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 RAAA96E8024Spar Cap · corrodedDURING SCHEDULED NR 1 CHECK, FOUND RT WING REAR BEAM UPPER CAP CORRODED AT WS 186 TO 190. REPAIRED PER LUNDBY DESIGN SERVICE DWG 188295.Aug 21, 1996 · N178RV · Lkheed 188CSDR P5CA9600759Spar Chord · corrodedFRONT SPAR LOWER CHORD FOUND CORRODED IN CENTER TANK DRY BAY RBL 77. LEVEL ONE CORROSION REMOVED AND FOUND WITHIN LIMITS IAW SRM 57-10-01. TREATED AND PRIMED IAW SRM 57-20-01.Aug 21, 1996 · N857FT · Boeing 747132SDR P5CA9600721Spar · corrodedCORROSION ON LOWER CHORD OF FRONT SPAR IN CENTER TANK DRY BAY RBL 77. CORROSION REMOVED PER BAC SRM 51-10-01 AND AREA REPROTECTED PER BAC SRM 51-10-02.Aug 21, 1996 · N857FT · Boeing 747132SDR P5CA9600671Spar · corrodedLEVEL 1 CORROSION CENTER WING FRONT SPAR UPPER CHORD DRY BAY FROM RBL 90 TO RBL 115. CORROSION REMOVED PER BOEING SRM 51-10-01, WITHIN LIMITS PER 57-10-01, REPROTECTED PER 51-10-02.Aug 21, 1996 · N857FT · Boeing 747132SDR P5CA9600617Spar · corrodedLEVEL 1 CORROSION ON FRONT SPAR LOWER CHORD IN CENTER TANK DRY BAY AT LBL77. REMOVED CORROSION IAW BOEING SRM 51-10-01 WITHIN LIMITS PER 53-10-01 PROTECTED PER 51-10-01.Aug 21, 1996 · N857FT · Boeing 747132SDR P5CA9600648Spar · corrodedLEVEL 1 CORROSION FRONT SPAR UPPER CHORD IN CENTER TANK DRY BAY FROM LBL 105 TO 115. REMOVED CORROSION PER BOEING SRM 51-10-01 WITHIN LIMITS PER 53-10-01, REPROTECTED PER 51-10-02.Aug 20, 1996 · N857FT · Boeing 747132SDR AU961171Spar · missing rivet(AUS) LH WING MAIN SPAR TOP CAP REAR FLANGE INBOARD MISSING RIVETS - NEW MAIN SPAR AND TOP REAR WING SKIN FITTED IN JUNE 1977 FOLLOWING HEAVY LANDING REPAIRS - PERSONNEL/MAINTENANCE ERRORAug 19, 1996 · Piper PA32300SDR HALA96116Spar · corrosionHNL - FOUND EXFOLIATION CORROSION ON REAR SPAR AFT LOWER TANG AT STATION 414, LEVEL 2. REPAIRED PER SRM 57-09, FIG 11 AND DACO TELEX SVC-HNL-0088/PPS. (M)Aug 14, 1996 · N679HA · Doug DC951SDR AU961133Spar Fitting · failed rivets(AUS) WING REAR SPAR FITTING ATTACHMENT RIVETS FAILED - HEADS FELL OFF - FOUND DURING INSPECTION IAW AD/PA28/40Aug 14, 1996 · Piper PA28R200SDR IXXA96135Spar · crackedWHILE ACCOMPLISHING THE REPLACEMENT OF THE RIGHT MAIN LANDING GEAR FITTING, THE RIGHT LOWER REAR SPAR WAS FOUND TO BE CRACKED BETWEEN WING STATION S XRS 13 AND XRS 20. THE REPAIR OF THE SPAR WAS ACCOMPLISHED IAW DOUGLAS DRAWINGS 5613917, 5613918, 5613919, 561Aug 6, 1996 · N61CX · Doug