JASC 5740

Service difficulty reports · 3,003

Reports filed under 5740 · 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 = '5740'
  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.

SDR IXXA0100059SHinge Fitting · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON THE RIGHT WING AILERON MECHANISM AREA LOWER SUPPORT HINGE FITTING "L" ANGLE. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED ANGLE, FABRICATION AND INSTALLATION OF NEW REPAIR ANGLE IN ACCORDANCE WITH DOUGLAS SMay 11, 2001 · N822BX · Doug DC871FSDR MQGR20013601Attach Fitting · corrodedDURING RECOMMENDED INSPECTION OF WINGLET ATTACH HARDWARE FOR CORROSION, FOUND CORROSION IN THE WINGLET TO WING ATTACHMENT FITTING. IT APPEARS THIS CORROSION IS THE RESULT OF IMPROPER SEALING OF THE ATTACHMENT HARDWARE SINCE WATER WAS FOUND TRAPPED IN THE ONLYApr 12, 2001 · N74A · Gulstm G1159BSDR RRXA10937Attach Angle · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT WING CENTER L/E VERT. ATTACH ANGLE AT LOWER END AT STA XS 520, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. FABRICATED PART AND INSTALLED IAAW DC-8 SRM 51-1-20D AND DWG 9753297.Apr 8, 2001 · N602AL · Doug DC873FSDR AU010313Fitting · corroded(AUS) LT AND RT UPPER MAIN SPAR ATTACHMENT FITTINGS CORRODED ANDPARTIALLY EXFOLIATED.Mar 30, 2001 · Piper PA31350SDR AU010312Fitting · corroded(AUS) LT AND RT UPPER MAIN SPAR ATTACHMENT FITTINGS CORRODED ANDPARTIALLY EXFOLIATED. WHEN THE FITTINGS WERE REMOVED THE ATTACHMENT RIVETS WERE FOUND TO BE SHEARED.Mar 30, 2001 · Piper PA31350SDR WEA010463Fitting · corrodedRIGHT WING FUEL TANK, MODERATE CORROSION ON STRINGER NR 22 FORWARD LOWER LEG, BETWEEN XRS 58 AND 69. BLENDED CORROSION, LOCATED AND DRILLED LOWER FLANGE OF STRINGER, INSTALLED STRINGER.Mar 28, 2001 · N800ME · Doug DC914SDR AU010291Fitting · corroded(AUS) WING SPAR CAP FITTING CONTAINED SEVERE EXFOLIATION CORROSION ON THE FORWARD FACE.Mar 23, 2001 · Cessna 402CSDR UPS01235402Fitting · crackedINSPECTION TYPE:C CHECK LT WING FRONT SPAR INTERIOR & LBBL 70.5 TERMINAL FITTING ATTACH V SHAPE FITTING TO UPPER SHOW CRACK MIGRATING FROM OB BOLT. REMOVED FITTING LT WING FRONT SPAR INTERIOR LBL 70.5 V SHAPE. INSTALLED LT WING UPPER FRONT SPAR CONER NEW FITFeb 26, 2001 · N919UP · Boeing 72730CSDR RRXA010527Fitting · corrodedDURING A MAINTENANCE VISIT FOUND A PITTED CANOE FITTING UNDER ROLLER TRACKS ON THE RT WING AT STA 98, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O. 01-024 WITH APPROVED 811Feb 7, 2001 · N8091U · Doug DC871FSDR RRXA010526Fitting · corrodedDURING A MAINTENANCE VISIT FOUND A PITTED CANOE FITTING UNDER FLAP ROLLER TRACKS ON THE RT WING AT STA 340, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O.01-024 WITH APPROVEFeb 7, 2001 · N8091U · Doug DC871FSDR RRXA010524Fitting · corrodedDURING A MAINTENANCE VISIT FOUND A PITTED CANOE FITTING UNDER FLAP ROLLER TRACKS LT WING AT STA 410, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O.01-024 WITH APPROVED 8110-Feb 7, 2001 · N8091U · Doug DC871FSDR RRXA010523Fitting · corrodedDURING A MAINTENANCE VISIT FOUND A PITTED CANOE FITTING UNDER FLAP ROLLER TRACKS LT WING AT STA 340, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O.