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"

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SDR USAA2011080100037Access Panel · corroded2S CHECK - LEVEL 2 INTERGRANULAR CORROSON ON COUNTERSINK HOLES OF RIGHT WING FUEL PANEL 640HB BETWEEN WS 7316 TO WS 792 & BETWEEN WING RIB 13 TO RIB 14. REPLACED RIGHT WING FUEL PANEL 640HB IAW A319 SRM 57-27-11.Jul 3, 2011 · N723UW · Airbus A319112SDR ASOA201101261Skin · crackedCRACK ON LT LOWER SKIN WING PLANK AT WS 148.019.Jul 2, 2011 · N850AS · Cndair CL6002B19SDR IPXA1M67952Doubler · crackedINSPECTION TYPE:2C, LT WING L/E COMPT CEILING BEADED DOUBLER CRACKED AT XOS701 REPAIRED LT WING FIXED L/E INTERIOR BEADED DOUBLER BETWEEN XOS 698-703 IAW SRM 57-40-02, REPAIR 9, FIG 203 AND EO MD11-5730-42916-A.Jul 1, 2011 · N276UP · Doug MD11FSDR AALA20110701TUL04Panel · damagedFASTENERS PULLING THRU UPPER WING PANEL AT WING REAR SPAR IN EMERGENCY WALKWAY AREA. ACCOMPLISHED DOUBLER REPAIR PER EA B757-53-017708.Jul 1, 2011 · N619AA · Boeing 757223SDR ASOA201101243Skin · chafedCENTER LEFT WING BOX LOWER SKIN CHAFED AND PITTED WITH POSSIBLE CORROSION .2500" WIDE, 18" LONG, .006 DEEP, UNDER PANEL 193AB. BLENDED CHAFING AND PITTING NO CORROSION FOUND 1.5 WIDE 30IN LONG. .006 DEEP IAW SRM 57-00-31. PERFORMED UT THICKNESS OF BLEND AREAJun 30, 2011 · N832AS · Cndair CL6002B19SDR USAA2011080500012Fairing · eroded2S CHECK - EROSION ON RIGHT WING FAIRING OF NR 1 SLAT ON INBOARD SIDE BETWEEN WS 0 TO WS 700 & BETWEEN RIB 1 TO RIB 2. REPAIRED RIGHT WING FAIRING OF NR 1 SLAT ON INBOARD SIDE IAW EA 133673 & A319 SRM 51-77-12 PAR 3 B.Jun 29, 2011 · N723UW · Airbus A319112SDR CHQA201100280Skin · dentedDURING INSPECTION, THE RIGHT WING LEADING EDGE II WAS FOUND TO HAVE TWO DENTS ON THE SKIN COUPLED WITH A CRACK ON THE RIGHT LEADING EDGE II RIB. THE TWO DENTS ON THE RIGHT LEADING EDGE SKIN (PN:145-11450-604) COUPLED WITH THE CRACK ON THE RIGHT LEADING EDGE IIJun 29, 2011 · N566RP · Emb EMB145LRSDR IPXA1M68046Skin · misrepairedINSPECTION TYPE:2C RT WING FIXED L/E COMPT TELESCOPIC DUCT CUT-OUT DOUBLER GOUGED AT INBD AND OTBD BULLNOSE. AFTER DOUBLER REMOVAL FOUND SHORT ED ON FASTENER HOLES. R & R RT WING REPAIR DOUBLER AT TELESCOPIC DUCT CUT-OUT CENTERED AT APPROX XOS.467 IAW STA SJun 29, 2011 · N276UP · Doug MD11FSDR IPXA1M67953Doubler · crackedINSPECTION TYPE:2C, RT WING FIXED L/E COMPT BEADED DOUBLER CRACKED AT XOS 649. REPAIRED RT WING FIXED L/E INTERIOR BEADED DOUBLER BEWTEEN XOS 637-647 IAW SRM 57-40-02, REPAIR 9, FIG 203 AND EO MD11-5730-42916-A.Jun 29, 2011 · N276UP · Doug MD11FSDR IPXA11M67871Doubler · crackedINSPECTION TYPE:2C, RT WING FIXED L/E COMPT BEADED DOUBLER CRACKED AT XOS615. REPAIRED RT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS609-6165 IAW SRM 57-40-02, REPAIR 9, FIG 203.Jun 29, 2011 · N276UP · Doug MD11FSDR IPXA11M67870Doubler · crackedINSPECTION