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 04FDEA02336Panel · dentedRT WING OB T/E PANEL ZONE 691 HAS 100 DENTS, OF WHICH 40 ARE DELAMINATED (TOP AND BOTTOM OF PANEL) ( AREA 2 INCHES X 12INCHES ) REMOVED DAMAGED T/E PNL AND INSTALLED NEW T/E PNL IAW A310/200 DWG 57243876.Aug 1, 2004 · N409FE · Airbus A310SDR IXXA060417SSkin · corrodedDURING ROUTINE C CHECK, FOUND LEFT WING LEADING EDGE SKIN CORRODED AT STATION XFS61. REPAIRED PER ALL APPLICABLE DATA.Jul 30, 2004 · N41CX · Doug DC862SDR UPS04242993Panel · delaminatedINSPECTION TYPE: C, PANEL ON LOWER SURFACE OF RT WING L/E FALSEWORK PANEL FSS 195 TO FSS 314 HAS DELAMINATION AT FWD EDGE. PANEL REMOVED IAW SRM 51-10-06. PANEL FABRICATED IAW DRG 65-21653 AND SRM 51-40-9. ON INSTALLATION OF PANEL, FUEL PIPE FOUND TO BE DAMJul 30, 2004 · N945UP · Boeing 72722CSDR 04FDEA02305Skin · crackedLEFT WING, THRU FUEL TANK ACCESS PANEL CUTOUT 536CB, UPPER STRINGER NR 10, STRINGER END FOUND WITH CRACK OF ABOUT 10 INCHES LONG. REPAIR CARRIED OUT AT LT WING FUEL TANK ACCESS PANEL CUT-OUT 536CB, UPPER STRINGER NR 10 AS PER SRM 57-20-00 FIG 10, VOL I. FABJul 30, 2004 · N613FE · Doug MD11SDR DHL2004745538Skin · dentedDURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; RT WING LE SKIN DENT 4 INCHES OB OF IB LANDING LIGHT LE STA 120. CUT OUT 2EA DAMAGED AREAS, FABBED FILLERS FROM 2024-T3 .050 PO NR 900920 DIM 1INCH X 1INCH EA, 1EA DOUBLER FROM 2024-T3 .063 PO NR 9007Jul 30, 2004 · N745DH · Boeing 727224SDR 04FDEA02322Panel · corrodedCORROSION ON MATING SURFACE OF PANEL 541BB. REMOVED CORROSION IAW DC10 SRM 51-21-01 VOL II. ORIGINAL THICKNESS .032 INCHES, 7075-T6 IAW DRW NR ARC0267. MATERIAL THICKNESS AFTER BLEND OUT .020 INCHES, PART OUT OF LIMITS IAW DC10 SRM 57- 00-01 VOL I. RECIEVEDJul 30, 2004 · N396FE · Doug MD1010FSDR 04FDEA02314Skin · chafedRIGHT HAND WING LEADING EDGE SKIN HAS CHAFFING MARKS FROM NR 4, 5, 6 & 7 LEADING EDGE SLATS, ALSO TEFLON PAINT MISSING IN SOME AREAS. CHAFFING AREA IS BETWEEN STATION XOS 660 AND XOS 1005. BLENDED LEADING EDGE BEHIND SLAT NR 4 AND 7, FOUND TO BE OUT OF LIMITJul 30, 2004 · N396FE · Doug MD11FSDR 04FDEA02304Skin · crackedLT WING, THRU FUEL TANK ACCESS PANEL CUTOUT 535BT, UPPER STRINGER NR 12, STRINGER END FOUND WITH CRACK OF ABOUT 10 INCHES IN LENGTH. REPAIR CARRIED OUT AT LT WING FUEL TANK ACCESS PANEL CUT-OUT 535BT, UPPER STRINGER NR 12 AS PER SRM 57-20-00 FIG 10, VOL I. FJul 30, 2004 · N607FE · Doug MD11SDR 2004F00370Skin · corrodedDURNG FA02 A-CHECK ACCOMPLISHGIN ATLAS AIR ROUTINE WORK CARD 12M15002 INSPECTION OF RIGHT WING FOUND BULGE AT LOWER FRONT SPAR CAP, CORROSION IS REPORTED AS LEVEL 1 AND IS