JASC 5711

Service difficulty reports · 5,587

Reports filed under 5711 · Wing Spar, 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 = '5711'
  ORDER BY difficulty_date DESC"

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SDR GUUA94557041611ASpar · corrodedDURING SCHEDULED ROUTINE X-RAY INSPECTION DISCOVERED CORROSION ON LEFT WING FORWARD SPAR AFT FLANGE WS 128.50. REMOVED CORROSION FROM FORWARD SPAR AFT FLANGE AND INSTALLED REINFORCEMENT DOUBLER STRAP.Apr 16, 2011 · N53545 · Beech 1900DSDR FDEA201104121443Spar · corrodedLT WING REAR SPAR WEB AT IRSS 188 ABOVE FUEL BOOST PUMP UPPER BONDING JUMPER FOUND WITH CORROSION. CORROSION REPAIR CARRIED OUT ON LT WING REAR SPAR WEB IAW EA F-5710-146438. (LT WING REAR SPAR WEB CORROSION BLEND REPAIR). REPAIR IS CLASSIFIED AS MAJOR.Apr 12, 2011 · N948FD · Boeing 757236SDR F3LA2011041300634Spar · dentedC-CHECK: NON ROUTINE NR30121; RT WING L/E STA 7792/RIB 14 IS DENTED WITH INTERNAL DAMAGE AT CLOSEOUT WEB. REPAIRED RIGHT WING L/E DAMANGE STATION 7792/RIB 14 REPAIRED IAW EA A9-57R-32036 INSTRUTIONS 1-4 AS WRITTEN. HFEC INSPECTED, NO CRACKS WERE FOUND.Apr 11, 2011 · N949FR · Airbus A319112SDR KGBR110411338ASpar · corrodedRIGHT WING, REAR SPAR WEB HAS CORROSION, WS 5940 AFT SIDE AT BOTTOM SPAR CAP (MARKED).Apr 11, 2011 · N392CA · Casa C212SDR CHQA201100131Spar · crackedDURING INSPECTION A CRACK WAS FOUND ON THE LEFT WING SPAR I TOP FLANGE CRACKED THRU AT RIB 19. THE CRACK WAS 2.745 INCHES LONG AND 0.001 INCHES WIDE THRU THE MATERIAL. THE DAMAGED AREA WAS REMOVED AND A REINFORCING PATCH WAS INSTALLED PER TI-145-11-095.Apr 10, 2011 · N978RP · Emb EMB145EPSDR IPXA1M66276Spar · corrodedINSP TYPE:4C, CORROSION UNDER LT WING UPPER T/E PANEL NEAR STA XOS.795 REPAIRED LT WING REAR SPAR UPPER AFT FLANGE REF EO MD11-5710- 42417-A AND STA SA EA 011-5710-01-A3034 REV IR STA XORS 782-798.Apr 6, 2011 · N251UP · Doug MD11FSDR 2011FA0000228Spar · corrodedCORROSION LOCATED ON RT WING SPAR AFT SIDE, WS 59-61, AT FUEL TANK FLEXIBLE ACCESS.Apr 6, 2011 · N4592R · Piper PA28140SDR DALA1503459228Spar · crackedWING REAR SPAR CRACKED. REPAIRED IAW AA 5710-01119.Mar 29, 2011 · N928DN · Doug MD9030SDR 2011FA0000210Spar · corrodedINSP OF WING CTR SECTION IAW AD 2002-26-02 INTER-GRANULAR CORROSION IN EXFOLIATION STAGE WAS DISCOVERED ON THE BOTTOM MAIN SPAR CAP, EXTREME REAR OTBD SECTIONS WHERE IT WAS MILLED TO ACCOMMODATE THE MLG TRUNNION AND JUST INBD. ALSO THE LT AND RT (WING WALK) IMar 29, 2011 · N99558 · Univar 415CSDR DALA1502730982Spar · crackedWING REAR SPAR CRACKING AT XRS 164. REPAIRED IAW AA 5710-01110.Mar 27, 2011 · N982DL · Doug MD88SDR AALA20110324TUL05Spar · crackedHFEC