TYPE:2C, RT WING FIXED L/E COMPT BEADED DOUBLER CRACKED AT XOS 703 REPAIRED RT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS 698-703 SRM 57-40-02, REPAIR 9, FIG 203.Jun 29, 2011 · N276UP · Doug MD11FSDR IPXA11M67869Skin · chafedINSPECTION TYPE:1C, CHAFE DAMAGE ON LT WING L/E EXTERIOR ALONG LOWER CONTACT AREA FOR SLAT, STA XOS727-762. REPAIRED LT WING L/E EXTERIOR IAW SRM 57-40-02. REPAIR 5, FIG 201.Jun 29, 2011 · N256UP · Doug MD11FSDR IPXA11M67868Skin · chafedINSPECTION TYPE:1C, CHAFE DAMAGE ON LT WING L/E EXTERIOR ALONG LOWER CONTACT AREA FOR SLAT, STA 780-869. REPAIRED LT WING L/E EXTERIOR IAW SRM 57-40-02, REPAIR 5, FIG 201.Jun 29, 2011 · N256UP · Doug MD11FSDR IPXA1M67812Skin · chafedINSPECTION TYPE:1C, CHAFE DAMAGE ON LT WING, FIXED L/E EXTERIOR ALONG LOWER CONTACT AREA FOR SLAT STA XOS 7679-706. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW 57-40-02, REPAIR 5, FIG 201.Jun 29, 2011 · N256UP · Doug MD11FSDR IPXA11M68247Doubler · crackedINSPECTION TYPE:3C, LT WING FIXED L/E BEADED DOUBLER CRACKED AT XOS759. REPAIRED LT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN STA XOS759 -763 IAW SRM 57-40-02 REPAIR 9, FIG 203.Jun 28, 2011 · N293UP · Doug MD11FSDR IPXA11M68246Doubler · crackedINSPECTION TYPE:3C, LT WING FIXED L/E BEADED DOUBLER CRACKED AT XOS698. REPAIRED LT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS698-703 IAW SRM 57-40-02 REPAIR 9, FIG 203.Jun 28, 2011 · N293UP · Doug MD11FSDR IPXA1M67811Skin · crackedINSPECTION TYPE:1C, DETECTED 10 EA CRACK INDICATIONS IN FASTENER HOLES COMMON TO RT WING LOWER SKIN ACCESS DOOR 636AB CUT-OUT WHILE PERFORMING NDT INSP ON ACCOMPLISHED STA-SA EA 011-5730-01-A3225 I/R AND EO MD11-5730- 43374-A.Jun 28, 2011 · N256UP · Doug MD11FSDR IPXA11M67898Access Panel · crackedINSPECTION TYPE:1C, DETECTED 17EA CRACK INDICATIONS AT FASTENER HOLES COMMON TO LT FUEL PANEL ACCESS DOOR 536AB WHILE PERFORMING NDT INSPECTION IAW ALI 57.23.01. REPAIRED LT WING LOWER SURFACE FUEL ACCESS DOOR (PANEL 536AB) AND CRACKS AT XORS696 IAW STASA EA-Jun 27, 2011 · N256UP · Doug MD11FSDR IPXA1M67738Doubler · crackedINSPECTION TYPE:1C, LT WING FIXED L/E INTERIOR BEADED DOUBLER HAS TEMP REPAIR INSTALLED BETWEEN XOS 610-616. REMOVED TEMP REPAIR. INSTALLED PERMANENT REPAIR TO LT WING FIXED L/E INTERIOR BEADED DOUBLER BETWEEN XOS 610-616 IAW SRM 57-40-02, REPAIR 9 FIG.203Jun 27, 2011 · N256UP · Doug MD11FSDR IPXA1M67724Doubler · crackedINSPECTION TYPE:1C, LT WING FIXED L/E INTERNAL BEADED DOUBLER HAS A TEMP REPAIR INSTALLED BETWEEN XOS 636-643. REMOVED TEMP REPAIR INSTALLED PERMANENT REPAIR IN LT WING FIXED L/E INTERIOR ON BEADED DOUBLER BETWEEN XOS 636-643 IAW SRM 57-40-02, REPAIR 9, FIG 2Jun 27, 2011 · N256UP · Doug MD11FSDR A6WA201140729Access Panel · chafedLT WING PANEL 559AB HAS CHAFING BLENDED AREA AND FOUND TO BE WITHIN SERVICEABLE LIMITS (MAX