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 USAA070263Skin · crackedRIVET HOLES IN LEADING EDGE LOWER SKIN (AFT FASTENER ROW) JUST FWD OF I/B HAS CRACKS. REMOVED DAMAGE, INSTALLED FILLER & EXTERNAL DOUBLER PER SRM 57-43-01, DEFECT SIZE: 7 INCHES TOTAL ACCUMULATIVE LENGTH, 2 EA.Apr 4, 2007 · N421US · Boeing 737401SDR 07FDEA01268Skin · corrodedLT WING LOWER SURFACE NR 40 HEAD FASTENERS ON SKIN FOUND MODERATE CORROSION. REPAIRED IAW FEDEX EA 8-5730-103735.Apr 3, 2007 · N554FE · Doug DC1010SDR 07FDEA01262Skin · corrodedRT WING L/E AT SLAT TRACK HOLE NR 2 FOUND SKIN CORRODED. REPAIRED IAW SRM 57-10-00 FIGURE 68 SHT 1-3 VOL 1.Apr 3, 2007 · N554FE · Doug DC1010SDR 07FDEA01258Skin · corrodedRT WING L/E AT SLAT TRACK HOLE NR 1 FOUND SKIN EDGE CORRODED AND DISBONDED. REPAIRED SKIN IAW SRM 57-10-00 FIGURE 68 VOL.1 SHT 1-3.Apr 3, 2007 · N554FE · Doug DC1010SDR 07FDEA01257Skin · corrodedDEVIATIONS AND CORROSION ON THE TOP SKIN PANEL OF THE CENTER WING BOX, LT/RT, FROM C42 TO C47. REPAIRS PERFORMED IAW SRM 57-10-12 FIG 101 SH 3 AND SRM 51-40-21, COVERED BY EA 6-5710-99220 AND RAS 044669/016/2006 ISSUE "A".Apr 3, 2007 · N814FD · Airbus A310324SDR 07FDEA01252Skin · corrodedFOUND CORROSION ON LT WING BOTTOM SKIN PANEL 2 IN THE AREA OF RIB 1-4 AROUND SEVERAL FASTENERS. REPAIR PERFORMED BY BLEND OUT CORROSION IAW EA 6-5720-101272 AND SRM 57-00-00 4.C.3(B), APPROVED BY RAS/BAE/1002868/2006 ISSUE "A".Apr 3, 2007 · N814FD · Airbus A310324SDR DHL2007806508Skin · delaminatedFOUND LT WING T/E LWR PANEL SKIN DELAMINATED (STA XF 219.000 - 339.000). REMOVED AND REPLACED LT WING T/E LWR PANEL (STA XF 219.000 - 339.000) IAW SRM 51-3-0, SRM 51-3-1 (TORQUE).Apr 2, 2007 · N806DH · Doug DC873FSDR 07FDEA01248Skin · puncturedLT WING I/B FLAP LOWER SEGMENT UPPER SKIN FOUND PUNCTURED. LT WING I/B FLAP LOWER SEGMENT REPAIR CARRIED OUT AS PER SRM 57-10-00 FIG 35, VOL I AND FEDEX EA 1-5750-106610, WINGS TRAILING EDGE AND TRAILING EDGE DEVICES, LT INBD FLAP UPPER SKIN REPAIR. CLASSIApr 2, 2007 · N594FE · Doug MD11FSDR 07FDEA01231Skin · corrodedRIGHT WING TIP LOWER SURFACE FOUND CORROSION. [SUP 4-19-07] REPAIRED AS PER FEDEX E.A. 1-5710-107829. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.Apr 2, 2007 · N587FE · Doug MD11FSDR HYT2007F00000Skin · damagedSMOKING RIVETS IN LEADING EDGE SKIN UPPER SEAM. EVERY COUNTERSUNK HOLE FROM WS 35 TO WS 141 WAS FRETTING AGAINST THE RIVET HEAD. SAME CONDITION TO SAME EXTENT ON BOTH WINGS. IT APPEARS THE SKIN WAS COUNTERSUNK TOO DEEPLY. SAME CONDITION TO LESSER EXTENT FOApr 1, 2007 · N900WA · Cessna 208BSDR 07FDEA01225Skin · crackedLEFT WING SMALL CRACK AND DENT IN WING TIP L/E ADJACENT TO O/B END. REMOVED AND REPALCED WING TIP SKIN PNL IAW SRM 51-30-2, P/N 65-16209-4. PAINTED SKIN IAW MM 51-20-151-7.Apr 1, 2007 · N461FE · Boeing 727225SDR 07FDEA01224Skin · crackedLEFT WING L/E CRACKED ABOVE NR 3 SLAT O/B TRACK. REPAIRED CRACKED ON LEFT WING ABOVE NR 3 SLAT O/B TRACK IAW SRM 57-30-4 FIG 11.Apr 1, 2007 · N461FE · Boeing 727225SDR EIA2007066Skin · corrodedRT WING AT HOLES 1467 AT LOWER CHORD CORRODED. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER ECRA 479-57-217-2.Mar 31, 2007 · N479EV · Boeing 747132SDR 07FDEA01221Panel · delaminatedRT WING, UPPER SURFACE AT WBL 462, PNL, JUST O/B OF NR 14 SPOILER IS DELAMINATED. REMOVED PANEL AND SENT OUT FOR REPAIR. PANEL REPAIRED ON AAR WO NR 11841/6300/0003. REMOVED DAMAGE AND DELAMINATED SKIN, AND REPAIRED, REF SRM 51-40-20. INSTALLED PANEL REF Mar 31, 2007 · N463FE · Boeing 727225SDR DHL2007806526Panel · delaminatedLT WING T/E UPPER PANEL EXTERNAL SKIN DELAMINATED (STA XA 507.000 - 566.000). REMOVED DELAMINATED T/E UPPER PANEL (STA XA 507.000 - 566.000) IAW SRM 51-3-0. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW T/E PANEL IAW SRM 51-3-0, SRM 51-3-1Mar 30, 2007 · N806DH · Doug DC873FSDR 2007FA0000322Skin · corrodedDURING A WING NDT INSPECTION OF THE UPPER RT WING PLANK AT FS 452 AND BL 33, CORROSION WAS NOTED IN THIS AREA. ENGINEERING HAS DETERMINED THIS CORROSION IS EXCESSIVE ENOUGH TO REQUIRE ACCOMPLISHMENT OF ASC 229, WHICH REMOVES THE CORROSION ON THE PLANK AND INSMar 30, 2007 · N300WY · Gulstm G1159ASDR A6WA200740173Skin · corrodedWING PLANK AT WS 54.897 HAS SEVERAL PITS ON AFT EDGE THE DEEPEST IS .005 INCH. (K) [SUP 05-01-07] MAINTENANCE REMOVED CORROSION AND REPAIRED AREA IAW REO 601R-57-21-030. (M)Mar 30, 2007 · N457AW · Cndair CL6002B19SDR 07FDEA01197Skin · crackedCOMPLIED WITH EA NR 8-5710-102030 WING LT WING UPPER SKIN CRACKED AT XORS 585 ADJACENT TO STR 7. ACCOMPLISH PART 2 AT SUBSEQUENT C CHECKS CONCURRENT WITH MAINTENANCE WORK CARD 57SI5503-02 MAJOR REPAIR. COMPLIED WITH EA NR 8-5710-102030 WING LT WING UPPER SKIMar 30, 2007 · N571FE · Doug MD1010FSDR HNAA0700068Plate · corrodedCORROSION FOUND ON BOTH LADDER PLATES AND ACCESS PANEL 523AT AND 623AT. CORROSION, ON LADDER PLATES AND PANELS 523AT AND 623AT. REMOVED AND PROTECTED IAW RD 8-57-0469, RD 8-57-0455 AND RD8-57-3617. HFEC CHECK, NO CRACKS FOUND. MAINTENANCE PROGRAM TO BE AMEMar 29, 2007 · N337EN · Dhav DHC8311SDR 07FDEA01180Skin Panel · damagedRT WING PANEL NR 8505 OUTER SURFACE FWD EDGE I/B IS DAMAGED REMOVED PANEL REF SRM 