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 EIAA2008101600058Skin · corrodedLEFT WING FWD OF SPAR RABBIT JOINT 8 FT FROM TIP CORRODED. REMOVED CORROSION, NDT AREA, FABBED AND INSTALLED REPAIR PER ECRA 487-57-047-2.Oct 15, 2008 · N487EV · Boeing 747230BSDR ZESA2008008Fuel Door · openFUEL DOOR AND CAP WERE NOT SECURED PRIOR TO FLIGHT. UPON TAKE OFF, CREW HEARD A BANGING FROM ACFT AND RETURNED TO POINT OF ORIGIN. INSPECTED AND FERRIED ACFT FOR REPAIRS. REMOVED AND REPLACED RT INBD LEADING EDGE AND POLISHED OUT FUSELAGE PANEL.Oct 13, 2008 · N228Y · Cessna 560XLSDR UIEA200800329Skin Panel · debondedRT WING UPPER SURFACE L/E PANEL AT ILES 328.5 HAS A PREVIOUS REPAIR AREA 7.0 BY 6.0 INCHES DISBONDING AND CRACKING. PERMANENT REPAIR ACCOMPLISHED IAW SRM 51-40-09, FIG 18, SHEETS 2 AND 5, PREPREG 250 DEGREE F CURE IAW SRM 51-40-12. ALSO, REF EO NR 4757A465.Oct 12, 2008 · N809MC · Boeing 747228FSDR UPS08M53625Doubler · crackedINSPECTION TYPE:1C LT WING FIXED L/E HAS 10 INCH CRACK SIGN ON DOUBLER OUTBOARD OF NR 4 AND NR 5 SLT TRACK XORS 562. REMOVED DOUBLER, FABRICATED, AND INSTALLED DOUBLER IAW DWG ARB3954 AND MD-11 SRM 51-33-01.Oct 12, 2008 · N288UP · Doug MD11FSDR UPS08M53627Skin · crackedINSPECTION TYPE:1C RT WING FIXED L/E BELOW SLAT TRACK 14 SKIN CRACKED. CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER IAW MD-11 SRM 57-10-00 FIG 21.Oct 10, 2008 · N288UP · Doug MD11FSDR 08FDEA04267Skin · crackedLEFT WING UPPER SURFACE SKIN CRACKED AT NR 4 SPOILER I/B ACTUATOR HINGE CUTOUT REMOVED AND REINSTALLLED NR 4 SPOILER PANEL, FABRICATED, TREATED, PRIMED, PAINTED, AND INSTALLED DOUBLER REF SRM 57-30-4, 51-10-2, 51-30-2 AND MM 51-20-000-7, MM 27-61-081-4. STOPOct 8, 2008 · N485FE · Boeing 727227SDR GLBA200810087Skin · damagedMAJOR REPAIR - DURING ROUTINE SCHEDULED MAINTENANCE A REPAIR AT THE LEFT INBOARD LOWER WING SKIN AT THE OUTBOARD AFT CORNER AND OUTBOARD FUEL PANEL AT APPROXIMATELY WS 2293 DOES NOT CONFORM WITH GIVEN DOCUMENTATION. MAINTENANCE REMOVED PATCH AND INSTALLED NEWOct 8, 2008 · N71GL · Emb EMB120ERSDR UPS08M53602Splice · crackedINSPECTION TYPE:1C LT WING L/E SKIN SPLICE STRAP XFS 791 CRACKED. FABBED AND INSTALLED REPAIR DOUBLER IAW, SRM, 51-33-01 VOL 2 PG 1, DWG ARB3954, 51-33-01 PG 29.Oct 7, 2008 · N260UP · Doug MD11FSDR UPS08M53591Splice · crackedINSPECTION TYPE:1C RT WING L/E SKIN SPLICE STRAP XFS 791 CRACKED. REMOVED AND REPLACED SKIN SPLICE STRAP IAW SRM DWG ARB3954, 51-33-01, 51-21-01.Oct 7, 2008 · N260UP · Doug MD11FSDR UPS08M53589Splice · crackedINSPECTION TYPE:1C RT WING L/E SKIN STRAP XFS994 CRACKED. REMOVED AND REPLACED SKIN SPLICE STRAP IAW, SRM