JASC 5741
Service difficulty reports · 544
Reports filed under 5741 · Wing, Fuselage 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 = '5741' 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 = '5741' 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 FDEA201906281480Fitting · crackedDURING PERFORMING ROTOTEST INSPECTION OF FRAME 40 TO CENTER WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION, LT MID HOLE FOUND CRACK SIGNAL COMPLIED WITH EA: 6-5710-T0347503 PT1, EA TITLE: WINGS - BASIC WING STRUCTURE - CRACK IN THE MIDDLE HOLE AT FR40 LHSDR SIMA20190507007Attach Fitting · crackedRT LOWER WING TO FUSELAGE ATTACHMENT ANGLE NR 2 IS CRACKED ON THE AFT EDGE APPROX. 4" LONG. C/A-REMOVED AND REPLACED LOWER WING TO FUSELAGE ATTACHMENT ANGLE NR 2 IAW ETN-EM-53-142 AND SRM 51-40-02.SDR SIMA20190507006Attach Angle · crackedLT LOWER WING TO FUSELAGE ATTACHMENT ANGLE NR 3 IS CRACKED ON THE FWD EDGE APPROX. 3/4" LONG. C/A-RAR ATTACHMENT ANGLE NR 3 IAW ETN-EM-53-142.SDR CA190425034Fitting · cracked(CAN) DURING A SCHEDULED WING STRUT EDDY CURRENT INSPECTION (5-15-MA) REQUIRED EVERY 5000HRS, ONE OF THE LEFT STRUT LOWER FITTINGS WAS FOUND CRACKED AND SEPARATED AT TIME OF STRUT REMOVAL PREPARING FOR THE INSPECTION. THE LAST COMPLIANCE OF THIS INSPECTION WASSDR A6WA2016101644520Bracket · crackedRIGHT WING PICCOLO TUBE SUPPORT BRACKET CRACKED AT WS 149.58SDR ASOA2016050514752Link · crackedCRACK FOUND AT LT LOWER SPA LINK BEARING DURING SPAN LINK INSP REF W/O 630639. REPAIRED BY REPLACING WING/FUSELAGE PICK-UP LINKS IAW SB601BA-57-016.SDR CA160121020Washer · wrong part(CAN) SUSPECT UNAPPROVED PART. FLAT WASHER P/N 35-105111-3 LOT#M3286BX QTY 1 AND LOT#212191 QTY 3 RECEIVED BY TRANSPORT CANADA, AIRCRAFT SERVICES STORES. ALL 4 WASHERS FOUND NOT TO BE OF PROPER THICKNESS AS PER BEECHCRAFT EMAIL CORRESPONDENCE. WASHERS WERE SUPSDR WVER0406201500009Fitting · gougedDURING THE INSPECTION OF THE RT WING TO FUSELAGE LINK AT BS 797, FOUND THE LT WING TO FUSELAGE LINK TO BE TOUCHING THE FUSELAGE FITTING AND WING FITTING.SDR SIMA20150315010Attach Angle · crackedLEFT WING TO FUSELAGE LOWER ATTACH ANGLE IS CRACKED AT FRAME 48. CRACK APPROX 1 INCH LONG. REPAIRED DAMAGED ANGLE IAW ETN-EM-53-142.SDR SIMA20150315011Attach Angle · crackedLEFT WING TO FUSELAGE LOWER ATTACH ANGLE IS CRACKED AT FRAME 47. CRACK APPROX 1 INCH LONG. REPAIRED DAMAGED ANGLE IAW ETN-EM-53-142.SDR SIMA20150315006Attach Angle · crackedRIGHT WING TO FUSELAGE LOWER ATTACH ANGLE IS CRACKED AT FRAME 46. CRACK APPROX 1 INCH LONG. R & R ATTACH ANGLE IAW SRM 51-40-02 & ETN EM-53-142.SDR SIMA20150315004Attach Angle · crackedLEFT WING TO FUSELAGE LOWER ATTACH ANGLE IS CRACKED AT FRAME 46. CRACK IS APPROX 1 INCH LONG. REPAIRED DAMAGED ANGLE IAW ETN-EM-53-142.SDR FDEA201407091670Fitting · crackedDURING PERFORM EA 6-5710-106445 PT 2, TITLE WINGS GENERAL CTR WING BOX AD 