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 IPXA12M75322Doubler · crackedINSPECTION TYPE:4C, LT WING FIXED L/E COMPT BEADED DOUBLER CRACKED AT STA XOS636. REPAIRED LT WING FIXED L/E COMPT BEADED DOUBLER AT XOS636 REF MD11-5730-42916-D.Aug 29, 2012 · N293UP · Doug MD11FSDR QXEA2012082900965Access Panel · damagedPOSSIBLE CORROSION ON RT WING SKIN FUEL ACCESS PANEL LANDING, MATING SURFACE FOR PANEL 622AT. REMOVED CORROSION IAW RD 8/4-57-441. MIN REMAINING THICKNESS NOTED .177/.279 (LANDING) T FITTING .210/.244. CONFIRMED CRACK FREE AREAS REF NTM 51-00-04-910-801 PT Aug 29, 2012 · N409QX · Bombdr DHC8402SDR QXEA2012082900964Access Panel · damagedPOSSIBLE CORROSION ON CHAFE DAMAGE ON RT WING SKIN FUEL ACCESS PANEL LANDING, MATING SURFACE FOR PANEL 622CT. REMOVED CORROSION IAW RD 8/4-57-441. MIN REMAINING THICKNESS NOTED LANDING .178, T FITTING .238", CONFIRMED CRACK FREE AREAS REF NTM 51-00-04-910-80Aug 29, 2012 · N409QX · Bombdr DHC8402SDR QXEA2012082900963Access Panel · damagedCHAFE DAMAGE ON LT WING SKIN FUEL ACCESS PANEL LANDING, MATING SURFACE FOR PANEL 522BT. REMOVED CHAFE DAMAGE IAW RD 8/4-57-441. MIN REMAINING THICKNESS NOTED .186", CONFIRMED CRACK FREE AREA REF NTM 51-00-04-910-801 PT 1 AND 51-00-06-910-801 PT 1. LANDING FAug 29, 2012 · N409QX · Bombdr DHC8402SDR QXEA2012082500962Access Panel · corrodedPOSSIBLE CORROSION ON LT WING SKIN FUEL ACCESS LANDING MATING SURFACE FOR PANEL 522CT. REMOVED CORROSION IAW RD 8/4-57-441. MIN REMAINING THICKNESS .180, CONFIRMED CRACK FREE AREA REF 51-00-04-910-801 PT 1 AND 51-00-06-910-801 PT 1. FOUND IN LIMITS IAW SRM Aug 25, 2012 · N409QX · Bombdr DHC8402SDR QXEA2012082500916Access Panel · corrodedPOSSIBLE CORROSION ON RT WING SKIN FUEL ACCESS PANEL LANDING MATING SURFACE FOR PANEL 621BT. REMOVED CORROSION IAW RD 8/4-57-441. MIN REMAINING THICKNESS .173", CONFIRMED AFFECTED AREA CRACK FREE REF 51-00-04-910-801 PT 1 AND 51-00-06-910-801 PT 1. PANEL LAAug 25, 2012 · N409QX · Bombdr DHC8402SDR 7AHR20120825003Panel · corrodedLT WING L/E PANEL 1171C HAS SURFACE CORROSION. REMOVED REPAIR DOULBLER FOR ACCESS TO CORROSION. AFTER REMOVAL OF CORROSION, IT WAS FOUND TO BE OUT OF LIMITS, IAW SRM 51-10-03, PG 34. FABRICATED A NEW REPAIR DOUBLER AND INSTALLED IAW SRM 51-01, PG 15-17 AND Aug 25, 2012 · N125MN · Doug DC983SDR SWAA2012120310145Panel · crackedRIGHT WING UPPER SURFACE, AFT PYLON AREA, PANEL 58710R PLASTIC NUT PLATE STRIP CRACKED. REMOVED AND REPLACED RIGHT WING UPPER SURFACE PANEL 58710R NUT STRIP AS PER SRM. SEE SAM 326 FOR INDIVIDUALS STEP AND FUEL TANK ENTRY SAM 1045 AND PERFORMANCE WO# 13027 FAug 24, 2012 · N387SW · Boeing 7373H4SDR SWAA2012120310144Nut Plate · crackedRIGHT WING UPPER SURFACE, AFT PYLON AREA, PANEL 58710R PLASTIC NUT PLATE STRIP CRACKED. REPAIRED NUT PLATE STRIP PER EA 1-354-1480.Aug 24, 2012 · N387SW · Boeing 7373H4SDR QXEA2012082400961Access