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 CALA2011121700814Spar · corrodedRIGHT WING L/E FRONT SPAR WEB FOUND CORRODED AT OFSS 455 TO OFSS 460. CORROSION REMOVED AND REPAIRED AS PER EC/RA 5721-01326 REV_- HFEC, NO CRACK FOUND.Dec 17, 2011 · N13227 · Boeing 737824SDR COEA2011120634801Spar · damagedHEAVY CK COE / MAJOR REPAIR/ LT WING REAR LOWER SPAR FLANGE TO LOWER SKIN PANEL HAS A GOUGE WITH POSSIBLE PREVIOUS BLENDING. SUBMITTED TO ATR / REPAIR PER STRUCTURAL REPAIR INSTRUCTIONS.Dec 6, 2011 · N801FX · Aerosp ATR72212SDR DALA1503889235Spar · crackedWING REAR SPAR CRACKED, REPAIRED IAW AA 5710-01119.Dec 5, 2011 · N935DN · Doug MD9030SDR ECPR2014061150605Spar · corrodedLT WING STA 56.0, UPPER OTBD QUADRANT OF AN ELECTRICAL WIRE PASSING THROUGH HOLE IN THE WING SPAR WEB WAS FOUND CORRODED. PASS THROUGH HOLE, WHICH IS IN THE LANDING GEAR WHEEL WELL AREA, HAD A CATEPILLAR GROMMET INSTALLED TO PREVENT THE WIRES FROM CHAFING. THDec 5, 2011 · N7701A · Piper PA44180SDR DALA1516970992Spar · crackedWING REAR SPAR CRACKING AT XRS 164 REPAIRED IAW AA 5710-01110.Nov 27, 2011 · N992DL · Doug MD88SDR UALA2011112706497Spar · corrodedLEFT WING REAR SPAR WEB CORRODED BETWEEN IRSS 340 AND 350 AT FUEL PUMP. REMOVED CORROSION, AREA CRACK FREE BY HFEC. FLAP PEENED AREA & AND RESTORED FINISH PER 777EN-57-0219 AND FAA FORM 8100-9.Nov 24, 2011 · N784UA · Boeing 777222SDR UALA2011112706496Spar · corrodedRIGHT WING REAR SPAR WEB CORRODED BETWEEN IRSS 340 AND 350 AT FUEL BOOST PUMP. REMOVED CORROSION, AREA CRACK FREE BY HFEC. FLAP PEENED AREA, RESTORED FINISH PER 777EN-57-0218 AND FAA FORM 8100-9.Nov 24, 2011 · N784UA · Boeing 777222SDR QXEA2011112801253Spar · crackedRT INBD SPAR FITTING FOUND CRACKED. FERRIED ACFT TO COE FOR REPAIRS.Nov 24, 2011 · N420QX · Bombdr DHC8402SDR FOTR2011112315020Spar · corrodedLT WING T/E LOWER AFT SPAR CAP CORRODED OTBD OF AILERON. REPAIRED ON FASI WO 21186, NR 15020.Nov 23, 2011 · N794AG · Doug DC982SDR FOTR2011112315114Spar · corrodedLT WING STA XRS 454 APPROX REAR SPAR LOWER SPAR CHORD HAS CORROSION. REPAIRED ON FASI WO 21186, NR15114.Nov 23, 2011 · N794AG · Doug DC982SDR UALA2011111506238Spar · corrodedRIGHT WING REAR SPAR CORROSION BETWEEN IRSS 340 AND 350 AT FUEL BOOST PUMP. BLEND, DPI, HFEC IAW 777EN-57-0212.Nov 15, 2011 · N218UA · Boeing 777222SDR GLBA20111115FSpar Cap · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE LT WING FRONT SPAR CAP AT RIB 17, 1 INCH IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-120-57-004. MATERIALS UTILIZED ARE INCLUDED IN THE ENGINNov 15, 2011 · N71GL · Emb EMB120ERSDR UALA2011111406203Spar · corrodedLEFT WING REAR SPAR CORR BETWEEN IRSS 340 AND 350 AT FUEL BOOST PUMP. BLEND, DPI, HFEC IAW AMECO 777EN-57-0213.Nov 13, 2011 · N218UA · Boeing 777222SDR DALA1511840908Spar · crackedWING REAR SPAR CRACKING AT XRS 164. REPAIRED IAW AA 5710-01110.Nov 8, 2011 · N908DL · Doug MD88SDR TX9Y20111111005Shear Tie · crackedWING CENTER SECTION FRONT SPAR LOCATION RBBL 33.89 SHEAR TIE (P/N:69B14267-9) WAS FOUND CRACK. A NEW SHEAR TIE WAS FABRICATED AS PER DRAWING 69B14267-9. THE REWORK OF TWO TAPER HOLES WAS PERFORMED PER BOEING MESSAGE NUMBER TEC-SOF-11-0096 AND SRM 51-30-05. DENov 8, 2011 · N783SA · Boeing 747281FSDR FDEA201111024731Spar · crackedCOMPLY WITH EA 6-5710-150047 REAR SPAR LOWER FLANGE AT FR 47. EXISTING CRACK REPAIR AT HOLE G LT SIDE COMPLIED WITH EA 6-5710-150047 REAR SPAR LOWER FLANGE AT FR 47.Nov 2, 2011 · N745FD · Airbus A300B4622RSDR FDEA201111024730Spar · crackedCOMPLY WITH EA 6-5710-150054 COMPLIED WITH EA 6-5710-150054 - WINGS - CTR WING BOX - AD 2005-23-08. REAR SPAR LOWER FLANGE AT FRAME 47, EXISTING CRACK REPAIR AT HOLES LT SIDE.Nov 2, 2011 · N726FD · Airbus A300B4622RSDR REXA201100752Spar · damagedNR 30 HOLE DRILLED IN LT FWD SPAR FLANGE AT WS 349. REPAIRED IAW BOMBARDIER REO 601R-57-21-1539.Nov 2, 2011 · N8908D · Cndair CL6002B19SDR CALA2011110200706Spar · corrodedLT WING HAS FRONT SPAR CORROSION AT OFSS 308. NOTED: LT WING FRONT SPAR WEB OFSS 303 TO OFSS 337 REPAIRED AS PER EC/RA 5721-01319 REV A PART 1 AND HFEC NIL CRACK FOUND ATTACH MAINTENANCE SHEET FORM 44.0008 ITEM 1 TO 62 ACCOMPLISHED.Nov 2, 2011 · N14249 · Boeing 737824SDR 2011FA0000723Spar · crackedINSPECTION OF FLEET ACFT SN IN THE BC AND BD RANGE HAVE REVEALED CRACKING OF THE MAIN WING SPAR WEB IN CARRY THROUGH OPENINGS AND END CAP SUPPORTS. IN THE WHEEL WELL AREA, THERE ARE 2 OPENINGS IN THE WING SPAR WEB FOR FUEL AND HYD LINE PASSAGE. ONE OPENING IS Nov 2, 2011 · Beech A200SDR DALA1516060907Spar · crackedWING REAR SPAR CRACKING AT XRS 164, REPAIRED IAW AA 5710-01110.Oct 31, 2011 · N907DL · Doug MD88SDR HYIA20111031001Spar Cap · corrodedDURING HEAVY CHECK CORROSION ZL-532-GVI-10000, 572220-DVI-10000, SPOTS WERE FOUND ON LT WING AT AFT SPAR UPPER CAP VERTICAL FLANGE BETWEEN RIBS 24-26. CORROSION WAS REMOVED AND DAMAGES BLENDED IAW PREVIOUS SRI. REVIEWED REPAIRS AND ISSUED STRUCTURAL REPAIR AOct 31, 2011 · N42836 · Aerosp ATR42320SDR CALA2011102700687Spar · corrodedLEFT WING HAS FRONT SPAR CORROSION AT OF SS 689. NOTED LT WING HAS FRONT SPAR AT CORRECT OFSS 668. CORROSION REMOVED & AMP; REPAIRED AS PER ECRA 5721-01320 REV- . HFEC NO CRACK FOUND ATTACH FORM 44.0008 ITEM 1-13 ACCOMPLISHED.Oct 27, 2011 · N14249 · Boeing 737824SDR CALA2011102700686Spar · corrodedRT WING FRONT SPAR SURFACE FOUND CORRODED AT OFFS 721. RT WING FRONT SPAR AT OFSS 721 SURFACE CORRSION REMOVED AREA REPAIRED AS PER EC/RA 5710-02203 REV - AND HFEC NIL CRACK FOUND ATTACH MAINTENANCE WORKSHEET FORM 44.0008 ITEM 1 TO ITEM 12 ACCOMPLISHED.Oct 27, 2011 · N14249 · Boeing 737824SDR DALA1508300906Spar · crackedWING REAR SPAR CRACKING AT XRS 164. REPAIRED IAW AA 5710-01110.Oct 25, 2011 · N906DL · Doug MD88SDR DALA1162290906Spar Cap · crackedFOUND 1.2 INCH CRACK IN RT WING LOWER SPAR CAP WHILE PERFORMING INSPECTION PER EA 09-471576-12 AD REV A OPN NR 0502. INSTALLED REPAIR PER EA 09-471576-12 AD REV A ME06 OPN NR 0601 AND DRAWING J060271 (TEMPORARY REPAIR).Oct 25, 2011 · N906DL · Doug MD88SDR FDEA201110254643Spar Cap · crackedRT WING REAR SPAR LOWER CAP EO 8-5710-7-5007, PT 2 INSP FOUND CRACK AT FWD, OTBD HOLE COMPLIED WITH EA 8-5710-156726 FOR RT WING REAR SPAR LOWER CAP REPAIR OF FWD OTBD HOLE.Oct 25, 2011 · N68054 · Doug MD1010FSDR FDEA201110204592Spar · damagedLT WING REAR SPAR UPPER FITTING FOUND SHIM MIGRATION AT LBL 70.5. REPAIR CARRIED OUT ON LEFT WING REAR SPAR AT LBBL 70.5 AS PER E.A. F- 5740-152567 PT 1. REPAIR IS CLASSIFIED AS MAJOR.Oct 20, 2011 · N951FD · Boeing 757236SDR HYIA201110200002Spar · corrodedLT WING-AFT SPAR LOWER CAP HORIZ FLANGE CORROSION BETWEEN RIBS 18-19. DAMAGE BEYOND THE LIMITS IAW THE SRM. DAMAGED SPAR CAP REPLACED IAW REPAIR.Oct 20, 2011 · N42836 · Aerosp ATR42320SDR IPXA1M70047Former · crackedINSPECTION TYPE:2C, RT WING FIXED L/E SUPPORT ANGLE (FORMER) CRACKED STA XOS 960. REMOVED FABRICATED AND INSTALLED REPLACEMENT IAW DWG ARB2920 AND SRM 51-31-01, 51-33-01, 51-35-01.Oct 13, 2011 · N275UP · Doug MD11FSDR HALA2011101200469Former · crackedLT WING OSS 499.603 NOSE FORMER CRACKED ON UPPER SURFACE ATTACH FASTENER LOCATION. NOSE FORMER INSTALLED UNDER A PULL UP LOAD. POSSIBLY USING LIQUID/PEELABLE SHIM TO REMOVE MISMATCH & PULL-UP ISSUES. UPPER SURFACES FASTENERS TO BE FULLY PULLED UP INTO POSITOct 12, 2011 · N582HA · Boeing 76733ASDR UIEA2011102100619Spar Cap · corrodedCORROSION ON SPAR CAP STA 176.000. REMOVED LIGHT CORROSION BETWEEN FASTENERS PERFORMED LT THICKNESS INSPECTION FOUND TO BE WITHIN LIMITS. TREATED AND PRIMED AREA.Oct 8, 2011 · N641GT · Boeing 76738ESDR QXEA2011101000961Access Panel · corrodedSUSPECTED SURFACE FRETTING CORROSION ON RT WING FUEL TANK ACCESS PANEL 624AT. REMOVED CORROSION IAW