JASC 5730

Service difficulty reports · 27,269

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 IXXA08SMN001SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING LOWER SKIN CENTRAL LEADING EDGE CRACKED AT STATION XF 428.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGE AREA. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION DETECTED AFTER TEST. FABRJan 11, 2008 · N41CX · Doug DC862FSDR NOCA00308Panel · delaminatedLEADING EDGE PANEL ON RIGHT WING INBOARD BELOW INBOARD LEADING EDGE SLAT PANEL IS TORN / DELAMINATED. PERFORMED TEMP REPAIR ON PANEL 611CB PER BOEING SERVICE REQUEST 1-750124783-5. PANEL SERVICEABLE FOR ONE TIME FLIGHT. Jan 11, 2008 · N767NA · Boeing 767324SDR NOCA003Panel · tornLEADING EDGE PANEL ON RIGHT WING INBOARD BELOW INBOARD LEADING EDGE SLAT PANEL IS TORN / DELAMINATED. PERFORMED TEMP REPAIR ON PANEL 611CB PER BOEING SERVICE REQUEST 1-750124783-5. PANEL SERVICEABLE FOR ONE TIME FLIGHT. Jan 11, 2008 · N767NA · Boeing 767324SDR UIEA200800011Panel · delaminatedLT WING UPPER FIXED L/E PANEL HAS AREA OF DELAMINATION, 4.0 INCH WIDE BY 45.0 INCH LONG. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 51-40-09 FIG 18 SHEET 3 AND 5, PREPREG 250 DEGREE CURE PER SRM 51-40-12. ALSO, REFERENCE ATLAS AIR EO NR 4757A409.Jan 10, 2008 · N523MC · Boeing 7472D7BSDR UIEA200800010Panel · crackedRT WING L/E FIXED UPPER PANEL WS426 CRACKED FROM THE L/E OF THE PANEL THROUGH TO THE FIRST RIVET HOLE. LOCATION IS 29" OUTBD OF INBD EDGE OF FIXED PANEL AT WS 426, 0.500" LONG. OUT OF LIMITS AS PER SRM 51-70-02.Jan 10, 2008 · N412 · Boeing 74747UFSDR 08FDEA00064Skin · cracked06 FASTENER HOLES FOUND CRACK INDICATION DURING HFEC, OPEN HOLE INSPECTION AT RT WING LWR SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS=685 AND STA XORS=710. COMPLIED WITH EA 1-5710-117258, CLASSIFIED AS A MAJOR REPAIR AS PER FEDEX GMM 6-2-100.Jan 7, 2008 · N583FE · Doug MD11FSDR 08FDEA00063Skin · cracked02 EACH FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION AT LT WING LWR SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS=690 AND STA XORS=700. COMPLIED WITH FEDEX E.A. 1-5710-117257, CLASSIFIED AS A MAJOR REPAIR AS PER FEDEX GMM 6-2-100.Jan 7, 2008 · N583FE · Doug MD11FSDR 08FDEA00055Access Panel · corrodedRIGHT WING FUEL TANK ACCESS PANEL 642AB HAS CORROSION ON LOWER SURFACE. REMOVED CORROSION ON PANEL 642AB IAW SRM 57-20-01, FOUND TO BE OUT OF LIMITS PER SRM 57-20-01, FIG 201, DETAIL I, SECTION AA, NOTE B. REPLACED ACCESS PANEL IAW AMM 28-11-01.Jan 6, 2008 · N901FD · Boeing 7572B7SDR 08FDEA00054Access Panel · corrodedRIGHT WING FUEL TANK ACCESS PANEL 641MB HAS CORROSION ON LOWER SURFACE. REMOVED CORROSION ON PANEL 641MB IAW SRM 57-20-01. AFTER REWORK AMOUNT REMAINING NOT WITHIN LIMITS IAW SRM 57-20-01, FIG 201, DETAIL II, III WITHIN 0.10" OF SEAL. REPLACED ACCESS PANEL Jan 6, 2008 · N901FD · Boeing 7572B7SDR 08FDEA00052Access Panel · corrodedRIGHT WING TANK ACCESS PANEL 643CB HAS SURFACE CORROSION ON LOWER SURFACE. REMOVED CORROSION ON PANEL 643CB IAW SRM 57-20-01, FOUND TO BE OUT OF LIMITS PER SRM 57-20-01, FIG 201, DETAIL I, SECTION AA, NOTE B. REPLACED ACCESS PANEL 643CB IAW AMM 28-11-01.Jan 6, 2008 · N901FD · Boeing 7572B7SDR 08FDEA00051Access Panel · corrodedRIGHT WING FUEL TANK ACCESS PANEL 641EB HAS CORROSION ON LOWER SURFACE REMOVED CORROSION ON PANEL 641EB PER SRM 57-20-01, FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01, FIG 201, DETAIL I, SECTION A-A, NOTE B. REPLACED PANEL IAW AMM 28-11-01.Jan 6, 2008 · N901FD · Boeing 7572B7SDR UPS08851533Doubler · crackedINSPECTION TYPE:C2 R/WING, OUTBD STUB WING HAS DOUBLER AT LWR SURFACE WITH 2" CRACK. REMOVED CRACK DOUBLER AT R/WING OUTBD STUB WING IAW SRM 51-1-20D. FABRICATED AND INSTALLED REPAIR DOUBLER ON R/WING OUTBD STUB WING STA XW 467.000 IAW SRM 57-02-01A-0 FIG 00Jan 5, 2008 · N702UP · Doug DC871FSDR 08FDEA00046Access Panel · corrodedRT WING TANK ACCESS PANEL 643BB HAS SURFACE CORROSION ON LOWER SURFACE. REMOVED CORROSION ON PANEL 643BB IAW SRM 57-20-01, FOUND TO BE OUT OF LIMITS PER DETAIL I, SEC AA, NOTE B, NOT ALLOWED DAMAGE PER FIG 201. ORDERED AND REPLACED WITH NEW PANEL.Jan 5, 2008 · N901FD · Boeing 7572B7SDR 2008UALA00103Skin · gougedRIGHT WING FIXED L/E GOUGED - PUNCTURED FROM DISLODGED UPSTOP JUST INBOARD OF NR 4 SLAT ACTUATOR. ACCOMPLISHED COMPOSITE SET-UP REPAIR PER SRM 51-70-17 REPAIR 7.Jan 4, 2008 · N339UA · Boeing 737322SDR C2XA08IA012Skin · crackedIAH, FLIGHT 2472, DURING PREFLIGHT INSPECTION THE CREW REPORTED A CRACK IN THE LEFT WING UPPER SKIN ADJACENT TO THE LEFT SPOILER INBOARD HINGE POINT. THE SKIN WAS INSPECTED AND PLACED ON DMI FO 500FC, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON Jan 4, 2008 · N14925 · Emb EMB145EPSDR WRLA2008002Access Panel · crackedDURING C-CHECK INSPECTION FOUND RT WING OUTBOARD SLAT DRIVE MECHANISM ACCESS PANEL SKIN CRACKED. REPAIRED RT WING ACTUATOR ACCESS DOOR OUTER SKIN AT XOS STA 490.85 PER EGAT EI NR W2008A57B-022.Jan 4, 2008 · N277WA · Doug MD11SDR QXEA200802072Skin · brokenPDX - C5 CHECK - APERTURE FOR PANEL 522AT HAS A BROKEN NUT PLATE LEFT HAND CORNER. REMOVED BROKEN NUTPLATE FOR PANEL 522AT AND REPLACED WITH NEW NUTPLATE FROM STOCK.Jan 1, 2008 · N348PH · Dhav DHC8202SDR QXEA200802096Skin · gougedPDX - C5 CHECK - RIGHT WING LOWER SKIN DOUBLER HAS NUMBEROUS SMALL GOUGES IN AN AREA APPROXIMATELY 8" BY 1" LOCATED AT YW225 AND 10" AFT OF MAGNA STICK. REPAIRED IAW RD8-57-2996, 1-82-7A PT 6 51-00-02, 1-82-7A PT 1 51-00-05 AND RD8-57-3821, AND -8 200 SRM 51Jan 1, 2008 · N348PH · Dhav DHC8202SDR UPS08M51760Doubler · crackedINSPECTION TYPE:C RT WING FIXED LE COMPT AT XORS 538 APPROX FOUND UPPER DOUBLER CRACK AS MARKED CRACK AREAS ON UPPER DOUBLER BET XOS 