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"

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 07FDEA01156Frame · crackedCRACK FINDINGS DURING ACCOMPLISHMENT OF EO 6-5710-7-3305 REV C1, SB A300-57-6050 REV 3-AD 2005-23-08 REPAIR PERFORMED BY REAM UP AND BUSHING INSTALLATION IAW EA 6-5710-106435 AND RAS/049856/032/2007 ISS. AMar 28, 2007 · N748FD · Airbus A300B4622RSDR QXEA200700541Spar · tool damageC4 PDX - RIGHT WING BOTTOM SPAR HAS TOOLING MARKS FROM LEADING EDGE REMOVAL, FROM NACELLE TO THE WING TIP. REPAIRED IAW RD8-57-1119.Mar 27, 2007 · N365PH · Dhav DHC8202SDR MWA70316066Spar Cap · damagedDISCOVERED DURING F-CHECK, DOUBLE-DRILLED HOLE LOWER FORWARD LT SPAR CAP AT APPROXIMATELY WS 81.5. REPAIRED IAW ENGINEERING REPORT 6631-1.Mar 27, 2007 · N166YV · Beech 1900DSDR 07FDEA01053Frame · crackedDEVIATIONS TO EO 6-5710-7-3322 (CRACKS IN HOLE 23 AND 62 LT). REPAIR PERFORMED BY OVERSIZING HOLE 23 AND 62 LT IAW EA 6-5710-106423 AND RAS/049817/013/2007 ISSUE "A".Mar 21, 2007 · N816FD · Airbus A310304SDR EIA2007081Spar · corrodedCORROSION FOUND AT TOP CHORD ASSY AT LT WING IN FRONT OF SPOILER NR 5 & NR 6. BEAM ASSY UPPER "T" CHORD REMOVED FROM WBL 285-WBL345. FABRICATED AS PER SRM 51-40-04 FIG 3. REPAIR CARRIED OUT PER B747 SRM 51-40-04 FIG 3.Mar 16, 2007 · N482EV · Boeing 747212BSDR 07FDEA00901Spar · crackedCENTER WING BOX, CRACKS IN FLANGE SPAR NR 4 RT, C44.1. REPAIR WAS PERFORMED BY CUT OUT AND MANUFACTURE AND REPAIR ANGLE IAW EA 6-5710-103404 AND RAS/047737/009/2006 ISSUE "A".Mar 15, 2007 · N813FD · Airbus A310324SDR USAA070209Spar · damagedRT WING UNDER SIDE FIRST 3 FASTENERS INBOARD AT ATTACH Z-ANGLE BELOW FWD SPAR HAS HOLES. REAMED HOLES TO .263 & INSTALLED FASTENERS PER SRM 51-40-09, DEFECT SIZE: .213 DIA.Mar 15, 2007 · N423US · Boeing 737401SDR 07FDEA00828Spar · crackedRIGHT WING REAR SPAR IS CRACKED AT NR 3 AFT FUEL BOOST PUMP, REMOVED PARTS. FABRICATED REPAIR DOUBLER AND INSTALLED REPAIR PARTS IAW SRM 57-10-00, FIG 52, VOL I.Mar 14, 2007 · N360FE · Doug MD1010FSDR 07FDEA00666Spar Cap · corrodedRIGHT WING REAR SPAR UPPER CAP FOUND CORROSION AT XORS 1043. SUPPLEMENTAL 21 MARCH 07; CORROSION REMOVED ON RIGHT HAND WING REAR SPAR UPPER CAP XORS 1043 AS PER SRM 51-21-01 VOLUME II. ORIGINAL THICKNESS = 0.119", MATERIAL REMOVED = 0.039", REMAINED THICKNESSMar 6, 2007 · N609FE · Doug MD11FSDR 07FDEA00622Spar Cap · corrodedFOUND LT WING, REAR SPAR LOWER CHORD AT STA 1063 - 1075 CORROSION. LT WING, REAR SPAR LOWER CHORD AT STA 1063 - 1075 REPAIRED AS PER FEDEX EA NR 1- 5710- 105615, WINGS, LEFT WING LOWER SPAR CAP AFT FLANGE CORROSION BETWEEN XORS=1063 AND XORS=1075 - REPAIR. Mar 1, 2007 · N586FE · Doug MD11SDR