JASC 5700

Service difficulty reports · 2,402

Reports filed under 5700 · Wing Structure, newest first.

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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 = '5700'
  ORDER BY difficulty_date DESC"

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SDR HSYA2013012800012Structure · corrodedDURING MX, CORROSION INSPECTION, FOUND CORROSION ON LT WING OTBD SIDE OF NR 1 NACELLE INBD T/E BETWEEN WS 160 & 175. MX REMOVED LT WING UPPER SKIN DOUBLERS AT WS 160 AT APPROX 7.5" FROM L/E SPAR AND APPROX 7.5" FROM THE REAR EDGE SPAR. ON REMOVAL AND FURTHEJan 23, 2013 · N330SB · Stbros SD330SDR REXA2012121201607Panel · chafedRS-2-20 (PANEL RACK) PANEL 584EB IS CHAFED. REMOVED & REPLACED PANEL 584EB IAW CRJ-900 SRM 51-42-11.Dec 12, 2012 · N926XJ · Cndair CL6002D24SDR REXA2012121201606Panel · chafedRS-2-20 (PANEL RACK) PANEL 584GB IS CHAFED. REMOVED & REPLACED PANEL 584GB IAW CRJ-900 SRSM 51-42-11.Dec 12, 2012 · N926XJ · Cndair CL6002D24SDR REXA2012121201605Panel · wornRS-2-22 PANEL 699AB HAS A WORN GROVE IN IT. LOCATED AND DRILLED THE REPLACEMENT PANEL 699AB P/N 601R-13-440-2 REF CRJ-900 SRM 51-40-11.Dec 12, 2012 · N926XJ · Cndair CL6002D24SDR 2012FA0000530Track · corrodedLEFT "C" TRACK CORRODED.Aug 3, 2012 · N424QS · Gulstm GIVSDR 2012FA0000529Track · corrodedRIGHT "B" TRACK CORRODED.Aug 3, 2012 · N424QS · Gulstm GIVSDR AALA20120623017Tab · dentedTWO DENTS WITH DELAMINATE CLOSE TOGETHER, LOCATED 12 AND 10.25 INCHES FROM OUTBOARD END OF TAB. HOT BONDED REPAIR DOUBLER PER ESO 80087 AND SRM 51-70-02.Jun 23, 2012 · N7539A · Doug DC982SDR AALA20120623016Tab · dentedTWO DENTS WITH DELAMINATE CLOSE TOGETHER, LOCATED 28.5 AND 27 INCHES FROM OUTBOARD END OF TAB. INSTALLED DOUBLER PER ESO 80087 AND SRM 51-70-02.Jun 23, 2012 · N7539A · Doug DC982SDR AALA20120623015Tab · dentedDENT WITH DELAMINATE LOCATED 19 INCHES FROM INBOARD END OF TAB. INSTALLED DOUBLER PER ESO 80087 AND SRM 51-70-02.Jun 23, 2012 · N7539A · Doug DC982SDR AALA20120623014Tab · dentedTWO DENTS WITH DELAMINATE CLOSE TOGETHER LOCATED AT 5.5 AND 7.5 INCHES FROM INBOARD END OF TAB. ACCOMPLISHED DOUBLER REPAIR PER ESO 80087 AND SRM 51-70-02.Jun 23, 2012 · N7539A · Doug DC982SDR DALA1517979236Support Fitting · not reportedMLG ACTUATOR SUPPORT FITTING REPAIRED IAW AA 5740-01140.Jan 3, 2012 · N936DN · Doug MD9030SDR UALA2011101005476Skin · damagedON ARRIVAL BIRD STRIKE ON LT WING OUTBD FLAP L/E HAS A HOLE ON END CAP. R & R LE FLAP CAP.Oct 9, 2011 · N456UA · Airbus A320232SDR FDEA201107082618Unknown · smokeON TAKEOFF, TOWER REPORTED "EXCESSIVE SMOKE TRAILING FROM LT WING." DID AN ATB, NO INDICATION OF SMOKE ON ACFT AND NO ECAM WARNINGS. MX NOTED NO LEAKS FROM LT WING OR ENGINE. CREW STATED NO ABNORMAL HYD QTY OR OIL QTY DECREASE DURING TAKEOFF. NO ABNORMAJul 8, 2011 · N720FD · Airbus A300B4622SDR CA110617009Bolt · crackedLOWER FOREWARD LT WING BOLT FOUND CRACKED DURING INSP SIRM 57-16-01, ITEM 10. THE AVIA DESIGN FRONT WING