RD 8/4-57-442. NDT PERFORMED ON PANEL, CONFIRMED CRACK FREE AND FOUND TO BE WITHIN LIMITS PER RD 8/4-57-442, MINIMUM THICKNESS REMAINING IS .115". ALODINED AOct 6, 2011 · N403QX · Bombdr DHC8402SDR HYIA20110927002Spar Cap · corrodedDURING HEAVY CHECK INSP RT WING AFT SPAR UPPER CAP WAS CORRODED REF:ZL-632-GVI-10000/572220-DVI-10000 BEYOND LIMITS IAW THE SRM 57-22-00. DAMAGE WAS SUBMITTED THEN ISSUED S.R.I. DO/TS-3027/11-15459. REPAIR WAS PERFORMED BY TECH SERVICES UNDER W/O 17010, TASKSep 27, 2011 · N42836 · Aerosp ATR42320SDR IPXA1M70206Spar Cap · corrodedINSPECTION TYPE:4C LT WING UPPER T/E FILLER STRIP BULGING BETWEEN XORS 980-995. REPAIRED CORROSION ON UPPER AFT FLANGE OF LT WING REAR SPAR IAW STA SA EA 011-5710-01-A3539 REV IR AND EO MD11-5710-44714-A.Sep 26, 2011 · N258UP · Doug MD11FSDR IPXA11M70193Spar · corrodedINSPECTION TYPE:4C, RT WING UPPER T/E FILLER STRIP BULGING AT XORS 1042. REPAIRED CORROSION ON UPPER AFT FLANGE OF RT WING REAR SPAR BETWEEN XORS 1030-1042 IAW STA SA EA 011-5710-01-A3537 REV IR & EO MD11- 5710-44978-A.Sep 26, 2011 · N258UP · Doug MD11FSDR ASOA201101798Spar · crackedUPON REMOVAL OF RT T/E SKIN PANEL, FOUND CAP ANGLE CRACKED. REMOVED DAMAGED RT T/E SKIN PANEL CAP ANGLE IAW SRM 51-42-21. LOCATED AND DRILLED UP NEW SERVICEABLE CAP ANGLE IAW SRM 51-40-11 AND INSTALLED SAME IAW SRM 51-42-21. THIS REPAIR REQUIRES MAJOR/MINOR Sep 23, 2011 · N838AS · Cndair CL6002B19SDR DALA1510629230Spar · crackedWING REAR SPAR CRACKED. REPAIRED IAW AA 5710-01119.Sep 22, 2011 · N930DN · Doug MD9030SDR IPXA1M69642Spar Cap · corrodedINSPECTION TYPE:3C, INTERGRANULAR CORROSION ON RT WING AFT SPAR T-CAP STA XORS580. REPAIRED CORROSION ON RT WING REAR SPAR UPPER CAP VERTICAL LEG BETWEEN XORS 570-590 IAW STA SA EA 011-5710-01-A3490 REV IR & EO MD11-5710-44570-A.Sep 22, 2011 · N272UP · Doug MD11FSDR IPXA1M69636Spar · corrodedINSPECTION TYPE:3C RT WING UPPER T/E FILLER STRIP BULGING BETWEEN XORS646-657. REPAIRED CORROSION ON UPPER AFT FLANGE OF RT WING REAR SPAR BETWEEN XORS 634-657 IAW STA SA EA 011-5710-01-A3497 REV IR AND EO MD11- 5710-44585-A.Sep 22, 2011 · N272UP · Doug MD11FSDR IPXA1M69583Spar · corroded3C CHECK, RT WING UPPER T/E FILLER STRIP BULGING BETWEEN XORS 548-559. REPAIRED CORROSION ON RT WING REAR SPAR UPPER AFT FLANGE BEWTEEN XORS 550-562 IAW STA SA EA 011-5710-01-A3495 & EO MD11-5710-44571-A.Sep 22, 2011 · N272UP · Doug MD11FSDR DALA1154893761Support Fitting · corrodedDURING TRIPLE GEAR CHANGE EA 12-487906-12 REV A ME 03 OPN 0301 WAS WORKED. CORROSION WAS FOUND ON THE INBOARD SURFACE OF THE