LOCAL. (M) T64RJul 29, 2004 · N809MC · Boeing 747228FSDR USAA040396Skin · delaminatedPIT - FOUND SKIN DELAMINATED, 5 INCH BY 6 INCH AREA OF DELAMINATION, OUTBOARD END OF T/E. REMOVED DAMAGED CORE MATERIAL AND REPLACED, INSTALLED DOUBLERS PER SRM 51-70-10. (M)Jul 29, 2004 · N356US · Boeing 737301SDR HNAA0400071Panel · corrodedDURING C-CHECK INSPECTION FOUND STRESS PANELS 523 AND 623 AT WITH CORROSION IN COUNTERSINKS. REMOVED AND REPLACED PANELS.Jul 29, 2004 · N982HA · Dhav DHC8102SDR 2004FA0000920Skin · corrodedINSPECTION OF WING CENTER SECTION PER AD 02-26-02 FOUND LIGHT CORROSION ON LOWER SKINS, MODERATE CORROSION ON 3 STIFFENERS. REPLACED STIFFENERS, CLEANED AND TREATED SKIN. AIRCRAFT WAS OUTSIDE WITHOUT COVER FOR AT LEAST 30 YEARS.Jul 28, 2004 · N9474 · Univar 415CDSDR 04FDEA02270Skin Panel · corrodedLEFT HAND WING UPPER SURFACE TRAILING EDGE PANEL FORWARD EDGE FOUND BULGING AT OUTBOARD OF NR 5 SPOILER XORS 827. REMOVED AS PER SRM 51-21-01, VOLUME II, MATERIAL THICKNESS=0.270, MATERIAL REMAINED=0.231, MATERIAL REMOVED=0.039 FOUND WITHIN LIMIT (0.054) ASJul 28, 2004 · N613FE · Doug MD11SDR 04FDEA02214Skin · corrodedLT WING UPPER SKIN FORWARD OF NR 4 SPOILER OUTBOARD HINGE FOUND CORRODED. BLENDED OUT CORROSION IAW SRM 51-21-01, VOLUME II AND FOUND OUT OF LIMIT AS IAW SRM 57-10-00, FIGURE 32, VOLUME I. ORIGINAL THICKNESS=0.180, MATERIAL REMOVED=0.020 AND REMAINING MATERJul 28, 2004 · N607FE · Doug MD11SDR 2004FA0000919Skin · corrodedINSPECTION OF WING CENTER SECTION PER AD 02-26-02 FOUND LIGHT CORROSION ON LOWER SKINS, MODERATE CORROSION ON 3 STIFFENERS. REPLACED STIFFENERS, CLEANED AND TREATED SKIN. AIRCRAFT WAS OUTSIDE WITHOUT COVER FOR AT LEAST 30 YEARS.Jul 28, 2004 · N9474 · Univar 415CDSDR 2004FA0000918Skin · corrodedINSPECTION OF WING CENTER SECTION PER AD 02-26-02 FOUND LIGHT CORROSION ON LOWER SKINS, MODERATE CORROSION ON 3 STIFFENERS. REPLACED STIFFENERS, CLEANED AND TREATED SKIN. AIRCRAFT WAS OUTSIDE WITHOUT COVER FOR AT LEAST 30 YEARS.Jul 28, 2004 · N9474 · Univar 415CDSDR 2004FA0000887Skin · crackedTHE RT WINGTIP HAS A CRACK APPROXIMATELY 7 INCHES LONG ON THE FAR OB END, AFT HALF OF THE WINGTIP. THE CRACK RUNS FORE / AFT ON THE WINGTIP.Jul 26, 2004 · N88ER · Raythn 390SDR DHL2004804530Skin · corrodedLT OUTER WING OB STUB WING SKIN CORRODED (UPPER PART) XOLDO 67.000. PERFORMED MAJOR REPAIR IAW EDEDW 27.3, DWG W27 R03 REV. IR. REMOVED FASTENERS IAW SRM 51-3-0 PG.1, SRM 51-1-21 PG.1. REMOVED CORROSION IAW SRM 51-1-8 PG. 17-18. FOUND OUT OF LIMITS IAW SRM 57Jul 25, 2004 · N804DH · Doug DC873FSDR UPS04842804Doubler · corrodedINSPECTION TYPE: C1, RT WING INTERIOR DOUBLER CORRODED AT STALL WARNING