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 FDEA201008052843Skin · crackedRT WING FIXED L/E ANTI ICE TELESCOPE DUCT DOOR CUT-OUT. EXTERIOR SKIN FOUND CRACKED. RT WING FIXED L/E ANTI ICE TELESCOPE DUCT DOOR CRACKED CUT-OUT EXTERIOR SKIN REPAIRED IAW EA 8-5710-140444, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.Aug 5, 2010 · N396FE · Doug MD1010FSDR QXEA2010080400469Panel · corrodedTHERE ARE SMALL AREAS OF CORROSION ON THE TOP SIDE OF PANEL 144JZ. REMOVED CORROSION IAW SRM 51-21-00. HFEC IAW NDTM PART 6, 51-00-01 AT BLENDED AREAS. NO CRACKS NOTED. LIGHT CORROSION ONLY WITH LESS THAN .002" MATERIAL REMOVED. ALODINED AND PRIMED AS REQAug 3, 2010 · N410QX · Bombdr DHC8402SDR QXEA2010080400468Skin · corrodedC-CHECK - THERE ARE SEVERAL AREAS OF FRETTING CORROSION ON THE BOTTOM SURFACE OF PANEL 624FT. BLENDED AREAS OF LIGHT FRETTING CORROSION ON THE BOTTOM SURFACE OF PANEL 624FT IAW SRM 51-21-00. ETCHED AND ALODINED BLENDED AREAS IAW SRM 51-21-00-PG2 PARA (A)(2)AAug 3, 2010 · N410QX · Bombdr DHC8402SDR QXEA2010080400467Panel · corrodedC CHECK - THERE ARE SEVERAL AREAS OF FRETTING CORROSION ON THE BOTTOM MATING SURFACE OF PANEL 624ET. REMOVED THE FRETTING CORROSION ON THE BOTTOM MATING SURFACE OF PANEL 624ET IAW SRM 51-21-00. REPROTECTED THE REQUIRED AREAS WITH ALODINE IAW SRM 51-21-00.Aug 3, 2010 · N410QX · Bombdr DHC8402SDR QXEA2010080400466Panel · corrodedC CHECK - THERE ARE SEVERAL AREAS OF FRETTING, CORROSION ON THE BOTTOM MATING SURFACE OF PANEL 624DT. REMOVED THE FRETTING, CORROSION ON THE BOTTOM MATING SURFACE OF PANEL 624DT IAW SRM 51-21-00. REPROTECTED THE REQUIRED AREAS WITH ALODINE IAW SRM 51-21-00.Aug 3, 2010 · N410QX · Bombdr DHC8402SDR QXEA2010080400465Panel · corrodedC CHECK - THERE ARE SEVERAL AREAS OF FRETTING, CORROSION ON THE BOTTOM MATING SURFACE OF PANEL 624CT. BLENDED AREAS OF LIGHT FRETTING, CORROSION ON THE BOTTOM MATING SURFACE OF PANEL 624CT. ETCHED AND ALODINED AND APPLIED PRIMER TO BLENDED AREAS THAT REQUIREDAug 3, 2010 · N410QX · Bombdr DHC8402SDR QXEA2010080400464Skin · corrodedC-CHECK - THERE ARE SEVERAL AREAS OF FRETTING, CORROSION ON THE BOTTOM MATING SURFACE OF PANEL 624BT. BLENDED AREAS OF LIGHT FRETTING CORROSION ON THE BOTTOM MATING SURFACE OF PANEL 624BT. REPROTECTED THE REQUIRED AREAS WITH ALODINED IAW SRM 51-21-00.Aug 3, 2010 · N410QX · Bombdr DHC8402SDR QXEA2010080300463Skin · corrodedC CHECK - THERE ARE SEVERAL AREAS OF FRETTING CORROSION ON THE BOTTOM MATING SURFACE OF PANEL 624AT. BLENDED AREAS OF LIGHT FRETTING CORROSION ON THE BOTTOM MATING SURFACE OF PANEL 624AT. ETCHED AND ALODINED BLENDED AREAS IAW SRM 51-21-00, PARA A(2)A-C.Aug 3, 2010 · N410QX · Bombdr DHC8402SDR FDEA201008032790Doubler · crackedRT