WORN. SURFACE IS ALSO CORRODED JUST FORWARD OF O/B SPOILER O/B END. NRC 001-0282:5720-2003/001 00081: REPAIRED COMPLIED WITH PER ER/A 576976-14 REV 0. (LP #1027898)Apr 12, 2019 · N980AT · Boeing 717200SDR REXA2019043010549Access Panel · corrodedL/H WING DRY BAY ACCESS PANEL 540BT LANDING HAS CORROSION. REMOVED CORROSION I.A.W. CRJ-200 SRM 51-21-06 AND FOUND TO BE WITHIN LIMITS I.A.W. DRAWING TOLERANCE DWG NO. 601R10042 VIEW P SHEET 2 ( .202" MIN REMAINING- DWG TOLERANCE .195"-.205" ).Apr 11, 2019 · N8918B · Cndair CL6002B19SDR REXA2019043010545Access Panel · corrodedL/H WING DRY BAY ACCESS PANEL 540AT LANDING HAS CORROSION. REMOVED CORROSION I.A.W. CRJ-200 SRM 51-21-06 AND FOUND TO BE WITHIN LIMITS I.A.W. DRAWING TOLERANCE DWG NO. 601R10042 VIEW P SHEET 2 (.204" MIN REMAINING-DWG TOLERANCE ( .195"- .205").Apr 11, 2019 · N8918B · Cndair CL6002B19SDR REXA2019043010544Access Panel · corrodedL/H WING DRY BAY ACCESS PANEL 540CT LANDING HAS CORROSION AND A SCRATCH. REMOVED CORROSION I.A.W. CRJ-200 SRM 51-21-16 AND REMOVED SCRATCH I.A.W. CRJ-200 SRM TR #51-44, FOUND TO BE WITHIN LIMITS I.A.W. BOMBARDIER DRAWING TOLERANCE DWG NO. 601R10042 VIEW R SHApr 11, 2019 · N8918B · Cndair CL6002B19SDR V6NA201904100002Skin · corrodedAT PAINT POST STRIPPING INSPECTION DETERMINED THE BELOW LISTED AREAS WERE CORRODED. CORROSION REMOVED AND DETERMINED BEYOND MANUFACTURES RECOMMENDATION.Apr 10, 2019 · N170LS · Lear 45LEARSDR AALA201904109007Access Panel · damagedAIRCRAFT IN BASE MAINTENANCE: LEFT WING FUEL ACCESS PANEL 540KB HAS ELONGATED FASTENER HOLE. REPLACED FUEL ACCESS PANEL 540KB PER SRM 57-27-11-283-002.Apr 9, 2019 · N172US · Airbus A321211SDR R61A201904080464Skin · cracked*****MAJOR*****WHILE AC WAS IN FOR HEAVY CHECK FOUND LT WING LOWER SKIN LE SUSPECTED CRACK BETWEEN SLATS 3 & 4 APPROX 4 INCHES IB OF RIB 20. MX PERFORMED A TEMP REPAIR OF LT WING LOWER LE SKIN PN 170-01424-003 APPROX 4 INCHES IB OF RIB 20. IAW ETD2019-170-0496Apr 8, 2019 · N650RW · Emb ERJ170100SESDR IPXA201904241380Skin · corrodedINSPECTION TYPE:4CRT WING UPPER SURFACE HAS CORROSION AROUND FASTENER AY XORS 294 & STRINGER 17.ACCOMPLISHED PERMANENT REPAIR OF RT WING UPPER FWD SKIN CORROSION AT STA XORS =295.5 & STRINGER 17 IAW VT-SAA EA 011-5720-01-A7721 I/R AND UPS EO MD11-5730-72329-A.Apr 8, 2019 · N294UP · Doug MD11FSDR HALA2019050700220Skin · corrodedDURING C CHECK THE LT LOWER WING SKIN FOUND TO HAVE CORROSION/BULGE NEAR XW 519. REAR SPAR. SEPARATED LOWER SKIN FROM REAR SPAR LOWER CAP APPROX 14" AT STATION YU519. TRIMMED OUT CORROSION ON LOWER SKIN C 148" S 3.75". HFEC OK. PERFORMED DVI OF SURROUNDING ARApr 7, 2019 · N488HA · Boeing 717200SDR IPXA2019041534991Doubler · crackedINSPECTION TYPE:4C, LT WING L/E HAS A CRACK IN THE PANEL LANDING (DOUBLER) FWD LIP JUST AFT OF #9 SLAT TRACK.REMOVED AND REPLACED LT WING CRACKED PANEL LANDING (DOUBLER) JUST