JASC 5711

Service difficulty reports · 5,586

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 FDEA201708282381Spar · crackedLEFT REAR SPAR INTERNAL ANGLE NR 62 HOLE FOUND CRACKED DURING AN NDT INSPECTION. REPAIRED IAW EA 6-5710-T0335292 P1. MAJOR REPAIR IAW GMM 6-2-100.Aug 28, 2017 · N811FD · Airbus A310324SDR FDEA201708282380Spar · crackedRIGHT REAR SPAR INTERNAL ANGLE NR 2 HOLE FOUND CRACKED DURING AN NDT INSPECTION. REPAIRED IAW EA 6-5710-T0335292 P1. MAJOR REPAIR IAW GMM 6-2-100.Aug 28, 2017 · N811FD · Airbus A310324SDR FDEA201708282379Spar · crackedRIGHT REAR SPAR INTERNAL ANGLE NR 8 HOLE FOUND CRACKED DURING AN NDT INSPECTION. REPAIRED IAW EA:6-5710-T0335292 P1. MAJOR REPAIR IAW GMM 6-2-100.Aug 28, 2017 · N811FD · Airbus A310324SDR FDEA201708282378Spar · crackedRIGHT REAR SPAR INTERNAL ANGLE, NR 14 HOLE FOUND CRACKED DURING AN NDT INSPECTION. REPAIRED IAW EA:6-5710-T0335292 P1. MAJOR REPAIR IAW GMM 6-2-100.Aug 28, 2017 · N811FD · Airbus A310324SDR 2017FA0000467Spar Cap · corrodedLEFT AND RIGHT WING REAR SPAR CAP CORROSION.Aug 26, 2017 · N958QS · Cessna 750SDR DALA2018051503329Spar · bentLT WING FRONT SPAR AT XFS=600 BENT LOWER CHORD.Aug 23, 2017 · N964DL · Doug MD88SDR SWAA2017083116043Spar · crackedCENTER WING SECTION REAR SPAR LOWER WEB CRACKED BETWEEN BAY 7L AND BAY 9L. REPAIRED WEB PER SRM.Aug 23, 2017 · N7843A · Boeing 737752SDR IPXA2017091321674Spar Cap · corrodedINSPECTION TYPE: 3C, LEFT WING REAR SPAR UPPER CAP AFT FLANGE CORRODED XORS 964 - 978. REPAIRED IAW EA 011-5710-01-A6982, REV IR, AND EO MD11-5710-65659-A.Aug 20, 2017 · N274UP · Doug MD11FSDR IPXA2017090621421Frame · crackedINSPECTION TYPE: 3C, LT WING LE FRAME CRACKED AT XORS. 683. REMOVED, FABRICATED, AND REPLACED THE LT WING LE FRAME IAW DWG ARB3954, AND SRM 51-33-01.Aug 20, 2017 · N274UP · Doug MD11FSDR EE4Y2017090304255Spar Web · damagedDURING A STRUCTURAL INSPECTION AT THE RT WING REAR SPAR WEB, FOUND TWO FASTENER HOLES ELONGATED AT RSS 206.11 AND RSS 273. THE ELONGATED FASTENER HOLES WERE REPAIRED IAW S/R 3-3949229341, AND EO COO-EO-2017-3990-R01.Aug 20, 2017 · N305GT · Boeing 7374H6SDR 2017F00129Spar · corrodedCENTER SPAR BULKHEAD FITTING CORROSION (4 AREAS).Aug 17, 2017 · N377QS · Cessna 680CESDR HYIA08242017001Spar Cap · corrodedWHILE REPAIRING A FUEL LEAK, CORROSION WAS DISCOVERED IN TWO PLACES INSIDE THE FUEL TANK, ON THE FORWARD RADIUS OF THE RT AFT OUTBOARD SPAR CAP. THE FIRST AREA OF CORROSION WAS DISCOVERED AT WS 208.1 AND WAS 1 INCH IN LENGTH. THE