CA070226008Spar Cap · cracked(CAN) WHILE PERFORMING AD CF92-26R1, A CRACK WAS DETECTED ON THE RT REAR LOWER SPAR CAP JUST OB OF RBL 51.00. WORK COMMENCED ON REPAIR IAW THE MFG SPEC. UPON REMOVAL OF REINFORCING STRIP (P/N 215-10032-76) AN ADDITIONAL CRACK WAS FOUND ON THE LOWER SPAR CAP AFeb 26, 2007 · Cndair CL2151A10SDR NWAA071079918Spar · crackedDURING "L" CHECK, FOUND CRACK IN LT WING TE SPAR EXISTING TEMPORARY REPAIR AT WS 267. SECTION I OF EA 99-208475 REMOVES EXISTING TEMPORARY REPAIR AND REINSTALLATION OF NEW TEMPORARY REPAIR. SECTION II OF EA REQUIRES PERMANENT REPAIR TO BE INSTALLED WITHIN 2 Feb 26, 2007 · N940N · Doug DC932SDR AMW070206033Spar Cap · corrodedBIO-CORROSION ON RT SPAR CAP FLANGE AT WS124. REPAIRED IAW AERODESIGN ENGINEERING REPORT NR6556-1.Feb 26, 2007 · N143YV · Beech 1900DSDR 07FDEA00549Spar Cap · corrodedLT WING REAR SPAR TOP CAP TAPER FILLER AT XORS=480 FOUND UPPER SURFACE CORRODED. COMPLIED WITH FEDEX EA 1-5720-106599. REPAIR CLASSIFIED AS MINOR AS PER FEDEX GMM 6-2-100.Feb 25, 2007 · N601FE · Doug MD11SDR 07FDEA00548Spar Cap · corrodedLT WING REAR SPAR LWR CAP XORS=1050 FOUND UPPER SURFACE CORRODED. COMPLIED WITH FEDEX EA 1-5720-106594. CLASSIFIED AS MINOR REPAIR AS PER FEDEX GMM 6-2-100.Feb 25, 2007 · N601FE · Doug MD11SDR A6WA200740072Spar · misdrilledWHILE PERFORMING E03/062/457 MODIFICATION LT AND RT WING REAR SPARS, A FASTENER HOLE WAS MISDRILLED. HOLE DIAMETER .213 INCH AT TRAILING EDGE WS 129, 2 INCHES IB OF JACKING PAD POINT ON RT WING. (M) MAINTENANCE REAMED HOLE TO ACCOMMODATE .25 INCH HOLE TO BE Feb 24, 2007 · N448AW · Cndair CL6002B19SDR AWXA200700284Spar · crackedMCN - FOUND RIGHT WING SPAR CHORD CRACKED, WBL 157, UNDER AFT OUTBOARD GEAR BEAM SUPPORT FITTING. REPAIRED RIGHT WING SPAR CHORD, WBL 157, UNDER AFT OUTBOARD GEAR BEAM SUPPORT FITTING IAW AWA ER 03-5700-07052-SS4.Feb 23, 2007 · N164AW · Boeing 73733ASDR AWXA200700283Spar · crackedMCN - FOUND LEFT WING SPAR CHORD CRACKED, WBL 157, UNDER AFT OUTBOARD GEAR BEAM SUPPORT FITTING. REPAIRED LEFT WING SPAR CHORD, WBL 157, UNDER AFT OUTBOARD GEAR BEAM SUPPORT FITTING IAW AWA ER 03-5700-07052-SS4.Feb 23, 2007 · N164AW · Boeing 73733ASDR EIA2007043Spar · corrodedRIGHT WING FRONT SPAR LOWER CHORD FORWARD SIDE HAS CORROSION ON VERTICAL FLANGE BETWEEN OLES/FSSO 1514-1521. REMOVED CORROSION, NDT'D AERA, FABBED AND INSTALLED REPAIR PER ECRA 477-57-117-2.Feb 22, 2007 · N477EV · Boeing 747SR46SDR EIA2007041Spar · corrodedRIGHT WING FRONT SPAR LOWER CHORD AT FSSO 1341 HAS CORROSION ON FORWARD SIDE OF THE VERTICAL FLANGE. REMOVED CORROSION, NDT'D AREA, FABBED AND INSTALLED REPAIRS AT FORWARD SIDE VERTICAL FLANGE FSSO 1261-1331 AND 1341 PER ECRA 477-57-118-2.Feb 22, 2007 · N477EV · Boeing 747SR46SDR 07FDEA00532Spar Cap · corrodedRT WING, REAR SPAR CAP FOUND TOP SURFACE AT XORS=1048 CORRODED. COMPLIED WITH FEDEX EA 1-5720-106595. