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 FDEA201405110978Doubler · crackedLEFT WING FIXED LE BEADED DOUBLER AT XOS 664 FOUND CRACKED DURING OTBD SLAT DRIVE CABLE INSPECTION. REPAIRED IAW SRM 57-40-02, FIGURE 203, REPAIR 15, REVISION 55. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 121.May 11, 2014 · N623FE · Doug MD11FSDR SWIA201437687Skin · crackedCRACK FOUND IN COLD WORK OF LT WING PLANK. REAMED AND COLD WORKED DISCREPANT HOLE. INSTALLED HST54AG-14-22 IAW REO.May 11, 2014 · N793SK · Cndair CL6002C10SDR FDEA201405110980Skin · crackedDURING WALK AROUND FOUND SUSPECTED CRACK IN RT WING AROUND SLAT DRIVE MECHANISM ACCESS DOOR. HFEC INSPECTED CRACK INDICATED IAW SOPM 20-30-00. REMOVED DAMAGE IAW SRM 57-40-02 REPAIR 7. PERFORMED HFEC OF CUT OUT AREA ON RT WING TO ENSURE CRACK REMOVAL IAW NTMay 11, 2014 · N582FE · Doug MD11FSDR FDEA201405110979Skin · crackedON WALK AROUND FOUND RT WING CRACK INBD FWD EDGE OF SLAT ACTUATOR DOOR. REMOVED DAMAGED SKIN IAW SRM CH 57-10-00. THIS RII IS FOR THE DAMAGED SKIN CUT OUT RII 263280. PERFORMED HFEC OF CUT OUT AREA TO ENSURE CRACK REMOVAL IAW NTM PT6, NO CRACKS NOTED. FABMay 11, 2014 · N570FE · Doug MD1010FSDR QXEA2014051500402Access Panel · corrodedFUEL TANK PANEL, 622BT HAS CORROSION/PITTING IN FASTENER HOLES MULTIPLE LOCATIONS. REWORKED 622BT FASTENER HOLES FOUND TO BE OUT OF LIMITS, REF SRM 57-10-35 6A (A) (2) PG 203. COMPLETED M-184. ORDERED /RECEIVED NEW PANEL 622BT, PANEL INSTALLED ON 5403735/505May 10, 2014 · N403QX · Bombdr DHC8402SDR FDEA201405090967Skin · crackedSUSPECT CRACK RT WING LE OF SLAT DRIVE ACCESS DOOR. HFEC VERIFIED CRACK IAW NTM 06-10-01. REMOVED PANELS 618FB 618EB & RT WEB PANEL INSIDE 618FB PN ARB1138-4 TO FOM FOR SHEET METAL REPAIR. REMOVED EXISTING FASTENERS TO ACCOMMODATE REPAIR DOUBLER IAW SRM 51-May 9, 2014 · N399FE · Doug MD1010FSDR SWAA2014060228590Skin · crackedLEFT WING LE SKIN CRACKED AT WBL 213. REPAIRED SKIN IAW EA.May 8, 2014 · N640SW · Boeing 7373H4SDR FDEA201405081043Skin · crackedRT WING SLAT DRIVE DOOR CUT OUT HAS 2 INCH CRACK INBD, APPEARS TO EXTEND TO RIVET. INSTALLED REPAIR DOUBLER IAW SRM 57-10-00 & EA 8-5710-T0308126.May 8, 2014 · N398FE · Doug MD1010FSDR ASOA2014052710598Skin · crackedLEFT FUEL ACCESS HOLE 550HB HAS MULTIPLE INDICATIONS ON INBD, FWD & AFT SIDE 50 PERCENT FSH, FAILED NDT. C/W ECTC EO 600-57-81 C/W IAW REO 601R-57-21-030, REV L.May 7, 2014 · N880AS · Cndair CL6002B19SDR DXTA2014051405771Skin · corrodedREPAIR OF LOWER WING SKIN CORROSION. REPAIRED IAW CESSNA S750-0224 11RD.May 7, 2014 · N919QS · Cessna 750SDR GTIA2014050701296Skin · corrodedDURING PHASED ARRAY INSPECTION, CORROSION FOUND ON RT WING TOP SKIN LWR SURFACE AT RIB 14. REMOVED CORROSION IAW SRM 51-74-00. FOUND WITHIN ALLOWABLE LIMITS IAW SRM 57-21-11. RESTORED FINISH IAW SRM 51-75-11.May 7, 2014 · N525NK · Airbus A319132SDR GTIA2014050701295Skin · corrodedDURING PHASED ARRAY INSPECTION, CORROSION FOUND ON LT WING T/E LWR SURFACE INBD RIB 