JASC 5341
Service difficulty reports · 489
Reports filed under 5341 · Fuselage, Wing Attach Fittings, 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 = '5341' 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 = '5341' 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 ASOA200900261Spherical Bearin · crackedRT AFT WING TO FUSELAGE ATTACH LINK AT FS 797.00 UPPER SPHERICAL BEARING CRACKED. PERFORMED DETAIL VISUAL INSPECTION OF THE RT UPPER SPHERICAL BEARING TO ENSURE THAT THE BALL IS PROPERLY RETAINED IN THE RACE OF THE BEARING. ALSO PERFORMED A DETAILED INSPECTISDR ASOATRAX200801036Spherical Bearin · crackedRT WING TO FUSELAGE PICK UP LINK AT FS 787.00 UPPER AND LOWER SPHERICAL BEARINGS CRACKED. REQUIRES REPEAT INSP EVERY 1000 FLT HRS.SDR ASOATRAX200801037Spherical Bearin · crackedRT WING TO FUSELAGE PICK UP LINK AT FS 787.00 UPPER AND LOWER SPHERICAL BEARINGS CRACKED DUE PERMANENT REPAIR. THIS SDR WILL REMAIN OPEN PENDING MAINTENANCE DETERMINATION OF AN APPROPRIATE CORRECTIVE ACTION.SDR LR7A08074Web · crackedDURING SCHEDULED C-8 CHECK, FOUND WEB CRACKED AT BOLT HOLE UPON REMOVAL OF RT WING ATTACH ANGLE AT FS 596, WL250, RBL61.5. REPAIR ACCOMPLISHED IAW LAC MEA 382-53-08-026.SDR ASMF200805001Structure · dentedCAPTAIN REPORTED A DENT IN RT FWD GALLEY DOOR. MAINT PERFORMED INSPECTION FOUNDING A DENT OF .2500 INCH DIAMETER AND .1250 INCH DEPTH, BETWEEN BS 309 AND 323 AND LONGERONS 17 AND 21 IN RT FWD GALLEY DOOR, WITHIN LIMITS IAW SRM 53-00-01, FIGURE 103.SDR TRAX200800560Bearing · crackedRIGHT WING-TO-FUSELAGE ATTACH LINK AT FS 797.00 UPPER SPHERICAL BEARING CRACKED.SDR 2008FA0000073Attach Fitting · corrodedTHIS FUSELAGE REAR WING ATTACH FITTING WAS BEING REPLACED DUE TO CORROSION PITTS ON FRONT SURFACE. UPON REMOVAL SOME SEVERE PITTING WAS NOTED JUST IB OF THE .3125 INCH WING ATTACH BOLT HOLE ON THE REAR SIDE OF THE FITTING. THIS AREA IS EXPOSED TO OUTSIDE AIRSDR HAEA002002007Attach Fitting · corrodedDURING TANK AND PLANK INSPECTION THE LT AND RT WING TO FUSELAGE ATTACH FITTINGS WERE DISCOVERED TO HAVE MINOR CORROSION ON THE LOWER OB SURFACE. THE WINGS WERE DEMATED TO INSURE THAT CORROSION HAD NOT MIGRATED TO BETWEEN THE WING TO FUSELAGE ATTACH FITTINGS. SDR 2007UALA01919Torque Tube · unstableFWD GALLEY DOOR CUTOUT TORQUE TUBE HAS MOVEMENT BEYOND 0.003. [07-03-07] REPLACED THE BEARING AND TORQUE TUBE.SDR GUUA05120701Attach Fitting · crackedAT SCHEDULED INSPECTION DISCOVERED RIGHT WING TO FUSELAGE FITTING UPPER ATTACH AREA CRACKED. REPAIRED RIGHT WING TO FUSELAGE FITTING IN ACCORDANCE WITH FAA APPROVED DATA CONTAINED IN RBHA CTA DER RCE2001C12-24, REPORT NUMBER IC2007-120/0203B.SDR CA070418007Fitting · corroded(CAN) A CURSORY INSPECTION REVEALED CORROSION ON THE LT PORK CHOP FITTING. BOTH LT AND RT FITTINGS WERE REPLACED WITH NEW UNITS. DEPTH OF CORROSION WAS APPROX 25 PERCENT OF PART OVERALL THICKNESS. THE MANUFACTURE WAS CONTACTED. THE PART IN QUESTION IS APPROX 1SDR 2007F00024Lift Strut · crackedFOUND RT WING STRUT CRACKED AT LOWER END DURING AICRAFT INSPECTION PROGRAM. 