JASC 5710
Service difficulty reports · 4,462
Reports filed under 5710 · Wing Main, Frame Structure, 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 = '5710' 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 = '5710' 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 ASAA0480322Splice Plate · crackedOKC - DURING HV CHECK, FOUND LEFT WING LEADING EDGE SPLICE PLATE IS CRACKED AT STATION XRS164. REMOVED DAMAGED SPLICE PLATE AND INSTALLED NEW PER SRM 51-10-4. (M)SDR UIEA200400045Beam · crackedD CHECK, CRACKS WERE FOUND AT RT WING LE LOWER OUTBOARD BEAM LOCATIONS AT ILES 414.50 AND 543.93. TRIMMED OUT CRACKED PORTIONS OF BEAM NDT INSPECTED TO ENSURE CRACK AND DEFECT FREE CONDITION. SPLICED IN REPLACEMENT SECTIONS OF BEAM BETWEEN TRIM LINES AND PROSDR MALA040311Structure · bird strikeBIRD STRIKE LEFT INBOARD WING. REPLACED LEFT I/B LEADING EDGE ASSY P/N 7257500-787, S/N OFF NSN, S/N ON 206069 PER AMM 57-20-05-4, OPS AND LEAK CHECK GOOD.SDR 18069Structure · crackedTHE CRACK/CORROSION IS LOCATED ON THE AFT VERTICAL SIDE OF STRINGER (HAT SECTION) NR 18. IT IS LOCATED IN THE LEFT HAND OUTER WING AT WING STATION 284. THE CRACK/CORROSION IS 1.25 INCH LONG AND RUNS SPAN WISE. THE CORROSION WAS REMOVED COMPLETELY AT .024 OFSDR 04FDEA01718Angle · crackedEXISTING REPAIR SPLICE ON LEFT WING STRINGER 4 CRACKED AT XORS 930. CRACKED REPAIR ANGLE REPLACED BY A NEW REPAIR ANGLE MADE FROM 7075-73511 THAT ARE MORE FATIGUE RESISTANT IAW FEDEX EA 8-5710-73240.SDR UPS04841955Wing Root · corrodedRIGHT WING ROOT HAS CORROSION (EXFOLIATION). A/C FERRIED TO TCO DEFERRED (276424) AND TRANSFERRED TO NRC 469644 RMVD RH OVERWING EMERGENCY HATCH TO FOM. RMVD R/H OVERWING TO FUSELAGE FILLET PNL 292F TO FOM. RMVD CORRODED PAD FR R/H W/W IAW DC8-SRM 51-1 -20. SDR GKZR200482304Structure · crackedLT WING INSIDE NR 1A FUEL TANK FROM ACCESS PANEL 505B BETWEEN STA. 495.665 AND 508.977 LWR STRINGER NR 53 CRACKED. CUT AND REMOVED STRINGER NR 53 BETWEEN STA 495 AND 508 IAW DC-8 SRM 57-2-2. CUT AND INSTALLED REPLACEMENT STRINGER AND SPICES IAW DC-8 SRM 57-2-SDR DHL2004741002Mount · crackedNR 6 LEADING EDGE K-FLAP ACTUATOR MOUNT ON SPAR APPEARS TO BE CRACKED AT INBOARD SIDE AT BASE OF TRUNNION CAP. REMOVED NR 6 LEADING EDGE K-FLAP ACTUATOR ASSEMBLY TO FOM. REMOVED INBOARD VERTICAL WEB SECTION OF NR 6 K-FLAP ACTUATOR MOUNT BOX, FABRICATED REPLASDR UIEA200400008Beam · crackedDURING (D) CHECK AT SIN, RT WING LEADING EDGE NOSE BEAM WEB FOUND WITH 4.2500 CRACK AT ILES 1042. REPAIR, TRIM OUT SECTION OF CRACKED WEB TO REMOVE DAMAGE. NDT INSPECTED TO ENSURE CRACK AND DEFECT FREE CONDITION. SPLICE IN REPLACEMENT WEB REPAIR SECTION WITSDR CALA0400049Beam · crackedINSPECTION FOUND A 2 INCH CRACK IN LT WING T/E BEAM (IN FRONT OF AILERON CENTER HINGE). REMOVED AND REPLACED BEAM IAW SRM 51-10-02.SDR 04FDEA00010Support Bracket · corrodedLT WING O/B FLAP O/B HINGE (FLAP SIDE) PIVOT I/B BORE HOLE FOUND CORROSION. REMOVED & FOUND WITHIN LIMITS AS PER FEDEX EA 1-5750-75220, WINGS - TE & TE DEVICES - LT O/B FLAP / O/B SUPPORT BRACKET CORROSION REMOVAL & REPAIR.SDR 04FDEA00006Bulkhead · gougedCOMPLY WITH EA 8-5710-73861 WINGS MAIN FRAME GOUGE REPAIR XORS 562.390 FLAP BULKHEAD UPPER CAP (LT). CLOSING ACTION ON N/R S00027, ON 13/30/03. COMPLIED WITH EA 8-5710-73861.SDR UPS04841681Rib · crackedINSPECTION TYPE:C2 LEFT WING CENTER L/E UPPER RIB IS CRACKED AT XS 448.581. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2.SDR 03FDEA02265Hinge · corrodedRIGHT WING - O/B FLAP I/B HINGE FITTING I/B MOUNT BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75199 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.SDR 03FDEA02263Hinge · corrodedRT WING O/B FLAP I/B HINGE FITTING O/B MOUNT BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75199 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.SDR 03FDEA02278Stop Fitting · corrodedRT WING, INBOARD FLAP VANE INBD STOP FITTING ATTACHMENT BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75225 - WINGS - TRAILING EDGES AND TRAILING EDGE DEVICES - RT INBOARD FLAP VANE STOP SUPPORT FABRICATION.SDR 03FDEA02192Fitting · wornRIGHT WING - INBOARD FLAP VANE, INBOARD TRACK ATTACHMENT FITTING, BOLT HOLES (3) FOUND EXCEED LIMIT. RT WING - INBD FLAP VANE, INBD TRACK ATTACHMENT FITTING, BOLT HOLES REPAIRED AS PER EA 1-5750-73366, TITLE : WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - SDR 03FDEA02191Fitting · wornLEFT WING - INBOARD FLAP VANE, OUTBOARD TRACK ATTACHMENT FITTING, BOLT HOLES, FOUND 3 THAT EXCEED LIMITS. LT WING - INBD FLAP VANE, OUTBOARD TRACK ATTACHMENT FITTING, BOLT HOLES REPAIRED AS PER EA 1-5750-75176, TITLE : WINGS - TRAILING EDGE AND TRAILING EDGSDR CA031203003Support · cracked(CAN) FUEL TANK SUPPORT BRACKETS FOUND CRACKED AT ENDS DIRECTLY OFF OF WELDS. 3 IB BRACKETS CRACKED IN RT WING NONE IN LT WING. NUMBER OF CRACKS VARY FROM 2 TO ALL 4 POINTS OF EACH BRACKET.SDR CA031203002Support · cracked(CAN) FUEL TANK SUPPORT BRACKETS CRACKED AT ENDS DIRECTLY OFF OF WELDS. 5 OUT OF 6 BRACKETS CRACKED IN LT WING AND ONLY 1 FOUND CRACKED IN RT WING.SDR CA031205007Strut · corroded(CAN) WING STRUT WAS REMOVED TO INSPECT/REPAIR SLOPPY STRUT ATACHMENT CONDITION. UPON REMOVING STRUT ASSEMBLY, LUG FACES (FORWARD/AFT) FOUND CORRODED. REF. PSM 1-3-3 FIG 2-1 (DHC-3 REPAIR MANUAL).SDR A6WA200340185Bushing · looseFOUND LT MLG AFT WING SPAR BUSHING MIGRATED .052 INCH. REMOVED MIGRATED BUSHING ON LEFT MLG, AND INSTALLED FIRST OVERSIZE BUSHING, P/N 601R-57-21-003-21 IAW REO 601R-57-21-003 REV B. (M)SDR 03FDEA01995Stop Fitting · crackedLT WING OUTBOARD FLAP STOP FITTING FOUND CRACK. LT WING OUTBOARD FLAP STOP FITTING CRACKED AREA REPAIR CARRIED OUT AS PER EA 1-5750-73349, - TRAILING EDGE AND TRAILING EDGE DEVICES - LT & RT OUTBOARD FLAP SECONDARY UP STOP REPAIR.SDR 03FDEA01994Stop Fitting · crackedRT WING OUTBOARD FLAP STOP FITTING FOUND CRACKED. CRACKED AREA REPAIR CARRIED OUT AS PER EA 1-5750-73349, TRAILING EDGE AND TRAILING EDGE DEVICES. LT & RT OUTBOARD FLAP SECONDARY UP STOP REPAIR.SDR AUS20031210Structure · bird strike(AUS) RT WING LEADING EDGE DAMAGED BY BIRDSTRIKE.SDR DHL2003742521Doubler · crackedDURING C-CHECK, RT WING L/E STA 130 INT FRAME DOUBLER TO UPPER SURF IS CRACKED ABOVE FASTENER. REMOVED DAMAGED AREA IAW B-727 SRM 51-30-2. FABRICATED NEW DOUBLER IAW SRM MAT ID 7075 T6 .050 PO 90096 DIM 10 X 1.75 INCH IAW B-727 SRM 51-40-4 FIG 1. TREATED PSDR 03FDEA01936Hinge · corrodedLEFT OUTBOARD FLAP, FOUND INBOARD HINGE FITTING ACTUATOR MOUNT HOLE INBOARD CORRODED (WING SIDE). COMPLIED WITH FEDEX EA 1-5740-74250 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSEMBLY CORROSION.SDR 03FDEA01937Hinge · corrodedLEFT OUTBOARD FLAP, FOUND INBOARD HINGE FITTING LOWER MOUNT BOLT HOLE OUTBOARD FLANGE SIDE CORRODED (WING SIDE). LT O/B FLAP, INBD HINGE FITTING LOWER BOLT HOLE O/B FLANGE SIDE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-08 AND DWG ARC0502.SDR 03FDEA01938Hinge · corrodedLEFT OUTBOARD FLAP, FOUND INBOARD HINGE FITTING LOWER MOUNT BOLT HOLE INBOARD FLANGE FACE CORRODED (WING SIDE). LT O/B FLAP INBD HINGE FITTING LOWER MOUNT BOLT HOLE I/B FLANGE FACE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-08 NAD DWG ARC0502.SDR GTIA030972Frame · crackedFTW - FOUND LEFT WING AT NR 1 SLAT AND WING ANTI-ICE TELESCOPING DUCT LOWER PANEL STRUCTURE CRACKED AT FORWARD OUTBOARD CORNER IN RADIUS. REMOVED AND REPLACED FRAME. (M)SDR A6WA200340154Beam · damagedRT WING FLAP HINGE BEAM AT WS 178 FORWARD EDGE AND LOWER SURFACE HAS MUSHROOMED METAL AND GOUGES. BLENDED AREAS SMOOTH, PERFORMED EDDY CURRENT INSPECTION OF AREAS, PERFORMED ROTO/FLAP PEEN OF REPAIR AREAS AND RESTORED FINISH TO ORIGINAL CONFIGURATION IAW WVACSDR 03FDEA01816Stop Fitting · crackedLEFT WING - OUTBOARD FLAP STOP FITTING FOUND CRACKED.SDR 03FDEA01815Stop Fitting · crackedRIGHT WING - OUTBOARD FLAP STOP FITTING FOUND CRACKED. TRAILING EDGE AND TRAILING EDGE DEVICES - LT & RT OUTBOARD. FLAP SECONDARY UP STOP REPAIR.SDR 03FDEA01635Support · crackedLT OUTBOARD FLAP FWD RIB SUPPORT ISLAND FOUND ONE ADDITIONAL CRACK APPROX .1875 INCH IN LENGTH AT OUTBOARD UPPER SIDE. LT OUTBOARD FLAP FWD RIB SUPPORT ISLAND REPAIR CARRIED OUT AS PER EA 1-5750-71897, TITLE : WINGS - TRAILING EDGE AND TRAILING EDGE DEVICESSDR 03FDEA01471Rib · crackedCRACK INDICATION NOTED AT BS 760 WL 208 RBL 70.5 IN THE FWD UPPER HOLE COMMON TO THE RIB CHORD UPPER VERTICAL FLANGE IN THE RIB CHORD LAYER AT THE 12 O'CLOCK POSITION. REPAIRED PER EA 7-5710-54691 AND EO 7-5710-7-2308 I PT 3.SDR AWXA200301148Attach Angle · crackedDURING C-16 CHECK A .75 INCH CRACK WAS FOUND ON RT WING TRAILING EDGE UPPER PANEL INBOARD ATTACH ANGLE AT WBL 198.6. MAINTENANCE REMOVED CRACKED ATTACH ANGLE AT WBL 198.6; FABRICATED A NEW REPLACEMENT ATTACH ANGLE; INSTALLED REPAIR PART IAW B737-300 SRM 51-40SDR 03FDEA01187Hinge · corrodedRT WING- O/B FLAP (WING SIDE) I/B HINGE I/B AND O/B ACTUATOR ATTACHMENT HOLES CORRODED. RT WING O/B FLAP (WING SIDE) I/B HINGE I/B AND O/B ACTUATOR ATTACHMENT HOLES REPAIRED AS PER FEDEX EA 1-5750-69405 