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.

SDR AUS20021409Fitting · cracked(AUS) LT WING ATTACHMENT FITTING CRACKED.Dec 2, 2002 · Piper PA36285SDR CA030417007Bushing · loose(CAN) MIGRATING BUSHINGS ON WING ATTACHMENT FITTINGS.Nov 22, 2002 · Cndair CL6002B19SDR CA030417003Bushing · loose(CAN) MIGRATING BUSHINGS ON WING ATTACHMENT FITTINGS.Oct 25, 2002 · Cndair CL6002B19SDR GAIA02147STBushing · deterioratedDURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE LEFT AFT BOTTLE PIN BUSHINGS WERE DETERIORATED. THE BUSHINGS WERE REPLACED IAW THE BOEING 727 MM 57-41-11 AND 57-41-1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Oct 24, 2002 · N936PG · Boeing 727225SDR AUS20021227Fitting · corroded(AUS) LH WING REAR UPPER ATTACHMENT BATHTUB FITTING CORRODED. PERSONNEL/MAINTENANCE ERROR.Oct 23, 2002 · Beech 58SDR AUS20021226Fitting · corroded(AUS) RH WING TOP FORWARD ATTACHMENT BATHTUB FITTING CORRODED.PERSONNEL/MAINTENANCE ERROR.Oct 23, 2002 · Beech 58SDR AUS20021225Fitting · corroded(AUS) RH WING REAR TOP ATTACHMENT BATHTUB FITTING CORRODED. PERSONNEL/MAINTENANCE ERROR.Oct 23, 2002 · Beech 58SDR AUS20021224Fitting · damaged(AUS) LH WING FORWARD TOP ATTACHMENT BATHTUB FITTING CORRODED AND DAMAGED. PERSONNEL/MAINTENANCE ERROR.Oct 23, 2002 · Beech 58SDR AUS20021223Fitting · damaged(AUS) RH WING FORWARD LOWER ATTACHMENT BATHTUB FITTING CORRODED AND DAMAGED. PERSONNEL/MAINTENANCE ERROR.Oct 23, 2002 · Beech 58SDR AUS20021222Fitting · damaged(AUS) LH WING FORWARD LOWER ATTACHMENT BATHTUB FITTING CORRODED AND DAMAGED. PERSONNEL/MAINTENANCE ERROR.Oct 23, 2002 · Beech 58SDR UPS02239896Pin · corrodedINSPECTION TYPE: C & SI, RT WING REAR SPAR TO BODY FITTING TERMINAL BOTTLE PIN AT BS 870 HAS EVIDENCE OF PITTING CORROSION. CORROSION OUT OF LIMITS, BOTTLE PIN REPLACED IAW MM 57-41-01.Oct 22, 2002 · N932UP · Boeing 72725CSDR CA021002006Bolt · cracked(CAN) WING BOLTS INSPECTED AS PER BEECH S.I.R.M. 57-16 INDEX 10. INDEX 1-11 DONE IN CONJUNCTION WITH CF-1981-25R6. CRACK FOUND IN LT UPPER AFT WING BOLT. CRACK FOUND WHERE SHAFT CONNECTS TO BOLT HEAD. WING BOLT REPLACED WITH NEW. CRACK FOUND 1 YEAR/324 HOURS ASep 24, 2002 · Beech B100SDR 2002FA0000899Nut · crackedFOUND RIGHT LOWER WING STRUT ATTACH HARDWARE LIGHTLY CORRODED. FURTHER INSPECTION FOUND THAT NUT WAS COMPLETELY CRACKED THROUGH. NEW NUT AND BOLT INSTALLED. PART MAY HAVE BEEN OVERTORQUED UPON INSTALLATION.Jul 23, 2002 · N208TW · Cessna 208BSDR CA020714001Attach Angle · 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 837 WATER DROPS SINCE THE LAST COMPLIANCE OF THIS AD.Jul 12, 2002 · Cndair CL2151A10SDR CA030417006Bushing · loose(CAN) MIGRATING BUSHINGS ON WING ATTACHMENT FITTINGS.Jun 25, 2002 · Cndair CL6002B19SDR 2002F00593Fitting · corrodedAT C-CHECK, FOUND LEFT WING REAR SPAR TO BODY 'BOTTLE PIN' INNER MATING SURFACE CORRODED. (M)Apr 24, 2002 · N8878Z · Boeing 727225SDR 02FDEA00259Pin · corrodedCORROSION AT FLANGE BASE OF TERMINAL PIN. REMOVED AND REPLACED PIN PER 75C011-00.Apr 13, 2002 · N463FE · Boeing 727225SDR 02FDEA00258Pin · corrodedCORROSION AT FLANGE BASE OF TERMINAL PIN. REMOVED AND REPLACED PIN PER 75C012-00.Apr 13, 2002 · N463FE · Boeing 727225SDR 02FDEA00247Pin · corrodedRT WING REAR TERMINAL PIN AT BS 870 HAS RUST