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 ZIAA96017Spar Cap · crackedYIP - DURING INSPECTION, FOUND RIGHT WING FRONT SPAR LOWER 'T' RAIL CRACKED AT STATION 70. INSTALLED REPAIR AS PER ZIAA DER APPROVED DRAWING NR A91-R01. (M)May 30, 1996 · N289F · Lkheed 188CSDR 96ZZZX2954Spar · corrodedDURING ANNUAL INSPECTION, MECHANIC BEGAN TO REPAIR FLOORBOARD UNDER FUSELAGE AUXILIARY FUEL TANK. UPON REMOVAL OF AUXILIARY FUEL TANK AND FLOORBOARD, DISCOVERED THE REAR CARRY-THROUGH SPAR WAS CORRODED BEYOND REPAIR. MECHANIC NOTES THAT ACCESS TO THIS AREA FMay 21, 1996 · N8426A · Beech A35SDR DLL10961231Spar Web · crackedTHE CENTER WING INTERMEDIATE SPARS AT FS 1043M RBL 116 AND FS 1103M LBL 116 HAD CRACKS IN WEB. ALSO, FS 1103 HAD MULTIPLE CRACKS THROUGH UPPER FASTENER HOLES. REV A ADDED ADDITIONAL CRACK LOCATIONS, REVISED DIRECTIONS AND DRAWINGS TO ACCOMODATE THIS, REV B AMay 16, 1996 · N722DA · Lkheed 10113851SDR 96ZZZX2959Spar · corrodedUPON REMOVING A SKIN PANEL FROM RT WING AFT OF LANDING GEARWELL TO FACILITATE REPAIR OF SMALL CRACKS IN WING SKIN, DISCOVERED CORROSION ON LOWER AFT SPAR CAP FROM WING ROOT TO WS 74.5. REMOVED CORROSION FROM AFFECTED AREAS OF SPAR CAP AFTER CONTACTING CESSNA May 16, 1996 · N45ME · Cessna 550SDR UPS96820221Spar Cap · crackedINSPECTION TYPE-C, CRACKS IN NR 5, NR 10 AND NR 11 HOLES IN SPAR CAP ON LEFT WING. REPAIRED CRACKS NR 5, NR 10, NR 11 HOLES IN SPAR CAP BY FABRICATING REPAIR DOUBLERS IAW SRM 51-3-2 AND EO DC8-5710-7761A.May 11, 1996 · N801UP · Doug DC873FSDR AU960653Spar Cap · corroded(AUS) LH AND RH WING SPAR CAPS PNO 5122031-1 (LH) AND PNO 512203-2 (RH)CORRODED IN AREA OF NACELLE FUEL TANKS - WING SKINS AND CHANNELS ALSO CORRODEDMay 10, 1996 · Cessna 310RSDR UPS96820217Support Ftg · damagedINSPECTION TYPE-C, WING FRONT SPAR AT PYLON SUPPORT FITTING NR 2 AND NR 3 REQUIRES REPLACEMENT. MODIFIED NR 2 AND NR 3 FOOT STOOL SKATE ANGLE IAW EO DC-8-5710-4080E AND TIMCO REO-01940.May 8, 1996 · N801UP · Doug DC873FSDR DL72P961090Aux Spar · chafedFOUND DURING C-CHECK, LT MLG STRUT DOOR CHAFING AUX SPAR I/B END MARKED, FWD OF NR 4 SCREWJACK. REPAIRED PER M/M 57-43-0 PG 802.May 6, 1996 · N8889Z · Boeing 727225SDR CA960527007Spar · cracked(CAN)THE REAR SPAR EXHIBITS SIGNS OF WOOD COMPRESSION FAILURE AT THE 46 INCH LOCATION OUTBOARD FROM THE ROOT.May 1, 1996 · Bbavia 8KCABSDR 96FDEA01045Spar · crackedLT WING FRONT SPAR UPPER CHORD CRACKED ABOVE AND O/B OF NR 2 LE FLAP ACTUATOR. REMOVED CRACK, VOID IN CORROSION AND CORROSION ABOVE AND O/B OF NR 2 LE FLAP ACTUATOR. INSTALLED REPAIR DOUBLER PER FEDEX