Panel · corrodedPOSSIBLE CORROSION ON RT WING SKIN FUEL ACCESS PANEL LANDING MATING SURFACE FOR PANEL 622BT. REMOVED CORROSION IAW RD 8/4-57-441. MIN REMAINING THICKNESS NOTED LANDING .181" T- FITTING .210(MIN) .244 (MAX), CONFIRMED ALL AREAS CRACK FREE REF NTM 51-00-04-910Aug 24, 2012 · N409QX · Bombdr DHC8402SDR QXEA2012082400915Access Panel · corrodedPOSSIBLE CORROSION ON LT WING SKIN FUEL ACCESS PANEL LANDING MATING SURFACE FOR PANEL 524AT. REMOVED CORROSION IAW RD 8/4-57-445. MIN REMAINING THICKNESS .076, CONFIRMED AFFECTED AREA CRACK FREE, REF NTM 51-00-04-910-801 PT 1 AND 51-00-06-910-801 PT 1. REPAAug 24, 2012 · N409QX · Bombdr DHC8402SDR QXEA2012082400914Access Panel · corrodedPOSSIBLE CORROSION ON RT WING SKIN FUEL ACCESS PANEL LANDING MATING SURFACE FOR PANEL 624BT. REMOVED CORROSION IAW RD 8/4-57-445. MIN REMAINING THICKNESS .075, CONFIRMED AREA IS CRACK FREE REF NTM 51-00-04-910-801 PT 1 AND 51-00-06-910-801 PT 1. REPAIR FOUNAug 24, 2012 · N409QX · Bombdr DHC8402SDR QXEA2012082400910Access Panel · corrodedRIGHT FUEL ACCESS PANEL 624BT HAS POSSIBLE CORROSION ON MATING SURFACE. REMOVED CORROSION IAW RD 8/4-57-442, FOUND WITHIN LIMITS OF RD 8/4-57-442. ALODINED IAW SRM 51-21-10-02-01. CONFIRMED MATING SURFACE CRACK FREE REF NDTM 51-00-06-910-801 PT 1. COMPLIEDAug 24, 2012 · N409QX · Bombdr DHC8402SDR USAA2012091000039Access Door · corrodedS2 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON LOWER LEFT WING FUEL ACCESS DOOR 540RB BETWEEN WING RIB 21 & RIB 22, ALSO BETWEEN S8L TO S11L. REPLACED LEFT WING FUEL ACCESS DOOR 540RB IAW A319 SRM 57-27-11.Aug 23, 2012 · N744P · Airbus A319112SDR RJEF2012082406Structure · damagedAT ARRIVAL, FLIGHT TP148, A BIRD STRIKE WAS FOUND NEAR LEFT WING TIP AREA OVER RIB 42. IAW FIM 05-50-02-200-801-A, THE RIB 42 WAS FOUND DAMAGED. PERFORMED PERMANENT REPAIR FOR STRUCTURAL DAMAGED LOCATED AT RIB 42 WING LT IAW EO ERJPR57-015/12 REVISION 00. Aug 23, 2012 · N984TA · Emb ERJ190100IGWSDR USAA2012082300002Fuel Door · corroded2S CHECK - LEVEL 2 INTERGRANULAR CORROSION ON LEFT WING LOWER FUEL DOOR 540JB BETWEEN WING RIB 14 TO RIB 15 & BETWEEN S8L TO S11L. REPLACED LEFT WING LOWER FUEL DOOR 540JB IAW A319 SRM 57-27-11.Aug 23, 2012 · N744P · Airbus A319112SDR CHQA20120822346Skin · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE LEFT WING UPPER SKIN AT THE GROUND SPOILER CENTER HINGE CUTOUT. THE LEFT WING UPPER SKIN AT THE GROUND SPOILER HINGE CUTOUT WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-011887.Aug 22, 2012 · N271SK · Emb EMB145LRSDR FDEA201208223103Panel · corrodedRT WING T/E PANEL NR 641JB CUT OUT LOWER SURFACE FOUND CORRODED. R & R IAW SRM 51-31-01, REV 50. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.Aug 22, 2012 · N582FE · Doug MD11FSDR FDEA201208223102Panel · corrodedLT WING T/E PANEL 541JB CUTOUT FOUND CORRODED. R & R IAW SRM 51-31-01, REV 50. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.Aug 22, 2012 · N582FE · Doug MD11FSDR QXEA2012082000825Access Panel · damagedLEFT WING FUEL ACCESS PANEL LANDING AT APPROX STA YW48.000 HAS A BOLT HOLE WITH EDGE DAMAGE. MEASURED DAMAGE AND FOUND OUT OF LIMITS IAW RD 8/4-57-526. CONFIRMED AFFECTED AREA CRACK FREE CONDITION REF NTM 51-00-05-250-801 PT 6. COMPLIED WITH REPAIR IAW RD 8/Aug 20, 2012 · N405QX · Bombdr DHC8402SDR CA120820003Skin · dented(CAN) AFTER LANDING, EVIDENCE OF A BIRD STRIKE TO THE LT WING L/E INBD SECTION WAS NOTICED. THERE WAS SOME DAMAGE TO THE L/E SO IT WAS REPLACED. L/E PN 85720220-003.Aug 18, 2012 · Bombdr DHC8400SDR USAA2012082200012Fuel Door · corrodedS2 CHECK - CORROSION ON RIGHT LOWER WING FUEL DOOR 640KB BETWEEN RIB 15 TO RIB 16 & BETWEEN S8R TO S11R. REPLACED RIGHT LOWER WING FUEL DOOR 640KB IAW A319 SRM 57-27-11.Aug 16, 2012 · N744P · Airbus A319112SDR USAA2012081700012Access Panel · corrodedS2 CHECK. LEFT WING ACCESS PANEL 540PB CORRODED AT FASTENER LOCATIONS. REMOVED AND REPLACED PANEL IAW JOB CARD 26C54057007.Aug 16, 2012 · N744P · Airbus A319112SDR USAA2012081700011Access Panel · corrodedS2 CHECK - RIGHT WING ACCESS PANEL 640LB CORRODED AT FASTENER LOCATIONS. REMOVED AND REPLACED PANEL IAW JOB CARD 26C54057007.Aug 16, 2012 · N744P · Airbus A319112SDR DALA1245980914Panel · corrodedRT WING PNL 1456C LANDING AREA HAS PITTING. BLENDED AREA AND FOUND WITHIN LIMITS IAW MD-88 SRM 57-32-4.Aug 15, 2012 · N914DL · Doug MD88SDR DALA1245960914Panel · corrodedRT WING FUEL PNL 1462C LANDING HAS PITTING ALL. BLENDED AREA AND FOUND WITHIN LIMITS IAW MD-88 SRM 57-32-4.Aug 15, 2012 · N914DL · Doug MD88SDR IPXA12M75176Skin · corrodedINSPECTION TYPE: 4C, CENTER WING UPPER SKIN IN MAIN CABIN SUBFLOOR CORRODED NEAR BS 1234 RBL 83 (STA XCW -81 BETWEEN S14 & S15). REPAIRED CORRODED CENTER WING UPPER SKIN AT XCW -81 BETWEEN S14 AND S15 IAW EA 011-5730-01-A4213 REV IR AND EO MD11-5730-48439-A.Aug 14, 2012 · N270UP · Doug MD11FSDR IPXA2M75147Skin · corrodedINSPECTION TYPE: 4C, CENTER WING UPPER EXTERIOR SKIN CORRODED IN MAIN CABIN SUBFLOOR ABOVE STRINGER 15 RBL102, NEAR F/STA 1227 (XCW 97-101). REPAIRED CORROSION ON CENTER WING UPPER SKIN ABOVE S15 BETWEEN XCW 91-101 IAW EA 011-5730-01-A4212 REV IR & EO MD11-57Aug 14, 2012 · N270UP · Doug MD11FSDR IPXA2M75146Skin · corrodedINSPECTION TYPE: 4C, CENTER WING UPPER EXTERIOR SKIN CORRODED IN MAIN CABIN SUBFLOOR ABOVE STRINGER 15 AT LBL 114 F/STA 1227 (XCW103-109). REPAIRED CORROSION ON CENTER WING UPPER SKIN ABOVE S15 BETWEEN XCW103-109 IAW STA SA EA 011-5730-01-A4214, REV IR & EO MAug 14, 2012 · N270UP · Doug MD11FSDR FDEA201208142989Skin · crackedRT WING FIXED L/E AT STATION XOS =717 SLAT TRACK CUTOUT OTBD CORNER CRACKED. REPAIR CARRIED OUT AS PER SRM 57-40-02 REPAIR 7 FIGURE 201 REVISION 50 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.Aug 