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 08FDEA01075Skin · corrodedFOUND CORROSION ON BOTTOM SKIN AT RIB 4 REAR SPAR AREA. REPAIR PERFORMED BY REWORK OF CORRODED AREA IAW RAS/BAE/1006318/2008, APPROVED BY EA 6-5720-114866.Mar 20, 2008 · N741FD · Airbus A300B4622RSDR 08FDEA01074Skin · corrodedFOUND OLD CORROSION REPAIR UNDER STATIC DISCHARGER, LT WING TIP WITHOUT DOCUMENTATION REPAIR PERFORMED BY BLEND OUT CORROSION AND INSTALLING A REPAIR PATCH IAW RAS/FOK/016/2008 ISS A, APPROVED BY EA 6-5730-114884.Mar 20, 2008 · N741FD · Airbus A300B4622RSDR 08FDEA01072Skin · corrodedFOUND CORROSION AROUND STATIC DISCHARGER OUTBOARD, WING TIP RT. REPAIR PERFORMED BY BLEND OUT OF CORRODED AREA AND INSTALLING A REPAIR PATCH IAW RAS/FOK/319/2007 ISS A, APPROVED EA 6-5730-114859.Mar 20, 2008 · N741FD · Airbus A300B4622RSDR UPS08M51993Splice · crackedINSPECTION TYPE:2C RIGHT WING L/E SPLICE STRAP XFS 669 CRACKED. REMOVED CRACKED SPLICE STRAP, FABRICATED REPLACEMENT SPLICE STRAP AND INSTALLED IAW DWG3954 & MD-11 SRM 51-33-01.Mar 19, 2008 · N256UP · Doug MD11FSDR UPS08M51992Splice · crackedINSPECTION TYPE:2C RIGHT WING L/E SPLICE STRAP XFS 791 CRACKED. REMOVED SPLICE STRAP, FABRICATED REPLACEMENT SPLICE STRAP AND INSTALLED IAW DWG ARB3954 AND MD-11 SRM 51-33-01.Mar 19, 2008 · N256UP · Doug MD11FSDR UPS08M51988Skin · crackedINSPECTION TYPE:2C RIGHT WING L/E SLAT TRACK NR 12 CUTOUT CRACKED. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER & FILLER IAW MD-11 SRM 57-10-00 FIG 21.Mar 19, 2008 · N256UP · Doug MD11FSDR UPS08M51986Skin · crackedINSPECTION TYPE:2C RIGHT WING L/E NR 14 SLAT TRACK CUTOUT CRACKED LOWER O/B CORNER. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER & FILLER IAW MD-11 SRM 57-10-00 FIG 21.Mar 19, 2008 · N256UP · Doug MD11FSDR 08FDEA01065Panel · chafedLT WING T/E NR 572 BB HAS CHAFING; BARE METAL AND PEELING PAINT ON THE INNER SURFACE. REMOVED DAMAGED AREA, FABRICATED FILLER PLATE & DOUBLER. LAID UP REPAIR,CURED, PLACED A BEAD OF SEALANT AROUND DOUBLER. INSTALLED NEW GROMMET, PRIMED PANEL & APPLIED FINISMar 19, 2008 · N425FE · Airbus A310203SDR 08FDEA01058Panel · chafedLT WING T/E UPPER SURFACE OF THE MOST INBD FIXED PANEL AFT EDGE HAS CHAFING WEAR ABOVE THE INBD FLAP VANE INBD EDGE. TRIMMED WORN EDGE IAW SRM 57-00-01. REPAIRED PUNCTURED AREA BY BONDING A FILLER & DOUBLER IAW SRM 51-71-00 VOL II. REMOVED CORROSION, ALODINEDMar 19, 2008 · N365FE · Doug MD1010FSDR 08FDEA01052Skin · crackedRT WING L/E EXT ZONE FOUND CRACKS ON UPPER SKIN. REPAIRED SKIN IAW SRM 57-10-00 FIG 68 VOL I.Mar 19, 2008 · N307FE · Doug DC1030FSDR 08FDEA01037Panel · tornRT WING L/E LOWER SURFACE PANEL 623 EB SPEED TAPE IS PEELING OFF AND TORN. REMOVED DAMAGED FOIL IAW SRM 57-41-12. APPLIED NEW FOIL IAW SRM 57-41-12. PRIMED IAW SRM 51-23-10.Mar 18, 2008 · N425FE · Airbus A310203SDR 08FDEA01036Panel · tornRT WING L/E LOWER SURFACE PANEL 623 FB SPEED TAPE IS PEELING OFF AND TORN. REMOVED DAMAGED FOIL IAW SRM 51-75-10. APPLIED NEW FOIL IAW SRM 57-41-12. PRIMED IAW SRM 57-41-12.Mar 18, 2008 · N425FE · Airbus A310203SDR 08FDEA01035Panel · tornRT WING L/E LOWER SURFACE PANEL 623 MB SPEED TAPE IS PEELING OFF AND TORN. REMOVED DAMAGED FOIL IAW SRM 57-41-12. APPLIED NEW FOIL IAW SRM 57-41-12. APPLIED SURFACE FINISH IAW SRM 51-75-10.Mar 18, 2008 · N425FE · Airbus A310203SDR 08FDEA01034Panel · tornRT WING L/E LOWER SURFACE PANEL 623 LB SPEED TAPE IS PEELING OFF AND TORN. REMOVED DAMAGED FOIL IAW SRM 57-41-12. APPLIED NEW FOIL IAW SRM 51-75-12. PRIMED IAW SRM 57-41-12.Mar 18, 2008 · N425FE · Airbus A310203SDR 08FDEA01033Panel · damagedRT WING L/E LOWER SURFACE ACCESS PANEL 623 JB UPPER SURFACE SPEED TAPE IS PEELING OFF AND TORN. REMOVED DAMAGED IAW SRM 57-41-12. APPLIED NEW FOIL IAW SRM 57-41-12. APPLIED SURFACE FINISH IAW SRM 57-41-12 PG 227.Mar 18, 2008 · N425FE · Airbus A310203SDR 08FDEA01032Access Panel · chafedRT WING L/E LOWER SURFACE ACCESS PANEL 623 GB EDGES IS CHAFED AND HAS 3 WEAK SPOTS. BLENDED CHAFED AREA IAW SRM 51-73-10. ORIGINAL THICKNESS 0.056. REMAINING THICKNESS 0.054 IAW A57243224 DWG. FOUND TO BE WITHIN LIMITS. ALODINED IAW SRM 51-21-01. PRIMED IAWMar 18, 2008 · N425FE · Airbus A310203SDR 08FDEA01031Panel · erodedLEFT WING LOWER SURFACE L/E DROP PANEL (RIB 28) EXTERNAL SURFACE HAS AN ERODED AREA. REPAIRED LT WING LOWER SURFACE L/E DROP PANEL BY REMOVING DAMAGE, APPLING FOIL REPAIR, ALODINING FOIL REPAIR, APPLING FR PRIMER, AND APPLING FINISH COAT IAW SRM 57-41-12,51-2Mar 18, 2008 · N425FE · Airbus A310203SDR 08FDEA01028Panel · corrodedLT WING T/E PANEL NR 572 DB IS CHAFED AND CORRODED WITH PAINT PEELING ON THE MATING SURFACES. REPAIRED PANEL BY REMOVING DAMAGE, FABRICATING FILLER PLATE AND DOUBLER, LAYING UP REPAIR DOUBLER AND FILLER PLATE & COMPLETING CURE & REMOVING EXCESS ADHESIVE FLASH,Mar 18, 2008 · N425FE · Airbus A310203SDR 08FDEA01027Panel · chafedLT WING L/E PANEL 517 AB OUTER SKIN EDGE IS CHAFED AND CRACKED. BLENDED AREA IAW SRM 57-00-01. FOUND TO BE OUT OF LIMITS IAW SRM 57-00-01 VOL I. CUT OUT DAMAGED AREA IAW SRM 57-00-01 VOL I. FABRICATED DOUBLER & FILLER IAW 57-00-01 VOL I. ALODINED, PRIMED & Mar 18, 2008 · N365FE · Doug MD1010FSDR 08FDEA01025Panel · corrodedLT WING T/E UPPER SURFACED