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.

SDR QXEA200601674Tee Fitting · damagedYYC C3 LEFT HAND UPPER CENTER WING ACCESS PANEL T-FITTINGS P/N 85713349 HAVE AREAS OF SCRATCHES AND CORROSION (YW79.70, YW117-50, YW157.825). REPAIRED IAW RD 8/4-57-526 DHC-8-400 SRM 51-40-07-320-801, 51-23-20-390-801 AND 51-40-15-370-801.Jun 9, 2006 · N425QX · Bombdr DHC8402SDR QXEA200601680Tee Fitting · damagedYYC C3 LEFT HAND AND RIGHT HAND WING HAVE DAMAGE T-FITTINGS AT YW117.5 LEFT HAND AND YW157.825 RIGHT HAND WITH CORRODED BORE HOLES. REPAIRED IAW RD 8/4-57-647, ISSUE 1 AND EA 6-57-470.Jun 8, 2006 · N425QX · Bombdr DHC8402SDR AWXA200601240Fitting · corrodedSAL - MAJOR REPAIR - CHECK NO. C7. NR NO. 5910102. CORROSION ON THE HOLE AROUND NO. 78 OF ACTUATING CYLINDER ANCHORAGE LEFT WING. CORROSION AROUND HOLE NO. 78 OF ACTUATING CYLINDER ANCHORAGE LEFT WING WAS REMOVED IAW PART A OF AWA ERN. 26 - 5721 - 06181 - ES2.Jun 2, 2006 · N605AW · Airbus A320232SDR AALA20060436Flange · damagedAFW - RIGHT WING INBOARD AILERON SUPPORT AT WING STATION 431.97 HAS DAMAGE AND VERTICAL FLANGES, LOWER HORIZONTAL FLANGES. AREA OF DAMAGE IS ONE INCH AND 0.6 INCH WITH A DEPTH OF .108 AND .098. REPAIRED PER ENGINEERING SPECIFICATION ORDER.Jun 1, 2006 · N353AA · Boeing 767323SDR 06FDEA2015Support Fitting · corrodedRIGHT WING O/B FLAP I/B HINGE SUPPORT FITTING AFT NR 1 BOLT HOLE FOUND CORROSION. REMOVED AND REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT AND OPERATIONAL CHECK CARRIED OUT AS PER AMM 27-50-00-5, FOUND SATIS.May 26, 2006 · N596FE · Doug MD11SDR 06FDEA2014Support Fitting · corrodedRIGHT WING O/B FLAP I/B HINGE SUPPORT FITTING O/B NR 3 BOLT HOLE FOUND CORROSION. REPAIRED AS PER FEDEX EA 1-5750-99659. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.May 26, 2006 · N596FE · Doug MD11SDR 06FDEA2013Support Fitting · corrodedLT WING O/B FLAP I/B HINGE SUPPORT FITTING O/B NR 3 BOLT HOLE FOUND CORROSION. REMOVED AND REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT AND OPERATIONAL CHECK CARRIED OUT AS PER AMM 27-50-00-5, FOUND SATIS.May 26, 2006 · N596FE · Doug MD11SDR QXEA200601336Clip · looseFUEL CELL OPENING 624AT HAS A LOOSE CLIP TO BOTTOM SKIN AT MID POSITION. RIVETS REMOVED, HOLE REAMED FOR HILOCK INSTALLATION, HLT418-6-4 INSTALLED, BUT THERE IS NO SUPPORTING DATA TO ALLOW HILOCK USE IN THIS AREA. MAINTENANCE REMOVED CLEAT AND REINSTALLED SAMEMay 18, 2006 · N406QX · Bombdr DHC8402SDR 06FDEA1936Bracket · corrodedRIGHT WING, OUTBOARD FLAP, INBOARD FLAP HINGE, FORWARD FITTING INBOARD AFT HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-97759, WINGS RT OUTBOARD TRAILING EDGE FLAP, INBD BRACKET OUTBD FORWARD AND INBD AFT ATTACHMENT BORE CORROSION REPAIR. REPAIR CLASSIMay 16, 2006 · N599FE · Doug MD11SDR 06FDEA1935Bracket · corrodedRIGHT WING OUTBOARD FLAP, INBOARD FLAP HINGE, FORWARD FITTING OUTBOARD FORWARD HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-97759 