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 98ZZZX51Fitting · crackedINSPECTION FOUND LEFT WING ATTACH FITTING CRACKED.Oct 19, 1997 · N6049L · Beech 76SDR 97FDEA00698Fitting · crackedNR 0835 050 UPON REMOVAL OF UPPER SPLICE FITTING FOR ACCESS FOR NR 0822, CORROSION ON BOTTLE PIN CASTING, FOUND FITTING TO BE CRACKED BS 876, WL 178 RT SIDE P/N 65-18595-1. REMOVED DAMAGED SPLICE FITTING, UPPER RT SIDE AT BS 876, WL 178, RBL 68-72. BACK DRILOct 1, 1997 · N143FE · Boeing 72721CSDR 97ZZZX4510Bolts · corrodedDURING REPLACEMENT OF PAN UNDER WING WALK IN THE GEAR WELL, RIB WAS FOUND CRACKED. THE WING WAS REMOVED AND FOUND SEVERAL WING ATTACHMENT BOLTS CORRODED. BOLTS AND SPECIAL WASHERS NOT IN PROPER LOCATIONS PER PA28 MM. (WING ATTACH). NO SHIMS AT EITHER WING SSep 30, 1997 · N4620J · Piper PA28R180SDR 97ZZZX4509Bolts · wrong placementDURING REPLACEMENT OF PAN UNDER WING WALK IN THE GEAR WELL, RIB WAS FOUND CRACKED. THE WING WAS REMOVED AND FOUND SEVERAL WING ATTACHMENT BOLTS CORRODED. BOLTS AND SPECIAL WASHERS NOT IN PROPER LOCATIONS PER PA28 MM. (WING ATTACH). NO SHIMS AT EITHER WING SSep 30, 1997 · N4620J · Piper PA28R180SDR 97FDEA00695Terminal Pin · corrodedRT WING REAR TERMINAL PIN CORRODED. REPLACED RT WIG REAR TERMINAL PIN PER M/M 57-41-1.Sep 29, 1997 · N496FE · Boeing 727227SDR CKSA97533Pin · corrodedDURING CPCP CHECK INSPECTION, FOUND CORROSION AROUND FLANGE ON LT AFT BOTTLE PIN. REMOVED AND REPLACED BOTTLE PIN IAW B727 MM 57-41-1. CORROSION TASK CARD NUMBER C53-100-05 PART 3 OF 4. NON-ROUTINE TASK CARD NUMBER 002024.Sep 17, 1997 · N727CK · Boeing 72722CSDR 98ZZZX44Fitting · crackedINSPECTION FOUND LEFT AND RIGHT WING ATTACH FITTINGS CRACKED.Sep 9, 1997 · N272BA · Beech 76SDR 98ZZZX43Fitting · crackedINSPECTION FOUND LEFT AND RIGHT WING ATTACH FITTINGS CRACKED.Sep 9, 1997 · N272BA · Beech 76SDR 98ZZZX49Fitting · crackedINSPECTION FOUND LEFT AND RIGHT WING ATTACH FITTINGS CRACKED.Aug 31, 1997 · N5424M · Beech 76SDR 98ZZZX48Fitting · crackedINSPECTION FOUND LEFT AND RIGHT WING ATTACH FITTINGS CRACKED.Aug 31, 1997 · N5424M · Beech 76SDR 98ZZZX42Fitting · crackedINSPECTION FOUND LEFT WING ATTACH FITTING CRACKED.Aug 25, 1997 · N24KK · Beech 76SDR 97ZZZX3808Attachment · damagedDAMAGED LEADING EDGE/MAIN SPAR/TRAILING EDGE AT WING CONNECTIONS TO FUSELAGE. A NEED FOR REINFORCEMENT IN THESE AREAS AND IN MAIN FUSELAGE SECTIONS NEED TO BE REINFORCED WITH