636 AND 643 AND XOS 644 AND XOS 648 02 EA LOCATIONS TRIMMED OUT INDIVIDUALLY PER EN NR 1016-08. HFEC INSP C/O PER DAC NDTSPM 0Dec 30, 2007 · N293UP · Doug MD11FSDR UPS08M51755Doubler · crackedINSPECTION TYPE:C RT WING FIXED LE COMPT AT STA XORS 597 APPROX, FOUND UPPER DOUBLER CRACKED AS MARKED. CRACKED AREA AT XOS 692 TO XOS 698 AND XOS 700 TO XOS 703 AREA TRIMMED OUT PER EN NR 1016-08. HFEC INSP C/O PER DAC NDTSPM R13,06-10-01.001 ON TRIMMED OUTDec 30, 2007 · N293UP · Doug MD11FSDR C2XA07IA257Skin · crackedIAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED THE LEFT WING SKIN TO BE CRACKED AT THE SPOILER HINGE POINT. THE CRACK WAS INSPECTED AND PLACED ON DMI, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THIS SDR FILED OPEN PENDING FINAL CORRECTIVE ACTIDec 27, 2007 · N14930 · Emb EMB145EPSDR 07FDEA05124Plate · crackedCRACKED ANGULAR PLATE INBD OF LT WING INBD TE FLAP O/B TRACK ALONG AFT SUPPORT FRAME REMOVED AND REPLACED CRACKED ANGULAR PLATE IAW SRM 51-40-3 PAINTED AREA IAW SRM 51-20-151-7.Dec 23, 2007 · N499FE · Boeing 727232SDR UPS07451337Panel · delaminatedRT WING UPPER INBD FIXED TRAILING EDGE PANEL DELAMINATED. REMOVED DISBONDED, DAMAGED SKIN FROM LEADING EDGE ACROSS PANEL TO LWR EDGE IAW 51-40-20. FABRICATED SKIN FILLER. REPLACED PANEL WITH SERVICEABLE PANEL.Dec 22, 2007 · N677UP · Boeing 747123FSDR LR7A07176Skin · crackedDURING SCHEDULED C-3 CHECK, PER SB382-57-85 R2 FOUND HOLE CRACK IN WING PLANK COMMON TO WING ATTACH ANGLE AT FS 597, CWS61R, WL256, NR 1 LOWER PLANK, HOLE 53Y. REPAIR ACCOMPLISHED IAW LAC MEA 382-57-07-076.Dec 19, 2007 · N406LC · Lkheed 382GSDR LR7A07175Skin · crackedDURING SCHEDULED C-3 CHECK, PER SB382-57-85 R2 FOUND HOLE CRACK IN WING PLANK COMMON TO WING ATTACH ANGLE AT CWS61R, WL256, STRINGER 20, HOLE 37Y. REPAIR ACCOMPLISHED IAW LAC MEA 382-57-07-087.Dec 19, 2007 · N406LC · Lkheed 382GSDR LR7A07174Skin · crackedDURING SCHEDULED C-3 CHECK, PER SB382-57-85 R2 FOUND HOLE CRACK IN WING PLANK COMMON TO WING ATTACH ANGLE AT CWS61R, WL256, NR 2 LOWER PANEL, HOLE 36X. REPAIR ACCOMPLISHED IAW LAC MEA 382-57-07-087.Dec 19, 2007 · N406LC · Lkheed 382GSDR LR7A07169Panel · corrodedDURING SCHEDULED C-3 CHECK, PER SB382-57-85 R2 FOUND RT LOWER CENTER WING PANEL CORROSION AT CWS190-208R STRINGERS 15-16. REPAIR ACCOMPLISHED IAW LAC MEA 382-57-07-083.Dec 19, 2007 · N406LC · Lkheed 382GSDR LR7A07168Panel · corrodedDURING SCHEDULED C-3 CHECK, PER SB382-57-85 R2 FOUND CORROSION LT CTR WING BOTTOM AFT PANEL AT CWS178-208L BETWEEN STRINGERS 21 TO 24. REPAIR ACCOMPLISHED IAW LAC MEA 382-57-07-082.Dec 19, 2007 · N406LC · Lkheed 382GSDR LR7A07155Panel · corrodedDURING SCHEDULED C-3 CHECK, PER SB382-57-85 R2 FOUND CORROSION ON WING PLANK HOLE COMMON TO LT ATTACH ANGLE AT FS 517, CWS72L, WL256. REPAIR ACCOMPLISHED IAW LAC MEA 382-57-07-076.Dec 19, 2007 · N406LC · Lkheed 382GSDR