51-30-02. REPAIRED PANEL REF SRM 51-40-20 PAGES 12, 46, 53 THRU 62. PRIMED AND PAINTED, REF MM 51-20-151-7. INSTALLED PANEL REF 20-10-023-4 PARA 4B (2).Mar 29, 2007 · N463FE · Boeing 727225SDR QXEA200700576Access Panel · chafedC3 OKC - LEFT WING INBOARD FLAP ACCESS PANEL 584LB IS CHAFED ON OUTER SURFACE BY ACTUATOR CUTOUT. REPAIRED IAW SRM 51-21-11, 57-52-01.Mar 28, 2007 · N615QX · Cndair CL6002C10SDR QXEA200700575Access Panel · chafedC3 OKC - LEFT WING INBOARD FLAP ACCESS PANEL 584GB IS CHAFED ON OUTER SURFACE BY ACTUATOR CUTOUT. REPAIRED IAW SRM 51-21-11, 57-52-01.Mar 28, 2007 · N615QX · Cndair CL6002C10SDR A6WA200740163Access Panel · corrodedLT LOWER WING PLANK FUEL ACCESS PANEL CUTOUT FOR FUEL PNL 540 CB HAS CORROSION IN NON-CRITICAL AREA APPROX 6.0 INCHES DEEP AND .020 WIDE. (K) [SUP 05-17-07] MAINTENANCE REPAIRED CORROSION BY BLENDING OUT CORROSION. PERFORMED NDT, ROTO PEENED AREA, SANDED RMar 28, 2007 · N416AW · Cndair CL6002B19SDR 07FDEA01168Skin · crackedRT WING NR 6 MOVEABLE FAIRING SKIN FWD OB EDGE IS CRACKED. REPAIRED FAIRING REF SRM 51-10-1, 57-20-2, 51-40-2 AND MM 51-20-151-7.Mar 28, 2007 · N463FE · Boeing 727225SDR 07FDEA01160Skin · corrodedFOUND CORROSION FINDINGS ON RT WING TOP SKIN RIB 1-25 REPAIR PERFORMED BY BLEND IAW EA 6-5720-106375 AND RAS/BAE/1004284/2007 ISS.A.Mar 28, 2007 · N748FD · Airbus A300B4622RSDR QXEA200700574Access Panel · chafedC3 OKC - LEFT WING INBOARD FLAP ACCESS PANEL 584EB IS CHAFED ON OUTER SURFACE BY ACTUATOR CUTOUT. REPAIRED IAW SRM 57-52-01, 51-21-11, AND 51-25-06.Mar 27, 2007 · N615QX · Cndair CL6002C10SDR CALA0700153Skin · crackedINSPECTION FOUND A 1.5 INCH CRACK IN RT WING FIXED LEADING EDGE LOWER SKIN AT PYLON O/B MIDSPAR FITTING. A DOUBLER WAS INSTALLED IAW ECRA 5731-01302.Mar 27, 2007 · N77303 · Boeing 7373T0SDR 07FDEA01142Skin · corrodedCORROSION SPOTS ON OUTER SHROUD BOX AND TOP SKIN REPAIR PERFORMED BY BLEND OUT IAW EA 6-5720-106376 AND RAS/BAE/1004287/2007 ISS. AMar 27, 2007 · N748FD · Airbus A300B4622RSDR 07FDEA01141Skin · corrodedCORROSION SPOTS ON LT WING TOP SKIN RIB 1-25 REPAIR PERFORMED BY BLEND OUT IAW EA 6-5720-106376 AND RAS/BAE/1004287/2007 ISS. A.Mar 27, 2007 · N748FD · Airbus A300B4622RSDR QXEA200700583Panel · corrodedC3 OKC - BUTE DOOR PANEL 691JB HAS LIGHT SURFACE CORROSION IN FASTENER HOLES. REPAIRED IAW SRM 51-21-06, 51-21-11, AND 51-25-16.Mar 26, 2007 · N615QX · Cndair CL6002C10SDR QXEA200700579Panel · gougedC3 OKC - RIGHT WING LEADING EDGE PANEL 622AR IS GOUGED/CHAFED ON LEADING EDGE. REPAIRED IAW SRM 57-00-01, 51-12-00.Mar 26, 2007 · N615QX · Cndair CL6002C10SDR 