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"

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SDR CA051107003Spar · cracked(CAN) DURING REPLACEMENT OF LT WING IB LEADING EDGE, AN APPROX 12-INCH CRACK IN LOWER SPAR FLANGE WAS DISCLOSED. THE CRACKED SPAR FLANGE PIECE FOLLOWED THE LEADING EDGE DURING REMOVAL. LOCATION, YW 136.30 TO YW 157.875. THE CRACKED SPAR FLANGE PIECE IS BEING RNov 7, 2005 · Bombdr DHC8400SDR FE5F200500003Spar · corrodedDURING THE C12 CHECK, PERFORMING THE TASK 0314 AND CPCP CARD 16-57301, AT RT WING REAR SPAR LOWER FOUND 6 X 1 INCH MAX D=0.150 INCH CORROSION AT XRS=188.5 TO 194.5. REQUEST BOEING ASSISTANCE AND IAW BOEING'S RESPONSE REPAIR THE CORROSION AREA. MANUFACTURE ISNov 1, 2005 · Doug MD83SDR GAIA05028STSpar · crackedDURING B-CHECK A FUEL LEAK WAS FOUND ON THE FUSELAGE AT STA 740. INSPECTION REVEALED A CRACK ON THE WING CENTER SECTION SPAR WEB. THE WING SPAR WEB WAS REPAIRED IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K)Oct 27, 2005 · N854AA · Boeing 727223SDR TSAA0557058Spar · corrodedRIGHT WING FRONT SPAR, LOWER CORD FWD FLANGE CORRODED AT SLAT STA 243.0 AND SLAT STA 254.0.Oct 24, 2005 · N821AL · Boeing 737230SDR 2005FA0001493Spar · separatedTHE MAIN SPARS (PN 4500-01 AND 4500-02, RT AND LT) WERE BROKEN AWAY FROM THE WINGLET. WINGLETS AND SPAR ARE PART OF STC INSTALLATION. SPAR IS ATTACHED TO INSIDE WINGLET WITH FIBERGLASS CLOTH. CLOTH WAS TORN AND DELAMINATED. SPAR WAS COMPLETELY SEPARATED FROct 20, 2005 · Airtrc AT402SDR UPS05245851Spar · corrodedAREA OF SUSPECT CORROSION ON WING CENTER SECTION REAR SPAR LWR CHORD BS 870 RBL36 DUE TO 2 POPPED FASTENER HEADS. PLEASE INVESTIGATE AND RECTIFY AS NECESSARY. AS PER BOEING INSTRUCTIONS THE LWR CHORD WAS REPLACED. NEW CHORD WAS CUT AT RBL 9.5. REPAIR SPLICEOct 16, 2005 · N918UP · Boeing 72730CSDR EIA2005230Spar · crackedRHW NR 3 MAIN TANK MID SPAR WEB UPPER FASTENER HOLES (2 EA) CRACKED BETWEEN WS 614 AND WS 642. REPAIRED DEFECTIVE CRACKED WEB PER SRM 57-1-06, FIG 5.Oct 8, 2005 · N486EV · Boeing 747212BSDR AU510001574Spar · crackedWING SPAR INNER WEB CUTOUT CRACKED IN THREE PLACES. THREE CRACKS WERE FOUND IN THE STARBOARD INNER WEB STRINGER 13 CUTOUT MEASURING 12.7MM (0.5IN), 3.175MM (0.125IN) AND 9.525MM (0.375IN). FOUND DURING INSPECTION IAW AD/SWSA226/86. SEE ATTACHMENTS FOR FURTHOct 7, 2005 · Swrngn SA227*SDR 2005FA0001349Spar Cap · crackedDURING COMPLIANCE WITH AD 89-25-10, 1,000 HOUR INTERVAL EDDY CURRENT INSPECTION, THE SPAR CAP WAS FOUND TO BE CRACKED 3 INCHES OB OF BATHTUB AT RT WING LOWER FORWARD SPAR ATTACH POINT.Oct 4, 2005 · N300MT · Beech E90SDR 2005FA0001364Spar Cap · corrodedDURING AN ANNUAL INSPECTION, SOME CORROSION WAS FOUND IN THE AREA OF THE RT WING TIE DOWN ASSY, UPON