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 05FDEA01481Skin · nickedLEFT WING LEADING EDGE, STA XORS 164 WITH NICKS. REPAIRED DAMAGED LEADING EDGE IAW SRM 57-10-00, FIG 28.May 30, 2005 · N571FE · Doug DC1010SDR 05FDEA01480Skin · damagedRIGHT WING, INBOARD FLAP, UPPER SKIN WITH EXISTING REPAIR WITH DEFORMED AREA. REMOVED EXISTING REPAIR PER SRM 51-35-01, PAGE 1/13. CUT OUT DAMAGED AREA PER SRM 57-10-00, PAGE 85. PERFORMED NEW REPAIR PER SRM 57-10-00, PAGE 85.May 30, 2005 · N571FE · Doug DC1010SDR ASAA0540267Skin · delaminatedRT WING OB AFT FLAP DELAMINATED AT IB TRAILING EDGE. REMOVED DAMAGED MATERIAL, INSTALLED CORE, SKIN, AND DOUBLER IAW SRM. (K)May 26, 2005 · N776AS · Boeing 7374Q8SDR UPS05844575Skin · damagedINSPECTION TYPE:C3 RIGHT WING CENTER L/E LWR SURFACE FASTENER HOLES ELONGATED AT XFS 527. FABRICATED REPAIR DOUBLER, INSTALLED CONICAL WASHERS, AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 57-2-0, 51-1-11, AND 51-1-21.May 25, 2005 · N840UP · Doug DC873FSDR UPS05844550Skin · corrodedINSPECTION TYPE:C3 RIGHT OUTBOARD L/E SKIN HAS CORROSION AT XFS 554. CUT OUT DAMAGED AREA OF L/E SKIN IAW DC-8 SRM 57-02-01 FIG 14. FABRICATED REPAIR DOUBLER & FILLER AND INSTALLED IAW DC-8 SRM 57-02-01 FIG 14, 51-1-26, AND 51-1-21.May 24, 2005 · N840UP · Doug DC873FSDR UPS05844549Doubler · crackedINSPECTION TYPE:C3 RIGHT OUTBOARD L/E INNER DOUBLER HAS 2 EA CRACKS AROUND DRAIN HOLE AT XFS 579. REMOVED CRACKED INNER DOUBLER, FABRICATED REPLACEMENT DOUBLER IAW DWG 5769600-40, AND INSTALLED IAW DC-8 SRM 51-1-20D AND 51-1-21.May 24, 2005 · N840UP · Doug DC873FSDR DHL2005807542Access Panel · corrodedRT WING ACCESS PANEL NR 505B LT UPPER EDGE CORRODED STA XRS 460.000. REMOVED CORROSION LEVEL II FROM RT ACCESS DOOR NR 505B IAW SRM 51-1-8 PG 17-18. MEASURED BLENDOUT, FOUND OUT OF ALLOWABLE LIMITS IAW SRM 57-2-0 PAGE 76. REMOVED CORRODED ACCESS DOOR IAW SRMay 20, 2005 · N807DH · Doug DC873FSDR 05FDEA01392Skin · corrodedRIGHT WING FUEL CUTOUT FOR PANEL 650HB HAS ONE EXISTING PLUG BROKEN ON ONE SIDE. REMOVED DOME NUT IAW A310 SRM 51-40-21. REMOVED PLUG IAW A310 SRM 51-40-51. REAMED HOLE TO 0.4215 TO REMOVE CRACK IAW A310-SRM 51-40-44. NO DEFECTS NOTED IAW NTM 51-10-01. RMay 20, 2005 · N403FE · Airbus A310203SDR 05FDEA01391Skin · corrodedRIGHT WING OUTER FUEL CUTOUT FOR PANEL 650PB HAS TWO HOLES DOUBLE DRILLED. CHAMFERED 1 EACH HOLE IAW SRM A310 51-40-44. FOUND TO BE WITHIN LIMITS IAW A310 SRM 57-20-12 FIG 201. REPAIRED 1 EACH HOLE WITH BUSHING IAW EA 6-5710-88828 PT1 AND TD/J1/S1/00726/200May 20, 2005 · N403FE · Airbus A310203SDR UPS05444653Skin · crackedINSPECTION TYPE:C RIGHT WING BS 1241 UPPER REAR SPAR BOLT HOLE NR 5 UPPER SKIN AND CHORD FOUND CRACKED (CRACK LENGTH 0.030 / 0.060 INCH). HOLE REWORKED AS PER EO B747-5740-17032-C.May 19, 2005 · N677UP · Boeing 747123FSDR 05FDEA01342Access Panel · corrodedRT WING LEADING EDGE ACCESS PANEL 626FB INSIDE LOWER SURFACE FOUND CORROSION. REMOVED AND REPAIRED AS PER FEDEX EA NR 1-5710-86606. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.May 17, 2005 · N580FE · Doug MD11SDR EIA2005126Skin · corrodedCORROSION ON LOWER SKIN IN SPAR CAVITY IN LEFT END OF LT WING AT WS 1275. CUT OUT DAMAGED SKIN, FABRICATED AND INSTALLED REPAIR IAW B747 SRM 57-30-03, FIG 9 AND BOEING MESSAGE 1-1JWDXE.May 17, 2005 · N481EV · Boeing 747132SDR CALA0500154Skin · crackedINSPECTION FOUND A 10 INCH CRACK IN RT WING FIXED LEADING EDGE SKIN AT FSS 416. REPAIRED IAW EA 5731-01010, REV D AND SRM 51-40-02 AND IAW MM 27-81-02.May 17, 2005 · N14107 · Boeing 757224SDR 05FDEA01338Panel · bulgedRIGHT WING TRAILING EDGE UPPER PANEL LEADING EDGE FOUND BULGING AT XORS 1042. REMOVED AND REPAIR CARRIED OUT AS PER FEDEX EA NR 1-5710-86607.May 17, 2005 · N580FE · Doug MD11SDR ASAA0580292Skin · delaminatedOKC - DURING HV-CHECK, FOUND LEFT ANTI-FLOAT TAB HAS A COMPOSITE REPAIR ON TRAILING EDGE, LOWER SURFACE IS DELAMINATING. REMOVED DAMAGE AND INSTALLED A REPAIR DOUBLER. (M)May 16, 2005 · N968AS · Doug DC983SDR 05FDEA01312Panel · wornOFF A/C PART LEFT WING PNL 512AT HAS WEAR MARKS ON BOTTOM SIDE OF PNL. COMPLIED WITH EA6-5740-89200.May 16, 2005 · N403FE · Airbus A310SDR 05FDEA01291Skin · corrodedLT WING UPPER SURFACE FOUND CORROSION AT XORS 77 STRINGER 21. CORRODED AREA REPAIRED AS PER FEDEX EA NR 1-5710-86605. THIS REPAIR CLASSIFIED AS MINOR REPAIR AS PER GMM 6-2-100.May 15, 2005 · N580FE · Doug MD11SDR ASOA05474Skin Panel · crackedDURING A C-CHECK, THE LOWER WING PLANK AT WS 148.019 LT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LOWER WING PLANK AT WS 148.019 LT SIDE IAW EO. (K)May 13, 2005 · N829AS · Cndair CL6002B19SDR 2005FA0000896Skin · corrodedDURING AN ANNUAL INSP, RT WING IB L/E SKIN WAS FOUND CORRODED THROUGH BENEATH STRINGER. A POSSIBLE CAUSE FOR THE EXCESSIVE CORROSION MAY BE WATER SEEPING THROUGH THE AIR INLET HOSE INSTALLED ABOVE THE AFFECTED AREA. THIS WATER ENTERS THROUGH THE L/E AIR INLEMay 12, 2005 · N30297 · Cessna 177ASDR CA050513001Skin · debondedDURING INSTALLATION OF A REPAIR DOUBLER INBOARD OF THE RT NACELLE AS PER RD6-57-618 IT WAS FOUND THAT 3 AREAS OF DISBOND HAD OCCURRED BETWEEN THE UPPER WING SKIN AND THE CORRUGATION . AS PER INSTRUCTIONS IN THE REPAIR DEFINITION THE MANUFACTURE WAS CONTACTED AMay 9, 2005 · Dhav DHC6300SDR USAA050592Skin · debondedCLT - FOUND NR 1 SLAT DISBOND 1 INCH, UNDERSIDE AT INBOARD AUX TRACK. SDA COMPLETED ACCOMPLISHED COMPOSITE REPAIR IAW SRM 57-43-02. (M)May 5, 2005 · N439US · Boeing 7374B7SDR USAA050590Skin · crackedCLT - FOUND WING SKIN CRACKED 1 INCH, LOWER WING SKIN AT STATION 135.72 JUST ABOVE THE OUTBOARD PYLON FUSE PIN. REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER IAW 57-41-02. (M)May 5, 2005 · N439US · Boeing 7374B7SDR QXEA200500921Skin · chafedYYC - LEFT WING LEADING EDGE PANEL FORWARD OPENING HAS RUB MARKS ON THE EDGE. REPAIRED IAW REO 670-57-41-074 AND HORIZON AIR EA R-51-118.May 5, 2005 · N611QX · Cndair CL6002C10SDR UPS05844486Skin · crackedINSPECTION TYPE: C3, LT WING L/E UPPER SKIN FASTENER HOLES CRACKED .125 INCH LONG AT XFS 450. CUT OUT DAMAGE, FABRICATED AND INSTALLED FILLER AND REPAIR DOUBLER IAW SRM 57-2-1-0 AND 51-3-2.May 4, 2005 · N808UP · Doug DC873FSDR