20 DAYS AND 16 HOURS LATER FOUND LT WING STRUT CRACKED AT LOWER END. AIRCRAFT HAS AOG 400 LB UP-GROSS STC SA00438NY INSTALLED.SDR N382006F00003Attach Fitting · corrodedIAW MM, TO COMPLY WITH THE 24 MONTH NDT REQUIREMENTS UNDER THE ULTRASONIC, CORROSION WAS FOUND UNDER THE LT FWD WING ATTACHMENT FITTING AT FUSELAGE STA 345, BUTT LINE 40. (K)SDR QXEA200601313Attach Angle · corrodedYYC - C4 FUSELAGE INTERIOR BAGGAGE COMPARTMENT, LOWER DOOR SILL ATTACH ANGLE ON THE FORWARD SIDE OF FRAME AT STATION X 600 AND LBL 30 IS CORRODED. REPAIRED IAW SRM 51-40-11.SDR 2006FA0000459Attach Fitting · out of limitsATTACHMENT CONNECTIONS AT RT AND LT SIDES ARE BELOW MINIMUM SPECIFIED IN AD. INSPECTION METHOD- ULTRASONIC. (K)SDR 11143Fitting · crackedLT AND RT WING ATTACH POINT FITTING AT FRAME 20 IS CRACKED. LT IS CRACKED APPROX. 1.0 INCHES IN LENGTH. RT IS CRACKED APPROX. 1.25 INCHES IN LENGTH.SDR UPS06846208Attach Angle · crackedINSPECTION TYPE:C3 RT WW LWR SPAR ATTACH ANGLE CRACKED 1" LONG STA 857.125. MACHINED REPAIR ANGLE IAW DWG 5649893 AND INSTALLED REPAIR ANGLE AT RT WW STA 857.125 IAW SRM 51-1-21 AND SRO 8570009.SDR QXEA200600572Seat Track · corrodedYYC C3 FUSELAGE INTERIOR, RIGHT HAND INBOARD SEAT TRACK, BETWEEN FUSELAGE STATION 485 AND 581, HAS SIX AREAS OF CORROSION AND/OR TOOL MARKS. REPAIRED IAW REO 670-53-00-013, REV A.SDR 1054822Frame · crackedFOUND CRACKS ON THE FUSELAGE SIDE OF FRAME 20 ON BOTH LT AND RT SIDE. FRAME 20 IS THE WING ATTACH POINT. ON THE LT SIDE THE LENGTH OF THE CRACK WAS 1.25 INCH IN LENGTH AND ON THE RT SIDE, 1.50 INCH.SDR 10548226Frame · crackedFOUND CRACKS ON THE FUSELAGE SIDE OF FRAME 20 ON BOTH LT AND RT SIDE. FRAME 20 IS THE WING ATTACH POINT. ON THE LT SIDE THE LENGTH OF THE CRACK WAS 1.25 INCH IN LENGTH AND ON THE RT SIDE, 1.5 INCH.SDR 2005FA0001244Attach Fitting · corrodedDURING THE ANNUAL INSPECTION, THE WING FITTING WAS FOUND TO BE CORRODED SO SEVERE THAT IT WAS ALMOST .2500 OF THE WAY THRU THE FITTING. PICTURES ENCLOSED THAT SHOW DAMAGE. FITTING WAS LOCATED ON THE LT SIDE, AFT TOP FITTING. (K)SDR 20050505Tube · crackedWHILE PERFORMING THE 1500 HOUR INSPECTION REQUIRED BY AD 82-16-08, A CRACK WAS FOUND ON THE RT VERTICAL TUBE OF THE CARRY THRU. THE CRACK WAS LOCATED AT THE TOP WELD OF THE TUBE. THE LENGTH OF THE CRACK IS ROUGHLY HALF THE CIRCUMFERENCE OF THE TUBE ON THE FRSDR 2005FA0000588Wing Root · loose(A) BEARING IN LT WING FOUND LOOSE WITH .0625 INCH PLAY UP AND DOWN. NO PLAY FORE AND AFT. PASTE FROM BEARING ATTACH FOUND LOOSE IN WING BAY. REMOVED BEARING AND FOUND NO