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.
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
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 VGCA200700003Attach Fitting · crackedDURING VISUAL INSPECTION OF WING ATTACH FITTING FOUND CRACKS BETWEEN RIVET HOLES UPPER FWD PORTION OF FITTING (LT AFT WING TO FUSELAGE ATTACH FITTING).SDR TRAX200701567Shear Tie · corrodedLEFT WING SKIN FLANGE FOR PANEL 522CT CORRODED. BLENDED IAW SRM 57-14-12 FIG 401U/T E/C IAW NTM NO CRACKS FOUND. INSTALLED SRM 51-25-01 FABRICATION COVER ON W/C 2000-206 MATERIAL THICKNESS: 0.753 MATERIAL REMOVED: 0.009 WITHIN LIMITS AS PER SRM: 57-14-12 FIGSDR TRAX200701566Shear Tie · corrodedLEFT WING SKIN FLANGE FOR PANEL 521DT CORRODED. BLENDED IAW SRM 57-14-12 FIG 401U/T E/C IAW NTM NO CRACKS FOUND IAW SRM 51-25-01.SDR CA071019002Nut Plate · misrepaired(CAN) UPON INSPECTING THE FUEL TANKS, FOUND SEVERAL NUTPLATES PREVIOUSLY DAMAGED. UPON FURTHER INSPECTION FOUND THAT AT A PREVIOUS TIME, SOME SCREWS BROKE OFF IN THE NUTPLATES AND RATHER REPAIR/REPLACE THE NUTPLATES, IT APPEARS THE DAMAGED NUTPLATES WERE DRILLSDR 2007UALA04309Support Bracket · crackedRIGHT WING OUTBOARD FLAP INBOARD JACK SCREW FWD JACKSCREW SUPPORT BRACKET INBOARD LWR RADIUS ABOVE BORE LUG CRACKED. RT WING OTBD FLAP INBD JACK SCREW FWD JACK SCREW SUPPORT BRACKET INBD LOWER RADIUS ABOVE BORE LUG CRACKED. REMOVED AND REPLACED FLAP JACKSCRSDR 07FDEA04633Attach Fitting · crackedRT AILERON (OTBD) CAVITY HAS CRACKED ATTACH CLIP LOCATED BET WING TRAILING EDGE RIB AT STA 658.63 AND CAVITY AFT SPAR FABRICATED CLIP BETWEEN WING TRAILING EDGE, STA 658.63 CAVITY AFT SPAR. REF SRM 51-30-02, DWG 65-19289 PG 1. THIS IS CLASSIFIED AS A MINOR RSDR SWIA200719151Bracket · crackedRIGHT GEAR AFT BRAKE TRANSDUCER BRACKET IS CRACKED, FOUND AT C-CHECK. REPLACED BRACKET IAW CRJ200 SRM REF 51-42-06 PG 11.
SDR SWIA200719150Bracket · crackedLEFT GEAR AFT BRAKE TRANSDUCER BRACKET IS CRACKED, FOUND AT C-CHECK. REPLACED BRACKET IAW CRJ200 SRM REF 51-42-06 PG 11.SDR AALA20071967Support · damagedAFW - FLAP SUPPORT ACTUATOR HAS HOLES FOR BEARING 165 THAT ARE BEYOND PUBLISHED SIZE OF ESO 20174. REPAIRED PER AA MRB 777 218.SDR SWIA200719120Bracket · crackedRIGHT FORWARD BRAKE TRANSDUCER BRACKET IS CRACKED, FOUND AT C-CHECK. REPLACED BRAKE TRANSDUCER BRACKET PER CRJ200 SRM REF 51-42-06.