2005-23-08 - CRACKS DURING ACCOMPLISHMENT OF SB A300-57-6050, CTR WING BOX REAR SPAR FRAME 47 HOLE 186 RT WITH CRACK SIGNAL. REAMED THE CENTER WING BOX REAR SPAR FR47 HOLE 186RH TO REMOSDR CA131113006Fitting · cracked(CAN) DURING A SCHEDULED EDDY CURRENT INSPECTION OF THE LOWER WING STRUT LUGS IAW INSPECTION 57-60-01. THE LT AFT LUG ON THE LOWER WING STRUT WAS FOUND CRACKED.SDR CA130528002Bolt · sheared(CAN) RIGHT SIDE AFT INBD WING/FUSELAGE STRUT ATTACHMENT JOINT BOLT FOUND SHEARED. THIS WAS DISCOVERED WHILE THE AME WAS PERFORMING AN INTERNAL GENERAL VISUAL INSPECTION OF THE RT ROOT FAIRING DURING A SCHEDULED C-CHECK. REF: MAINTENANCE ZONAL TASK NR 264. HESDR SWAA2013011711508Attach Fitting · crackedCRACKED CLIP ATTACH TO LEFT WING ROOT TO FUSELAGE STA 636. REPAIRED STRAPS IAW SRM AND DWG.SDR SWAA2012121710701Support · crackedLEFT WING TO FUSELAGE ANGLE SUPPORT CRACKED. REMOVED ANGLE SUPPORT ARM IAW B717 SRM 51-41-02 LEFT WING. FABRICATED NEW PART FROM 6061-0-.063" PO 2208633 DIM 4.5" APPROX IAW B717 DRW PL5919110 AND INSTALLED NEW PART IAW B717 SRM 51-41-05.SDR SWAA2012121710700Support · crackedRIGHT WING TO FUSELAGE ANGLE SUPPORT ARM CRACKED. REMOVED ANGLE SUPPORT ARM IAW B717 SRM 51-41-02 AT RIGHT WING FABRICATED NEW PARTS FROM 6061-0-.063" PO 2208633 DIM 9" APPROX IAW B717 DRW PL5919110 AND INSTALLED NEW PART IAW B717 SRM 51-41-05.SDR UIEA2012110600516Beam · crackedCRACK ON THE UPPER SECTION OF LT WING NOSE BEAM NEAR WS 1093. REPAIR IAW EI NR T2012A57B-2495, REV 00.SDR CA120626016Fitting · cracked(CAN) WHEN COMPLETING A PHASE 5 INSPECTION WING AREA, IT WAS NOTICED THAT THE AFT PORTION OF THE UPPER STRUT FITTING WAS CRACKED. THE FITTING EAR WAS CRACKED WITH ONLY ABOUT A .2500 INCH OF MATERIAL LEFT. THE CRACKED STRUT HAS AN INTERVAL OF 10,000 HRS FOR EDSDR ABXR2012033100032Fitting · corrodedLEFT KICK FITTING CORRODED. R & R KICK FITTING IAW REA 46938REA21.SDR 2012FA0000147Attach Fitting · crackedLEFT WING FORWARD ATTACH FITTING CRACKED AND SEPARATED FROM FUSELAGE. RT WING FORWARD ATTACH FITTING FOUND CRACKED AT BEND RADIUS OF GUSSETS THAT SANDWICH THE ATTACH FITTING.SDR 2012FA0000146Attach Fitting · crackedLEFT WING FORWARD ATTACH FITTING OF FUSELAGE CRACKED. CRACK LOCATED AT THE TOP OF BEND AREA OF THE FRONT AND REAR GUSSETS THAT SANDWICH THE ATTACH PLATE. CRACK IS THROUGH ALL 3 LAYERS OF METAL (FRONT GUSSET, ATTACH PLATE, REAR GUSSET) AND EXTENDS .3750" VERSDR CA120223004Attach Fitting · cracked(CAN) DURING A BLOCK INSPECTION IT WAS NOTICED VISUALY THAT THE FRONT SPAR REAR WING ATTACH FITTING WAS CRACKED. ONCE THE FITTING WAS REMOVED, ADDITIONAL DEFECTS WERE NOTICED ON THE UNDER SIDE. THE ADDITIONAL DEFECT COULD ONLY BE DETECTED BY EDDY CURRENT.SDR ABXA20111205156Fitting · corrodedCORROSION ON RT WING, UPPER SURFACE AT WING TO BODY SPLICE FITTING, BS 950 APPROX., UNDER BRACKET. BLENDED CORRODED AREA IAW B767 SRM 