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.Feb 21, 2007 · N601FE · Doug MD11SDR EIA2007048Spar · corrodedCORROSION ON FRONT SPAR WEB UNDER RIGHT WING JACK PAD FITTING AT WING STATION 1290. REMOVED CORROSION, NDT'D AREA, FABBED AND INSTALLED REPAIR PER ECRA 477-57-113-2.Feb 20, 2007 · N477EV · Boeing 747SR46SDR SAI020701Spar · crackedCRACKS WERE LOCATED OUT OF THE RADIUS GOING TO A RIVET ON ALL FOUR LOCATIONS OF THE MAIN SPAR WEB ABOVE THE UPPER MAIN SPAR CAP AT FS 154.50. THE FWD AND AFT MAIN SPAR WEB EXTENDS ABOVE THE CAP WHEN IT EXITS THE FUSELAGE AND FORMS A FLANGE WHERE THE UPPER SKIFeb 20, 2007 · N33NC · Cessna 402BSDR QXEA200700289Spar Cap · scratchedC4 PDX - FOUND RIGHT WING FRONT SPAR CAPS BOTH UPPER AND LOWER FROM STATION YW 171 TO YW 200 HAVE SCRATCHES IN AND NEAR THE BEND RADIUS. REPAIRED IAW RD8-57-1119, AND SRM 51-20-16, 51-20-36.Feb 16, 2007 · N366PH · Dhav DHC8202SDR UPS07849597Spar Cap · crackedINSPECTION TYPE:C3 DURING WING FORWARD SPAR INSPECTION FOUND 1EA ATTACHMENT HOLE CRACKED. REPAIRED LEFT WING FRONT SPAR LWR CAP BETWEEN XFS 515 AND 526.76 IAW SAA EA 008-5710-01-A0733, UPS EO DC8-5710-26430-A, AND FAA FORM 8100-9.Feb 14, 2007 · N811UP · Doug DC873FSDR QXEA200700259Spar · gougedC4 PDX - LEFT LEADING EDGE UPPER SPAR FLANGE HAS GOUGE AT STATION YW 288.0. REPAIRED IAW RD8-57-1119 AND RD8-57-3584.Feb 14, 2007 · N366PH · Dhav DHC8202SDR QXEA200700258Spar · gougedC4 PDX - LEFT LEADING EDGE UPPER SPAR FLANGE HAS GOUGE AT STATION YW 306.5. REPAIRED IAW RD8-57-3584 AND RD8-57-1119.Feb 14, 2007 · N366PH · Dhav DHC8202SDR UPS07849413Frame · crackedINSPECTION TYPE:C3 CRACK IN DRILL START IN FRAME ON OUTBOARD LWR SIDE OF NR 3 ENG STUB WING. STOP DRILLED CRACK IN FRAME AT RIGHT STUB WING STA 252.351 IAW SRM 54-2-0, AND SRM TR 54-38. FABRICATED AND INSTALLED REPAIR ANGLE AND DOUBLER AT RIGHT STUB WING STAFeb 13, 2007 · N701UP · Doug DC871FSDR 07FDEA00452Spar · crackedC/W EA 8-5710-102021 WING LT WING REAR SPAR WEB CRACK AT XORS 217 COMPLIED WITH EA 8-5710-102021 IAW SRM 57-10-00 FIG 52.Feb 12, 2007 · N372FE · Doug MD1010FSDR 07FDEA00390Spar · crackedON FRAME STA 1841 LEFT SIDE STRINGER 9L FOUND CRACK FROM ONE FASTNER HOLE THRU THE SECOND FASTENER HOLE (APROX 2"). REMOVED DOUBLER 2 CLIPS AND 2 INTERCOASTALS. RECEIVED FROM FAB ON T7/661087 AND T7/661086 2 DOUBLERS 7075T6 .080 T20631,193413. FAB 2 CLIPS FFeb 9, 2007 · N372FE · Doug MD1010FSDR 2007FA0000168Spar · crackedDURING REMOVAL OF LT WING FOR INSTALLATION OF WING FUEL TANK, A