14, 2012 · N603FE · Doug MD11FSDR NI6R20120814004Skin · looseFOUND WING SKIN AT THE ATTACHING FASTENERS AT THE RT LOWER FWD SPAR CAP, RT WS 120, RUNNING FOR APPROX 4.25 INCHES TO HAVE WORKED LOOSE. SKIN CAN BE PUSHED UP AND DOWN APPROX .005. NO ADDITIONAL STRUCTURES WERE FOUND TO BE DISCREPANT BY VISUAL INSPECTION ANDAug 14, 2012 · N96264 · Lkheed P2V5FSDR NI6R20120814003Wing · crackedAT LEFT WING STATION 40, A CRACK IN THE WING SKIN, JUST OUTBOARD OF THE FUSELAGE SKIN, APPROXIMATELY 4 INCHES LONG WAS DISCOVERED UNDER AN EXISTING REPAIR USING EDDY CURRENT INSPECTION. THE CRACK RUNS FORE AND AFT BETWEEN STRINGERS 17 AND 18. NO OTHER DAMAGE HAug 14, 2012 · N9855F · Lkheed P2V5FSDR USAA2012082900032Fuel Door · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON LEFT WING LOWER FUEL DOOR 540MB BETWEEN WS 9235 TO WS 9704 & BETWEEN RIB 17 TO RIB 18. REPLACED LEFT WING LOWER FUEL DOOR 540MB IAW A319 AMM 57-27-11-400-002-A.Aug 13, 2012 · N745VJ · Airbus A319112SDR NI6R20120814006Skin · crackedFOUND WING SKIN AT THE ATTACHING FASTENERS AT THE RT LOWER FWD SPAR CAP RUNNING FOR APPROX 20 INCHES TO HAVE WORKED LOOSE. SKIN CAN BE PUSHED UP AND DOWN APPROX .020. UPON REMOVAL OF THE LEADING EDGE AND NACELLE PANEL, A FOUR INCH CRACK IN THE WING SKIN, DISAug 13, 2012 · N443NA · Lkheed P2V7SDR NI6R20120814005Skin · looseFOUND WING SKIN AT THE ATTACHING FASTENERS AT THE RT LOWER FWD SPAR CAP, R WS 120, RUNNING FOR APPROX 5.0 INCHES TO HAVE WORKED LOOSE. SKIN CAN BE PUSHED UP AND DOWN APPROX .005. NO ADDITIONAL STRUCTURES WERE FOUND TO BE DISCREPANT BY VISUAL INSPECTION AND NAug 13, 2012 · N807NA · Lkheed P2V5FSDR 2012FA0000564Skin · looseFOUND WING SKIN AT THE ATTACHING FASTENERS AT THE RT LOWER FWD SPAR CAP RUNNING FOR APPROX 20" TO HAVE WORKED LOOSE. SKIN CAN BE PUSHED UP AND DOWN APPROX .020". UPON REMOVAL OF THE L/E AND NACELLE PANEL, A 4" CRACK IN THE WING SKIN WAS DISCOVERED RUNNING AFAug 13, 2012 · N443NA · Lkheed P2V7SDR GLBA2012081300030Skin · dentedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION FOUND A DENT AT WS 290.06 ON RT WING, 9" BY 4" AREA. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-57-009. MATERIALS UTILIZED ARE INCLUDED IN THE EO.Aug 11, 2012 · N202UX · Beech 1900DSDR USAA2012081300005Access Panel · corrodedS2 CHECK - RIGHT WING FUEL ACCESS PANEL 640RB HAS CORROSION AT FASTENER HOLES. REMOVED AND REPLACED PANEL IAW JOB CARD 26C64057007.Aug 11, 2012 · N744P · Airbus A319112SDR USAA2012081300004Access Panel · corrodedS2 CHECK - RIGHT WING FUEL ACCESS PANEL 640PB HAS CORROSION AT FASTENER HOLES. REMOVED AND REPLACED PANEL IAW JOB CARD 26C64057007.Aug 11, 2012 · N744P · Airbus A319112SDR USAA2012081300003Access Panel · corrodedS2 CHECK - RIGHT WING FUEL ACCESS PANEL 640MB HAS CORROSION AT FASTENER HOLES. REMOVED AND REPLACED PANEL IAW JOB CARD 26C64057007.Aug 11, 2012 · N744P · Airbus A319112SDR