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 2009FA0000298Fitting · corrodedFOUND CORROSION ON 4 EA HOLES AND LUG FACES OF RT FRAME FITTING. REMOVED CORROSION AND INSTALLED REPAIR BUSHINGS IAW ARP-TPR-09-0014-04B. (K)SDR FDEA200904091247Fitting · corrodedCORROSION-INBD FLAP INBD TRACK NR 1 SUPPORT FITTING LOWER AFT HOLE. RT WING INBOARD FLAP INBOARD TRACK NR 1 SUPPORT FITTING LOWER AFT HOLE REPAIRED AS PER EA 1-5750-127817. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200904091246Support Fitting · corrodedFOUND CORROSION INBD FLAP INBD TRACK NR 1 SUPPORT FITTING LOWER FWD HOLE. REPAIRED AS PER EA 1-5750-127817. REPIAR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200904091245Fitting · corrodedCORROSION INBD FLAP INBD TRACK NR 1 SUPPORT FITTING UPPER FWD HOLE. RT WING INBOARD FLAP TRACK NR 1 SUPPORT FITTING UPPER FORWARD HOLE REPAIRED AS PER EA 1-5750-127817, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR DU4R2009339Fitting · elongatedS/O NR 312003 NR 25711, DURING SCHEDULED INSPECTION FOUND RT WING FIXED L/E HAS ELONGATED HOLE AT FASTENER ATTACHMENT OF ROLLER RIB FITTING 65C26208-10 AT SS 31.135.SDR DLM88090627Support Fitting · crackedRT MLG DOOR ACTUATOR UPPER MOUNT TRAPEZOIDAL FITTING CRACKED AFT SIDE AT RADIUS. REPAIRED PER REPLACEMENT PER 51-30-05 ON NR 240818.SDR 2009FA0000269Bolt · failedWHILE REPLACING THE RT WING FWD WING BOLT AND BARREL NUT, HEARD A POP WHILE TIGHTENING THE NEW BOLT BEFORE REACHING FINAL TORQUE. REMOVED NEW BOLT/BARREL NUT AND FOUND THE THREADS DAMAGED AND PULLED-OUT OF BARREL NUT. THE BOLT WAS ALSO DAMAGED BUT APPEARED TO SDR DLM88090566Pulley Bracket · corrodedLT ELEVATOR PULLEY SECTOR BRACKET CORRODED. REPLACED BRACKET.SDR CA090324008Fitting · mismanufactured(CAN) DURING THE REPLACEMENT OF A (VALTBS1209-1R) WING STRUT GEAR ATTACH FITTING, THE OLD FITTING WAS COMPARED TO THE NEW FITTING AND IT WAS NOTED THAT THE HOLE PATTERNS DID NOT MATCH. THE NEW FITTING WOULD NOT FIT.SDR CA090324007Fitting · corroded(CAN) DURING A 800 HR INSP WINGS REMOVED FOR PAINT AND CORROSION WAS FOUND UNDER WING STRUT FITTING ON PN VALTBS1209-1R, REMOVED PART AND INSTALLED NEW ATTACH FITTING.SDR CA090402003Screw · missing(CAN) THE PILOT NOTED HIS AILERON CONTROLS WERE SLUGGISH DURING FLIGHT AND THE CONTROL WHEEL WAS OFF CENTER DURING LEVEL FLIGHT. DURING ROUTINE INSP IT WAS FOUND THAT THE UPPER AILERON PULLEY BRACKET SCREW AND NUT WERE MISSING. THE PULLEY BRACKET WAS SLIGHTLY SDR 2009FA0000238Fitting · crackedDURING PHASE DEPOT INSP THE LWR FWD LT RING FITTING, PN 903220-1 WAS FOUND FRACTURED THRU THE HORIZONTAL BOTTOM FLANGE AT THE FILLET NUT PLATE HOLE AND HAD PROPAGATED ACROSS THE BOTTOM WEB AND UP THE VERTICAL THROUGH TWO FASTENERS; THE FIRST .1875 INCHAND THE SDR FDEA200903140917Attach Fitting · crackedLT