WING L/E UPPER SKIN INTERNAL BEADED DOUBLER HAS CRACKS EXTENDING BEYOND THE REPAIR DOUBLER (8 PLACES ) AT XORS 570. CUT OUT BEADED DOUBLER AND FABRICATED DOUBLER, FILLER AND REPAIR ANGLES IAW EA 8-5710-123547 "WINGS - RT WING L/E BEADED DOUBLER CRACKED - REAug 3, 2010 · N567FE · Doug MD1010FSDR R61A20100366Skin · crackedWHILE A/C WAS IN FOR MID C CHECK PERFORMED ETD 2010-170/06372 AND RE572008.Aug 1, 2010 · N802MD · Emb ERJ170100SDR 2010FA0000917Skin · cracked(SPUY) RT WING NR 4 STUB WING LWR SKIN CRACKED APPROX 1.5" (CORRECTING SOURCE DOCUMENT: INS-100R-5700).Jul 31, 2010 · N71CX · Doug DC862FSDR 2010FA0000915Skin · corroded(SPUY) RT WING OTBD L/E OUTER SECTION LWR SKIN CORRODED (XFS 710.000-760.000).Jul 31, 2010 · N71CX · Doug DC862FSDR 2010FA0000913Skin · corroded(SPUY) RT WING UPPER SKIN CORRODED AT AROUND STA XRS 74.889.Jul 31, 2010 · N71CX · Doug DC862FSDR 2010FA0000905Skin · corroded(SPUY) LT WING - UPPER PANEL EXTERNAL SKIN CORRODED AT STA XRS 204.000 S-14.Jul 31, 2010 · N71CX · Doug DC862FSDR FDEA201007302730Skin · crackedLH WING DEEP WEAR ON UPPER EXTERNAL SKIN L/E AT STA XOS405 PERFORMED REPAIR IAW SRM 57-10-00 PAG.96 FIG.28 VOL.1Jul 30, 2010 · N320FE · Doug MD1030FSDR FDEA201007302731Skin · chafedLEFT WING DEEP WEAR ON EXTERNAL SKIN L/E FROM STA XOS 430 TO STA XOS 465 PERFORMED REPAIR IAW SRM 57-10-00 FIG.40 SH.1 VOL.1Jul 30, 2010 · N320FE · Doug MD1030FSDR IPXA10M61558Doubler · chafedINSPECTION TYPE:1C, LT TELESCOPIC DUCT CUTOUT DOUBLER CHAFED. REMOVED DOUBLER, CUT OUT SKIN, FABRICATED AND INSTALLED REPAIR FILER AND DOUBLER IAW SRM 57-40-01, REPAIR 10.Jul 28, 2010 · N250UP · Doug MD11FSDR FDEA201007272677Skin · crackedDURING HFEC OPEN HOLE INSPECTION 13 EA FASTENER HOLES FOUND CRACK INDICATION AT R/H WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN STA. XORS= 690 AND STA. XORS= 700. REPAIR CARRIED OUT AT RT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN STA XORS= 690 AND STA.Jul 27, 2010 · N613FE · Doug MD11FSDR FDEA201007272676Skin · crackedDURING HFEC OPEN HOLE INSPECTION 09 EA FASTENER HOLES FOUND CRACK INDICATION AT LT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN STA. XORS= 690 AND STA. XORS= 700. REPAIR CARRIED OUT AT LT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN STA XORS= 690 AND STA. XORJul 27, 2010 · N613FE · Doug MD11FSDR IPXA10M61557Skin · chafedINSPECTION TYPE:1C, RT WING TELESCOPIC DUCT CUTOUT DOUBLER CHAFED. REMOVED DOUBLER, CUTOUT DAMAGE,FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLERS IAW SRM 57-40-01, REPAIR 10.Jul 27, 2010 · N250UP · Doug MD11FSDR UALA2010072702710Panel · damagedLEFT T/E PANEL HAS FASTENERS PULLING THROUGH REPAIR. REPLACED FASTENERS PER MM. NOW WITHIN TOLERANCE.Jul 27, 