DC862SDR P5CA9600610Spar · crackedFOUND CRACK ON UPPER CHORD AT STATION 669 NEAR THE FRONT SPAR. REMOVED AND REPLACED CHORD IAW SB 57-2273.Aug 5, 1996 · N832FT · Boeing 747121SDR AALA961174Spar · corrodedTUL - FOUND CORROSION ON FORWARD WING SPAR AND LOWER CHORD ANGLE. CORROSION REMOVED INSTALLED DOUBLERS PER SRM 57-10-6 PG 2A-2C, 6, 7, AND 9. (M)Aug 5, 1996 · N709AA · Boeing 727223SDR 96FDEA01315Spar Chord · corrodedCENTER WING TANK INTERNAL BS 870 REAR SPAR UPPER CHORD CORRODED FROM RBL 6 TO 48. REMOVED CORROSION, CUT OUT SPAR WEB FROM RBL 54 TO LBL 51, INSTALLED WEB DOUBLER AND NEW SPAR CHORD. ALL WORK ACCOMPLISHED PER SRM 51-40-4 FIG 1 ESO 11782 DATE 7-23-96, FAR 811Aug 5, 1996 · N181 · Boeing 72722SDR MWEA96386Spar · corrodedDURING D-CHECK, RT WING REAR SPAR UPPER TANG WAS FOUND CORRODED AT STA XRS 380.0 JSUT ABOVE OUTBD FLAP HINGE. FABRICATED AND INSTALLED REPAIR IAW SRM 57-09, FIG 12.Jul 31, 1996 · N501ME · Doug DC932SDR MWEA96325Spar · corrodedDURING D-CHECK, LT WING AFT SPAR UPPER AND LOWER CAPS WERE CORRODED FROM STA XRS 513 TO XRS 551. REPAIRED THE SPAR AND CAPS PER DAC TELEX SVC-MSP-0411/PDG DATED 30 MAY, 96 AND SRM 57-09, FIG 24.Jul 31, 1996 · N501ME · Doug DC932SDR MWEA96320Spar Cap · corrodedDURING D-CHECK, THE RT WING LEADING EDGE HAD MODERATE SURFACE CORROSION INSIDE BOTTOM SPAR CAP BETWEEN STATIONS XRS 506 TO XRS 545. COMPLETED REPAIR IAW DAC TELEX SVC-MSP-0427/RMK DATED 6/3/96.Jul 31, 1996 · N501ME · Doug DC932SDR 96FDEA01319Spar Web · corrodedCTR FUEL TANK BAY 3, AFT SPAR WEB AT STA 870 BULGED, CRACKED AND CORRODED WITH POPPED RIVETS AT APPROX LBL 40 NEAR UPPER CHORD ANGLE. UPPER CHORD ANGLE HAS POPPED RIVETS IN THIS AREA ALSO.Jul 31, 1996 · N107FE · Boeing 72722CSDR HALA96114Spar · corrosionHNL - FOUND SEVERE CORROSION ON AFT SIDE OF REAR SPAR, LOWER FLANGE AT APPROX STATION 129. REPAIRED PER DACO TELEX SVC-HNL-0092/PPS. (M)Jul 30, 1996 · N679HA · Doug DC951SDR UPS96420964Spar Web · crackedINSPECTION TYPE-C, RT WING FRONT SPAR WEB FOUND TWO CRACKS OUTSIDE OF SB747-57A2266. INSPECTION AREA REF NRC 710789, THE FIFTH HOLE 2MM, SEVENTH HOLE .5MM. REPAIRED TWO CRACKS ACC KLM DFX 96-0165 ISSUE 4 APPR ACC TO FAA FORM 2110-3 AND UPS EO B747-5720-8543-Jul 26, 1996 · N675UP · Boeing 747123SDR UPS96420965Spar Web · crackedINSPECTION TYPE-C, RT WING FRONT SPAR FOUND DURING NDO INSPECTION OF SB 747-57A2266 CRACK IN FRONT SPAR WEB AT STIFFENER FS 655.75 FOURTH