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 QXEA0300203Spar · chafedPDX - WING LEADING EDGE LOWER SPAR FLANGE AT WS 56 IS CHAFED. REPAIRED IAW RD 8-57-811.Jan 21, 2003 · N346PH · Dhav DHC8202SDR 2003FA0000041Spar Cap · corrodedFUEL INTERCONNECT ACCESS PANEL CUT OUT DOUBLER IS CRACKED AT LT AND RT PANEL NUMBERS 53L AND 53R. LT AND RT UPPER CENTER WING BOX BEAM COVERS HAVE MODERATE TO MILD CORROSION ON THE UPPER HAT SECTIONS AND THE SKIN BETWEEN WING STATIONS 84.5 TO 192 LT AND RT. Jan 21, 2003 · N139HP · Lkheed P2V7SDR MWEA030038Spar · damagedLEFT WING STATION XRS 157 AFT SPAR REPAIR. -- FABRICATED AND INSTALLED REPAIR PARTS, FABRICATED AND INSTALLED NEW TEE.Jan 20, 2003 · N401ME · Doug DC932SDR AUS20030025Spar · corroded(AUS) LT WING REAR LOWER SPAR CAP ANGLE CORRODED IN AREA BETWEEN WS 318 AND WS 357.Jan 14, 2003 · Doug C54ESDR AUS20030024Spar Cap · corroded(AUS) RT OUTER WING PANEL UPPER SPAR CAP CORRODED BETWEEN WS 585 AND WS 613.Jan 14, 2003 · Doug C54ESDR AUS20030023Spar Cap · corroded(AUS) RT OUTER WING UPPER SPAR CAP CORRODED BETWEEN WS 399 AND WS 421.Jan 14, 2003 · Doug C54ESDR AUS20030022Spar · corroded(AUS) RT OUTER WING UPPER SPAR CAP CORRODED AT WS 378.Jan 14, 2003 · Doug C54ESDR AUS20030270Spar · corroded(AUS) LT WING REAR LOWER SPAR CONTAINED LEVEL 3 CORROSION AT WS 200. FOUND DURING CPCP INSPECTION IAW C57-581-03.Jan 2, 2003 · Boeing 727277SDR QXEA0202261Spar Cap · corrodedPDX - FRETTING CORROSION ON BOTTOM SIDE OF LOWER SPAR CAP, RIGHT HAND WING APPROXIMATELY YW57.0R. REPAIRED IAW RD 8-57-811, PAGE 4 AND DHC-8 SRM 51-40-11.Dec 23, 2002 · N367PH · Dhav DHC8202SDR AUS20021447Spar · cracked(AUS) RT WING REAR SPAR CRACKED AROUND FASTENER HOLE. FOUND DURING INSPECTION IAW ER B73-57-40-17 AND BOEING SB 737-57-1216.Dec 20, 2002 · Boeing 737377SDR 2002FA0001377Spar · crackedWHILE COMPLYING WITH AD 2000-25-02 R1 (WING SPAR INSPECTION) FOUND BOTH FORWARD SPARS CRACKED AT SPAR ROOT. EACH SPAR HAD TWO CRACKS RUNNING THE LENGTH OF THE WOOD GRAIN AND ADJACENT TO UPPER AND LOWER ATTACH BOLT HOLES. PAINT FROM THE AREA HAD TO BE REMOVED PDec 9, 2002 · N11687 · Bbavia 7KCABSDR 2002FA0001368Spar Cap · corrodedINSPECTION MADE DURING INSTALLATION OF SHOULDER HARNESSES REVEALED EXFOLIATION OF AFT CARRY THRU SPAR AND ADJACENT SKINS. CENTER RUDDER ATTACHMENT POINT WAS CORRODED TO SUCH AN EXTENT THAT THE AIRFRAME SUCH THAT REMOVAL OF RUDDER WAS POSSIBLE WITHOUT REMOVINGDec 4, 2002 · N8418Z · Cessna 2105ASDR QXEA0202098Spar Cap · gougedPDX - RIGHT WING SPAR LOWER CAP FORWARD BOTTOM EDGE GOUGED AT YW202.00. REPAIRED IAW HORIZON AIR EA 2-57-212.Dec 3, 2002 · N365PH · Dhav DHC8202SDR AUS20021363Spar Cap · corroded(AUS) LH WING MAIN LOWER SPAR CAP CORRODED. CORROSION IS LOCATED AT WS62 AS INDICATED IN AWB/51-4 ISSUE 1.Nov 20, 2002 · Piper PA30SDR AUS20021362Spar Cap · corroded(AUS) RH WING MAIN LOWER SPAR CAP CORRODED. CORROSION IS LOCATED AT WS62 AS INDICATED