ADDITIONAL BRACE AND HEAVY DUTY CONNECTION BRACING PLATES DUE TO EXCESSIVE ICE AND Aug 14, 1997 · N7377T · Cessna 172ASDR 97FDEA00523Terminal Fitting · corrodedWHILE WORKING NR 0696, FOUND CORROSION THE AFT EDGE OF L/W AFT TERMINAL FITTING. *S/D* REMOVED BOTTLE PIN AND BUSHING, REAMED FITTING, INSTALLED NEW BUSHING AND BOTTLE PIN AFTER CORROSION REMOVED IAW FED-EX SRM 51-10-1, FED-EX M/M 57-41-11.Aug 11, 1997 · N145FE · Boeing 72727CSDR UPS98227489Bottle Pin · corrodedINSPECTION TYPE:D RT BS 750 REAR SPAR BOTTLE PIN FOUND CORRODED (PITTING CORROSION). PIN REPLACED IAW WITH MM 57-41-00.Aug 5, 1997 · N905UP · Boeing 72751CSDR AALA971119Bottle Pin · crackedTUL - CRACK IN RIGHT WING FORWARD BOTTLE PIN CASTING. INSTALLED SERVICEABLE RT WING FORWARD BOTTLE PIN CASTING PER DRAWING 64-08336 AND DRAWING 65-16200. TST: 75,765 HOURS. CYCLES: 52,034. (X)Jun 19, 1997 · N6835 · Boeing 727223SDR AALA971116Bushing · corrodedTUL - RIGHT WING FORWARD BOTTLE PIN BUSHING CORRODED BEYOND LIMITS. REPLACED BOTTLE PIN BUSHING SRM 51-10-1. TST: 75,765 HOURS. CYCLES: 52,034. (X)Jun 18, 1997 · N6835 · Boeing 727223SDR 97ZZZX2918Angle · corrodedDURING ANNUAL INSPECTION, INTERGRANULAR CORROSION WAS FOUND IN ANGLE REINFORCEMENT AT RT WING SPAR BUTT WHERE SPAR BOLTS TO FUSELAGE SPAR CARRY-THROUGH. DIFFICULT AREA TO INSPECT WITHOUT REMOVAL OF COCKPIT HEADLINER. SUBMITTER STATED IMPROPER HEAT TREATMENT Jun 9, 1997 · N66221 · Cessna 150MSDR DHL9770264DFitting · crackedAT D-CHECK, RT 870 BOTTLE PIN HOLE HAS CRACK AT FWD LOWER RADIUS. ACCOMPLISH NDT HFEC INSPECTION, REMOVED RIGHT AFT BS 870 TERMINAL FITTING, HFEC ALL FASTENER HOLES. REPLACED BOTTLE FITTING PER AVITAS MODIFICATION ORDER 97PMSI-155M-2, N/R 3311.May 28, 1997 · N702DH · Boeing 72730CSDR UPS97223082Bottle Pin · corrosionINSPECTION TYPE:D, CORROSION ON FLANGE OF FRONT SPAR BOTTLE PINS AT BS 740 LT AND RT. LT AND RT BOTTLE PIN REPLACED IAW MM 57-41-1 AND RT BOTTLE PIN BS 740 FITTING REPLACED.Apr 24, 1997 · N913UP · Boeing 72762CSDR UPS97222521Casting · corrosionINSPECTION TYPE: SI. R/W AFT BOTTLE PIN WING AND BODY FORGING BUSHINGS ARE WATER CONTAMINATED. REPAIRED R/W AFT BOTTLE PIN WING AND BODY FORGING PER SB 727-57- 0152 AND UPS SRM ADDENDUM B727-5710-1910D.Apr 4, 1997 · N909UP · Boeing 72727CSDR UPS97222520Casting · corrosionINSPECTION TYPE: SI. L/W AFT BOTTLE PIN WING AND BODY FORGING BUSHINGS ARE WATER CONTAMINATED. REPAIRED L/W