INBOARD LUG OF SUPPORT FITTING ON REAR SPAR OF LEFT WING WHERE THE MLG FWD TRUNNION BLOCK ATTACHES WITH FUSE PINS. REPAIRED PER B737-Sep 22, 2011 · N3761R · Boeing 737832SDR DALA1154883761Support Fitting · corrodedDURING TRIPLE GEAR CHANGE EA 12-487906-12 REV A ME 06 OPN 0601 WAS WORKED. CORROSION WAS FOUND ON THE UPPER INBOARD FACE OF SUPPORT FITTING ON REAR SPAR OF THE RIGHT WING WHERE THE MLG FWD TRUNNION BLOCK ATTACHES TO FUSE PINS. REPAIRED PER B737-800 SRM 57-20Sep 22, 2011 · N3761R · Boeing 737832SDR 2011FA0000609Spar · 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 TSep 20, 2011 · N4316U · Piper PA44180SDR DALA1152893757Support Fitting · corrodedDURING TRIPLE GEAR CHANGE, EA12-487906-12 REV A MEO6 OPN 0601 WAS WORKED. CORROSION ON THE OUTSIDE FACES-I/B AND O/B OF SUPPORT FITTING ON THE REAR SPAR WAS FOUND IN STEP 3. REPAIRS ON N/R CARDS NR 1&2.Sep 12, 2011 · N3757D · Boeing 737832SDR DALA1152883757Support Fitting · corrodedDURING TRIPLE GEAR CHANGE EA 12-487906-12 REV A MEO3 OPN.0301 WAS WORKED. CORROSION ON THE OUTSIDE FACES -I/B AND O/B OF SUPPORT FITTING ON THE REAR SPAR WAS FOUND IN STEP 3. REPAIRS C/W ON N/R CARD NR 3 LT SIDE.Sep 12, 2011 · N3757D · Boeing 737832SDR HYIA20110910001Spar Cap · corrodedDURING HEAVY CHECK INSP ZL-530/533-GVI-10000, 5722220-DVI-10000, CORROSION WAS FOUND ON RT WING AFT SPAR LOWER CAP VERTICAL FLANGE BETWEEN RIBS 24 AND 25. CORROSION WAS REMOVED, BLENDED AND INSPECTED USING UT INSP. REMAINING THICKNESS WAS SUBMITTED FOR EVAULSep 10, 2011 · N42836 · Aerosp ATR42320SDR IPXA11M69269Former · crackedINSPECTION TYPE:3C, LT WING XOS 1025 PANEL LANDING BRACKET (FORMER) CRACKED BETWEEN AFT FASTENERS. REMOVED, FABRICATED, & INSTALLED REPLACEMENT FORMER IN LT WING FIXED L/E INTERIOR AT STA XOS1025 IAW SRM 51-35-01, 51-33-01, AND DWG ARB2920.Sep 6, 2011 · N295UP · Doug MD11FSDR FDEA201109013618Spar Cap · corrodedLT WING REAR SPAR UPPER CAP XORS 1042 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-21-01, REV 47. ORIGINAL MATERIAL THICKNESS = 0.145"; MATERIAL REMOVED= 0.032"; MATERIAL REMAINED = 0.113" - FOUND OUT OF LIMITS IAW SRM 57-00-10, REV 47, FIG 101. ACCOMPLISHSep 1, 2011 · N643FE · Doug MD11FSDR FDEA201109013617Spar Cap · corrodedLT WING REAR SPAR UPPER CAP FORWARD OF NR 4 SPOILER FOUND CORRODED. CORROSION REMOVED IAW SRM 51-21-01 AND FOUND OUT OF LIMITS IAW SRM 57-00-10, REV 47, FIG 201. ORIGINAL MATERIAL THICKNESS = 0.290"; MATERIAL REMOVED = 0.060"; MATERIAL REMAINED = 0.230". RSep 1, 2011 · N643FE · Doug MD11F
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