UPPER BULKHEAD LUG CRACKED. REPAIRED AREA IAW SRM 57-20-00, FIG 38, STEP 1-6 AND 11/12, VOL I.SDR FDEA200903060855Lug · corrodedRT WING MLG BAY RIB NR 5 FWD LUG HAS CORROSION IN HOLE BORE AND ON FWD AND AFT SPOTFACE. REMOVED LEVEL 1 CORROSION AND REPAIRED RT RIB NR 5 LUG IAW EA 6-5710-124226 .SDR FDEA200903060854Lug · corrodedLT WING MLG BAY RIB NR 5 FWD LUG HAS CORROSION IN HOLE BORE AND ON FWD AND AFT SPOTFACE. REMOVED LEVEL 1 CORROSION AND REPAIRED LT RIB NR 5 LUG IAW EA 6-5710-124226.SDR 2009FA0000180Fitting · corrodedREPORTED TO MFG IAW INSTRUCTIONS STIPULATED IN THEIR SUPPLEMENTAL INSPECTION DOCUMENTS FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. FOUND RT LOWER FWD FITTING CORRODED. REPLACED FITTING PN 0811350-10.SDR 2009FA0000179Fitting · corrodedREPORTED TO MFG IAW INSTRUCTIONS STIPULATED IN THEIR SUPPLEMENTAL INSPECTION DOCUMENTS FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. FOUND LT LWR FWD FITTING CORRODED. REPLACED FITTING PN 0811350-10.SDR FDEA200903020781Attach Fitting · corrodedRT WING OTBD FLAP VANE NR 2 FROM INBD TRACK FITTING ATTACH BORE FOUND WITH CORROSION. COMPLIED WITH E.A. 1-5750-127473. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.SDR FDEA200903020778Attach Fitting · corrodedLT WING OTBD FLAP VANE NR 2 TRACK FITTING ATTACH BORES FOUND WITH CORROSION. COMPLIED WITH EA 1-5750-127466. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR FDEA200902270753Attach Bracket · crackedNR 8 SLAT ACTUATOR INBD AND OTBD ATTACH BRACKET INSIDE PLATES ARE CRACKED. REMOVED I/B & O/B BRACKETS AT NR 8 SLAT ACTUATOR IAW EA 7-5750-126801 AND SRM 51-30-2 AND S.B. B727-57-0130. FABRICATED 2EA. STEEL DOUBLERS AND 2EA. WEBS IAW EA 7-5750-126801 AND S.B. SDR 2009FA0000119Fitting · corrodedPREVIOUSLY REPORTED IAW INSTRUCTIONS BY MFG SUPPLEMENTAL INSPECTION DOCUMENTS FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. THE RT WING LWR FWD ATTACH FITTING PN0811350-10 FAILED NDT INSPECTION. REPLACED WING FITTING.SDR 2009FA0000118Fitting · misrepairedPREVIOUSLY REPORTED IAW INSTRUCTIONS BY MFG SUPPLEMENTAL INSPECTION DOCUMENTS FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. THE RT WING UPPER FWD ATTACH FITTING PN 0822550-30 HAD UNAPPROVED STEEL BUSHING UNABLE TO PERFORM NDT INSPECTION. REPLACED WING FITTINGSDR CA090227009Attach Fitting · corroded(CAN) DURING AN INSP, A TECH FOUND LIGHT CORROSION ON STEEL WING STRUT ENDS. STRUTS REMOVED DECORRODED AND REPAINTED. PRIOR TO REINSTALLATION OF STRUTS, STRUT ATTACH LUGS CLEANED AND INSPECTED. DURING INSP THE TECH FOUND CORROSION LINES IN FWD FACE OF REAR ATSDR FDEA200902170562Attach Bracket · brokenFAIRING 632 BB RIGHT AFT ATTACH BRACKET, SAFETY WIRE ATTACH POINT IS BROKEN. SAFETY WIRED BOLTS PER EA 6-5750-127916.SDR FDEA200902170561Attach Bracket · brokenFAIRING 635 BB LEFT