LR7A07154Panel · crackedDURING SCHEDULED C-3 CHECK, PER SB382-57-85 R2 FOUND CRACK ON WING PLANK HOLE COMMON TO RT ATTACH ANGLE AT FS 517, CWS72R, WL256. REPAIR ACCOMPLISHED IAW LAC MEA 382-57-07-076.Dec 19, 2007 · N406LC · Lkheed 382GSDR LR7A07152Skin · corrodedDURING SCHEDULED C-3 CHECK, PER SB382-57-85 R2 FOUND CORROSION ON RT UNDERWING SURFACE NR 1 AND NR 3 WING PLANKS BEHIND NR 3 ENGINE AFT NACELLE AREA CWS178-212 STRINGER 21-24. REPAIR ACCOMPLISHED IAW LAC MEA 382-57-07-072 AND CORROSION REMOVED AND TREATED IAWDec 19, 2007 · N406LC · Lkheed 382GSDR DHL2007763002Panel · delaminated7 BY 5 INCH AREA OF DELAMINATION ON PANEL JUST O/B OF NR 1 SPOILER. DELAMINATION LOCATED JUST ABOVE JACKSCREW GEAR BOX, PANEL NR 8155.Dec 18, 2007 · N763AT · Boeing 727264SDR C2XA07IA249Skin · crackedIAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED A CRACK IN THE UPPER LT WING SKIN. THE CRACK WAS INSPECTED AND PLACED ON A 500 FLIGHT CYCLE DEFERRAL IN ACCORDANCE WITH EMBRAER IC2007-145/08980, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Dec 16, 2007 · N14937 · Emb EMB145EPSDR C2XA07IA248Skin · crackedIAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED A CRACK IN THE UPPER RT WING SKIN. THE CRACK WAS INSPECTED AND PLACED ON A 500 FLIGHT CYCLE DEFERRAL IN ACCORDANCE WITH EMBRAER IC2007-145/08976, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Dec 16, 2007 · N15932 · Emb EMB145EPSDR DHL2007783Skin Panel · debondedUPON VISUAL INSPECTION OF THE LEFT WING UPPER SURFACE FOUND THE PANEL JUST OUTBOARD OF THE NR 1 SPOILER WITH SKIN DISBONDING. W/S629-656.5 IS PANEL LOCATION. DISBONDING AREA IS APPROX 56 SQ IN. PANEL TO BE REPLACED.Dec 14, 2007 · N783DH · Boeing 727227SDR UIEA200700493Panel · delaminatedLT WING UPPER SURFACE LEADING EDGE TO FRONT SPAR PANEL (BEHIND NR 8 LEADING EDGE FLAP WS 917) HAS EVIDENCE OF DELAMINATION. PANEL REPAIRED IAW SRM 51-40-9 AND 51-40-12.Dec 12, 2007 · N526MC · Boeing 7472D7BSDR UIEA200700492Panel · delaminatedLT WING UPPER SURFACE LEADING EDGE TO FRONT SPAR PANEL (BEHIND NR 6 LEADING EDGE FLAP WS 1028) HAS EVIDENCE OF DELAMINATION. PANEL REPAIRED IAW SRM 51-40-9 AND 51-40-12. Dec 12, 2007 · N526MC · Boeing 7472D7BSDR UIEA200700497Panel · delaminatedLEFT HAND WING UPPER SURFACE PANEL NR 521 HAS EVIDENCE OF DELAMINATION 3 INCHES LONG, 2INCHES AWAY FROM OUTBOARD EDGE AND 5 INCHES FROM THE LEADING EDGE. REPAIRED PANEL IAW SRM 51-40-12 AT 250 DEGREES AND 26" HG VACUUM AND XEO 57-121207.Dec 12, 2007 · N526MC · Boeing 7472D7BSDR UIEA200700496Panel · gougedLEFT WING UPPER SURFACE PANEL NR 521 HAS A CIRCULAR SHAPED GOUGE ABOUT 12 INCHES OUTBOARD OF THE INBOARD EDGE ( 7.5 INCHES LONG BY 5.5 WIDE). INTERIM REPAIR ACCOMPLISHED IAW SRM 51-40-15 AND XEO 57-121207.Dec 12, 2007 · N526MC · Boeing 7472D7BSDR UIEA200700494Panel · crackedLT WING UPPER SURFACE LEADING EDGE TO FRONT SPAR