QUESTIONABLE PREVIOUS REPAIR WAS FOUND AT THE FRONT WOOD SPAR ROOT. FURTHER INVESTIGATION FOUND LONGNATUDINAL CRACKS OF THE LT AND RT, FOR AND AFT WOOD WING SPARS. THESE CRACKS WERE VISIBLE WITHFeb 6, 2007 · N6609H · Piper J3C65SDR 07FDEA00262Spar · corrodedOLD BLEND OUT REPAIR ON RT OUTER WING AT PANEL 3, BOTTOM SKIN, CLOSED TO RIB 28 ON REAR SPAR REPAIR WAS PERFORMED BY BLEND OUT THE CORROSION WITH CAL EO AB 6-57-00-0001 AND APPROVED BY RAS/BAE/0573/2002 ISS. AFeb 3, 2007 · N740FD · Airbus A300B4622RSDR 2007FA0000105Spar Cap · corrodedLT TOP WING SPAR CAPS AND TOP SKINS SEVERELY CORRODED IN AREA OF FACTORY NACELLE FUEL BLADDERS. LT-PN 5122031-1.Feb 2, 2007 · N465DL · Cessna T310RSDR CA070209019Spar · cracked(CAN) RT IB FLAP P/N 50-160003-97 REMOVED FOR HINGE BRACKET REPLACEMENT. UPON TEARDOWN OF FLAP FOR HINGE BRACKET REMOVAL, AN 8 INCH CRACK WAS NOTED ON THE SPAR UPPER RADIUS. THE CRACK EXTENDED 4 INCHES EITHER SIDE OF THE FLAP ACTUATOR BRACKET ATTACH AREA. PRJan 31, 2007 · Beech 100BEECHSDR 200600083Spar Cap · crackedWHILE PERFORMING THE REQUIREMENTS IN AD 2003-18-01, CRACKS WERE NOTED THRU-OUT THE WING. THE MAJOR CRACK IS A 4-5 INCH CRACK IN THE FWD LT LOWER SPAR CAP AFT ANGLE AT THE WING ATTACH POINT TO THE BELT FRAME. THE CRACK IS IN THE ANGLE (SPAR CAP AFT LEG), DOUBJan 31, 2007 · N2872G · Cvac PB4Y2SDR 200700105Spar Cap · crackedWHILE PERFORMING THE REQUIREMENTS IN AD 2003-18-01, CRACKS WERE NOTED THRU-OUT THE WING. THE MAJOR CRACK IS A 1.5 INCH CRACK IN THE FWD LT LOWER SPAR CAP AFT ANGLE AT THE WING ATTACH POINT TO THE BELT FRAME. THE CRACK IS IN THE ANGLE (SPAR CAP AFT LEG), DOUBJan 31, 2007 · N2871G · Cvac PB4Y2SDR CA070119010Spar · failed(CAN) DURING REPLACEMENT OF LOWER OB SKIN, EDGE DISTANCE OF RIVETS THROUGH LOWER FLANGE LESS THAN MINIMUM ALLOWED IN 32 PLACES FROM STAT. 100.0 TO STAT. 154.00 REPLACEMENT OF PARTS REQUIRED TO REPAIR PROBLEM. (TC NR 20070119010)Jan 16, 2007 · Cessna TU206GSDR CA070119009Spar · failed(CAN) EDGE DISTANCE OF RIVETS ON LOWER FLANGE LESS THAN MINIMUM ALLOWED. REPLACEMENT OF PART REQUIRED TO REPAIR PROBLEM. (TC NR 20070119009)Jan 16, 2007 · Cessna TU206GSDR 0700099995Spar · damagedDURING SPECIAL VISIT AIRCRAFT SUSTAINED DAMAGED FROM LT WING JACK. THE LT WING FRONT SPAR LOWER CHORD, LEADING EDGE LOWER DOUBLER AND LEADING EDGE RIB WERE DAMAGED. REPAIR WAS ACCOMPLISHED PER EA 99-208716 SECT I, SECTION II TO CALLS FOR A DETAILED FATIGUE AJan 16, 2007 · N8978E · Doug DC931SDR ABXA070020Spar Cap · corrodedLEFT WING LOWER OUTBOARD SPAR CAP CORRODED, RIVETS POPPED, CUPPED AND SKIN BULGING AT XRS 509. REPAIRED LEFT WING LOWER OUTBOARD SPAR CAP IAW REA D957-55323MR.Jan 12, 2007 · N971AX · Doug DC941SDR