UPS05844470Skin · damagedINSPECTION TYPE:C3 LT WING L/E AT XFS 454, LWR SURFACE FASTENER HOLES ARE ELONGATED. REMOVE DAMAGE AND INSTALLED DOUBLER AND FILLER IAW EO DC-8 5720- 7767-A AND SRM 51-1-21.May 4, 2005 · N808UP · Doug DC873FSDR A6WA200540165Skin · frettedRIGHT LOWER WING PLANK HAS FRETTING DAMAGE AT FUEL TANK ACCESS DOOR CUT OUTS AT WS 116.366 AND WS 136-676. MEASURES .001 TO .002 WIDTH DEEP AROUND ENTIRE CUT OUT. REPAIRED FRETTING DAMAGE BY BLENDING IAW BOMBARDIER INC REO 601R-57-21-030 REV C. (M)May 3, 2005 · N451AW · Cndair CL6002B19SDR DHL2005807525Cap · corrodedLT WING INBOARD L/E SLANT PANEL UPPER CAP CORRODED STA XFS 138.750 - 151.250. PERFORMED MAJOR REPAIR. REMOVED FASTENERS IAW SRM 51-3-0 PG 1. PERFORMED BLENDEOUT (7.125*1.875*0.092) FOUND OUT OF LIMITS IAW SRM 57-2-1 FIG 37. PERFORMED VISUAL DETAIL INSPECTIMay 3, 2005 · N807DH · Doug DC873FSDR DHL2005807519Skin · damagedLEFT WING CTR L/E EXTERNAL SKIN HOLES ELONGATED STA XFS 526.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 04-16-05, EO AST050404 DATED 04-13-05. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. CUT OUT DAMAGED SECTION IAW EOASMay 3, 2005 · N807DH · Doug DC873FSDR COMA0560289Skin · corrodedFRETTING CORROSION LOWER WING PLANK 193A. REPAIRED IAW REO 601R-57-21-588.May 3, 2005 · N708CA · Cndair CL6002B19SDR ASOA05395Skin Panel · crackedDURING A C-CHECK IN MCN, THE LOWER WING PLANK AT WS 148.019 LEFT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LOWER WING PLANK AT WS 148.019 LEFT IAW ASA EO 600-57-0134A. (M)May 2, 2005 · N849AS · Cndair CL6002B19SDR QXEA200500933Access Panel · corrodedYYC - RIGHT WING, FUEL ACCESS PANEL 611AB SOME FRETTING CORROSION FOUND. REPAIRED IAW CRJ700 SRM 51-21-11-001-001-A01.May 2, 2005 · N611QX · Cndair CL6002C10SDR QXEA200500856Panel · damagedYYC - LEFT WING LEADING EDGE PANEL HAS RUBBING MARKS AT TWO LOCATION. REPAIRED IAW CRJ-700 SRM 51-12-00-001-001-A01 AND SRM 51-25-00-001-001-A01.May 2, 2005 · N611QX · Cndair CL6002C10SDR 05FDEA01187Access Panel · damagedRIGHT WING FUEL TANK OPENING 650PB AT APPROX 8 O`CLOCK POS HAS 1 EA ELONGATED HOLE REF N00645. COMPLIED WITH EA 6-5710-87830.Apr 30, 2005 · N662FE · Airbus A300B4605RSDR 05FDEA01186Access Panel · damagedRIGHT WING FUEL PANEL OPENING 650PB AT APPROX 3 O`CLOCK POS 1 EA ELONGATED FASTENER HOLE REF N00641. COMPLIED WITH EA 6-5710-87830.Apr 30, 2005 · N662FE · Airbus A300B4605RSDR 05FDEA01185Access Panel · damagedLEFT WING FUEL CELL ACCESS PANEL CUTOUT 550PB 1 EA SCREW HOLE WITH ELONGATED OUTER FACE REF N00406. COMPLIED WITH EA 6-5710-87830.Apr 30, 2005 · N662FE · Airbus A300B4605RSDR 05FDEA01184Access Panel · damagedRIGHT WING FUEL OPENING 650PB AT APPROX 830 POSITION 1 EA ELONGATED FASTENER HOLE REF N00646. COMPLIED WITH EA 6-5710-87830.Apr 30, 2005 · N662FE · Airbus A300F4605RSDR 05FDEA01181Panel · damagedRIGHT WING O/B TANK 660BB HAS 2 EA ELONGATED FASTENER HOLES REF N00383. COMPLIED WITH EA 6-5710-87830.Apr 30, 2005 · N662FE · Airbus A300B4605RSDR IXXA05SMN27SSkin · crackedRT WING CTR L/E LOWER OUTER PLATING CRACKED. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3, SEMAN DWG ED-3944. REMOVED FASTENERS FROM REPAIR AREA IAW DC-8 SRM. REMOVED DAMAGED AREA IAW SEMAN DWG ED-3944. PERFORMED NDT INSPECTION IAW DC-8 NDT SPM PART 06-10-01-Apr 29, 2005 · N828BX · Doug DC871FSDR IXXA05SMN26SSkin · crackedRT WING CTR L/E OUTER PLATING UPPER SURFACE CRACKED STA. XFS 430.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3, SEMAN DWG ED-3937. REMOVED FASTENERS IAW DC-8 SRM. REMOVED DAMAGED AREA IAW SEMAN ED-3937. PERFORMED NDT INSPECTION IAW NDT SPM PART 06-10-01-001Apr 29, 2005 · N828BX · Doug DC871FSDR IXXA05SMN25SDoubler · crackedRT WING CTR L/E INTERNAL DOUBLER CRACKED. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 AND SEMAN DWG ED-3953. REMOVED FASTENERS FROM REPAIR AREA IAW DC-8 SRM. REMOVED DAMAGED AREA IAW SEMAN ED-3953. PERFORMED NDT INSPECTION TO AREA IAW NDT SPM PART 06-10-01-Apr 29, 2005 · N828BX · Doug DC871FSDR IXXA05SMN14SSkin · crackedRT WING, LE LWR SKIN WITH 03 CRACKS , XW 422.750. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3. REMOVED EXISTING REPAIR DOUBLER IAW SEMAN DWG ED-3950, DC-8 SRM. REMOVED DAMAGED AREA IAW SEMAN DWG ED-3950. PERFORMED NDT INSPECTION IAW DC-8 NDT SPM PART 06-10-Apr 29, 2005 · N828BX · Doug DC871FSDR QXEA200500720Panel · corrodedPDX - RT WING DRY BAY PANEL 622AT FASTENER COUNTER SINK HOLES ARE CORRODED. REPAIRED IAW DHC-8-200 SRM 51-20-51 AND 57-30-00-400-802, PAGE 403-406.Apr 22, 2005 · N346PH · Dhav DHC8202SDR 05FDEA01099Skin · damagedLT WING, 560CB HAS 1 EA ELONGATED HOLE. COMPLIED WITH EA 6-5710-87212.Apr 22, 2005 · N402FE · Airbus A310203SDR 05FDEA01079Skin · damagedL/WING, 550JB HAS ONE EACH ELONGATED HOLE. COMPLIED WITH EA 6-5710-87121.Apr 22, 2005 · N402FE · Airbus A310203SDR 05FDEA01066Skin · damagedWHILE WORKING EO 6-5710-7-5008PT3, LT WING FOR LANDING ASSY FOR PANEL 575CB 4 EA HOLES NOTED ARE LARGER THAN DRAWING SIZE. THIS IS AN INCOMING CONDITION. HOLE NR 9 .263 INCH, EM PLANK .6 INCH, NR 10 .328 INCH, EM RIB .610 INCH, EM PLANK .760 INCH, NR17 .328 IApr 22, 2005 · N402FE · Airbus A310SDR 05FDEA01065Panel · damagedRT WING FAIRING 633BB 2 MOUNTED BRACKETS REQUIRES INSTALLATION. NOTE 7 EA HOLES IN WING PLANK ARE COUNTERSUNK. RT WING BRACKETS FOR FAIRING 633BB REAMED HOLES TO 2ND OVERSIZE, SEALED FITTINGS (2EA.). INSTALLED CONICAL WASHERS, AND FITTINGS IAW A310 SRM 5Apr 22, 2005 · N402FE · Airbus A310SDR SWAA051180Skin · crackedDURING SCHEDULED D-CHECK, FOUND RIGHT WING UPPER SKIN CRACKED AT RSS 238. REPAIRED SKIN PER PAE ER.Apr 21, 2005 · N313SW · Boeing 7373H4SDR ABXA050100Panel · damagedDURING REMOVAL OF LOWER REAR SPAR FASTENERS SB 57-88, DOUBLER WAS DAMAGED ON EDGE FROM TRAP PANEL ON LEFT WING. REPAIRED AREA IAW REA D857-51393MR.Apr 20, 2005 · N819AX · Doug DC863FSDR COMA0560271Skin · crackedCRACK FOUND ON RIGHT WING PLANK. REPAIRED IAW REPAIRED CRJ REO 601R-57-21-130.Apr 20, 2005 · N981CA · Cndair CL6002B19SDR COMA0560267Skin · crackedCRACK FOUND ON LEFT WING PLANK. REPAIRED IAW CRJ REO 601R-57-21-130.Apr 20, 2005 · N981CA · Cndair CL6002B19
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