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 FDEA200911043833Skin · corrodedRT WING LWR SKIN NEAR ROOT AT APPROX RBL71.0 IN BETWEEN WING LWR STR STA L13 AND L14 WITH CORROSION. CORROSION ON RT WING LWR SKIN AT APPROX RBL 71.0 REPAIRED IAW EA NR F-5710-133422 (TITLE: SEVERAL AREAS OF CORROSION ON RT CTR WING LWR SKIN). REPAIR IS CLASNov 4, 2009 · N934FD · Boeing 75721BSDR ZZDA2009333Rub Strip · corrodedRIGHT WING ACCESS PANEL 620CT RUB STRIP, CORROSION. ACCOMPLISHED WING ACCESS PANEL 620CT RUB STRIP REPLACEMENT REPAIR PER B717 SRM 51-41-02 AND B717 SRM 57-10-01. SEE NR 2674.Nov 3, 2009 · N950AT · Boeing 717200SDR WRLA20091101282Stiffener · crackedCRACK - STIFFENER OF PANEL 616ET RT WING L/E UPPER SURFACE, 1 PLACE AT XW 297. REPAIRED CRACK AREA IAW MD11 SRM 57-40-02 FIG 201 REV 41.Nov 1, 2009 · N274WA · Doug MD11FSDR WRLA20091101276Stiffener · crackedCRACK - ZEE STIFFENER OF LEFT WING FIXED L/E UPPER PNL 516ET QTY = 1EA AT XW 303. REPAIRED CRACK AREA IAW MD11 SRM 57-40-02 REV 41.Nov 1, 2009 · N274WA · Doug MD11FSDR WRLA20091101272Stiffener · crackedCRACK - STIFFENER OF PNL 616ET AT RT WING UPPER SURFACE 1 PLACE AT XW 291. REPAIRED CRACK AREA IAW MD11 SRM 57-40-02 FIG 201 REV 41.Nov 1, 2009 · N274WA · Doug MD11FSDR WRLA20091101271Stiffener · crackedCRACK - ZEE STIFFENER OF LT WING FIXED L/E UPPER PNL 516ET 1 EA AT XW291. REPAIRED CRACK AREA IAW MD11 SRM 57-40-02 FIG 201 REV 41.Nov 1, 2009 · N274WA · Doug MD11FSDR WRLA20091101270Stiffener · crackedCRACK - ZEE STIFFENER OF LT WING FIXED L/E UPPER PNL 516ET 1 EA AT XW 297. REPAIRED CRACK AREA IAW MD11 SRM 57-40-02 FIG 201 REV 41.Nov 1, 2009 · N274WA · Doug MD11FSDR WRLA20091101269Stiffener · crackedCRACK - STIFFENER OF PNL 616ET AT RT WING UPPER SURFACE 1 PLACE AT XW 327. REPAIRED CRACK AREA IAW MD11 SRM 57-40-02 FIG 201 REV 41.Nov 1, 2009 · N274WA · Doug MD11FSDR IPXA09657851Skin · crackedINSPECTION TYPE:ETOP LHW NR 4 SLAT OTBD NOSE SUPPORT WEB SKIN RIVET HOLE FOUND CRACKED LHW NR 4 SLAT OTBD AREA AT OSS641.6 NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 ORG MAT'L IS CLAD7075T6-0063IN, CRACK LENGTH IS 0.125 INCH DAMAGED CUTOUT IS 7.735 INCNov 1, 2009 · N324UP · Boeing 76734AFSDR EIAA200900119Skin · corrodedRT WING LEADING EDGE CAVITY LWR SKIN "PAD UP" AT LES 1291 HAS CORROSION. REMOVED CORROSION, FABBED AND INSTALLED REPAIR PER ECRA 486-57-074-2 REV A.Oct 29, 2009 · N486EV · Boeing 747212BSDR GUUA93957102609ASkin · delaminatedDURING SCHEDULED ROUTINE INSP, DISCOVERED LT WING SKIN DELAMINATED AROUND FUEL PANEL 532 EB. OPENOct 26, 2009 · N82539 · Beech 1900DSDR GUUA93957102509BSkin · delaminatedDURING SCHEDULED ROUTINE INSPECTION DISCOVERED RIGHT WING LOWER SKIN DELAMINATED AROUND FUEL PANEL 631DB. REPAIRED RIGHT WING