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 AUS20030967Spar · corroded(AUS) LT UPPER AFT REAR SPAR WEB CONTAINED LIGHT EXFOLIATION CORROSIONIN AREA ADJACENT TO MAIN LANDING GEAR. FOUND DURING INVESTIGATION FOLLOWING CORROSION IN RT WING SPAR. SEE MDR 03/0900.Sep 17, 2003 · Socata TB10TOBAGOSDR MZZA0300004Spar · corrodedINSPECTION FOUND HEAVY INTERGRANULAR CORROSION AT THE LT WING NR 1 FORWARD PUMP BONDING STRAP (FRONT SPAR WEB). FRONT SPAR WEB WAS REPAIRED IAW ECRA. RESISTANCE CHECK WAS GOOD IAW MM. (K)Sep 10, 2003 · N14250 · Boeing 737823SDR QXEA200301123Spar · out of limitsFRONT SPAR 2 LEADING EDGE ATTACH FLANGE HOLES ARE OUT OF LIMITS. BEYOND .263" DIAMETER Y150.300. REPAIRED IAW Q400 RD 8/4-57-203, TASK 51-00-02-250-801 AND HORIZON AIR EA 6-57-173Sep 9, 2003 · N413QX · Bombdr DHC8401SDR 2003FA0000911Spar · crackedDURING MAINTENANCE OF THE AIRCRAFT IN WHICH THE RIGHT FUEL TANK WAS OPENED UP, A CRACK WAS FOUND IN THE AFT SPAR. THE CRACK EXTENDS FROM WS 33.0 TO 34.375 AND IS APPROX 1.375 INCHES LONG. THE CRACK IS LOCATED IN THE UPPER BEND RADIUS OF THE AFT SPAR.Sep 9, 2003 · N3517S · Cessna 172RSDR AUS20030901Spar · corroded(AUS) LT AND RT WING MAIN SPAR AFT LOWER WEBS CONTAINED EXFOLIATION CORROSION. CORROSION MAINLY LOCATED IN AREA ADJACENT TO MAIN LANDING GEAR.Sep 8, 2003 · Socata TB10TOBAGOSDR AUS20030900Spar · corroded(AUS) RT WING MAIN SPAR AFT LOWER WEB CONTAINED EXFOLIATION CORROSION. CORROSION WAS MAINLY LOCATED IN AREA ADJACENT TO MAIN LANDING GEAR LEG.Sep 8, 2003 · Socata TB10TOBAGOSDR CA030915006Spar · corroded(CAN) RT WING FORWARD UPPER SPAR PLATE HAS SEVERAL AREAS OF EXHALATION. PART REPLACED.Sep 5, 2003 · Cessna 172MSDR AUS20030913Spar Cap · corroded(AUS) RT WING UPPER SPAR CAP ANGLE CORRODED. ANGLE IS LOCATED IN FUEL TANK BAY.Sep 5, 2003 · Cessna 172NSDR AUS20030872Spar · corroded(AUS) LT WING VENT TANK SKIN ATTACHMENT FLANGES AND WEBS OF STIFFENERSNO9, NR 10 AND NR 11 CORRODED BEYOND LIMITS. LOWER SECTION OF REAR SPAR ALSO CORRODED.Aug 29, 2003 · Boeing 737377SDR AUS20030845Spar · cracked(AUS) LT LOWER WING FORWARD SPAR CRACKED.Aug 20, 2003 · Dhavxx DH82AROBRTSNSDR QXEA200301030Spar · gougedPDX- GOUGE IN RADIUS OF RIGHT FORWARD SPAR TOP FLANGE TO SKIN JOINT FROM YW318.0 TO YW327.0. REPARIED IAW DHC-8 SRM 51-00-06 AND RD 8-57-1675.Aug 20, 2003 · N347PH · Dhav DHC8202SDR QXEA200301029Spar · gougedGOUGE IN RADIUS OF RIGHT HAND FORWARD SPAR TOP FLANGE TO SKIN JOINT FROM YW286.5 TO YW297.5. REPAIRED IAW DHC-8 SRM 51-00-06 AND RD 8-57-1675.Aug 20, 2003 · N347PH · Dhav DHC8202SDR QXEA200301028Spar · gougedGOUGE ON RIGHT HAND WING FORWARD SPAR TOP FLANGE AT YW201.9. REPARIED IAW DHC-8 SRM 51-00-06 AND RD 8-57-1675.Aug 20, 2003 · N347PH · Dhav DHC8202SDR AUS20030844Spar · corroded(AUS) LT AND RT