AFT BOTTLE PIN WING AND BODY FORGING PER SB 727-57-0152 AND UPS SRM ADDENDUM B727-5710-1910D.Apr 4, 1997 · N909UP · Boeing 72727CSDR UPS97222514Fitting Pin · corrodedINSPECTION TYPE: SI. LEFT REAR BODY BUSHING AND TERMINAL PIN REQUIRE REPLACEMENT DUE TO CORROSION. REMOVED AND REPLACED LT REAR (870) BOTTLE PIN AND BUSHING IAW MM 57-41-11 AND MM 57-41-01.Apr 3, 1997 · N209UP · Boeing 727247SDR AALA970678Fitting · crackedTUL - LEFT WING ATTACH FITTINGS IS CRACKED AT STATION 1159, BETWEEN LONGERON 34L AND 35L. REPAIRED CRACKED WING ATTACHMENT FITTING PER SRM 57-20-00 VOL I PG 25. (M)Apr 3, 1997 · N134AA · Doug DC1010SDR 97ZZZX1936Attach Fitting · corrodedA COMMON WATER CORROSION PROBLEM HAS BEEN FOUND WITH THESE SERIES OF AIRCAFT. ALMOST WITHOUT EXCEPTION, WATER HAS BEEN ENTERING THE INTERIOR OF THE CABIN AT FS 187.84 AND FS 138.63. THEN WATER IS ABSORBED BY THE INSULATION AND CARPET. THIS CREATES A POTENTIApr 1, 1997SDR 97ZZZX1935Attach Fitting · corrodedA COMMON WATER CORROSION PROBLEM HAS BEEN FOUND WITH THESE SERIES OF AIRCAFT. ALMOST WITHOUT EXCEPTION, WATER HAS BEEN ENTERING THE INTERIOR OF THE CABIN AT FS 187.84 AND FS 138.63. THEN WATER IS ABSORBED BY THE INSULATION AND CARPET. THIS CREATES A POTENTIApr 1, 1997SDR 97ZZZX1698Fitting · corrodedDURING ANNUAL INSPECTION, FOUND AFT WING FITTINGS AND ADJACENT STRUCTURE CORRODED. PIPER SB977 ADDRESSES THIS PROBLEM. CAUSE DUE TO WINDOW SEALS FAILING AND MOISTURE REMAINING IN THE INSULATION.Mar 27, 1997 · N15597 · Piper PA28R200SDR 97ZZZX1697Fitting · corrodedDURING ANNUAL INSPECTION, FOUND AFT WING FITTINGS AND ADJACENT STRUCTURE CORRODED. PIPER SB977 ADDRESSES THIS PROBLEM. CAUSE DUE TO WINDOW SEALS FAILING AND MOISTURE REMAINING IN THE INSULATION.Mar 27, 1997 · N15597 · Piper PA28R200SDR EISA97053Pin · pittedRIGHT FORWARD BOTTLE BIN PITTED AND SCRATCHED, ON LT WING. REPLACED WITH NEW BOTTLE PIN PER MM 57-41-1. (M)Mar 10, 1997 · N6815 · Boeing 727223SDR EISA97052Pin · bad platingRIGHT AFT BOTTLE PIN, PLATING MISSING IN SEVERAL PLACES. REPLACED WITH NEW BOTTLE PIN PER MM 57-41-1. (M)Mar 10, 1997 · N6815 · Boeing 727223SDR EISA97051Pin · corrosionRIGHT AFT BOTTLE PIN OUT OF LIMITS PER MM 57-41-11, ON RIGHT WING. REPLACED RIGHT AFT BOTTLE PIN PER MM 57-41-1. (M)Mar 10, 1997 · N6815 · Boeing 727223SDR 97ZZZX1862Strap · corrodedREAR WING ATTACH STRAP FOUND CORRODED BEHIND FLAP. STRAP DIFFICULT TO SEE THROUGH SPAR