DWG ARB3954, 51-21-2, 51-33-01.Oct 7, 2008 · N260UP · Doug MD11FSDR WRLA2008087Skin · corrodedDURING BRIDGE CHECK, MX FOUND CENTER WING TANK UPPER SKIN SURFACE CORROSION AT STA Y1229, X-100- -120. REPAIRED THE CENTER WING TANK UPPER SKIN CORROSION IAW EI W2008A57B-1061 REV.00Oct 6, 2008 · N384WA · Doug MD11FSDR WRLA2008081Skin · corrodedDURING BRIDGE CHECK, MX FOUND CENTER WING TANK LT UPPER SKIN SURFACE CORROSION AT STA Y1159-1239, X27-120. REPAIRED IAW ENGINEERING INSTRUCTION W2008A57B-106 REV 00.Oct 6, 2008 · N384WA · Doug MD11FSDR WRLA2008079Skin · corrodedDURING BRIDGE CHECK, MX FOUND CENTER WING TANK RT UPPER SKIN SURFACE CORROSION AT STA Y1150-1239, X-8 TO -120. REPAIRED CENTER WING TANK UPPER SKIN CORROSION AREA IAW ENGINEERING INSTRUCTION W2008A57B-1061 REV 00.Oct 6, 2008 · N384WA · Doug MD11FSDR 08FDEA04222Skin · dentedLT WING I/B FLAP LOWER SURFACE SCRATCH AND DENT FOUND AT WS 151.3. REPAIR CARRIED OUT AT LT WING INBOARD FLAP LOWER SEGMENT AT STA XW = 151.3 AS PER SRM 57-10-00. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Oct 6, 2008 · N576FE · Doug MD11FSDR 08FDEA04221Skin · dentedLT WING I/B FLAP LOWER SURFACE AT WS 288.14 DENT FOUND. REPAIR CARRIED OUT AT LH WING I/B FLAP LOWER SURFACE AT STA. 288.140 AS PER SRM 57-10-00 FIG. 13 VOL. I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Oct 6, 2008 · N576FE · Doug MD11FSDR 08FDEA04220Skin · cracked05 EA FASTENER HOLES FOUND CRACK DURING HFEC INPECTION ON RT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN XORS=683.4 AND XORS=713.6. REPAIRED AS PER E.A. 1-5710-122580 - A.D. 2007-07-04. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Oct 6, 2008 · N576FE · Doug MD11FSDR 08FDEA04219Skin · cracked06 EA FASTENER HOLES FOUND CRACK DURING HFEC INPECTION ON LT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN XORS=683.4 AND XORS=713.6. REPAIRED AS PER E.A. 1-5710-122579- A.D. 2007-07-04. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Oct 6, 2008 · N576FE · Doug MD11FSDR COMA0860409Skin · corrodedLT WING FUEL ACCESS HOLE AT 540BB FLANGE HAS FRETTING CORROSION. REPAIRED AREA OF FUEL ACCESS PANEL CUTOUT PER CRJ REO 601R-57-21-030 REV D.Oct 5, 2008 · N967CA · Cndair CL6002B19SDR UPS08853677Skin · misrepairedINSPECTION TYPE:SV RT LWR LEADING EDGE DOUBLER STA XFS 524 NEEDS VALIDATION. DOES NOT MEET CRITERIA APPENDIX H STEP 5. 