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 QXEA2010041200252Skin · damagedC-CHECK. COMPLY WITH HORIZON TASK CARD REO 670-57-52-134/3. DRILLED OUT ALL BLIND RIVETS IAW REO 670-57-52-134. REMOVED DAMAGED SKIN IAW REO 670-57-52-138. PERFORMED LPI ON CUT LINES. NO CRACKS FOUND. IAW NDTM LPI 51-20-008-230-A01. REO 670-57-52-138. SDR USAA2010040990747Panel · corrodedPIT - S4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON LEFT WING FUEL PANEL 540JB. REPLACED LEFT WING FUEL PANEL 540JB IAW B757 SRM 57-21-11.SDR REXA201000059Skin · corrodedLEFT WING LOWER PLANK CORROSION AT FUEL PANEL 540FB AT WS 136.676 NR 8 HOLE ON EDGE OF CUTOUT MEASURED .007 INCH DEEP FORWARD AND .006 INCH DEEP IN AFT CRITICAL REGIONS. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV H. REPAIR DEPTH IS .008 INCH FORWARD AND SDR REXA201000058Skin · corrodedLEFT WING LOWER PLANK AT WS 253.022 HOLE NR 13 EDGE OF ACCESS DOOR CUTOUT CORROSION FOUND .003 INCH DEEP. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV H. REPAIR DEPTH IS .003 INCH.SDR BQVA2010041200006Skin · corrodedDURING A WING NDT INSPECTION OF THE LT WING PLANK AT FS 452 BL 33, CORROSION WAS FOUND. ENGINEERING HAS DETERMINED THIS CORROSION IS EXCESSIVE ENOUGH TO REQUIRE ACCOMPLISHMENT OF ASC 229, WHICH WILL REMOVE THE CORROSION ON THE PLANK AND INSTALL A THREE PIECE SDR FDEA201004071096Skin · crackedLT WING - L/E NR 7 SLAT TRACK CUT OUT INBD SIDE FOUND CRACKED. REPAIRED IAW SRM 57-40-02, FIG 201, REPAIR 7, REV 43. CLASSIFIED MINOR REPAIR IAW GMM 6-2-100, REV 110.SDR FDEA201004071095Skin · crackedLT WING - L/E NR 6 SLAT TRACK CUT OUT INBD SIDE FOUND CRACKED. REPAIRED IAW SRM 57-40-02, FIGURE 201, REPAIR 7, REVISION 43. CLASSIFIED MINOR REPAIR IAW GMM 6-2-100, REV 110.SDR UALA2010040701166Winglet · unknownBLENDED WINGLET RETROFIT. ACP COA 506741 ON TASKCARD 5C0674248.SDR FDEA201004061061Skin · crackedCRACK FOUND AT RT WING NR 3 L/E SLAT TELESCOPIC DUCT CUTOUT. RT WING NR 3 L/E SLAT TELESCOPIC DUCT CUTOUT REPAIRED IAW EA NR 1-5710-132397, CLASSIFIED MAJOR REPAIR IAW GMM 6-2-100, REVISION 110.SDR USAA2010041290758Panel · saturatedPIT - S4 - MAJOR REPAIR - RIGHT WING LOWER FUEL PANEL 640FB WEIGHT IS EXCEEDING ITS LIMIT. ACTUAL WEIGHT IS 1.29KG. MAX ALLOWABLE WEIGHT IS 1.10 KG +/- 0.1KG. REPLACED RIGHT WING LOWER FUEL PANEL 640FB IAW JOB CARD 26C60057091.SDR USAA2010040990746Panel · corrodedPIT - S4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON LEFT WING FUEL PANEL 540NB. REPLACED LEFT WING FUEL PANEL 540NB IAW B757 SRM 57-21-11.SDR EIAA2010014Skin · damagedLEFT WING LEADING EDGE SPAR AT F550/1512 HAS EXFOLIATION LIFTING UPPER SKIN. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER ECRA 471-57-272-2.SDR A6WA201040330Panel · damagedFUEL PANEL 640BB HAS GRINDING MARKS IN THE RED SEAL AREA. REPAIRED FUEL PANEL 640BB IAW REO 601R-52-21-1263.SDR COMA2010040150080Skin · crackedA LT BOOST PUMP MOUNT HOLE IS CRACKED. REPAIRED DAMAGED HOLE IAW REO 601R-57-21-169.SDR FDEA201003311039Skin · crackedDROOP L/E HAS CHAFED AT LEADING INBD AND OTBD SIDES AND CRACK ON THE UPPER SKIN AT RT WING. REPAIR CRACK UPPER SKIN WITH A 0.100" 301-50 STAINLESS STEEL DOUBLER IAW SRM 57-10-00 FIG 55, MAJOR REPAIR.SDR FDEA201003261015Skin · crackedCRACK IN THE RT WING LOWER SKIN INBD OF RIB 9 (FASTENER THROUGH JOGGLE SECTION) SHOWN ON FIG 3. (VERIFIED WITH EDDY CURRENT) COMPLIED WITH EA 6-5710-139432 "WINGS - AD 2008-06-17- RT WING LWR SKIN PANEL INBD OF RIB 9".SDR GUUA93957032510ASkin · corrodedDURING SCHEDULED ROUTINE INSP, DISCOVERED RT WING T/E TOP SURFACE HAS CORROSION AT WS 223.48. CUT OUT CORRODED SECTION OF RT WING T/E AT WS 223.48 AND INSTALLED EXTERNAL DOUBLER REPAIR.SDR REXA201000056Skin · corrodedLEFT WING LOWER PLANK CORROSION AT FUEL PANEL 540CB AT WS 76.161 HOLE NR 5 ON EDGE OF CUTOUT. MEASURES .007 INCH DEEP IN FORWARD AND .005 INCH DEEP IN AFT CRITICAL REGIONS. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV H. REPAIR DEPTH .008 INCH FORWARD ANDSDR IPXA10M59047Skin · chafedINSPECTION TYPE:C1 EXISTING DOUBLER ON RT WING TELESCOPIC DUCT CUTOUT HAS DEEP CHAFE ON IB AND OB SIDES. REMOVED OLD DOUBLER AND FILLERS. FABRICATED AND INSTALLED REPAIR REF SRM57-40-01 FIG 201 REPAIR 10.SDR GLBA20100324FSkin · dentedMAJOR REPAIR - PILOTS REPORTED THAT A BIRD STRIKE OCCURRED ON SHORT FINAL ON THE LT WING, LT OTBD SECTION OF THE WING. BETWEEN WING SIDE 249.5 & WING SIDE 261.5. DENT IS APPROX 12" IN LENGTH AND APPROX .5" IN DEPTH.SDR SWIA201023946Skin · crackedLEFT WING LOWER PLANK TRUNNION FASTENER HOLES CRACKED. (C CHECK) REPAIRED PER REO.SDR IPXA10M59012Skin · crackedINSPECTION TYPE:1C, LT WING FIXED L/E TELESCOPIC DUCT C/OUT OTBD CORNER CRACKED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLER IAW REV 43, SRM 57-40-01, REPAIR 10, FIG 201.SDR EIAA2010010Skin · corrodedLT WING L/E LOWER SKIN AT FRONT SPAR EXFOLIATED STA OLES 1534. REMOVED CORROSION, CUT OUT DAMAGE, NDT AREA, FABBED AND INSTALLED REPAIR PER ECRA 780-57-020-2.SDR UALA2010032200933Panel · leakingRT WING MID SEAM FWD OF PLATE 641FB IS LEAKING 24 INCHES IN 30 MINS, LOWER WING SURFACE. FUELED RT WING TO 33,000 LBS RT WING MID SEAM FWD OF PLATE 641FB IS LEAKING 24 INCHES IN 30 MINS. LOWER WING SURFACE. SEALED ON SMC24, FUELED AND LEAK CHECK GOODSDR SWIA201023910Skin · crackedLEFT WING LOWER PLANK AT TRUNNION FITTING FASTENER HOLES CRACKED. (C CHECK) REPAIRED PER REO.SDR UALA2010032200949Panel · crackedRT WING NEAR ROOT SMALL PANEL BELOW SLAT IS DAMAGED, CRACKED. PANEL IS 621BB, OUT OF LIMITS FOR SRM. CRACK IS APPROX 6 INCHES, ACROSS ENTIRE