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 UPS96220745Bottle Pin · corrodedINSPECTION TYPE-C, SLIGHT SURFACE CORROSION ON INNER SURFACE OF LT REAR BOTTLE PIN. NEW BOTTLE PIN INSTALLED IAW MM 57-41-01.SDR 96ZZZX3789Fitting · corrodedOWNER/OPERATOR FOUND RT WING WOULD CREAK AND GROAN WHEN WING WAS FLEXED. INSPECTION REVEALED THE LOWER FORWARD MAIN SPAR ATTACH FITTINGS WERE WORN AROUND THE ATTACH BOLT. THE BOLT WAS FOUND TO BE IN GOOD CONDITION. AFTER REMOVAL OF THE FITTINGS, FOUND THE BSDR 96ZZZX3788Fitting · corrodedOWNER/OPERATOR FOUND RT WING WOULD CREAK AND GROAN WHEN WING WAS FLEXED. INSPECTION REVEALED THE LOWER FORWARD MAIN SPAR ATTACH FITTINGS WERE WORN AROUND THE ATTACH BOLT. THE BOLT WAS FOUND TO BE IN GOOD CONDITION. AFTER REMOVAL OF THE FITTINGS, FOUND THE BSDR 96ZZZX3787Fitting · corrodedOWNER/OPERATOR FOUND RT WING WOULD CREAK AND GROAN WHEN WING WAS FLEXED. INSPECTION REVEALED THE LOWER FORWARD MAIN SPAR ATTACH FITTINGS WERE WORN AROUND THE ATTACH BOLT. THE BOLT WAS FOUND TO BE IN GOOD CONDITION. AFTER REMOVAL OF THE FITTINGS, FOUND THE BSDR AU961102Fitting · cracked(AUS) LH AND RH WING FRONT SPARS CRACKED ON LOWER RADIUS OF FRONT AND REAR WING TO FUSELAGE ATTACHMENT LUGSSDR DHL9672163CBottle Pin · corrosionAT C-CHECK, LEFT HAND BOTTLE PIN HAS CORROSION AND WEAR MARKS IN SIDE WALL. REMOVED DAMAGE PER S/B 57-0175, FABRICATED REPAIR SLEEVES PER SRM 57-10-7, INSTALLED SLEEVES BUSHINGS AND BOTTLE PIN PER SRM 57-10-7 AND MM 57-41-1.SDR DHL96721104Fitting · gougedAT C-CHECK, LEFT WING FRONT SPAR TERMINAL FITTING DAMAGED. REAMED DAMAGED AREA, MADE BUSHING SLEEVE PER DRAWING 65C36176, INSTALLED PER BOEING TELEX, INSTALLED BOTTLE BUSHING AND PIN PER M/M 57-41-1.SDR DHL9672184CFitting · corrodedAT C-CHECK, RT WING FWD BOTTLE PIN HOLE END FITTING CORRODED. REAMED DAMAGED TERMINAL FITTING, FABRICATED BUSHING SLEEVE PER DRAWING 65C36176, INSTALLED SLEEVE AND INSTALLED BOTTLE PIN AND BUSHING PER MM 57-41-1 AND 57-41-11.SDR 96FDEA00980Terminal Pin · corrodedCORROSION C53-100-05-1/3 LEFT AFT WING TO BODY FITTING TERMINAL PIN. REMOVED AND REPLACED LEFT WING REAR SPAR TO BODY FITTING TERMINAL PIN PER FEDEX MM 57-41-1.SDR 96FDEA00979Terminal Pin · corrodedCORROSION C53-100-05-2/4 RIGHT WING REAR SPAR TO BODY FITTING TERMINAL PIN FOUND TO BE CORRODED. REMOVED AND REPLACED RIGHT WING REAR SPAR TO BODY FITTING TERMINAL PIN PER FEDEX MM 57-41-1.SDR UPS96220052Bushing · corrodedINSPECTION TYPE 'C', RT WING FWD BOTTLE PIN HOLE HAS