FIXED PANEL LOWER SURFACE SKIN HAS CORROSION AND DELAMINATION JUST ABOVE THE OUTBD FLAP TRACK. REPAIRED IAW DWG ARC0822, TPS 1001 REV E & EA 8-5710-7-116966.Mar 18, 2008 · N365FE · Doug MD1010FSDR 08FDEA01007Paint · peelingPANEL 613 JR RT WING LEADING EDGE HAS PEELING PAINT. REMOVED DAMAGE; MATERIAL ID; CLEANED & PREPPED FOR REPAIR. FILLED DAMAGED AREAS; CURED; SANDED & APPLIED FOIL REPAIR. ALODINED, PRIMED & RESTORED FINISH IAW SRM 57-41-12 & SRM 51-75-10 PARA 5-A (5) &Mar 17, 2008 · N803FD · Airbus A310203SDR 08FDEA00991Panel · crackedRIGHT WING UPPER L/E PANEL NR 617 CT IS CRACKED IN 2 PLACES. PERFORMED HFEC PER NDT SPM 06-10-09-09. MARKED CRACKS. STOP DRILLED CRACKS. FABBED DOUBLERS REF SRM 57-10-00 VOL I. ALODINED & PRIMED REF SRM 51-21-01 VOL II. INSTALLED DOUBLERS REF SRM 51-35-01 VOMar 17, 2008 · N365FE · Doug MD1010FSDR 08FDEA00978Panel · gougedLT WING LOWER SURFACE HINGED PANEL 551 DB UPPER SURFACE IS GOUGED AND BENT ON THE AFT MID SECTION. REPAIRED IAW SRM 51-71-00 VOL II. ALODINED & PRIMED REPAIR AREA IAW SRM 51-21-01 VOL II. SEALED REPAIR IAW SRM 51-71-00 & 51-71-01 VOL II. PAINTED REPAIR IMar 17, 2008 · N365FE · Doug MD1010FSDR 08FDEA00977Panel · chafedRT WING LOWER T/E PANEL NR 651 BB AT THE OUTBD FLAP IS CHAFED ON THE INBD INNER SKIN. REPAIRED IAW SRM 51-71-00 VOL II & DWG ARC 0781. REMOVED & INSTALLED PANEL & SEAL IN REF TO SRM 51-31-01 VOL II.Mar 17, 2008 · N365FE · Doug MD1010FSDR C2XA08TY034Skin Panel · crackedTYS - DURING A CURRENT 5A INSPECTION THE RT WING UPPER SKIN I/B GROUND SPOILER WAS FOUND CRACKED. MAINTENANCE REMOVED THE DAMAGED SKIN, FABRICATED A FILLER, THE DOUBLER TRIPLED DRILL AND COUNTERSUNK. ALODINED, PRIMED AND INSTALLED IAW EC5740-01141. RESTOREDMar 16, 2008 · N14939 · Emb EMB145EPSDR A6WA200840205Skin · crackedRIGHT WING LE, 620AT, AT WS 140 EDGING IS CRACKED IN RADIUS. RIGHT WING INBOARD L/E (620AT) WS 140 SHROUD CRACK REMOVED IAW REO 601R-57-41-502. (M)Mar 14, 2008 · N440AW · Cndair CL6002B19SDR 08FDEA00975Panel · damagedLEFT WING PANEL (WS 66-151) FOIL ON THE BACK OF THE PANEL IS PEELING OFF AND THE PANEL IS PUNCTURED. REPAIRED LT WING PANEL WS 66-151, BY APPLYING REPAIR PLIES IAW SRM 51-77-10 & 51-77-12. REMOVED DAMAGED FOIL IAW SRM 57-42-12. APPLIED NEW FOIL IAW SRM 57-41-1Mar 14, 2008 · N425FE · Airbus A310203SDR 08FDEA00972Skin · chafedRIGHT WING INBD SLAT; INBD OF NR 1 TRACK; INNER SURFACE FASTENERS ARE CHAFING ON THE WING L/E SKIN. BLENDED AREA SMOOTH & REMOVED DAMAGE IAW SRM 51-73-10. FOUND TO BE OUT OF LMITS IAW SRM 57-40-00. DAMAGED SECTION OF THE L/E SKIN IAW SRM 57-41-12. HEAT TREAMar 14, 2008 · N425FE · Airbus A310203SDR 08FDEA00971Panel · damagedRIGHT WING L/E PANEL UPPER SURFACE; APPROX RIB 14 HAS THE PROTECTIVE METAL TAPE LOOSE AND PAINT PEELING. REMOVED DAMAGED FOIL IAW SRM 57-41-12. APPLIED NEW FOIL IAW SRM 57-41-12. APPLIED PROTECTIVE FINISH IAW A310 SRM 51-75-10. PRIMED IAW SRM 57-41-12.Mar 14, 2008 · N425FE · Airbus A310203SDR 08FDEA00970Panel · chafedRIGHT WING PANEL NR 672 CB UPPER SKIN IS CHAFED. REPAIRED IAW SRM 51-77-10 & BONDED IT IAW SRM 51-77-12. REFINISHED AREA IAW SRM 51-75-10.Mar 14, 2008 · N425FE · Airbus A310203SDR 08FDEA00965Panel · delaminatedRIGHT WING LOWER T/E PANEL NR 641LB IS DELAMINATED. REPAIRED PANEL BY FABRICATING & BONDING SKINS, CORE, DOUBLERS AND PHENOLIC FILLER IAW EA 8-5720-118473; DWG ARC0357 & TPS 1001, REV E.Mar 14, 2008 · N365FE · Doug MD1010FSDR 08FDEA00964Panel · delaminatedRIGHT WING UPPER L/E PANEL NR 618 BT IS DELAMINATED. REPAIRED PANEL IAW DWG ARB1100, TPS 1001 REV E & EA. 8-5710-116969.Mar 14, 2008 · N365FE · Doug MD1010FSDR 08FDEA00960Panel · delaminatedLEFT WING LOWER T/E PANEL NR 541 NB IS DELAMINATED. REPAIRED IAW SRM 51-71-00; VOL II.Mar 14, 2008 · N365FE · Doug MD1010FSDR 08FDEA00959Panel · debondedRIGHT WING PANEL NR 641 EB; CORNER IS DISBONDED. RESTORED TO ORIGINAL IAW SRM 51-71-00, 51-21-01 & 51-21-02 VOL II.Mar 14, 2008 · N365FE · Doug MD1010FSDR 08FDEA00955Skin · chafedCHAFED INTERIOR SKIN REPAIR DOUBLER ON PANEL NR 535 DL. REMOVED DAMAGED DOUBLER. CLEANED & PREPPED AREA. FABRICATED NEW DOUBLER & FILLER. APPLIED A HOT BOND, SEALED EDGES WITH SEALANT. PRIMED & PAINTED IAW SRM 51-71-00 VOL II.Mar 14, 2008 · N365FE · Doug MD1010FSDR 08FDEA00954Skin · dentedPANEL NR 541 CR EXTERNAL SKIN IS DENTED AND GOUGED. REPAIRED DENT & GOUGED PANEL BY REMOVING THE DAMAGE AT THE OUTER SKIN SECTION. FABRICATING & BONDING A REPAIR SKIN SECTION & DOUBLER IAW SRM 51-71-00 VOL II. ALODINED & PRIMED REPAIR AREA IAW IAW 51-21-01Mar 14, 2008 · N365FE · Doug MD1010FSDR 08FDEA00950Skin · corrodedRIGHT WING UPPER SURFACE SKIN HAS AREAS OF CORROSION ALONG FRONT SPAR ATTACH ROW STA 556-565. REMOVED CORROSION IAW SRM 51-74-10 & WAS FOUND TO BE OUT OF LIMITS. ACCOMPLISHED HFEC OF HOLES IAW NTM 51-10-01. FLAT PEENED AREA IAW SRM 51-25-00. ALODINED IAW SRM Mar 14, 2008 · N803FD · Airbus A310324SDR 08FDEA00945Skin · debondedRT WING UPPER L/E SKIN PANEL AT STA WQFS 66-151 LINER FOIL IS DISBONDED AND TORN. REMOVED & REPLACED DAMAGED FOIL IAW SRM 57-41-12.Mar 14, 2008 · N425FE · Airbus A310203SDR 08FDEA00934Panel · delaminatedLEFT WING PANEL 577 BT IS DELAMINATED IN NUMEROUS PLACES. REMOVED DAMAGED; PREPED FOR BOND, LAYED UP, VAC BAGGED & CURED REPAIR IAW SRM 51-77-12 & 51-77-10. RESTORED PROTECTIVE FINISH IAW SRM 51-75-10.Mar 14, 2008 · N425FE · Airbus A310203SDR IXXA080022SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT RIGHT WING UPPER AFT SKIN PANEL. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. CLEANED, TRMar 13, 2008 · N602AL · Doug DC873FSDR IXXA08SMN092SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT LEFT WING UPPER AFT SKIN PANEL. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. CLEANED, TREMar 13, 2008 · N602AL · Doug DC873FSDR WRLA2008039Skin · corrodedDURING C-CHECK INSPECTION FOUND RIGHT WING UPPER SURFACE AT REAR SPAR, FROM XORS 264 TO XORS 480 SKIN CORRODED AT SEVERAL PLACES. REPAIRED RIGHT WING SURFACE AT REAR SPAR FROM XORS 264 - XORS 480 AT AREAS OF CORROSION PER ECRA 242NW-57-DC10-017.Mar 13, 2008 · N138WA · Doug DC1030SDR 08FDEA00906Retainer · gougedLEFT WING INBD T/E PANEL 541 GB SEAL HOLDER IS GOUGED. REMOVED GOUGED SEAL RETAINER AND REPLACED IAW SRM 51-35-01 VOL II. MINOR REPAIR.Mar 12, 2008 · N365FE · Doug MD1010FSDR 08FDEA00905Panel · crackedLEFT WING OUTBD L/E PANEL 527 AB OUTBD END ACCESS DOOR HINGE MOUNT IS CRACKED. REMOVED & REPLACED THE HINGE IAW SRM 51-35-01 VOL II.Mar 12, 2008 · N365FE · Doug MD1010FSDR 08FDEA00828Panel · crackedRT WING LOWER SKIN IS CRACKED IN THE TRAILING EDGE AREA AT WING STA 653, JUST INBD OF RIB 11. COMPLIED WITH EA 6-5730-118457 REV A.Mar 10, 2008 · N425FE · Airbus A310203SDR A6WA200840176Skin · delaminatedREQUEST INSPECTION RIGHT WINGLET TRAILING EDGE DELAMINATED/PILOT FOUND ON WALK AROUND. (M)Mar 9, 2008 · N458AW · Cndair CL6002B19SDR UIEA200800080Skin · corrodedLEFT WING UPPER SKIN REAR SPAR CORRODED LEVEL 1. CORROSION CLEANED UP AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02.Mar 9, 2008 · N355MC · Boeing 747341SDR 08FDEA00798Skin · crackedRT WING, DROOP LEADING EDGE SURFACE FOUND CRACKED AT FASTENER HOLE. REPAIRED AS PER SRM 57-10-00 FIGURE 30 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Mar 9, 2008 · N521FE · Doug MD11FSDR 08FDEA00797Skin · crackedLEFT WING, NR 3 LEADING EDGE SLAT TELESCOPIC DUCT CUTOUT INBOARD CORNER FOUND CRACK. REPAIRED AS PER SRM 57-10-00 FIGURE 43 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Mar 9, 2008 · N521FE · Doug MD11FSDR C2XA08TY033Skin · crackedA 1.26 LONG CRACK WAS DISCOVERED ON THE LT WING UPPER TRAILING EDGE SKIN ADJACENT TO THE CENTER SPOILER HINGE CUTOUT. REPAIRED CRACK IAW EC5740-01140. AIRCRAFT RELEASED AND RETURNED TO SERVICE.Mar 7, 2008 · N14930 · Emb EMB145EP
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