2007UALA00872Skin · damagedRTFL UNDER AMBER ALERT DUE TO INFLIGHT DAMAGE TO NR 4 ENGINE INBOARD SAILBOAT FAIRING. [SUP 4-20-07] FOUND ONE SAILTAIL PANEL MISSING & ONE DAMAGED. ROBBED MISSING UNIT & INSTALLED. ACCOMPLISHED HFEC INSPECTION OF BLENDED RT LOWER WING SKIN JUST INBD OF NMar 25, 2007 · N127UA · Boeing 747422SDR QXEA200700493Access Panel · corrodedC4 PDX - FUEL TANK ACCESS PANEL 524AT HAS FRETTING ON INBOARD AND OUTBOARD SIDE WING STRUCTURE. REPAIRED IAW RD8-57-984.Mar 25, 2007 · N365PH · Dhav DHC8202SDR QXEA200700492Access Panel · corrodedC4 PDX - FUEL TANK ACCESS PANEL 524CL HAS FRETTING ON WING STRUCTURE AT STATION YW404.00, YW387.00, YW369.00 AND YW334.00. REPAIRED IAW RD8-57-611.Mar 25, 2007 · N365PH · Dhav DHC8202SDR QXEA200700491Access Panel · corrodedC4 PDX - FUEL TANK ACCESS PANEL 524BT HAS FRETTING ON INBOARD AND OUTBOARDWING STRUCTURE. REPAIRED IAW RD8-57-633.Mar 25, 2007 · N365PH · Dhav DHC8202SDR DLM90070264Skin · crackedRT WING L/E SKIN CRACKED AT O/B END OF THE REFUELING PANEL CUT OUT. REPAIR PER SRM 57-20-01 FIG 2 HMV 2 REF N/R 6200-0002.Mar 25, 2007 · N901DA · Doug MD9030SDR N865R1076007Access Door · corrodedLT WING XFS 836 OUTBD L/E INNER LOWER SECTION ACCESS DOOR NR 517B JAMB WITH CORROSION CPCP 107L 0552.Mar 23, 2007 · N865F · Doug DC863FSDR 07FDEA01082Skin · damagedELONGATED HYDRAULIC FITTING HOLES IN THE LOWER SKIN PANELS OF LT WING. REPAIR PERFORMED BY OVERSIZING AND BUSHING HOLES IAW EA 6-5720-99228, APPROVED BY RAS/BAE/1002610/2006 ISSUE "A".Mar 22, 2007 · N814FD · Airbus A310324SDR IXXA070018SSkin · crackedDURING ROUTINE CPCP INSPECTION, FOUND RIGHT WING UPPER SKIN CRACKED AT STATION XRS 74 STRINGER 9. REMOVED DAMAGE AREA, NO CRACK'S OR CORROSION FOUND AFTER DAMAGE REMOVED. MANUFACTURED REPAIR PARTS. TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIRMar 22, 2007 · N821BX · Doug DC871FSDR IXXA070017SSkin · crackedDURING ROUTINE CPCP INSPECTION, FOUND RIGHT WING UPPER SKIN CRACKED AT STATION XRS 74 STRINGER 16. REMOVED DAMAGE AREA, NO CRACK'S OR CORROSION FOUND AFTER DAMAGE REMOVED. MANUFACTURED REPAIR PARTS. TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIMar 22, 2007 · N821BX · Doug DC871FSDR 07FDEA01098Skin · corrodedFOUND CORROSION ON RT WING TOP SKIN IN AREA OF RIB 4/5 NEAR PICK UP FITTING. CORROSION REMOVED BY BLEND OUT AND INSTALLATION OF PACKING WASHERS FOR FLAT SEATING OF LOCALIZED SPOTFACING OF OVERWING BRACKET HOLES IAW EA 6-5720-99218, APPROVED BY RAS/BAE/1002737Mar 22, 2007 · N814FD · Airbus A310324SDR 07FDEA01086Skin · corrodedCORROSION ON LOWER SKIN PANEL NR 2 AND REINFORCING