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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR UIEA200800135Skin · corrodedRIGHT WING WS 917 TO WBL 834 FROM MID SPAR SURROUND AREA TO REAR SPAR SURROUND AREA HAS CORROSION. BLENDED OUT CORROSION PER SRM 51-10-01, REPROTECTED PER SRM 51-10-02.
SDR UIEA200800134Skin · corrodedRIGHT WING WS 1196 TO WS 1392 FROM MID SPAR SURROUND AREA TO REAR SPAR HAS 15 AREAS OF CORROSION. BLENDED OUT CORROSION PER SRM 51-10-01, REPROTECTED PER SRM 51-10-02.SDR UIEA200800132Skin · corrodedRIGHT WING WBL 470 TO WS 510 FROM FRONT SPAR TO REAR SPAR UPPER SKIN FOUND LIGHT CORROSION. BLENDED OUT CORROSION PER SRM 51-10-01, REPROTECTED PER SRM 51-10-02.SDR UIEA200800131Skin · corrodedLEFT WS 640 TO 1120 HAS CORROSION EVIDENT BETWEEN MIDSPAR TO REAR SPAR. BLENDED OUT CORROSION PER SRM 51-10-01, REPROTECTED PER SRM 51-10-02.
SDR UIEA200800130Skin · corrodedLEFT WBL 150 TO 470 HAS CORROSION EVIDENT BETWEEN MIDSPAR TO NR 1 BEAM. BLENDED OUT CORROSION PER SRM 51-10-01, REPROTECTED PER SRM 51-10-02.
SDR UIEA200800128Skin · corrodedLEFT WING FROM WS 1120 TO 640 UPPER SKIN CORROSION EVIDENT BETWEEN FRONT SPAR AND MID SPAR. BLENDED OUT CORROSION PER SRM 51-10-01, REPROTECTED PER SRM 51-10-02.SDR 08FDEA01296Fairing · delaminatedNR 5 RIGHT WING FLAP FAIRING OUTER SKIN IS DELAMINATED 5 INCHES AFT OF THE FWD ATTACH POINT. REPAIRED THE DELAMINATION BY REMOVING DAMAGE & APPLYING A WET PAY UP IAW SRM 57-20-35. PAINTED IAW AMM 51-75-10-08.SDR 08FDEA01278Skin · cracked08 EACH FASTENER HOLES FOUND WITH CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION AT RIGHT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS = 690 AND STA XORS = 700. REPAIR CARRIED OUT AS PER EA 1-5710-120551, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-10SDR 08FDEA01277Access Panel · corroded06 EACH FASTENER HOLES FOUND WITH CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION AT LEFT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS = 690 AND STA XORS = 700. REPAIR CARRIED OUT AS PER EA 1-5710-120550, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100SDR DHL2008760510Skin · crackedFABRICATED AND INSTALLED REPAIR DOUBLER AT R/WING NR 6 L/E SLAT O/B HOOK SEAL CUT-OUT, BETWEEN RWS 519 TO 546, PER B727 SRM 57-30-4 FIG 9.SDR SWIA200819428Skin · damagedLEFT WINGLET OUTBOARD SKIN WAS DAMAGED BY BAGGAGE CART. REPLACED WINGLET SKIN IAW CRJ SRM 51-40-11, REO 601R-57-31-330 AND BOMBARDIER DRAWING NR 600-15108.