AFT ATTACH BRACKET, SAFETY WIRE ATTACH POINT IS BROKEN. SAFETY WIRED BOLTS PER EA 6-5750-127916. NO FURTHER ACTION IS REQUIRED.SDR FDEA200902170560Attach Bracket · brokenFAIRING 636 BB LEFT AND RIGHT AFT ATTACH BRACKETS, SAFETY WIRE ATTACH POINTS ARE BROKEN. COMPLIED WITH E.A. 6-5750-127916.SDR WRLA2009044Tee Fitting · crackedDURING C-CHECK IN TPE INSPECTION FOUND LT WING I/B AILERON LEADING EDGE O/B SIDE HAD TEE CHORD CRACKED AT XORS 412.369. REPLACED WITH NEW TEE CHORD IAW SRM VOL II 51-33-01 REV 40.
SDR DL76S090180Fitting · crackedFOUND AT PSV21 RT OB FLAP DEFLECTION CONTROL TRACK FITTING CRACKED. REPLACED FITTING.SDR FDEA200902040447Fitting · crackedFITTING CRACKED. REPAIRED AREA IAW SRM 57-00-01, FIG 11, VOL I.SDR SWIA200921803Support · crackedC-CHECK, SUPPORT FOR FORWARD END OF FLAP ACTUATOR CRACKED. REPLACED PER SRM.SDR FDEA200901290386Angle · crackedRIGHT WING LOWER CHORD ANGLE CRACKED AT NR 8 SPOILER FITTING.SDR AALA2009012300019Fitting · crackedGROUND SPOILER ACTUATOR FITTING CRACKED INBOARD SIDE. NEW 8130 SPOILER CASTING INSTALLED PER SRM 57-00 AND SRM 51-30-00.SDR FDEA200901160226Rib · crackedLEFT WING RIB 5 FWD ATTACHMENT FLANGE AT THE AFT SPAR HAS A CRACK INDICATION AT HOLE "N". STARTED REAMING HOLE "N" TO 0.816. COLD WORKED HOLE "N" USING STDN 26-2-N TOOLING. FINAL REAMED HOLE "N" TO 843. ROTOPROBE INSPECTED HOLE IAW NTM 51-10-01. INSTALLEDSDR FDEA200901160225Rib · crackedLEFT WING RIB 5 FWD ATTACHMENT FLANGE AT THE AFT SPAR HAS A CRACK INDICATION AT HOLE "L". STARTED REAMING HOLE "L" TO 0.816. COLD WORKED HOLE "L" USING STDN 26-2-N TOOLING. FINAL REAMED HOLE "L" TO 843. ROTOPROBE INSPECTED HOLE IAW NTM 51-10- 01. INSTALLSDR FDEA200901160224Fitting · crackedLEFT WING RIB 5 FWD ATTACHMENT FLANGE AT THE AFT SPAR HAS A CRACK INDICATION AT HOLE "N". STARTED REAMING HOLE "N" TO 0.816. COLD WORKED HOLE "N " USING STDN 26-2-N TOOLING. FINAL REAMED HOLE "N" TO 843. ROTOPROBE INSPECTED HOLE IAW NTM 51-10-01. INSTALLSDR FDEA200901160223Fitting · crackedLEFT WING PICK-UP FITTING AT THE AFT SPAR, RIB 4 HAS A CRACK INDICATION AT HOLE "E". STARTED REAMING HOLE "E" TO 0.723. COLD WORKED HOLE "E" USING STDN 26-2-N TOOLING. FINAL REAMED HOLE "E" TO 0.750. ROTOPROBE INSPECTED HOLE IAW NTM 51-10-01. INSTALLED NESDR FDEA200901160222Fitting · crackedLEFT WING PICK-UP FITTING AT THE AFT SPAR; RIB 4 HAS A CRACK INDICATION AT HOLE "C". STARTED REAMING HOLE "C " TO 0.666. COLD WORKED HOLE "C" USING STDN 26-2-N TOOLING. FINAL REAMED HOLE "C" TO 0.687. ROTOPROBE INSPECTED HOLE IAW NTM 51-10-01. INSTALLED NSDR FDEA200901160221Fitting · crackedLEFT WING PICK UP FITTING AT THE AFT SPAR RIB 4 HAS A CRACK INDICATION AT HOLE "A". STARTED REAMING HOLE "A" TO 0.973. COLD WORKED HOLE "A" USING STDN 26-2-N TOOLING. FINAL REAMED HOLE "A " TO 1.00. ROTOPROBE INSPECTED