MATERIAL REMOVED .004" IAW REO 601R-57-60-020.Jun 26, 2011 · N463AW · Cndair CL6002B19SDR UALA2011062703132Panel · damagedDAMAGE NOTED ON PANEL 621EB TRAILING EDGE. DAMAGED ON OUTBOARD SECTION NEAR ENG 2. REPLACED PANEL 621EB RT WING.Jun 26, 2011 · N828UA · Airbus A319131SDR A6WA201140518Panel · chafedLT WING PANEL 599AB HAS CHAFING BLENDED AREA AND FOUND TO BE WITHIN SERVICEABLE LIMITS ( MAX MATERIAL REMOVED .004" IAW REO 601R-57-60-020.Jun 26, 2011 · N463AW · Cndair CL6002B19SDR UALA2011062703177Skin · deterioratedLEFT WING UPPER WING PANEL AT APPROXIMATE LOCATION WS 1056 INBOARD OF NR 1 ENG HAS DETERIORATED SURFACE PROTECTION AND EXPOSED MATERIAL. REPAIRED PER SRM. REPAIR TAP CHECKED GOOD.Jun 25, 2011 · N173UA · Boeing 747422SDR IPXA1M67737Doubler · crackedINSPECTION TYPE:1C, LT WING L/E COMP'T BETWEEN XOS728-740 APPROX CEILING BEADED DOUBLERS HAVE TEMP REPAIRS INSTALLED. REMOVED TEMP REPAIRS. INSTALLED PERMANENT REPAIR TO LT WING L/E INTERIOR BEADED DOUBLERS BETWEEN XOS 728-740 IAW SRM 57-40-02, REPAIR 9 FIGJun 25, 2011 · N256UP · Doug MD11FSDR ASMF201107001Access Panel · crackedDURING TRANSIT CHECK, TECH DETECTED A FUEL LEAK IN LT WING MAIN TANK DUE TO A CRACK IN THE FUEL TANK ACCESS DOOR PANEL, NR 532QB; SO IT WAS TIGHTEN AND THE FUEL LEAK WAS EVALUATED IAW MM 28-11-00 FOUND IT WITHIN LIMITS, DISPATCHING THE ACFT IN THIS CONDITION. Jun 25, 2011 · N859AM · Boeing 7378Q8SDR IPXA11167613Skin · crackedINSPECTION TYPE:4C, UPON REPLACEMENT OF T/E CRACKED WEB BELOW NR3 SPOILER, FOUND CRACKED UPPER SKIN AT RIB 9 STA ABX 93, LT WING ACCOMPLISHED REPAIR ON LT WING UPPER SKIN IAW SRM 57-21-12, PARA 4P, FIG 215.Jun 25, 2011 · N141UP · Airbus A300F4622RSDR REXA201100412Skin · damagedLT LOWER WING PLANK TRAILING EDGE HAS SEVERAL SMALL TOOLING MARKS COVERING A 1 SQUARE AREA AT APPROX WS 294.50. WORST SINGLE MARKS MEASURES APPROX .25 L X .005 W X .005D. REPAIRED IAW SRM 57-21-31, AND 51-12-00.Jun 24, 2011 · N8896A · Cndair CL6002B19SDR IPXA11567520Panel · dentedINSPECTION TYPE:SV, LT UPPER OTBD TORQUE BOX PANEL REQUIRED ALTERNATE FASTENERS FOR REPLACEMENT. INSTALLED ALTERNATE FASTENERS IAW EO B757-5730-43000A.Jun 23, 2011 · N421UP · Boeing 75724APFSDR IPXA11567519Panel · dentedINSPECTION TYPE:SV, RT WING UPPER OTBD TORQUE BOX PANEL REQUIRED ALTERNATE FASTENERS FOR REPLACEMENT. INSTALLED ALTERNATE FASTENERS IAW EO B757-5730-43000A.Jun 23, 2011 · N421UP · Boeing 75724APFSDR QXEA2011062400454Access Panel · damagedC2 - LT WING FUEL TANK ACCESS PANEL 524FT MATING SURFACE HAS FRETTING. REMOVED AND BLENDED DAMAGE IAW RD 8/4-57-442. PANEL IS WITHIN TOLERANCE FOR REWORK IAW RD 8/4-57-442. TREATED AND PRIMED IAW RD 8/4-57-442.Jun 23, 2011 · N422QX · Bombdr DHC8402SDR C2XA11TY090Skin · dentedTYS - A/C WAS ON GROUND ON ORD WHEN REPORTS OF A TORNADO ACTIVITY AT THE FIELD, A/C WAS EVALUATED FOR DAMAGE OVER THE WINGS DUE