AROUND BASE OF PIN. REMOVED AND REPLACED PIN.Apr 12, 2002 · N207FE · Boeing 7272S2FSDR AUS20020269Nut · wrong part(AUS) UPPER LT WING FORWARD ATTACHMENT NUT INCORRECT PART. UNAPPROVED PART.Mar 20, 2002 · Beech 58SDR AUS20020345Fitting · faulty(AUS) LH WING ATTACHMENT FITTING CONTAINED A SUBSURFACE DEFECT IN THE AREA ADJACENT TO BUT NOT INTO THE MAIN WING ATTACHMENT BOLT HOLE. FOUND DURING EDDY CURRENT INSPECTION.Mar 3, 2002 · Cessna 210MSDR CA030417005Bushing · loose(CAN) MIGRATING BUSHINGS ON WING ATTACHMENT FITTINGS.Feb 8, 2002 · Cndair CL6002B19SDR AUS20011225Fitting · corroded(AUS) RH WING UPPER FORWARD ATTACHMENT FITTING CONTAINED INTERGRANNULAR CORROSION IN THE UPPER SURFACES AND TWO AREAS OF PITTINGCORROSION. FOUND DURING INSPECTION IAW AD/C310/53.Nov 20, 2001 · Cessna 310RSDR CA030417008Bushing · loose(CAN) MIGRATING BUSHINGS ON WING ATTACHMENT FITTINGS.Sep 19, 2001 · Cndair CL6002B19SDR CA010628008Bolt · damaged(CAN) DURING INSPECTION ON SPAR, WHEN BOLT WAS BEING INSTALLED IT WAS FOUND THAT AFTER FINAL TORQUE THE BOLT COULD STILL BETURNED QUITE EASILY. BOLT WAS REMOVED AND MAINTENANCE FOUND THAT THREADS WERE RAGGED AND CAUSING THE NUT TO BIND ON THE BOLT. THIS IS THEJun 28, 2001 · Beech B99SDR AUS20010670Bolt · loose(AUS) LT WING REAR SPAR ATTACHMENT BOLTS LOOSE WITH NUT HOLDING BY ONLY THREE THREADS. SUSPECT NUTS NOT TIGHTENED AT LAST MAINTENANCE INSPECTION FOLLOWING WORK CARRIED OUT IN THE AREA.PERSONNEL/MAINTENANCE ERROR.Jun 27, 2001 · Piper PA28161SDR CA010628009Bolt · damaged(CAN) DURING INSPECTION THE THREADS OF THE BOLTS WERE FOUND TO HAVE JOGGED THREADS.Jun 18, 2001 · Beech B99SDR CA010529009Attach Fitting · improper part(CAN) OUTER WING ATTACHMENT HARDWARE CONSISTS OF 224 NUTS AND BOLTS FOR BOTH WINGS. APPROXIMATELY 40% OF THE NUTS USEDWERE OF A TYPE USED IN SHEAR APPLICATIONS (NAS679). CORRECT HARDWARE SHOULD HAVE BEEN AN365-428 AND AN365-524 NUTS AS CALLED FOR IN THE HARVARMar 27, 2001 · Namer HARVARDMK4SDR UPS01235227Pin · corrodedINSPECTION TYPE:C+SI, RIGHT BS 740 BOTTLE PIN CORRODED. BOTTLE PIN REPLACED IAW MM 57-41-01.Feb 15, 2001 · N941UP · Boeing 72722CSDR CA010206003Attach Fitting · worn(CAN) DURING ROUTINE MAINTENANCE TECHNICIAN NOTICED MOVEMENT IN RIGHT WING FRONT SPAR ATTACHMENT. FURTHER INVESTIGATION REVEALED THAT THE LOOSENNESS WAS CAUSED BY WORN BUSHINGS AND BOLT P/N 130909B175. BEECH CRAFT WAS NOTIFIED AND FIELD CREW ARE ON THEIR WAY TJan 8, 2001 · Beech B300SDR CA001212018Nut · cracked(CAN) THREE NUTS USED TO ATTACH THE LOWER END OF THE MAIN WING LONGERON TO THE INTERIOR LONGERON WERE FOUND CRACKED.ACCORDING TO A PIPER REP FOR API, THE SAME TYPE OF INSPECTION SHOWN IN PIPER SB 602 WOULD APPLY TO OUR AIRCRAFT. THE PROBLEM IS HOWEVER THAT OUNov 24, 2000 · Piper PA34200TSDR CA001218020Attach Angle · cracked(CAN) CRACKS FOUND IN 90 DEGREES RADIUS OF UPPER ATTACH ANGLES. LOWER ATTACH ANGLES CRACKS FOUND ON FUSELAGE ATTACH POINT.Oct 15, 2000 · Airtrc AT401SDR AU000929Fitting · corroded(AUS) RIGHT OUTER WING BOTTOM ATTACHMENT FITTING CRACKED AND PITTED. (X)Sep 27, 2000 · Wsk M18ASDR AU000928Fitting · corroded(AUS) LEFT OUTER WING BOTTOM ATTACHMENT FITTING PITTED. (X)Sep 27, 2000 · Wsk M18ASDR AU000847Angle · corroded(AUS) LEFT AND RIGHT WING FORWARD ATTACHMENT