SECOND AREA WAS LOCATED AT WAug 15, 2017 · N771EA · Cessna 402CSDR SIMA20170805002Spar · crackedPERFORM HFEC INSPECTION ON LT WING SPAR I LOWER FLANGES AT RIB NR 9 IAW NDTM CRACK NOTED AND MARKED. ACCOMPLISHED REPAIR TO LT WING SPAR I LOWER FLANGE AT RIB 9 IAW ERS-EM-57MR-843.Aug 5, 2017 · N680AE · Emb EMB145LRSDR IPXA2017082921097Spar Cap · corrodedINSPECTION TYPE: 3C, LT WING REAR SPAR UPPER CAP HAS CORROSION BETWEEN XORS. 582.5 TO 589 AND XORS. 591.5 TO 598. REPAIRED THE LT WING REAR SPAR UPPER CAP IAW EA 011-5710-01-A6939, REV. I/R, AND EO MD11-5710-65339-A.Aug 3, 2017 · N254UP · Doug MD11FSDR SWAA2017082815916Spar · corrodedLEFT MAIN LANDING GEAR WHEEL WELL AT BOOST PUMP TANK 1 AFT, AFT SPAR CORRODED AT UPPER AND LOWER BONDING STRAPS. REPAIRED AFT SPAR IAW EA.Aug 3, 2017 · N741SA · Boeing 7377H4SDR EE4Y2017082204082Spar · crackedDURING THE STRUCTURAL INSPECTION, THE RT WING REAR SPAR WEB AND UPPER CHORD WERE FOUND WITH A CRACK AT RSS 224. THE AFFECTED WEB AND UPPER CHORD SECTIONS WERE REPAIRED IAW SRM 57-20-10, REPAIRS 4 AND 6.Aug 1, 2017 · N305GT · Boeing 7374H6SDR EE4Y2017082204080Spar · crackedDURING THE STRUCTURAL INSPECTION THE LT WING REAR SPAR UPPER CHORD WAS FOUND CRACKED AT RSS 223, THE AFFECTED SPAR SECTION WAS REPAIRED IAW SRM 57-20-10, REPAIR 4.Aug 1, 2017 · N305GT · Boeing 7374H6SDR SWAA2022012884220Web · corrodedRIGHT WING FRONT SPAR AFT OF #3 KREUGER FLAP; SPAR H AS CORROSION AT FUEL BOOST PUMP UPPER AND LOWER BOND ING STRAPS. / RIGHT WING FRONT SPAR AFT OF #3 KREUGER FLAP SPAR HA S CORROSION AT FUEL BOOST PUMP UPPER AND LOWER BONDI NG STRAPS. REPAIRED I/A/W EA 17031Jul 19, 2017 · N754SW · Boeing 7377H4SDR FDEA201707151956Spar · crackedRIGHT WING REAR SPAR INTERNAL ANGLE NR 60 HOLE, NDT INSPECTION FOUND A CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0334453, P1. MAJOR REPAIR IAW GMM 6-2-100.Jul 15, 2017 · N808FD · Airbus A310324SDR FDEA201707151951Spar · crackedRIGHT WING REAR SPAR INTERNAL ANGLE NR 16 HOLE, NDT INSPECTION FOUND CRACK SIGNAL. COMPLED WITH EA 6-5710-T0334453, P1. MAJOR REPAIR IAW GMM 6-2-100.Jul 15, 2017 · N808FD · Airbus A310324SDR FDEA201707151950Spar · crackedRIGHT WING REAR SPAR INTERNAL ANGLE NR 12 HOLE, NDT INSPECTION FOUND A CRACK SIGNAL. COMPLED WITH EA 6-5710-T0334453, P1. MAJOR REPAIR IAW IAW GMM 6-2-100.Jul 15, 2017 · N808FD · Airbus A310324SDR FDEA201707151949Spar · crackedRIGHT REAR SPAR INTERNAL ANGLE NR 7 HOLE, NDT INSPECTION FOUND A CRACK SIGNAL. COMPLED WITH EA 6-5710-T0334453, P1. MAJOR