IN AWB/51-4 ISSUE 1.Nov 20, 2002 · Piper PA30SDR DL733021346Spar · damagedWHILE REPLACING THE MLG BEAM SUPPORT FITTING A FASTENER HOLE WAS DAMAGED IN THE REAR SPAR CHORD AND REAR SPAR WEB. THE HOLE WAS OVERSIZED AND A REPAIR BUSHING INSTALLED.Nov 20, 2002 · N306WA · Boeing 737347SDR AUS20021335Spar · corroded(AUS) LH WING SPAR CONTAINED LIGHT CORROSION AND MINOR PITTING LOCATEDIN AREA JUST ABOVE LOWER SPAR CAP RADIUS. AREA OF CORROSION APPROXIMATELY 25MM (1IN) LONG BY 6MM (0.236IN) WIDE. FOUND DURING INSPECTION IAW AWB51-4.Nov 13, 2002 · Piper PA30SDR QXEA0201914Spar Cap · chafedPDX - FRONT SPAR LOWER CAP HAS PAINT CHAFE AREA EXPOSING BARE METAL AT YW58.200. REPAIRED IAW RD 8-57-811 AND DHC-8 SRM 51-20-57 AND SRM 51-20-26.Nov 9, 2002 · N369PH · Dhav DHC8202SDR TSAA0253238Spar · corrodedFOUND CORROSION ON RIGHT FRONT SPAR LOWER CHORD VERTICAL WEB SURFACE AT WSL 554. CONFIRMED COMPLETE REMOVAL OF CORROSION WITH HFEC INSPECTION. FABRICATED TAPERED FILLERS TO FIT IN THE BLENDOUT AREA. FABRICATED A REPAIR DOUBLER AND REPAIR ANGLE. INSTALLED THNov 7, 2002 · N827AL · Boeing 737209SDR TSAA0253239Spar · corrodedFOUND CORROSION ON RIGHT FRONT SPAR LOWER CHORD SURFACE AT WSL 557. CONFIRMED COMPLETE REMOVAL OF CORROSION WITH HFEC INSPECTION. FABRICATED A REPAIR FILLER TO FIT IN THE BLENDOUT AREA. FABRICATED A REPAIR STRAP. REPAIR COMPLETED IAW ECO. AIRCRAFT RETURNENov 7, 2002 · N827AL · Boeing 737209SDR AUS20021303Spar Cap · cracked(AUS) LH WING SPAR CAP CRACKED. PREVIOUS CRACK HAD BEEN REPAIRED USINGSTAINLESS STEEL LAMINATIONS. DURING EDDY CURRENT INSPECTION IAW AD/P68/43 AMDT1 IT WAS FOUND THAT THE CRACK HAD GROWN FROM 10MM (0.39IN) TO 21MM (0.826IN) ON THE VERTICAL FACE.Nov 6, 2002 · Parten P68BSDR AK62003F00002Fitting · corrodedDURING AN ANNUAL INSPECTION, DISCOVERED THE RIGHT WING UPPER SPAR FITTING CORRODED INSIDE THE AFT WHEELWELL SPAR ACCESS PANELS. THE WING WAS REMOVED AND THE FITTING WAS REPLACED.Nov 5, 2002 · N2664L · Cessna 414ASDR AK62003F00001Fitting · corrodedDURING AN ANNUAL INSPECTION IT WAS DISCOVERED THAT THE LT WING UPPER REAR SPAR FITTING WAS CORRODED. UPON REMOVAL OF THE WING TO CHANGE THE FITTING, IT WAS DISCOVERED THAT THE LOWER AFT SPAR FITTING ALSO HAD CORROSION. BOTH FITTINGS WERE REPLACED. THE CORRONov 1, 2002 · N6562C · Cessna 414ASDR AK62003F00000Fitting · corrodedDURING AN ANNUAL INSPECTION IT WAS DISCOVERED THAT THE LT WING UPPER REAR SPAR FITTING WAS CORRODED. UPON REMOVAL OF THE WING TO CHANGE THE FITTING, IT WAS DISCOVERED THAT THE LOWER AFT SPAR FITTING ALSO HAD CORROSION. BOTH FITTINGS WERE REPLACED. THE CORRONov 1, 2002 · N6562C · Cessna 414ASDR AUS20021254Spar · damaged(AUS) RT WING SPAR REPAIRED DUE TO CORROSION. A LARGE DOUBLER IS ATTACHED TO THE AFT SIDE OF THE SPAR WEB. NO RECORD OF REPAIR OR REFERENCE TO AN ENGINEERING ORDER OR APPROVED DATA IS RECORDED IN THE LOGBOOK. THE OWNER STATES THE REPAIRS WERE CARRIED OUT IN