PANEL. REPLACED DAMAGED PANEL AND INSPECTED AREA WITH NO DAMAGE FOUND.SDR ABXA201003260013Skin · corrodedDISCOVERED CORROSION ON WING SKIN UNDER RIGHT WING PANEL P/N 113T1655-22 APPROX RT WING WS 916.75. REPAIRED AREA IAW REA'S B657-58728, B657-58729 AND B657-58730.SDR FDEA201003200949Panel · delaminatedRT WING T/E NR 2 DEFECTOR PANEL RUBBED TAPE LOOSE AND PEELING REPAIRED IAW EA 6-5720-136631. REMOVED T/E NR 2 DEFLECTOR TO FOM. REMOVED DAMAGED FOIL. APPLIED NEW ALUMINUM FOIL. INSTALLED HARDWARE IAW EA 6-5720-136631, N/R N00389 FOR ORIGINAL EA N/R N01255SDR FDEA201003200946Panel · delaminatedRT WING T/E NR1 DEFLECTOR PANEL RUBBED TAPE LOOSE AND PEELING REPAIRED IAW EA 6-5720-136631. R & R WS HARDWARE IAW SRM 51-40-00. REMOVED AND INSTALLED OF RT WING T/E NR 1 DEFLECTOR PANEL ACCOPMPLISHED IAW AMM 27-54-41-4. NR N01255 FOR THE APPLICATION OF THESDR FDEA201003190929Skin · crackedCRACK - LT WING L/E DROOP UPPER SURFACE. LT DROOP LEADING EDGE REPLACED AS PER AMM 27-80-10-4 REV 64.SDR FDEA201003180869Skin · crackedHFEC OPEN HOLE INSP AT RT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN STA XORS 690 AND XORS 700 FOUND CRACK INDICATION ON 09 EACH FASTENER HOLE. REPAIRED AS PER EA 1-5710-132384. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 109.SDR FDEA201003180868Skin · crackedHFEC OPEN HOLE INSP AT LT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN STA XORS 690 AND XORS 700. FOUND CRACK INDICATION ON 02 EACH FASTENER HOLE. REPAIRED AS PER EA 1-5710-132383SDR FDEA201003170858Skin · corrodedRT WING MLG TRUNNION FAIRING FWD MOUNT AREA WING LOWER SKIN HAS CORROSION REPAIRED RT WING MLG TRUNNION FWD ATTACH POINT IAW EA F-5730-131581, DATED MAR 1, 2010. CLASSIFIED CATEGORY "A" MAJOR REPAIR.SDR FDEA201003170857Skin · corrodedLT WING MLG TRUNNION FAIRING FWD ATTACH POINT SKIN IS CORRODED UNDER AND AROUND MOUNT REPAIRED LT WING LOWER SKIN AT MLG FAIRING FWD ATTACH POINT 7 IAW EA F-5730-131581, DATED MAR 1, 2010. CLASSIFIED CATEGORY "A" MAJOR REPAIR.SDR EE4Y1003030Skin · delaminatedRIGHT WING T/E CENTER BUTE DOOR P/N: 5919572-2 SN:1725 DELAMINATED.SDR UALA2010031500866Panel · crackedFOUND 5 INCH CRACK ON L/E COMPOSITE PANEL, O/B OF NR 2. ENGINE ABOUT 3 FT BACK OF LEADING EDGE. STARTED PREP FOR COMPOSITE REPAIR STARTED BLENDING AREA.SDR FDEA201003150823Skin · crackedRT WING L/E AT NR 5 SLAT TRACK CTR TRACK CUT OUT LOWER OTBD CORNER FOUND CRACKED. RT WING L/E NR 5 SLAT CTR TRACK LOWER OTBD CORNER TRIMMED OFF AND REPAIR CARRIED OUT IAW SRM 57-40-02 FIG 201 REV 43. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REVISION 109.SDR AALA20100314TUL02Skin · damagedTOP CENTER OUTER SKIN HAS LARGE CREASE IN TRAILING EDGE. FABRICATED AND INSTALLED DOUBLER PER ESO80174, PAGE 6(B)MRT025229.SDR FDEA201003130801Skin · unknownEXISTING REPAIR AT LEFT WING INBOARD FLAP UPPER SURFACE STA XIFH 216. REPAIR AS PER SRM 57-00-01 FIG 201 REPAIR 1 REV 43 (MAJOR REPAIR).SDR FDEA201003130800Panel · damagedEXISTING REPAIR AT RIGHT WING DROOP LEADING EDGE LOWER SURFACE INBOARD EDGE. REPAIR AS PER EA 1-5740-132379 TITLE: "WINGS - RT DROOP LEADING EDGE SKIN, REPAIR" (MAJOR REPAIR).SDR FDEA201003130799Panel · damagedEXISTING REPAIR AT LEFT WING DROOP LEADING EDGE LOWER SURFACE INBOARD EDGE. LT DROOP LEADING EDGE REPLACED AS PER AMM 27-80-10-4 REV 64.SDR FDEA201003130808Fairing · chafedRT WING FIXED L/E FAIRING LOWER SURFACE HAS CHAFED MARK AT INBD FAIRING TO NR 3 PYLON. REPAIRED RT WING FIXED L/E FAIRING LOWER SURFACE IAW SRM 57-10-00 AND SRM 51-31-01, REPAIR CLASSIFIED AS MAJOR.SDR FDEA201003130814Skin · crackedRT INBD FOREFLAP CARRIAGE ATTACH FITTING AREA AT STA 224, SKIN CRACKED FWD OF ATTACH FITTING. CUT OUT DAMAGED AREA, DIMENSIONS .750" X .218" IAW SRM, REV 102, 57-50-4, FIG. 1. FABRICATED FILLER USING 2024 T-3, PO NR 9002222, DIMENSIONS .050" X .750" X .218" SDR FDEA201003130802Skin · unknownEXISTING REPAIR AT LT WING INBD FLAP UPPER SURFACE STA XIFH 200. REPAIR AS PER SRM 57-00-01 FIG 201 REPAIR 1 REV43 (MAJOR REPAIR).SDR SAJ2010F00000Access Panel · cracked(B-18608) DAILY CHECK FOUND LT FUEL TANK ACCESS PANEL 532LB FUEL SEEPING TRACE. THE ACCESS PANEL WAS REMOVED AND FOUND A CRACKED DOME. THE ACCESS PANEL WAS REPLACED WITH NEW ONE. LEAK TEST WAS NORMAL. HAVE FOUND THAT A BUILDUP OF MOISTURE IN THE DOME OF TSDR SAJFCAL2010001Access Panel · crackedDURING DAILY CHECK, FUEL SEEPING TRACE WAS FOUND ON LT FUEL TANK ACCESS PANEL 532LB. THE ACCESS PANEL WAS REMOVED AND A CRACKED DOME WAS FOUND. MFG HAS FOUND THAT A BUILD-UP OF MOISTURE IN THE PANEL DOME CAN CAUSE A CRACK AFTER GOING THROUGH MUTIPLE FREEZE ANSDR UALA2010031200840Panel · bowedFOUND RT WING LWR PANEL BOWED. FOUND WIGGLE PLATES C, D, G, WITH PULLED RIVETS AS VIEWED IN IPC. WING PANELS 661GB,WS698, AFFECTED. 3 EA WAFFEL OR RIPPLE SUPPORT PANELS REMOVED FROM RT WING PANELS ARE IN SMC OFFICE. RETRIEVED SUPPORT PANELS. MFG NEW SUPPOSDR IXXA10SMN044SSkin · crackedDURING ROUTINE C-CHECK INSP FOUND FWD CARGO COMPARTMENT INTERNAL SKIN CORRODED AT STA FS 285.000 LONGERON 35 RT- LONGERON 36. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO SDR P5CA2010031001624Winglet · damagedDURING PARKING OPERATION OF N452PA, THE LEFT WINGLET OF N450PA AND DAMAGED IT. THE LEFT WINGLET WAS REMOVED IAW CDL 57-28-1 AND AMM 57-28-01. NO FURTHER DAMAGED WAS NOTED.SDR P5CA2010031001623Winglet · damagedDURING PARKING OPERATION THE LEFT WINGLET MADE CONTACT WITH THE LEFT WINGLET OF AIRCRAFT N450PA. THE LEFT WINGLET WAS REMOVED IAW CDL 57-28-1 AND AMM 57-28-01. NO FURTHER DAMAGE WAS NOTED.
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