EA 7-5710-28691 DATE 5-22-96.Apr 29, 1996 · N120FE · Boeing 72725CSDR SCNA96127Spar · crackedDURING HEAVY MAINTENANCE VISIT, CRACKS WERE FOUND IN SKIN AROUND RIVETS JUST BELOW THE LOWER CHORD OF THE REAR SPAR UNDER NR 2 AND NR 3 SPOILERS. FABRICATED AND INSTALLED A WAFFLE DOUBLER IN ACCORDANCE WIITH B727 SRM 51-40-3, FIGURE 1.Apr 26, 1996 · N283SC · Boeing 727225SDR ARWR961166Spar Doubler · corrodedDURING C-CHECK, FOUND LEFT WHEELWELL WING REAR SPAR DOUBLER AT STA XCW 60 HAS LOCAL CORROSION AT UPPER AREA. REMOVED CORROSION, FOUND AREA BEYOND LIMITS IAW SRM 53-2-0. FABRICATED MACHINED DOUBLER AND CLIP. TREATED AND PRIMED IAW SRM 52-1-8. INSTALLED REPAApr 26, 1996 · N8969U · Doug DC862SDR 96ZZZX2578Spar · corrodedINSPECTION FOUND WING SPARS WITH HEAVY CORROSION AND EXFOLIATION. SUSPECT CAUSE, SALT INTRUSION.Apr 26, 1996 · N59BW · Beech B19SDR AU960950Spar Web · cracked(AUS) LH OUTER WING REAR SPAR WEB CRACKED AT APPROXIMATELY STN 5115 RUNNING FROM LOWEST RIVET - CRACK LENGTH 5MM (0.196IN) - FOUND DURING EDDY CURRENT INSPECTION IAW ER F28-57-10-22C PART 2Apr 24, 1996 · Fokker F28MK4000SDR UPS96820055Spar · crackedINSPECTION TYPE 'C', REAR SPAR UPPER CHORD ANGLE 9 CRACK APPROX XCW60 FS 850 LT W/W. REPAIRED SPAR CHORD PER SRM 53-2-5 FIG 2 AND DOUBLER DRAWING 3646971.Apr 23, 1996 · N880UP · Doug DC873FSDR UPS96420063Spar Web · corrodedINSPECTION TYPE 'C', LT WING REAR SPAR WEB OF LT WING REAR SPAR HAS CORROSION AT WS 550. REPAIRED CORROSION IAW UPS EFN 747-57-0323.Apr 19, 1996 · N676UP · Boeing 747123SDR UPS96820107Spar · crackedINSPECTION TYPE: C. RIGHT WING REAR SPAR UPPER CHORD ANGLE CRACKS AT STA XRS624. REPAIRED PER UPS EO DC8-57-0671.Apr 18, 1996 · N880UP · Doug DC873FSDR 96ZZZX3749Spar · crackedTHIS IS THE THIRD TIME THIS SPAR HAS BEEN CRACKED. THIS AIRCRAFT IS ON EDO 88-1650 FLOATS. IT IS NECESSARY TO REMOVE THE FORWARD END OF THE HEADLINER TO INSPECT THIS AREA. AIRCRAFT TT, 3,042.39 HOURS.Apr 18, 1996 · N2408N · Cessna 140SDR 96ZZZM1045Spar · crackedDURING PYLON MODIFICATION ON THIS A/C, AN INSPECTION OF THE LEFT WING FRONT SPAR REVEALED CRACKS AT FOUR LOCATIONS AT WING STATION 669.5. REF ATTACHED QUERY NOTE S/N 16/95 FOR DETAILS.Apr 16, 1996 · N691UP · Boeing 747121SDR CA960527006Spar · cracked(CAN)ON INSPECTION THE REAR SPAR WAS FOUND FAILED (CRACKED) AT THE RIGHT HAND REAR SPAR ROOT END BISCUIT. IT WAS NOTED TO HAVE FAILED ACROSS THE TOP AT THE SECTION OF THE SPAR THAT IS MILLED OUT TO ACCOMMODATE THE BISCUIT DOUBLERS. SUBMITTER STATES THAT THE AIApr 15, 1996 · Bbavia 7BCMSDR AU960480Spar · cracked(AUS) FUSELAGE