AUOct 31, 2002 · Beech A23ASDR AUS20021269Spar · corroded(AUS) LH WING REAR SPAR CONTAINS SEVERE EXFOLIATION CORROSION BETWEEN THE SPAR AND ATTACHMENT PLATE.Oct 30, 2002 · Piper PA32260SDR UPS02239908Frame · corrodedINSPECTION TYPE: C &SI, APU EXHAUST, SUSPECT CORROSION ON AFT WING FRAME UNDER TADPOLE SEAL OF UPPER EXHAUST. FRAME CORRODED BEYOND LIMITS. NEW FRAME FABRICATED AND INSTALLED IAW DRAWING 65-31997.Oct 24, 2002 · N932UP · Boeing 72725CSDR AUS20021249Doubler · cracked(AUS) LT WING AFT SPAR OUTBOARD AILERON HINGE DOUBLER CRACKED FOR APPROXIMATELY 50 PERCENT OF ITS LENGTH.Oct 16, 2002 · Piper PA28235SDR TSAA0253214Spar · crackedREMOVED A CRACK AND CORROSION LOCKED AT RIGHT WING FRONT SPAR WEB AT FSS 124.79 AND FSS 134.80. HFEC INSPECTED TO ENSURE THE DAMAGE COMPLETELY REMOVED. FABRICATED REPAIR PARTS AND INSTALLED REPAIR PARTS IAW ECO. AIRCRAFT RETURNED TO SERVICE.Oct 16, 2002 · N802AL · Boeing 7372S5CSDR QXEA0201722Spar · chafedPDX - LT WING LEADING EDGE FORWARD SPAR LOWER FLANGE CHAFED AT STATION 58.00. REPAIRED IAW RD 8-57-811.Oct 15, 2002 · N364PH · Dhav DHC8202SDR QXEA0201721Spar · chafedPDX - LT WING LEADING EDGE FORWARD SPAR LOWER FLANGE CHAFED AT STATION YW138.0. REPAIRED IAW RD 8-57-20-54Oct 15, 2002 · N364PH · Dhav DHC8202SDR QXEA0201737Spar Cap · chafedPDX - RT WING FRONT SPAR LOWER CAP IS CHAFED APPROXIMATELY YW57.0. REPAIRED IAW RD 8-57-811.Oct 15, 2002 · N364PH · Dhav DHC8202SDR QXEA0201736Spar · chafedPDX - LT WING FORWARD SPAR FLANGE CHAFED AT UPPER SURFACE YW58.00. REPAIRED IAW RD 8-57-2054.Oct 15, 2002 · N364PH · Dhav DHC8202SDR DHL2002720528Spar · corrodedDURING C CHECK, LT WING FWD. SPAR UPPER CHORD IS CORRODED AT WS 130 UPPER SURFACE AT BULGED SEALANT. REPAIRED IAW SRM.Oct 14, 2002 · N720DH · Boeing 727228SDR DL733021199Spar · crackedINSPECTION OF THE MLG BEAM ATTACH FITTINGS AND REAR SPAR ON THE LT WING REVEALED 6 HOLES COMMON TO THE FITTINGS AND SPAR WITH CRACK INDICATIONS. ADDITIONAL HOLES WERE DAMAGED OR ELONGATED DURING REWORK OF AREA. THE HOLES WERE OVERSIZED TO REMOVE ALL CRACKS AOct 14, 2002 · N951WP · Boeing 7373B7SDR 2002FA0001219Spar · corrodedOBSERVED THE CARRY THRU SPAR CORROSION WHEN LOOKING AT THE AIRCRAFT. THIS ITEM HAD SURFACE CORROSION THAT HAS BLISTERING THAT COULD BE PICKED AT AND MOST OF THE SURFACE AREA HAD WHITE DUSTING AND DISCOLORATION INDICATING CORROSION THAT REQUIRES TREATMENT. CAOct 11, 2002 · N2692V · Cessna 177RGSDR AUS20021145Spar · corroded(AUS) LT AND RT AFT SPAR ASSEMBLIES CORRODED BETWEEN SPAR AND ATTACHMENT PLATE PNO 66762-00.Oct 9, 2002 · Piper PA28140SDR CA021016033Spar · cracked(CAN) UPON COMPLETION OF S/B 215-A463R3 (FRONT SPAR) A REJECTABLE INDICATION AT 4-7 IN THE DEFECT WINDOW 85 PERCENT SCREEN HEIGHT WAS DISCOVERED IN THE LT FWD LOWER SPAR CAP. EDDY CURRENT & LPI CONFIRMED THE INDICATION. 