15. REMOVED CORROSION IAW SRM 51-74-00. FOUND WITHIN ALLOWABLE LIMITS IAW SRM 57-21-11. RESTORED FINISH IAW SRM 51-75-11.May 7, 2014 · N525NK · Airbus A319132SDR GTIA2014050701294Skin · corrodedDURING PHASED ARRAY INSPECTION, CORROSION FOUND ON RT WING TOP SKIN T/E LOWER SURFACE BETWEEN RIBS-11-12. REMOVED CORROSION IAW SRM 51-74-00. FOUND WITHIN ALLOWABLE LIMITS IAW SRM 57-21-11.May 7, 2014 · N525NK · Airbus A319132SDR GTIA2014050701293Skin · corrodedDURING PHASE ARRAY INSPECTION, CORROSION FOUND ON RT WING TOP SKIN T/E LOWER SURFACE BETWEEN RIBS-14-15. REMOVED CORROSION IAW SRM 51-74-00. WITHIN LIMITS IAW SRM 57-21-11.May 7, 2014 · N525NK · Airbus A319132SDR GTIA2014050701292Skin · corrodedDURING PHASE CHECK ARRAY INSPECTION OF LT WING, FOUND CORROSION AT TOP SKIN T/E IR SURFACE JUST OTBD IR RIB 14.May 7, 2014 · N525NK · Airbus A319132SDR FDEA201405060963Skin · crackedON POST FLIGHT WALK AROUND FOUND CRACK LT WING SLAT TRACK CUT OUT OTBD OF REFUELING PANEL. COMPLIED WITH HFEC INSPECTION & VERIFIED CRACK TO BE 1.1" IN LENGTH. REMOVED PANEL 579DB FOM & PLACED IN CREW AREA. IAW SRM MD10 57-10-00 MATERIAL ID 6AL4V .063 TITMay 6, 2014 · N372FE · Doug MD1010FSDR QXEA2014051500401Access Panel · corrodedFUEL TANK PANEL 622CT HAS CORROSION/PITTING IN THE FASTENER HOLES IN MULTIPLE LOCATIONS. EVALUATE FUEL PANEL 622CT. REWORKED FASTENER HOLES ON 622CT, FOUND TO BE OUT OF LIMITS, REF SRM 57-10-35 6.A (1) AND (2) PAGE 2 OF 3. COMPLIED WITH M-184. PANEL 622CT REMay 6, 2014 · N403QX · Bombdr DHC8402SDR ASOA2014052710596Skin · crackedRT BOOST PUMP CUTOUT HAS MULTIPLE INDICATIONS ALL AROUND THE VERTICAL & HORIZONTAL LANDING 50 PERCENT FSH FAILED NDT. BLENDED RT WING LOWER SKIN PLANK AT BOOST PUMP LANDING IAW STS EA 26-2014-050.May 5, 2014 · N880AS · Cndair CL6002B19SDR FDEA201405050950Skin · crackedDURING WALK AROUND, RT WING FWD INBD CORNER OF SLAT DRIVE MECHANISM ACCESS DOOR APPEARS TO HAVE AN 1.5 INCH CRACK IN FIXED PANEL SKIN. INSTALLED DOUBLER REPAIR IAW SRM.May 5, 2014 · N318FE · Doug MD1030FSDR UIEA2014050500167Skin · corrodedBULGE SKIN, UPPER SURFACE OF RT WING LE UPPER FIXED PANEL, ILES 822.50. REPAIRED CORROSION AREA IAW EI NO T2014A57B-1401 REV 0.May 5, 2014 · N464MC · Boeing 747446SDR UIEA2014050500165Strap · bulgedBULGE SKIN UPPER SURFACE OF RT WING LE UPPER FIXED PANEL ILES 630.72. REPLACED WITH NEW STRAP IAW SRM 51-40-02 REV 89.May 5, 2014 · N464MC · Boeing 747446SDR ERAA20140026Access Panel · corrodedDURING C CHECK FOUND RT WING FUEL PANEL 624CT, TWO HOLES CORRODED REPAIRED IAW DWG.May 5, 2014 · N889EA · Dhav DHC8106SDR ERAA20140025Access Panel · corrodedDURING C CHECK FOUND LT WING FUEL PANEL 524AT, TWO HOLES CORRODED, REPAIRED IAW DWG.May 5, 2014 · N889EA · Dhav DHC8106SDR FDEA201405040951Skin · crackedDURING WALK AROUND, FOUND LE CRACK AT RT WING FUELING PANEL INBD SIDE. INSTALLED DOUBLER REPAIR IAW SRM.May 4, 2014 · N363FE · Doug MD1010FSDR ASOA2014051510499Skin · corrodedLT WING ACCESS PANEL LANDING