FRONT SPAR CARRY THROUGH SECTION CRACKED AT BOTH OUTBOARD SIDESApr 15, 1996 · Beech V35ASDR UPS96805978Spar · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT WING LWR SPAR HOLE NR 6 FOUND CRACKED WHILE PERFORMING EO DC8-5710-7761-A. FAB REPAIR DOUBLER, FILLER AND BUSHINGS AND INSTALLED IAW DAC DWG J060232 AND EO DC8-5710-7761A.Apr 12, 1996 · N803UP · Doug DC873FSDR AWXA960199Spar Chord · crackedPAE - FLT 3802 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND CRACK ON FORWARD UPPER SPAR CHORD AT BS 663, LBL 24, WL 201. REMOVED DAMAGED SECTION AND REPAIRED IAW, AWA ER 2-53-13-34. (M)Apr 11, 1996 · Boeing 737275SDR CA960418006Spar Cap · cracked(CAN) SPAR CAP FOUND CRACKED IN THE RIGHT HAND WHEEL WELL. SECONDARY DAMAGE FOUND TO BE CRACKED SPLICE PLATES.Apr 9, 1996 · Beech 99ASDR DLL17960936Rear Spar · crackedON THE RT WING, REAR SPAR, CRACKS WERE FOUND EMANATING FROM FASTENER HOLES BETWEEN IWS 293.58 AND IWS 346.109. CRACKS WERE FOUND IN THE UPPER CAP, WEB, AND UPPER WING SKIN. ACCOMPLISHED REPAIRS PER DL ERA 273600-14AD.Apr 8, 1996 · N767DA · Lkheed 10113853SDR DLL17960935Rear Spar · crackedON THE LT WING, CRACKS WERE FOUND EMANATING FROM FASTENER HOLES BETWEEN IWS 293.58 AND IWS 346.109. CRACKS WERE FOUND IN THE UPPER CAP, WEB AND UPPER WING SKIN. ACCOMPLISHED REPAIRS PER DL ERA 273597-14AD.Apr 8, 1996 · N767DA · Lkheed 10113853SDR CA960419006Spar Cap · cracked(CAN)CRACK FOUND RUNNING FROM RIVET TO RIVET WHERE THE FORWARD SPAR WEB ATTACHES TO THE CAP. THIS WAS NOTICED THROUGH A LIGHTENING HOLE. SPAR CAP IS ON FORWARD SPAR WHICH SECURES TO THE FORWARD WING ATTACH NOT THE MAIN WING SPAR THAT THE STRUT ATTACHES TO.Apr 2, 1996 · Dhav DHC6300SDR AU960589Spar · corroded(AUS) LH WING CONTAINED SEVERE EXFOLIATION CORROSION IN THE UPPER FORWARD SPAR EXTRUSIONS, EXFOLIATION CORROSION AND CRACKING IN THE MAIN SPAR AND CORROSION IN THE INNER SPAR WEB - CORROSION APPEARS TO HAVE BEEN PREVIOUSLY TREATED WITH LPS TYPE COMPOUNDApr 1, 1996 · Cessna 182NSDR 97ZZZX547Carry Thru Spar · crackedINSP FOUND CRACKS IN CARRY THRU STRUCTURE. AD 95-0-03 NOT VALID BY SERIAL NUMBER.Mar 29, 1996 · N5599P · Beech F33ASDR UPS96205818Spar · corrodedWHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON FRONT SPAR CUTOUT 7340 HAS CORROSION ON THE INSIDE. REPAIRED FRONT SPAR CUTOUT ON INSIDE OF TANK AT PNL 7340, IAW UPS EO 727-57-1687.Mar 28, 1996 · N907UP · Boeing 72727CSDR 96ZZZX2467Fitting · crackedDISMANTLED LEFT WING FOR THE PURPOSE OF RECOVERING. AS A PRECAUTION, THE WING SPAR ATTACHMENT FITTINGS WERE MAGNAFLUXED. THE LEFT REAR