SURFACE INSPECTION OF LEFT WING REAR SPAR CAP AT XRS 164.0 INDICATES A CRACK .250 AT 5 O`CLOCK POSITION OF THE LOWER INBOARD FLAP FAIRING ATTACH HOLE. REMOVED AND SPLICED IN NEW SECTION OF REAR SPAR PER EA MD80-57-015745.Mar 24, 2011 · N271AA · Doug DC982SDR DALA1404200976Spar · crackedWING REAR SPAR CRACKED AT XRS 164. REPAIRED IAW AA 5710-01110.Mar 21, 2011 · N976DL · Doug MD88SDR FOTR2102212307Spar · crackedNR 1 SLAT ACTUATOR OTBD MOUNT SUPPORT ON LT WING FRONT SPAR CRACKED. REMOVED CRACKED WEB FROM L/E LT WING SLAT STA 398.1 IAW SRM 51-30-2. FABRICATED NEW WEB FROM 7075T6 .063 PO 9009533 DIM 4.5" X 9" IAW SB 727-57-0130 FIG 1. INSTALLED REPAIR WEB IAW SB 727-Mar 15, 2011 · N287SC · Boeing 7272A1SDR DALA1515590986Spar · crackedWING REAR SPAR CRACKING AT XRS 164 REPAIRED IAW AA 5710-01110.Mar 14, 2011 · N986DL · Doug MD88SDR AALA20110502TUL03Spar Cap · crackedRIGHT WING LOWER REAR SPAR CAP AT STATION XRS 164 HAS CRACK INDICATION APPROXIMATELY 1/4 INCH LONG CONFIRMED WITH HFEC SCAN. REPAIRED PER EA MD80-57-016677.Mar 14, 2011 · N70401 · Doug DC982SDR FDEA201103140966Rib · misrepairedRE-EVALUATION OF EXISTING REPAIR ON RT WING CTR FLAP BULLNOSE RIBS 19-20 LOCATION CARRIED OUT USING ORIGINAL NRC 0003346 AND SRM 57-50-00, FIG 208. REPAIR SUSPECTED TO HAVE 1 ROW OF SPLICE FASTENERS MISSING FROM THE OTBD SPLICE. REPAIR WAS REMOVED AND SKMar 14, 2011 · N727FD · Airbus A300B4622RSDR GUUA95557031211ASpar · corrodedDURING SCHEDULED X-RAY INSP, DISCOVERED RT WING CORROSION ON MAIN SPAR 1.3 X 0.06 INCHES AT WS 124.25. REMOVED CORROSION FROM RIGHT WING LOWER FORWARD SPAR CAP COMPLIED WITH FLOURESCENT PENETRANT INSPECTION ON BLEND OUT AREA NO SIGNS OF CORROSION FOUND ALL AREMar 12, 2011 · N87555 · Beech 1900DSDR SWIA201125963Spar Cap · crackedLEFT WING FORWARD SPAR CAP INBOARD OF NACELLE CRACKED AT HI-LOK. (C-CHECK) REPAIRED LEFT WING AUX SPAR PER EMBRAER TECHNICAL DISPOSITION.Mar 8, 2011 · N584SW · Emb EMB120ERSDR GLBA20110307GSpar · wornMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE LH WING REAR SPAR BOTTOM LEADING EDGE CHAFFED AT 2 LOCATIONS BY EXT PWR CABLE, OB CHAFF .4" IN LENGTH .1" DEEP, IB CHAFFR .3" IN LENGTH .05" DEEP. MAINTENANCE REPAIRED THE AFFECTED AREMar 7, 2011 · N100UX · Beech 1900DSDR CA110321004Spar · deteriorated(CAN) AILERON HINGE FLAP HINGE ATTACH POINT SPRUCE SPARS, WOOD DETERIORATED AT HINGE ATTACH POINT, FALSE SPARS REPLACED. DESCRIBED WITH DWG.Mar 4, 2011 · Mncoup 90AF100SDR UALA2011030401069Spar · corrodedLT WING REAR SPAR WEB CORRODED AROUND FASTENERS BETWEEN IRSS 340 AND IRSS 350 WHERE A FUEL BOOST PUMP IS INSTALLED. REPAIRED IAW 777EN-57-0156.Mar 4, 2011 · N212UA · Boeing 