894-W4-19 AREA PREVIOUSLY REPAIRED & AND ADDED EXTRA ROW OF FASTENERS IAW DC8 SRM 57-2-1 TR 57-95 AND SRM 51-1-21.Oct 5, 2008 · N894UP · Doug DC873FSDR UPS08853650Doubler · unknownINSPECTION TYPE:SV RT UPPER LEADING DOUBLER NEEDS VALIDATION AT STA XFS627 FAIL APP H ST STEP 5 894-W4-12 REPAIRED IAW 57-2-1 AND 51-01-04.Oct 5, 2008 · N894UP · Doug DC873FSDR UPS08853647Doubler · unknownINSPECTION TYPE:SV RIGHT LEADING EDGE DOUBLER NEEDS VALIDATION AT STA XFS 455 FAILED APPH STEP 5 894-W4-07. REPLACED DOUBLER IAW DC8 SRM 57-2-1 FIG 38.Oct 5, 2008 · N894UP · Doug DC873FSDR UPS08853636Skin · unknownINSPECTION TYPE:SV RT UPPER LEADING EDGE DOUBLER NEEDS VALIDATION AT STA 325 FAILS APPEN DIX "H" STEP 5 SURVEY SEQ 894-W4-5. REMOVED AND REPLACED REPAIR PER DC 8 SRM 57-2-1 FIG 38 TR 57-85.Oct 5, 2008 · N894UP · Doug DC873FSDR UPS08853623Skin · misrepairedINSPECTION TYPE:SV RT WING LEADING EDGE LOWER DOUBLER I/B SIDE OF NR 4 PYLON NEED VALIDATION AT STA XFS 500. DOES NOT MEET CRITERIA IN APPENDIX H STEP 5. 894-W4- 32 AREA PREVIOUSLY REPAIRED FEF SRM 57-3-1 T/R 57-83.Oct 5, 2008 · N894UP · Doug DC873FSDR WRLA2008092Skin · deformedDURING BRIDGE CHK + 4C CHK, EGAT MECH FOUND NOSE GEAR TRUNNION FITTING SKIN DEFORMED AT STA Y=595, L50L, REFER TO EGAT NRC NR U05188. REMOVE TRUNNION FITTING AND DAMAGED DOUBLER PER MD-11F SRM VOL 2 51-35-01 REV 40. FABRICATED NEW DOUBLER IAW ENGINEERING INSOct 4, 2008 · N384WA · Doug MD11FSDR 2008UALA05989Skin · corrodedRIGHT WING, UPPER SKIN AT WBL 95, STA 970 IS CORRODED. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SKIN AND INSTALLED DOUBLER REPAIR.Oct 4, 2008 · N547UA · Boeing 757222SDR KCSA081509Skin · corrodedLT WING STA 700 NR 4 AFT BOOST PUMP CUT OUT CORRODED.Oct 2, 2008 · N712CK · Boeing 747122SDR 08FDEA04165Skin Panel · crackedLT WING LWR SURFACE T/E FOUND CRACK ON SKIN PANEL REF IPC 57-32-60-01 ITEM 210 VIEW "A". REPAIRED PANEL IAW SRM 51-71-00 PAR 18 B & SRM 57-10-00 FIG 73 SHT 5 VOL I.Oct 1, 2008 · N40061 · Doug MD1010FSDR ASM2008F00006Access Panel · leakingDURING FUEL SUPPLY SERVICE MX PERSONNEL DETECTED A FUEL LEAK UNDER THE RT WING. THE MAIN TANK ACCESS DOOR 632EB AND ITS RUDDER DOOR SEAL WERE REPLACED AND TESTED IAW MM 28-11-11, TASK 28-11-00-790-801 ALL CORRECT.Sep 30, 2008 · N852AM · Boeing 737*SDR 08FDEA04120Panel · delaminatedLEFT WING LOWER T/E PANEL NR 541 HB DELAMINATED AROUND EDGE. REPAIRED BY REMOVING; FABRICATING & BONDING A NEW OUTER SKIN, INNER DOUBLER, HONEYCOMB CORE AND INNER SKIN IAW E.A. 8-5720-123638 AND TPS 1001; REV " E ". PRIMED; SEALED & PAINTED PANEL IAW E.A. 8Sep 29, 2008 · N550FE · Doug MD1010FSDR 2008UALA05901Panel · damagedRIGHT WING INBOARD LWR FIXED T/E PANEL NEXT TO BODY FAIRING DAMAGED AT WBL 71.26. REPLACED PANEL.Sep 28, 2008 · N912UA · Boeing 737522SDR GUUA09270801Skin · corrodedDURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED LEFT OUTBOARD WING UPPER