#01-024 WITH APPROVED 8110Feb 7, 2001 · N8091U · Doug DC871FSDR RRXA010522Fitting · corrodedDURING A MAINTENANCE VISIT FOUND A PITTED CANOE FITTING UNDER FLAP ROLLER TRACKS LT WING AT STA 219, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM E.O.#01-024 WITH APPRFeb 7, 2001 · N8091U · Doug DC871FSDR RRXA010530Fitting · gougedDURING A MAINTENANCE VISIT FOUND A GOUGE TO THE AFT END OF THE CANOE FITTING AT STA 219, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Feb 6, 2001 · N8091U · Doug DC871FSDR CALA0100077Fitting · corrodedINSPECTION FOUND LT WING REAR SPAR ATTACH FITTING CORRODED IN O/B LOWER FASTENERS AT WS 200. THE ATTACH FITTING WAS REPAIRED IAW SRM 51-20-05.Jan 27, 2001 · N17316 · Boeing 7373T0SDR SWAA010220Fitting · crackedDURING SCHEDULED 1/2D CHECK, FOUND RT WING AILERON FITTING CRACKED, 2ND FROM INBOARD. REMOVED AND REPLACED FITTING PER SRM.Jan 23, 2001 · Boeing 7372H4SDR SWAA010191Angle · crackedDURING SCHEDULED D-CHECK, FOUND LT WING, RSS 541, INBOARD CENTER AILERON HINGE RIB OUTBOARD UPPER ANGLE CRACKED. REMOVED AND REPLACED ANGLE PER SRM & BAC DWG.Jan 22, 2001 · Boeing 7372H4SDR 20010416CW006Attach Fitting · crackedINSPECTED AIRFRAME, FOUND THREE SEPARATE CRACKS IN THE LEFT WING FORWARD ATTACH FITTING AREA.Jan 8, 2001 · N6873C · Piper PA32RT300SDR 20010205CW004Fitting · corrodedAFT SPAR REAR TOP WING ATTACH FITTING CORRODED. INSTALLED NEW FITTING.Jan 5, 2001 · N401TJ · Cessna 402CSDR MWEA001289Former · crackedRIGHT WING INBOARD LEADING EDGE HAS A CRACKED FORMER. -- FABRICATED REPAIR DOUBLERS AND INSTALLED.Dec 22, 2000 · N800ME · Doug DC914SDR MWEA001285Former · crackedLEFT WING LEADING EDGE HAS A CRACKED FORMER. -- FABRICATED AND INSTALLED REPAIR DOUBLERS.Dec 22, 2000 · N800ME · Doug DC914SDR MWEA001284Former · crackedLEFT WING INBOARD LEADING EDGE HAS TWO FORMERS WITH PREVIOUS REPAIRS CRACKED. -- FABRICATED AND INSTALLED REPAIR DOUBLERS.Dec 22, 2000 · N800ME · Doug DC914SDR RRXA003611Fitting · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE BATHRUB FITTING BETWEEN STA 1690 & 1700 AND L34L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM Dec 20, 2000 · N795FT · Doug DC873FSDR SPAA0000029Carriage · corrodedDURING ACCOMPLISHMENT OF CPCP TASK C57-306-04 1OF2 CORROSION WAS FOUND ON THE LEFT WING OUTBOARD MIDFLAP, OUTBOARD CARRAIGE SPINDLE. REMOVED AND REPLACED OUTBOARD FLAP CARRAIGE IAW BOEING MM 27-51-81. RIGGED FLAP SYSTEM PER BOEING MM 27-51-12 A/TDec 15, 2000 · N703S · Boeing 7372T4SDR AU001324Fitting · cracked(AUS) LT WING REAR SPAR INBOARD ATTACHMENT BRACKET CRACKED. CRACKSAPPEAR TO INITIATE FROM THE ACCESS PANEL ON THE LOWER WING SKIN PANELS ARE NON STANDARD ACCESS PANELS.Dec 13, 2000 · Avions R2160SDR AU001323Fitting · cracked(AUS) RT WING REAR SPAR INBOARD ATTACHMENT BRACKET CRACKED. CRACKSAPPEAR TO INITIATE FROM THE ACCESS PANEL ON THE LOWER WING SKIN PANELS ARE NONSTANDARD ACCESS PANELS.Dec 13, 2000 · Avions R2160SDR QXEA0003290Fitting · crackedPDX- SUSPECT CRACK AT TOP DEAD