AFT OF #9 SLAT TRACK IAW MD-11 SRM 51-33-01. (MINOR)Apr 6, 2019 · N294UP · Doug MD11FSDR IPXA2019041984169Doubler · crackedINSPECTION TYPE:4CR/H WING FIXED L/E SKIN SPLICE DOUBLER IS CRACKED AT STA. XOS.906.REMOVED, FABRICATED AND REPLACED DOUBLER AT SAID LOCATION IAW DWG. ARB3954 AND SRM 51-31-01. (MINOR)Apr 5, 2019 · N294UP · Doug MD11FSDR IPXA2019041761101Skin · crackedINSPECTION TYPE:4C, R/H WING FIXED L/E LOWER SKIN IS CRACKED AT CUT-OUT AT STA. XOS. 776.8.REPAIRED CRACKED R/H WING FIXED L/E LOWER SKIN AT STA. XOS. 776.8 IAW SRM 57-40-02 REPAIR 7 FIG. 201. (MAJOR)Apr 5, 2019 · N294UP · Doug MD11FSDR AALA201904089015Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING SURFACE SKIN PLATE AT WS 779 AND RIB 14. REPAIRED SKIN PLATE PER EA 291506.Apr 5, 2019 · N170US · Airbus A321211SDR DALA2019040502208Skin · corrodedLT WING UPPER SKIN CORROSION AT REAR SPAR. FWD OF O/B SPOILER I/B END. REPAIRED COMPLIED WITH PER ER/A 575477-14 REV. O.Apr 4, 2019 · N964AT · Boeing 717200SDR SWAA2022030705462Skin · crackedRH WING FIXED L/E SKIN JUST INBD OF ENGINE PYLON #2 FASTENER HOLE IN ZONE 1 HAS A CRACK INDICATION IN COUNTERSINK PER NDT PART 6 53-30-05 / REPAIRED CRACK PER EA 1-757-16135 AND SRM 57-41-01-2R-7 REPAIR 7.Apr 3, 2019 · N216WR · Boeing 7377H4SDR SWAA2022030746132Panel · crackedRIGHT WING LOWER LEADING EDGE PANEL 621TB HAS 1 HOLE CRACKED ON BACK SIDE / REPAIRED DAMAGE TO FASTENER HOLE ON L/E PNL 621TB IAW B737 SRM 52-41-01-2A-1 AND 51-70-04-22-9. BONDED ALUMINUM FOIL I.A.W. SRM 51-70-14-2R-3 AND RSTORED FINISH I.A.W. AM 57-21-99--0G-Apr 3, 2019 · N8613K · Boeing 7378H4SDR CA190403015Skin · corroded(CAN) CORROSION AREAS ON LHS AFT UPPER WING PLANK (DWG: CC670-10042 REF) AND AFT LOWER WING PLANK (DWG: CC670-10043 REF) AT OUTBOARD TRAILING EDGE FAIRING (56LAT) ATTACHMENT LAND (DWG: CC670-10235 REF) BETWEEN WS353.00-WS398.00. (TC# 20190403015)Apr 3, 2019 · Cndair CL6002C10SDR FDEA2019042530903Skin · wornLT WING: DROOP L/E, OUTBD SKIN SURFACE WORN THROUGH AND RIVETS WORN THROUGH. INSTALLED REPAIR FILLER AND DOUBLER IN REF TO SRM 57-10-00 FIG. 96 PAGE 413 VOL. 1Apr 3, 2019 · N313FE · Doug MD1030FSDR AALA201904059018Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING UPPER SURFACE TRAILING EDGE OVERHANG SKIN AT WS 7800 BETWEEN RIB 10 AND RIB 11. REPAIRED SKIN PER EA 291500.Apr 3, 2019 · N170US · Airbus A321211SDR DALA2019040302114Access Panel · corrodedCORROSION IN ACCESS #520FT ON SETTLEMENT AREA AND COUNTERSINK HOLES AT FUEL TANK LEFT. (AI). NRC 00565: CORROSION LEVEL 2, CORROSION ON FUEL ACCESS PLATE #520FT AT SETTLEMENT AND COUNTERSINK HOLES AREA WAS REMOVED PER B717-200 SRM 51-10-04-0G PAR 26, WAS FOUNDApr 3, 2019 · N940AT · Boeing 717200SDR SWAA2022030749621Panel · crackedLEFT WING REAR SPAR UPPER FIXED TRAILING EDGE PANEL OUTBOARD RIB CRACKED / REMOVED AND REPLACED LEFT WING REAR SPAR