SDR 07FDEA04446Lug · corrodedFOUND CORROSION ONE BEARING BORE OF RT WING PYLON OUTBOARD MOUNTING LUG REPAIR PERFORMED BY BLEND OUT CORROSION, NDT FOR DAMAGE FREE IAW EA 6-5720- 81124 AND RAS/BAE/1000347/2005 ISS A.SDR TRAX200701404Attach Angle · crackedLT WING L/E 530JL I/B ATTACH ANGLE IS CRACKED IN UPPER AND LOWER RADIUS. REMOVED LT L/E WING ATTACH ANGLE THAT WAS CRACKED, AND LOCATED NEW SERVICEABLE P/N 600-12045-11 AND INSTALLED, IAW CRJ SRM 51-40-11.SDR 07FDEA04187Fitting · damagedAREAS OF IMPACT DAMAGE FOUND ON THE AFT FACE OF THE OUTBOARD LUG ON THE RT WING PYLON MOUNTING (ATTACH FITTING), RIB 8-9. REPAIR PERFORMED BY BLENDING DAMAGE TO REMOVE ALL SHARP EDGES, HFEC INSPECTION AND INSTALLING NEW SELF-LUBRICATING BEARING IAW EA 6-5720-SDR 1214834312170Bracket · corrodedRIGHT WING AT RIB 17 OF LOWER REAR SPAR SIDE STAY BRACKET CORRODED. REMOVED AND REPLACED FITTING IN ACCORDANCE WITH SRM 51-25-04.SDR 07FDEA04133Fitting · crackedCRACKS FOUND AT FRAME 47 INTERNAL FITTING LT HOLE NR E (1MM) IN REAR SPAR, HOLE NR G (2MM) IN CORNER FITTING, HOLE NR I (2MM) IN FWD FITTING, HOLE NR N (2MM) IN FWD FITTING, REPAIR PERFORMED BY OVERSIZING THE HOLES (E,G,N) UNTIL CRACK REMOVAL AND CUT OUT THE ESDR 2007FA0000956Bracket · inoperativeTHE RT MAIN LANDING GEAR WOULD NOT RETRACT INTO WHEEL WELL. PILOT REPORTED LOUD BANG HEARD AFTER RETRACTING OF GEAR. WHEN EXTENDING THE GEAR FOR LANDING, THE RT GEAR WOULD NOT INDICATE GREEN BUT WAS VISUALLY CONFIRMED DOWN. PILOT LANDED WITHOUT INCIDENT ANDSDR A6WA200740515Attach Fitting · damagedLT ELEVATOR NR 2 HYD SYSTEM PCU ATTACHMENT FITTING ASSY ON ELEVATOR, P/N 601R24056-443, HAS SHEARED LOCK FASTENER AFT BOTTOM OF LINK. IAW SRM 51-42-21. (M)SDR A6WA200740514Attach Fitting · damagedLT ELEVATOR NR 1 HYD SYSTEM PCU ATTACHMENT FITTING ASSY ON ELEVATOR, P/N 601R24056-45, HAS SHEARED LOCK FASTENER AT BOTTOM OF LINE. 10-25-07 MAINTENANCE REPLACED LOCK FASTENER IAW SRM 51-42-21. (M)SDR 07FDEA03953Tee Fitting · corrodedAFTER BUSHING REMOVAL, LEFT HAND WING INBOARD FLAP VANE INBOARD TEE FITTING BORE FOUND CORRODED. LEFT HAND WING INBOARD FLAP VANE INBOARD TEE FITTING REMOVED AND REPLACED AS PER AMM 27- 50-22-4. FLAP OPERATION TEST CARRIED OUT AS PER AMM 27-50-00-860-80SDR 07FDEA03952Tee Fitting · corrodedAFTER BUSHING REMOVAL, RIGHT WING INBOARD FLAP VANE OUTBOARD TEE FITTING BORE FOUND CORRODED. RIGHT WING INBOARD FLAP VANE OUTBOARD TEE FITTING REMOVED AND REPLACED AS PER AMM 27-50-22-4.SDR 07FDEA03951Tee Fitting · corrodedAFTER BUSHING REMOVAL, RIGHT WING INBOARD FLAP VANE INBOARD TEE FITTING BORE FOUND CORRODED. RIGHT WING INBOARD FLAP VANE INBOARD TEE FITTING REMOVED AND REPLACED AS PER AMM 27-50-22-4.SDR 07FDEA03793Fitting · wornLEFT WING DIAGONAL BRACE ATTACH FITTING (WING SIDE) HAS MIGRATING