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 HYIA20140628002Spar Cap · corrodedDURING SCHEDULED INSPECTION, AREAS OF EXFOLIATING CORROSION WAS FOUND AT RT WING LWR FWD SPAR CAP STRAP OEM PN 5292029-2 PREVIOUSLY INSTALLED TO SATISFY REQUIREMENT OF AD2005-12-13 CONCURRENT WITH MEB05-2 AS TERMINATING ACTION FOR AD2005-05-52. THE DAMAGE HASJun 26, 2014 · N375R · Cessna 402CSDR HYIA20140628001Spar Cap · corrodedDURING SCHEDULED INSPECTION, AREAS OF EXFOLIATING CORROSION WAS FOUND AT LT WING LWR FWD SPAR CAP STRAP OEM PN 5292029-1 PREVIOUSLY INSTALLED TO SATISFY REQUIREMENT OF AD2005-12-13 CONCURRENT WITH MEB05-2 AS TERMINATING ACTION FOR AD2005-05-52. THE DAMAGE HASJun 26, 2014 · N375R · Cessna 402CSDR ABXA20140624240Splice Plate · corrodedRIGHT WING LOWER LE FALSE SPAR CRACKED AT NR 9 SLAT AREA NEAR OTBD AUX TRACK. REMOVED DAMAGED SECTION OF RT WING LE LOWER SPLICE PLATE AT LES 612 - 708. FABRICATED NEW SECTION IAW REA B654-61068, INSTALLED NEW SECTION AT SPLICE PLATE IAW SRM 51-40-02 & REA BJun 24, 2014 · N792AX · Boeing 767200SDR R61A201406230857Spar · chafedDURING HEAVY CHECK, HYD PRESSURE LINE JAMNUT LOOSE & CHAFING ON SPAR 3 LT WING JUST OTBD OF RIB 4. MX LT SPAR 3, FCBS57-10-00-001, BETWEEN RIB 4A-6 WAS REPAIRED IAW ETD 2014-170-053811, REV B. FOR WORK DETAILS THIS REPAIR REQUIRES REINSPECT IAW ETD 2014-170-Jun 23, 2014 · N827MD · Emb ERJ170100SUSDR HYIA20140621001Spar Cap · corrodedDURING SCHEDULED INSPECTION, AREAS OF EXFOLIATING CORROSION WERE FOUND AT RT WING LWR SPAR CAP STRAP OEM PN 5292029-2 PREVIOUSLY INSTALLED TO SATISFY REQUIREMENT OF AD2005-12-13 CONCURRENT WITH MEB02-5. THE CORRECTIVE ACTION WILL BE TO PERFORM A DETAILED INSPJun 20, 2014 · N4652N · Cessna 402CSDR ABXA20140616220Spar · corrodedLOWER LE PANEL SPAR CRACKED & CORRODED AT NR 1 SLAT INBD AUX TRACK AREA. REMOVED DAMAGED & CORRODED SECTION OF LOWER LE SPLICE PLATE & INSTALLED NEW SECTION OF SPLICE PLATE IAW REA B657-61054. ACFT WAS GROUNDED.Jun 16, 2014 · N792AX · Boeing 767200SDR UHLA2014061400517Spar · crackedCRACKED SPAR 3 AT LOWER FLANGE OF RIB 10 LOCATION. R & R SPAR 3 REF ETD2014-170-053799. MAJOR REPAIRJun 14, 2014 · N654RW · Emb ERJ170100SESDR UHLA2014061200516Spar · gougedSPAR 3 EXTERNAL SURFACE HAS SMALL GOUGE BETWEEN RIB 4A AND 6. R & R SPAR 3 REF ETD2014-170-053799. MAJOR REPAIRJun 12, 2014 · N654RW · Emb ERJ170100SESDR HYIA20140614002Spar Cap · corrodedSERVICE KIT SK402-47, CONCURRENT WITH AD2005-12-13 & MEB02-5, WAS INSTALLED ON 07/24/2003 AT AFTT 20,019.7 AS TERMINATING ACTION FOR AD2005-05-52. EDDY CURRENT