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 ZZDA5327897Spar · crackedDURING C-CHECK AT AERO CORP, ACCOMPLISHED AD 90-06-02, REPLACED THE LT WING CRACKED FRONT SPAR UPPER CHORD BETWEEN FS 97 TO FS 225 IAW SB 737-57A1081 (R10) PART III OR IV OF ACCOMPLISHMENT INSTRUCTIONS. REMOVED CRACKED LT UPPER WING SPAR CHORD FROM STA 90 - SAug 15, 1997 · N460AT · Boeing 737214SDR DLL10971623Spar Cap · crackedTWO CENTER WING INTERMEDIATE SPAR CAPS WERE FOUND TO HAVE CRACKS IN THE TYPICAL MANNER DEPICTED IN L1011 SRM 57-11-00, FIGURE 809 AND LAC S/B 093-57-087. THE CRACKS IN THE SUBJECT SPAR CAPS ARE BEYOND THE LIMITS PRESENTED IN THE NOTED REFERENCES AND REQUIRE RAug 15, 1997 · N714DA · Lkheed 10113851SDR CALA9701309Spar · corrodedINSPECTION FOUND RT WING LOWER LEADING EDGE SPAR CORRODED AT STA 429.44 AND 484.51. THE AREAS WERE REPAIRED IAW ECRA 5710-01829.Aug 9, 1997 · N68043 · Doug DC1010SDR 97ZZZX3737Spar · corrosionCOMPLIED WITH AD 96-24-17 IAW LUSCOMBE RECOMMENDATION NR 2. INSTALLED O.L.A.H.F. KIT NR 2. NO DAMAGING CORROSION WAS FOUND. SUBMITTER RECOMMENDED SPRAYING WING INTERIOR WITH CF 50 CORROSION PROOFING.Aug 9, 1997 · N2066K · Luscom 8ASDR RRXA97232Spar · crackedDURING ACCOMPLISHMENT OF DAC SB 57-88, ON LEFT WING, HOLES 1 THUR 5 AND A, B AND C HAD CRACKS INDICATED. HOLES WERE ABOVE SIZE ALLOWED IAW SB 57-88. *S/D* IDENTIFIED CRACKS AND REAMED OUT DAMAGE IAW FAA APPROVED DER TIMCO REO-03479. FABRICATED AND INSTALLEAug 8, 1997 · N8079U · Doug DC871FSDR P5CA9701525Spar Chord · corrodedLEVEL 2 CORROSION RIGHT WING FRONT SPAR CAVITY AT OLES 1385 TO 1395. REPAIRED PER BOEING SRM 57-30-03 FIG 9 AND HAECO RS R-57-21-33503.Aug 7, 1997 · N853FT · Boeing 747122SDR 97ZZZX3923Rib · separationINVESTIGATION FOR RIB SEPARATION FROM WING SPAR FOUND THE DESIGN OF LANDING GEARINSTALLATION TO BE A CAUSAL FACTOR. THIS INSTALLATION (EXTENDING FORWARD AND ATTACHED TO MAIN SPAR) INDUCES A TWISTING MOTION ON THE MAIN SPAR DURING LANDING. A HARD 3-POINT OR OAug 7, 1997 · N2FOR · Amtr EMERAUDSUPERSDR 97ZZZX3934Web · crackedINSPECTION FOUND FORWARD SPAR CARRY-THROUGH CRACKED. A CRACK OF 1.3 INCHES IN LENGTH WAS DISCOVERED IN MID-SECTION OF LOWER BEND RADIUS IN A VERTICAL DIRECTION FOLLOWING THE BEND. THE CRACK SEEMS TO OCCUR IN THE AREA OF THE FORWARD SUPPORT (RT SIDE). POSSIBAug 6, 1997 · N1568P · Beech F33ASDR CALA9701301Spar · gougedINSPECTION FOUND A GOUGE IN THE NR 2 ENGINE FORWARD SPAR. THE GOUGE WAS BLENDED OUT. REPAIR STRAP AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 51-21-01 AND ECRA 5410-01451.Aug 5, 1997 · N68043 · Doug DC1010SDR MWEA97704Spar Tang · corrodedDURING D-CHK, FOUND CORROSION RT WING AFT SPAR UP TANG. MTC REPAIRED IAW DAC DWG 5911358 AND SRM 51-30-5.Aug 4, 1997 · N216ME · Doug DC932SDR 97ZZZX3975Spar · brokenDURING TOW OPERATION, WING CENTER SECTION SPAR FAILED NEAR RIGHT FUSELAGE ATTACH POINT. WOOD DETERIORATION DUE TO AGE AND WATER ACCUMULATION POSSIBLE. HARDWARE FOUND RUSTY. AIRCRAFT WAS BEING OPERATED OVER DESIGN GROSS WEIGHT WITH AN AFT C.G. CONDITIONS OFAug 2, 1997 · N5516V · Amtr BG12ASDR 97ZZZX4202Spar Capstrip · separatedAS REQUIRED, CONDUCTED THE WING INSPECTION ON LUSCOMBE METAL WING IAW APPENDIX TO FAA AD96-24-17. FOUND NO INTERGRANULAR CORROSION. DID FIND SOME LOOSE INSULATION AND URINE STAINS WHICH WAS EASILY REMOVED WITH COAT HANGERS AND BY SPRAYING OUT THE WING WITH AAug 1, 1997 · Luscom 8ASDR CALA9701302Spar · corrodedINSPECTION FOUND LEFT WING SPAR CORRODED AT STA XORS 264 TO XORS 272. THE CORROSION WAS REMOVED IAW SRM 51-21-01. A REPAIR WAS INSTALLED IAW SRM 57-20-00 AND ECRA 5311-01033.Jul 31, 1997 · N68043 · Doug DC1010SDR 97ZZZX3862Spar · corrodedRIGHT REAR SPAR, WS 40, BENT AND CRACKED. LOG RESEARCH SHOWS INCIDENT 2 YEARS PRIOR. WING CORROSION WAS VISABLE AT A GLANCE.Jul 31, 1997 · N45434 · Cessna 150MSDR 9717306623Spar Web · corrosionDURING PREFLIGHT CHECK, FOUND FUEL LEAK OUTBOARD OF NR 4 ENGINE. FURTHER INSPECTION REVEALED CORROSION ON FORWARD SPAR WEB AT WS 1345. REPAIRED PER EA 66-150487 AND 66-151496.Jul 30, 1997 · N623US · Boeing 747251BSDR 9717576642Spar Web · corrodedDURING M-CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON LEFT WING FRONT SPAR WEB FS 1543 TO 1572. REPAIRED PER EA 66-151128.Jul 29, 1997 · N642NW · Boeing 747212BSDR ABXA9701324Rear Spar · corrosionCORROSION ON RT WING REAR SPAR LOWER CAP VERTICAL FLANGE AT STA XRS 575 TO XRS 579. REPAIRED PER REA D857-16814-MR.Jul 28, 1997 · N849AX · Doug DC861SDR ABXA9701322Front Spar · elongated holesELONGATED HOLES (3 PLACES) ON LT WING LOWER FRONT SPAR CAP FLANGE AT STA XFS 301.62, XFS 304.32 AND XFS 306.62. REPAIRED PER REA D857-16775-DE, REV A. REF: (1) DWG DC8C 5740-001, (2) PSE 57-08-011.Jul 28, 1997 · N849AX · Doug DC861SDR ABXA9701320Front Spar · crackedCRACK DETECTED BY NDT IN FASTENER HOLE ON LT WING FRONT SPAR LOWER CAP FWD TANG AT STA XFS 483. REPAIRED PER REA D857-16769-MR. REF: (1) DWG DC8C-5740-002, (2) PSE 57-08-021.Jul 28, 1997 · N849AX · Doug DC861SDR ABXA9701319Front Spar · crackCRACK DETECTED BY NDT IN FASTENER HOLE ON RT WING FRONT SPAR LOWER CAP FWD TANG AT STA XFS 483. REPAIRED PER REA D857-16768-MR. REF: (1) DWG DC8C 5740-002, (2) PSE 57-08-022.Jul 28, 1997 · N849AX · Doug DC861SDR ABXA9701318Front Spar · crackedCRACK DETECTED BY NDT IN NR 4 FASTENER HOLE ON RT WING FRONT SPAR LOWER CAP FWD TANG STA XFS 206. REPAIRED PER REA D857-16767-DE, REV A REF: (1) AD 84-13-02, (2) SB 57-89, (3) PSE 57-08-040.Jul 28, 1997 · N849AX · Doug DC861SDR ABXA9701317Front Spar · corrodedDEEP CORROSION ON LT WING LOWER FRONT SPAR FWD TANG OUTBOARD OF PYLON NR 1 BETWEEN STA XFS 568 AND XFS 574. REPAIRED PER REA D857-16764-MR REF: PSE 57-08-021.Jul 28, 1997 · N849AX · Doug DC861SDR ABXA9701315Front Spar · crackedHAIRLINE CRACKS (3 PLACES) DETECTED BY NDT IN FASTENER HOLES ON FRONT SPAR LOWER CAP FWD TANK AT PYLON NR 2. REPAIRED PER REA D857-16763-DE, REV A REF (1) AD 84-13-02, (2) SB 57-89, (3) PSE 57-08-039.Jul 28, 1997 · N849AX · Doug DC861SDR MWEA97677Spar · corrosionDURING D-CHK, FOUND CORROSION LT WING AFT SPAR UP TANG. MTC REPAIRED IAW DAC DRWG 5911358 AND TELEX SVC-MSP-0300/GLP 10 MAR 97.Jul 23, 1997 · N216ME · Doug DC932SDR 97ZZZX3472Spar · corrodedDURING AN ANNUAL INSPECTION OF THIS AIRCRAFT, A CONSIDERABLE AMOUNT OF CORROSION OF THE RIGHT WING SPAR WAS FOUND WITH SOME FORM OF DELAMINATION. THE PRIMARY CORROSION WAS FOUND ON THE RIGHT WING SPAR NEAR THE RIB ONTO WHICH THE LANDING GEAR IS ATTACHED.Jul 21, 1997 · N2527E · Socata TB20TRINIDADSDR UPS97824463Spar Cap · crackedINSPECTION TYPE-C/CK, CENTER WING LOWER REAR SPAR CAP CRACKED BETWEEN 2 FASTENRS IN AFT TANG 32 RT OF KEEL BEAM. PERFORMED HFEC INSP IAW MIL-S-271F AND FOUND CRACK. FABRICATED REPAIR ANGLE FROM 7075-T6511 PO 111040, IAW REO 03412 AND DC8 SRM 51-9- 0. CUT OUJul 16, 1997 · N807UP · Doug DC873FSDR UPS97824276Spar Cap · crackedINSPECTION TYPE:C/CK CENTER WING LOWER REAR SPAR CAP CRACKED, BETWEEN 2 FASTENERS IN AFT TANG, 32 IN RIGHT OF KEEL BEAM. PERFORMED HFEC INSPECTION IAW MIL S 271F AND FOUND CRACK BETWEEN 2 FASTENERS HOLES, FABRICATED REPAIR PARTS IAW REO 03412 AND DAC DWG 9 8Jul 16, 1997 · N807UP · Doug DC873FSDR P5CA9701342Spar Cap · corrodedLEVEL 1 CORROSION, WING FRONT SPAR UPPER CAP HAS LIGHT SURFACE CORROSION AT NAC ST 305 RWBL 472-473. REMOVED CORROSION IAW BOEING SRM 51-10-01 NON ROUTINE CARD S/N 7059.Jul 16, 1997 · N854FT · Boeing 747122SDR DL72W971452Spar Cap · damagedTHE SUBJECT AIRCRAFT EXPERIENCED A COLLAPSE OF THE RT MAIN LANDING GEAR DURING LANDING ROLLOUT. THIS RESULTED IN DAMAGE TO THE RT WING FRONT SPAR LOWER CAP ON THE OUTBOARD END. THE EXTENT OF THE DAMAGE REQUIRED THAT THE LOWER CAP TO BE CUT AT APPROX FS 770 AJul 15, 1997 · N2809W · Boeing 727247SDR DHL9770392DVertical Flange · corrodedAT D-CHECK, WING CENTER SECTION AFT LOWER SPAR HAS