FURTHER INVESTIGATION AN AREA OF APPROXIMATELY 8 INCHES IN LENGTH WITH SEVERE INTERGRANULAR CORROSION WAS DISCOVERED ON THE LOWER SPAR CAP POSSIBLY CAUSED BY DSep 28, 2005 · N1071T · Beech 95B55SDR 2005FA0001356Spar · crackedCRACKED SPAR PLATE AT WING STRUT ATTACHMENT LT WING. APPEARS THAT SOME ONE HAS ATTEMPTED TO ADD GLUE TO PLATE FROM A HOLE CUT INTO FABRIC ON TOP WING. IN OTHER WORDS, THIS CRACK HAS BEEN THERE FOR SOME TIME. COULD NOT DETERMINE IF MAIN SPAR CRACKED OR SPLITSep 22, 2005 · N5033V · Bbavia 7GCBCSDR 05FDEA02860Spar · damagedDURING AIRPLANE'S CONVERSION FROM P TO F FOUND DOUBLE HOLE 0.187* 0.291 ON TE. RT WING LOWER CAP AT STA XORS 728 AND HOLE OVALIZED IN FRG PANEL. NORMALIZED HOLE AND INSTALLED REPAIR BUSHING PER SRM 51-31-01 VOL II, REPAIRED PANEL PER SRM 57-00-01 FIG 4 SH 2.Sep 14, 2005 · N571FE · Doug MD1010FSDR 05FDEA02734Spar · corrodedLT WING TOPSIDE FOUND CORROSION UNDER T/E PANEL JUST FWD OF O/B AILERON XORS 917.0 AND XORS 1040.0. REPAIR CARRIED OUT AS PER EA1-5710-87601.Sep 2, 2005 · N575FE · Doug MD11SDR SWAA052548Spar · crackedDURING SCHEDULED 1/4D CHECK, FOUND RT WING FWD SPAR PLATE CRACKED AT WBL 70.85. REPAIRED WING SPAR PER SWA EA & SRM.Aug 24, 2005 · N369SW · Boeing 7373H4SDR 2005FA0001194Spar · crackedTWO COMPRESSION CRACKS ON RIGHT WING REAR SPAR, ONE ON EITHER SIDE OF PLYWOOD DOUBLER AT STRUT ATTACH POINT. OUT BOARD CRACK EXTENDS APPROX ONE THIRD DEPTH OF SPAR, EXTENT OF INBOARD CRACK AS YET UNKNOWN, MAY GO BEHIND DOUBLER, CRACKS FOUND DURING INSPECTION RAug 21, 2005 · N8305V · Bbavia 7GCAASDR 05FDEA02489Spar Cap · damagedA TEMPORARY REPAIR (PER S/B DC10-57A137) INSTALLED BY A PREVIOUS OPERATOR ON THE RT REAR SPAR LOWER CAP AT STATION XORS 417.00 REQUIRES REPLACEMENT. E.A. 8-5710-86514 PROVIDES INSTRUCTIONS FOR THE REPLACEMENT OF THE TEMPORARY WITH A PERMANENT REPAIR. THE PERMAug 16, 2005 · N396FE · Doug MD1010FSDR 2005FA0001137Spar · crackedAFT RT SPAR HAS LONGITUDINAL CRACK ON LOWER END. CRACK OCATED AT STRUT ATTACH POINT. SPAR ALSO SHOWS SIGNS OF ROTTING IB OF CRACK AREA. (K)Aug 11, 2005 · N84286 · Bbavia 7ACSDR DL76S050692Spar · crackedFRONT SPAR AND WING LEADING EDGE RIB HAS CRACK INDICATION. HOLE WAS OVERSIZED TO REMOVE THE CRACK PER ER/A 450059-14AD, REF AD 2004-16-12 AND 01-074906-03AD.Aug 10, 2005 · N116DL · Boeing 767332SDR 05FDEA02180Frame · crackedONE CRACK 0.5 INCH LONG ON FRAME SIDE RT WING AT STA XORS 623. REPAIRED CRACK IAW SRM 57-20-00 FIG 1 VOL 1.Aug 2, 2005 · N381FE · Doug MD1010FSDR 05FDEA02177Frame · crackedONE CRACK 0.25 INCH LONG INSIDE FRAME LEADING EDGE LT WING AT XORS 368. REPAIR CRACK IAW SRM 57-20-00 FIG 1 VOL 1.Aug 2, 2005 · N381FE · Doug MD1010FSDR 05FDEA02173Frame · crackedONE EACH CRACK .5 INCH LONG, ON LEADING EDGE FRAME LT