DAMAGE TO END RIB. FOUND WITH WING OFF DURING 1000 HOUR INSPECTION.SDR 05FDEA00990Tee Fitting · corrodedCOMPLY WITH EA 8-5340-55468, FUSELAGE-CORROSION IN WING-TO-FUSE TEE ATTACH HOLE. CLOSING ACTION ON 04/12/05. ON N/R S00011. COMPLIED WITH EA8-5340-55468SDR 05FDEA00414Wing Root · corrodedTWO AREAS OF CORROSION AT RT WING TO FUSE FILLET AREA FR 39 STR 34-35 REF N00735 & E-6-5310-7-3315 A1 PT8. C/W AIRBUS S/B A310-53-2069 AND EO 6-5310-7-3315 ERF N00735.SDR UPS05844016Attach Angle · crackedINSPECTION TYPE: C1, SPAR-TO-WING ATTACH ANGLE CRACKED IN MAIN CABIN SUBFLOOR, STA 798 RBL 55. FAB REPLACEMENT ANGLE REF DWG3643112 ON SAA SERVICE ORDER 7034920. REMOVED & REPLACED ANGLE REF SRM 51-1-20D, 51-3-2, 51-1-24, 51-1-20D. FUEL LEAK CHECK C/W ON TCSDR CA050223012Fitting · cracked(CAN) DURING AD-81-25 THIS FITTING WAS FOUND CRACKED AND IT WAS REPLACED IAW THE SIRM.SDR SWIA200414448Bracket · crackedWING CENTER SECTION LEFT SIDE LOWER FUSELAGE BRACKET CRACKED. ITEM FOUND AT C-CHECK INSPECTION. BRACKET REPLACED IAW EMB SRM 51-25-00, 51-30-01, 51-40-02.SDR QFY2004F00000Link · inadequateLT FRONT WING LINK NOT SAFETYED FROM FACTORY. UPON PERFORMING WING LINK INSPECTION TO RID AIRCRAFT OF CLUNKING NOISE, FOUND LINK NOT SAFETYED. THE BOLT WAS STILL TIGHT AT THIS POINT, BUT THE WING LINK INSPECTION WAS BEING ACCOMPLISHED 3 YEARS EARLIER AS WELLSDR 2004FA0000679Attach Fitting · corrodedLOWER AFT WING TO CENTER BOX ATTACH SKATE FITTING IS EXFOLIATED, LT WHEEL WELL, FUSELAGE STATION 1366 TO 1381. REFERENCE NON-ROUTINE NR 39431.SDR CA040519013Fitting · cracked(CAN) DURING THE ROUTINE COMPLETION OF CF1981-35 SITES NR 1 AND NR 2, A SMALL CRACK WAS DISCOVERED ON THE LOWER RT, IB BATHTUB FITTING. THE CRACK APPEARED TO START ON THE FEATHERED EDGE AT THE CENTER OF THE RADIUS AND PROPOGATE TOWARD THE MATING SURFACE OF THESDR 2004FA0000374Attach Fitting · looseDURING A ROUTINE INSPECTION, THE LT AFT WING ATTACHMENT FITTING WAS FOUND TO HAVE A LOOSE ATTACHING BOLT. THIS PROBLEM HAS BEEN TYPICAL ON A FLEET OF 6 AIRCRAFT OF THIS MODEL. THE PARTS IN QUESTION ARE: P/N-401-187 BOLT (AN5-7A), P/N-66762-00 (PLATE-AFT SPAR) SDR CA040510002Frame · crackedWHILE PERFORMING AD CF-1997-07R2 A CRACK WAS DISCOVERED BY EDDY CURRENT ABOUT ONE AND A HALF INCHES LONG ON THE OUTBOARD RT REAR WING TO FUSELAGE FRAME ANGLE. THE CRACK BECAME VISUALLY APPARENT AFTER BEING DETECTED BY NDT. THE CRACK STARTED AT THE TOP OF FRASDR BHA04RSAttach Fitting · corrodedIN COMPLYING WITH SUPPLEMENTAL INSPECTION 57-10-20, FOUND THE RT WING LOWER SPAR ATTACH FITTING HAD SIGNIFICANT CORROSION IN SOME OF THE FITTING MOUNTING HOLES. THE FITTING WAS REPLACED. NO FURTHERDEFECTS WERE NOTED.SDR AUS20040006Washer · wrong part(AUS) LT AND RT WING LOWER ATTACHMENT BOLT WASHERS INCORRECTLY FITTED. DAMAGE TO BATHTUB