2010 · N199UA · Boeing 747422SDR FDEA201007272675Skin · crackedLT WING DROOP L/E UPPER OTBD SKIN CRACKED. REPAIR CARRIED OUT AT LT WING DROOP L/E UPPER OTBD SKIN IAW SRM 57-40-01, FIG 201, REV 43. FABRICATED REPAIR DOUBLER AND INSTALLED IAW SRM 57-40-01, FIG 201, REV 43. THIS REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-1Jul 27, 2010 · N613FE · Doug MD11FSDR FDEA201007262691Skin · crackedRIGHT WING LEADING EDGE SKIN AT THE NR 3 SCREW JACK CUTOUT UPPER INBD CORNER. VERIFIED CRACK BY HFEC IAW NTM PT6 51-10-08, CRACK FOUND. REMOVED DAMAGED SKIN SECTION IAW SRM 57-44-12, FIG 203. MATERIAL ID FOR A REPAIR PARTS 0.063 7075-T6, PO 678296.3 PER A30Jul 26, 2010 · N741FD · Airbus A300B4622RSDR CNMA20100028Panel · corrodedEXFOLIATED CORROSION ON RT WING LOWER PLATE BELOW ACCESS PANEL 616BB AT XQRS 346. REMOVED DAMAGED SECTION OF LOWER WING SKIN, ACCOMPLISHED SURFACE SCAN AND OPEN HOLE HFEC INSP, ROTO PEENED AFFECTED AREA. FABRICATED ALL REPAIR PARTS. INSTALLED ALL REPAIR PARTSJul 24, 2010 · N522AX · Doug DC1030SDR FDEA201007232649Skin · misrepairedEXISTING REPAIR FOUND AT LT WING (TELESCOPIC DUCT) L/E UPPER SKIN. EXISTING REPAIR FOUND AT LT WING (TELESCOPIC DUCT) L/E UPPER SKIN EVALUATED AND FOUND NOT IAW ANY SRM REPAIR SCHEME. EXISTING REPAIR REMOVED AND NEW REPAIR CARRIED OUT IAW EA8-5710-138589. Jul 23, 2010 · N383FE · Doug MD1010FSDR A6WA201040551Skin · chafedLT AILERON LOWER L/E SKIN CHAFED, EVALUATED LT AILERON LOWER L/E SKIN. BLENDED CHAFE AREAS MATERIALS THICKNESS FOUND TO BE WITHIN LIMITS IAW REO 601R-57-60-020.Jul 23, 2010 · N449AW · Cndair CL6002B19SDR UALA2010072602689Panel · damagedLT WING LWR LEADING EDGE PANEL 511DB COUNTERSUNK HOLES TOO LOOSE FOR FASTENERS TO SECURE PANEL. PANEL WAS SENT TO SHOP 273 R&R R25419. PANEL REPAIRED ON R&R R25419, RE-INSTALLED PANEL.Jul 23, 2010 · N545UA · Boeing 757222SDR UALA2010072302645Panel · damagedPANEL NR 3 LEFT AFT LEADING EDGE LANDING DAMAGED. REMOVED DAMAGED PART. FASTENERS ARE STILL INTACT IN WING. DRILLED OFF ANGLE. BEGAN TO MFG PART FROM 7075-T6 .040 ANGLE IS TEMPORARILY ATTACHED TO ACFT AND PILOT DRILLED WITH NR11. INSTALLED ANGLE. REMOVEDJul 23, 2010 · N459UA · Airbus A320232SDR A6WA201040559Skin · damagedDENT ON TOP FUSELAGE BETWEEN STR 0 AND BETWEEN FUSELAGE STATIONS 625 AND 640. REPAIRED DENT ON TOP FUSELAGE BETWEEN STR 0 & STR 11 AND FS 625 AND 640.Jul 21, 2010 · N449AW · Cndair CL6002B19SDR UALA2010072202617Access Panel · leakingFOUND FUEL LEAKING FROM UNDERSIDE LT WING FUEL OVAL PANEL, OUTBOARD OF LF ENG 2ND PANEL INBOARD OF FUEL VENT. REPLACED LEFT WING FUEL TANK ACCESS PANEL 542DB, LEAK CHECKS OK.Jul 21, 2010 · N546UA · Boeing 757222SDR FDEA201007202612Skin · misrepairedLT WING NR4 SLAT INNER SKIN AT STA XOS 549 FOUND EXISTING REPAIR. EXISTING REPAIR AT LT WING NR4 SLAT INNER SKIN AT STA XOS 549 EVALUATED AND FOUND NOT IAW ANY SRM REPAIR SCHEME. EXISTING REPAIR REMOVED IAW SRM 51-31-01 VOL II, REV 96 AND NEW REPAIR CARRIED Jul 20, 2010 · N383FE · Doug MD1010FSDR IPXA10M61495Skin · crackedINSPECTION TYPE:2C, RT WING TELESCOPIC DUCT CUT-OUT CRACKED AT UPPER INBD AND OTBD CORNER. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLER IAW SRM 57-40-01, REPAIR 10, FIG 201, REV 43.Jul 20, 2010 · N272UP · Doug MD11FSDR FDEA201007202624Skin Panel · crackedLT WING LWR SKIN PANEL INBD OF RIB 9 SUPPORT FLANGE CRACKED, JOGGLED SECTION. DAMAGED FLANGE CUT AND REPAIRED IAW E 6-5710-7-5013 PT5.Jul 20, 2010 · N661FE · Airbus A300F4605RSDR FDEA201007202622Skin Panel · crackedOPEN R 1EA BOLT HOLE (POSITION G) WAS FOUND CRACK AT THE RI B 9 BOTTOM SKIN PANEL OF RT WING. IAW EO E6-5710-7-501 PT6. SKIN CRACK AREA REPAIRED IAW EA:6-5710-141607.Jul 20, 2010 · N661FE · Airbus A300F4605RSDR FDEA201007202626Skin Panel · crackedTPE OPEN R 1 EA CRACK WAS FOUND FROM THE FASTENER HOLE AT THE R IB 9 BOTTOM SKIN PANEL OF LT WING. THE CRACK LENGTH IS .5" IAW EO E6-5710-7-5013 PT1. SKIN CRACK AREA REPAIRED IAW EA 6-5710-141607. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jul 20, 2010 · N661FE · Airbus A300F4605RSDR FDEA201007202625Skin Panel · crackedTPE OPEN R 1 EA CRACK WAS FOUND FROM THE FASTENER HOLE AT THE R IB 9 BOTTOM SKIN PANEL OF RT WING. THE CRACK LENGTH IS .2500" IAW EO E6-5710-7-5013 PT2. SKIN CRACK AREA REPAIRED IAW EA 6-5710-141607. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jul 20, 2010 · N661FE · Airbus A300F4605RSDR FDEA201007202623Skin Panel · crackedOPEN R 1 EA BOLT HOLE (POSITION G) WAS FOUND CRACKED AT THE R INBD 9 BOTTOM SKIN PANEL OF LT WING . IAW EO E6-5710-7 -5013. SKIN CRACK AREA REPAIRED IAW EA 6-5710-141607 (WINGS-AD 2008-06-18-EO 6-5710-5013 PT1- INSPECT AND MOD LOWER SKIN PANEL INBD OF RIB 9 Jul 20, 2010 · N661FE · Airbus A300F4605RSDR 2010FA0000754Access Panel · corrodedCORROSION ON LT WING FUEL TANK ACCESS PANEL. NO CORROSION REMOVAL LIMITS FOUND IN SRM. PANEL IS LISTED AS A PRIMARY STRUCTURAL ELEMENT. REMOVED PANEL AND REPLACED WITH NEW PANEL.Jul 20, 2010 · N526JL · Airbus A320232SDR 2010FA0000753Access Panel · corrodedCORROSION ON LT WING FUEL TANK ACCESS PANEL 540MB. NO CORROSION REMOVAL LIMITS FOUND IN SRM. PANEL IS LISTED AS A PRIMARY STRUCTURAL ELEMENT. REMOVED PANEL AND REPLACED WITH NEW PANEL.Jul 20, 2010 · N526JL · Airbus A320232SDR 2010FA0000752Access Panel · corrodedCORROSION ON RT WING FUEL TANK ACCESS PANEL 640KB . NO CORROSION REMOVAL LIMITS IN SRM. PANEL IS LISTED AS A PRIMARY STRUCTURAL ELEMENT. REMOVED PANEL AND