WING AT XORS 372. REPAIR IAW SRM 57-20-00 FIG 1 VOL 1.Aug 2, 2005 · N381FE · Doug MD1010FSDR SIM2005F00011Spar · damagedLT AILERON AND WING WERE DAMAGED BY A CATERING TRUCK. MAINTENANCE REPLACED LT WING SPAR SEGMENT AND WING SKIN. REPLACED LT AILERON IAW EO. AIRCRAFT WAS RETURNED TO SERVICE. (K)Jul 20, 2005 · N925AE · Emb EMB145LRSDR AALA20050480Spar · corrodedAFW - REAR SPAR WEB WING CENTER SECTION OUTBOARD SIDE OF THE INBOARD LEG OF THE PICKLE FORK HAS BLEND IN AREA APPROXIMATELY 3 INCH BY 0.5 INCH WITH A DEPTH OF 0.067 INCH. REMOVED EXPOSED CORROSION FROM THE REAR SPAR SURFACE. UNDERCUT THE SPAR AND PICKLE FORKJul 15, 2005 · N386AA · Boeing 767323SDR 2005FA0001007Spar Cap · damagedSMOKING MS20470DD8 RIVETS OBSERVED AT WS122 - 140 PROX DURING SCHEDULED INSPECTION. THESE RIVETS ARE CRITICAL TO WING INTEGRITY. IT APPEARS THAT THE RIVETS DID NOT PROPERLY ENGAGE THE HOLE DURING OEM INSTALLATION. SUGGEST ALL WING BOXES WITHIN 10 SERIAL NUJul 12, 2005 · N8PMLK · Dhav DHC6300SDR UPS05845059Spar Cap · crackedLT AFT LWR WING SPAR CAP F/S 857 IS CRACKED IN THREE PLACES FROM LBL27-LBL45. REPAIRED LT LWR SPAR CAP IAW SRO DWG 8570009, SRM 51-1-20D, 51-1-24.Jun 30, 2005 · N851UP · Doug DC873FSDR UPS05444870Spar · crackedINSPECTION TYPE: C, LT WING REAR SPAR UPPER CHORD HORIZONTAL FLANGE FWD FASTENER HOLE AT WS 392 CRACK RUNNING AFT APPROX 0.080 INCH. LEFT WING REAR SPAR UPPER CHORD HORIZONTAL FLANGE FWD FASTENER HOLE REPAIRED AT WS 392 AREA AS PER HX RS R57-25-35337 & UPS EOJun 30, 2005 · N672UP · Boeing 747123SDR UPS05845056Spar · crackedFS 855 AFT SIDE OF REAR SPAR LOWER CHORD UPPER SURFACE FROM RBL36.5 -45.00 HAS 8.5" CRACK. REPAIRED REAR SPAR IAW SRO 8570009.Jun 28, 2005 · N851UP · Doug DC873FSDR 05FDEA01646Spar · corrodedCORROSION ON RT WING FUEL CELL FWD SPAR WEB FWD FACE AROUND CUTOUT 7540R. *S/D* REPAIRED RIGHT WING FUEL CELL FWD SPAR WEB FACE AROUND PANEL 7540 PER FED EX EA 7-5710-86300.Jun 22, 2005 · N482FE · Boeing 727200SDR CA050617007Doubler · cracked(CAN) DURING ROUTINE LPI INSPECTION OF THE FRONT WING SPAR CARRY THRU STRUCTURE AND REPAIR DOUBLERS IN ACCORDANCE WITH AD90-08-14, THE LT FWD REPAIR DOUBLER WAS FOUNDCRACKED IN THE LOWER BEND RADIUS IN THE SAME SPOT AS THE ACTUAL WING SPAR WHICH THE DOUBLER WAJun 15, 2005 · Beech 95B55SDR AU510001967Bolt · shearedCENTER FUEL TANK WING SPAR ATTACHMENT BOLTS (4OFF) HAD SHEAR BOLT HEADS. FUEL LEAKING FROM CENTER TANK AT RT FRONT CORNER ABOVE THE WING TO FUSELAGE ATTACHMENT LINK AT FRAME 26 RIB 2.Jun 10, 2005 · Bag BAE146300ASDR CALA0500194Spar · corrodedINSPECTION FOUND LT WING FRONT SPAR CORRODED AT LT NR 1 BOOST PUMP UPPER BONDING JUMPER STRAP CONTACT, WS 120-121. REPAIRED IAW ECRA 5711-01140.Jun 10, 2005 · N27213 · Boeing 737824SDR