BUSHINGS. REMOVED, FABRICATED AND REPLACED MIGRATED BUSHINGS IN ACCORDANCE WITH FEDEX EA NR F-5720-110765, DATED 7/30/2007 AND MAE TRAVELER NR T7/695654. CLASSIFIED AS A "MAJOR REPAIR" WITH NSDR 07FDEA03792Fitting · wornRIGHT WING DIAGONAL BRACE ATTACH FITTING (WING SIDE) HAS MIGRATING BUSHING. REMOVED, FABRICATED AND REPLACED MIGRATED BUSHINGS IN ACCORDANCE WITH FEDEX EA NR F-5720-110765, DATED 7/30/2007 AND MAE TRAVELER NR T7/695654. CLASSIFIED AS A "MAJOR REPAIR" WITH NSDR 07FDEA03791Bracket · crackedLT WING T/E PANEL BRACKET IS CRACKED, 2 EA. PLACES ABOVE AND JUST INBOARD OF THE NR 7 SPOILER ACTUATOR REPLACED PANEL BRACKET AS PER SRM 51-30-02, AT WBL 71 TO 153, LT. THIS IS CLASSIFIED AS A MINOR REPAIR.SDR CA070907003Attach Fitting · faulty(CAN) AD 96-18-02 AND THE AIRWORTHINESS LIMITATIONS FOR THIS AC REQUIRE THAT THE WING SPAR/STRUT ATTACH FITTINGS BE REMOVED AND NDI WITH FLUORESCENT DYE PENETRANT EVERY 1000 HOURS. NDI DISCLOSED A FLAW WITHIN THE METAL, APPARENTLY EXISTING WITHIN THE RAW STOCSDR 07FDEA03278Fitting · corrodedFOUND HEAVY CORRODED FITTING ON RT WING IN KRUEGER FLAP AREA, FRAME 38-39. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 57-45-11.SDR 07FDEA03277Bracket · corrodedFOUND HEAVY CORRODED BRACKET ON RT WING IN KRUEGER FLAP AREA, FRAME 38-39. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 57-45-11.SDR 07FDEA03276Bracket · corrodedFOUND HEAVY CORRODED BRACKET ON RT WING IN KRUEGER FLAP AREA, FRAME 38-39. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 57-45-11.SDR 07FDEA03275Bracket · corrodedFOUND HEAVY CORRODED BRACKET ON LT WING IN KRUEGER FLAP AREA, FRAME 38-39. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 57-45-11.SDR 07FDEA03274Fitting · corrodedFOUND HEAVY CORRODED FITTING ON LT WING IN KRUEGER FLAP AREA, FRAME 38-39. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 57-45-11.SDR 199WA0830007Attach Fitting · crackedLEFT HAND UPPER FWD WING ATTACH FITTING (INBOARD) WAS FOUND WITH CRACK DURING DYE PENETRANT INSPECTION IN ACCORDANCE WITH SRM AND AD 92-15-13. CRACK WAS ON THE TOP OF THE FITTING WRAPPING AROUND INTO THE COUNTER BORE RADIUS WITH THREE MICRO CRACKS NEXT TO IT.SDR 07FDEA03194Fitting · crackedFOUND SEVERAL HOLES WITH CRACKS AT C47 REAR SPAR INTERNAL ANGLE FITTING. REPAIR PERFORMED BY REAM UP THE HOLES UNTIL CRACK REMOVAL, INSTALLING BUSHINGS AND CUT OUT THE LT INTERNAL ANGLE FITTING IN AREA OF HOLE NR 1 LT IAW EA 6-5710-101281 AND RAS/046699/025/2SDR SWIA200718858Bracket · crackedBRAKE TRANSDUCER IN LEFT WHEEL WELL IS CRACKED, FOUND AT C-CHECK. INSTALLED BRAKE TRANSDUCER BRACKET PER CRJ200 SRM 51-42-06 PG 1-18.SDR SWIA200718857Bracket · crackedBRAKE TRANSDUCER IN RIGHT WHEEL WELL IS CRACKED, FOUND AT C-CHECK. INSTALLED BRAKE TRANSDUCER BRACKET PER CRJ200 SRM PGS 4-14.