LOWER SKIN AROUND FUEL ACCESS PANEL 631DB.Oct 25, 2009 · N82539 · Beech 1900DSDR GUUA93957102509ASkin · delaminatedDURING SCHEDULED ROUTINE INSPECTION DISCOVERED LEFT WING LOWER SKIN DELAMINATED AROUND FUEL PANEL 531DB. REPAIRED LEFT WING LOWER SKIN AROUND FUEL ACCESS PANEL 531DB.Oct 25, 2009 · N82539 · Beech 1900DSDR FDEA200910243658Skin · corrodedCABIN - CENTER WING TANK UPPER SURFACE SKIN AT STA 1227, X = -73 TO X = -79 FOUND CORROSION. REPAIR CARRIED OUT AS PER E.A. 1-5710-132250, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 108.Oct 24, 2009 · N590FE · Doug MD11FSDR FDEA200910243656Skin · crackedRIGHT HAND WING - WING LEADING EDGE SKIN AT ANTI-ICE TELESCOPIC DUCT UPPER CUTOUT INBOARD AFT FOUND CRACKED (APPROXIMATELY 0.5"). CRACKED SKIN AT RIGHT HAND WING LEADING EDGE SKIN AT ANTI-ICE TELESCOPIC DUCT UPPER CUTOUT INBOARD AFT REPAIR CARRIED OUT AS Oct 24, 2009 · N590FE · Doug MD11FSDR WRLA20091023256Skin Panel · corrodedCORROSION WAS FOUND ON FIXED L/E OF LT WING NEAR PNL 518CB. PERFORM EI W2009A57B-1425 REV 00 REPAIR CORROSION ON LT WING FIXED LEADING EDGE SKIN PANEL AT XOS 464.00. COND CHECK NORMAL AND JOB COMPLETED.Oct 23, 2009 · N274WA · Doug MD11FSDR GUUA94057102309ASpar · damagedDURING BELLY SKIN REPAIR, DISCOVERED RT MAIN SPAR LWR FLANGE HAS 2 ELONGATED FASTENER HOLES AT FS288.00. COLD WORK FASTENER HOLES AND INSTALLED BLIND FASTENERS. PREVIOUSLY SUBMITTED OPEN UNDER CONTROL NR GUUA94053102309A UPDATED TO GUUA94057102309AOct 23, 2009 · N16540 · Beech 1900DSDR A6WA200940726Access Panel · damagedRT WING L/E ACCESS PANEL ABOVE LANDING LIGHT BTW W/S 50.54 TO W/S 66.20 FOUND DENTED. RT WING L/E ACCESS PANEL ABOVE LANDING LIGHT BTW W/S 50.54 TO W/S 66.20. REPLACED IAW SRM 51-40-1 SRM 51-40-1 AND SRM 51-24-36. (K)Oct 21, 2009 · N469AW · Cndair CL6002B19SDR CA091022006Skin · dented(CAN) THE STUDENT PILOT WAS CARRYING OUT THE PREFLIGHT INSPECTION OF THE ACFT & NOTED SEVERAL INDENTATIONS ON UPPER SKIN ON THE RT WING. FURTHER INSPECTION BY MX BY "TAP TESTING" REVEALED THE EXTENT OF THE DELAMINATION. OUTBOARD EDGE OF OUTBOARD DELAMINATION Oct 21, 2009 · Grob G120ASDR SIMA200929501Skin · dentedDURING MAINTENANCE CHECK IN ABI, THE AIRCRAFT FELL OFF JACK DENTING WING. ENTERED TIME DEFERRED MAINTENANCE ITEM TO PERFORM PERMANENT REPAIR OF LEFT LOWER WING SKIN ON OR BEFORE 250 FLIGHT CYCLES IAW EO EM-5700-425 PART C. AIRCRAFT REMOVED FROM SERVICE. PEROct 21, 2009 · N711PH · Emb EMB135LRSDR UIEA201000130Skin · delaminatedDURING LETTER "A" CHECK IN MIA, DELAMINATION WAS FOUND ON THE LEFT WING TRAILING EDGE AT WBL 208 UPPER EXTERNAL SKIN, RT LEADING EDGE ILES 760 UPPER EXTERNAL SKIN, AND RT LEADING EDGE ILES 672 GAP PANEL. ENGINEERING ORDER 4757A490 DATED 20 OCT 2009 WAS ISSUEDOct 20, 