KIT IS INSTALLED ON THIS ACFT. TOTAL TIME ON THIS BOLT IS 12331.0 HOURS AND 12 YEARS, LIFE LIMIT ON THIS BOLT IS 15000 HOURS OR 15 YEARS.Jun 17, 2011 · Beech A100SDR ASOA201001940Unknown · corrodedLEFT WING HAS CORROSION. BLENDED CORROSION AND CHECKED WITH DEPTH GAUGE IS.010" DEEP AND UNDER THE HEAD OF THE FASTENERS IS BEYOND LIMITS IAW SRM 53-11-10-991-804. REMOVED LT WEB GOT NEW WEB, INSTALLED LT WEB IAW SRM 51-42-06-001-001-A01 AND 51-42-13-001-001Dec 14, 2010 · N376CA · Cndair CL6002C10SDR DALA1018800186Fitting · damagedWHILE ACCOMPLISHING SB767-54 A0080, FIG 48. FOUND LT WING AFT PITCH LOAD BACKUP FITTING PN 112T6006-5 TO HAVE SEM CONDITION AS SHOWN IN FIG 1. ADDED A RADIUS FILLER TO THE FITTING INSIDE THE SEM FTG HOLE IAW ERA 482262-14AD, REV O/ REF NRC 52674.Aug 6, 2010 · N186DN · Boeing 767332SDR NSVA201089Structure · damagedRJ STRUCK 251CJ'S RIGHT WING CAUSING DAMAGE. THE INCIDENT OCCURRED DURING THE BOARDING PROCESS. THE PASSENGERS WERE DEPLANED. NO INJURIES OR ILLNESS REPORTED. FERRIED AIRCRAFT TO IAD AND REMOVED AND REPLACED THE LEADING EDGE.May 31, 2010 · N251CJ · Saab 340BSDR FDEA201003100748Bolt · unknownUNABLE TO INSTALL IEA FASTENER IAW EO F-5450-7-5003C PT3 & PT4, FOR THE LT & RT WING ISLF. INSTALLED 2EA BACB30US10K BOLTS IAW EA F-5450-131166 IN THE LT & RT WING ISLF. FAA FORM 8100-9 ATTACHED. ( LOCATION PP-RBL 9, WS 285.65 ). MAJOR REPAIR.Mar 10, 2010 · N924FD · Boeing 757204SDR 2009F00136Windshield · crackedIN CRUISE PILOTS WINDSHIELD CRACKED JUST RT OF CTR LINE FROM BOTTOM TO THE TOP OF THE PANE. DIVERTED FOR INSPECTION. MX INSPECTED AND APPLIED TAPE IAW CH56-10-01. MEL'D THE WINDSHIELD HEAT. CONTINUED ON.Dec 10, 2009 · N881TW · Cndair CL6002B16SDR 2009FA0000870Rod End · corrodedA MAJOR PORTION OF THE ROD END IS CORRODED. THE TOP OF THE SPHERICAL END OF THE BALL (ROD END) IS AGAINST THE BOTTOM OF THE WING SKIN. THE ROD END IS VERY DIFFICULT IF NOT IMPOSSIBLE TO INSPECT WITHOUT REMOVING THE WING STRUT AND PERFORMING A GOOD VISUAL INSPEOct 22, 2009 · N4222N · Cessna 120SDR EE4Y090277Skin · delaminatedRT WING INBOARD VANE FLAP OUTER AND INNER SKIN DELAMINATED.Sep 21, 2009 · N583MD · Doug MD83SDR CA090730002Fairing · improper partPART DOES NOT HAVE PROPER CERTIFICATION.Jun 24, 2009 · Cessna 172NSDR GUUA94057030709ASkin · corrodedDURING FUTHER INSPECTION OF SURFACE CORROSION DISCOVERED SEVERE CORROSION EXTENDS FROM WS 140.00 TO 190.00 APROXIMATELY. CUT OUT DAMAGED AREA AND INSTALLED AN EXTERNAL DOUBLER REPAIR.Mar 7, 2009 · N16540 · Beech 1900DSDR CA080722007Bushing · missing(CAN) BUSHINGS MISSING FROM WING PICKUP LUGS ON ORIGINAL FRAMES INSTALLED IN ACFT.Jul 18, 2008 · Dhav DHC6SDR HALA0800592Stiffener · crackedCRACK ON RIGHT WING FIXED T/E, JUST FORWARD OF O/B AILERON LENGTH WISE STIFFENER. REPAIRED RIGHT WING T/E, JUST FWD OF O/B AILERON STIFFENER PER SRM 51-20-11-OG-0, AND SRM 51-01-OG-0.May 17, 2008 · N581HA · Boeing 76733ASDR FDKA200805196Bonding Strap · corrodedBONDING STRAP IS CORRODED ON PANEL 5731. THE CORRODED STRAPS HAVE BEEN REMOVED AND REPLACED.May 7, 2008 · N837MJ · Emb EMB145LRSDR 08FDEA00944Fairing · dentedRT WING FAIRING 634 AT IS DENTED AND DELAMINATED. REPAIRED IAW SRM 57-20-35.Mar 14, 2008 · N425FE · Airbus A310SDR C2XA07SH103Access Panel · damagedRT PNL 191FR HAS COMPOSITE DAMAGE AT SCREW HOLES. MAINTENANCE REPAIRED RT PNL 191 FR IAW EC5750-01315. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.Dec 15, 2007 · N18120 · Emb EMB145XRSDR C2XA07SH071Plate · corrodedSHV - DURING C-CHECK PANEL 191 BONDING PLATES HAVE CORROSION. MX REMOVED AND REPLACED CORRODED BONDING PLATES ON PANEL 191 IAW EC 5750-01315 REV D. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.Sep 19, 2007 · N14947 · Emb EMB145EPSDR RAIA00706039Skin · crackedSTL - DURING INSPECTION, LT WING TRAILING EDGE SKIN WAS FOUND TO HAVE A 1.125 INCH CRACK PROPAGATING FROM RIVET TO TRAILING EDGE NEAR GROUND SPOILER ACTUATOR CUTOUT. MAINTENANCE INSPECTED IAW MANUFACTURER'S SERVICE INFORMATION AND PLACED ON TIME CARRYOVER FORJun 22, 2007 · N815HK · Emb EMB145LRSDR COMA0760258Unknown · unknownFLIGHT 5576 - LEFT WING OVERHEAT ON BEGINNING OF TAKEOFF THRUST. DEFERRED PER MEL 30-12-03-1.Mar 15, 2007 · N989CA · Cndair CL6002B19SDR QXEA200700545Unknown · damagedC4 PDX - AT LEFT UNDER WING STATION YW222.4 THERE IS AN AREA OF SMALL NICKS. REPAIRED IAW RD8-57-2996 AND SRM 51-20-11.Mar 9, 2007 · N367PH · Dhav DHC8202SDR CA070108010Bolt · cracked(CAN) SCHEDULED WING BOLT INSPECTION, NOTED RT UPPER AFT WING BOLT CRACKED ON BOLT HEAD TO SHANK RADIUS. BOLT REPLACED WITH NEW. (TC NR 20070108010)Jan 5, 2007 · Beech 100BEECHSDR TRAX200601108Hose · twistedBWO 6042035-790 SNAG SHEET C-1026405 NR 2 BRADED STEEL HOSE ON LEFT COLLECTOR TANK FOUND FOULING ON RIB STIFFENER P/N 600-10221-1. RIB BLENDED IAW SRM 57-00-00 SERVICABLE.Dec 12, 2006 · N860AS · Cndair CL6002B19SDR 06FDEA04075Skin · unknownRT WING L/E SKIN LOWER SIDE SLAT DRIVE MECHANISM ACCESS DOOR CUT OUT AT STA XORS 402 EXISTING SKIN REPAIR. REMOVED EXISTING REPAIR IAW SRM 57-10-00 VOL 1. INSTALLED REPAIR IAW SRM 57-10-00 FIG 68 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER NR N01203 ANDNov 21, 2006 · N304FE · Doug DC1030SDR CA061020007Unknown · unknown(CAN) TYPE CERTIFICATE HOLDER (TCH) RECEIVED CALL INDICATING THIS AIRCRAFT WAS IN LEVEL FLIGHT WITH AN INDICATED AIRSPEED OF 120 KNOTS. THE PILOT FELT A VIBRATION IN THE AIRFRAME, LOOKED OUT THE LT WINDOW AND SAW THAT THE LT WING WAS FLUTTERING UP AND DOWN. THOct 17, 2006 · Dhav DHC6300SDR 2006UALA01836Skin · crackedNR 3 SLAT LWR EXT SKIN CRACKED AT 3 FASTENERS BELOW ACTUATOR. MAJOR REPAIR: SLAT REPAIRED PER SRM 57-43-01 REPAIR 6.Sep 22, 2006 · N309UA · Boeing 737322SDR UIEA200600220Fairing · damagedN493MC WAS AT PIK FOR A-2 CHECK. AS PER NON-MEL 06-068 AND N/ROUTINE 41. A HOLE WAS FOUND IN LEADING EDGE OF RIGHT WING BODY FAIRING AT STA 840. INTERIM REPAIR CARRIED OUT AS PER SRM 53-00-70 (NOTE B). TAP TEST ON EVERY CHECK AND PERMANENT REPAIR