VANE, STA XFS371- 376. REMOVED CORRODED INTERNAL DOUBLERS SRM51-1-21. FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW DWG5769589, AND SRM 51-1-21, & 51-1-8.Jul 22, 2004 · N802UP · Doug DC873FSDR IXXA060416SSkin · corrodedDURING ROUTINE C CHECK, FOUND LEFT WING LEADING EDGE SKIN CORRODED BETWEEN STATIONS XRS710 TO XRS761. REPAIRED PER ALL APPLICABLE DATA.Jul 21, 2004 · N41CX · Doug DC862FSDR 2004F00359Panel · delaminatedDURING FA12 A-CHECK ACCOMPLISHING ROUTINE WORK CARD 11M15002 INSPECTION OF LEFT WING UPPER SURFACE, FOUND LEFT LEADING EDGE INBOARD OF NR 1 PYLON PANEL VOIDED UPPER SURFACE WING STATION 1116 PANEL. T64R (M)Jul 21, 2004 · N524MC · Boeing 7472D7BSDR DL767040678Skin · crackedRT LOWER WING SKIN SIDE LINK FITTING ATTACH FASTENER FOUND CRACKED. REPAIRED IAW ERA 091372-14AD.Jul 20, 2004 · N114DL · Boeing 767232SDR ARWA20040704Skin Panel · crackedDURING C-CHECK INSPECTION, RT WING BETWEEN XRS.428 AND XRS.463 AT STRINGER S-64 LOWER SKIN PANEL WITH CRACK, LENGTH 5.25 INCHES.Jul 19, 2004 · N661AV · Doug DC863FSDR 04FDEA02101Plate · corrodedFUSELAGE RT BASE PLATE INBOARD FLAP SUPPORT SURFACE CORROSION REPAIR P/N ANB7170-2. COMPLIED WITH EA 8-5310-80573.Jul 17, 2004 · N326FE · Doug DC1030SDR 04FDEA02081Panel · damagedPANEL 550HB HAS 2 EA ELONGATED HOLES. REPAIRED 1 EA HOLE IAW A310/200 SRM 51-40-44 FIG 1 CHAMBER CODE-J, COMPLIED WITH EA 6-5730-55328A PT 1 ON 1EA HOLE.Jul 15, 2004 · N449FE · Airbus A310222SDR 04FDEA02080Panel · damagedPANEL LAND 650 KB HAS 1 EA ELONGATED HOLE. COMPLIED WITH EA 6-5730-55328A PT1.Jul 15, 2004 · N449FE · Airbus A310222SDR C1HA200479003Panel · delaminatedRIGHT WING APU EXHAUST PANEL DELAMINATED AND CORRODED AT EXHAUST CUTOUT.Jul 12, 2004 · N679MG · Boeing 727225SDR UPS04242996Skin · crackedINSPECTION TYPE: C, 0.5 INCH CRACK IN LOWER WING SKIN AT LEFT WING TIP, APPROX 8 INCHES FROM TIP AND JUST FWD OF STRINGER FAIRING. CRACK STOP DRILLED IAW SRM 51-10-1. CRACK CONTAINED WITHIN DRILLED AREA. HOLE DRILLED IN RIB COMMON TO REPAIR SCHEME FOR NDT. Jul 9, 2004 · N945UP · Boeing 72722CSDR 04FDEA02025Panel · dentedRIGHT HAND WING TRAILING EDGE INBOARD LOWER PANEL NUMBER 641 BB HAS NUMEROUS DENTS IN ITS UPPER SURFACE. REPAIRED BY FABRICATING AND BONDING NEW METAL OUTER SKIN, CORE, INNER SKIN AND INNER DOUBLER IAW TPS 1001 REV E AND DWG ARC 2067 AND EA 8-5710-77592. REFJul 7, 2004 · N386FE · Doug MD1010FSDR DHL2004745513Skin · crackedDURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; LEADING EDGE SKIN AT CUTOUT FOR NR 6 SLAT HAS BROKEN FASTENERS AND SHARP EDGES RW5-525. REMOVED NR 6 L/E SLAT IAW MM 27-81-11. REMOVED DAMAGED FASTENERS IAW SRM 51-30-2 REMOVED SHARP