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES SDR 03FDEA01147Bracket · crackedNR 1010 RIGHT WING LOWER SPAR-TO-RIB FITTING IS CRACKED AT STA XORS 402 LWR SPAR S36. CLOSING ACTION ON 07/23/03, REMOVED BUTTERFLY BRACKET IAW SRM 51-33-01, INSTALLED NEW BRACKET IAW SRM 51-33- 01. TORQUE HI-LOCKS IAW SRM 51-31-01. SEALED IAW SRM 51-41-0SDR A6WA200340110Structure · chafedLT INBOARD FLAP VANE HAS A PROTRUSION THAT IS CHAFING THE FLAP STUB WING STRUCTURE. PERFORMED A MAJOR REPAIR TO LEFT FLAP VANE BY REPLACEMENT OF LOOSE FASTENERS. WORK ACCOMPLISHED IAW WEST VIRGINIA AIR CENTER. EO 601R-57-4131 AS APPROVED BY FAA 8110-3. (M)SDR AUS20030767Structure · misrepaired(AUS) LOWER RT WING FAULTY. SUSPECT CAUSED BY FAULTY WORKMANSHIP WHEN REPAIRING DAMAGE AND AGED COMPONENTS. PERSONNEL/MAINTENANCE ERROR. UNAPPROVED PART.SDR 03FDEA01099Pivot · corrodedLT INBD FLAP,OUTBOARD HINGE (FLAP SIDE ) INBD AND OUTBOARD PIVOT BORES CORRODED. REPAIR CARRIED OUT AS PER SRM 51-21-01 VOL. 2 AND FEDEX EA - 1-5750-71842 WINGS - TRAILING EDGE FLAPS - INBOARD TRAILING EDGE FLAP - OUTBOARD FLAP HINGE BRACKET CORROSION REPAISDR SWAA031378Shear Tie · crackedDURING SCHEDULED D CHECK, FOUND RT WING SHEAR TIE CRACKED AT STA 135.5 LOWER REAR SPAR. REPAIRED SHEAR TIE PER SRM.SDR 03FDEA00939Hinge · looseRT- O/B FLAP I/B HINGE (FLAP SIDE) I/B PIVOT POINT BUSHING FOUND LOOSE. RT WING O/B FLAP I/B HINGE (FLAP SIDE) I/B PIVOT POINT BUSHING REPLACED IAW EA 1-5750-69375, TITLE: WINGS- TRAILING EDGE FLAP- RT OUTBOARD FLAP- INBOARD SUPPORT BRACKET- CORROSION RESDR 03FDEA00897Fitting · crackedRT WING O/B FLAP STOP FITTING (NR 2 FLAP VANE TRACK) FOUND CRACKED. COMPLIED WITH FEDEX EA 1-5750-67554 PT 1 - WINGS OUTBOARD TRAILING EDGE FLAPS - SECONDARY UP STOP - REPAIRSDR UPS03840857Stiffener · crackedINSPECTION TYPE: C3, LEFT WING TE. VERTICLE STIFFNER IS CRACKED TWO PLACES AT XW 11.5 REMOVED,FABRICATED AND REPLACED STIFFNER I.A.W. DWG. 9887427 AND SRM 51-1-20D.SDR 03FDEA00889Clip · brokenLT WING PANEL 572LB END CLIP IS BROKEN. REMOVED AND REPLACED CLIP IAW SRM 51-40-21 ON N00595 AT MAE.SDR GTIA030425Structure · brokenRIGHT WING LEADING EDGE LIP AT RE-FUELING PANEL OPENING IS BROKEN OFF AT INBOARD LATCH. TRIMMED OUT DAMAGE. FABRICATED 11 DOUBLER. FABRICATED 13 FILLER. I NSTALLED REPAIR DOUBLER AND FILLER. (M)SDR DHL2003746506Angle · crackedDURING C-CHECK, N/R 54144 RT WING LEADING EDGE L-ANGLE IS CRACKED JUST INBOARD OF NR 4 KRUEGER FLAP AT L/E STA 130.7. NR 4 L/E FLAP REMOVED AND REINSTALLED ON NR 54306. REMOVED FASTENERS AND SUB-STRUCTURE FOR ACCESS IAW B-727 SRM 51-30-2. CUT-OUT DAMAGED SESDR 03FDEA00781Hinge · corrodedS 16 COMPLY WITH E.A.8-5740-70384. WINGS INBD FLAP OUTBD HINGE SUPPORT FITTING TO WING ATTACH HOLES REWORK. CLOSING ACTION ON 05/19/03. COMPLIED WITH E.A.8-5740-70384.SDR 03FDEA00784Hinge · damagedS 26 COMPLY WITH E.A.8-5740-70391. WINGS LT I/B FLAP HINGE ASSY ATTACH LUG REWORK. CLOSING ACTION ON 05/19/03. COMPLIED WITH E.A.8-5740-70391
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