HOLE FROM UPPER SIDE 4MM. AFTER INSP ALSO FOUND CRACKS AT FIFTH AND SEVENTH HOLE 2MM, .05MM. REPAIRED FOURTH HOLE FROM UJul 23, 1996 · N675UP · Boeing 747123SDR 96FDEA01271Ctr Wing Spar · corrodedNR0702 AND 703, CORROSION CTR WING TANK, STA 866 SPAR AND UPPER CHORD CORRODED FROM LBL 50 TO RBL 50. *S/D* REMOVED AND REPLACED REAR SPAR UPPER CHORD PER 51-40-4 FIG 1 AND EA 7-5710-28808.Jul 19, 1996 · N181FE · Boeing 7272D4SDR DLL10961878Spar Cap · crackedDURING HMV, THE INTERMEDIATE SPAR UPPER CAP AT WS 1163 WAS FOUND IN NEED OF REPAIR. THE DAMAGE WAS REMOVED AND A NEW PART WAS SPLICED IN.Jul 11, 1996 · N727DA · Lkheed 10113851SDR 96ZZZX3778Carry-Through · crackedINSPECTION FOUND CRACKS IN CARRY-THROUGH STRUCTURE. AD 95-04-03 NOT VALID BY SERIAL NUMBER.Jul 11, 1996 · N8268T · Beech F33ASDR 96ZZZX3773Carry-Through · crackedINSPECTION FOUND CRACKS IN CARRY-THROUGH STRUCTURE. AD 95-04-03 NOT VALID BY SERIAL NUMBER.Jul 11, 1996 · N5544P · Beech F33ASDR 96ZZZX3761Carry Through · crackedINSPECTION FOUND CRACKS IN CARRY-THROUGH STRUCTURE. AD 95-04-03 NOT VALID BY SERIAL NUMBER.Jul 11, 1996 · N1570A · Beech F33ASDR 96ZZZX3760Carry Through · crackedINSPECTION FOUND CRACKS IN CARRY-THROUGH STRUCTURE. AD 9504-03 NOT VALID BY SERIAL NUMBER.Jul 11, 1996 · N1564A · Beech F33ASDR 96ZZZX3759Carry Through · crackedINSPECTION FOUND CRACKS IN CARRY-THROUGH STRUCTURE. AD 95-04-03 NOT VALID BY SERIAL NUMBER.Jul 11, 1996 · N1556A · Beech F33ASDR DHL9671567DSpar · corrodedAT D-CHECK, RIGHT WING HAS CORROSION ON REAR SPAR JUST FWD OF APU EXHAUST. REMOVED DAMAGED AREA, INSTALLED REPAIR PER SRM 57-10-6, 11 INCHES BY 5 INCHES.Jul 7, 1996 · N715DH · Boeing 727155CSDR DHL9671563DSpar · crackedAT D-CHECK, RIGHT WING UPPER SPAR SHOWS CRACK ON VERTICAL FLANGE OUTBD SIDE OF NR 13 SPOILER ACTUATOR MOUNT CASTING. CUT OUT DAMAGED SECTION PER S/B 57-145 , 23 INCHES BY 2 INCHES. INSTALLED REPAIR PER S/B 57-145, DRAWING 65C19647 AND AVITAS DRAWING 96PMSI1Jul 7, 1996 · N715DH · Boeing 727155CSDR 9615379983Spar · corrodedDURING H-CHECK, FOUND CORROSION ON THE LEFT WING FORWARD SPAR LOWER CAP FROM XFS 547 - 554. REPAIRED CAP (P/N 5919153-1) PER EA 99-110821.Jul 4, 1996 · N983US · Doug DC932SDR 96ZZZX4159Spar · corrodedREPORTING FINDINGS OF INSPECTION REQUIRED IN AD 94-18-04. EVIDENCE FOUND OF CORROSION BETWEEN PARTS OF REAR SPAR IN LEFT WING. SAME CONDITION FOUND IN RIGHT WING AS WELL AS A PORTION OF EXFOLIATION