57-20-01 FIG 101, AWG.SDR A6WA201240087Structure · chafedRT WING ROOT LOWER AFT SIDE CHAFING. BLENDED CHAFED AREA IAW REO 601R-57-21-880.SDR CA110812004Attach Fitting · crackedDURING REMOVAL OF THE CRACKED AFT WING TO FUSELAGE ATTACH FITTING THE FORWARD HALF OF THE ASSY WAS DAMAGED. ON REMOVAL, IT WAS DISCOVERED THAT THE FITTING WAS CRACKED. THE FLAW COULD NOT BE SEEN WITHOUT REMOVING THE SEALANT.SDR 2011FA0000359Attach Fitting · damagedWING MOVEMENT FOUND IN 3 ACFT DURING INSPECTION. MEASUREMENT OF THE AFT ATTACH LUG FOUND SIGNIFICANT ELONGATION OF THE AFT WING ATTACH LUG ON THE SPACE FRAME AT THE 0 AND 180 DEGREE POSITIONS. IN THE FIRST INSTANCE IT WAS DETERMINED THAT IMPROPER REAMING ANDSDR REXA201100303Fitting · chafedRT FWD OUTBOARD WING TO FUSELAGE FITTING IS CHAFED AT FWD CORNER .565" L X 0.170" W X 0.11D. REPAIRED IAW BOMBARDIER REO 601R-57-21-1433.SDR CA110209023Bolt · brokenWHILE INSPECTING FOR POSSIBLE HYD LEAK AT THE RT WING ROOT, MX DISCOVERED THAT 1 OF THE WING BOLTS FOR THE REAR SPAR STEEL SUPPORT STRUTS HAD FAILED. THE BOLT HEAD HAD SEPARATED FROM THE SHANK OF THE BOLT AND WAS DANGLING FROM THE SAFETY WIRE. UPON REMOVAL, ISDR CA091113008Fitting · cracked(CAN) CRACK INDICATION WAS FOUND DURING MPI INSP AT RT WING STA (RWS) 90 (LWR WING ATTACH FITTING CLUSTER). CRACK WAS WELD REPAIRED AND RE INSPECTED BY MPI AND NO FAULTS WERE FOUND.SDR RU3A0918Bolt · crackedLOWER AFT WING ATTACH BOLT CRACKED AT DRIVE END. WING ATTACH BOLTS REMOVED FOR NDT AS PART OF ROUTINE INSPECTION OF WING ATTACH FITTINGS AND ATTACH BOLTS. LOWER AFT ATTACH BOLT WAS FOUND TO BE CRACKED AT THE HEAD END (SOCKET HEAD BOLT). BOLTS WERE REPLACED SDR LR7A07171Rib · crackedDURING SCHEDULED C-3 CHECK, PER SB382-57-85-R2 FOUND CENTER WING LOWER RIB CRACKED AT CWS61L STGR 23-24. REPAIR ACCOMPLISHED IAW LAC MEA 382-57-07-077.SDR CA070913005Fitting · corroded(CAN) ON A SCHEDULED 100 HOUR INSPECTION, BOTH THE LT AND RT LOWER COCKPIT FITTINGS THAT THE REAR WING SPARS ATTACH TO WERE FOUND TO BE HEAVILY CORRODED. THE PARTS WERE REMOVED, THE AREA DECORRODED AS REQUIRED AND NEW FITTINGS INSTALLED. LT P/N 62448-02 AND RTSDR QXEA200700962Barrel Nut · crackedC4 PDX - RIGHT WING TO FUSELAGE FORWARD MOUNT VERTICAL TIE BOLTS HAVE CRACKED BARREL NUTS. REPAIRED IAW RD8/4-51-102.SDR CA070608003Attach Fitting · worn(CAN) DURING 2400 HR INSPECTION, IT WAS DISCOVERED THAT A NR OF THE WING TO FUSELAGE LINKS HAD WORN PAINT OFF THE ATTACH FITTINGS. ALL AFFECTED FITTINGS AND LINKS INSPECTED. NO DAMAGE FOUND. MFG ADVISED OF FINDINGS. MFG FOLLOWED UP WITH A LETTER OF APPROVASDR 06FDEA1975Pin · corrodedFOUND LEFT WING FORWARD TERMINAL PIN IS CORRODED. REPLACED TERMINAL PIN ON FED EX CARD 75C011-00.SDR 2006FA0000465Bolt · crackedMAG PART INSP FOUND FWD WING ATTACH POINTS BOLT P/N 130909B103 AND 131790-3 CRACKED. BOLTS INSTALLED NEW IN FWD WING BOLT FITTINGS ON BEECH