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 20010509CW009Spar · crackedIN RECOVERING AIRFRAME, FOUND CRACK IN RIGHT WING REAR SPAR. AIRCRAFT WRECKED IN A NOSE OVER. NO LOG RECORD OF REPAIR TO REAR SPAR.Apr 13, 2001 · N62667 · Bbavia 7ECSDR 20010606CW003Spar · corrodedWING WAS BEING DISASSEMBLED FOR RIB REPLACEMENT. REINFORCEMENT PLATE WAS DRILLED OFF AND CORROSION FOUND ON AFT FACE OF SPAR WEB AND FACE OF REINFORCEMENT PLATE. CAUSE: MOISTURE WICKING BETWEEN PLATES AND LACK OF CORROSION PROTECTION.Apr 12, 2001 · N7031Z · Piper PA25235SDR MWEA010572Spar · corrodedLIGHT CORROSION ON XCW 58 TEE LOWER SIDE JUST UNDER THE INBOARD FORWARD LOWER END OF STRINGER 22, LEFT WING INTERNAL. -- REMOVED CORROSION. BLEND OUT IS ACCEPTABLE FOR STRENGTH, IAW BOEING TELEX MWX-ORD-01-00146H.Apr 11, 2001 · N209ME · Doug DC932SDR MWEA010571Spar · corrodedLEFT WING INTERNAL, LIGHT CORROSION ON XCW 58 TEE HORIZONTAL LEG BETWEEN STRINGER 15 AND 16. REMOVED CORROSION. BLENDOUTS ARE ACCEPTABLE FOR STRENGTH, IAW BOEING TELEX MWX-ORD-01-00146H.Apr 11, 2001 · N209ME · Doug DC932SDR MWEA010570Spar · corrodedLEFT WING INTERNAL, LIGHT CORROSION ON XCW 58 TEE HORIZONTAL LEG BETWEEN STRINGER 12 AND 13. REMOVED CORROSION AND BLENDED. BLENDOUTS ARE ACCEPTABLE FOR STRENGTH, IAW BOEING TELEX MWX-ORD-01-00171H DATED 2/28/01.Apr 11, 2001 · N209ME · Doug DC932SDR MWEA010569Spar · corrodedLEFT WING INTERNAL, 4 AREAS OF LIGHT CORROSION ON BOTTOM HORIZONTAL LEG OF FORWARD SPAR FROM XCW 58 TO 12 INCHES OUTBOARD OF XCW 58. -- BLENDED AREAS. AREAS ARE ACCEPTABLE FOR STRENGTH, IAW BOEING TELEX MWX-ORD-01-00147H DATE 21 FEB 01.Apr 11, 2001 · N209ME · Doug DC932SDR MWEA010555Spar · corrodedAFT SPAR SPLICE TEE REMOVED TO FACILITATE OTHER MAINTENANCE, STATION 111.5. FOUND CORROSION. FABRICATED AND INSTALLED SPLICE TEE.Apr 9, 2001 · N209ME · Doug DC932SDR MWEA010552Spar · corrodedRIGHT WING INTERNAL: LIGHT CORROSION ON OUTBOARD EDGE OF XCW 58 SPAR TEE LOWER LEG, FORWARD OF STRINGER 22. REMOVED CORROSION AND BLENDED AREA; WING TEE IS WITHIN SERVICEABLE LIMITS PER TELEX MWX-ORD-01-00200H DATED 07 MARCH 2001.Apr 9, 2001 · N209ME · Doug DC932SDR MWEA010551Spar · corrodedRIGHT WING INTERNAL: FOUR AREAS OF LIGHT TO MODERATE CORROSION ON XCW 58 TEE LOWER LEG BETWEEN STRINGEER 21 AND 22. REMOVED CORROSION AND BLENDED AREAS; WING TEE IS WITHIN SERVICEABLE LIMITS PER MWX-ORD-01-00200H DATED 07 MARCH 2001.Apr 9, 2001 · N209ME · Doug DC932SDR MWEA010550Spar · corrodedRIGHT WING INTERNAL: LIGHT TO MODERATE CORROSION ON XCW 58 SPAR TEE LOWER LEG FORWARD OF STRINGER 16. REMOVED CORROSION; WING