FOUND IN BOTTOM SPAR CAP, AFT SIDE, ABOUT A FOOT FROM THE OUJul 1, 1996 · Univar 415ESDR 96ZZZX3572Spar · corrodedINSPECTION REQUIRED IN AD 94-18-04. FOUND EVIDENCE OF CORROSION BETWEEN PARTS OF REAR SPAR IN LEFT WING. SAME CONDITION FOUND IN RIGHT WING AS WELL AS A PORTION OF EXFOLIATION FOUND IN BOTTOM SPAR CAP, AFT SIDE, ABOUT A FOOT FROM THE OUTBOARD END.Jul 1, 1996 · N94841 · Univar 415ESDR 9615339941Spar · corrodedDURING H-CHECK, FOUND CORROSION ON THE LEFT WING LOWER REAR SPAR CAP (XW 58 - XRS 91) AND SPAR CAP SPLICE T (XRS 112). REPAIRED CAP (P/N 5911305-503) AND T (P/N 5911357-1) PER EA 99-110801, 99-110805.Jul 1, 1996 · N3324L · Doug DC932SDR AALA960985Spar · corrodedTUL - CORROSION LOWER LEADING EDGE WING PANELS OUTBOARD NR 8 SLAT ACTUATOR. REMOVED CORROSION, NDT CHECK, INSTALL DOUBLER STRAP PER SRM 57-30-00, FIGURE NR 2. TST: 64,997 HOURS. CYCLES, 44,491. (X)Jun 29, 1996 · N720AA · Boeing 727227SDR AALA960981Spar · corrodedTUL - CORRODED AND BULGED AROUND RIVETS. REMOVED CORROSION AND INSTALLED DOUBLER PER ESO 11697. REF: E-58 NR 1771442, DATED 6-17-56. TST: 64,997 HOURS. CYCLES, 44,491. (X)Jun 29, 1996 · N720AA · Boeing 727227SDR UPS96820784Spar · crackedINSPECTION TYPE CS2, RT LOWER AUX SPAR IS CRACKED AT BOLT HOLE. REPLACED AUX SPAR PER TASK CARD NR 1057.Jun 28, 1996 · N750UP · Doug DC871FSDR DLL10961541Rear Spar · crackedREAR SPAR WEB CRACKED AT WS 0.00 BEGINNING AT THE LOWER END OF WEB AND EXTENDING UP THROUGH TWO ATTACHMENTS TO THE LOWER SPAR ANGLE FOR 2. THE REAR SPAR WEB IS M/F .150 7075-T6511 PLATE. REPAIRED PER ERA273915-14.Jun 25, 1996 · N729DA · Lkheed 10113851SDR 9615289941Chord · corrodedDURING H-CHECK, FOUND CORROSION ON THE FORWARD SPAR LOWER CAP, WS 58 - 76, LEFT SIDE. REPAIRED CAP (P/N 5911307-505) PER EA 99-110530.Jun 24, 1996 · N3324L · Doug DC932SDR UPS96820647Spar Cap · crackedINSPECTION TYPE: C. CRACKS IN RIGHT LOWER SPAR CAP IN HOLES 4, 5, 6, 7, AND 10 -XW 454. REAMED HOLE NR 10, ALODINED AND PRIMED IAW SRM 51-1-8, AND INSTALLED BUSHING IAW DWG J060232 HOLES 4, 5, 6, 7. REAMED HOLES, STRESS COINED HOLES IAW DPS 3.67-56 AND DACJun 20, 1996 · N851UP · Doug DC873FSDR UPS96220546Spar · corrodedINSPECTION TYPE SI, CORROSION R/W UPPER REAR SPAR CHORD AT WBL 86 JUST ABOVE NR 3 ENGINE FUEL SHUTOFF VALVE. REPAIRED UPPER REAR SPAR CHORD IAW SB 727-57-0145, SRM 57-10-6 AND BOEING DRAWING 65-C19647.Jun 20, 1996 · N929UP · Boeing 72722CSDR 