777222SDR DALA1505270985Spar · crackedWING REAR SPAR CRACKING AT XRS 164. REPAIRED IAW AA 5710-01110.Mar 3, 2011 · N985DL · Doug MD88SDR 2011FA0000608Spar · corrodedAT APPROX LT WING STA 56.0, THE UPPER OTBD QUADRANT OF AN ELECTRICAL WIRE PASS THROUGH HOLE IN THE WING SPAR WEB WAS FOUND TO HAVE EXFOLIATION CORROSION. THE PASS THROUGH HOLE, WHICH IS IN THE LANDING GEAR WHEEL WELL AREA, HAD A CATERPILLAR GROMMET INSTALLED TFeb 26, 2011 · N5911L · Piper PA44180SDR FDEA201102200639Spar · damagedSPAR REF EO 6-5710-7-3305 PART 2, STEP 15 HOLE (I) DIAMETER OF HOLE EXCEEDED EO REQUIREMENT LIMIT. HOLE (I) DIAMETER = 0.572" (MAXIMUM DIAMETER ALLOWED = 0.531"). EO 6-5710-7-3305 PART 2, STEP 15 HOLE (I) DIAMETER REPAIR HAS EXISTING REPAIR RECORD AND PREVIFeb 20, 2011 · N728FD · Airbus A300B4622RSDR IPXA11M65152Spar · corrodedINSPECTION TYPE:3C, SIGNFICANT MATERIAL LOSS DUE TO LATCH WEAR ON LT WING LOWER FWD SPAR FLANGE AT DOOR 526FB. AFTER REMOVAL OF LATCH WEAR PLATES FOUND SPAR FLANGE CORRODED UNDER EACH PLATE STA XFS910 & XFS924. REPAIRED SPAR FLANGE REF EO MD11- 5720-41719-A Feb 17, 2011 · N260UP · Doug MD11FSDR FXGA20110217001Spar · crackedTHE CENTER SPAR WEB WAS FOUND CRACKED AT W/S 90R. REPAIRED PER EAC EO 1103 AND 8110-3 DATED 2/12/11Feb 17, 2011 · N6174C · Doug DC6ASDR SWIA201125966Spar Cap · crackedLEFT WING INBOARD INTERNAL SPAR CAP IS CRACKED AT HI-LOK. (C-CHECK) REPAIRED LEFT INBOARD WING INTERNAL SPAR CAP PER EMBRAER TECHNICAL DISPOSITION.Feb 14, 2011 · N290SW · Emb EMB120ERSDR SWAA110886Spar · crackedDURING SCHEDULED 20Y CHECK, FOUND LT WING CRACKED ON UPPER CHORD REAR SPAR RSS 223.14. REPAIRED SPAR PER EA.Feb 12, 2011 · N512SW · Boeing 7375H4SDR IXXA11SMN048SSpar Cap · crackedDURING ROUTINE C-CHECK INSP FOUND RT WING FRONT SPAR L/E LOWER CAP CRACKED AT STA XFS 500.233. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. PERFORMED NDT INSP, NO DISCREPANCY FOUND. FABRICATED SPLICE ANGLES, EXTERNAL DOUBLER, STRAP. CLEANED, TREATED, PRIMFeb 11, 2011 · N821BX · Doug DC871FSDR QXEA2011021400150Spar · chafedC1 CHECK - AFT WING SPAR PANEL MONTING FLANGE FOR PANEL 262AT HAS FRETTING. BLENDED OUT CHAFE DAMAGE IAW RD 8/4-53-451. CONFIRMED CRACK FREE CONDITION AND FOUND WITHIN LIMITS IAW RD 8/4-53-451. REPAIR COMPLETED IAW RD 8/4-53-451.Feb 11, 2011 · N436QX · Bombdr DHC8402SDR QXEA2011021400149Spar · chafedC1 CHECK - AFT WING SPAR PANEL MOUNTING FLANGE UNDER PANEL 262FT HAS FRETTING. BLENDED OUT CHAFE DAMAGE IAW RD 8/4-53-451. CONFIRMED CRACK FREE CONDITION AND FOUND WITHIN LIMITS IAW RD 8/4-53-451. REPAIR COMPLETED IAW RD 8/4-53-451.Feb 11, 2011 · N436QX · Bombdr DHC8402SDR QXEA2011021400148Spar · chafedC1 