REPAIR IAW GMM 6-2-100.Jul 15, 2017 · N808FD · Airbus A310324SDR FDEA201707151948Angle · crackedLEFT REAR SPAR INTERNAL ANGLE NR 61 HOLE, NDT INSPECTION FOUND A CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0334453 P1. MAJOR REPAIR IAW GMM 6-2-100.Jul 15, 2017 · N808FD · Airbus A310324SDR FDEA201707151947Spar · crackedLEFT WING REAR SPAR INTERNAL ANGLE NR 13 HOLE, NDT INSPECTION FOUND A CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0334453 P1. MAJOR REPAIR IAW GMM 6-2-100.Jul 15, 2017 · N808FD · Airbus A310324SDR FDEA201707151946Angle · crackedLEFT REAR SPAR INTERNAL ANGLE NR 53 HOLE, NDT INSPECTION FOUND A CRACK SIGNAL. REAM THE HOLE IAW SRM 51-40-44, PERFORM ROTOTEST INSPECTION OF THE HOLE IAW NTM51-10-01 & NTM51-10-18 AND NO CRACK FOUND. WET INSTALLED A FASTENER IAW SRM 51-40-21 & EO 6-5710-7Jul 15, 2017 · N808FD · Airbus A310324SDR FDEA201707151957Spar · crackedRIGHT REAR SPAR INTERNAL ANGLE NR 63 HOLE NDT INSPECTION FOUND CRACK SIGNAL. RIGHT REAR SPAR INTERNAL ANGLE 63 HOLE NDT INSPECTION FOUND CRACK SIGNAL. REAM THE AFFECTED HOLE THROUGH ALL LAYERS STEP BY STEP WITH INCREASING DIA OF 0.4 MM IAW SRM 51-40-44, PERJul 15, 2017 · N808FD · Airbus A310324SDR FDEA201707151955Spar · crackedRIGHT WING REAR SPAR INTERNAL ANGLE NR 38 HOLE, NDT INSPECTION FOUND A CRACK SIGNAL. REAMED THE HOLE IAW SRM 51-40-44, PERFORM ROTOTEST INSPECTION IAW NTM 51-10-01, & NTM 51-10-18 AND NO CRACK FOUND. WET INSTALLED A FASTENER IAW SRM 51-40-21, & 6-5710-7-3Jul 15, 2017 · N808FD · Airbus A310324SDR FDEA201707151954Spar · crackedRIGHT WING REAR SPAR INTERNAL ANGLE NR 35 HOLE, NDT INSPECTION FOUND A CRACK SIGNAL. REAMED THE HOLE IAW SRM 51-40-44, PERFORM ROTOTEST INSPECTION IAW NTM 51-10-01, & NTM 51-10-18 AND NO CRACK FOUND. WET INSTALLED A FASTENER IAW SRM 51-40-21, & EO 6-5710Jul 15, 2017 · N808FD · Airbus A310324SDR FDEA201707151953Spar · crackedRIGHT WING REAR SPAR INTERNAL ANGLE NR 33 HOLE, NDT INSPECTION FOUND A CRACK SIGNAL. REAMED THE HOLE IAW SRM 51-40-44, PERFORM ROTOTEST INSPECTION OF THE HOLE IAW NTM51-10-01, & NTM51-10-18 AND NO CRACK WAS FOUND. WET INSTALLED A FASTENER IAW SRM 51-40-21, Jul 15, 2017 · N808FD · Airbus A310324SDR FDEA201707151952Spar · crackedRIGHT REAR SPAR INTERNAL ANGLE NR 30 HOLE, NDT INSPECTION FOUND A CRACK SIGNAL. REAM THE HOLE IAW SRM 51-40-44, PERFORM ROTOTEST INSPECTION OF THE HOLE IAW NTM51-10-01 & NTM51-10-18 AND NO CRACK FOUND. WET INSTALLED A FASTENER IAW SRM 51-40-21 & EO 6-571Jul 15, 2017 · N808FD · Airbus