96ZZZX3355Bolt · brokenRIGHT WING SPAR LOWER BOLT BROKEN CAUSED BY MOISTURE SETTLING AROUND NUT AND THREADS AND CORRODING BOLT. CORROSION EVIDENT AT BREAK THROUGH 99 PERCENT OF BOLT DIAMETER. SUBMITTER STATES RECURRING PROBLEM ON OLDER AIRCRAFT. OPERATOR KNOWS OF MULTIPLE LIKE FAJun 18, 1996 · N666HL · Piper PA34200TSDR 9614406612Spar · corrodedDURING P-CHECK, FOUND CORROSION ON THE RIGHT WING FORWARD SPAR UPPER CHORD FS 1517. REPAIRED CHORD (P/N 65B10849-2) PER EA 66-101949.Jun 16, 1996 · N612US · Boeing 747251BSDR MWEA96250Spar · corrosionDURING CERT INSP, LT WING INTERIOR AFT SPAR FOUND WITH MILD CORROSION ON REAR SPAR HORIZONTAL SURFACE AT STA XRS 69.000 AND XRS 91.000. REMOVED CORROSION IAW SRM 51-03-3, SHOT PEENED AFFECTED AREA OF SPAR, TREATED, PRIMED AND INSTALLED STRAP PER DAC TELEX SVCJun 14, 1996 · Doug DC932SDR TSAA9657042Spar Cap · corrodedDURING HEAVY MAINTENANCE VISIT, FOUND RIGHT WING FRONT SPAR LOWER CAP FORWARD LOWER SIDE. EXFOLIATION CORROSION AT FSS 280, 300, AND 416.8. REPAIRED PER ECO 2135. AIRCRAFT RETURNED TO SERVICE. (M)Jun 13, 1996 · N806AL · Boeing 7372S2CSDR 96FDEA01126Spar Chord · crackedNR 0490 AND 009. LEFT WING AFT UPPER SPAR CHORD VERTICAL LEG HAS CRACK BETWEEN NR 2 AND NR 3 SPOILERS. REMOVED DAMAGE FROM LEFT WING UPPER REAR SPAR STA 531 - 539. FABRICATED AND INSTALLED REPAIR PER FEDEX SRM 57-10-6, MM 27-61-0, MM 28-1-0.Jun 13, 1996 · N199FE · Boeing 727173CSDR UPS96820517Spar · corrosionINSPECTION TYPE CS2, HEAVY CORROSION ON HOLE CENTER WING UPPER INBOARD FRONT SPAR AT STA XFS64.76 RIB. REPAIRED PER UPS EO.Jun 11, 1996 · N705UP · Doug DC871FSDR AU960894Spar Cap · corroded(AUS) LH WING MAIN SPAR UPPER SPAR CAP CONTAINED SCATTERED PATCHES OF EXFOLIATION CORROSION IN AREA FROM OUTBOARD OF ENGINE NACELLE TO THE WING TIPJun 11, 1996 · Cessna 402CESSNASDR ABXA9600571Spar · corrodedDURING C-CHECK INSPECTION, FOUND CORROSION ON THE LEFT WING LOWER SPAR. REPAIRED IAW ABX REA D957-15400-MR.Jun 11, 1996 · N938AX · Doug DC931SDR ABXA9600570Spar · corrodedDURING C-CHECK INSPECTION, FOUND CORROSION ON THE LEFT WING UPPER SPAR. REPAIRED IAW ABX REA D957-15400-MR.Jun 11, 1996 · N938AX · Doug DC931SDR 9614009905Spar · crackedDURING H-CHECK, FOUND A .75 INCH CRACK IN THE RIGHT WING REAR SPAR AT THE NR 2 FLAP HINGE LOWER INBOARD FASTENER HOLE. REPAIRED SPAR PER EA 99-110507.Jun 7, 1996 · N955N · Doug DC931
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