EDGES AT NR 6 SLATJul 4, 2004 · N745DH · Boeing 727224SDR CALA0400561Panel · crackedINSPECTION FOUND A 6 INCH CRACK IN RIGHT WING PANEL AT WING STA XFS 70-196. THE PANEL WAS REMOVED AND REPLACED IAW SRM 51-30-2.Jul 2, 2004 · N14871 · Doug DC981SDR ASOA04477Panel · crackedDURING A C-CHECK IN MCN, THE LEFT WING LOWER AFT PANEL AT WS 148.019 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LT WING LOWER AFT PANEL AT WS 148.019 IAW ASA EO 600-57-0134. (M)Jul 1, 2004 · N844AS · Cndair CL6002B19SDR IXXA060448SSkin · wornDURING ROUTINE C CHECK, FOUND RIGHT WING SKIN WORN AT STATION XOLDO67. REPAIRED PER ALL APPLICABLE DATA.Jun 29, 2004 · N41CX · Doug DC862FSDR IXXA060440SSkin · corrodedDURING ROUTINE C CHECK, FOUND RIGHT WING SKIN CORRODED AT STATION XOLDI6.224. REPAIRED PER ALL APPLICABLE DATA.Jun 29, 2004 · N41CX · Doug DC862SDR IXXA060407SSkin · corrodedDURING ROUTINE C CHECK, FOUND LEFT WING LEADING EDGE LOWER SKIN CORRODED BETWEEN STATION XFS710 AND XFS635. REPAIRED PER ALL APPLICABLE DATA.Jun 29, 2004 · N41CX · Doug DC862FSDR IXXA060406SSkin · corrodedDURING ROUTINE C CHECK, FOUND LEFT WING LEADING EDGE SKIN CORRODED BETWEEN STATION XW257 AND XW223. REPAIRED PER ALL APPLICABLE DATA.Jun 29, 2004 · N41CX · Doug DC862FSDR IXXA060132SSkin · dentedDURING ROUTINE C CHECK, FOUND RIGHT WING DENTED AT STATION XFS-45 OUTBOARD OF LIFT ATTACH POINT. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGE. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED REPJun 29, 2004 · N605AL · Doug DC873FSDR IXXA060405SSkin · corrodedDURING ROUTINE C CHECK, FOUND LEFT WING UPPER SKIN CORRODED BETWEEN STATION XW0 AND XRS74. REPAIRED PER ALL APPLICABLE DATA.Jun 28, 2004 · N41CX · Doug DC862FSDR SIMA200417701Skin · crackedDURING ROUTINE MAINTENANCE, A CRACK WAS FOUND IN THE LEFT WING LOWER TRAILING EDGE SKIN. A DOUBLER REPAIR WAS COMPLETED IAW ENGINEERING ORDER EM 57MR-123R6. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Jun 22, 2004 · N624AE · Emb EMB145LRSDR A6WA200440089Access Door · corrodedRIGHT WING LOWER PLANK FUEL TANK ACCESS DOOR CUT OT AT WS 54.897 HAS FRETTING DAMAGE IN TWO AREAS, INBOARD AND FORWARD .004 IN CHES DEEP AT WORST AREA. REMOVED FRETTING CORROSION ON LOWER WING PLANK FUEL ACCESS DOOR IN THREE PLACES (.004 DEEP) WS 54.897 PANEL Jun 16, 2004 · N410AW · Cndair CL6002B19SDR USAA040304Skin · delaminatedPIT - FOUND WING DELAMINATION 1 SQUARE INCH, NR 3 SLAT INBOARD END TRAILING EDGE. REMOVED DAMAGE, INSTALLED FILLER INTERNAL DOUBLER AND NEW CORE AND TOP DOUBLER PER SRM 51-70-10. (M)Jun 15, 2004 · N575US · Boeing 737301SDR USAA040305Skin · delaminatedPIT - FOUND WING DELAMINATED 1.5 SQUARE