A310324SDR FDEA201707151945Spar · crackedLEFT REAR SPAR INTERNAL ANGLE NR 35 HOLE NDT INSPECTION FOUND A CRACK SIGNAL. REAMED THE AFFECTED HOLE THROUGH ALL LAYERS IAW SRM 51-40-44, PERFORM ROTOTEST INSPECTION OF THE HOLE IAW NTM51-10-01 & NTM51-10-18 AFTER EACH STEP AND NO CRACK FOUND. WET INSTAJul 15, 2017 · N808FD · Airbus A310324SDR JGVR20170714003Spar · corrodedSEVEN SPOTS OF CORROSION ON THE LT WING AFT SPAR ANGLE IN THE FLAP WELL AT APPROX WS 77.5. MECHANICALLY REMOVED CORROSION IAW SRM 51-70-08. THIS IS A PSE AREA IAW SRM 51-00-04. CORROSION IS BEYOND LIMITS IAW 51-10-01.Jul 12, 2017 · N557QS · Cessna 560XLSDR JGVR20170714001Spar Cap · corrodedCORROSION ON LEFT LOWER SPAR CAP, PSE AREA BEHIND WHEEL WELL PANEL 512DB. CORROSION IS BEYOND LIMITS IAW SRM 51-10-01 AND DESCRIPTION 4 OF GMM 2.2.2. REPAIRED ER 5559/07RD WITH SUBMITTAL LETTER REPORT NR 17-1732 FORM 8100-9.Jul 12, 2017 · N557QS · Cessna 560XLSDR DALA2017071205364Spar · crackedDURING REMOVAL OF OUTBD FLIGHT SPOILER LOCKED TOOL ONE CRACK WAS MADE TO RT WING AFT SPAR MEMBRANE BTW STA XRS=350 AND XRS=355. RT WING AFT SPAR MEMBRANE BTW STA XRS=350 AND XRS=355 WAS REPAIRED PER ETI -17-17-097 REV 2 AND ER/A 559526-14 REV ORIG.Jul 11, 2017 · N980AT · Boeing 717200SDR KO0R201707060031Spar · damagedZONE 518, LEFT WING LEADING EDGE SPAR AREA HAS SCRAPES AND CORROSION ON THE LEADING EDGE OF THE SPARJul 6, 2017 · N435KD · Doug MD11FSDR FDEA201707041848Former · crackedRT WING LEADING EDGE INTERIOR, FOUND THE FORMER AT XOS 584 CRACKED. REMOVED AND REPLACED IAW SRM 51-31-01-0G.Jul 4, 2017 · N522FE · Doug MD11FSDR 2017FA0000267Spar · corrodedREPAIR OF CORROSION ON CENTER SPAR WEBS NEAR WS 39.90. REF CESSNA ENGINEERING REPORT S-680-0081/RD REV A AND FAA 8100-9 DATED 3-20-2017. WORK RECORD ON FILE AT THIS FACILITY UNDER WORK ORDER 48500.Jun 30, 2017 · N369QS · Cessna 680CESDR B4VR2017060700001Spar · delaminatedMULTIPLE DELAMINATED AREAS NOTED ALONG THE FORWARD AND AFT SIDES OF THE AFT (MAIN) CARRY THROUGH SPAR. VARIOUS SIZES AND LOCATIONS NOTED. PICTURES SENT TO SDR PROGMGR.Jun 6, 2017 · N372SE · Diamon DA40SDR B4VR201706070002Spar · delaminatedMULTIPLE DELAMINATED AREAS NOTED ALONG THE FORWARD AND AFT SIDES OF THE AFT (MAIN) CARRY THROUGH SPAR. VARIOUS SIZES AND LOCATIONS NOTED. PICTURES SENT TO SDR PROGRAM MANAGER.Jun 6, 2017 · N4174B · Diamon DA40SDR FQAR20170601029Doubler · damagedTHE AIRCRAFT WAS UNDERGOING INSPECTION OF THE WING SPAR IAW SB 978A. DAMAGE TO THE RIGHT WING LOWER AFT SPAR DOUBLER