REPLACED WITH NEW PANEL.Jul 20, 2010 · N526JL · Airbus A320232SDR 2010FA0000751Access Panel · corrodedCORROSION ON LT WING FUEL TANK ACCESS PANEL 540KB. NO CORROSION REMOVAL LIMITS FOUND IN SRM. PANEL IS LISTED AS A PRIMARY STRUCTURAL ELEMENT. REMOVED PANEL AND REPLACED WITH NEW PANEL.Jul 20, 2010 · N526JL · Airbus A320232SDR LR7A2010072000024Skin · crackedDURING SCHEDULED C-9 CHECK WHILE REPLACING LT RAINBOW FITTINGS FOUND LOWER CTR WING NR 2 PLANK LAYERS AT STRINGER 16 AND BETWEEN STRINGER 16 & 17, & STRINGER 12 SWORD FITTING LAYERS WITH FASTENER HOLES CRACKED AT CWS 220, WL 256.5. REPAIRED IAW LAC MEA 382-57Jul 19, 2010 · N404LC · Lkheed 382GSDR LR7A2010072000023Skin · crackedDURING SCHEDULED C-9 CHECK WHILE REPLACING LT RAINBOW FITTINGS FOUND LOWER CTR WING PLANK & STRINGER 15 SWORD FITTING LAYERS WITH FASTENER HOLE CRACKS AT CWS 220, WL 256.5. REPAIRED IAW LAC MEA 382-57-10-014.Jul 19, 2010 · N404LC · Lkheed 382GSDR 2010FA0000747Access Panel · corrodedCORROSION ON FUEL TANK ACCESS PANEL 640HR. NO CORROSION REMOVAL LIMITS FOUND IN SRM. PANEL IS LISTED AS A PRIMARY STRUCTURAL ELEMENT. REPLACED PANEL WITH NEW PANEL.Jul 19, 2010 · N526JL · Airbus A320232SDR 2010FA0000745Access Panel · corrodedCORROSION ON RT WING FUEL TANK ACCESS PANEL 640MB. NO CORROSION REMOVAL LIMITS FOUND IN SRM. PANEL IS LISTED AS A PRIMARY STRUCTURAL ELEMENT. REPLACED PANEL WITH NEW PANEL.Jul 19, 2010 · N526JL · Airbus A320232SDR 2010FA0000744Access Panel · corrodedCORROSION ON LEFT WING FUEL TANK ACCESS PANEL 540QB. NO CORROSION REMOVAL LIMITS FOUND IN SRM. PANEL IS LISTED AS A PRIMARY STRUCTURAL ELEMENT. REPLACED PANEL WITH NEW PANEL.Jul 19, 2010 · N526JL · Airbus A320232SDR 2010FA0000743Access Panel · corrodedCORROSION ON LT WING FUEL TANK ACCESS PANEL 550AB. NO CORROSION REMOVAL LIMITS FOUND IN SRM. PANEL IS LISTED AS A PRIMARY STRUCTURAL ELEMENT. REPLACED PANEL WITH NEW PANEL.Jul 19, 2010 · N526JL · Airbus A320232SDR 2010FA0000742Access Panel · corrodedCORROSION ON FUEL TANK ACCESS PANEL 540PB. NO CORROSION REMOVAL LIMITS FOUND IN SRM. PANEL IS LISTED AS A PRIMARY STRUCTURAL ELEMENT. REPLACED PANEL WITH NEW PANEL.Jul 19, 2010 · N526JL · Airbus A320232SDR 2010FA0000741Access Panel · corrodedCORROSION ON FUEL TANK ACCESS PANEL 540NB. NO CORROSION REMOVAL LIMITS FOUND IN SRM. PANEL IS LISTED AS PRIMARY STRUCTURAL ELEMENT. REPLACED PANEL WITH NEW PANEL.Jul 19, 2010 · N526JL · Airbus A320232SDR 2010FA0000740Access Panel · corrodedCORROSION ON RT WING FUEL TANK ACCESS PANEL 640NB. NO CORROSION REMOVAL LIMITS FOUND IN SRM. PANEL IS LISTED AS A PRIMARY STRUCTURAL ELEMENT. REPLACED PANEL WITH NEW PANEL.Jul 19, 2010 · N526JL · Airbus A320232
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