CAP. SUBMITTER SUGGESTED LOWERING FLAP AND LOOK ABOVE FLAP UNDER TRAILING EDGE OF WING WHERE IT ATTACHED TO FUSELAGE FOR STRAP CORROSION.Mar 6, 1997 · N38557 · Piper PA28R201TSDR CA970226008Fitting · chafed(CAN) FUSELAGE TO WING ATTACH FITTINGS AT FUSELAGE STRINGER 3 WERE FOUND CHAFED BY FLAP SECONDARY DRIVE CABLE SHEATHS.Feb 4, 1997 · Dhav DHC8311SDR CA970226007Fitting · chafed(CAN) FUSELAGE TO WING ATTACH FITTINGS AT FUSELAGE STRINGER 3 WERE CHAFED BY FLAP SECONDARY DRIVE CABLE SHEATHS.Feb 4, 1997 · Dhav DHC8311SDR 97ZZZX571Fitting · crackedREMOVED THE REAR WING SPAR ATTACH BLOCK FITTINGS, CESSNA P/N C512122, FROM EACH END OF THE REAR SPAR/DOORPOST CARRY-THROUGH CHANNEL FOR INSPECTION. AFTER CLEANING, IT WAS NOTED THE RIGHT FITTING WAS CORRODED AND CONTAINED A CRACK EXTENDING DIAGONALLY FROM THEJan 22, 1997 · N7046S · Cessna 150HSDR AU970075Fitting · corroded(AUS) REAR SPAR RH WING FITTING CORRODED - WING BOLT, NUT AND WASHER ALSO CORRODED - FOUND DURING INSPECTION IAW AD/BEECH55/79Jan 15, 1997 · Beech D55SDR AALA970077H Link · corrodedTUL - MAIN LANDING GEAR H-LINK HAS HOLE AT STA 940 AND CORROSION AFT FOLD AROUND THE PIN HOLE. REMOVED AND REPLACED H-LINK PER MM 57-15-01 AND PERFORMED GEAR SWINGS PER MM. TST: 52,368 HOURS. CYCLES, 32,263. (X)Jan 13, 1997 · N873AA · Boeing 727223SDR 97ZZZX622Spar Bolts · corrodedWHEN INSP WINGS PER SB 88C, FOUND ALL WING SPAR ATTACH BOLTS TO BE CORRODED WITH PITS. BOLTS INSTALLED 101 HRS PRIOR ON 4-20-92. BOLTS WERE APPARENTLY INSTALLED USED AND WITHOUT LUBE.Jan 12, 1997 · Piper PA28R201TSDR AU970383Angle · cracked(AUS) LH INBOARD AND OUTBOARD WING ATTACHMENT ANGLES CRACKED IN THE AREA OF THE TOP RADIUS - CRACK LENGTHS 20MM TO 25MM BY 1MM DEEP (0.787IN TO 0.98IN BY 0.039IN DEEP) - CRACKING WAS FOUND WITH THE NAKED EYE AND CONFIRMED BY DYE PENETRANTJan 7, 1997 · Airtrc AT301SDR 97ZZZX531Fitting · looseDURING ANNUAL INSPECTION, IT WAS DISCOVERED THAT THERE WAS MOVEMENT IN THE WING ATTACH FITTINGS WHERE ATTACH PIN ATTACHES WING TO FUSELAGE. THE AMOUNT OF MOVEMENT WAS .0035 INCH BY MEASUREMENT.Dec 3, 1996 · N13468 · Cessna 177BSDR 97ZZZX4Bolt · corrodedFOUND THE RT WING SPAR BOLT HEAD CORRODED DURING INSPECTION. AFTER REMOVAL SHANK ALSO CORRODED. SUBMITTER RECOMMENDS LIBERAL POLICY OF REPLACING HARDWARE ON OLD AIRCAFT WHEN CORROSION IS SHOWING.Dec 3, 1996 · N2405G · Cessna 182BSDR 9624379986Wing Attach Ftg · corrodedDURING