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 ABXA000368Angle · crackedANGLE CRACKED AT LEFT WING LEADING EDGE SKIN SPLICE, STATION XRS 267. REPLACED ANGLE IAW DC9 SRM 51-30-5.Jul 27, 2000 · N965AX · Doug DC941SDR SWAA001402Fitting · corrodedDURING SCHEDULED D-CHECK, FOUND LT MLG SUPPORT BEAM STABILIZER LINK AFT FITTING CORRODED. REMOVED AND REPLACED FITTING PER MM.Jul 27, 2000 · Boeing 7372H4SDR UPS00233512Fitting · corrodedINSPECTION TYPE:SI, NR 6 FLAP TRACK SPOILER BEAM MOUNT FITTINGS CORRODED OUT OF LIMITS IAW SRM 51-30-2 ON RT WING. FOUND WHILE WORKING NRC 178771. REMOVED CORRODED MOUNT FITTINGS AND REPLACED WITH NEW PART IAW SRM 51-30-2.Jul 26, 2000 · N933UP · Boeing 72725CSDR UPS00833548Fitting · crackedINSPECTION TYPE:C123, LEFT WING AT XRS 90 HAS A CRACKED SPLICE FITTING AT STRINGER 16 TO FRONT SPAR. REMOVED, FABRICATED, AND REPLACED FITTING IAW DEG 3645275, AND SRM 51-1-20D.Jul 22, 2000 · N806UP · Doug DC873FSDR UPS00833628Fitting · damagedINSPECTION TYPE:C123, RIGHT WING L/E PAN FITTING HAS ELONGATED HOLES AT XS 520. REMOVED AND REPLACED FITTING IAW DWG 5769857 AND SRM 51-1-20D, 51-3-0.Jul 21, 2000 · N806UP · Doug DC873FSDR DHL200070962DFitting · crackedRT WING FRONT SPAR TERMINAL FITTING CRACKED IN BOTTLE PIN HOLE (APPROX 3 IN CRACK) VERIFIED BY HFEC. REMOVED LEADING EDGE PER SRM 51-30-2. REMOVED WIRING AS PER M/M 27-82-00. REMOVED FUEL LINE S PER M/M 28-22-0. PLACED A/C IN JIG POSITION PER SRM 51-50-1 AJul 7, 2000 · N709DH · Boeing 72782CSDR DHL200070959DFitting · damagedLEFT WING FWD TERMINAL PIN BORE DAMAGED. REMOVED PNEUMATIC DUCTS AND HYD LINES FOR ACCESS PER M/M 20-10-15. REMOVED L/E PER SRM 51-30-2. PERFORMED HFEC PER NDT MAN 6-51-00-00. NO CRACK NOTED. FLAP PEEN AREA PER DHL-00-00015F. INSTALLED BUSHINGS AND PIN PJul 7, 2000 · N709DH · Boeing 72782CSDR USAA000927Support Fitting · crackedCLT - FOUND SUPPORT FITTING CRACKED .200 INCH, RT WING LANDING GEAR BEAM. ACCOMPLISHED PART A PER TR 57-40-10. (M)Jul 3, 2000 · N244US · Boeing 737201SDR RRXA002718Retainer · misinstalledDURING A MAINTENANCE VISIT FOUND CANOE FITTING BOLT RETAINER INSTALLED ON WRONG SIDE OF FITTING AT STA 340, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW EO NR 00-107 WITH APPRJun 23, 2000 · N8084U · Doug DC871FSDR 20000626SH002Fitting · corrodedEXFOLIATION CORROSION AT LEAST .01 INCH TO .1250 INCH DEEP AND GROWING. SUBMITTER STATES THAT AIRCRAFT WAS BASED IN SAN FRANCISCO BAY AREA AND SALT AIR MAY HAVE CONDENSED INSIDE THE AIRCRAFT INSULATION AND DRIPPED DOWN ON THE FITTINGS. HOWEVER, SUBMITTER BELJun 13, 2000 · N3079L · Cessna 310JSDR AU000567Fitting · corroded(AUS) LEFT ABD RIGHT WING ATTACHMENT BLOCKS CONTAIN EXFOLIATION CORROSION.Jun 12, 2000 · Cessna 182SDR UPS00233385Pin · corrodedINSPECTION TYPE:C, RIGHT WING FRONT SPAR WING-TO-BODY FITTING BOTTLE PIN CORRODED. RIGHT WING FRONT SPAR WING-TO-BODY FITTING BOTTLE PIN REPLACED IAW B727 MM 57-41-01.Jun 10, 2000 · N917UP · Boeing 72730CSDR CA000621009Attach Fitting · corroded(CAN) LEVEL 3 CORROSION FOUND ON PLATE BETWEEN ATTACH POINTS.Jun 10, 2000 · Dhav