PRESCRIBED IN SID 57-10-16 REVEALED MULTIPLE AREAS OF SUBSURFACE CORROSION IN LWR FWD SPAR CAP STRAJun 12, 2014 · N121PB · Cessna 402CSDR HYIA20140614001Spar Cap · corrodedSERVICE KIT SK402-47, CONCURRENT WITH AD2005-12-13 & MEB02-5, WAS INSTALLED ON 07/24/2003 AT AFT 20,019.7 AS TERMINATING ACTION FOR AD2005-05-52. EDDY CURRENT PRESCRIBED IN SID 57-10-16 REVEALED MULTIPLE AREAS OF SUBSURFACE CORROSION IN LWR FWD SPAR CAP STRAPJun 12, 2014 · N121PB · Cessna 402CSDR ECPR2014061261983Spar · corrodedCORROSION FOUND ON THE UPPER SURFACE OF THE BOTTOM CAP OF THE RT WING SPAR ASSY, AT APPROXIMATLEY WING STATION 60, JUST INBD OF THE RT LANDING GEAR FORWARD TRUNION FITTING ASSY. CORROSION APPEARED TO HAVE STARTED INSIDE THE SPAR MATERIAL AND HAD NO EXTERNAL Jun 12, 2014 · N4905E · Piper PA44180SDR ECPR2014061261660Spar · corrodedTWO AREAS OF CORROSION WAS FOUND ON THE UPPER SURFACE OF ANGLE ATTACHED TO THE LOWER PORTION OF THE LT WING SPAR ASSY, AT WING STATIONS 41.00 & 47.50. AREAS OF CORROSION APPEARED TO HAVE STARTED INSIDE THE MATERIAL OF THE ANGLE WITH NO EXTERNAL INFLUENCE.Jun 12, 2014 · N7710A · Piper PA44180SDR ECPR2014061260422Spar · corrodedLT WING STA 56.0, 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 CATEPILLAR GROMMET INSTALLED TO PREVENT THE Jun 12, 2014 · N5413P · Piper PA44180SDR CA141014002Spar Cap · chafed(CAN) MINOR CHAFING ON LOWER AFT WING SPAR CAP SURFACE FROM LOOSE FENDER BRACKET (BOTH LH AND RH SIDES). RECTIFICATION: REPAIR CARRIED OUT IAW FR-CO-102496 REV 2. CHAFING REMOVED. NDT CARRIED OUT TO ENSURE NO FURTHER DAMAGE EVIDENT. SHIM FILLER PLATES INSTAJun 10, 2014 · Beech 1900DSDR UHLA2014060700515Spar · chafedCHAFE SPAR III AT HYD LINE FEED THRU BETWEEN RIB 4A AND 6A. R & R SPAR 3 REF ETD2014-170-053799. MAJOR REPAIRJun 7, 2014 · N654RW · Emb ERJ170100SESDR ABXA20140605196Spar · corrodedRIGHT WING FRONT SPAR LOWER CHORD AT APPROX WS 416 IS CORRODED. REPAIRED RT WING FRONT SPAR LOWER CHORD FROM OFSS 370 - 460 IAW REA B657-60910-MR. SDR INFO CORRODED L2, PN 112T2005-2, PART NAME FRONT SPAR LOWER CHORD, LOCATION STRINGER & WS FROM OFSS 370 RTJun 5, 2014 · N773AX · Boeing 767281SDR CA141014001Spar Cap · cracked(CAN) VERTICAL FWD PORT & STARBOARD CAPS FOUND CRACKED AT UPPER ATTACH POINT FASTENERS. IAW RDO FR-CO-102431. UPPER DAMAGED PORTIONS OF SPAR CAPS CUT AWAY. INSERTION PIECES OF SPAR CAPS AND DOUBLER REPAIR ANGLES CUT FROM NEW SPAR CAPS WITH SPLICE CARRIED OUT Jun 2, 2014 · Beech 1900DSDR CALA2014060200713Spar · corrodedRIGHT WING OTBD LE FRONT SPAR FOUND CORRODED AT OFSS 736 - 