HOLE IAW NTM 51-10- 01. INSTALLED NSDR CMRR200901001Bolt · wrong partWING/FUSELAGE REAR SPAR CONNECTION HAS IMPROPER BOLTS INSTALLED FROM THE MFG. NOTICED FUEL LEAK FROM AROUND BOLTS AND CONFIRMED FROM THE MFG THAT IMPROPER BOLTS WHERE INSTALLED IAW THE DESIGN DRAWINGS. THE BOLTS INSTALLED WHERE A D23 AND SHOULD HAVE BEEN A DSDR DHLA7432009648Attach Fitting · crackedLT WING NR 7 SPOILER ACTUATOR SUPPORT FITTING CRACKED. REPLACED NR 7 SPOILER ACTUATOR SUPPORT FITTING IAW B727 SRM 51-10-1 PARA 7. INSTALLED RIVETS, LOCK FASTENERS, BOLTS IAW B727 SRM 51-30-2 PARA 4B, PARA 7D AND PARA 9B.SDR FDEA200812115121Bracket · crackedRT WING NR 7 SLAT ACTUATOR MOUNTING BRACKETS BOTH INBD AND OTBD ON WING SIDE ARE CRACKED AT WS 635. REMOVED AND REPLACED INBD AND OTBD NR 7 SLAT ACTUATOR MOUNTING BRACKETS AND STEEL DOUBLERS IAW FEDEX EA 7-5750-126869, WINGS, RT NR 7 SLAT STA 281.4 AND 288.6 SDR AALA20081094Fitting · crackedCRACK IN GROUND SPOILER ACTUATOR FITTING LEFT WING. REPAIRED PER AARD 57-20-00-15 AND ESO 80559 DATED 12-05-08.SDR USAA2008121992282Support Fitting · corrodedSAL - C17 - MAJOR REPAIR - CORROSION ON STABILIZER BEAM AFT SUPPORT FITTING AT LT MAIN LANDING GEAR. REPLACED STABILIZER BEAM AFT SUPPORT FITTING IAW AMM 57-15-00-4.SDR SWIA200821023Attach Fitting · crackedC-CHECK, RIGHT WING RIB NR 16 LOWER CLIP CRACKED. REPLACED PER SRM.SDR DHLA2008745693Attach Fitting · corrodedNR 1 T/E FLAP TRACK FWD ATTACH FITTING OTBD LUG CORRODED. ACCOMPLISHED REPAIR TO LUG BORE IAW COOPESA EO COO-2-57-335-08 DATED 10/04/08 AND BOEING MSG 1-1000885726-2 DATED 10/02/08. REF FAA FORM 8100-9 DATED 11/5/08 AND ASTAR EVA B257-00144 FOR REPAIR APPROVSDR FCP2008F00000Attach Fitting · crackedWHILE COMPLYING WITH AD AD 91-12-10 AMENDMENT 39-7021, FOUND THE LT WING PANEL LOWER FORWARD ATTACH POINT HAD A .125 INCH CRACK.SDR COMA0860453Fitting · crackedLT MLG SIDE STAY ACTUATOR UPPER FITTING CRACKED. R&R SERVICEABLE LT SIDE STAY ACTUATOR UPPER FITTINGS.SDR S9BA2008031Clamp · looseON PREFLIGHT FUEL ODOR NOTICED IN CABIN. FOUND CLAMP AT FWD RT FUEL CELL NIPPLE LOOSE. TIGHTENED CLAMP AND CHECKED FOR LEAKS. NO LEAKS NOTED. REQUEST CHECK FLIGHT TO CHECK FOR FUEL SMELL IN CABIN. CHECK FLIGHT WAS SATISFACTORY.SDR USAA920081962Attach Angle · crackedCLT Q5 MAJOR REPAIR NR 03052980086/002 CRACK ON LT WING LOWER SKIN ATTACH ANGLE AT WBL 135.5, 6 INCHES FORWARD OF REAP SPAR. REPAIRED LT WING LOWER SKIN ATTACH ANGLE AT WBL 135.5, 6 INCHES FORWARD OF REAR SPAR IAW US AIRWAYS EA NR 100682.SDR 08FDEA04449Lug · corrodedWHILE COMPLYING WITH EO 6-5710-7-5010 CORROSION WAS FOUND ON BOTH LEFT AND RIGHT WING RIB 5 FORWARD LUG. COMPLIED WITH EA 6-5710-125482 IN THE REMOVAL OF CORROSION ON THE AFFECTED AREAS IN ACCORDANCE WITH EO 6-5710-7-5010.
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