FITTING. PERSONNEL/MAINTENANCE ERROR.SDR QXEA200301152Flange · chafedWING TO FUSELAGE FAIRING FORWARD APERTURE FLANGE IS CHAFED AT PANEL 262AT. REPAIRED IAW Q400 SRM 51-00-02 AND RD 8/4-53-451.SDR QXEA200301151Flange · chafedWING TO FUSELAGE FAIRING FORWARD APERTURE FLANGE IS CHAFED AT PANEL 262FT. REPAIRED IAW Q400 SRM 51-00-02 AND RD 8/4-53-451.SDR QXEA200301150Flange · chafedWING TO FUSELAGE FAIRING FORWARD APERTURE FLANGE IS CHAFED ON PANEL 262HT. REPAIRED IAW Q400 RD 8/4-53-451 AND SRM 51-00-02.SDR UPS03440829Fitting · corrodedINSPECTION TYPE: C, LT BS 1241 WING REAR SPAR LOWER SPLICE PLATE ONE EACH BOLT HOLE -K- LOCATION FOUND CRACK AND CORROSION AT 3 O'CLOCK POSITION 0.040 INCH DEPTH APPROX AND 5 O'CLOCK POSITION 0.040 INCH APPROX RESPECTIVELY. REPAIRED AS PER R57-12-35029 AND ESDR AUS20030514Spacer · fractured(AUS) WING TO FUSELAGE RT SPACER FRACTURED.SDR AUS20030432Bolt · corroded(AUS) RT WING ATTACHMENT LUG MOUNT BOLTS (3 OFF) CORRODED. LT WING ATTACHMENT LUG MOUNT BOLT HEAD DISLODGED. FOUND DURING INSPECTION IAW AD/BAE146/052 AMDT1.SDR AUS20021255Bracket · cracked(AUS) LT AND RT WING FORWARD ATTACHMENT BRACKETS CRACKED. CRACKS ARE LARGE AND EASILY VISIBLE TOTHE NAKED EYE. LAST PERIODIC INSPECTION WAS 20.7 HOURS PREVIOUSLY. FOUND DURING INSPECTION IAW AD/BEECH23/14A2 AND BEECH SI NO 0042-031 REVII. PERSONNEL/MAINTENANCESDR AUS20021161Gusset · broken(AUS) FORWARD FRONT WING SPAR PICKOFF STRUCTURE CRACKED AND LOOSE. FLANGED GUSSET LOCATED AT BS 94.00 BROKE FREE FROM FUSELAGE STRUCTURE.SDR AUS20021126Fitting · corroded(AUS) WING ATTACHMENT TOP BATHTUB FITTINGS CORRODED AND DRAIN HOLES BLOCKED. NO CORROSION PROTECTION ON FITTINGS.SDR CA020715001Structure · cracked(CAN) CRACK FOUND AT UPPER ATTACH FASTENER HOLE DURING NDT REQUIRED BY AD 1997-07R2 WHOSE REQUIREMENTS ARE EVERY 415 FLIGHT HOURS OR 1500 WATER DROPS, WHICHEVER COMES FIRST. THIS AIRCRAFT HAD 1011 WATER DROPS SINCE THE LAST COMPLIANCE OF THIS AD. IT WAS ACCOMPSDR AUS20020715Bolt · cracked(AUS) LT AND RT WING UPPER REAR AND LOWER REAR ATTACHMENT BOLTS EXHIBIT SIGNS OF CRACKING IN RADIUS. FOUND DURING INSPECTION IAW AD/BEECH 300/8 AND RAYTHEON S.I.R.M.SDR AUS20020710Bolt · cracked(AUS) UPPER FORWARD WING ATTACHMENT BOLT SUSPECT CRACKED. FOUND DURINGFLUORESCENT INSPECTION IAW AD/B200/38 A4 AND BEECH S.I.R.M.SDR QXEA0200816Angle · crackedPDX - 2 INCH CRACK IN RADIUS OF FORWARD RT WING TO FUSELAGE CONNECTION ANGLE UNDER PULLEYS BRACKET YW23.85X AND X384.500. REPAIRED IAW RD 8-53-5192.SDR AUS20020278Fitting · cracked(AUS) LH WING ATTACHMENT LUG BROKEN. SUSPECT DAMAGED DURING A PREVIOUSCRASH.SDR DHL2002805043Attach Angle · crackedMAIN CARGO COMPT FUS AFT CENTER SPAR FRAME TO WING ATTACH ANGLE CRACKED 2 INCHES AT STA 759.000, LBL 48.
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