WILL BE CAug 30, 2006 · N493MC · Boeing 74747UFSDR 2006750001Wing · crackedWING CRACKED, REMOVED AND REPLACED LEFT WING.Apr 11, 2006 · N750DH · Boeing 7272M7SDR 06FDEA0842Repair · noneREPAIR LOCATED ON RT WING NR 2 SLAT L/E REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUS INSTALLED REPAIR ON NR 2 SLAT L/E WAS DETERMINED TO BE COMPLIED WITH IAW EA 6-5743-94774 AND S00007 NOV Feb 25, 2006 · N455FE · Airbus A310222SDR 06FDEA0799Repair · unknownFLUSH REPAIR LT WING NR1 SLAT STA. XORS 60, LE, MARKED NR 93. REPAIR REQUIRES EVALUATION FOR MAJOR/ MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. VISUALLY INSPECTED REPAIR L/W NR 1 SLAT STA. XORS 60 L/E, MARKED NR 93. FOUND TOFeb 21, 2006 · N68050 · Doug MD1010FSDR DHL2006760521Skin · crackedFOUND NR 5 SLAT IB FRAME AT ACTUATOR ROD END ATTACH IS CRACKED IN LOWER FWD RADIUS. REMOVED NR 5 SLAT I/B FRAME AT ACTUATOR ROD END IAW B727 SRM 51-30-2. REPLACED NR 5 SLAT I/B FRAME IAW B727 SRM 51-10-1 AND B727 SRM 51-30-2 P/N 65-17276-11. THIS REPAIR IS Feb 19, 2006 · N760AT · Boeing 7272B7SDR 06FDEA0641Skin Panel · unknownFOUND REPAIR LOCATED LT AILERON WS 513-538. LOWER SURFACE. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA.Feb 10, 2006 · N430FE · Airbus A310SDR 06FDEA0594Repair · unknownDISCREPANCY RIGHT HAND WING L/E SLAT TRACK NR 10 CUT OUT ON LOWER SKIN HAS AN EXTERNAL DOUBLER REPAIR AT STA XOS 657 DIM. 7.5" X 5" CORRECTIVE ACTION R/R REPAIR IAW SRM 57-10-00 FIG 68 VOL 1 FABRICATED PART IAW DETAIL PART TRAVELER N01213 AND SRM 57-10-Feb 8, 2006 · N563FE · Doug DC1010SDR 06FDEA0586Repair · unknownFOUND REPAIR LOCATED ON UPPER SURFACE OF LEFT WING AFT OF NR 4 L/E FLAP, STA 410. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA.Feb 7, 2006 · N487FE · Boeing 727200SDR 06FDEA0585Repair · unknownFOUND 2 REPAIRS LOCATED ON UPPER SURFACE OF RT WING AFT OF NR 6 L/E, STA 546. REPAIRS REQUIRE EVALUATION FOR MAJOR MINOR DETERMINATION AND IF REPAIRS WERE ACCOMPLISHED USING FAA APPROVED DATA.Feb 7, 2006 · N487FE · Boeing 727200SDR 06FDEA0584Repair · unknownFOUND REPAIR ON LEFT I/B FORE FLAP UPPER SURFACE. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA.Feb 7, 2006 · N487FE · Boeing 727200SDR 06FDEA0583Repair · unknownFOUND REPAIR ON RIGHT OUTBOARD FORE FLAP L/E REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA.Feb 7, 2006 · N487FE · Boeing 727200SDR 06FDEA0567Repair · noneFOUND PREVIOUSLY REPAIR INSTALLED AT R/H WING LEADING EDGE 12 INCHES OUTBD OF LANDING LIGHT WAS DETERMINED TO BE ACCOMPLISHED IAW SRM 57-30-4, FIG 2, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE AND SIZE, MATERIAL TYPE AND THICKNESFeb 7, 2006 · N487FE · Boeing 727200SDR 06FDEA0563Repair · noneFOUND PREVIOUSLY REPAIR INSTALLED AT RIGHT WING LEADING EDGE, ON FRAME OF LANDING LIGHT WAS DETERMINED TO BE ACCOMPLISHED IAW SRM 57-10-4 FIG. 4, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTFeb 7, 2006 · N487FE · Boeing 727200
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