748 POSITION. REPAIR CARRIED OUT IAW ECRA 5710-02383.Jun 1, 2014 · N35236 · Boeing 737824SDR ECPR2014052861586Spar · corrodedTWO AREAS OF EXFOLIATION CORROSION WERE FOUND ON THE UPPER SURFACE OF ANGLE, WHICH IS ATTACHED TO THE LOWER PORTION OF THE PN 86152-00 LT WING SPAR ASSY, AT APPROXIMATELY WING STATIONS 41.00 & 47.50. DUE TO THE AMOUNT OF MATERAIL REQUIRED TO BE REMOVED THESE May 28, 2014 · N7707G · Piper PA44180SDR COEA2014061306917Spar · corrodedRIGHT WING REAR SPAR LOWER CHORD HAS LEVEL 2 CORROSION RIB 25. REPAIR IAW SRAS S572R0166 2852 DATED 6/12/2014.May 25, 2014 · N917FX · Aerosp ATR42300SDR COEA2014061305917Spar · corrodedLEFT WING REAR SPAR LOWER CHORD HAS LEVEL 2 CORROSION RIB 25 - 26. REPAIR IAW SRAS S572R0167 2851 DATED 6/12/2014.May 25, 2014 · N917FX · Aerosp ATR42300SDR ASOA2014060610646Spar · crackedRT WING SPAR CRACKED AT WS 148.019. COMPLIED WITH ECTC REO 601R-57-21-130-01.May 19, 2014 · N860AS · Cndair CL6002B19SDR UHLA2014051800422Spar · unknownSPAR 2 LOWER FLANGE REINFORCEMENTS. COMPLIED WITH SHUTTLE EO 170EO-57-10-0003. MAJOR REPAIR.May 18, 2014 · N632RW · Emb ERJ170100SESDR SWAA2014053028519Spar · crackedLEFT WING FWD SPAR WEB CRACKED AT BS 540, WBL 70.85. R & R WEB IAW SRM & DWG.May 13, 2014 · N386SW · Boeing 7373H4SDR P48S2014FA0000339Spar · crackedACFT CAME BACK FROM TRAINING FLIGHT WITH LEFT GEAR LIGHT NOT ILLUMINATED, AFTER A QUICK VISUAL INSPECTION FOUND THAT AFT WING SPAR WHERE LT LANDING GEAR MOUNTS HAD BEEN CRACKED, TEARING THE BOTTOM AFT SKIN AND SHEARING TOP SKIN MOUNTING RIVETS.May 13, 2014 · N4998J · Piper PA28R180SDR AALA20140512014Spar · corrodedCORROSION AT LT FWD SPAR BOOST PUMP. REMOVED CORROSION & ACCOMPLISHED REPAIR IAW EA B737-57-034860.May 12, 2014 · N925AN · Boeing 737823SDR FDEA201405110981Rib · corrodedRIGHT RIB 5 FWD LUG HAS CORROSION IN BORE, FWD & AFT FACES. COMPLIED WITH EA 6-5710-T0307941 P-2, WING BASIC WING STRUCTURE, LT & RT RIB 5 FWD LUG CORROSION. MAJOR REPAIR.May 11, 2014 · N804FD · Airbus A310324SDR YENA20140510093Spar · corrodedDURING HEAVY MAINTENANCE CHECK, FOUND LT WING AFT SPAR HAS CORROSION AT RIB 17 UNDER OVERHANG PANEL. REMOVED CORROSION AND FOUND LOWEST READING TO BE .137”, MATERIAL REMOVED WAS .060”. MATERIAL ORIGINAL THICKNESS WAS .197”. ACCOMPLISHED REPAIR ON LH WING TOP May 10, 2014 · N633JB · Airbus A320232SDR SWAA2014053028535Rib · crackedRIGHT WING LOWER RIB CHORD CRACKED AT WBL 135.5, BETWEEN STRINGER 2 TO STRINGER 3. REPAIRED CHORD IAW EA.May 9, 2014 · N640SW · Boeing 7373H4SDR DALA14028979223Spar · corrodedLEFT WING REAR