CORRODED AT 510AB. COMPLIED WITH REO 601R-57-21-030 AND ECTC EO 600-57-81.May 3, 2014 · N852AS · Cndair CL6002B19SDR ASOA2014051510498Skin · corrodedLT WING ACCESS PANEL LANDING CORRODED AT 540BB. COMPLIED WITH REO 601R-57-21-030 AND EO 600-57-81 AND REF AMM 28-11-01-400-801.May 3, 2014 · N852AS · Cndair CL6002B19SDR ASOA2014051510497Skin · corrodedACCESS PANEL LANDING, CORRODED AT 640AB RT WING. COMPLIED WITH REO 601R-57-21-030 AND EO 600-57-81.May 3, 2014 · N852AS · Cndair CL6002B19SDR FDEA201405030936Skin · crackedFOUND CRACK ON RT WING FWD OF SLAT DRIVE DOOR. TRIMMED OUT CRACK AREA, FABRICATED FILLER & LOCATED FASTENER HOLES IAW SRM 57-10-00.May 3, 2014 · N319FE · Doug MD1030FSDR DALA14028040958Access Panel · corrodedCORROSION ON RT FUEL TANK ACCESS PLATE NR 1460C AT COUNTERSINK AREA, MRB 57-083-02, REF 20000005843, CORROSION ON COUNTERSINK WAS REMOVED AND MAXIMUM DIAMETER ALLOWABLE IS 0.532" AND WERE FOUND 4 COUNTERSINK ADJACENT OUT OF LIMITS MEASURED 0.545", 0.570", 0May 2, 2014 · N958DL · Doug MD88SDR CALA2014050500554Access Panel · wornPANEL 192 DR FWD OTBD LATCH STRIKE AREA WORN, HOLE IN STRIKE AREA, ACCESS PANEL ON RT ACFT BAY DOOR. INSTALLED INTERIM REPAIR ON CHORD IAW ECRA 5713-01025 & CREATED DIP WITH THIS LP FOR PART 2 OF INSPECTION REQUIREMENT OF ECRA 5713-01025. INSTALLED INTERIM RMay 2, 2014 · N18243 · Boeing 737824SDR ASOA2014052310579Skin · crackedLT LOWER WING PLANK CRACKED APP 1" AT 148.019. COMPLIED WITH ECTC REO 601R-57-21-130 AND GREO 601R-57-21-130, REV K.May 1, 2014 · N880AS · Cndair CL6002B19SDR ABXA20140430159Skin Panel · corrodedUPPER WING SURFACE PANEL SEPARATING ON LE JUST FWD OF NR 10 SPOILER, UPPER SURFACE OF THE WING. REMOVED TE WING PANEL TO FOM CORROSION ON WING SKIN IAW SRM 57-20-01 FIG 01 IAW REA B657-60934-MR. CORRODED LEVEL 2, PN 112T3101-6, PART NAME UPPER SKIN, SN N/A, Apr 30, 2014 · N747AX · Boeing 767232SDR VNAA2014043000024Skin · chafedDURING SCHEDULED MAINTENANCE, THE RIGHT AFT LOWER WING PLANK WAS CHAFED. THE AREA WAS INSPECTED AND REPAIRED USING AMM. ACFT WAS RELEASED FOR SERVICE.Apr 30, 2014 · N245PS · Cndair CL6002B19SDR DALA14027230964Access Panel · corrodedCORROSION ON COUNTERSINK OF FUEL TANK ACCESS PANEL 1414C. CORROSION REMOVED IAW SRM 51-22-2A AND FOUND OUT OF LIMITS IAW SRM 51-22-2A. ACCESS PANEL REPLACED.Apr 30, 2014 · N964DL · Doug MD88SDR USAA2014060200024Access Panel · corrodedS2 CHECK LEVEL 2 FRETTING CORROSION ON LT WING LOWER FUEL PANEL 540KB BETWEEN RIB 15 TO 16 & BETWEEN STRINGER 8L TO 11L. REPLACED LT WING LOWER FUEL PANEL 540KB IAW SRM 57-27-11.Apr 29, 2014 · N188US · Airbus A321211SDR SWAA2014053028508Access Panel · crackedRIGHT WING NR 7 SLAT ACCESS PANEL 624DB CRACKED AT INBD LOWER FASTENER HOLE. R & R PANEL IAW SRM & DWG.Apr 29, 2014 · N717SA · Boeing 7377H4SDR FDEA201404290889Skin · crackedDURING WALK AROUND, FOUND ACRACK ON RT WING LE SKIN AT FWD LT CORNER OF FUELING PANEL. PERFORMED HFEC OF SUSPECT AREA, VERIFIED CRACK & IAW NTM PT6 