AWXA200500779Spar · damagedDURING C-10 CHECK FOUND TWO ELONGATED HOLES ON BRACKET, FORWARD FLAP SPAR AND FLAP SKIN LOCATED ON THE LT WING INBOARD MAIN FLAP, FORWARD OF LOWER SPAR AND SKIN. MAINTENANCE REMOVED DAMAGE FROM ELONGATED HOLES ON BRACKET, FORWARD FLAP SPAR AND FLAP SKIN LOCAJun 6, 2005 · N905AW · Boeing 7572S7SDR 2005FA0000849Spar Cap · corrodedLT WING REAR UPPER SPAR CAP IN NACHELL/EXHAUST AREA AND OUTBOARD WS 80.0-100.0 APPROX. 20 INCHES, WAS FOUND DURING VISUAL INSPECTION, TO HAVE SEVERE EXFOLIATED INTERGRANULAR CORROSION RINDERING THIS SECTION OF SPAR TO BE UNSERVICABLE. ALSO JUST I/B OF BATTERYJun 6, 2005 · N3031R · Cessna 310DSDR SWAA051606Spar · crackedDURING SCHEDULED D-CHECK, FOUND LT & RT WING REAR SPAR UPPER CHORDS CRACKED AT MLG BEAM 2ND INBOARD CUTOUT HOLE. REMOVED AND REPLACED REAR SPAR UPPER CHORDS PER BFG ER.May 31, 2005 · N660SW · Boeing 737301SDR AWXA200600798Spar · crackedSAL - DURING C8 CHECK DISCOVERED CRACK IN HOLE NR 84 OF THE LT WING REAR SPAR, LT GEAR SUPPORT RIB 5 POSITION THAT REQUIRED OVERSIZE BEYOND SERVICE BULLETIN LIMITS. MAINTENANCE REAMED HOLE AND INSTALLED OVERSIZED FASTENER AT THE NR 84 HOLE OF THE LT WING REARMay 21, 2005 · N639AW · Airbus A320232SDR AWXA200600800Spar · crackedSAL - DURING C8 CHECK DISCOVERED CRACK IN THE NR 52, 54 AND 55 HOLES OF THE LT WING REAR SPAR, ACTUATOR CYLINDER ANCHORAGE. REQUIRES OVERSIZING THE HOLES BEYOND SERVICE BULLETIN LIMITS. MAINTENANCE REAMED HOLE AND INSTALLED OVERSIZED FASTENER AT THE NR 52, 5May 19, 2005 · N639AW · Airbus A320232SDR UPS05444654Splice · crackedINSPECTION TYPE:C LEFT BS 1241 WING REAR SPAR UPPER SPLICE BOLT HOLE NR 8 CRACKED AT CHORD (CRACK LENGTH 0.08 INCH). HOLE REWORKED AS PER EO B747-5740-17032-C.May 19, 2005 · N677UP · Boeing 747123FSDR UPS05444655Spar · corrodedINSPECTION TYPE:C RIGHT BS 1241 WING UPPER REAR SPAR NR 3 BOLT HOLE FOUND CORROSION. HOLE REWORKED AS PER EO B747-5740-17032-C. HOLE OVERSIZED TO 1 INCH.May 18, 2005 · N677UP · Boeing 747123FSDR DHL2005741541Spar · corrodedRT WING AT LOWER REAR SPAR WBL 124.2 HAS A CORRRODED TEE ANGLE FITTING. REMOVED AND REPLACED TEE FITTING P/N 65-16201- 188 PO NR 5096248 IAW B727 SRM 51-30-2.May 17, 2005 · N741DH · Boeing 7272Q9SDR 05FDEA01340Spar Cap · corrodedRT WING REAR SPAR UPPER CAP FOUND CORROSION AT XORS 450. REPAIRED AS PER FEDEX EA NR 1-5710-86608. THIS REPAIR CLASSIFIED AS MAJOR REPAIR AS PER GMM 6-2-100.May 17, 2005 · N580FE · Doug MD11SDR 05FDEA01339Spar Cap · corrodedRT WING REAR SPAR UPPER CAP FOUND CORROSION AT XORS 470. REPAIRED AS PER FEDEX EA NR 1-5710-83099 THIS REPAIR CLASSIFIED AS MAJOR REPAIR AS PER GMM 6-2-100.May 17, 2005 · N580FE · Doug MD11SDR AWXA200600799Spar · crackedSAL - DURING C8 CHECK DISCOVERED CRACK IN HOLE NR 54 