TO FLYING DEBRIS. ALL PAX WAS DEPLANED AND NO INJURIES REPORTED. AC WAS FERRIED TO TYS WHERE MAINTENANCE REPLACED THE RT WING NR 3Jun 22, 2011 · N12195 · Emb EMB145XRSDR TRBA201120210Skin · corrodedDURING THE MX BASE CHECK FOUND CORROSION ON THE LT WING ASSY LOWER SKIN SURFACE AROUND WATER DRAIN AT RIB 5 BETWEEN STIFFNERS 6-7. THE ACFT WAS REMOVED FROM SERVICE. CORROSION WAS FOUND OUT OF LIMITS ON LT WING ASSY LOWER SKIN SURFACE AROUND WATER DRAIN AT RIJun 21, 2011 · N429AT · Aerosp ATR72212SDR TRBA201120209Skin · corrodedDURING THE MX BASE CHECK FOUND CORROSION ON THE RT WING ASSY LOWER SLAT-STRIP UPPER SUFACE NEAR RIB 12. THE ACFT WAS REMOVED FROM SERVICE. CORROSION WAS FOUND OUT OF LIMITS ON RT L/E WING ASSY LOWER SLAT-STRIP UPPER SURFACE NEAR RIB 12. PERFORMED SRI DO/TSJun 21, 2011 · N429AT · Aerosp ATR72212SDR TRBA201120208Skin · corrodedDURING THE MX BASE CHECK FOUND CORROSION ON THE RT WING ASSY LOWER SKIN SURFACE AT RIB 10 JACK POINT. THE ACFT WAS REMOVED FROM SERVICE. CORROSION WAS FOUND OUT OF LIMITS ON RT WING ASSY LOWER SKIN SURFACE AT RIB 10 JACK POINT. PERFORMED SRAS DO/TS-1209/05Jun 21, 2011 · N429AT · Aerosp ATR72212SDR TRBA201120207Skin · corrodedDURING THE MX BASE CHECK FOUND CORROSION ON THE RT WING ASSY LOWER SKIN SURFACE INBD AND OTBD OF RIB 8 FLAP ATTACH FITTING. THE ACFT WAS REMOVED FROM SERVICE. CORROSION WAS FOUND OUT OF LIMITS ON RT T/E WING ASSY LOWER SKIN SURFACE INBD AND OTBD OF RIB 8 FLJun 21, 2011 · N429AT · Aerosp ATR72212SDR USAA2011062800046Access Panel · corrodedSAL - 2S - CORROSION IN COUNTERSINK HOLES OF LEFT WING LOWER FUEL ACCESS PANEL 540JB BETWEEN WS 7792 TO WS 8268 & BETWEEN RIB 14 TO RIB 15. REPLACED LEFT WING LOWER FUEL ACCESS PANEL 540JB IAW A320 AMM 57-27-11.Jun 21, 2011 · N108UW · Airbus A320214SDR QXEA2011060220044Access Panel · damagedC2 - RT WING FUEL TANK ACCESS PANEL 624AT MATING SURFACE HAS FRETTING. REMOVED DAMAGE IAW RD 8/4-57-442. REMAINING THICKNESS IS .108". PANEL IS WITHIN TOLERANCE FOR REWORK IAW RD 8/4-57-442. TREATED AND PRIMED REPAIR REF RD 8/4-57-442.Jun 21, 2011 · N422QX · Bombdr DHC8402SDR QXEA2011062200441Access Panel · damagedCOE - C2 - RT WING FUEL TANK ACCESS PANEL 624CT MATING SURFACE HAS FRETTING. REMOVED DAMAGE IAW RD 8/4-57-442. REMAINING THICKNESS IS .121". PANEL IS WITHIN TOLERANCE FOR REWORK IAW RD 8/4-57-442. TREATED AND PRIMED REPAIR REF RD 8/4-57-442.Jun 21, 2011 · N422QX · Bombdr DHC8402SDR QXEA2011062200440Access Panel · damagedC2 - RT WING FUEL TANK ACCESS PANEL 624DT MATING SURFACE HAS FRETTING. REMOVED DAMAGE IAW RD 8/4-57-442. REMAINING THICKNESS IS .118". PANEL IS WITHIN TOLERANCE FOR REWORK IAW RD 8/4-57-442. TREATED AND PRIMED REPAIR REF RD 8/4-57-442.Jun 21, 2011 · N422QX · Bombdr DHC8402SDR QXEA2011062200439Access Panel · damagedC2 - RT WING FUEL TANK ACCESS PANEL 624ET MATING SURFACE HAS FRETTING. REMOVED