WINGS RT OUTBOARD TRAILING EDGE FLAP. INBD BRACKET OUTBD FORWARD AND INBD AFT ATTACHMENT BORE, CORROSION REPAIR. REPAIR May 16, 2006 · N599FE · Doug MD11FSDR 06FDEA1914Fitting · corrodedRIGHT WING - OUTBOARD FLAP, INBOARD HINGE FITTING OUTBOARD LOWER BORE HOLE FOUND CORRODED. RIGHT WING OUTBOARD FLAP ASSEMBLY REMOVED AND REPLACED AS PER MM 27-50- 30-4 AND FLAP ADJUSTMENT CARRIED OUT AS PER MM 27-50-00-830-805. FLAP SYSTEM RANGE OF MMay 13, 2006 · N599FE · Doug MD11FSDR QXEA200602243Attach Fitting · corrodedYYC: LT WING, L/E 513AL, UPPER ATTACHMENT STRIP IS CORRODED. MAINTENANCE REPAIRED IAW SRM TASK 51-14-00-350-803, SRM 51-42-05-330-801, SRM 51-21-10-380-801 AND SRM 51-25-95-370-801.May 12, 2006 · N424QX · Bombdr DHC8402SDR 06FDEA1830Attach Fitting · brokenLT O/B AILERON ATTACHMENT STUDS BROKEN AND HEAVILY CORRODED. REMOVED 4 STUDS AND CLEANED OLD SEALENT AROUND THE HOLES AFSR 45 QC 47028 OK TO INSTALL 4 NEW STUDS QC 67028. INSTALLED 4 NEW STUDS AS PER EA-5740-7-5000 PT1 STEP 9 AFS 69 QC 97972. PEFORMED FINAMay 11, 2006 · N393FE · Doug DC1010FSDR 06FDEA1738Attach Fitting · unknownN01182 COMPLY WITH EO 7-5710-7-2314D PT5- WINGS MLG TRUNION ATTATCH FITTING MODIFICATION SB 727-57A0132R3 AD 2004-18-08, LT SIDE. COMPLIED WITH FED EX EO 7-5710-7-2314D PT 5 AND FED-EX EA 7-5710-96632.May 8, 2006 · N192FE · Boeing 727100SDR 2006FA0000493Fitting · crackedDURING ANNUAL INSP FOUND LT STUB WING AFT SPAR, UPPER FITTING CRACKED AT OB BOLT HOLE. FOUND NO CORROSION OR STRESS IN SURROUNDING AREAS. SUSPECT BOLT WAS OVERTORQUED. (K)May 4, 2006 · N352TS · Cessna 414SDR 06FDEA1677Attach Fitting · corrodedCORROSION OUTBOARD HINGE (WING SIDE) SIDE LINK ATTACHMENT SPOT FACE OF OUTBOARD FLAP IN RIGHT WING. REPAIRED AS PER CMM 57-44-09 PAGE 402-408 AND EA 1-5750-94688.May 2, 2006 · N526FE · Doug MD11SDR 06FDEA1676Attach Fitting · corrodedCORROSION OUTBOARD HINGE (WING SIDE) SIDE LINK ATTACHMENT BARREL NUT BORE OF OUTBOARD FLAP IN RIGHT WING. REPAIRED AS PER CMM 57-44-09 PAGE 402-408 AND EA 1-5750-94688.May 2, 2006 · N526FE · Doug MD11SDR 06FDEA1675Attach Fitting · corrodedCORROSION OUTBOARD HINGE (WING SIDE) ACTUATOR ATTACHMENT OUTBOARD BORE OF OUTBOARD FLAP IN RIGHT WING. REPAIRED AS PER CMM 57-44-09 PAGE 402-408 AND EA 1-5750-94688.May 2, 2006 · N526FE · Doug MD11SDR 06FDEA1674Attach Fitting · corrodedCORROSION OUTBOARD HINGE (WING SIDE) ACTUATOR ATTACHMENT INBOARD BORE OF OUTBOARD FLAP IN RIGHT WING. REPAIRED AS PER CMM 57-44-09 PAGE 402-408 AND EA 1-5750-94688.May 2, 2006 · N526FE · Doug MD11SDR 06FDEA1673Attach Fitting · corrodedCORROSION INBOARD HINGE (WING SIDE) SIDE LINK ATTACHMENT SPOT FACE OF OUTBOARD FLAP IN RIGHT WING. CORROSION REMOVED AS PER CMM 57-44-08 PAGE 612-615 AND FOUND WITHIN LIMIT AS PER DAG DRAWING ARC0502 AND REPAIRED AS PER CMM 57-44-08.May 2, 2006 · N526FE · Doug MD11SDR 06FDEA1672Attach Fitting · corrodedCORROSION INBOARD