CORROSION. REMOVED AND REPLACED BOTTLE PIN BUSHING FWD IAW MM 57-41-11.SDR UPS96220051Bottle Pin · corrodedINSPECTION TYPE 'C', RT WING FWD BOTTLE PIN HAS CORROSION ON MATING FLANGE. REMOVED AND REPLACED RT TERMINAL PIN IAW MM 57-41-1.SDR AU960453Bolt · cracked(AUS) WING SHOULDER BOLTS (2OFF) CRACKED - FOUND DURING MAGNETIC PARTICLE INSPECTION (MPI)SDR 96ZZZX2024Attach · defectiveINSPECTED AIRCRAFT FOR NDT-UTT PER AD 95-12-01, RIGHT FORWARD WING SPAR ATTACH. PRELIMINARY INSPECTION SHOWED VISIBLE POCKET INBETWEEN THE STEEL PLATES. WHEN TESTING UTT, A LOW READING WAS DETECTED IN THIS AREA WHICH WAS BELOW THE MINIMUM THICKNESS ALLOWED. SDR 96ZZZX2746Shoulder Bolt · mismanufacturedDURING C/W AD 95-19-15, ONE OF THE FOUR INBOARD WING ATTACH BOLTS WAS FOUND TO HAVE BEEN INCORRECTLY MANUFACTURED, WITH AN AREA OF THE THREADED SHANK MISSING, AND AN AREA OF THE HEX HEAD MIS-MACHINED.SDR UPS96205694Bushing · corrodedWHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION LEFT FRONT BOTTLE PIN BUSHING, ON FWD FACE. REMOVED AND REPLACED BUSHING IAW MM 57-41-11 AND 57-10-7.SDR AU960308Dowel · worn(AUS) WING TO FUSELAGE LOCATING DOWEL PINS WORN ALLOWING MOVEMENT AT ATTACHMENT POINTS - SUSPECT CAUSED BY USE OF ACF 50 MATERIAL WORKING BETWEEN MATING SURFACES AND CAUSING MOVEMENTSDR 96ZZZX1984Block · corrodedSPAR BEARING BLOCK (FWD WING SPAR ATTACH POINT) FOUND SEVERELY CORRODED.SDR 96ZZZX1786Attach Fitting · corrodedDURING C/W AD 95-12-01, (FWD SPAR FITTING INSPECTION), HEAVY RUST FOUND INSIDE RT TUBE CLUSTER; MAINLY BEHIND THE CLOSE-OUT PLATE BETWEEN THE ATTACH FITTING LUGS. THIS AREA USUALLY CANNOT BE INSPECTED, BUT IN THIS CASE, THE CLOSE-OUT PLATE WAS EASILY REMOVED SDR AALA960068Fitting · crackedTUL - CAST FITTING BETWEEN LONGERONS 28 AND 29 AT STA 1156 ARE CRACKED FROM TOP AFT HOLE THROUGH FASTENER TO RADIUS. CUT OUT CRACKED AREA PER 53-30-00, PAGE 27. DRILLED REPAIR PARTS PER SRM 53-30-00, PAGE 27 AND PRIMED AND TREATED PARTS PER SRM 51-21-01 AND SDR 95ZZZX6933Bolt · crackedWING ATTACH BOLTS REMOVED FOR 5-YEAR MAGNAFLUX INSPECTION. ONE BOLT, THE UPPER AFT SHOWED INDICATIONS OF A CRACK.SDR 96ZZZX200Fitting · corrodedCORROSION FOUND ON BOTH WING REAR ATTACH FITTINGS. THIS PROBLEM IS ADDRESSED BY PIPER SB 977. IT APPEARS THERE IS SURFACE CORROSION ON THE STEEL FITTING AND DISSIMILAR METAL CORROSION ON THE SPAR CARRY-THROUGH STRUCTURE. SUBMITTER RECOMMENDED THIS SB BE MADSDR 95FDEA01720Pin · corrodedR/W REAR SPAR TO BODY FITTING PIN CORRODED. REMOVED RUSTED