1165 LOADS SINCE LAST INSPECTIONOct 9, 2002 · Cndair CL2151A10SDR SWIA200211362Spar Cap · crackedLEFT WING FORWARD LOWER SPAR CAP HAS A CRACK BETWEEN 4533.5 AND 4945. RIVET ROW ON LOWER SKINS MARKED WHERE SKIN SEAMS MEET, OUTBD OF RIB NR17. DISCOVERED DURING LINE INSPECTION OF FUEL LEAK. REPAIRED IAW EMB 120 SRM 57-20-05 AND RII CARD RII 57-301 AND RIIOct 7, 2002 · N199SW · Emb EMB120ERSDR QXEA0201596Spar · chafedPDX- CHAFE DAMAGE ON WING FRONT SPAR STIFFNER RIB NEXT TO LT EJECTOR IN CENTER FUEL TANK. REPAIRED IAW HORIZON AIR EA R-57-16.Oct 5, 2002 · N601QX · Cndair CL6002C10SDR QXEA0201595Spar · chafedPDX- CHAFFE DAMAGE ON WING FRONT SPAR STIFFNER RIB NEXT TO RT EJECTOR IN CENTER FUEL TANK. REPAIRED IAW HORIZON AIR EA R-57-16Oct 5, 2002 · N601QX · Cndair CL6002C10SDR UPS02239769Spar · corrodedDURING PREPARATION FOR CENTER SECTION REAR SPAR WEB SPLICE REPAIR, ADDITIONAL CORROSION WAS NOTED ON UPPER CHORD INBOARD OF LBL 34.20. WEB, CHORD, SPLICE AND STIFFENERS FABRICATED IAW DRG NR 65C21531 REPAIR COMPLETED IAW SMRO EO 2002-052-013. UPS ENG FILE NROct 3, 2002 · N930UP · Boeing 72722CSDR ABXA020287Spar · corrodedLT WING INBOARD TRAILING EDGE MAIN FLAP FRONT SPAR LOWER CHORD VERTICAL FLANGE BETWEEN FS 286 - 290, FOUND CORROSION. REPAIRED AREA IAW REA B657-44906MR.Sep 30, 2002 · N794AX · Boeing 767200SDR QXEA0201634Spar · chafedPDX - RT INBOARD LOWER WING SPAR IS CHAFED APPROXIMATELY YW56.000. REPAIRED IAW DHC-8 SRM 51-40-11 AND RD 8-51-811.Sep 30, 2002 · N368PH · Dhav DHC8202SDR 2002FA0001174Spar · corrodedINTERGRANULAR CORROSION, FOUND IN THE FOLLOWING WING COMPONENTS DURING A REPAIR/REBUILD PROCESS. LT AND RT MAIN SPAR BEAMS, REAR, LEFT MAIN SPAR BEAM, FRONT.Sep 29, 2002 · N1291B · Luscom 8ASDR ABXA020286Spar · corrodedRT WING INBOARD TRAILING EDGE MAIN FLAP MID SPAR UPPER FORWARD CHORD HAD CORROSION, WS 177 - 186 AND BETWEEN WS 252 - 261. REPAIRED AREA IAW REA B756-44900MR.Sep 27, 2002 · N794AX · Boeing 767200SDR MWEA020602Spar · gougedLEFT WING, LOWER ANGLE FITTINGS ON FALSE SPAR HAS A DEEP GOUGE IN IT. DOT NS01. -- BLENDED GUAGE, REMOVED AND INSTALLED FITTINGS FABRICATED REPAIR AND INSTALLED BUSHINGS. FIT AND DRILLED AND INSTALLED AUX SPAR FITTING.Sep 27, 2002 · N302ME · Doug DC932SDR QXEA0201556Spar · chafedPDX - LEFT HAND INBOARD WING FRONT SPAR BOTTOM FLANGE CHAFED AT INBOARD END FROM CONTACT WITH LEADING EDGE AT YW50.0. REPAIRED IAW RD 8-57-2054.Sep 26, 2002 · N368PH · Dhav DHC8202SDR UIEA200200046Spar · corrodedDURING CURRENT C CHECK, FOUND CENTER WING LOWER REAR SPAR WEB CORRODED AT LBBL66 TO 75. BLENDED CORROSION. PERFORMED HFEC OPEN HOLE INSPECTION AND SURFACE INSPECTION OF BLENDED AREAS. NO DEFECTS FOUND. MEASURED CORROSION DEPTH, MEASUREMENTS EXCEEDED SRM LISep 20, 2002 · N505MC · Boeing 7472D3BSDR ASA2002F00002Spar · crackedDURING C CHECK FOUND RT LEADING EDGE INBOARD OF NR 2 ENGINE HAS 2 INCH CRACK ON PRIMARY STRUCTURE. REPAIRED CRACK PER EA.Sep 17, 2002 · N780AS · Boeing 7374Q8
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