AMW1061010024Spar Cap · corrodedDURING STRUCTURAL INSPECTION, MAINTENANCE FOUND SOME BIO-CORROSION ON LT WING MAIN SPAR LOWER CAP BETWEEN WS 114 AND WS 124. REPAIRED IAW MFG FR-CO-01443 REV. 4 SPAR CAP PLUG INSTALLATION ACCOMPLISHED IAW MFG FR-CO-01444 REV 2 IN CONJUNCTION WITH MFG FR-CO-0Jan 10, 2007 · N127ZV · Beech 1900DSDR UPS07848998Spar Cap · crackedINSPECTION TYPE:C3 POSSIBLE CRACK AT NR 4 ALT BETWEEN LWR FRT SPAR CAP FLANGE AND STRINGER 64 JUST OUTBOARD XRS428. REMOVED, FABRICATED AND INSTALLED SPAR CAP FLANGE IAW SRM 51-1-20D & DWG 3644046.Jan 6, 2007 · N744UP · Doug DC871FSDR 07FDEA00021Spar Cap · corrodedLT WING, TRAILING EDGE REAR SPAR UPPER CAP LOWER SURFACE AT XORS= 1047 WAS FOUND WITH CORROSION. COMPLIED WITH FEDEX E.A. 1-5710-105595, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jan 4, 2007 · N579FE · Doug MD11FSDR 07FDEA00019Spar Cap · corrodedRT WING REAR SPAR UPPER CAP LOWER SURFACE FOUND CORROSION AT X0RS= 1047 TO X0RS= 1053. COMPLIED WITH FEDEX E.A.# 1-5710-105597, REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.Jan 3, 2007 · N579FE · Doug MD11FSDR 07FDEA00018Spar Cap · corrodedRIGHT WING REAR SPAR CAP UPPER SURFACE FOUND CORROSION AT XORS=1046. COMPLIED WITH FEDEX E.A. 1-5710-105597, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jan 3, 2007 · N579FE · Doug MD11FSDR UPS07849071Spar · crackedINSPECTION TYPE:C2 FOUND CRACK ON LOWER CENTER SPAR CHORD AND WEB JUST I/B OF XRS 255 NR 1 MAIN TANK. REPAIRED CRACKED SPAR CHORD AND WEB AT NR 1 MAIN TANK JUST I/B OF XRS 255 IAW SAA EA# 008-5710-01-A0595, UPS EO DC8-5710-25944-A, BAC SERV MSG NR 1-270145772Jan 2, 2007 · N744UP · Doug DC871FSDR 07FDEA00005Spar Cap · corrodedRT WING REAR SPAR LOWER CAP UPPER SURFACE FOUND CORROSION AT XORS 1050 TO 1059. REPAIRED AS PER FEDEX E.A. 1-5710-105596, REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.Jan 1, 2007 · N579FE · Doug MD11FSDR 07FDEA00004Spar Cap · corrodedRT WING REAR SPAR LOWER CAP UPPER SURFACE FOUND CORROSION AT XORS 1062 TO 1072. COMPLIED WITH FEDEX E.A. 1-5710-105596, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jan 1, 2007 · N579FE · Doug MD11FSDR 07FDEA00003Spar Cap · corrodedRT WING REAR SPAR LOWER CAP UPPER SURFACE FOUND CORROSION AT XORS 1075 TO 1082. COMPLIED WITH FEDEX E.A. 1-5710-105596, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2- 100.Jan 1, 2007 · N579FE · Doug MD11FSDR 07FDEA00002Spar · corrodedLT WING, TRAILING EDGE REAR SPAR LOWER CHORD AT XORS 1042 TO 1070 FOUND WITH CORROSION. COMPLIED WITH FEDEX E.A. 1-5710-105594, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jan 1, 2007 · N579FE · Doug MD11F
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