DHC6200SDR RRXA002689Fitting · damagedDURING A MAINTENANCE VISIT FOUND A BROKEN TAB AND GOUGED FITTING ON THE 508 CAN''T WEB SUPPORT ATTACHMENT FITTING TO FRONT SPAR LOWER ATTACHMENT AT STA XCW 463, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-Jun 9, 2000 · N8084U · Doug DC871FSDR RRXA002715Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE CANOE FITTING ON THE RT WING AT STA 410, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8 AND EO NR 00-107 WITH APPROVED 8110-3 DATED 6-6-00. (CORROJun 8, 2000 · N8084U · Doug DC871FSDR RRXA002690Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE CANOE FITTING AT STA 410 LT WING, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8 AND EO NR 00-107 WITH APPROVED 8110-3 DATED 6-6-00. (CORROSION DAJun 8, 2000 · N8084U · Doug DC871FSDR LR7A0082Fitting · corrodedDURING SCHEDULED C2 INSPECTION PER JOB CARD HST 5713, FOUND CWS 220 RT CENTER WING UPPER AFT CORNER FITTING CORRODED. REPLACED FITTING PER SRM SMP 583-51-60.Jun 3, 2000 · N402LC · Lkheed 382GSDR RRXA002671Bracket · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE BRACKET AT BOTTOM ON THE L/E SECTION ABOVE NR 1 PYLON I/B AT STA 526, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DJun 1, 2000 · N8084U · Doug DC871FSDR 20000601SH022Fitting · corrodedON ANNUAL INSPECTION, LT WING AFT SPAR WING ATTACH FITTINGS, PN''S 5011023-1 AND 5-11024-1, INTERGRANULAR CORROSION FOUND IN AREAS READILY VISIBLE EACH AREA OF CORROSION APPROXIMATELY 1.50 SQUARE INCH AND APPROXIMATELY .1250 INCH DEEP. NO IDEA ON SPECIFIC CAJun 1, 2000 · N6672C · Cessna 414ASDR EIA2000162Fitting · crackedC2-CHECK, NR 1 NACELLE U/W DIAGONAL BRACE FITTING OUTBOARD FLANGE MOST AFT FASTENER HOLE FOUND CRACKED. FITTING REPLACED PER BSB-57-2288, BOEING MSG EVR-HKG-00-00108H, AND RS R57-04-34383. (M)May 29, 2000 · N470EV · Boeing 747273CSDR AWXA0000347Attach Fitting · damagedC-CHECK, NR 5 SPOILER I/B HINGE ATTACH FITTING HAS ELONGATED HOLES. REMOVED DAMAGE, FABRICATED, AND INSTALLED FREEZE PLUGS AND REPAIR STRAPS IAW ER 03-5722-00140-J54, TREATED AND PRIMED IAW 737 SRM 51-20-01.May 25, 2000 · N305AW · Boeing 7373G7SDR 2000UALA00280Bolt · crackedNR 1 PYLON O/B SIDE LOAD FITTING I/B BOLT HAD CRACK INDICATION. *S/D* BOLT MATERIAL IS H11 STEEL AND CRACK IS THE RESULT OF STRESS CORROSION, A CHARACTERISTIC OF H11 MATERIAL. INCONEL 718 BOLTS WERE INSTALLED PER PROCEDURES OUTLINED IN BOEING SERVICE BULLETMay 18, 2000 · N608UA · Boeing 767222SDR RRXA002685Attach Angle · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE L/E ABOVE NR 2 PYLON UPPER FORWARD FORMER ATTACH ANGLE AT STA XFS 256, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW May 15, 2000 · N8084U · Doug DC871FSDR COMA0060431Fitting · chafedTHE LEFT AILERON FLUTTER DAMPER FITTING LUG WAS DAMAGED BY A ROTARY CUTTER WHILE TRYING TO REMOVE THE BOLT OF THE FLUTTER DAMPER ATTACH POINT. REMOVED DAMAGED FITTING AND INSTALLED NEW FITTING IAW WVAC EO 601R-57-1304.May 7, 2000 · N926CA · Cndair CL6002B19SDR RRXA002196Fitting · chafedDURING A MAINTENANCE VISIT FOUND CHAFING AT THE RT WING FLAP