SDR 08FDEA01250Access Panel · crackedRIGHT WING, LEADING EDGE LOWER SURFACE ACCESS PANEL 619CB INBOARD CORNER CUTOUT AREA FOUND CRACK. REPAIR CARRIED OUT PER SRM 57-10-00 FIGURE 21 VOLUME I. FABRICATED FILLER AND DOUBLER INSTALLED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMMSDR 08FDEA01249Skin · corrodedFOUND CORROSION UNDER STATIC DISCHARGER SUPPORT PLATE, LT WING TIP. REPAIR PERFORMED BY REMOVE OF CORROSION AND INSTALLING A REPAIR PATCH IAW, RAS /FOK/047/2008 ISS A, APPROVED BY EA 6-5730-117164.SDR 08FDEA01241Panel · chafedRIGHT WING PANEL NR 612 AT IS CHAFED ON THE MATING SURFACES. COMPLIED WITH EA 6-5720-118459 PT 1.SDR 08FDEA01240Panel · chafedLEFT WING PANEL 512 AT IS CHAFED IN SEVERAL AREAS ON THE BACK SIDE. COMPLIED WITH EA 6-5720-118459 PT1.SDR 08FDEA01237Panel · chafedLEFT WING OUTBD L/E PANEL NR 527 AB INNER SURFACE IS CHAFED AT THE END OF THE ACCESS DOOR HINGE. BLENDED AREA. FOUND TO BE OUT OF LIMITS IAW SRM 57-00-01 VOL I. FABRICATED DOUBLER IAW SRM 57-00-01 VOL I & 57-31-01 VOL III. ALODINED & PRIMED IAW SRM 51-21-0SDR ASAA0842854Skin · dentedTWO DENTS FOUND ON LWR SURFACE FOUND TO BE BEYOND ALLOWABLE DAMAGE LIMITS, PERMANENT REPAIR IAW BOEING SRM 51-70-10 REPAIR 2.SDR UIEA200800147Skin · damagedRIGHT WING REAR SPAR UPPER SKIN AT WS 1490 FOUND EXISTING EXCESSIVE BLEND OUT AS MARKED. CHECKED THE BLENDOUT AREA AND FOUND AS PER ATLAS EO 4757A338 THE BLENDOUT IS PERMITTED.SDR UIEA200800146Skin · damagedRIGHT WING REAR SPAR UPPER SKIN AT WS 1390 FOUND EXISTING EXCESSIVE BLEND OUT AS MARKED. CHECKED THE BLENDOUT AREA AND FOUND AS PER ATLAS EO 4757A338 THE BLENDOUT IS PERMITTED.SDR C2XA08IA094Skin · crackedIAH - FLIGHT 2695, DURING PREFLIGHT INSPECTION, THE CREW REPORTED CRACKS AT THE SPOILER HINGE POINTS. MAINTENANCE INSPECTED THE AIRCRAFT, AND DETERMINED THAT ONLY THE RIGHT HAND UPPER CENTER HINGE CUTOUT TO HAVE AN 18MM CRACK. THE CRACK WAS PLACED ON DMI FORSDR UPS08M52671Skin · corrodedINSPECTION TYPE-C, CORROSION AROUND FASTENER HEADS ON O/WING CTR FUEL TANK UPPER SURFACE AT STA 1229 X=-87 TO -107. LOCK FASTENER ON AFFECTED AREA REMVD FOR ACCESS. CORROSION REMOVED, MEASURED THK: 0.170", MAT'L REMOVED:0.067", MAT'L REMN:0.103". FOUND OUT SDR VNAA0803012Panel · damagedCREW REPORTED A LIGHTNING STRIKE DURING DESCENT INTO LEX. MAINTENANCE PERFORMED AN EN ROUTE AND A DETAILED LIGHTNING STRIKE INSPECTION. MAINTENANCE FOUND DAMAGE TO THE RIGHT WING PANELS. MAINTENANCE REPAIRED DAMAGE PER REO 601R-57-31-1005. OPERATIONAL CHECSDR C2XA08TY039Skin · crackedWING SKIN CRACK ON LEFT I/B CENTER SPOILER HINGE CUTOUT. REPAIRED CRACK IAW EC5740-01143. AIRCRAFT RELEASED AND RETURNED TO SERVICE.SDR 08FDEA01191Panel · chafedRIGHT WING ROOT HYD SHELF GROUND CONNECTION ACCESS PANEL MATING SURFACE IS WORN. CLEANED CUTOUT AREA REF A310-200 SRM 51-73-10. (NO MATERIAL LOSS); FOUND ONLY PAINT