MODEL 36 SER A/C S/N EA-455 ON 1/25/2002. THE LT UPPER BOLT (P/N 130909B103) REMOVED FOR FIRST 5 YEAR NDT INSPECTION ANSDR 2006FA0000464Bolt · crackedMAG PART INSP FOUND FWD WING ATTACH POINTS BOLT P/N 130909B103 AND 131790-3 WITH CRACKS. THE BOLTS WERE INSTALLED NEW IN FWD WING BOLT FITTINGS ON BEECH MODEL 36 SERIES AIRCRAFT S/N EA-455 ON 1/25/2002. THE LH UPPER BOLT (P/N 130909B103) WAS REMOVED FOR IT'S SDR SIMA200529312Control Unit · inoperativeDURING GEAR EXTENTION OBSERVED MOMENTARY EICAS MESSAGE MAIN PITCH TRIM FAIL AND BACKUP PITCH TRIM FAIL. WARNING WENT OUT AFTER GEAR EXTENDED. TROUBLESHOT SYSTEM REPLACED HORIZONTAL STABILIZER UNIT. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (K)SDR 2005FA0000967Attach Fitting · corrodedIAW MM TO COMPLY WITH THE 24 MONTH NDT REQUIREMENTS UNDER THE ULTRASONIC PART OF THE INSPECTION CORROSION WAS FOUND ON BOTH THE LT AND RT WING ATTACHMENT FITTINGS AT FS 452, BL33, LT AND RT. TECH OPS REQUIRES COMPLIANCE WITH ASC FOR A 3 PIECE FITTING PLATE. SDR UPS05443695Fitting · crackedINSPECTION TYPE:C RT WING BS 1241 UPPER REAR SPAR SIDE-TO-BODY KICK FITTING AREA FOUND CRACK AT TERMINAL FITTING NR 2 HOLE. HOLE REPAIRED AS PER SB 747-57A2314.SDR CA041217004Link · unserviceable(CAN) DURING INSPECTIONS CARRIED OUT ON THE ABOVE NOTED ACRFT FOR THE LEASE RETURN, ENGINEERS FOUND WING TO FUSELAGE CONNECTING LINKS AT REAR SPAR FITTING S, FRAME 29 CORRODED IN THE BORE ON BOTH ENDS OF THE LINKS. BOLTS ASSOCIATED WITH THE LINKS WERE ALSO COSDR 0402139759Angle · crackedDURING H-CHECK FOUND CRACKED RT WING TO FUSELAGE ATTACH ANGLE AT BS 644. REPAIRED PER EA 97-201426.SDR C2XA04SH510Torque Box · crackedDURING C-CHECK EDDY CURRENT INSPECTION OF THE RIGHT WING INBOARD TORQUE BOX INDICATED A CRACK AT THE FORWARD TWO HI-LOK POSITION. REAMED THE AFFECTED HI-LOK HOLES TO THE NEXT OVERSIZE IAW EMB SRM 51-40-04. AIRCRAFT RETURNED TO SERVICE.SDR SWIA200413485Structure · crackedLEFT ZONE 193 LOWER FLANGE WING TO FUSELAGE IS CRACKED IN THREE LOCATIONS. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED ANGLE IAW EMB 120 SRM 53-20-13 PG 205-206 FIG 202.SDR C2XA03TY204Tie Rod · corrodedDURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE RIGHT HAND WING TO FUSELAGE TIE ROD ASSEMBLY. MAINTENANCE REMOVED AND REPLACED THE TIE ROD IAW EMB IC 2003-145/4092. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.SDR C2XA03TY203Tie Rod · corrodedDURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE LEFT HAND WING TO FUSELAGE TIE ROD ASSEMBLE. MAINTENANCE REMOVED AND REPLACED THE TIE ROD IAW EMB IC 2003-145/4092. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.SDR AUS20031089Bolt · damaged(AUS) LT WING UPPER FORWARD ATTACHMENT BOLT THREADS DAMAGED.SDR AUS20030893Bolt · cracked(AUS) LT AFT UPPER WING ATTACHMENT BOLT CRACKED IN THREADED AREA.
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