STRUCTURE OF THE LT WING INBOARD RIB 1-3. REPAIRED BY BLENDING OUT AND TRIMMING OUT EXFOLIATION CORROSION IAW EA 6-5720-99216, APPROVED BY RAS/BAE/1002613/2006 ISSUE "A".Mar 22, 2007 · N814FD · Airbus A310324SDR 07FDEA01085Skin · corrodedCORROSION ON LOWER SKIN PANEL NR 2 AND REINFORCING STRUCTURE OF THE RT WING INBOARD RIBS 1-3. REPAIRED BY BLENDING OUT AND TRIMMING OUT EXFOLIATION CORROSION IAW EA 6-5720-99216, APPROVED BY RAS/BAE/1002613/2006 ISSUE "A".Mar 22, 2007 · N814FD · Airbus A310324SDR 07FDEA01043Skin · corrodedFOUND EXTENSIVE CORROSION ON RT WING BOTTOM FRONT SPAR OVERHANGS. LOOK FOR AFFECTED AREAS IN EA 6-5720-99230. REPAIR PERFORMED BY BLEND AND/OR CUT OUT AND INSTALLING REPAIR PLATES ALL IAW EA 6-5720-99230, APPROVED BY RAS/BAE/1002584/2006 ISSUE "A".Mar 21, 2007 · N814FD · Airbus A310324SDR 07FDEA01041Skin · corrodedEXTENSIVE CORROSION ON THE LT WING BOTTOM SKIN FRONT SPAR OVERHANGS. LOOK FOR AFFECTED AREAS IN MENTIONED EA. REPAIR PERFORMED BY BLEND OUT AND/OR CUT OUT AND INSTALLING REPAIR PLATES ALL IAW EA 6-5720-99230, APPROVED BY RAS/BAE/1002584/2006 ISSUE "A".Mar 21, 2007 · N814FD · Airbus A310324SDR 07FDEA01040Skin · corrodedEXTENSIVE CORROSION ON LT WING TOP SKIN. AFFECTED AREAS SHOWN ON PAGES 4 THROUGH 6 IN MENTIONED EA. REPAIR PERFORMED BY BLEND OUT AND OVERSIZING IAW EA 6-5720-101319, APPROVED BY RAS/BAE/1003173/2006 ISSUE "A".Mar 21, 2007 · N814FD · Airbus A310324SDR 07FDEA01037Skin · corrodedFOUND CORROSION ON TOP SKIN RT WING. AFFECTED AREAS MENTIONED IN EA 6-5720-99229. REPAIR PERFORMED BY BLEND OUT AND OVERSIZING IAW EA 6-5720-99229 AND RAS/BAE/1002732/2006.Mar 21, 2007 · N814FD · Airbus A310324SDR 07FDEA00999Skin · damagedPYLON SUPPORT BRACKET AND BOTTOM WING SKIN (LT WING), ELONGATED HOLES REPAIR WAS PERFORMED IAW DRAWING R571-50532 REV A, APPROVED BY EA 6-5720-106407 AND RAS/BAE/1004134/2007 ISS A.Mar 19, 2007 · N748FD · Airbus A300B4622RSDR 07FDEA00980Skin · dentedRT WING O/B FLAP O/B END LOWER SKIN DENTED, JUST I/B OF EXISTING REPAIR. REMOVED DAMAGED DOUBLER IAW MD10/DC10 SRM 51-31-01 VOL11 MAT ID FOR REPAIR DOUBLER 2024-T3 0.040 IAW DC10/MD10 SRM 57-52-01 VOL 111. PO NR 557785.5 AND PO NR 541694.2. FAB`D PARTS IAW Mar 18, 2007 · N566FE · Doug MD1010FSDR A6WA200740136Skin · corrodedRT WING PLANK ACCESS HOLE AT FUEL PANEL 650CB HAS MINOR CORROSION AROUND APPROX 90 PERCENT OF BONDING AREA. (K) [SUP 06-05-07] MAINTENANCE SANDED CORRODED AREA TO REMOVE DAMAGE MAX BLEND .004 IAW BSC EO NR 601R-57-11217. (M)Mar 17, 2007 · N415AW · Cndair CL6002B19
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