2009 · N524MC · Boeing 7472D7BSDR CA091022001Screw · wrong part(CAN) FUEL PANELS HAD BEEN OPEN FOR MAINTENANCE, WHEN IT CAME TIME FOR RE-TORQUE OF THE SCREWS, THE SCREWS BOTTOMED OUT, AS THEY WERE THE WRONG LENGTH. MAINTENANCE CONTRACTOR HAS BEEN ADVISED. PROPER SCREWS HAVE BEEN INSTALLED (TC 20091022001)Oct 20, 2009 · Boeing 737275CSDR A6WA200940724Skin · gougedLT WING LWR PLANK ACCESS HOLE CUT OUT 540DB VERTICAL SURFACE FOUND GOUGED (.100 X .005" W X .008 DEEP APPROX). LT WING LWR PLANK ACCESS HOLE CUTO OUT 540DB VERTICAL SURFACE REPAIR C/O IAW EO NR E06/021/457. (K)Oct 16, 2009 · N469AW · Cndair CL6002B19SDR A6WA200940725Skin · gougedLT WING LOWER PLANK ACCESS HOLE CUT OUT 540FB VERTICAL SURFACE FOUND GOUGED (.100L X .005" W X .006" DEEP). LT WING LWR PLANK ACCESS HOLE CUT OUT 540FB VERTICAL SURFACE REPAIR C/O IAW EO E06/021/457. (K)Oct 14, 2009 · N469AW · Cndair CL6002B19SDR A6WA200940723Skin · corrodedLT WING LOWER PLANK ACCESS HOLE CUT OUT 540BB LOWER SURFACE CORRODED. LT WING LOWER SURFACE PLANK ACCESS HOLE CUT OUT 540BB LOWER SURFACE REPAIR C/O IAW E06/021/457. (K)Oct 14, 2009 · N469AW · Cndair CL6002B19SDR VNAA2009102100008Panel · damagedCREW REPORTED A BIRD STRIKE ABOVE THE RT WING LANDING LIGHT LENS AT MOB. EVIDENCE OF BIRD STRIKE DEBRIS ENTERING THE COWLING ON THE RT ENGINE WAS ALSO REPORTED. MAINTENANCE INSPECTED AND REWORKED THE DENTED RT WING LEADING EDGE PANEL IAW REO 601R-57-41-629. Oct 14, 2009 · N250PS · Cndair CL6002B19SDR TRBACPCP20090021Skin · corrodedFOUND CORROSION SPOT ON LOWER SKIN OF LEFT WING AROUND RIB 13 AND TRAILING EDGE 531BB. PERFORMED BLENDING IAW SRM 51-21-58 AND EO NR E2-57MR-347.Oct 14, 2009 · N426AT · Aerosp ATR72212SDR FDEA200910133548Skin · cracked02 EACH FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSP AT LT WING LWR SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS = 690 AND STA XORS = 700. REPAIR CARRIED OUT IAW EA NR 1-5710-133896, TITLE: A.D. 2007-07-04 - WINGS - LT LWR SKIN PLANK CUT OUTOct 13, 2009 · N584FE · Doug MD11FSDR IPXA09M57788Doubler · crackedINSPECTION TYPE:2C RIGHT WING BEADED DOUBLER BETWEEN STA XOS 698 AND STA XOS 703 12" INB OF # 11 SLAT COMMON IDLER TRACK CRACKED REMOVE DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER, FILLER, AND ANGLES IAW MD-11 SRM 57-40-02 REPAIR 9 FIG. 203Oct 10, 2009 · N287UP · Doug MD11FSDR 2009FA0000839Skin · corrodedUPON REMOVAL OF THE LEFT SIDE UNDER-WING (RIVETED ON) AFT EXHAUST FAIRING WHILE PERFORMING SID 20000 CYCLES/8100 LANDINGS INSPECTION, AN AREA OF MODERATE TO SEVERE EXFOLIATION CORROSION WAS DISCOVERED ON THE WING SKIN UNDERNEATH THE EXHAUST FAIRING. THIS CORROOct 10, 2009 · N969BW · Casa C212SDR IPXA09M57789Skin · crackedINSPECTION TYPE:2C LT WING L/E UPPER SKIN