MISSING. ALODINED REF A310-200 SRM 51-21-10; PG 4. PRIMED AND PAINTED REF A310-200 SRM 51-2SDR HALA0800463Skin · corrodedLEVEL 1 CORROSION ON RIGHT WING LOWER SURFACE AT STRINGER L-15, WS 620-646. REWORKED IAW SRM 51-10-02.SDR HALA0800462Skin · corrodedLEVEL 1 CORROSION ON RIGHT WING LOWER SURFACE AT STRINGER L-15 AT WS 577-608. REWORKED IAW SRM 51-10-02.SDR HALA0800461Skin · corrodedLEVEL 1 CORROSION ON RIGHT WING LOWER SURFACE AT STRINGER L-15, WS 522-552. REWORKED IAW SRM 51-10-02.SDR HALA0800460Skin · corrodedLEVEL 1 CORROSION ON RIGHT WING LOWER SURFACE AT STRINGER L-15, AT WS 470-491. REWORKED IAW SRM 51-10-02.SDR HALA0800459Skin · corrodedCORROSION ON RIGHT WING LOWER SURFACE AT STRINGER L-15 AT WS 426. REWORKED IAW SRM 51-10-02.SDR UPS08M52041Skin · crackedINSPECTION TYPE:4C LEFT WING LE NR 14 SLAT TRACK CUT OUT CRACKED. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW MD-11 SRM 57-10-00 FIG 21 AND 51-33-01.SDR UPS08M52040Skin · crackedINSPECTION TYPE:4C LEFT WING LE SKIN SPLICE STRAP XFS 669 CRACKED. REMOVED CRACKED SKIN SPLICE STRAP. FABRICATED AND INSTALLED REPLACEMENT SKIN SPLICE STRAP IAW DWG ARB3954 AND 51-33-01.SDR UPS08M52038Skin · crackedINSPECTION TYPE:4C RT WING LE ACCESS PNL LANDING AT SLAT TRACK FITTING 9 STRINGER CRACKED. REMOVED CRACKED STRINGER DOUBLER. FABRICATED AND INSTALLED REPLACEMENT STRINGER DOUBLER IAW DWG ARB1180 AND MD-11 SRM 51-33-01.SDR UPS08M52035Skin · crackedINSPECTION TYPE:4C RIGHT WING LE SKIN SPLICE STRAP XFS669 CRACKED. REMOVED CRACKED SPLICE STRAP, FABRICATED AND INSTALLED REPLACEMENT SPLICE STRAP IAW DWG ARB3954 AND MD-11 SRM 51-33-01.SDR UPS08M52034Skin · crackedINSPECTION TYPE:4C RIGHT WING LE SKIN SPLICE STRAP XFS791 CRACKED. REMOVED CRACKED SKIN SPLICE. FABRICATED AND INSTALLED REPLACEMENT SKIN SPLICE IAW DWG ARB3954 AND MD-11 SRM 51-33-01.SDR UIEA200800096Panel · delaminatedLT WING UPPER SURFACE FLYING PANEL AT T/E CLOSEST TO FUSELAGE HAS DELAMINATION AT OUTBOARD EDGE APPROX 18 INCHES INBOARD FROM NR 6 SPOILER. DELAMINATION REPAIRED IAW ATLAS EO NR 4457A137 AND SRM 51-70-07.SDR 08FDEA01158Panel · chafedLEFT WING FUEL TANK PLATE NR 540 FB HAS FRETTING FROM THE MESH GASKET. EVALUATED AND FOUND TO BE OUT OF LIMITS FOR PANEL 540 FB DUE TO NO DAMAGE ALLOWED IN AREA PER FEDEX A310 SRM 57-20-16; PG 109. ORDERED AND RECEIVED A NEW CLAMP PLATE FOR PANEL 540 FB P/N SDR 08FDEA01140Panel · corrodedRIGHT WING FUEL PANEL 650 HB HAS FRETTING CORROSION AROUND THE ATTACHMENT HOLES. PANEL FOUND TO BE OUT OF LIMITS REF A310-200 SRM 57-50-16. FOR INSTALLATION SEE FEDEX WIC 46X5042 ALI.SDR 08FDEA01139Panel · corrodedLEFT WING FUEL PANEL 550 HB HAS FRETTING CORROSION AROUND THE ATTACHMENT HOLES. PANEL FOUND TO BE OUT OF LIMITS REF A310-200 SRM 57-20-16, FOR INSTALLATION OF THE NEW PANEL SEE FEDEX WIC 45X5052ALI.SDR 08FDEA01138Panel · gougedRIGHT WING FUEL PANEL 650KB HAS GOUGING ON THE UNDERSIDE. PANEL FOUND TO BE OUT OF LIMITS REF A310-200 SRM 57-20-16. FOR THE INSTALLATION OF THE PANEL SEE FEDEX WIC 46X5042ALI.SDR DHL2008805506Skin · damagedLT WING INBD L/E LWR SURFACE HAS ELONGATED HOLES AT STA XILD 42. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-24-08, EVA D853-00046, DWG AF12-57-101 REV IR DATED 02-22-08. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-3-0. CUT OUT DAMAGED SECTION IAW DWGSDR 08FDEA01134Panel · corrodedRIGHT FUEL TANK PANEL 640 FB HAS FRETTING CORROSION ON OUTER PANEL MATING SURFACES. FUEL PANEL IS OUT OF LIMITS REF A310-200 SRM 57-20-16; FIG 103; SHEET 4. REPLACED FUEL PANEL TO BE INSTALLED ON FEDEX WIC 46X5052ALI.SDR 08FDEA01133Panel · corrodedRIGHT WING FUEL PANEL 650LB HAS FITTING CORROSION ON THE INNER BOLT HOLES. FUEL PANEL WAS FOUND TO BE OUT OF LIMITS REF A310-200 SRM 57-20-16; FIG 103; SHEET 4, TO BE INSTALLED ON FEDEX WIC 46X5042ALI.SDR 08FDEA01126Panel · chafedRIGHT WING LOWER L/E PANEL 616 HB IS CHAFED ALONG THE EDGE. CLEANED RIGHT WING LOWER L/E PANEL 616 HB TO EVALUATE DAMAGE AND PANEL WAS FOUND TO BE OUT OF LIMITS IAW SRM 57-00-01; VOL I. PANEL REQUIRED A SRM REPAIR. FABRICATED REPAIR DOUBLER IAW DC/MD-10 SRSDR 08FDEA01125Panel · chafedLEFT WING LOWER INBD L/E PANEL 516 HB IS CHAFED ALONG THE EDGE. BLENDED THE AREA IAW SRM 57-00-01; VOL I. ORIGINAL MATERIAL .090; MATERIAL REMOVED .020; MATERIAL REMAINING .070 TOOL NR T8225P. FOUND TO BE OUT OF LIMITS IAW SRM 57-00-01; VOL I. FABRICATESDR USAABB08039Fitting · crackedPHL FLT 1250 MCO TO PHL. AFTER A JOLT FROM APPARENT WAKE TURBULENCE, APPROXIMATELY 45 MILES FROM BWI, AT FL 270 AND 320 KIAS, A PANEL ON THE UPPER LEFT WING SEPARATED FROM THE AIRCRAFT IN FLIGHT. THE PANEL WAS LOCATED AFT OF THE REAR SPAR BUT FORWARD OF THE SDR BB08039Panel · separatedPHL- FLT 1250 - MCO TO PHL - AFTER A JOLT FROM APPARENT WAKE TURBULENCE, APPROXIMATELY 45 MILES FROM BWI, AT FL 270 AND 320 KIAS, A PANEL ON THE UPPER LEFT WING SEPARATED FROM THE AIRCRAFT IN FLIGHT. THE PANEL WAS LOCATED AFT OF THE REAR SPAR BUT FORWARD OF TSDR ABXA080135Skin · crackedRIGHT WING UPPER SURFACE XRS 164.00, THE BONDED PANEL JUST INBOARD OF INBOARD SPOILER BOARD HAD 6 EACH SHEARED FASTENERS. REPAIRED CRACKED SKIN IN AREA OF LOOSE RIVETS IAW DC9 SRM 57-01, FIGURE 2.SDR 08FDEA01090Skin · wornRT WING L/E DROPPED (REMOVED PART) FOUND WEAR ON LWR SKIN. REPAIRED SKIN IAW SRM 57-10-00 FIG 39 SHT 2 VOL I.SDR 08FDEA01089Skin · wornRT WING L/E DROPPED (REMOVED PART) FOUND WEAR ON SKIN. REPAIRED SKIN IAW SRM 57-10-00 FIG 39 SHT 2 VOL I.SDR 08FDEA01087Skin · crackedLEFT WING LEADING EDGE ANTI-ICE TELESCOPIC DUCT DOOR CUT OUT CORNER SKIN CRACKED. REPAIRED AS PER SRM 57-10-00, FIGURE 43, VOLUME 1. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
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