PORK CHOP FITTING AT STA 219, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. ACCEPTABLE TO RETURN TO SERVICE PER EO NR 00-047 WITH APPROVED 8May 5, 2000 · N995CF · Doug DC862SDR EIA2000131Fitting · crackedFOUND CRACK REVEALED ON RT WING RIB SUPPORT FITTING AT WS 669.5 RIB, AT MOST FORWARD UPPER HOLE, APPROX .5 INCH LONG. RIB SUPPORT FITTING REPLACED PER BOEING SB 747-57-2273 REV 2 FIG 5 AND EO 57-747-1403-95. (M)Apr 21, 2000 · N482EV · Boeing 747212BSDR 20000523SH026Beam · crackedCRACK SEEMS TO ORIGINATE FROM A PUNCHED THROUGH .1250 INCH JIG HOLE, 2.50 INCHES OUT FROM REAR SPAR ATTACH BOLT. CAN BE SEEN FROM GEAR WALL .3750 INCH LONG CRACK. (X)Apr 14, 2000 · N14032 · Lakeac 250LAKESDR LR7A0040Fitting · crackedDURING SCHEDULED B2 INSPECTION PER JOB CARD HB0503, FOUND RT WING OWS 28.0 FLAP TRACK ATTACH FITTING CRACKED. REPLACED FITTING IAW LAC MEA 382-57-00-049 AND SRM SMP 583-51-70-1. NR 26212.Apr 4, 2000 · N403LC · Lkheed 382GSDR RRXA001971Fitting · chafedDURING A MAINTENANCE VISIT FOUND A CHAFED CANOE FITTING ON THE LEFT I/B FLAP O/B FITTING AT STA 98, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW EO NR 00-055 WITH APPApr 3, 2000 · N961R · Doug DC873FSDR RRXA001911Fitting · chafedDURING A MAINTENANCE VISIT FOUND CHAFING IN 2 PLACES AT RT WING NR 4 FLAP CANOE FITTING LWR I/B SIDE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. BLENDED AREAS TO ALLOWABLE LIMITS AND RETURNED TO SERApr 3, 2000 · N961R · Doug DC873FSDR RRXA001775Fitting · chafedDURING A MAINTENANCE VISIT, FOUND A CHAFED CANOE FITTING ON THE LWR I/B SIDE OF THE RT WING NR 4 FLAP, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. BLENDED AREAS SMOOTH AND RETURNED TO SERVICE IAWApr 3, 2000 · N961R · Doug DC873FSDR GAIA00153Fitting · damagedDURING HEAVY C-CHECK AT TIMCO/OSC, FOUND NR 5 FLAP TRACK FORWARD SUPPORT FITTING UPPER HOLE DAMAGED. REPLACED SUPPORT FITTING IAW 727 MM 27-51-31. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Mar 30, 2000 · N6808 · Boeing 727223SDR DL72K000568Beam · corrodedDURING OVERHAUL THE I/B FLAP, I/B TRACK ASSY TYPICAL CORROSION WAS FOUND AT THE MLG AND SPOILER BEAM ATTACH PADS AREAS AND WEAR AT THE FWD ATTACH LUGS AND TOGGLE DETENT HOLE. REPAIR PER ER/A 387256-14AD AND BF GOODRICH REPAIR NR 23-0592.Mar 24, 2000 · N410DA · Boeing 727232SDR CA000329016Bolt · cracked(CAN) CF 81-25R5 WAS BEING CARRIED OUT EARLY, 417.2 HRS. FOUND LEFT WING TOP REAR BOLT (P/N 81786-10-18) WAS INSPECTED AND FOUND CRACKED AND REJECTED. NEW BOLT INSTALLED.Mar 14, 2000 · Beech B100SDR CA000209008Fitting · cracked(CAN) DURING SCHELDULED NDT RT UPPER FWD ATTACH LUG FOUND CRACKED.Jan 28, 2000 · Lkheed 1329SDR RRXA000039Doubler · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, I/B FLAP O/B SCISSORS HUNGE AREA ATTACH ANGLE DOUBLER CRACKED. