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 DL72S990487Fitting · corrodedCORROSION WAS FOUND IN THE BORE OF THE RT WING AFT TERMINAL FITTING. REPAIRED PER ERA 366788-14, REV A.SDR RRXA991139Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, WING, LEFT W/W OVERHEAD O/B SIDE STUB FITTING AT LONGERON 24 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLERS IAW SRM 53-2-0 PG 43/44.SDR AU990057Bolt · cracked(AUS) WING SPAR BOLTS CRACKED UNDER THE BOLT HEAD. PART TC: 3,547.SDR AU990017Bolt · cracked(AUS) WHEN WING SPAR BOLTS WERE MAGNAFLUXED, (NOT A REQUIREMENT OF THIS AD), ALL 12 BOLTS WERE FOUND CRACKED UNDER HEAD. FOUND DURING COMPLIANCE WITH AD/ROBIN/8A2. PART TC: 5,707.SDR QXEA9900165Fitting · damagedPDX - LEFT WING TO FUSELAGE ATTACH CASTING AT FRONT SPAR HAS (3) DINGS APPROXIMATELY .010 DEEP, BY TOP MOUNT BOLT AT RADIUS OF CASING. REPAIRED IAW FOKKER SRM 51-10-4.SDR QXEA9900164Fitting · damagedPDX - RIGHT WING TO FUSELAGE ATTACH CASTING AT FRONT SPAR HAS (2) DINGS APPROXIMATELY .010 DEEP, BY TOP MOUNT BOLT AT RADIUS OF CASTING. REPAIRED IAW FOKKER SRM 51-10-4.SDR 98ZZZX4280Bottle Pin · corrodedDURING A C-CHECK, CORROSION NOTED AT RT REAR SPAR BOTTLE PIN.SDR CALA9801931Fitting · corrodedRIGHT WING TO FUSELAGE AT BS 870 FACE AND BORE HAVE CORROSION. ACCOMPLISHED REPAIR BY OVERSIZE HOLE TO REMOVE CORROSION PER ECRA 5310-63775.SDR CALA9801912Bottle Pin · corrodedINSPECTION FOUND RT WING TO FUSELAGE BOTTLE PIN, BUSHING, AND RETAINING BOLT CORRODED AT BS 870. THE BOTTLE PIN, BUSHING, AND RETAINING BOLT WERE REMOVED AND REPLACED IAW MM 57-41-1, PAGE 403 AND 57-41-11, PAGE 404.SDR CALA9801558Bottle Pin · corrodedINSPECTION FOUND RT AFT BOTTLE PIN CORRODED. THE BOTTLE PIN AND FORWARD AND AFT BUSHINGS WERE REMOVED AND REPLACED, THEN SAFETIED AND SEALED IAW MM 57-41-1.SDR 98ZZZX3125Fitting · corrodedWING FITTING CORRODED. THERE IS NO ACCESS FOR INSPECTION OF PART. AFTER ONE AIRCRAFT HAD WING SEPARATION AND DISCOVERED PART THAT CORRODED, INSPECTED ENTIRE FLEET OF 10 SUPER CUBS AND FOUND CONDITION ON 2 AIRCRAFT (THIS BEING ONE OF THEM). ALL FOUND TO BE FSDR UPS98227488Bottle Pin · corrodedINSPECTION TYPE:D LT BS 750 BOTTLE PIN FOUND WITH LIGHT PITTING CORROSION. PIN REPLACED IAW MM 57-41-00.SDR UPS98227524Bottle Pin · corrosionINSPECTION TYPE-D, RT BS 740 BOTTLE PIN FOUND WITH PITTING CORROSION. PIN REPLACED IAW MM 57-41-00.SDR UPS98227498Bottle Pin · corrodedINSPECTION TYPE:D, LT BS 740 BOTTLE PIN FOUND WITH PITTING CORROSION. PIN REPLACED IAW MM 57-41-00.SDR DL72S981630Fitting · corrodedLEFT WING FWD WING FITTING BORE HAS CORROSION AND SCORING, FOUND WHEN BUSHING REMOVED. REMOVED BTL PIN ON R/C 59, OPN 5508AD AND REMOVED FWD BUSHING PER M/M 57-41-11. FOUND