SPAR LOWER ANGLE CORRODED AT XRS 164, REPAIRED IAW ERA 525623-14, REV O.May 5, 2014 · N923DN · Doug MD9030SDR FDEA201405050948Spar · crackedFUSELAGE CTR WING BOX REAR SPAR & BOTTOM PANEL LT SIDE HOLE T FOUND CRACK SIGNAL. REPAIRED IAW EA 6-5710-T0307901 P1. MAJOR REPAIR IAW GMM6-2-100.May 5, 2014 · N653FE · Airbus A300F4605RSDR ABXA20140504150Spar Cap · corrodedLEFT WING LOWER SPAR CAP SPLIT & CORRODED AT WD 453. REPAIRED LT WING LOWER SPAR CAP IAW 2 EA B657-60985 ON STATION OFSS 450 PN 114T 0222-5. CORRODED, PN 114T0222-5, SN NS, PART NAME LOWER SPLICE PLATE, FS & BS LOCATION FROM LT WING LE WE LOCATION FROM OFSS May 4, 2014 · N785AX · Boeing 767281SDR FDEA201405040943Spar · crackedFUSELAGE CTR WING BOX REAR SPAR & BOTTOM PANEL RT SIDE HOLE C FOUND CRACK SIGNAL. REPAIRED IAW EA 6-5710-T0307901 P1. MAJOR REPAIR IAW GMM6-2-100.May 4, 2014 · N653FE · Airbus A300F4605RSDR FDEA201405040942Spar · crackedFUSELAGE CTR WING BOX REAR SPAR & BOTTOM PANEL RT SIDE HOLE E FOUND CRACK SIGNAL. REPAIRED IAW EA 6-5710-T0307901 P1. MAJOR REPAIR IAW GMM6-2-100.May 4, 2014 · N653FE · Airbus A300F4605RSDR FDEA201405040941Spar · crackedFUSELAGE CTR WING BOX REAR SPAR & BOTTOM PANEL RT SIDE HOLE F FOUND CRACK SIGNAL. REPAIRED IAW EA 6-5710-T0307901 P1. MAJOR REPAIR IAW GMM6-2-100.May 4, 2014 · N653FE · Airbus A300F4605RSDR FDEA201405040940Spar · crackedFUSELAGE CTR WING BOX REAR SPAR & BOTTOM PANEL LT SIDE HOLE G FOUND CRACK SIGNAL. REPAIRED IAW EA 6-5710-T0307901 P1. MAJOR REPAIR IAW GMM6-2-100.May 4, 2014 · N653FE · Airbus A300F4605RSDR FDEA201405040939Spar · crackedFUSELAGE CTR WING BOX REAR SPAR & BOTTOM PANEL LT SIDE HOLE F FOUND CRACK SIGNAL. REPAIRED IAW EA 6-5710-T0307901 P1. MAJOR REPAIR IAW GMM6-2-100.May 4, 2014 · N653FE · Airbus A300F4605RSDR FDEA201405040938Spar · crackedFUSELAGE CTR WING BOX REAR SPAR & BOTTOM PANEL LT SIDE HOLE E FOUND CRACK SIGNAL. REPAIRED IAW EA 6-5710-T0307901 P1. MAJOR REPAIR IAW GMM6-2-100.May 4, 2014 · N653FE · Airbus A300F4605RSDR FDEA201405040937Spar · crackedFUSELAGE CTR WING BOX REAR SPAR & BOTTOM PANEL LT SIDE HOLE S FOUND CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0307901 P1 EA TITLE, WINGS BASIC WING STRUCTURE AD2005-23-08--CRACK HOLES AT FRAME 47-SB57-6086 EMBODIMENT. REPAIRED THE FUSELAGE CTR WING BOX REAR SPAMay 4, 2014 · N653FE · Airbus A300F4605RSDR DALA14030189223Spar · corrodedCORROSION FOUND ON THE LOWER SURFACE OF THE LEFT WING REAR SPAR, LOWER ANGLE. AREA WAS BLENDED IAW ERA 92-525623.May 2, 2014 · N923DN · Doug MD9030SDR HYIA05032014005Spar · crackedDURING