UPPER FIXED TRAILING EDGE OUTBOARD RIB PANEL PER SRM 51-10-02 & 51-40-02Apr 2, 2019 · N447WN · Boeing 7377H4SDR IPXA2019041981184Skin · corrodedINSPECTION TYPE:4CL/H WING UPPER AFT SKIN HAS CORROSION BETWEEN STA, XORS. 277-293 AND BETWEEN STR. 2 &3.REPAIRED CORRODED L/H WING UPER AFT SKIN AT NOTED LOCATIONS IAW VT-SAA EA 011-5730-01-A7709 REV. I/R AND UPS EO MD11-5730-72264-A. (MINOR)Apr 2, 2019 · N289UP · Doug MD11FSDR IPXA2019041941225Skin · corrodedINSPECTION TYPE:4CL/H WING UPPER AFT SKIN HAS CORROSION AT STR. #3 AND BETWEEN STA. XOS. 348.7 TO XOS. 353.REPAIRED CORRODED L/H WING UPPER AFT SKIN AT STR. #3 BETWEEN STA. XOS. 348.7 TO XOS. 353 IAW VT-SAA EA 011-5730-01-A7710 REV. I/R AND UPS EO MD11-5730-72Apr 2, 2019 · N289UP · Doug MD11FSDR IPXA2019041741139Cap · crackedINSPECTION TYPE:4C, R/H UNDER WING CANTED PANEL CAP IS CRACKED AT STA. 1236.8, Z=-100.REPAIRED CRACKED R/H UNDER WING CANTED PANEL CAP AT STA. 1236.8 AND Z=-100 IAW VT-SAA EA 011-5310-01-A7689 REV. I/R AND UPS EO MD11-5340-72140-A. (MAJOR)Apr 2, 2019 · N289UP · Doug MD11FSDR DALA2019040302113Access Panel · corrodedCORROSION ON COUNTERSUNK AND SETTLEMENT ON FUEL ACCESS PLATE #620FT AT FUEL TANK RIGHT. (AD). NRC 00577: CORROSION LEVEL 2, CORROSION ON FUEL ACCESS PLATE #620FT AT SETTLEMENT AND COUNTERSINK HOLES AREA WAS REMOVED PER B717-200 SRM 51-10-04-0G PAR 26, WAS FOUNApr 2, 2019 · N940AT · Boeing 717200SDR DALA2019040302112Access Panel · corrodedCORROSION ON COUNTERSUNK AND SETTLEMENT ON FUEL ACCESS PLATE #520DB AT FUEL TANK LEFT. (AI). NRC 00576: CORROSION LEVEL 2, CORROSION ON FUEL ACCESS PLATE #520DB AT SETTLEMENT AND COUNTERSINK HOLES AREAS WAS REMOVED PER B717-200 SRM 51-10-04-0G PAR 26, WAS FOUNApr 2, 2019 · N940AT · Boeing 717200SDR DALA2019040302111Access Panel · corrodedCORROSION IN ACCESSES 520CT AND 620CT ON SETTLEMENT AREA AND COUNTERSINK HOLES AT FUEL TANK. (AI) (AD). NRC 533: CORROSION LEVEL 2, ACCESS PLATES 520CT AND 620CT WERE REPLACED PER B-717 SRM 57-10-01 REPAIR 2 PAR. 5 CONDITION III. (LP #1013646)Apr 2, 2019 · N940AT · Boeing 717200SDR CA190404004Skin · deformed(CAN) SKIN DEFORMATION BOTH SIDES AT STA. 237 FOUND AFTER REMOVING WINGTIPS, P/NS 45412-10 40585-13 (TC# 20190404004)Apr 1, 2019 · Piper PA31325SDR IPXA2019041941210Doubler · crackedINSPECTION TYPE:4CR/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS. 648-653.REPAIRED CRACKED R/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS. 648-653 IAW VT-SAA EA 011-5730-01-A7706 REV. I/R AND UPS EO MD11-5730-72294-A. (MAJOR)Apr 1, 2019 · N289UP · Doug MD11FSDR IPXA2019041541046Skin · crackedINSPECTION TYPE:4C, R/H WING FIXED L/E LOWER SKIN IS CRACKED AT STA. XOS. 776.REPAIRED CRACKED R/H WING FIXED L/E LOWER SKIN AT STA. XOS. 776 IAW SRM 57-40-02 REPAIR 7 FIG. 201. (MAJOR)Apr 1, 2019 · N289UP · Doug MD11FSDR IPXA2019041541043Skin · crackedINSPECTION