CORROSION AND CRACK FROM TOP VERTICAL FLANGE AND POPPED FASTENERS LBL 4 FS 870. REMOVED PREVIOUS WEB REPAIR. REMOVED CORROSION, OUT OF LIMITS, INSTALLED REPAIR PER SRM 51-40-4, 4 BY 16.Jul 14, 1997 · N703DH · Boeing 72730CSDR CKSA97347Spar · corrodedDURING C1-12 CHECK INSPECTION FOUND LEVEL 2 CORROSION: EXFOLIATION CORROSION ON FRONT SPAR LWR CHORD AT WS 1390. REPAIRED LOWER FWD CHORD IAW AIA/E/2578 DWG. REPAIRED LOWER FWD SKIN IAW SRM 57-30-03 FIG 9, (7075-T6). C-CHECK WORK CARD NUMBER 7CI6112. NON-Jul 11, 1997 · N708CK · Boeing 747269BSDR DLL13971382Spar Cap · crackTHE CENTER WING INTERMEDIATE SPAR UPPER CAP LOCATED AT STA 1163 WAS FOUND TO HAVE A CRACK ON THE RT OUTBOARD SIDE. THE CRACK IS TYPICAL OF THAT DESCRIBED IN S/B 093-57-087 BUT IS BEYOND THE ALLOWABLE CRACK LIMITS. THE DAMAGE WAS REPAIRED BY CUTTING AWAY THE Jul 10, 1997 · N783DL · Lkheed 10113851SDR 97FDEA00417Spar Chord · corrodedCORROSION (C57-174-01) BS 870 REAR SPAR UPPER CHORD, RBL 30 TO 50, LBL 20 TO 40, WL 178. *S/D* BLENDED REMOVED CORROSION ON BS 870 REAR SPAR UPPER CHORD FOUND TO BE OUT OF LIMITS PER FED-EX 727 SRM 53-10-1. REMOVED AND REPLACED CHORD PER FED-EX EA 7-5710-36Jul 9, 1997 · N143FE · Boeing 72721CSDR UPS97223710Rear Spar · corrodedINSPECTION TYPE:SI CORROSION (C57-174-01.01-01) ON WING CENTER SECTION UPPER REAR SPAR CHORD RBL 25 TO 45 BETWEEN HORIZONTAL FLANGE AND UPPER SKIN. REWORK OUT OF LIMITS IAW SRM 57-50-1. REMOVED AND REPLACED UPPER REAR SPAR CHORD IAW TRAMCO/BFG EWO 97-2283 UPJul 8, 1997 · N916UP · Boeing 727172CSDR UPS97223712Spar Web · corrodedINSPECTION TYPE:SI, CORROSION (C57-571-01.05-02) ON INSIDE SURFACE OF L/E FUEL CELL CUTOUT RT SIDE. REMOVED CORROSION AND REPAIRED FUEL CELL CUTOUT ON THE RT SPAR WEB IAW TRAMCO/BFG EWO 97-2286 UPS FILE NR 727-57-1864.Jul 7, 1997 · N916UP · Boeing 727172CSDR DLL13971345Spar · crackedTHE CENTER WING INTERMEDIATE SPAR UPPER CAP LOCATED AT STA 1103 WAS FOUND TO HAVE A 2 INCH CRACK ON THE RT O/B SIDE. THE CRACK WAS TYPICAL OF THOSE DESCRIBED IN S/B 093-57-087, BUT IS BEYOND THE ALLOWABLE LIMITS. THIS ER/A REPAIRS THE CRACKED UPPER CAP BY CUJul 4, 1997 · N786DL · Lkheed 10113851SDR DL72S971344Spar Web · crackedTHE WING CENTER SECTION REAR SPAR WEB IS CRACKED AT RBL 20.5. THE CRACK IS 2.625 LONG IN A CHEM-MILL RADIUS JUST BELOW THE SPAR UPPER CHORD. INSTALLED DOUBLER PER FAA/DER FORM 8110-3, DER DESIGNATION SO-775, DATED 7-3-97.Jul 3, 1997 · N528DA · Boeing 727232SDR 9713329938Spar Web · corrodedDURING H CHECK, FOUND CORROSION ON SPAR WEB AT XCW 21.0. REPAIRED PER EA 99-113317.Jul 3, 1997 · N1798U · Doug DC931SDR QXEA9700489Spar · scratchedRIGHT WING FRONT SPAR FROM APPROX YW 288.0 TO APPROX YW 243.00 HAS A DEEP SCRATCH APPROX .001 TO .003 DEEP. REPAIRED FRONT SPAR PER EA 9-57-249.Jun 30, 1997 · N812PH · Dhav DHC8102SDR MWEA97597Spar · corrodedDURING D-CHK, FOUND STA XRS250 TO XRS477 RT WING LWR FWD SPAR BLENDED BEYOND LIMITS. MAINT REPAIRED IAW AC TELEX SVC-ORD-0129/KJL.Jun 30, 1997 · N216ME · Doug DC932SDR DLL10971334Spar Cap · crackedTHE CENTER WING INTERMEDIATE SPAR UPPER CAP LOCATED AT STA 1103 WAS FOUND TO HAVE A CRACK 2.3437 ON THE RT OUTBOARD SIDE. THE CRACK IS TYPICAL OF THOSE DESCRIBED IN S/B 093-57-087, BUT IS BEYOND THE ALLOWABLE LIMITS. DURING THE INSTALLATION OF THE REPAIR, TWJun 30, 1997 · N730DA · Lkheed 10113851SDR 97FDEA00434Spar Chord · corrodedNR 0145 002 CORROSION (C53-132-02-1/2) ON 870 UPPER CENTER WING SPAR CHORD, VERTICAL FLANGE, RBL 16 TO RBL 24. REPLACED BS 870 UPPER CHORD PER BCE DRAWING 65C2153. REPAIRED CORROSION ON UPPER SKIN OF CENTER FUEL TANK BS 870 TO BS 843, RBL 70.5 TO RBL 37 PER Jun 30, 1997 · N128FE · Boeing 72725CSDR 97ZZZX3331Spar · corroded2.5 INCH BY 2.5 INCH AREA OF INTERGRANULAR CORROSION ON WING SPAR FOUND WHILE INSTALLING DLAHF S.R. NR 2 PRIOR TO ISSUANCE OF AD 96-24-17. AD 96-24-17 ADEQUATELY DESCRIBED PROBLEM AND SOLUTION. SPAR REPLACED 6/97.Jun 28, 1997 · N71599 · Luscom 8ASDR AU970738Spar Cap · cracked(AUS) RH WING LOWER SPAR CAP CRACKED FROM BOLT HOLE - CRACK LENGTH 3.048MM (0.120IN) - FOUND DURING MAGNETIC PARTICLE INSPECTIONJun 27, 1997 · Ayres S2RT65SDR MWEA97570Spar · corrosionDURING D-CHECK, FOUND CORROSION ON RIGHT WING AFT SPAR JUST OUTBOARD OF RIGHT MLG TRUNNION. MTC REMOVED AND REPLACED AFT SPAR UPPER CAP SECTION IAW DOUGLAS DRAWING NUMBER J060165.Jun 25, 1997 · N216ME · Doug DC932SDR DHL97803005Spar Cap · crackedRIGHT WING TRAILING EDGE REAR UPPER SPAR CAP XR 238 HAS CRACK 6 LONG. REPAIRED UPPER SPAR CAP AT XRS = 217 AND XRS= 268 PER DAC ENGINEERING ROD SKETCH 8-97-02-003.Jun 24, 1997 · N803DH · Doug DC873FSDR MWEA97562Spar · crackedDURING C-CHECK, STA 718 TRAP PAN ATTACH FIT RT WING AFT SPAR CRACKED/CORRODED. MAINT REMOVED AND REPLACED IAW SRM 57-01 PG 1.Jun 22, 1997 · N302ME · Doug DC932SDR AU970695Web · cracked(AUS) LH WING INBOARD WEB CRACKED - DUPLICATE OF MDR 97/0667Jun 17, 1997 · Ayres S2RT34NORMALSDR AU970667Web · cracked(AUS) LH WING INBOARD WEB CRACKEDJun 17, 1997 · Ayres S2RT34NORMALSDR UPS97823671Rib · crackedINSPECTION TYPE:D, L/WING L/E RIB CRACKED ON UPPER ARM STA XFS 828. REPAIRED IAW SRM 57-3-3 AND 57-2-0.Jun 15, 1997 · N851UP · Doug DC873F
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