TEE IS WITHIN SERVICEABLE LIMITS PER TELEX MWX-ORD-01-00200H DATED 07 MARCH 2001.Apr 9, 2001 · N209ME · Doug DC932SDR MWEA010549Spar · corrodedLEFT AUX SPAR WEB HAS INTERGRANULAR CORROSION. FABRICATED AND INSTALLED WEB.Apr 9, 2001 · N209ME · Doug DC932SDR MWEA010547Spar · corrodedRIGHT WING INTERNAL: LIGHT CORROSION ON LOWER HORIZONTAL LEG OF FORWARD SPAR, STARTING 3 INCHES OUTBOARD OF XCW58 FOR A STRETCH OF APPROXIMATELY 12 INCHES OUTBOARD. REMOVED CORROSION AND BLENDED AREA ACCEPTABLE PER MWE/BOEING TELEX #MWX-ORD-01-00206H.Apr 9, 2001 · N209ME · Doug DC932SDR 01FDEA00266Spar · corrodedDURING ROUTINE INSP, FWD FACE OF THE BS 870 BULKHEAD BL 0 UP 9 INCHES FROM OPEN FOR HOT AIR DUCT IN KEELBEAM FOUND CORRODED. *S/D* REPAIRED REAR SPAR WEB PER IAW FEDEX EA 7-5710-57223.Apr 6, 2001 · N124FE · Boeing 72725CSDR MWEA010246Spar · corrodedREMOVE RIGHT LOWER WING TEE P/N 9911603-4 DUE TO NUMEROUS CORROSION DISCREPANCIES. REMOVED AND REPLACED RIGHT LOWER WING SPAR TEE.Apr 5, 2001 · N800ME · Doug DC914SDR 2002FA0000253Spar · crackedWHILE COMPLYING WITH AD, A LONGITUDINAL CRACK IN THE RIGHT FOREWARD WOODEN WING SPAR APPROXIMATELY 30 INCHES LONG.Apr 3, 2001 · N6309N · Bbavia 7ECASDR GAIA01087STFrame · corrodedDURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED RIGHT WING UPPER SPAR LEADING EDGE CORRODED AT WS 90. ACCOMPLISHED RIGHT WING UPPER SPAR CHORD REPAIR WS 130-139 PER REPAIR ORDER FASI-007RO-1 REV I/R DATED MAR 27, 2001 AND STRUCTURAL SUBSTANTIATION REApr 2, 2001 · N6833 · Boeing 727223SDR 20010419CW012Spar · crackedA LONGITUDINAL CRACK IN THE RIGHT FORWARD WOODEN WING SPAR, APPROXIMATELY 30 INCHES LONG.Apr 2, 2001 · N6309N · Bbavia 7ECASDR LAO2002F00000Spar · crackedDURING AN ANNUAL INSPECTION AD (WING SPAR CRACKING) WAS COMPLIED WITH IAW SB PER AD. A LONGITUDINAL CRACK WAS FOUND IN THE FRONT LEFT HAND WING SPAR THAT STARTED NEAR THE LIFT STRUT ATTACH POINT AND RAN INBOARD APPROXIMATELY 36 INCHES TOWARDS THE WING ROOT.Apr 1, 2001 · N5151X · Bbavia 7GCBCSDR 01FDEA00244Spar · corrodedDURING ROUTINE INSP, THE AFT FACE OF THE CENTER WING TANK FOUND CORRODED 9 INCHES UP FROM BOTTOM OF THE TANK AT RBL 9. *S/D* REPAIRED REAR SPAR PER IAW FEDEX EA 7-5710-57223.Mar 31, 2001 · N124FE · Boeing 72725CSDR 01FDEA00246Spar · corrodedDURING ROUTINE INSP, THE CTR FUEL TANK AFT WEB FOUND CORRODED ON THE AFT FACE FROM LBL 15 TO LBL 18, 6-8 IN UP FROM BOTTOM OF TANK. *S/D* REPAIRED REAR SPAR WEB PER IAW FEDEX EA 7-5710-57223.Mar 31, 2001 · N124FE · Boeing 72725CSDR AUS20010536Spar · corroded(AUS) LT AND RT WING FORWARD AND AFT SPAR LOWER