OF THE RT WING REAR SPAR, ACTUATOR CYLINDER ANCHORAGE. REQUIRES OVER SIZING THE HOLE BEYOND SERVICE BULLETIN LIMITS. MAINTENANCE REAMED HOLE AND INSTALLED OVERSIZED FASTENER AT THE NR 54 HOLE OF THE RT WINMay 14, 2005 · N639AW · Airbus A320232SDR UPS05M44674Spar Cap · corrodedINSPECTION TYPE: 2C, LT WING, UPPER SURFACE, AFT WING SPAR JUST FWD OF NR 3 SPOILER, STRAP HAS BULGE & CRACKED SEALANT, NEED TO EVALUATE FOR CORROSION (2 SPOTS). PERFORMED CORROSION REPAIR ON LT WING UPPER SURFACE AFT WING SPAR IAW SAA SK 254-796823 & UPS REPMay 8, 2005 · N254UP · Doug MD11FSDR 2005FA0000897Spar · crackedDURING ANNUAL INSPECTION, NOTE THAT SEVERAL RIVETS ATTACHING THE RT WING SKIN TO THE LOWER WING SPAR WERE BECOMING LOOSE (SMOKING) JUST OB OF THE MAIN GEAR DOOR AND INBOARD OF THE RIB AT WS79.5. DURING INSP OF INSIDE OF WING IN SAME AREA, A CRACK WAS FOUND ONMay 6, 2005 · N27PG · Piper PA46350PSDR 2005UALA00426Spar · crackedLT & RT MLG SUPPORT BEAMS OUTBOARD FITTINGS AND RT WING SPAR UPPER CHORD ARE CRACKED AT HOLE C. INTERIM REPAIR. ACP. PER EVA IMC-10243. ACP HFEC INSP. OF THE LOWER VERTICAL CHORD FOR CRACK INDICATIONS AT EVERY "C" CHECK. IF A CRACK IS FOUND AT HOLE "C", CONTMay 6, 2005 · N311UA · Boeing 737322SDR 05FDEA01188Spar · corrodedLT WING REAR SPAR TOPSIDE WING CORROSION FOUND AT XORS 725. SKIN TRIMMED, REPAIR DOUBLER AND FILER FABRICATED AND INSTALLED AS PER EA 1-5720-80383.Apr 30, 2005 · N576FE · Doug MD11SDR AWXA200500534Spar · crackedSAL - MAJOR REPAIR - DURING C-08 CHECK A .5 INCH CRACK WAS FOUND ON RT REAR SPAR HOLE 54 NEXT TO RIB NR 3. MAINTENANCE REPAIRED DAMAGE BY REWORKING RT REAR SPAR HOLE IAW AIRBUS REPAIR INSTRUCTION R572-58325 ISSUE D AND ER 26-5700-05121-SS1.Apr 15, 2005 · N638AW · Airbus A320232SDR AWXA200500533Spar · corrodedSAL - MAJOR REPAIR - DURING C-08 CHECK CORROSION WAS FOUND ON RT ACTUATING CYLINDER HOLES 52, 53, 55, 56, 58, 59, & 79-81. MAINTENANCE REPAIRED DAMAGE BY REWORKING RT ACTUATING CYLINDER HOLES PER AIRBUS REPAIR INSTRUCTION R572-58325 ISSUE D AND ER 26-5700-051Apr 15, 2005 · N638AW · Airbus A320232SDR AWXA200500532Spar · corrodedSAL - MAJOR REPAIR - DURING C-08 CHECK CORROSION WAS FOUND ON LT REAR SPAR HOLES 52, 53, 54, 56, & 60. MAINTENANCE REPAIRED DAMAGE BY REWORKING LT REAR SPAR HOLES PER AIRBUS REPAIR INSTRUCTION R572-58325 ISSUE D AND ER 26-5700-05121-SS1.Apr 15, 2005 · N638AW · Airbus A320232SDR AWXA200500531Spar · corrodedSAL - MAJOR REPAIR - DURING C-08 CHECK CORROSION WAS FOUND ON RT REAR SPAR HOLES 52, 53, 55-59, & 79-81. MAINTENANCE REPAIRED DAMAGE BY REWORKING RT REAR SPAR HOLES PER AIRBUS REPAIR INSTRUCTION R572-58325 ISSUE D, AND ER 26-5700-05121-SS1.Apr 15, 2005 · N638AW · Airbus A320232
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