TYPE:4C, R/H WING FIXED L/E LOWER SKIN IS CRACKED AT STA. XOS.490.850.REPAIRED CRACKED R/H WING FIXED L/E LOWER SKIN AT STA. XOS. 490.850 IAW SRM 57-40-01 REPAIR 17 FIG. 201.Apr 1, 2019 · N289UP · Doug MD11FSDR IPXA201904124956Cap · wornINSPECTION TYPE:4CR/H WING FIXED L/E LOWER CAP AT STA. XOS.464.0 IS WORN TO A KNIFE EDGE.REMOVED, FABRICATED AND REPLACED CAP AT SAID STA. IAW DWG ARB1284 AND SRM 51-33-01. (MINOR)Apr 1, 2019 · N289UP · Doug MD11FSDR IPXA2019041941223Doubler · crackedINSPECTION TYPE:4C, LT WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS. 625.56 TO 636.84.REPAIRED CRACKED L/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS. 625.56 TO 636.84 IAW VT-SAA EA 011-5740-01-A7703 REV. I/R AND UPS EO MD11-5740-72274-A. (MAMar 31, 2019 · N289UP · Doug MD11FSDR IPXA2019041764194Doubler · crackedINSPECTION TYPE:4CL/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS. 703.5 TO 708.9.REPAIRED CRACKED L/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS. 703.5 TO 708.9 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)Mar 31, 2019 · N289UP · Doug MD11FSDR IPXA2019041541044Doubler · crackedINSPECTION TYPE:4C, L/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS. 789.6 TO 795.7.REPAIRED CRACKED L/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS. 789.6 TO 795.7 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)Mar 31, 2019 · N289UP · Doug MD11FSDR DALA20190402080Panel · looseON ARRIVAL RT WING LOWER L/E PANEL LOOSE & DAMAGED. 2ND PANEL FROM O/B. INSPECTED PER MD88 M/M 51-00-01-201 FOUND 3 SCREWS OUT OF 27 INSTALLED. REMAINING SCREWS LOCATED ALONG T/E & I/B EDGE. R/R LEADING EDGE PANEL, TORQUED SCREWS PER MD88 AMM 20-30. OK FOR SVCMar 31, 2019 · N961DL · Doug MD88SDR SWIA2019050145809Skin · corrodedRIGHT WING PLANK. FUEL TANK ACCESS 650HB HAS CORROSION AND FRETTING DAMAGE. (C-CHECK) RO: 04/28/2019 BLENDED, ROTOPEENED AND REPAIRED WING TANK ACCESS HOLE 650HB IAW SRM AND REO. ALL CHECKS GOOD.Mar 30, 2019 · N429SW · Cndair CL6002B19SDR AALA201905069019Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING REAR SPAR TRAILING EDGE UPPER SKIN PANEL 2 LOWER SURFACE BETWEEN RIB 8 AND RIB 9. REPAIRED SKIN PANEL PER EA 292650.Mar 29, 2019 · N176UW · Airbus A321211SDR UIEA2019032903699Skin · gougedGOUGE ON RT WING LWR SKIN LWR SURFACE AT WBL 743.828 BETWEEN S-5 AND S-10(<P>1. REPAIR DAMAGE AREA IAW EI NO. T2019A57M-1310 REV.1</P><P>2. JOB COMPLETED AND CONDITION CHECK NORMAL</P>)Mar 28, 2019 · N492MC · Boeing 74747UFSDR CA190403016Skin · corroded(CAN) MULTIPLE BLENDED CORROSION AREAS TO AFT UPPER WING PLANK (DWG: CC670-10042, REF) BETWEEN WS353.00 - WS387.50, RHS. MINIMUM REMAINING THICKNESS IS 4.53MM [0.I78 ] OUT OF 0.200 +/-0.005 NOMINAL, REF, AND 2.25MM [0.089 ] OUT OF 0.100 +/-0.005 NOMINAL,Mar 27, 2019 · Cndair CL6002C10
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