CHECK - AFT WING SPAR PANEL MOUNTING FLANGE UNDER PANEL 262HT HAS FRETTING. BLENDED OUT CHAFE DAMAGE IAW RD 8/4-53-451. VERIFIED CRACK FREE CONDITION AND FOUND WITHIN LIMITS IAW RD 8/4-53-451. REPAIR COMPLETED IAW RD 8/4-53-451.Feb 11, 2011 · N436QX · Bombdr DHC8402SDR EE4Y20110094Anchor Fitting · corrodedLEFT OUTER WING REAR SPAR AFT FACE RETRACTION JACK ANCHORAGE FITTING CORRODED AROUND THE BORE UPPER AND LOWER AND IN THE BORE INNER SURFACE. DAMAGED PART IS GOING TO BE REPAIRED FOLLOWING REPAIR INSTRUCTIONS.Feb 6, 2011 · N503NK · Airbus A319132SDR H5GR20110218001Spar · crackedDURING THE ANNUAL INSP, A CRACK IN THE RT FWD SPAR, FWD WEB BEND RADIUS WAS NOTICED DURING A VISUAL INSP OF THE AREA. A DYE PENETRANT INSP WAS PERFORMED AND CRACK VERIFIED. INSP WAS PERFORMED FOLLOWING MM, PN: 55-590000-13G, REV G2, SECTION 53-00-00, PAGE 202Feb 4, 2011 · N219CH · Beech 58SDR FDEA201102010439Spar Cap · corrodedRT WING T/E UPPER AFT SPAR CAR TOP SURFACE FOUND CORRODED AT WING STA XORS 980. SPAR CAP CORROSION REPAIRED AS PER E.A. 1-5710-143520, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 111.Feb 1, 2011 · N614FE · Doug MD11FSDR MU1Z2011020200001Spar · corrodedDURING HEAVY AND DELIVERY MAINTENANCE CHECK; RIGHT MAIN LANDING GEAR W/W AT CENTER WING REAR SPAR RBBL 74.57" AND 2 INCH DOWNWARD OF THE WL 178.02 CHORD WAS FOUND CORROSION (LEVEL 3).Jan 28, 2011 · N728CG · Boeing 767283ERSDR CA110131010Aap · chafed(CAN) ACM LOUVERED EXHAUST PLENUM REMOVED TO CARRY OUT "F" CHECK PROCEDURE. NOTED AFTER REMOVAL OF LOUVERED PLENUM THAT THE PLENUM WAS CHAFING INTO THE LOWER MAIN SPAR CAP FORWARD FLANGE AT LWS 35-LWS 40. LWS 35 SPAR CAP FLANGE CHAFED TO 0.06 INCH AND DECREASEJan 27, 2011 · Beech 1900DSDR DALA1514330987Spar · crackedWING REAR SPAR CRACKED AT XRS 164 REPAIRED IAW AA 5710-01110.Jan 26, 2011 · N987DL · Doug MD88SDR FDEA201101250355Spar · crackedDURING HFEC OPEN HOLE INSPECTION CRACK INDICATION FOUND AT RT CTR WING BOX OF REAR SPAR HOLE (I) ON SECOND LAYER EDGE FROM FWD APPROX 0.5" (L2) LONG. THE THIRD LAYER CRACK IS NOT A CRACK AT ALL. INSTEAD IT IS A STRAIGHT LINE BUTT-JOINT BETWEEN THE REAR SPAR Jan 25, 2011 · N663FE · Airbus A300F4605RSDR FDEA201101210328Frame · crackedDURING HFEC OPEN HOLE INSP CRACK INDICATION FOUND AT LT CTR WING BOX OF REAR SPAR HOLE (N) ON SECOND LAYER EDGE FROM AFT APPROX 0.012" (L1) DEPTH AND 0.010" (L2) LENGTH. REPAIR CARRIED OUT IAW EO 6-5710-7-3305D PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100Jan 21, 2011 · N663FE · Airbus A300F4605RSDR FDEA201101210327Frame · crackedDURING HFEC OPEN HOLE INSP CRACK INDICATION FOUND AT LT CTR WING BOX OF REAR SPAR HOLE (M) ON SECOND