USAA2012081300002Access Panel · corrodedS2 CHECK. LEFT WING FUEL ACCESS PANEL 540QB HAS CORROSION AT FASTENER HOLES. REMOVED AND REPLACED PANEL IAW JOB CARD 26C64057007.Aug 11, 2012 · N744P · Airbus A319112SDR USAA2012081300001Access Panel · corrodedS2 CHECK - LEFT WING FUEL ACCESS PANEL 540NB HAS CORROSION AT FASTENER HOLES. REMOVED AND REPLACED PANEL IAW JOB CARD 26C64057007.Aug 11, 2012 · N744P · Airbus A319112SDR FDEA201208112941Skin · crackedLT WING L/E NR 10 SLAT TRACK CUT OUT INBD CORNER FOUND CRACKED. REPAIRED IAW SRM 57-10-00, FIG 68, VOLUME I, REV 99. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.Aug 11, 2012 · N10060 · Doug MD1010FSDR IPXA12M75093Skin · crackedINSPECTION TYPE: 4C, NDT INSPECTION OF ALI 57.23.01.2 FOUND CRACKS AROUND 4 FASTENER HOLES FOR LT WING ACCESS PANEL 536AB BETWEEN XORS 683-713. REPAIRED LT WING LOWER SURFACE PANEL IAW EA 011-5730-01-A4188 REV IR, EO MD11-5730-48311-A AND SRM 57-20-02, REAug 9, 2012 · N270UP · Doug MD11FSDR IPXA2M75072Skin · crackedINSPECTION TYPE: 4C, NDT INSPECTION OF ALI 57.23.01.2, FOUND 10 CRACKS AT FASTENER HOLES AROUND CUT-OUT FOR LT WING LOWER ACCESS PANEL 536AB BETWEEN XORS 683-713. REPAIRED LT WING LOWER SURFACE PANEL CUT-OUT BETWEEN XORS 683-713 IAW EA 011-5730-01-A4187 REVAug 9, 2012 · N270UP · Doug MD11FSDR DALA12005433124Skin Panel · damagedRIGHT WING TOP SKIN PANEL NR 2, OVERWING REFUEL HOLE, BETWEEN RIBS 19 AND 20 REQUIRES FOLLOW-ON INSPECTION. REPAIR WAS ACCOMPLISHED ON N/R 640/6 DURING M CHECK AT BFM AUG 2012.Aug 8, 2012 · N324NB · Airbus A319114SDR ASOA2012091002186Skin · corrodedLEFT LOWER WING PLANK ACCESS HOLE NR 15 AT WS 294.048, 550GB HAS CORROSION MEASURING APPROX 1.3" LONG X 1.0" WIDE X .002" DEEP. COMPLIED WITH ECTC EO 600-57-81 & REO 601R-57-21-030, REV H.Aug 7, 2012 · N903EV · Cndair CL6002B19SDR ASOA2012091002185Skin · corrodedLEFT LOWER WING PLANK ACCESS HOLE NR 12 AT WS 230.415, 550DB HAS CORROSION AT INBD AND OTBD ENDS. INBD CORROSION MEASURES APPROX 1" LONG X .07" WIDE X .001" DEEP. OTBD CORROSION MEASURES APPROX 1.1" LONG X .08" WIDE X .001" DEEP. COMPLIED WITH ECTC EO 600-57Aug 7, 2012 · N903EV · Cndair CL6002B19SDR ASOA2012091002184Skin · corrodedLEFT LOWER WING PLANK ACCESS HOLE NR 10 AT WS 188.040, 550BB HAS CORROSION AT INBD AND OTBD ENDS. INBD CORROSION MEASURES APPROX 1.3" LONG X .10" WIDE X .002" DEEP. OTBD CORROSION MEASURES APPROX 1.5" LONG X .11" WIDE X .002" DEEP. COMPLIED WITH ECTC EO 600-Aug 7, 2012 · N903EV · Cndair CL6002B19SDR ASOA2012091002183Skin · corrodedLEFT LOWER WING PLANK ACCESS HOLE 8 AT WS 136.676, 540FB HAS CORROSION AT INBD, OTBD ENDS AND 2 PLACES ON AFT EDGE. INBD CORROSION MEASURES APPROX 2" LONG X .12" WIDE X .002" DEEP. OTBD CORROSION MEASURES APPROX 4.7" LONG X .11" WIDE X .002" DEEP. CORROSION ONAug 7, 2012 · N903EV · Cndair CL6002B19
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