SPAR ATTACHMENT FITTING WAS FOUND TO HAVE SEVERAL IMPERFECTIONS IN THE WELD AREAS OF BOTH THE TOP AND BOTTOM GUSSETS. THE Mar 28, 1996 · N83032 · Bbavia 7ACSDR 96ZZZX2387Fitting · crackedDISMANTLED LEFT WING FOR THE PURPOSE OF RECOVERING. AS A PRECAUTION, THE WING SPAR ATTACHMENT FITTINGS WERE MAGNAFLUXED. THE LEFT FRONT WING SPAR ATTACHMENT FITTING WAS FOUND TO HAVE SEVERAL IMPERFECTIONS IN THE WELDED AREA OF BOTH THE TOP AND BOTTOM GUSSETSMar 28, 1996 · N83032 · Bbavia 7ACSDR 96ZZZX2386Spar · crackedDISMANTLED BOTH LEFT AND RIGHT WINGS FOR RECOVERING. ALL SPARS WERE REMOVED FOR CLEANING, INSPECTION, AND VARNISHING. WITH THE WING SPAR FITTINGS REMOVED, FOUND THE SPAR FITTING HOLES HAD CRACKS EMANATING FROM THE TWO INBOARD HOLES THROUGH THE BUTT OF THE SPAMar 28, 1996 · N83032 · Bbavia 7ACSDR 96ZZZX2385Spar · damagedDISMANTLED LEFT AND RIGHT WING FOR THE PURPOSE OF RECOVERING. WITH THE OLD FABRIC REMOVED, FOUND BOTH REAR SPARS HAD BEEN CHEWED BY MICE MIDWAY BETWEEN THE WING ROOT AND THE STRUT ATTACH FITTING. IT APPEARS THIS DAMAGE WAS PRESENT WHEN THE WINGS WERE LAST REMar 28, 1996 · N83032 · Bbavia 7ACSDR AU960531Spar · corroded(AUS) WING REAR SPARS CORRODED IN AREA BENEATH STEEL FITTINGS AS REFERRED TO IN AD/PA28/40 AND AD/PA32/27 - THE CORROSION WAS ONLYFOUND FOLLOWING REMOVAL OF THE FITTINGSMar 20, 1996 · Piper PA32300SDR MZZA96025Spar · corrodedTNN - DURING 1/2D CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON RIGHT WING FRONT SPAR LOWER CHORD PLATE BELOW NR 5 SLAT ACTUATOR. THE CORRODED CHORD PLATE WAS CLEAN UP AND REPAIRED PER B727 51-10-6 AND 51-40-4. HANGAR NON ROUTINE REMar 17, 1996 · N15781 · Boeing 727232SDR DLL17960751Rear Spar · crackedCRACKS WERE FOUND EMANATING FROM EXISTING FASTENER HOLES BETWEEN IWS 293.58 AND IWS 346.109 ON THE LT AND RT WING. THE CRACKS WERE FOUND IN THE REAR SPAR UPPER CAP, WEB, UPPER WING SKIN. THE SUBJECT FASTENER HOLES WERE OVERSIZED TO REMOVE THE CRACKS IN THE DMar 15, 1996 · N766DA · Lkheed 10113853SDR 96FDEA00555Spar Chord · corrosionCORROSION (C53-132-02) ON THE WING CENTER SECTION REAR LOWER CHORD, STA 870 LBL 20 TO 26 WL 140. REMOVED AND REPLACED LOWER CHORD PER FEDEX EA 7-5710-27481.Mar 11, 1996 · N194FE · Boeing 72722SDR 96FDEA00554Spar Chord · corrosionCORROSION (C53-132-02) ON THE WING CENTER SECTION REAR UPPER SPAR CHORD, STA 870 LBL 30 RBL 30 WL 174. REMOVED AND REPLACED UPPER CHORD PER FEDEX EA 7-5710-27481.Mar 11, 1996 · N194FE · Boeing 72722SDR 96FDEA00535Spar Chord · corrosionCORROSION (C53-132-02, 1) ON THE WING CENTER SECTION UPPER SPAR CHORD STA 870 