CORRODED BODY FITTING PIN. INSTALLED NEW R/W REAR TO BODY FITTING PIN MM 57-41-1.SDR A6WR95003Bolts · looseDURING STRUCTURAL INSPECTION, FOUND LT WING TO FUSELAGE TOP AND BOTTOM ATTACH BOLTS AT FRAME 26 SHOWING EVIDENCE OF SPINNING. REMOVED SEALANT, INSPECTED BOLT, AND FOUND SECURE. RESEALED BOLT. UNDER INVESTIGATION BY AVRO ENGINEERING. (X)SDR A6WR95002Bolt · looseDURING STRUCTURAL INSPECTION, FOUND LT WING TO FUSELAGE BOTTOM ATTACH BOLT AT FRAME 29 SHOWING SIGNS OF SPINNING. REMOVED SEALANT, INSPECTED BOLT AND FOUND SECURE, RESEALED BOLT. UNDER INVESTIGATION BY AVRO ENGINEERING. (X)SDR 95FDEA01488Fitting Pin · corrodedRIGHT WING REAR SPAR BODY FITTING FWD AND REAR BUSHINGS WORN, BODY FITTING PIN FLANGE CORRODED. INSTALLED NEW RT WING REAR SPAR BODY FITTING PIN PER SRM 51-10-1 PG 4, REPLACED FWD AND REAR BUSHINGS PER 51-10-1 PG 4, ESO 11782 AND FEDEX EA NR 7-5310-25827.SDR EISA95399Bottle Pin · corrodedLEFT FORWARD WING TERMINAL FITTING BOTTLE PIN IS PITTED AND CHROME IS FLAKING OFF. REMOVED AND REPLACED BOTTLE PIN WITH SEREVICEABLE UNIT IAW BOEING MAINTENANCE MANUAL CHAPTER 57. (M)SDR EISA95398Bottle Pin · corrodedLEFT AFT WING TERMINAL FITTING IS PITTED AND CHROME IS FLAKING. REMOVED AND REPLACED WITH SERVICEABLE UNIT, P/N 69-13901-5, IAW BOEING MM 57-00-00. (M)SDR EISA95397Bottle Pin · corrodedRIGHT AFT WING FITTING TERMINAL BOTTLE PIN IS PITTED AND CHROME IS FLAKING OFF. REMOVED AND REPLACED RIGHT AFT WING BOTTLE PIN, P/N 69-13901-5, IAW MM 57-00-00. (M)SDR EISA95396Bottle Pin · corrodedRIGHT FORWARD WING TERMINAL FITTING BOTTLE PIN IS PITTED AND CHROME IS FLAKING OFF. REMOVED AND REPLACED RIGHT FORWARD BOTTLE PIN WITH SERVICEABLE UNIT IAW BOEING MM CH 57-00-00. (M)SDR DL72S953767Fitting · corrodedDURING HMV, FOUND LT AFT WING ATTACH BODY FITTING WAS CORRODED AT 6 O'CLOCK POSITION. REPAIRED PER SRM 57-10-7.SDR DL72S952935Fitting · corrodedAT HMV, LT FWD TERMINAL PIN BODY FITTING IS CORRODED IN SEVERAL AREAS. REPAIRED PER SRM 57-10-7.SDR 96ZZZX4416Shoulder Bolt · shearedPART OF HANGAR FELL ON TAIL ASSEMBLY RENDERING PLANE UNFLYABLE. WHEN REMOVED WINGS FOR TRANSPORTATION TO REPAIR SHOP, A RIGHT WING SHOULDER ATTACH BOLT WAS SHEARED (DID NOT HAPPEN WHEN THE TAIL WAS DAMAGED). ONLY TWO HOURS SINCE ANNUAL. AD IN EFFECT, 94-CE-1SDR UPS203320Bottle Pin · corrodedWHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON BOTTLE PIN FOR RIGHT WING, ZONE 6 AREA 75. REMOVED AND REPLACED BOTTLE PIN IAW SRM 57-41-01, 57-10-7, 57-41-11.SDR 95ZZZX2610Spar