WAS NOTED DURING VISUAL INSPECTION. THE DAMAGE IS A RESULT OF IMPROPER WASHERS INSTALLED WHEN WINGS WERE LAST REINSTALLED ON AIRCRAFT. THE CORJun 1, 2017 · N926PA · Piper PA28181SDR 2017FA0000228Spar · corrodedLEFT WING AFT SPAR WEB FEED THRU FITTING CORRODED.Jun 1, 2017 · N350QS · Cessna 680CESDR B4VR201706010001Spar · crackedMULTIPLE SUBSURFACE CRACKS ALONG THE AFT, MAIN CARRY THROUGH SPAR ON THE FORWARD SURFACE BOTH RIGHT AND LEFT SIDES. CRACKS RANGE FROM .5 TO 3 INCHES AND COVER MOST OF THE FACE OF THE SPAR.May 31, 2017 · N4139B · Diamon DA40SDR COEA2017052847923Spar · damagedRIGHT WING FRONT SPAR UPPER FLANGE HAS TWO WORN HOLES AT RIB 10. REPAIRED THE SPAR IAW ES-2663/17.May 28, 2017 · N923FX · Aerosp ATR42300SDR FQAR20170524028Spar · corrodedWING SPAR INSPECTION WAS BEING UNDERTAKEN AS PART OF AN AGING/HIGH TIME AIRCRAFT INSPECTION. WHEN THE WINGS WERE REMOVED FROM AIRCRAFT TO FACILITATE INSPECTION, DAMAGE TO THE RIGHT SIDE OF THE SPAR BOX ASSY IN THE FUSELAGE WAS SEEN. DAMAGE APPEARED TO BE FROM May 24, 2017 · N4177L · Piper PA28181SDR IPXA2017060818030Spar · corrodedINSPECTION TYPE: 2C, LEFT WING UPPER T/E SKIN AND ADJACENT REAR SPAR UPPER CAP AFT FLANGE CORRODED XORS 653 - 672. REPAIRED IAW EA 011-5730-01-A6823, REV IR, AND EO 5710-64482-A.May 22, 2017 · N271UP · Doug MD11FSDR IPXA2017060617966Spar Cap · corrodedINSPECTION TYPE: 2C, LEFT WING REAR SPAR UPPER CAP AFT FLANGE CORRODED XORS 551 - 565. REPAIRED THE SPAR CAP IAW EA 011-5710-01-A6821, REV IR, AND EO MD11-5710-64468-A.May 22, 2017 · N271UP · Doug MD11FSDR IPXA2017060617964Spar Cap · corrodedINSPECTION TYPE: 2C, LEFT WING REAR SPAR UPPER CAP AFT FLANGE CORRODED XORS 1039 - 1049. REPAIRED THE SPAR CAP IAW EA 011-5720-01-A6822, REV IR, AND EO MD11-5710-64477-A.May 22, 2017 · N271UP · Doug MD11FSDR IPXA2017060617983Spar Cap · corrodedINSPECTION TYPE: 2C, RT WING REAR SPAR UPPER CAP HAS CORROSION BETWEEN XORS.542 - 547 AND XORS 556.5 - 572.5. REPAIRED THE SPAR CAP IAW EA 011-5710-01-A6820, REV I/R, AND EO MD11-5710-64472-A.May 22, 2017 · N271UP · Doug MD11FSDR IPXA2017060517928Spar Cap · corrodedINSPECTION TYPE: 2C, RT WING REAR SPAR UPPER CAP HAS CORROSION BETWEEN XORS 486 - 492. REPAIRED THE SPAR CAP IAW EA 011-5710-01-A6816, REV I/R, AND EO MD11-5730-64428-A.May 22, 2017 · N271UP · Doug MD11FSDR UIEA2017042600640Spar · corrodedCORROSION ON LT WING FRONT SPAR ON FSS 1440. REMOVED CORROSION.May 16, 2017 · N464MC · Boeing 747446
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