PANEL (BEHIND NR 9 LEADING EDGE FLAP WS 862) HAS 2 INCH CRACK. PANEL REPAIRED IAW SRM 51-40-9 AND 51-40-12.Dec 12, 2007 · N526MC · Boeing 7472D7BSDR UIEA200700495Panel · delaminatedLEFT WING UPPER SURFACE PANEL NR 521 HAS EVIDENCE OF DELAMINATION ABOUT 3 INCHES LONG 6 INCHES FORWARD OF THE TRAILING EDGE AND 18 INCHES INBOARD OF THE OUTBOARD EDGE. ALSO AN AREA 3 INCHES LONG 21 INCHES AWAY FROM THE OUTBOARD EDGE AND 5 INCHES AFT OF THE LEDec 12, 2007 · N526MC · Boeing 7472D7BSDR ABXA080008Panel · corrodedLEFT WING TRAILING EDGE ASSEMBLY NUMEROUS AREAS OF CORROSION AND DISBONDING AT INTERVAL FINGER DOUBLER AND LEADING EDGE DOUBLER. REMOVED AND REPLACED TRAILING EDGE ASSEMBLY IAW DC9 SRM.Dec 10, 2007 · N932AX · Doug DC933FSDR UIEA200700484Panel · crackedDURING ROUTINE INSPECTION FOUND LT WING L/E FIXED FIBERGLASS PANEL UPPER SURFACE AT WS 577/586 CRACKED LONGITUDINAL AND AT WS 752 PREVIOUS REPAIR DELAMINATED. PERMANENT REPAIRS ACCOMPLISHED IAW 51-40-09 AND 51-40-12, DOCUMENTED ON EO 4757A406.Dec 10, 2007 · N522MC · Boeing 7472D7BSDR UIEA200700483Panel · crackedDURING ROUTINE INSPECTION FOUND RT WING L/E FIXED FIBERGLASS PANEL UPPER SURFACE CRACKED LATERAL 4" AT WS 1322. PERMANENT REPAIRS ACCOMPLISHED IAW SRM 51-40-09 AND 51-40-12. DOCUMENTED ON EO 4757A407.Dec 10, 2007 · N522MC · Boeing 7472D7BSDR AMWA071001017Skin · chafedFRICTION CHAFING DURING ENGINE OPERATION CREATED WORN SEGMENTS ON THE RT ENGINE NACELLE. CHAFING WAS ALONG THE ENTIRE LENGTH AND SHAPE OF THE NACELLE. OBTAINED APPROVED DATA AND REPAIRED WING SKIN.Dec 6, 2007 · N244YV · Beech 1900DSDR DHL2007770Skin · delaminatedRT WING UPPER SURFACE HAS PANEL O/B OF APU EXH WITH 2 LARGE AREAS OF DELAMINATION APPROX W/S 224 TO 330. TWO AREAS EQUAL TO ABOUT 120 SQ IN.Dec 6, 2007 · N770AT · Boeing 7272B7SDR CALA0700732Skin · crackedLEFT WING FIXED L/E TOP SURFACE CRACKED BW WSS380 TO WSS420. REPAIR PER EA 5731-01010 OP 4 AND SRM 51-70-07.Dec 5, 2007 · N12114 · Boeing 757224SDR C2XA07SH097Plate · corrodedSHV - DURING C-CHECK 191 WING TO FUSELAGE FAIRING HAS CORRODED BONDING PLATE ON LOWER TRAILING EDGE. MAINTENANCE REPAIRED 191 PNL LOWER TRAILING EDGE BONDING PLATE IAW EC5750-01315 REV-E. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.Dec 5, 2007 · N17115 · Emb EMB145XRSDR QXEA200801942Skin · corrodedPDX - C5 CHECK - RIGHT WING INBOARD LEADING EDGE LOWER FLANGE HAS FRETTING CORROSION AT APPROXIMATELY STATION YW57. BLENDED AND REPAIRED IAW RD8-57-811 AND DASH 8 200 SRM 51-00-01, 51-40-11.Dec 4, 2007 · N347PH · Dhav DHC8202SDR 07FDEA04993Skin · misrepairedLEFT WING EXTERNAL REPAIR DOUBLER ON TRAILING EDGE END RIB, APPROXIMATE WING STATION 1278 BETWEEN WING RIBS 20 AND 21 REAR SPAR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EVALUATED REPAIR, FOUND Dec 4, 2007 · N402FE · Airbus A310203
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