CORROSION TO BE WITHIN .15 OF INNER EDGE OF TERMINAL FITTING AT 10 AND 11 O'CLOCK POSSDR CALA9801333Bottle Pin · corrodedINSPECTION FOUND LT FORWARD WING TO FUSELAGE BOTTLE PIN BLEEDING RUST AT SEALANT AREA. THE BOTTLE PIN WAS REMOVED AND REPLACED IAW MM 57-41-1.SDR COMA9860187Bushing · migratedDURING C-CHECK, FOUND RIGHT FORWARD WING TO FUSELAGE FITTING AFT BUSHING TO HAV E MIGRATED .020. TEMPORARILY REPAIRED IN ACCEPTANCE WITH CANADAIR REPAIR ENGINEERING ORDER NR 601R-57-21-032.SDR UPS98227137Fitting · corrodedINSPECTION TYPE:SI RIGHT WING REAR SPARS BOTTLE PIN AND BODY SIDE ARE DAMAGED (CORROSION C53-100-05-4B). REMOVED BUSHING FOUND CORROSION OUT OF LIMITS IAW SRM 53-40-1 AND HAD BOEING REPAIR IAW DRAWING 65C36301 AND BOEING AGREEMENT NR 6-1171-TA954.SDR CA980706018Fitting · cracked(CAN) STRUT REMOVED TO REPLACE NEW UPPER BUSHINGS. STRUT END SHOWED INDICATION OF SKIN MOVEMENT AT UPPER RIVETS THEN A SCRATCH FOUND ACROSS FACE OF UPPER STRUT END SB 2/41. INSPECTION CARRIED OUT AND A SMALL CRACK WAS FOUND.SDR B4MR98035Bushing · damagedDURING ROUTINE CPCP INSPECTION, FOUND LEFT FRONT SPAR WING TO BODY FITTING BOTTLE PIN BUSHING HAS SECTION OF LINING MISSING. REMOVED AND REPLACED LEFT FRONT SPAR WING TO BODY FITTING BOTTLE PIN BUSHINGS IAW B727 MM 57-41-11. CORROSION TASK CARD NUMBER C53-13SDR B4MR98034Bushing · damagedDURING ROUTINE CPCP INSPECTION, FOUND RIGHT FRONT SPAR WING TO BODY FITTING BOTTLE PIN BUSHING HAS SECTION OF LINING MISSING. REMOVED AND REPLACED RIGHT FRONT SPAR WING TO BODY FITTING BOTTLE PIN BUSHINGS IAW 727 MM 57-41-11. CORROSION TASK CARD NUMBER C53-1SDR AU980621Fitting · corroded(AUS) RT WING LOWER REAR FITTINGS CORRODED.SDR AU980545Fitting · corroded(AUS) LT AND RT UPPER AND LOWER STUB WING ATTACHMENT FITTINGS P/N 0811350-7 AND P/N 0811350-8 CONTAINED SEVERE EXFOLIATION CORROSION.SDR AU980507Angle · cracked(AUS) LT AND RT WING OUTER ATTACHMENT ANGLES CRACKED. CRACK LENGTH APPROXIMATELY 25.4 MM (1 INCH). FOUND DURING INSPECTION IAW AD/AT/16. AIRCRAFT WAS PREVIOUSLY REGISTERED IN NEW ZEALAND AS ZK-SNO.SDR UPS98226694Bottle Pin · pittingINSPECTION TYPE:D PITTING ON FWD EDGE OF RT AFT REAR SPAR TO BODY BOTTLE PIN. BOTTLE PIN REPLACED IAW MM 57-41-01.SDR AU980570Angle · broken(AUS) RT WING ATTACHMENT ANGLE BROKEN THROUGH THE UPPER BOLT HOLE. ALL ATTACHMENT BOLTS FRETTING. FRETTING ALSO FOUND ON THE ANGLE TO SPAR INTERFACE. THE VERTICAL BOLT/NUT ASSEMBLIES CONTAINED DRIED CHROMATE JOINING PASTE.SDR AU980567Angle · cracked(AUS) LT WING ATTACHMENT ANGLE SUSPECT CRACKED AND MOUNTING BOLTS LOOSE. FOLLOWING REMOVAL AND INSPECTION, NO CRACK WAS FOUND IN THE ANGLE, HOWEVER, FRETTING WAS FOUND ON THE ANGLE MOUNTING FACES. CHROMATE JOINING COMPOUND