SKIN TRAILING EDGE HAD CORROSION AND DEBOND BETWEEN WS 121 THROUGH 194.85. REMOVED DAMAGED SKIN, FABRICATED AND INSTALLED AN EXTERNAL REPAIR DOUBLER.Sep 27, 2008 · N81546 · Beech 1900DSDR KCSA081497Skin Panel · bulgedRT WING UPPER T/E PANEL HAS BULGE ABOVE REAR SPAR AT WBL 241. (K)Sep 27, 2008 · N712CK · Boeing 747122SDR 08FDEA04051Skin · chafedRIGHT WING LEADING EDGE ANTI-ICE TELESCOPIC DUCT CUT-OUT DOUBLER INBOARD AND OUTBOARD LOWER SECTION FOUND WITH CHAFE MARKS. REPAIR CARRIED OUT AS PER EA NR 1-5740-122551, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 26, 2008 · N623FE · Doug MD11FSDR 08FDEA04031Panel · chafedFOUND CHAFING ON PANEL 471AT, LT WING, RIB 7-8 PANEL REPLACED IAW DRAWING R572-40275, APPROVED BY RAS/BAE/1007905/2008 ISS A AND EA 6-5741-123099.Sep 25, 2008 · N744FD · Airbus A300B4622RSDR 08FDEA04029Panel · delaminatedFOUND DELAMINATION ON RT OUTBOARD TRAILING EDGE PANEL REPAIR PERFORMED IAW SRM 57-51-12 PAGE 201 PARA 4, FIG 216, APPROVED BY RAS/1007710/2008 ISS A AND EA 6-5751-123095.Sep 25, 2008 · N744FD · Airbus A300B4622RSDR DHLA2008745666Skin · corrodedRT WING AT WBL 446 BETWEEN REAR SPAR AND S-5 WING LOWER SKIN, LOWER SURFACE WITH CORROSION. REPAIRED RT WING LOWER SKIN SECTION AT REAR SPAR AND STIFFENER 5 AT WBL 442 DUE TO CORROSION IAW COOPESA EO COO-2-57-354-08.Sep 24, 2008 · N745DH · Boeing 727224SDR UPS08653456Skin · gougedINSPECTION TYPE:N/A DMID383810 - RT WING L/E SKIN GOUGE TEMP REPAIR I/B NR 2 ENG ABOVE KRUEGER FLAP. RT WING L/E SKIN AT BETWEEN ISS337.6-345.5 AREA SKIN REPAIRED AS PER RS R57-41-36117 & UPS EO B767-5730-30466-A.Sep 24, 2008 · N330UP · Boeing 76734AFSDR QXEA2008103101047Skin · dentedPDX - C4 - PERMANENT REPAIR FOR DENT TO RT FIXED LEADING EDGE SKIN AT SS156.28. CUT OUT DAMAGE REF REO 670-57-41-154/3. HFEC IAW CRJ 700 NDTM PART 1, 51-20-006 AT CUTOUT, NO CRACKS NOTED. FABRICATED REPAIR DOUBLER FROM .063" 2024T3 AND REPAIR SHIM FROM .032Sep 23, 2008 · N611QX · Cndair CL6002C10SDR UPS08853667Fastener · looseINSPECTION TYPE:SV SURVEY SEQ NO 894-W3-13 LT WING L/E ABOVE NR 2 PYLON AT XFS 275 SKIN REPAIR DOUBLER HAS 4 FASTENERS LOOSE AND 1 FASTENER PULLED THROUGH. REMOVED AND INSTALLED 5 NEW FASTENERS IAW DC8 SRM 51-3-0 FIG 52A.Sep 22, 2008 · N894UP · Doug DC873FSDR UPS08853666Fastener · brokenINSPECTION TYPE:SV SURVEY SEQ NO 894-W3-01 LT WING L/E LOWER SURFACE SKIN REPAIR DOUBLER HAS 1EA FASTENER HEAD BROKEN AT XFS 404.000 BETWEEN NR 1 AND NR 2 ENG. REPLACED FASTENER IAW UPS DC8 SRM 51-03-00.Sep 22, 2008 · N894UP · Doug DC873FSDR UPS08853665Skin · misrepairedINSPECTION TYPE:SV SURVEY SEQ NO 894-W3-03 LT WING L/E LOWER SURFACE