WEB IS CRACKED AT 2 PLACES BETWEEN XOS 759 AND STA XOS 768 UPPER RIBS REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER, DOUBLER, AND ANGLES IAW 57-40-02 REPAIR 9 FIG. 203Oct 9, 2009 · N287UP · Doug MD11FSDR IPXA09M57787Skin · crackedINSPECTION TYPE:2C L/H WING L/E UPPER SKIN WEB IS CRACKED ACROSS 2 RIVETS BETWEEN XOS 698 AND STA XOS 703 REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER, DOUBLER, AND ANGLES IAW MD-11 SRM 57-40-02 REPAIR 9 FIG. 203Oct 9, 2009 · N287UP · Doug MD11FSDR IPXA09M57786Skin · crackedINSPECTION TYPE:2C LH WING L/E UPPER SKIN WEB IS CRACKED AT 2 RIVETS BETWEEN STA XOS 692 AND STA XOS 698 REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER, FILLER, AND ANGLES IAW MD-11 SRM 57-40-02 REPAIR 9 FIG. 203Oct 9, 2009 · N287UP · Doug MD11FSDR IPXA09M57785Doubler · crackedINSPECTION TYPE:2C LEFT WING BEADED DOUBLER BETWEEN STA. XOS 616 AND XOS 610 IS CRACKED AROUND FASTNERS REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER, DOUBLER, AND ANGLES IAW MD-11 SRM 57-40-02 REPAIR 9, FIG. 203Oct 9, 2009 · N287UP · Doug MD11FSDR IPXA09M57783Doubler · crackedINSPECTION TYPE:2C LEFT WING BEADED DOUBLER AT STA XOS 621.69 TO XOS 625.56 CRACKED AROUND FASTNEER REMOVED DAMAGE, FABRICATED, AND INSTALLED REPAIR DOUBLER, FILLER, AND ANGLES IAW MD-11 SRM 57-40-02 REPAIR 9 FIG. 203Oct 9, 2009 · N287UP · Doug MD11FSDR IPXA09M57782Doubler · crackedINSPECTION TYPE:2C LEFT WING BEADED DOUBLER AT STA XOS 625.56 TO XOS 629.62 CRACKED AROUND FASTNERS REMOVED DAMAGE, FABRICATED, AND INSTALLED REPAIR DOUBLER, ANGLES, AND FILLER IAW MD-11 SRM 57-40-02 REPAIR 9 FIGURE 205Oct 9, 2009 · N287UP · Doug MD11FSDR FDEA200910093522Skin · corrodedRT WING UPPER SURFACE FOUND CORROSION AT XORS 97 AFT OF FWD EDGE 6 INCHES. REPAIRED AS PER E.A. NR 1-5710-132239, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 108.Oct 9, 2009 · N619FE · Doug MD11FSDR IPXA09M57849Doubler · gougedINSPECTION TYPE:2C REPAIR SURVEY SEQ NR 287-W3-03 LT WING LT WING FIXED LE APPROX BETWEEN STA XIS 237-256 EXISTING DOUBLER GOUGED. REMOVED EXISTING REPAIR AT LT WING FIXED LE UPPER SKIN BETWEEN XIS 237 AND XIS 256 FORWARD OF FRONT SPAR. FABRICATED AND INSTALOct 8, 2009 · N287UP · Doug MD11FSDR IPXA09M57842Skin · misrepairedINSPECTION TYPE:2C REPAIR SURVEY SEQUENCE NR 287-W4-04 RT WING FIXED LE LOWER SKIN XOS 879-901 HAS EXISTING REPAIR THAT DOES NOT CORRELATE TO SRM 57-40-02 FIG 201 SHEET 1 AND 3. REMOVED REPAIR, FABRICATED AND INSTALLED REPAIR IAW MD-11 SRM 57-40-02 REPAIR 7 FOct 8, 2009 · N287UP · Doug MD11FSDR IPXA09M57790Skin · gougedINSPECTION TYPE:2C REPAIR SURVEY SEQUENCE 287-W4-05 RT WING BTWN STA XOS 458-475 EXISTING REPAIR DOUBLER GOUGED. REMOVED EXISTING DOUBLER, REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW 57-40-01 FIG. 201 REPAIR 10Oct 8, 2009 · N287UP · Doug MD11FSDR IPXA09M57784Skin · crackedINSPECTION TYPE:4C LT WING L/E UPPER SKIN WEB IS CRACKED AT STA 524 ACROSS 5 RIVETS REMOVED DAMAGE, FABRICATED AND INSTALLED, REPAIR FILLER, DOUBLER, AND ANGLES IAW MD-11 SRM 57-40-02 REPAIR 9 FIG. 203 SHT. 1-4Oct 8, 2009 · N287UP · Doug MD11FSDR FDEA200910083509Skin · crackedRT WING LWR SKIN CUTOUT FOR PANEL 675 FB: APPROX 1/8" (0.125") CRACK IN SKIN, BEGINNING AT FWD ROW OTBD HOLE (POS G), HOLE COMMON TO DOOR SURROUND ITEM (2) AS SHOWN IN FIG 1, PROTRUDING AFT FROM HOLE APPROX 5 O-CLOCK (VIEWED LOOKING FWD AND DOWN). CRACK DOOct 8, 2009 · N659FE · Airbus A300F4605RSDR FDEA200910083508Skin · crackedLT WING LWR SKIN CUTOUT FOR PANEL 575 FB: APPROX 3/16 " (0.187") CRACK ON LWR WING SKIN, FWD EDGE OF PANEL CUTOUT, BEGINNING AT THE OUTBD HOLE (POS G), HOLE COMMON TO DOOR SURROUND ITEM (2) AS SHOWN IN FIGS 1,2 AND 3, PROTRUDING AFT APPROX 5 O-CLOCK DIREOct 8, 2009 · N659FE · Airbus A300F4605RSDR SWAA096404Skin · crackedDURING SCHEDULED SPV CHECK, FOUND RT WING LOWER SKIN CRACKED. REPAIRED SKIN PER SRM.Oct 7, 2009 · N335SW · Boeing 7373H4SDR SWAA096378ASkin · crackedDURING SCHEDULED SPV CHECK, FOUND RT WING LOWER SKIN CRACKED. REPAIRED SKIN PER SRM.Oct 7, 2009 · N335SW · Boeing 7373H4SDR IPXA09557702Skin · crackedINSPECTION TYPE:C LT WING FIXED LEADING EDGE SKIN AT FSS 436 HAS CRACK ACCOMPLISHED PERMANENT REPAIR OF FIXED LEADING EDGE SKIN IAW EO B757-5740-11855 APPENDIX B.Oct 5, 2009 · N466UP · Boeing 75724APFSDR FDEA200910043468Skin · corrodedMAIN DECK CARGO UNDERFLOOR, CTR AUX FUEL TANK UPPER SURFACE, CORROSION FOUND ALONG STA 1227 AT X =-32.00. REPAIR CARRIED OUT EA NR1-5710-132222, THIS REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 REVISION 108.Oct 4, 2009 · N584FE · Doug MD11FSDR VNAA2009100700002Skin · dentedCREW REPORTED A BIRD STRIKE ON DESCENT. AIRCRAFT LANDED WITHOUT INCIDENT AT EWN. MAINTENANCE INSPECTED AND REMOVED AND REPLACED RT MID WING LEADING EDGE PER THE AIRCRAFT MAINTENANCE MANUAL. NO OTHER DAMAGE WAS NOTED AND AIRCRAFT RELEASED FOR SERVICE.Oct 4, 2009 · N216PS · Cndair CL6002B19SDR IPXA09M57775Skin · dentedINSPECTION TYPE:1/C REPAIR SURVEY SEQ. 283-W4-01, REPAIR DOUBLER IS DENTED REPAIRED AS PER UPS EO MD11-5730-35269-B, AND SAA EA 011-5730-01-A20 62, ISSUE B, REF RCD# 358207Oct 3, 2009 · N283UP · Doug MD11FSDR GUUA94657100309ASkin · damagedDURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED FASTENERS PULLING THROUGH THE RIGHT UPPER WING SKIN BETWEEN W.S 124.25 AND 143.00. REMOVED LEAKING RIVETS, FABRICATED AND INSTALLED AN EXTERNAL DOUBLER REPAIR.Oct 3, 2009 · N81546 · Beech 1900D
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