SDR UPS07850665Fitting · crackedINSPECTION TYPE:C2 LEFT INBOARD FLAP ACTUATOR FITTING IS CRACKED, STA 97. REMOVED AND REPLACED LEFT INBOARD FLAP ACTUATOR FITTING AT STA 97 IAW DWG 7981564, AND DC8 AMM 20-16-00.SDR 07FDEA02869Bushing · misalignedRT WING OUTBOARD UPPER LINK FITTING HAS MIGRATING BUSHINGS. REMOVED BUSHINGS PER SOPM 20-50-03. INSPECTED FITTING PER NTM 51-00-00, PT.6, NO DEFECTS NOTED. HONED, CHAMFERED FLAP PEENED AND SWAGED PER F-5450-108892 FINAL DIA OF THE LUG BORE IS 1.7507. TRESDR 07FDEA02704Fitting · corrodedLT WING LOWER WINGLET AFT FITTING FORWARD AND AFT HOLES FOUND CORRODED. [08-17-07] REPAIRED AS PER FEDEX EA 1-5730-114787, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 07FDEA02703Fitting · corrodedRT WING LOWER WINGLET AFT FITTING FORWARD AND AFT HOLES FOUND CORRODED. [08-17-07] REPAIRED AS PER FEDEX EA 1-5730-114786, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR COEA0705901Mount Fitting · damagedDAMAGE FOUND DURING HEAVY CHECK. LT WING AILERON HINGE FITTING AT RIB 24 ACCIDENTAL DAMAGE AT IB AND OB LUGS. DAMAGE BLENDED OUT IAW ATR/SRI DO/TS-3041/07-8984 WITH REFERENCE TO SRAS DO/ TS-3041/07 4181. (K)SDR COEA0704901Mount Fitting · corrodedDAMAGE TO LT WING REAR SPAR AILERON CENTER MOUNT LUG FOUND DURING HEAVY CHECK IN COE. REMOVED MOUNT AND BLENDED DAMAGE, FOUND BLENDED AREA TO BE OUT OF LIMITS. NEW FITTING WAS FABRICATED AND INSTALLED IAW ATR42 SRM. (K)SDR AWXA200700899Fitting · corrodedSAL - MAJOR REPAIR- BC-6 CHECK - NR 5964268, 5964269, 5964270 AND 5964344, CORROSION FOUND ON HOLE 52, 53, AND 54 OF LT MAIN LANDING GEAR ANCHORAGE FITTING ON LT WING INNER REAR SPAR BETWEEN RIB 2 TO RIB 5. CORROSION REMOVED FROM HOLE 52, 53, AND 54 OF LT MASDR DHL2007784505Support · crackedNR 6 K-FLAP ACTUATOR SUPPORT IS CRACKED AT INBD CORNERS, W/S 304. REMOVED NR 6 K-FLAP ACTUATOR TRUNNION SUPPORT ANGLES INBD AND OUTBD IAW B727 SRM 51-30-2. FABRICATED SUPPORT ANGLES FROM 7075T6, .071, 8.25 BY 6.25 IAW B727 SRM 57-20-2, FIG 1 AND 51-20-1, FIGSDR IXXA07SMN182SBracket · crackedDURING ROUTINE C CHECK INSPECTION, FOUND NUMBER 1 ALT FUEL TANK BOOSTER PUMP SUPPORTS CRACKED AT STRINGER 59 STATION XW 456.000. REMOVED CRACKED BRACKET. INSTALLED NEW BRACKET AT STATION XW 456.000, STRINGER 59 IAW DC8 SRM 51-1-20D AND 51-3-1.SDR DHL2007785005Support Fitting · crackedNR 8 SPOILER ACTUATOR SUPPORT FITTING IS CRACKED. REMOVED FITTING AND REPLACED WITH NEW FITTING PER B727 SRM 51-30-2 FIG 1, FIG 15, AND B727 MM 27-61-91.SDR 2007UALA02267Bolt · incorrectNR 1 LEADING EDGE SLAT INTRANSIT LIGHT IS ILLUMINATED WITH FLAPS UP. ROOT CAUSE UNKNOWN. FOUND INCORRECT LEADING EDGE SLAT ACTUATOR ROD END BOLT. REPLACED NR 1 LEADING EDGE SLAT ACTUATOR AND ROD END BOLT.SDR 07FDEA02238Attach Angle · crackedRT WING O/B T/E UPPER SURFACE PANEL JUST INBD OF AILERON, JACKSCREW FAIRING ATTACH ANGLE CRACKED INSIDE FAIRING. REMOVED DAMAGED ANGLE, DRILLED UP, PRIMED AND PAINTED NEW ANGLE ON PANEL INBD OF AILERON, REF SRM 51-30-2.SDR 07FDEA02224Attach Bracket · crackedNR 5 FLAP TRACK FAIRING INBD MIDDLE ATTACH BRACKET IS CRACKED. REMOVED AND REPLACED BRACKET REF, FED EX J/C 76C07500 AND BOEING DWG 65-21795 AND SRM 51-30-2 PG 4&5.SDR ABXR070240Attach Fitting · corrodedFORWARD AND AFT SURFACE OF FIXED BRACE ATTACH LUG ON RIGHT TRUNNION WAS CORRODED. REPLACED TRUNNION ON JOB CARD 0317 AND EA 57430026.SDR ABXR070239Attach Fitting · corrodedFORWARD AND AFT SURFACE OF FIXED BRACE LUG ON LEFT TRUNNION WAS CORRODED. REPLACED TRUNNION ON JOB CARD 0317 AND EA 57430025.SDR 07FDEA02151Fitting · corrodedLT WING LOWER WINGLET AFT FITTING AFT HOLE FOUND CORRODED. [06-29-07] COMPLIED WITH FEDEX EA 1-5730-109909, CLASSIFIED AS MINOR REPAIR AS PER FEDEX GMM 6-2-100.
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