CENTER INBOARD FACE OF LOWER RIGHT HAND OUTBOARD LUG. REPAIRED IAW HORIZON AIR EA 4-57-514.Dec 11, 2000 · N492US · Fokker F28MK4000SDR RRXA003803Gusset · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO GUSSETT AT STA 980 AND INSIDE RT MAIN GEAR WHEEL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-4.Dec 6, 2000 · N795FT · Doug DC873FSDR QXEA0003160Attach Angle · corrodedYXX-REAR SPAR WING CENTER SECTION TOP FAIRING ATTACH ANGLE HAS FRETTING CORROSION UNDER TURTLE BACK PANELS 262 DT, AND 262 PT. REPAIRED IAW DHC-8 SRM 51-00-06 AND RD8-57-1434.Nov 28, 2000 · N367PH · Dhav DHC8202SDR QXEA0003159Attach Angle · corrodedYXX-FRONT SPAR, WING CENTER SECTION, TOP FAIRING ATTACH ANGLE HAS FRETTING DAMAGE UNDER PANELS 261 DT, GT, JT, AND NT. REPAIRED IAW DHC-8 SRM 51-00-06 AND SRM 51-20-00, PAGE 28.Nov 28, 2000 · N367PH · Dhav DHC8202SDR QXEA0003161Bracket · crackedYXX-LEFT HAND LOWER LEADING EDGE (511AL) ATTACH BRACKET AT STATION YW138.00 IS CRACKED. REPAIRED IAW DHC-8 SRM 51-40-11, PAGE 1-4.Nov 24, 2000 · N367PH · Dhav DHC8202SDR AWXA0000898Fitting · gougedLEFT WING NR 3 FLAP TRACK FAIRING FITTING A-FRAME FOUND TO HAVE 2 GOUGE AREAS. BLENDED GOUGE ON A-FRAME TOP SURFACES OF ATTACH ARMS IAW B737-300 SRM PROCEDURES; NDT HFEC OR FLUORESCENT DYE-PENETRANT INSP PER B737 NDT MANUAL PT.6,51-00-00 TO ENSURE NO CRACKINGNov 17, 2000 · N329AW · Boeing 7373Y0SDR 20001109SH041Fitting · crackedFOUND LEFT FORWARD AND AFT WING FITTINGS CRACKED. THIS AIRCRAFT HAS HIGH AFTT AND THE CRACKS WERE DISCOVERED WHILE PERFORMING AEROSTAR SB 600-136. (X)Oct 31, 2000 · N90609 · Piper PA60600SDR 20001109SH040Fitting · crackedFOUND LEFT FORWARD AND AFT WING FITTINGS CRACKED. THIS AIRCRAFT HAS HIGH AFTT AND THE CRACKS WERE DISCOVERED WHILE PERFORMING AEROSTAR SB 600-136. (X)Oct 31, 2000 · N90609 · Piper PA60600SDR CA001030006Fitting · cracked(CAN) CRACK IS FROM THE FORWARD I/B SPAR CAP TO FITTING RIVET AND GOES TO THE EDGE OF THE FITTING. THE CRACK WAS DISCOVERED DURING A SCHEDULED WING INSPECTION. CRACK WAS VERIFIED USING LEVEL 2 PENETRANT.Oct 16, 2000 · Beech A100SDR DL733002036Fitting · crackedTHE MLG BEAM OUTBOARD AFT ATTACH FITTING WAS FOUND WITH A TYPICAL CRACK EMANATING FROM AN ATTACHMENT HOLE COMMON TO THE REAR SPAR UPPER CHORD. BOLT HOLE HFEC INSPECTION REVEALED A CRACK IN THE SPAR WEB AT THE FASTENER LOCATION. THE HOLE WAS OVERSIZED TO REMOOct 16, 2000 · N951WP · Boeing 7373B7SDR SWAA002036Fitting · corrodedDURING SCHEDULED D-CHECK, FOUND LT MLG STAB LINK FITTING CORRODED. REMOVED AND REPLACED FITTING PER MM.Oct 15, 2000 · N657SW · Boeing 7373L9SDR SWAA001969Fitting · corrodedDURING SCHEDULED SERVICE CHECK, FOUND LT AND RT MLG WALKING BEAM HANGAR SUPPORT FITTINGS CORRODED. REMOVED AND REPLACED LT AND RT FITTINGS PER SRM.Oct 8, 2000 · N674AA · Boeing 7373A4SDR TWAA0015207Fitting · crackedDURING CHECK-C MAINT, LT WING GROUND SPOILER AFT ACTUATOR ATTACH FITTING HAD A 1.5 INCH LONG CRACK ON I/B SIDE OF FITTING. CRACK CONTAINED STOP DRILLED CRACK PER MD80 80-57-180. INSTALLED DOUBLER FILLER AND STIFFENER PER 80-57-180.Sep 22, 2000 · N954U · Doug