FITTING ANGLES CONTAINED INTERGRANNULAR CORROSION. (X)Sep 13, 2000 · Cessna U206BSDR DL767001704Fitting · damagedTHE O/B HOLE IN THE I/B SIDE OF THE LT KICKLOAD FITTING FOUND DAMAGED. THE HOLE WAS SLIGHTLY ELONGATED AND WORN UNDER THE NUT. THE HOLE WAS OVERSIZED AND SPOTFACED TO REMOVE DAMAGE. ER/A 334858-14AD.Sep 1, 2000 · N115DA · Boeing 767232SDR CA000712024Fitting · cracked(CAN) CRACKED AT RADIUS OF WING ROOT ATTACH FLANGE ON FORWARD SIDE OF FITTING. SLOT AREA.Jul 4, 2000 · Beech A100SDR CA000712023Fitting · cracked(CAN) WING FITTING CRACKED AT RADIUS PORTION OF UPPER SURFACE OF WING FITTING. SLOT AREA.Jul 4, 2000 · Beech 99SDR CA000712022Fitting · cracked(CAN) CRACKED AT RADIUS OF WING ROOT ATTACH FLANGE ON FORWARD SIDE OF FITTING.Jul 4, 2000 · Beech 99ASDR CA000712021Fitting · cracked(CAN) CRACK DISCOVERED DURING LPI OF FITTINGS CALLED UP BY AD. CRACK WAS FOUND AT RADIUS OF WING ROOT ATTACH FLANGE ON FORWARD SIDE OF FITTING. BY THE SLOT ON THE SIDE.Jul 4, 2000 · Beech 99ASDR CA000614019Strut · corroded(CAN) DURING INSPECTION AS DIRECTED BY CF-98-37R1, THE STRUTS WERE FOUND BEYOND THE LIMIT SET BY THE AD. BOTH LEFT AND RIGHT STRUTS ARE BEING REPLACED.Jun 6, 2000 · Dhav DHC2MK1SDR ABXA000159Bracket · crackedRIGHT WING BRACKET AT STATION XRS 58.00 CRACKED. REPLACED BRACKET IAW DC9SRM 51-30-05.Mar 22, 2000 · N969AX · Doug DC941SDR ABXA000161Bracket · crackedLEFT WING BRACKET AT STATION 58.00 CRACKED. REPLACED BRACKET IAW DC9 SRM 51-30-5.Feb 22, 2000 · N969AX · Doug DC941SDR CA991103016Bolt · cracked(CAN) NEW WING ATTACHMENT BOLTS NDT'D PRIOR TO INSTALLATION REVEALED THAT 9 OUT OF 24 BOLTS (AN 7-23A) WERE REJECTED. BOLTS ARE MADE OF ROLLED STEEL AND THERE WAS AN INDICATION OF AN INCOMPLETE ROLLING PROCESS. SUBMITTER STATED IT IS UNKNOWN IF THE SEAMS WEROct 20, 1999 · Scwzer SGS233ASDR UPS99230934Pin · corrodedINSPECTION TYPE:SI, CORROSION (C53-100-05.00-03) FOUND ON LEFT WING REAR BOTTLE PIN. REMOVED LT REAR BOTTLE PIN FOR CORROSION. CORROSION WAS OUT OF LIMITS. INSTALLED NEW REAR LT BOTTLE PIN, ALL WORK DONE IAW MM 57-41-1 PG 403-404.Sep 14, 1999 · N951UP · Boeing 72725CSDR 99FDEA00462Bottle Pin · corrodedRT FWD BOTTLE BOLT (SPAR TERMINAL PIN) HAS CORROSION. REMOVED AND REPLACED NEW BOTTLE BOLT PIN SEALED.Sep 10, 1999 · N190FE · Boeing 72722SDR CA990804034Spar · hole oversized(CAN) REQUIRED WASHERS NOT INSTALLED BETWEEN BUSHING AND FUSELAGE FITTING. THIS ALLOWED BUSHING TO MOVE FORWARD. BECAUSE THERE WAS NOT ENOUGH BEARING SURFACE, THIS ALLOWED BUSHING TO ENLARGE HOLE IN SPAR AND FILLER CAUSING CRACKS TO RADIATE FROM HOLE AND ALLJul 20, 1999 · Beech A24RSDR CA990804033Spar · hole oversized(CAN) WASHERS ARE REQUIRED BETWEEN BUSHING AND FUSELAGE ATTACH FITTING TO HOLD BUSHING IN PLACE. THESE WASHERS WERE MISSING AND ALLOWED THE BUSHING TO MOVE FORWARD. THERE WAS NOT ENOUGH BEARING SURFACE AVAILABLE, SO THE BUSHING MOVED ENLARGING THE HOLE IN THJul 15, 1999 · Beech A24RSDR AU990430038Strap · cracked(AU) AD 98-08-19, SB 223 ACCOMPLISHED. FUSELAGE TO WING STRAPS REVEALED CRACKS.Apr 21, 1999 · Gulstm 500SSDR AU990430037Strap · cracked(AU) AD 98-08-19, SB 223 ACCOMPLISHED. FUSELAGE TO WING STRAPS REVEALED CRACKS.Apr 21, 1999 · Gulstm 500S
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