LBL TO RBL 60 WL 178. REMOVED AND REPLACED UPPER SPAR CHORD.Mar 11, 1996 · N187FE · Boeing 72722SDR 96FDEA00534Spar Chord · corrosionCORROSION (C53-132-02, 1) ON THE WING CENTER LOWER SPAR CHORD STA 870 LBL 36 TO 40 WL 138. REMOVED AND REPLACED LOWER SPAR CHORD.Mar 11, 1996 · N187FE · Boeing 72722SDR 9606129962Spar Cap · corrodedDURING PERIODIC CHECK, FOUND LEFT WING OUTBOARD AFT TOP SPAR CAP CORRODED AT WS XFS 530. INSTALLED REPAIR PER EA 99-109480.Mar 11, 1996 · N914RW · Doug DC931SDR TC8A96024Spar Cap · crackedRIGHT WING REAR SPAR CAP AT XW 69.50 HAS 2 CRACKS BETWEEN STIFFENERS, 2.5-7 INCHES. REPAIRED AFFECTED AREA AS PER SRM 57-5-0. (M)Mar 10, 1996 · N808CK · Doug DC8F55SDR 96ZZZM695Spar Cap · crackedRIGHT WING REAR SPAR CAP AT XW 69.50 HAS 2 CRACKS BETWEEN STIFFENERS, 2.5 THROUGH 7 INCHES. REPAIRED AFFECTED AREA AS PER SRM 57-5-0. REFERENCE TC8A96024.Mar 10, 1996 · N808CK · Doug DC8F55SDR RAAAB196003Spar Cap · corrodedDURING SCHEDULED C-CHECK, INSPECTION OF RIGHT WING FOUND FORWARD LOWER SPAR CAP CORRODED AT WS 410. REPAIRED PER BOEING MSG 7271-96-0571. (M)Mar 8, 1996 · N831RV · Boeing 72722CSDR 96FDEA00642Spar Chord · crackedWS 304 RT WING 3RD STRINGER AFT OF FWD UPPER STAR CHORD CRACKED. REPAIRED STRINGER AT WS 304, 3RD FROM TOP FRONT SPAR CHORD. REPAIRED PER SRM 57-10-4.Mar 8, 1996 · N119FE · Boeing 727227SDR DLL17960907Rear Spar · fatigueDURING THE ACCOMPLISHMENT OF EO 7-59089-3AD, CRACKS WERE FOUND EMANATING FROM EXISTING FASTENER HOLES BETWEEN IWS 293.58-346 ON THE LT AND RT WING. THE CRACKS WERE FOUND IN THE REAR SPAR UPPER CAP, WEB, UPPER WING SKIN. THE SUBJECT FASTENER HOLES WERE OVERSIMar 4, 1996 · N766DA · Lkheed 10113853SDR UPS96805896Spar · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT WING REAR SPAR AT WW IS CRACKED AT LOWER HORIZONTAL CAP RBL 30 FS 857. REPAIRED PER UPS EO DC8-5710-8088A.Mar 1, 1996 · N797UP · Doug DC871FSDR AU960228Spar · corroded(AUS) RH WING AFT SPAR TO STEEL PLATE PN 66762-00 SEPARATED DUE TO CORROSION OF JOINING RIVETS - WHEN THE PLATE WAS REMOVED SEVERECORROSION WAS ALSO FOUND ON THE REAR SPAR - CAUSED BY CORROSION ACTION BETWEEN SPAR AND STEEL PLATE - SEE MDR 96/0226 AND MDR96/0Feb 29, 1996 · Piper PA28235SDR AU960226Spar · corroded(AUS) LH WING MAIN SPAR CONTAINED EXFOLIATION CORROSION IN AREA OF REAROUTBOARD ATTACHMENT BOLT HOLE - FOUND WHEN WING REMOVED FROM FUSELAGE - AIRCRAFT WAS MANUFACTURED IN 1963 AND HAD BEEN PARKED IN THE OPEN FOR THE LAST 12 MONTHS - SEE MDR 96/0227 AND MDR 96Feb 29, 1996 · Piper PA28235
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