DC982SDR RRXA003759Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AND A CRACK TO THE ATTACH ANGLE REAR SPAR UPPER CENTER WING IN CABIN Z-21 AT STA 857 +25 TO -45, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA ISep 12, 2000 · N500MH · Doug DC871FSDR ABXA000453Attach Fitting · crackedLEFT WING UPPER INBOARD TRAILING EDGE SEGMENT LOWER CENTER ATTACH FITTING CRACKED. REPLACED ATTACH FITTING IAW DC9 SRM 51-30-1.Sep 8, 2000 · N931AX · Doug DC933FSDR AU000797Fitting · out of adj(AUS) AIRCRAFT MAIN PLANE ATTACHMENT FITTING CONCENTRIC BUSHES OUT OF ADJUSTMENT CAUSING AIRCRAFT TO ROLL TO THE LEFT. LEFT WING WAS UNABLE TO BE ADJUSTED AS THE BUSH WAS FOUND TO BE IN THE MAXIMUM POSITION. THE ADJUSTMENT HAD TO BE CARRIED OUT ON THE RIGHT WSep 4, 2000 · Cessna 150FSDR CA000927012Washer · failed(CAN) WHILE REASSEMBLING THE WING FOLLOWING INSPECTION IN ACCORDANCE WITH CF-81-25R5, A NEW PRELOAD INDICATING WASHER ASSY INSTALLED ON THE LT LOWER FORWARD WING BOLT INDICATED THE BOLT WAS TORQUED AT AN ABNORMALLY LOW TORQUE. THE BOLT WAS UNDONE AND THE WASHESep 3, 2000 · Beech A100SDR AU000665Fitting · scored(AUS) LEFT UPPER FORWARD WING ATTACHMENT FITTING SCORED IN THE BORE OFTHE BARREL NUT RECESS IN THE BATHTUB FITTING. CAUSED BY THE BARREL NUT INSERT BEING INSERTED 90 DEGREES OUT FROM ITS CORRECT POSITION. SUBMITTER SUSPECTED OCCURRED DURING THE PREVIOUS INSPSep 1, 2000 · Beech 200BEECHSDR 20000913SH012Bracket · crackedAIRCRAFT WAS INSPECTED IAW SPECIAL AIRWORTHINESS INFO BULLETIN NR CE-00-27 DATED JULY 11, 2000. VISUAL INSPECTION REVEALED CRACKS IN UPPER AND LOWER CUT-OUT SLAT. (X)Aug 28, 2000 · N2297L · Wsk M18ASDR 20000913SH011Fitting · crackedAIRCRAFT WAS INSPECTED IAW SPECIAL AIRWORTHINESS INFO BULLETIN NR CE-00-27, DATED ULY 11, 2000. MAG PARTICAL INSPECTION REVEALED CRACK IN RIGHT BOTTOM FITTING, BACK SIDE. (X)Aug 28, 2000 · N2297L · Wsk M18ASDR DL767001612Fitting · tool damageNR 8 RIB ENGINE SUPPORT FITTING DAMAGED AT THE EDGE OF HOLE LOCATION COMMON TO THE FITTING AND FRONT SPAR. THE HOLE IS THE FOURTH ONE UP FROM THE BOTTOM OF THE FITTING IN THE O/B ROW. ER/A 334807-14AD.Aug 14, 2000 · N112DL · Boeing 767232SDR 20000809SH029Fitting · corrodedEXTENSIVE INTERGRANULAR CORROSION FOUND ON THE BOTTOM OF THE UPPER AFT WING ATTACH FITTING ON THE LEFT WING. THE SAME FITTING ON THE RIGHT WING STUB WAS CORRODED TO A LESSER DEGREE. MOISTURE ENTRAPMENT IS BELIEVED TO CONTRIBUTE. (X)Aug 1, 2000 · N414FC · Cessna 414ASDR RRXA002980Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE ON THE SIDE BRACE MOUNT BOSS ON THE LT WING LWR REAR SPAR FLAP FITTING AT STA 219, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED, PRIMED AND PAINTED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAJul 31, 2000 · N603AL · Doug DC873FSDR RRXA002979Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORRISION DAMAGE ON THE SIDE BRACE MOUNTING BOSS ON THE RT WING LWR REAR SPAR FLAP FITTING AT STA 219, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR ANDJul 31, 2000 · N603AL · Doug DC873F
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