LAYER EDGE FROM AFT APPROX 0.012" (L1) DEPTH AND 0.010" (L2). REPAIR CARRIED OUT IAW EO 6-5710-7-3305D, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REVJan 21, 2011 · N663FE · Airbus A300F4605RSDR FDEA201101210326Frame · crackedDURING HFEC OPEN HOLE INSP CRACK INDICATION FOUND AT LT CTR WING BOX OF REAR SPAR HOLE (LT) ON SECOND LAYER EDGE FROM AFT APPROX 0.012" (L1) DEPTH AND 0.010" (L2) LENGTH. REPAIR CARRIED OUT IAW EO 6-5710-7-3305D, PART 1. REPAIR CLASSIFIED MAJOR GMM 6-2-100Jan 21, 2011 · N663FE · Airbus A300F4605RSDR FDEA201101170213Spar Cap · crackedLT WING AFT LWR SPAR CAP, FOUND 3 CRACKED HOLES ON THE OTBD ROW AND 1 CRACKED HOLE ON THE FWD MOST INBD LT WING AFT LOWER SPAR HAS BEEN REPAIRED AND COMPLIES WITH EA NR 8-5710-142566.Jan 17, 2011 · N569FE · Doug MD1010FSDR GUUA93757011711CSpar Cap · corrodedDURING SCHEDULED X-RAY INSP DISCOVERED LT WING CORROSION AT LOWER FWD SPAR CAP NEAR FUEL DRAIN WS 125.5. REMOVED CORROSION FROM LEFT WING AT LOWER FORWARD SPAR CAP NEAR FULE DRAIN WS 125.5 AND INSTALLED AN EXTERNAL DOUBLER REPAIR.Jan 17, 2011 · N38537 · Beech 1900DSDR GUUA93757011711BSpar Cap · corrodedDURING SCHEDULED X RAY INSP DISCOVERED RT WING CORROSION AT LOWER FWD SPAR CAP NEAR FUEL DRAIN. REMOVED CORROSION FROM RIGHT WING LOWER FORWARD SPAR CAP COMPLIED WITH FLOURESCENT INSPECTION ON BLEND OUT AREA NO SIGNS OF CORROSION FOUND,ALL AREAS WITHIN LIMITSJan 17, 2011 · N38537 · Beech 1900DSDR FDEA201101170214Spar · crackedLEFT WING REAR SPAR LOWER CHORD ANGLE AT STA.XORS 345 HAS A CRACK INDICATION THROUGH 3 FWD FWD HOLES AND CAN BE SEEN ON THE AFT SIDE EXTENDING OUT OF THE RADIUS APPROX.1" AFT AND UP THE VERTICAL LEG UNDER THE FITTING. (VERIFIED BY N.D.T) REPAIRED AND COMPLIJan 17, 2011 · N569FE · Doug MD1010FSDR FDEA201101160183Frame · crackedDURING HFEC OPEN HOLE INSP CRACK INDICATION FOUND AT LT CTR WING BOX OF REAR SPAR HOLE. REPAIRED IAW EO 6-5710-7-3305D PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV I 111.Jan 16, 2011 · N663FE · Airbus A300F4605RSDR VGQY2011011500009Spar Cap · corrodedRT MAIN LANDING GEAR WHEEL WELL - FOUND CORROSION AT OUTER WING REAR SPAR CAP, UPPER SIDE-BOTTOM SURFACE - STA XORS 118.200. COMPLIED WITH EA DC10-5730-1133.Jan 15, 2011 · N220AU · Doug DC1010SDR VGQY2011011500007Spar · corrodedLT WING INNER REAR SPAR APPROX STA XORS 264 FOUND EXTRUSION CORRODED. COMPLIED WITH EA DC10-5710-1131.Jan 15, 2011 · N220AU · Doug DC1010SDR VGQY2011011500006Spar Cap · corrodedLT WING INNER REAR SPAR APPROX STA XORS 197 FOUND EXTRUSION CORRODED. COMPLIED WITH EA DC10-5710-1132.Jan 15, 2011 · N220AU · Doug DC1010
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