20-30-00. REMOVED CRACK DAMAGE IAW SRM 57-10-00 FIG 68. INSTALLED REPAIR DOUBLER & COMPLIED WITH EA 8-5730Apr 29, 2014 · N308FE · Doug MD1030FSDR USAA2014050700003Access Panel · corroded2S CHECK LT WING FUEL ACCESS PANEL 550BB CORRODED AT FASTENER HOLES. R & R ACCESS PANEL IAW SRM 57-27-11.Apr 29, 2014 · N188US · Airbus A321211SDR REXA2014050300083Skin · corrodedLEFT WING PLANK ACCESS HOLE FOR PANEL 540BB AT WS 54.897 HAS FRETTING CORROSION MEASURING 0.002" DEEP. REPAIRED IAW GREO 601R-57-21-030.Apr 29, 2014 · N8883E · Cndair CL6002B19SDR ASOA2014052110541Skin · crackedDURING EDDY CURRENT INSPECTION OF LT WING LOWER PLANK AND TRUMION HOLES CRACK INDICATIONS IN 1EA FASTENER HOLE. REPAIRED IAW REO 670-57-21-694, REV P2.Apr 28, 2014 · N608QX · Cndair CL6002C10SDR SWIA201437575Skin · corrodedRIGHT WING LOWER WING PLANK ACCESS HOLE, 640BB HAS FRETTING. C-CHECK, BLENDED DAMAGED IN 3EA LOCATIONS REF REO.Apr 28, 2014 · N779CA · Cndair CL6002B19SDR SWIA201437574Skin · corrodedLEFT WING LOWER WING PLANK ACCESS HOLE, 540BB, HAS FRETTING. C-CHECK, BLENDED DAMAGED IN 3 EA LOCATIONS REF REO.Apr 28, 2014 · N779CA · Cndair CL6002B19SDR CALA2014043090928Access Panel · leakingSUBSTANTIAL FUEL LEAK AT RT WING AT UNDETERMINED LOCATION. ISOLATED LEAK TO RT WING SURGE TANK ACCESS PANEL. REMOVED PANEL, CLEANED GASKET & SEAL. REPLACED ALL PANEL BOLTS & CLOSED PANEL IAW MM28-11-03.Apr 28, 2014 · N654UA · Boeing 767322SDR DALA14028805641Skin · corrodedLEFT WING UPPER INBD SURFACE, IN THE WING WALK AREA NUMEROUS AREAS OF CORROSION. WS 70.5-W.S 150 FROM SKIN SPLICE TO REAR SPAR. REMOVED CORROSION, PERFORMED DVI HFEC OF REWORKED AREA & FASTENERS HOLES, PENETRANT INSP. NO DEFECTS NOTED. FLAP, TOP COATED WORKEApr 27, 2014 · N541US · Boeing 757251SDR SWIA201437578Skin · crackedCRACK ON LT WING PLANK, C-CHECK, REPAIRED CRACK ON LT WING PLANK REF REO.Apr 26, 2014 · N779CA · Cndair CL6002B19SDR VNAA2014042600018Skin · dentedCREW REPORTED BIRD STRIKE TO MIDDLE L/E OF LT WING DURING CLIMBOUT. CREW LANDED AT DESTINATION WITHOUT INCIDENT. MAINTENANCE INSPECTED AND PERFORMED REPAIR FOR DENT ON LT WING L/E SKIN IAW AMM AND REO. ACFT RELEASED FOR SERVICE.Apr 26, 2014 · N207PS · Cndair CL6002B19SDR DALA2016111008668Access Panel · corrodedRT WING FUEL TANK ACCESS PANEL 1460 CORRDED. REPLACED THE ACCESS PANEL.Apr 25, 2014 · N958DL · Doug MD88SDR DXTA2014051405772Skin · corrodedREPAIR OF LT & RT LWR WING SKIN CORROSION. REPAIRED IAW CESSNA S-750-0193 13RD.Apr 25, 2014 · N939QS · Cessna 750SDR SWIA201437482Skin · corrodedFUEL ACCESS PANEL ON LT LOWER WING PLANK UNDER PANEL 550GB HAS CORROSION. C-CHECK, REMOVED CORROSION UNDER PANEL 550GB ON WING PLANK IAW REO.Apr 25, 2014 · N629BR · Cndair CL6002B19SDR SWIA201437481Skin · corrodedFUEL ACCESS PANEL ON LT LOWER WING PLANK UNDER PANEL 550DB HAS CORROSION. C-CHECK, REMOVED CORROSION UNDER PANEL 550DB ON WING PLANK IAW REO.Apr 25, 2014 · N629BR · Cndair CL6002B19
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