H-CHECK, FOUND CORROSION ON THE CENTER WING FITTING AT FS 600 AND LONGERON 19R. REPLACED FITTING PER SRM 51-10, 51-30-1.Nov 13, 1996 · N986US · Doug DC932SDR 97ZZZX117Bolt · corrosionAIRCRAFT HAS IN EXCESS OF 5,000 HRS. REMOVED WING ATTACH BOLTS AT CUSTOMER'S REQUEST AND FOUND SEVERE CORROSION AND PITTINGS. REPLACED BOLTS WITH NEW. RECOMMEND INSPECTING BOLTS ANNUALLY.Nov 10, 1996 · N345T · Swrngn SA226ATSDR CALA9700025Fitting · corrodedINSPECTION FOUND LT AND RT WING TO BODY KICK FITTINGS CORRODED. THE BODY KICK FITTINGS WERE REPAIRED IAW ECRA 5340-01283.Nov 1, 1996 · N17025 · Boeing 747238BSDR 97ZZZX109Bolt · corrodedAIRCRAFT HAS IN EXCESS OF 5,000 HRS. REMOVED WING ATTACH BOLTS AT CUSTOMER'S REQUEST AND FOUND SEVERE CORROSION AND PITTING. REPLACED BOLTS WITH NEW. RECOMMEND INSPECTING BOLTS ANNUALLY.Nov 1, 1996 · N1YC · Swrngn SA226ATSDR COMA9630152Fitting · chafed7-YEAR THRESHOLD, 4-YEAR INTERVAL CHECK. TASK 191-01I, UPPER ATTACH FITTING FOR LEFT WING AFT SPAR TO FUSELAGE FITTING HAS A DEEP GOUGE. C/W NDT INSPECION, BLENDED OUT DAMAGE IAW SRM. AIRCRAFT TOTAL CYCLES, 27,592.Oct 9, 1996 · N320CA · Saab SF340ASDR 9621919908Fitting · crackedDURING H-CHECK, FOUND A CRACK IN THE WING TO FUSELAGE ATTACH FITTING, FS 609 BETWEEN LONGERONS 22R TO 23R. REPAIRED FITTING (P/N 5910006-44) PER EA 99-111296.Sep 28, 1996 · N958N · Doug DC931SDR 96ZZZX5332Nuts · crackedFOUND 2 NUTS SPLIT ON LT LOWER WING SPAR ATTACH POINT OUTSIDE CABIN. NUTS WERE CRACKED WHEN A/C WAS PAINTED 3 YEARS AGO. PIPER SB 602 COVERS INSPECTION OF THESE NUTS, NO RECORD OF COMPLIANCE.Sep 10, 1996 · N68KS · Piper PA34200TSDR AALA961287Bottle Pin · corrodedTUL - FOUND LEFT WING STATION 870 BOTTLE PIN HAS CORROSION ON PIN. INSTALLED NEW BOTTLE PIN PER 57-41-1. (M)Aug 29, 1996 · N850AA · Boeing 727223SDR 96ZZZX5005Bolt · rustedWHILE REMOVING BOTH WINGS FROM ACFT, FOUND FORWARD WING ATTACH BOLT EXTREMELY DIFFICULT TO TURN. AFTER LUBRICATION, BOLT STILL HARD TO TURN. AFTER BOLT WAS REMOVED, PLATING WAS OBSERVED TO BE GONE, THE BOLT WAS BENT, AND IT HAD SEVERE PITTING FROM RUST, WITHJul 31, 1996 · N89969 · Cessna 152SDR UPS96220729Bottle Pin · corrodedINSPECTION TYPE SI, CORROSION (C53-100-05-4B) RT WING AFT BOTTLE PIN RUSTED AND PITTED AT INTERNAL MATING SURFACE. REMOVED AND REPLACED BOTTLE PIN IAW T/C C53-100-05-4D.Jul 24, 1996 · N920UP · Boeing 727180C
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