Plate · holes wornLEFT WING REAR SPAR BOLT FOUND LOOSE AND CHAFING AT ANNUAL INSPECTION. BOLT HOLE IN THE FUSELAGE MOUNT WORN SPANWISE .030 INCH OVERSIZE, WING SPAN ATTACH PLATE IN THE WING WORN SPANWISE .025 INCH OVERSIZE (HOLES ELONGATED).SDR 95ZZZX1976Fitting · rustedDURING ANNUAL INSPECTION, THE AFT WING SPAR STEEL ATTACHMENT FITTINGS INSIDE THE FUSELAGE WERE FOUND SEVERELY RUSTED WAS ABLE TO BREAK OFF FLAKES OF RUST WITH A FINGERNAIL. THIS AREA SEEMS PRONE TO TRAP WATER. THE INSULATION HAD BEEN PREVIOUSLY REMOVED FROM SDR 95ZZZX1975Fitting · rustedDURING ANNUAL INSPECTION, THE AFT WING SPAR STEEL ATTACHMENT FITTINGS INSIDE THE FUSELAGE WERE FOUND SEVERELY RUSTED, WAS ABLE TO BREAK OFF FLAKES OF RUST WITH A FINGERNAIL. THIS AREA SEEMS PRONE TO TRAP WATER. THE INSULATION HAD BEEN PREVIOUSLY REMOVED FROMSDR 95ZZZX1885Attach · bolt looseLEFT FORWARD WING ATTACH BOLT WAS FOUND LOOSE WHICH CAUSED ELONGATION OF THE CABIN BOLT HOLE. REPAIRED BY REPLACING ITEMS NOTED IN BEECH SI 0042-031RII. FOUND DURING ANNUAL INSPECTION.SDR DL72W951020Fitting · crackDURING HMV, FOUND LEFT REAR BOTTLE PIN FITTING INDICATING CRACK AT 10 O'CLOCK POSITION. REPAIRED PER SRM 57-10-7.SDR BIER950005Attach Fitting · corrodedAT COMPLIANCE WITH PIPERS SB 977, FOUND WING REAR ATTACH FITTING, LEFT, FLAKING AT POINT WHERE BRACKET PASSES THROUGH AIRCRAFT SKIN. REMOVED FITTING AND REPLACED WITH NEW PIPER PART.SDR 95ZZZX1735Support · corrodedWHILE PERFORMING PIPER SB 977, THE REAR WING ATTACH BRACKETS ON BOTH THE RIGHT AND LEFT WERE FOUND BADLY CORRODED. WHEN PART WAS REMOVED, MORE RUST WAS FOUND THAT WAS VERY DIFFICULT TO SEE UNTIL PART WAS REMOVED. SUBMITTER STRONGLY RECOMMENDS SB BE FOLLOWED SDR 95ZZZX1734Support · corrodedWHILE PERFORMING PIPER SB 977, THE REAR WING ATTACH BRACKETS ON BOTH THE RIGHT AND LEFT WERE FOUND BADLY CORRODED. WHEN PART WAS REMOVED, MORE RUST WAS FOUND THAT WAS VERY DIFFICULT TO SEE UNTIL PART WAS REMOVED. SUBMITTER STRONGLY RECOMMENDS SB BE FOLLOWED SDR 9502332284Chord · damagedDURING PERIODIC CHECK, MAINTENANCE FOUND WING TO BODY UPPER RIB CHORD AT FS 760, RBL 70.5 DAMAGED. REPAIRED PER NWA EA 22-093804.SDR 95ZZZX958Fitting · rustedIN COMPLYING WITH PIPER SB 977, BOTH FORWARD AS WELL AS THE AFT WING ATTACH FITTINGS WERE FOUND SEVERELY RUSTED. THE BRACKETS FOR THE ATTACHMENT OF THE FORWARD SEAT BELTS WERE FOUND IN THE SAME CONDITION. AT THE FORWARD UPPER FUSELAGE FITTINGS AT STA 73, REA
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