SCHEDULED INSPECTION, MULTIPLE SPAR WEB CRACKS WERE NOTED INITIATING FROM SPAR WEB MOUSE HOLE CUT OUTS AT AFT CARRY THROUGH SPAR ASSEMBLY, PN 5211173-2, AT CTR LOWER SECTION OF FWD & AFT WEBS. THIS DAMAGE WILL BE REPAIRED IAW REPAIR DEFINITION SUPPLIEDMay 1, 2014 · N258PB · Cessna 402CSDR HYIA05032014004Spar · crackedDURING SCHEDULED INSPECTION, MULTIPLE SPAR WEB CRACKS WERE NOTED INITIATING FROM SPAR WEB, MOUSE HOLE CUT OUTS AT FWD CARRY THROUGH SPAR ASSEMBLY, PN 5211171-2, AT CTR LOWER SECTION OF FWD & AFT WEBS. THIS DAMAGE WILL BE REPAIRED IAW REPAIR DEFINITION SUPPLIEMay 1, 2014 · N258PB · Cessna 402CSDR HYIA05032014003Spar · crackedDURING ROUTINE SCHEDULED INSPECTION, MULTIPLE WEB FLANGE CRACKS WERE NOTED AT AFT FUSELAGE CARRY THROUGH SPAR ASSEMBLY, PN 5211173-2 AT CTR UPPER SECTION FWD & AFT WEBS. THIS DAMAGE WILL BE REPAIRED, REPAIR DEFINITION SUPPLIED & SUBSTANTIATED BY DER. A SUPPLMay 1, 2014 · N258PB · Cessna 402CSDR HYIA05032014001Strap · corrodedDURING ROUTINE SCHEDULED INSPECTION, AREAS OF CORROSION WERE FOUND AT LT & RT LOWER WING SPAR CAP STRAPS PREVIOUSLY INSTALLED VIA SK402-47B ON 12/05/2005 TO SATISFY REQUIREMENT OF AD2005-12-13 & MEB02-5. THE CORRECTIVE ACTION TO REMEDIATE CONDITION WILL BE TOMay 1, 2014 · N258PB · Cessna 402CSDR UHLA2014041700379Spar · unknownSPAR LOWER FLANGE REINFORCEMENTS. COMPLIED WITH EO 170EO-57-10-0003. MAJOR REPAIRApr 29, 2014 · N823MD · Emb ERJ170100SUSDR HYIA20140439114Spar · crackedDURING A SCHEDULED MX EVENT, TWO CRACKS WERE FOUND AT THE AFT CARRY THROUGH SPAR WEB FLANGES. THE CRACKS WERE APPROXIMATELY .75 INCHES IN LENGTH & WERE LOCATED AT FS 186.15, RBL 7.75 AT THE FWD & AFT SPAR FLANGE. THE DAMAGE WAS REPAIRED IAW ENGINEERING DRAWIApr 28, 2014 · N2611X · Cessna 402CSDR DALA14026500937Spar Cap · damagedRT WING REAR SPAR, XRS 164 LOWER CAP DAMAGED. DOUBLER REPAIR INSTALLED IAW SEC 06 OF WC 5710-01110-06. SEC 05,Apr 28, 2014 · N937DL · Doug MD88SDR SWAA2014062329336Spar · crackedRIGHT WING REAR SPAR UPPER CHORD CRACKED BETWEEN RSS 224.14 TO 215.97. REPAIRED CHORD IAW EO & EA NO.Apr 24, 2014 · N387SW · Boeing 7373H4SDR SWAA2014062329335Spar · crackedLEFT WING REAR SPAR UPPER CHORD CRACKED BETWEEN RSS 224.14 TO 215.97. REPAIRED CHORD IAW EO & EA.Apr 24, 2014 · N387SW · Boeing 7373H4SDR IPXA2014052383017Spar Cap · corrodedDURING A 1C INSPECTION, LT WING T/E UPPER FALSE SPAR CAP CORRODED, XW170- XW233. PERFORMED SPLICE REPAIR IAW EA 011-5720-01-A5300, REV IR AND EO 5720-54374-A.Apr 23, 2014 · N272UP · Doug MD11F
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