FLANGES CORRODED IN THE AREA BETWEEN RIB 13 AND RIB 18.Mar 30, 2001 · Bag BAE146200ASDR 2001UALA00366Spar · crackedRT WING SPAR UPPER CHORD CRACKED. REPAIRED CRACKED CHORD. MAJOR REPAIR ACCOMPLISHED.Mar 29, 2001 · N310UA · Boeing 737322SDR CA010529011Spar · cracked(CAN) AIRCRAFDT HEAVILY INSPECTED FOLLOWING GROUND LOOP. CRACK DISCOVERED PROPOGATING FROM AILRON CENTRE HINGE BOLT HOLE AND EXTENDING FOR SEVERAL FEET FOLLOWING THE GRAIN LINE. WING WAS REMOVED FROM AIRCRAFT, AND REAR SPAR WAS SPLICE REPAIRED.. . . .Mar 27, 2001 · Boeing A75N1SDR UPS01235554Spar · crackedINSPECTION TYPE: C & SI, CRACK ON REAR SPAR WEB AT APPROX LBBL 16 AT TOP CORNER OF CUTOUT FOR ACCESS PANEL WEB REPAIR CARRIED OUT IAW SRM 51-40-2 FIG 1Mar 26, 2001 · N926UP · Boeing 72731CSDR 20010326CW005Spar · crackedDURING ANNUAL INSPECTION, FOUND COMPRESSION CRACKS ON THE RIGHT WING REAR SPAR AT TOP LOCATION ON TOP SIDE OF SPAR. THIS COMPRESSION CRACK WAS HIDDEN UNDER OLD SPAR VARNISH AND WOULD HAVE BEEN MISSED IF TOP INSPECTION HOLES WERE NOT INSTALLED.Mar 26, 2001 · N70824 · Bbavia 7ECSDR EIA2001128Spar · crackedHKG-HAECO - FOUND RT WING REAR SPAR WEB, WBL 445 WEB OUTBOARD VERTICAL CHANNEL CRACKED. REPLACED VERTICAL STIFFENER PER SRM 51-10-01. (M)Mar 23, 2001 · N470EV · Boeing 747273CSDR UPS01235558Spar · damagedINSPECTION TYPE:C&SI SEVERAL RIVET HEADS POPPED ON THE CENTER SECTION REAR SPAR UPR CHORD & VERT. WEB AT LBL 37 LBL 17. REPAIR CARRIED OUT IAW SRM 51-30-2 & SRM 51-30-01Mar 22, 2001 · N926UP · Boeing 72731CSDR UPS01235553Spar · crackedINSPECTION TYPE: C, WING CENTER SECTION FRONT SPAR T FITTING CRACKED LWR CHORD STA 740 LBL 42. REPLACED WING CENTER SECTION FRONT SPAR T FITTING T LWR CHORD STA 74 0 LBL 42 IAW B727 SRM 51-30-2Mar 21, 2001 · N932UP · Boeing 72725CSDR MALA010338Spar · chafedFOUND DURING C-CHECK, LT WING FWD SPAR LOWER CAP IB OF NACELLE IS CHAFED. MAINTENANCE LIGHTLY BLENDED AREA, ALODINED BARE METAL IAW SRM 51-20-43. FOUND DEEP CORROSION PITS, OUT OF ALLOWABLE LIMIT REF SRM 51-10-10. REMOVED 511BL/CL/AL TO FOM, REINSTALLED I/ES Mar 19, 2001 · N430XJ · Saab 340BSDR MALA010337Spar · chafedFOUND DURING C-CHECK, RT WING FWD SPAR LOWER CAP IB OF NACELLE IS CHAFED. MAINTENANCE LIGHTLY BLENDED AREAS IAW SRM 51-10-10, ALODINED BARE METAL IAW SRM 51-20-43. FOUND DEEP CORROSION PITS, OUT OF ALLOWABLE LIMIT REF SRM 51-10-10. REMOVED 611BR TO FOM IAW AMMar 19, 2001 · N430XJ · Saab 340BSDR DHL2001741511Spar · corrodedRIGHT WING, LOWER SPAR HAS EXFOLIATED CORROSION UNDER CAVITY CUTOUT FOR NR 8 LEADING EDGE SLATACTUATOR. REMOVED L/E ACCESS PANELS 6542; 6543 