SKIN REPAIR DOUBLER A HAS 5EA FASTENER HEADS PROTRUDING AT XFS 462.000 AFT OF SLOT DOOR. RE-COUNTERSINK HOLES AND INSTALLED SCREWS IAW DC8 SRM 51-3-0.Sep 22, 2008 · N894UP · Doug DC873FSDR UPS08853504Skin · damagedINSPECTION TYPE:CV EVALUATION AND DISPOSITION REPAIR SURVEY SEQUENCE NR: 894-W4-09. RIGHT UPPER LEADING EDGE DOUBLER REPAIR STA XFS 512 MISSING 8 EACH FA FASTENERS. INSTALLED FASTENERS IAW DC-8 SRM 51-03-00.Sep 22, 2008 · N894UP · Doug DC873FSDR DHLA2008745626Skin · corrodedRT WING UPPER SKIN WITH CORROSION AT WS 619 REAR SPAR SECTION. REPAIRED RT WING UPPER SKIN AT REAR SPAR AT WS 619 IAW BOEING MESSAGE 1-1000735864-2 DTD 10/2/08 AND COOPESA EO COO-2-57-330-08.Sep 20, 2008 · N745DH · Boeing 727224SDR 08FDEA03949Skin · crackedDURING HFEC INSPECTION, FOUND 14 FASTENER HOLES WITH CRACK INDICATIONS AT RIGHT WING LOWER SKIN PANELS OUTER WING ACCESS DOOR CUTOUT BETWEEN XORS 683.400 AND 713.600. REPAIRED AS PER EA 1-5710-122560, THIS REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.Sep 19, 2008 · N606FE · Doug MD11FSDR 08FDEA03948Skin · crackedDURING HFEC INSPECTION, FOUND 11 FASTENER HOLES WITH CRACK INDICATIONS AT LEFT WING LOWER SKIN PANELS OUTER WING ACCESS DOOR CUTOUT BETWEEN XORS 683.400 AND XORS 713.600. REPAIRED AS PER EA 1-5710-122559, THIS REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Sep 19, 2008 · N606FE · Doug MD11FSDR 2008UALA05842Panel · splitRT WING LOWER PANEL 651VB (REAR OF LDG GEAR) HAS 5.5 INCH SPLIT IN FWD EDGE. REPAIRED T/E PANEL ON R&R. COMPLETED GEAR SWINGS FOR ADEQUATE CLEARANCE BTWN RIGHT GEAR FIXED STRUT DOOR & LWR WING PANEL. Sep 18, 2008 · N653UA · Boeing 767322SDR UPS08853347Panel · crackedINSPECTION TYPE:N/A LEFT WING TRAILING EDGE PANEL CRACK.Sep 18, 2008 · N772UP · Doug DC871FSDR AALA200802545Skin · corrodedCORROSION FOUND ON LT WING SKIN AT THE EMERGENCY WALKWAY. REPAIRED IN ACCORDANCE WITH ESO 90309 DATED 17 SEP 2008.Sep 17, 2008 · N624AA · Boeing 757223SDR 08FDEA03918Panel · wornLEFT WING OUTBD L/E PANEL 527 AB IS WORN AT THE LATCH. FABBED DOUBLER REF SRM 57-00-01; VOL I. BLENDED WORN AREA AND FOUND OUT OF LIMITS REF SRM 57-00-01; VOL I. ALODINED AND PRIMED REF SRM 51-21-01, VOL II. INSTALLED DOUBLER REF SRM 51-35-01; VOL II.Sep 17, 2008 · N550FE · Doug MD1010FSDR 08FDEA03898Skin · wornLEFT WING INBD LOWER TE PANEL 545 BB IS WORN. PANEL FOUND TO BE OUT OF LIMITS IAW SRM 57-00-01. FABRICATED IAW DWG ARC 1283. HEAT TREATED IAW TPS 1003. ALODINED & PRIMED IAW SRM 51-21-01. PAINTED IAW SRM 51-21-02. PART MARKED IAW GMM 7-0-1001.Sep 16, 2008 · N550FE · Doug MD1010F
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