WAS FOUND TO HAVE DRIED OUT.SDR AU980566Angle · cracked(AUS) RH WING ANGLE BRACKET CRACKED AT OUTER VERTICAL BOLT POSITIONS. ALL VERTICAL BOLTS FRETTING UNDER THE HEADS. DRIED CHROMATE JOINING PASTE FOUND IN BOLT/NUT ASSEMBLIES.SDR C2XA98IA119Fitting · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT WING AUXILLARY SPAR TO FUSELAGE ATTACH FITTING WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE FITTING IAW DER APPROVED EMBRAER FAX NR SST-0618/98, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR 98ZZZX1581Bolt · corrodedIN C/W AD 85-22-05, WING BOLT REJECTED DUE TO MINUTE GALLING CORROSION SPOT IN THE INNER RADIUS. BOLT REMOVED FROM THE LT LOWER FORWARD OUTER WING PANEL ATTACHMENT.SDR AU980460Fitting · loose(AUS) INSPECTION OF WING FITTINGS REVEALED RELATIVE MOVEMENT BETWEEN FITTINGS AND SPAR. THE AIRCRAFT HAD BEEN TREATED WITH 'BOESHIELD' IN FEB 93. PART TC: 4,830.SDR UPS98226170Bottle Pin · corrodedINSPECTION TYPE-SI, RT WING AFT BOTTLE PIN CORRODED. REPLACED BOTTLE PIN PER 727 MM 57-41-01.SDR CALA9800508Bottle Pin · corrodedINSPECTION FOUND RT FORWARD BOTTLE PIN CORRODED AT HEAD FLANGE AND NECK AREA. THE RT FORWARD BOTTLE PIN WAS REPLACED IAW MM 57-41-1.SDR 98ZZZX919Bolt · wornDURING WING REMOVAL, BOTH AFT SPAR TO FUSELAGE ATTACH BOLTS (AN4-13) WERE FOUND EXTREMELY WORN. THE HOLES IN THE FUSELAGE ATTACH POINTS WERE ALSO WORN OVERSIZE (APPROXIMATELY .3125 INCH). APPARENT CAUSE OF THIS DEFECT IS INSUFFICIENT BEARING AREA OF THE FUSESDR ABXA9800099Fitting · corrodedDURING C-CHECK, FOUND THE RIGHT WING, LOWER OUTBOARD HORIZONTAL FLANGE OF THE BULKHEAD/AILERON HINGE FITTING AT STA XRS477 INSIDE THE FUEL VENT TANK CORRODED BEYOND LIMITS. INSTALLED REPAIR IAW ABX REA D957-22556MR.SDR DHL9872464CBottle Pin · corrodedAT C-CHECK, CORROSIN BLEEDING FROM RT WING SPAR TO BODY FITTING. REMOVED CORROSION, BLENDED OUT FACE OF FITTING. FLAP PEENED FITTING, INSTALLED BUSHING AND INSTALLED BOTTLE PIN PER AVITAS EO PMSI191R0-3. N/R 7815.SDR DL72W980346Fitting · corrodedCORROSION RT AFT WING TERMINAL FITTING AFT BUSHING BORE. BORED FITTING BORE TO 4.500 PER SRM 53-40-01 TO REMOVE CORROSION. TURNED BUSHING TO PROPER FIT. TREATED BUSHING. OK TO TREAT FITTING BORE. TREATED BORE, OK TO INST SLEEVE. INSTALLED SLEEVE PER SRM SDR 98ZZZM693Bolt · wrong partLEFT FRAME 29 WING TO FUSELAGE LUG ATTACH BOLT DIFFERENT TYPE FASTENER INSTALLED AND DOES NOT HAVE ANY MARKINGS ON HEAD OF BOLT. REPORTED DETAILS TO BAE RDO, THE OVERSIZE BOLT FOUND AT FR 29 LEFT HYLT STRINGER NR 12 POSITION WAS INSTALLED AT BUILD. (M)SDR UPS98225664Bottle Pin · corrodedINSPECTION TYPE-SI, R/W REAR BOTTLE PIN IS CORRODED. ALSO, FWD AND AFT BUSHINGS ARE MISSING SECTION OF MICARTA INNER SLEEVE CORROSION (C53-100-05.00-04). REMOVED AND REPLACED R/W AFT BOTTLE PIN ON NRC 657574 IAW MM 57-41-01, BUSHING REPLACED ON AOG (BOEING) SDR MZZA98070Nut · missingKUL - Q-CHECK - DURING INSPECTION OF RT WING HIP TANK, FOUND A BOLT MIGRATED AND BOTH NUTS MISSING OFF SUPPORT STRUT AT WBL 74 THAT SECURES RT AFT WING TERMINAL BOTTLE PIN FITTING. MIGRATED BOLT INSPECTED AND REINSTALLED. BOTH NUTS REPLACED IAW SRM 51-30-2. SDR 98ZZZX530Bolt Kit · wrong partsTHE BOLT KIT LISTED IS FOR THE UPPER AND LOWER AFT WING ATTACH FITTINGS FOR A BEECH SERIES 200, UPON RECEIVING 4 OF THESE KITS, NOTICED THE WASHERS INCLUDED IN THE KIT DID NOT HAVE A SMOOTH CONTINUOUS OUTER RADIUS WHICH IS NOTED IN BEECH 200 SRM CH 57-17-01 PSDR 98ZZZX531Bolt Kit · wrong partsTHE BOLT KIT LISTED IS FOR THE UPPER FORWARD WING BOLTS FOR A BEECH 200. UPON RECEIVING 2 EACH KITS, NOTED THE WASHERS INCLUDED WERE NOT PROPERLY RADIUSED ON THE OUTER EDGE. THE BEECH 200 SRM CH 57-17-01 P 212 SPECIFICALLY INSTRUCTS TO INSTALL SMOOTH CONTINUSDR UPS98225581Bottle Pin · pittedINSPECTION TYPE-D, RIGHT HAND REAR BOTTLE PIN HAS WEAR AND LIGHT PITTING. RIGHT HAND AFT BOTTLE PIN REPLACED IAW MM 57-41-01.SDR UPS98225580Bottle Pin · pittedINSPECTION TYPE-D, LT REAR SPAR BOTTLE PIN HAS WEAR AND LIGHT PITTING. LT AFT BOTTLE PIN REPLACED IAW MM 57-41-01.SDR 98ZZZX538Barrel Nut · wrong partKIT 101-4024-1S CONTAINS THE FORWARD LOWER WING BOLT, PL WASHER AND BARREL NUT FOR INSTALLATION ON BEECH 200 SERIES ARICRAFT. THE BARREL NUT ASSY PN 80691CF-1612 WAS OF IMPROPER TOLERANCES AND WOULD NOT FIT IN WING 'BATHTUB' FITTING. FURTHER INVESTIGATION RESDR AU980003Bracket · cracked(AUS) LH WING REAR ATTACHMENT BRACKET BROKEN THROUGH LOWER BOLT HOLE. SUSPECT CAUSED BY UNREPORTED HEAVY LANDING.SDR 98ZZZX489Bearing Block · corrodedUPON REMOVING BOTH WINGS TO INSTALL MONARCH PLASTIC FUEL TANKS, THE REAR SPAR INBOARD ATTACH BLOCKS, LEFT AND RIGHT, WERE FOUND TO HAVE INTERGRANULAR CORROSION IN THE INBOARD SLOT AREA ABOVE THE LARGE BOLT HOLES. CORROSION AREA ABOUT .50 INCH WIDE BY .1250 INSDR DL72S972579Fitting · corrosionCORROSION ON RT FRONT SPAR WING TO BODY FWD FITTING. REMOVED CORROSION AT PER SRM 51-10-6. TREATED AND PAINTED PER PS 900-3-6.SDR DL72S972578Fitting · corrosionCORROSION ON LEFT AFT SPAR WING TO BODY FITTING (AFT END). REMOVED CORROSION IAW SRM 53-40-1 PG 18. TREATED AND PAINTED PER PS 900-3-6.SDR 97ZZZX4814Crush Washer · deformedUPON INSPECTION OF AIRCRAFT, FOUND LEFT WING SETTING AT A HIGHER ANGLE OF INCIDENCE. FURTHER INSPECTION REVEALED THE UPPER AFT CRUSH WASHER AND BOLT HAD SLIPPED DOWN APPROXIMATELY .25 INCH CAUSING LEFT WING TO HAVE MORE LIFT. AIRCRAFT HAD JUST FINISHED WITH
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