6546 AND 6540 AT RIGHT WING LOWER SURFACEAS PER B727 SRM 51-30-2. REMOVED FUEL ACCESS PANELS AT RT WING LOWER SURFACMar 19, 2001 · N741DH · Boeing 7272Q9SDR C2XA01IA221Spar Cap · crackedEMB - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE RIGHT WING SPAR CAP WAS FOUND TO BE CRACKED BETWEEN RIBS 17 AND 18. MAINTENANCE REPAIRED THE WING SPAR IN ACCORDANCE WITH EMB-120 SRM 57-20-05, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Mar 17, 2001 · N17728 · Emb EMB120ERSDR AALA20010548Spar Cap · corrodedTUL - FOUND NR 6 L/E FLAP GAP PANEL SPAR CAP CORRODED. INSTALLED DOUBLER PER BOEING REPAIR DOCUMENT 57-30-00-2, PATES 1-3. (M)Mar 15, 2001 · N891AA · Boeing 727223SDR AALA20010544Spar · corrodedTUL - FOUND CORROSION ON LOWER CHORD OF FRONT SPAR BELOW ACTUATOR FOR THE NR 2 SLAT, WS 629. REMOVED CORROSION AND INSTALLED DOUBLER STRAP PER SRM 57-30-00. (M)Mar 15, 2001 · N891AA · Boeing 727223SDR EIA2001158Spar · corrodedFOUND BS 1241 LEFT AND RIGHT WING CENTER SECTION REAR SPAR WEB AFT SURFACE AT BULKHEAD FTG AREA CORRODED AND BLENDOUT EXCEEDS SRM LIMITS. REMOVED CORROSION AND REPAIRED PER BSB 57-2263. SECTION OF PX WEB ANGLE TRIMMED FOR ACCESS, NEW SECTION SPLICEDIN PER BOMar 12, 2001 · N471EV · Boeing 747273CSDR DHL2001741507Spar · corrodedRIGHT WING LOWER SPAR HAS EXFOLIATED CORROSION UNDER CAVITY CUT OUT FOR NR 8 LEADING EDGE SLAT ACTUATOR. REMOVE L/E ACCESS PANELS 6542, 6543, 6546, AND 6540 AT RIGHT WING LOWER SURFACE AS PER B727 SRM 51-30-2. REMOVED FUEL ACCESS PANELS 17, 18, 19 AT RIGHT WMar 10, 2001 · N741DH · Boeing 7272Q9SDR ABXA010143Structure · leakingTHE SPAR CAP WAS FOUND TO BE LEAKING FUEL JUST INBOARD OF THE NR 1 PYLON AT WS 444. MAINTENANCE INSPECTED AND REPAIRED THE AREA IAW ABX REA D857-40311MR.Mar 9, 2001 · N814AX · Doug DC863FSDR USAA010260Spar · damagedPIT - FOUND REAR SPAR WITH PLY SEPARATION .5 INCH BY .5 INCH, BOTTOM INBOARD SPAR END. REMOVED SPLINTER PLY THEN COMPLETED 2 WET LAY UP THEN RESEALED EDGES PER EA 70365 AND SRM 51-70-17. (M)Mar 8, 2001 · N587US · Boeing 737301SDR U2RB030101Spar Cap · crackedDURING COMPLIANCE OF MCDONNELL DOUGLAS DC-8 S/B 57-90 R5 (NPRM 99-NM-60-AD) DETECTED CRACK ATLOWER FORWARD SPAR AT ATTACH FASTENERS STA XFS 524. CRACK BEYOND S/B 57-90 R5 REPAIR LIMITS.Mar 7, 2001 · N865F · Doug DC863FSDR AUS20010537Spar · corroded(AUS) LT AND RT WING FORWARD AND AFT SPAR LOWER FLANGES CORRODED IN THE AREA BETWEEN RIB 13 AND RIB 18.Mar 1, 2001 · Bag BAE146200ASDR DL73K010347Spar · crackedWHILE ACCOMPLISHING INSPECTIONS PER S/B 737-57-1216 SEVERAL CRACKS WERE FOUND IN 9 FASTENER HOLES COMMON