DAMAGE IAW RD 8/4-57-442. REMAINING THICKNESS IS .113". PANEL IS WITHIN TOLERANCE FOR REWORK IAW RD 8/4-57-442. TREATED AND PRIMED REPAIR REF RD 8/4-57-442.Jun 21, 2011 · N422QX · Bombdr DHC8402SDR QXEA2011062200438Skin · corrodedC2 - RT WING SKIN CUT OUT LANDING FOR ACCESS PANEL 624CT HAS FRETTING. FRETTING REMOVED IAW RD 8/4-57-445. REMAINING THICKNESS .081" IS WITHIN TOLERANCE FOR REWORK IAW RD 8/4-57-445. PANEL IS WITHIN TOLERANCE FOR REWORK IAW RD 8/4-57-442. TREATED AND PRIMEDJun 21, 2011 · N422QX · Bombdr DHC8402SDR QXEA2011062200437Access Panel · damagedC2 - LT WING FUEL TANK ACCESS PANEL 524DT MATING SURFACE HAS FRETTING. REMOVED DAMAGE AND BLENDED IAW RD 8/4-57-442. REMAINING THICKNESS IS .112". PANEL IS WITHIN TOLERANCE FOR REWORK IAW RD 8/4-57-442. TREATED AND PRIMED REPAIR REF RD 8/4-57-442.Jun 21, 2011 · N422QX · Bombdr DHC8402SDR QXEA2011062200436Access Panel · damagedCOE - C2 - RT WING FUEL TANK ACCESS PANEL 624BT MATING SURFACE HAS FRETTING. REMOVED DAMAGE IAW RD 8/4-57-442. PANEL IS WITHIN TOLERANCE FOR REWORK IAW RD 8/4-57-442. MIN REMAINING THICKNESS .110" CONFIRMED CRACK FREE REF NTM 51-00-02-250-801 AND 51-00-01-2Jun 21, 2011 · N422QX · Bombdr DHC8402SDR QXEA2011062200435Access Panel · corrodedC2 - LT WING FUEL TANK ACCESS PANEL 524CT MATING SURFACE HAS FRETTING CORROSION. REMOVED DAMAGE AND BLENDED IAW RD 8/4-57-442. PANEL IS WITHIN TOLERANCE FOR REWORK IAW RD 8/4-57-442. TREATED AND PRIMED REPAIR REF RD 8/4-57-442.Jun 21, 2011 · N422QX · Bombdr DHC8402SDR QXEA2011062200434Access Panel · corrodedC2 - LT WING FUEL TANK ACCESS PANEL 524ET HAS FRETTING CORROSION. FRETTING REMOVED IAW RD 8/4-57-442. PANEL IS WITHIN TOLERANCE FOR REWORK IAW RD 8/4-57-442. TREATED AND PRIMED REPAIR REF RD 8/4-57-442.Jun 21, 2011 · N422QX · Bombdr DHC8402SDR QXEA2011062200433Skin · corrodedC2 - LT WING SKIN CUT-OUT LANDING FOR ACCESS PANEL 524BT HAS FRETTING CORROSION. FRETTING REMOVED IAW RD 8/4-57-445. REMAINING THICKNESS .081" ABOVE MINIMUM REF RD 8/4-57-445. COMPLETED REPAIR REF RD 8/4-57-445.Jun 21, 2011 · N422QX · Bombdr DHC8402SDR EE4Y1106037Skin · dentedRIGHT WING FIXED L/E AT XRS 34 SKIN WITH DENT AND NICKS. REPAIRED IAW EO APPROVED BY FAA DER.Jun 21, 2011 · N787TW · Doug DC983SDR QXEA2011062100432Skin · damagedC2 - LT WING SKIN CUT OUT LANDING FOR ACCESS PANEL 524AT HAS FRETTING. REMOVED FRETTING DAMAGE IAW RD 8/4-57-445. MINIMUM REMAINING MATERIAL WITHIN LIMITS IAW RD 8/4-57-445. COMPLETED REPAIR IAW RD 8/4-57-445.Jun 20, 2011 · N422QX · Bombdr DHC8402SDR QXEA2011062100431Skin · damagedC2 - LT WING SKIN CUT OUT LANDING FOR ACCESS PANEL 524CT HAS FRETTING. REMOVED FRETTING DAMAGE IAW RD 8/4-57-445. MINIMUM REMAINING MATERIAL WITHIN LIMITS IAW RD 8/4-57-445. COMPLETED REPAIR IAW RD 8/4-57-445.Jun 20, 2011 · N422QX · Bombdr DHC8402
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