HINGE (WING SIDE) LOWER ATTACHMENT SPOT FACE OF OUTBOARD FLAP IN RIGHT WING. CORROSION REMOVED AS PER CMM 57-44-08 PAGE 602-605 AND FOUND WITHIN LIMIT AS PER DAG DRAWING ARC0502 AND REPAIRED AS PER CMM 57-44-08.May 2, 2006 · N526FE · Doug MD11SDR 06FDEA1671Attach Fitting · corrodedCORROSION INBOARD HINGE (WING SIDE) ACTUATOR ATTACHMENT OUTBOARD BORE OF OUTBOARD FLAP IN RIGHT WING. REPAIRED AS PER CMM 57-44-08 PAGE 602-607 AND EA 1-5750-94697.May 2, 2006 · N526FE · Doug MD11SDR 06FDEA1670Attach Fitting · corrodedCORROSION INBOARD HINGE (WING SIDE) ACTUATOR ATTACHMENT INBOARD BORE OF OUTBOARD FLAP IN RIGHT WING. REPAIRED AS PER CMM 57-44-08 PAGE 602-607 AND EA 1-5750-94697.May 2, 2006 · N526FE · Doug MD11SDR 2006FA0000403Bracket · crackedFWD WING ATTACHMENTS, LEFT & RIGHT WINGS, FWD & AFT BRACKETS WERE NEVER RIVETED TO TOP & BOTTOM WING SKINS & INBOARD RIB FLANGES ALLOWING ALL LOADING TO BE TAKEN BY BRACKET FLANGES & INBD WING RIBS. ALL 4 BRACKETS ARE CRACKED. PICTURES AVAILABLE. IT SEEMED MOApr 19, 2006 · N78LS · Piper PA60600SDR QXEA20061168Nut Plate · crackedPDX: FWD SPAR WING ATTACH BOLT LT INBOARD NUT PLATE DOME BUSHING SUSPECT CRACKED. VIEWED THROUGH ARMPIT PANEL 263AL. MAINTENANCE REPAIRED IAW NDTM PART 1, 51-00-06, HORIZON EA 6-57-449 AND NDTM PART 6, 51-00-02.Apr 17, 2006 · N405QX · Bombdr DHC8402SDR QXEA200601120Attach Angle · crackedPDX - C4 CENTER MOUNT ANGLE FOR WING DEICE TEE DUCT IS CRACKED AT RIGHT HAND END. REPAIRED IAW DHC-8-200 SRM 51-40-11 AND 51-40-00.Apr 16, 2006 · N356PH · Dhav DHC8202SDR DHL2006801551Fitting · crackedNR 1 ALT TANK FITTING CRACK 2.500" STA 408.000 S-59. PERFORMED MAJOR REPAIR IAW SRM 57-1-0. REMOVED CRACKED FITTING IAW SRM 51-1-21A. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. APPLIED TOP COATING MATERIAL TO AREA IAW SRM 51-1-12 PG 7-21. INSTALLEDApr 16, 2006 · N801DH · Doug DC873FSDR IXXA06RNG022SFitting · crackedDURING ROUTINE C CHECK, FOUND A CRACK ON THE OUTBOARD FLAP STATION XFS 339.723, INBOARD FITTING LEFT HAND. STOP DRILLED THE END OF THE CRACK. REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW EWO ATI 57-075. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR.Apr 15, 2006 · N823BX · Doug DC871FSDR 06FDEA1350Bracket · corrodedFOUND CORROSION LT WING O/B FLAP I/B HINGE FITTING (ARC1984) O/B NR 3 BOLT HOLE . CORROSION AT LT WING O/B FLAP I/B HINGE FITTING (ARC1984) O/B NR 3 BOLT HOLE. REPAIRED AS PER FEDEX EA NR 1-5750-95810, TITLE: "WINGS - LT OUTBOARD TRAILING EDGE FLAP, I/B BRACApr 10, 2006 · N595FE · Doug MD11SDR DHL2006801532Fitting · crackedNR 3 MAIN TANK FITTING 2" CRACK STA XRS 139.000 BETWEEN S-7 AND S-8. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND APPLIED TOP POLYURETHANE YELLOW COATING IAW SRM 51-1-12 PG 7-25. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-1. REFER TApr 10, 2006 · N801DH · Doug DC873FSDR DHL2006764506Attach Fitting · crackedL/WING INSIDE NR 4 SLAT LE ACTUATOR ATTACH POINT FOUND CRACK ON INNER SKIN AT WS 410. CUTOUT AREA AT L/WING INSIDE NR 4 SLAT LE ON INNER SKIN AT WS 410 DIM 10.5"X 5.250" IAW B727 SRM 57-30-4 FIG 3. FABRICATED FILLER MAT USED 2024T3 .040 PO# 9002787 AND DIM. Apr 6, 2006 · N764AT · Boeing 727264SDR UPS06146710Attach Fitting · crackedINSPECTION TYPE: 5YR, LT WING KRUGER BOX AREA CURVED DOUBLER FWD ATTACHING CLIP CRACKED. REMOVED AND REPLACED CLIP PER A300 SRM 51-40-00 AND 51-40-21.Apr 6, 2006 · N133UP · Airbus A300F4622RSDR DHL2006764510Angle · crackedLEFT WING LE WBL117.0 CHORD ANGLE CRACKED TO FWD END. REMOVED CHORD ANGLE AT LEFT WING LE WS117 IAW B727 SRM 51-30-2. FABRICATED NEW ANGLE MATERIAL USED 7075T6 .063 PO# 9003002 DIM. 46"X 2" IAW B727 SRM 57-20-2 FIG 1 AND MAT SUBSTUITION 51-20-1 FIG 2. LOCATApr 4, 2006 · N764AT · Boeing 727264SDR DHL2006764509Support Angle · crackedLEFT WING LE WBL117.0 LWR PANEL SUPPORT ANGLE SHOW CRACK BETWEEN FASTENER HOLES. NDT CONFIRM. REMOVED SUPPORT ANGLE AT LEFT WING LE WBL 117 LWR PANEL IAW B727 SRM 51-30-2. FABRICATED NEW ANGLE SUPPORT MATERIAL USED 7075T6 .050 PO# 9002787 DIM 18"X 1 3/4" IAApr 4, 2006 · N764AT · Boeing 727264SDR AWXA200600747Attach Fitting · galledDURING C12 CHECK DISCOVERED LUG SURFACES GALLED FROM BUSHING CONTACT ON THE INBOARD AND OUTBOARD SIDES OF LEFT WING INBOARD STRUT ATTACH FITTING FOR PYLON AT WBL 248L. MAINTENANCE REMOVED INBOARD BUSHING IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 19-5704Mar 28, 2006 · N910AW · Boeing 7572G7SDR 06FDEA1213Support Fitting · crackedRIGHT WING OUTBOARD FLAP OUTBOARD LOWER FASTENER HOLES COMMON TO INBOARD HINGE SUPPORT FITTING ARC4009 FOUND OUTBOARD LOWER HOLE REVEALED CRACK INDICATION. OUTBOARD LOWER HOLE AT RIGHT WING OUTBOARD FLAP OUTBOARD LOWER FASTENER HOLES COMMON TO INBOARD HINGE SMar 24, 2006 · N588FE · Doug MD11SDR 06FDEA1229Attach Fitting · corrodedNR 1 FLAP TRACK FWD FITTING I/B FACE IS CORRODED. *S/D* REPAIRED PER FED EX EA 7-5710-7-96574.Mar 24, 2006 · N492FE · Boeing 727200SDR 06FDEA1228Attach Fitting · corrodedNR 8 FLAP TRACK FWD FITTING IS CORRODED. *S/D* REPAIRED PER FED EX EA 7-5710-96574.Mar 24, 2006 · N492FE · Boeing 727200SDR UPS06846719Fitting · crackedINSPECTION TYPE:C3 STA 98 FLAP ACTUATOR REAR SPAR FITTING O/B LUG FOR SUPPORT LINK ARM IS BROKEN. FABRICATED AND INSTALLED NEW FITTING FROM 7050-T7451 PER AMS 4050 PLATE IAW UPS ENG FILE # DC8-57-20160, SAA EA#008-2760-01- A0133 REV A, DOUGLAS PSAMSL DWG 7981Mar 21, 2006 · N706UP · Doug DC871FSDR ABXA060148Fitting · crackedFOUND RIGHT WING FUEL, NR 6 STRINGER TIE INSIDE PANEL 505C CRACKED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D.Mar 13, 2006 · N813AX · Doug DC863SDR IXXA06SMN091SFitting · crackedDURING ROUTINE C CHECK INSPECTION, LEFT WING NR 2 MAIN TANK LOWER FORWARD FITTING CRACKED, AT STATION 74.000, STRINGER-50. REMOVED AND REPLACED CRACKED FITTING ON LEFT WING NR 2 MAIN TANK LOWER PART, STATION 74.000 S-50 IAW DC8 SRM 51-1-20D DC8 SRM 51-3-1.Mar 9, 2006 · N602AL · Doug DC873FSDR IXXA06SMN090SFitting · crackedDURING ROUTINE C CHECK INSPECTION, LEFT WING NR 2 MAIN TANK LOWER FITTING CRACKED, STA 220.00 STRINGER-59. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D. FABRICATED NEW FITTING (AL 7075 T6 51) IAW ATI REPAIR SPECIFICATION NR 2003-05 EA SEMAN NR 20061966 DATE Mar 9, 2006 · N602AL · Doug DC873FSDR QXEA200600712Support Angle · crackedYYC - C4 WING ISOLATION CHECK VALVE DUCT SUPPORT ANGLE LEFT HAND SIDE IS CRACKED, UNDER ACCESS PANEL 261GT FORWARD OF WING FRONT SPAR WING STATION 18L. REPAIRED IAW HORIZON AIR EA 2-53-706, 2-28-06 AND 2-53-705.Mar 8, 2006 · N350PH · Dhav DHC8202SDR UIEA200600017Fitting · shearedFOUND SHEARED HI-LOKS IN NR 4 PYLON AFT DIAGONAL BRACE FITTING.Mar 5, 2006 · N809MC · Boeing 747228FSDR 06FDEA0867Attach Fitting · corrodedDURING AIRPLANE'S CONVERSION FROM P TO F/ACF FOUND: RT WING, OUTBOARD FLAP, INBD ATTACH BRACKET, CORROSION ON LOWER ATTACK SURFACE, INSIDE THE BORES AND IN THE LATERAL BORE OF THE FITTING. REMOVED FAIRING ATTACHING STRUCTURE IAW SRM 51-35-01 VOL II. SENT OUFeb 28, 2006 · N568FE · Doug DC1010SDR CA060227015Mount · failedFLAP PULLEY MOUNT INSTALLED IN AFT FUSELAGE CABIN AS PER STC SA578AL AT UNKNOWN TIME, FAILED IN FLIGHT. MOUNT WAS WELDED TO FUSELAGE BRACE TUBE 5/8".035 WALL. TUBING FATIGUED AROUND WELD AND PULLEY MOUNT SHIFTED CAUSING MISALIGNMENT OF PULLEY TO CABLE. THISFeb 23, 2006 · Piper PA12SDR AALA20060135Attach Fitting · crackedAFW - NUMBER TWO SPOILER OUTBOARD HINGE ATTACH FITTING HAS SMALL CRACK ON LOWER OUTBOARD LEG. AREA OF CRACK IS 0.5 INCH BY 0.2 INCH WITH AT DEPTH OF 0.2 INCH. CRACK LENGTH IS 0.5 INCH. BLEND/ROUTE OUT CRACK. PERFORMED HIGH FREQUENCY EDDY CURRENT TO VERIFY Feb 22, 2006 · N362AA · Boeing 767323SDR 2006FA0000248Attach Bracket · crackedDURING A 6000 HOUR INSPECTION, THE LT AND RT WING TIP ASSEMBLIES WERE REMOVED TO FACILITATE FURTHER INSPECTION OF THE AILERON SYSTEM. AFTER REMOVAL OF THE TIPS THE INSPECTING TECHNICIAN NOTED CRACKS IN BOTH THE LT AND RT AILERON OB ATTACH POINTS. THE BRACKETFeb 21, 2006 · N701QD · Socata TBM700SDR 2006FA0000247Support Bracket · crackedDURING A 6000 HOUR INSPECTION, THE LT AND RT WING TIP ASSEMBLIES WERE REMOVED TO FACILITATE FURTHER INSPECTION OF THE AILERON SYSTEM. AFTER REMOVAL OF THE TIPS THE INSPECTING TECHNICIAN NOTED CRACKS IN BOTH THE LT AND RT AILERON OB ATTACH POINTS. THE BRACKETFeb 21, 2006 · N701QD · Socata TBM700SDR 2006FA0000246Attach Bracket · crackedDURING A ROUTINE PHASE INSPECTION, THE LT WING TIP ASSY WAS REMOVED TO FACILITATE FURTHER INSPECTION OF THE AILERON CABLE. AFTER REMOVAL OF THE TIP, THE INSPECTING TECHNICIAN NOTICED A CRACK IN AT THE OB ATTACH POINT. THE BRACKET WAS REMOVED AND INSPECTED WIFeb 21, 2006 · N703QD · Socata TBM700
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