TO THE LT MLG BEAM AFT FITTING AND THE REAR SPAR. THE AFT FITTING WAS REPLACED AND THE FASTENER HOLES WERE OVERSIZED PER ERA 397280-14 AT HMV.Mar 1, 2001 · N315DL · Boeing 737232SDR GAIA01067STSpar · corrodedDURING A LTC INSPECTION AT FLIGHTSTAR JAX, FOUND LEFT WING STATION 431.5 CORROSION ON FRONT SPAR WEB AT LOWER CHORD. ACCOMPLISHED LEFT WING FRONT SPAR WEB REPAIR WS 431.5 IAW B727 SRM 57-10-6 FIG 1 MATERIAL 2024-T3 .250 PO NR 20093117. DIM''S 12 INCH BY 14 IFeb 28, 2001 · N281KH · Boeing 7272J0SDR ABXA010067Spar · crackedTHE FORWARD WING SPAR HAD A THREE INCH CRACK AT BL 0 DIRECTLY ABOVE THE PRESSURE WEB. MAINTENANCE INSPECTED AND REPAIRED THE CRACK IAW ABX REA D953-38815-MR.Feb 28, 2001 · N972AX · Doug DC941SDR QXEA0100147Spar · crackedYYC- RIGHT HAND WING REAR SPAR WEB PLATE IS CRACKED AT STATION 5010. REPAIRED IAW HORIZON AIR EA 4-57-533 AND FOKKER SRM 51-31-01 PAGES 13 AND 14.Feb 27, 2001 · N475AU · Fokker F28MK4000SDR 20010403CW017Spar · corrodedCORROSION FOUND EXFOLIATING (1) SPAR CUP ON RIGHT WING HEAVY CORROSION ON UPPER CABIN (2) CARRY THRU STRUCTURE. (3) VERTICAL STABILIZER SKIN PILLOWED AND RIVETS POPPED. FOUND 15 RIVET HEADS PULLED THRU SKIN ON (4)CANTED BULKHEAD AT FUSELAGE STATION 20.5 BOTTFeb 26, 2001 · N3232X · Cessna 150GSDR 20010403CW016Spar Cap · corrodedCORROSION FOUND EXFOLIATING SPAR CAP OR RIGHT WING HEAVY CORROSION ON UPPER CABIN CARRY THRU STRUCTURE. VERTICAL STABILIZER SKIN PILLOWED AND RIVETS POPPED. FOUND 15 RIVET HEADS PULLED THRU SKIN ON CANTED BULKHEAD AT FUSLAGE STATION 20.5 BOTTOM FUSELAGE. AIRFeb 26, 2001 · N3232X · Cessna 150GSDR QXEA0100380Spar · corrodedYYC-LEFT HAND WING FRONT SPAR CAPS (UPPER AND LOWER) HAVE LIGHT FRETTING BETWEEN STATION 1825 AND 6440. REPAIRED IAW FOKKER SRM 57-01-01.Feb 26, 2001 · N497US · Fokker F28MK4000SDR ABXA010058Rib · corrodedLEFT WING TRAILING EDGE RIB AT STATION 140 WAS CORRODED. MAINTENANCE INSPECTED AND REPAIRED THE RIB IAW ABX REA D957-40000.Feb 20, 2001 · N954AX · Doug DC941SDR UPS01235251Spar · corrodedINSPECTION TYPE:C+SI, AFTER REMOVING A STIFFENER LOCATED AT FWD SIDE OF LT AUX SPAR, THE UPPER CHORD OF THE AUX SPAR WAS FOUND TO HAVE CORROSION IN A 2 INCH SECTION AROUND WS 277. UPPER CHORD REPAIRED IAW SRM 51-10-01.Feb 19, 2001 · N941UP · Boeing 72722CSDR UPS01235243Spar · corrodedINSPECTION TYPE:C+SI, CORROSION FOUND ON REAR SPAR UPPER CHORD OUT OF LIMITS. CHORD REPLACED IAW BOEING DRG 65C21531 AND SMRO EO 2001-006-004 UPS ENGINEERING FILE NR B727-5710-4094-A.Feb 18, 2001 · N941UP · Boeing 72722C
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