INCH, TOP SURFACE AT OUTBOARD TRACK AREA TRAILING EDGE OF NR 3 SLAT. REMOVED DAMAGE. INSTALLED FILLER/CORE MATERIAL, INSTALLED TOP DOUBLER PER SRM 51-70-10. (M)Jun 15, 2004 · N575US · Boeing 737301SDR COMA0460371Skin · crackedLEFT LOWER WING PLANK CRACKED AT WS 148.019. COMPLIED WITH EO 57-020 REV A. MODIFICATIONS OF THE LEFT WING LOWER WING PLANK AT WS 148.Jun 15, 2004 · N962CA · Cndair CL6002B19SDR COMA0460373Skin · corrodedFRETTING DAMAGE NOTED ON RIGHT HAND WING LOWER ACCESS HOLE AT 650CB. BLENDED FRETTING AREAS OF RIGHT HAND ACCESS HOLE AT 650CB IAW REO 601R-57-21-030. ALODINED AND PRIMED IAW CRJ SRM 51-21-11. PERFORMED ELECTRICAL BOND CHECK ON FUEL PANEL 650CB IAW CRJ AMM Jun 15, 2004 · N962CA · Cndair CL6002B19SDR COMA0460374Skin · corrodedFRETTING DAMAGE NOTED ON RIGHT HAND WING LOWER ACCESS HOLE AT 650BB. BLENDED FRETTING AREAS OF RIGHT HAND ACCESS HOLE AT 650BB IAW REO 601R-57-21-030. ALODINED AND PRIMED IAW CRJ SRM 51-21-11. PERFORMED ELECTRICAL BOND CHECK ON FUEL PANEL 650BB IAW CRJ AMM Jun 15, 2004 · N962CA · Cndair CL6002B19SDR COMA0460375Skin · corrodedFRETTING DAMAGE NOTED ON RIGHT HAND WING LOWER ACCESS HOLE AT 650BB. BLENDED FRETTING AREAS OF RIGHT HAND ACCESS HOLE AT 650BB IAW REO 601R-57-21-030. ALODINED AND PRIMED IAW CRJ SRM 51-21-11. PERFORMED ELECTRICAL BOND CHECK ON FUEL PANED 650BB IAW CRJ AMM Jun 15, 2004 · N962CA · Cndair CL6002B19SDR COMA0460376Skin · corrodedFRETTING DAMAGE NOTED ON LEFT HAND WING PLANK LOWER ACCESS HOLE AT 550 CB. BLENDED FRETTING AREAS IAW 601R-57-21-030. ALODINED AND PRIMED IMW CRJ SRM 51-21-11. PERFORMED ELECTRICAL BOND CHECK ON PANEL 550 CB AMM 51-80-00. BOND CHECK GOOD.Jun 15, 2004 · N962CA · Cndair CL6002B19SDR COMA0460379Skin · corrodedFRETTING DAMAGE NOTED ON RIGHT HAND WING LOWER ACCESS HOLE AT 640FB. BLENDED FRETTING AREAS OF RIGHT HAND ACCESS HOLE AT 640FB IAW REO 601R-57-21-030. ALODINED AND PRIMED IAW CRJ SRM 51-21-11. PERFORMED ELECTRICAL BOND CHECK ON FUEL PANEL 640FB IAW CRJ AMM Jun 15, 2004 · N962CA · Cndair CL6002B19SDR UPS04842747Doubler · corrodedINSPECTION TYPE: C-3, RT WING L/E CENTER SECTION HAS CORROSION AROUND STALL WARNING SWITCH AND NUT PLATES. BASE DOUBLER FOR STALL WARNING SWITCH IS FOUND TO BE OUT OF LIMITS IAW DC8 SRM 57-2-0. MAT ID 7075-T6 .063 PO 442960.4 FOR FAB OF NEW DOUBLER IAW DAC DJun 14, 2004 · N803UP · Doug DC873FSDR A6WA200460023Skin · damagedFOUND LEFT INBOARD LEADING EDGE HAS WEAR DAMAGE OT THE INBOARD LEADING EDGE WHERE THE STALL BAR ATTACHES. MAINTENANCE REQUESTED REPAIRS FROM BAE SYSTEMS REF AVMAX FAX 612-190-006. (M)Jun 14, 2004 · N612AW · Bac 146300A
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