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8.Jan 17, 2000 · N792FT · Doug DC873FSDR CA000110067Window · failed(CAN) AFTER LANDING, WHILE TAXING, THE A/C WAS CAUGHT IN SEVERE WIND GUST. LT WING WAS LIFTED OFF THE GROUND, RT WING TIP CONTACTED THE RUNWAY, LT COCKPIT SIDE WINDOW SHATTERED. AWAITING CREW REPORT. UPDATEAS INFO COMES AVAILABLE.Jan 5, 2000 · Cndair CL6002B19SDR CA000110017Fitting · damaged(CAN) REMOVED FITTING FOR BEARING REWORK AND FOUND HIDDEN DAMAGE. THREE OF FOUR BOLTS FROZEN IN BORES, TWO BOLTS SHEARED, EVIDENCE OF EXTENSIVE CORROSION TO SHEAR FACE. FWD INBD BOLT CUT FOR REMOVAL. FITTING REPLACED.Dec 20, 1999 · Boeing 7372T7SDR CA991229044Attach Fitting · damaged(CAN) DAMAGE FOUND ON COUNTERBORE FITTINGS FACE OF UPPER AND LOWER AFT WING ATTACH POINTS.FOUND INCORRECT PART NUMBER WASHER, USED ON BOLT STACK-UP FOR AFT FITTINGS.Dec 17, 1999 · Beech B200SDR CA991230022Attach Fitting · nicked(CAN) DURING A PHASE 5 INSPECTION, A NICK WAS FOUND ON THE AFT LUG OF THE UPPER FWD WING ATTACH FITTING. FOLLOWING A REPAIR WHICH INCLUDED BLENDING OF THE AFFECTED AREA OF THE FITTING, AN EDDY CURRENT CHECKOF THE FITTING REVEALED FERROUS METAL INCLUSIONS AT SEDec 13, 1999 · Cessna 550SDR UPS99231131Fitting · corrodedINSPECTION TYPE:SI WHILE WORKING TASK CARD NR 1249 FOUND THE NR 4 FLAP TRACK FITTING THAT ATTACHES TO FWD LANDING GEAR TRUNION BEARING TO BE CORRODED. REPLACED FITTING PER SRM 51-30-4.Nov 12, 1999 · N950UP · Boeing 72725CSDR MWEA99697Vane · dentedLEFT INBOARD FIXED VANE HAS A SMALL DENT APPROX 24 INCHES FROM INBOARD END. MTC FABRICATED AND INSTALLED DOUBLER ON LEFT FIXED VANE.Oct 19, 1999 · N401ME · Doug DC932SDR 99ZZZX4104Fitting · corrodedSEVERE CORROSION OF LIFT STRUT ATTACH FITTING. FRONT OF FRONT SPAR IN RIGHT WING LOCATED UNDER LEADING EDGE COVERING CAUSED BY LACK OF ACCESS FOR INSPECTION.Oct 7, 1999 · N3088Z · Piper PA18A150SDR CA030417004Bushing · loose(CAN) MIGRATING BUSHINGS ON WING ATTACHMENT FITTINGS.Oct 4, 1999 · Cndair CL6002B19SDR CA991004030Fitting · damaged(CAN) FITTING REPLACED DUE TO EXCESSIVE TOOL DAMAGE.Sep 17, 1999 · Beech 99SDR CA991004029Fitting · cracked(CAN) ON SCHEDULED INSPECTION, INDICATIONS WERE PRESENT WHEN DOING LEVEL 2 LPI. FITTING REPLACED AND AIRCRAFT RETURNED TO SERVICE.Sep 16, 1999 · Beech 99SDR 99ZZZX3618Fitting · crackedINSPECTION OF LEFT MAIN GEAR WELL AREA FOUND WING ATTACH FITTINGS TO HAVE VERTICAL CRACKS APPROXIMATELY .50 INCH IN LENGTH BETWEEN RIVETS THAT ATTACH FITTING TO SPAR. THESE CRACKS ARE LOCATED IN THE WEB/RADIUS AREA OF THE FITTING ANGLE.Aug 5, 1999 · N600VF · Piper PA60600SDR 99ZZZX3181Bolt · misinstalledFOUND LEFT AND RIGHT UPPER WING STRUT ATTACH BOLTS INSTALLED BACKWARDS FACING AFT TO FORWARD. IPC SHOWS BOLTS INSTALLED FORE TO AFT.Aug 2, 1999 · N9539P · Cessna 182SSDR 99ZZZX1937Fitting · corrodedDURING EXECUTION OF PIPER SB NR 977 TITLED 'INSPECTION OF WING REAR ATTACH FITTING AND ADDITION OF INSPECTION ACCESS PANELS', CORROSION DAMAGE WAS DISCOVERED ON THE FORWARD FACE OF THE WING REAR ATTACH FITTINGS NEAR THE FLOOR LINE. (P/N 62488-02 AND P/N 62488Apr 28, 1999 · N7454W · Piper PA28180SDR CA990614030Lift Strut · corroded(CAN) DURING ROUTINE ANNUAL INSPECTION TO ACCOMPLISH AWD 99-01-05, FRONT STRUT WAS FOUND CORRODED THROUGH NEW N2 FILLED STRUTS AND FORK ENDS ORDERED FROM UNIVAIR.Mar 26, 1999 · Piper PA20
Back to JASC 5740