WING MAIN SPARS CONTAINED SEVERE EXFOLIATION CORROSION.Aug 19, 2003 · Socata TB10TOBAGOSDR DHL2003805527Frame · crackedRIGHT WING OTBD STUB WING FRAME ANGLE DOUBLER CRACKED 2.000 AT STA XW 454.000. REMOVED ANGLE DOUBLER IAW SRM 51-1-21 PG 1. FABRICATED ANGLE DOUBLER (7075-0.071) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED ANGLE DOUBLER IAW SRM 51-1-8B. PERFORMED HEAug 18, 2003 · N805DH · Doug DC873FSDR MALA030417Spar · crackedDURING C-CHECK IN CVG, RT WING FALSE SPAR CRACK BETWEEN RIB NR 5 AND 6. MAINTENANCE REPAIRED IAW BAE/FAX:BARA/AVR/6476/03-MK. A/C RELEASE DATE 9/2/03. REFER TO 409 NR 190372 FOR DETAIL.Aug 16, 2003 · N523XJ · Bac AVRO146RJ85ASDR MALA030416Spar · crackedDURING C-CHECK IN CVG, LT WING FALSE SPAR CRACKED BETWEEN RIBS NR 5 AND 6. MAINTENANCE REPAIRED IAW BAE FAX: BARA/AVR/6475/03-MK. A/C RELEASE DATE 9/2/03. REFER TO 409 NR 190364 FOR DETAIL.Aug 15, 2003 · N523XJ · Bac AVRO146RJ85ASDR 2003FA0000847Spar Cap · blisteredON INSPECTION, LARGE BLISTER WAS OBSERVED ON RIGHT WING, OB OF WING TANK FROM WING STA 95 TO STA 108. AREA OF BLISTER WAS APPROX 10 INCHES X 15 INCHES X 3 INCHES. SMALL BLISTER WAS ALSO OBSERVED IB OF FUEL TANK BETWEEN WING STA 55 TO 65. RIVETS WERE DRILLEDAug 14, 2003 · N9753J · Piper PA28180SDR EIA2003109Spar · corrodedLT WING STA 1440 EXFOLIATION CORROSION ON THE LOWER CHORD OF THE FWD SPAR, LEADING EDGE CAVITY. REPAIRED LT WING LEADING EDGE LOWER CHORD AT WS 1440 BY REMOVING CORROSION, NDT AREA FABRICATED AND INSTALLED REPAIR PER ECRA 477-57-096-2 REV A.Aug 8, 2003 · N477EV · Boeing 747SR46SDR DHL2003805591Frame · crackedLEFT WING CTR L/E FORMER CRACKED 0.500 AT STA XS 442.185. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLERS IAW SRM 57-2-0 PG 9-10 (2024-T3 0.032, 2024-T3 0.040). CLEANED, TREATED ANDAug 7, 2003 · N805DH · Doug DC873FSDR DHL2003805502Frame · crackedRT WING CTR L/E FORMER 0.250 CRACKED, STA XFS 291.500. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER (AL2024-T3 0.040) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED ANGLE DOUAug 7, 2003 · N805DH · Doug DC873FSDR DHL2003805508Frame · crackedRIGHT WING CTR L/E FRAME 1.000 CRACKED, STA XFS 429.000 (LWR SECTION). REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLERS (2024-T3 0.040) 92024-T3 0.050) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED ANDAug 3, 2003 · N805DH · Doug DC873FSDR DHL2003805509Frame · crackedRT WING CTR L/E FRAME 1.000 CRACKED, STA XFS 454.976. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER (2024-T3 0.042) (2024-T3 0.050) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51Aug 3, 2003 · N805DH · Doug DC873FSDR DHL2003805507Frame · crackedRT WING CTR L/E FRAME 0.250 CRACKED, STA XFS 347.750. REMOVED FASTENERS IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER (2024-T3 0.040) (2024-T3 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FAug 3, 2003 · N805DH · Doug DC873FSDR DHL2003805506Frame · crackedRT OUTER WING OTBOARD L/E LOWER PART SHOWS FRAME CRACKED (1.000) STA XFS 841.250. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER (2024-T3 AL0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIJul 31, 2003 · N805DH · Doug DC873FSDR DHL2003805540Frame · crackedLEFT OUTER WING OUTBD L/E FRAME CRACKED 0.500 AT STA XFS 835.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER (2024-T3 0.032). INSTALLED ANGLE DOUBLER WITH NEW FASTENERS IAW SRM 57-2-0 PG 9-10Jul 29, 2003 · N805DH · Doug DC873FSDR DHL2003805547Frame · crackedLEFT OUTER WING OUTBD L/E FRAME 0.500 CRACKED STA XFS 747.500. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP HOLE CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER (2024-T3 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INJul 28, 2003 · N805DH · Doug DC873FSDR DHL2003805538Frame · crackedLEFT OUTER WING OTBD L/E FRAME CRACKED 0.500 AT STA XFS 785.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP HOLE CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER (2024-T3 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. Jul 28, 2003 · N805DH · Doug DC873FSDR AUS20030835Spar · corroded(AUS) RT WING MAIN SPAR UPPER CAP CONTAINED CORROSION ON THE AFT FACE. RT WING LEADING EDGE INTERCOSTAL CONTAINED CORROSION ON THE LOWER FLANGE. FOLLOWING REMOVAL OF WINGS FOR REPAIR FURTHER CORROSION WAS FOUND ON THE TOP SURFACE OF THE LT AND RT MAIN SPAR UPPJul 24, 2003 · Socata TB10TOBAGOSDR AUS20030829Spar · corroded(AUS) RT WING VENT BOX CORRODED. NR 10 STIFFENER AFT FACE CORRODED IN AN AREA LOCATED BETWEEN WS563 & WS 578 OVER AN AREA APPROX 381MM BY 63.5MM. RT WING UPPER SKIN INNER SURFACE CORRODED BETWEEN WS 557 & 583 IN AN AREA BETWEEN STIFFENER NR 11 & WING REAR SPARJul 24, 2003 · Boeing 737376SDR AUS20030828Spar · corroded(AUS) LT WING VENT BOX NR 10 STIFFENER CORRODED ON AFT FACE BETWEEN STN 557 & 583. CORROSION WAS FOUND IN 4 AREAS. 3 AREAS WERE LOCATED BETWEEN 100MM & 177.8MM OUTBOARD OF WS 557 & WERE APPROX 25.4MM INDIAMETER. ONE AREA LOCATED BETWEEN 304.8MM & 381MM OUTBOARJul 24, 2003 · Boeing 737377SDR QXEA200300911Spar Cap · gougedPDX- RIGHT HAND WING FRONT SPAR UPPER CAP, UPPER SURFACE HAS MINOR GOUGES/SCRATCHES INTO BASE METAL BETWEEN STATIONS YW315 AND YW387. REPAIRED IAW DHC-8 RD 8-57-1675 AND 8-57-1119.Jul 24, 2003 · N345PH · Dhav DHC8202SDR QXEA200300910Spar Cap · scratchedPDX- ON LEFT HAND WING FRONT SPAR CAP FOR LEADING EDGE MOUNT, LOWER SPAR CAP HAS 12 AREAS WHERE PRIMER IS SCRATCHED FROM STATION YW214.0 TO YW326.0. REPAIRED IAW DHC-8 SRM 51-20-16 AND RD 8-57-1675.Jul 24, 2003 · N345PH · Dhav DHC8202SDR DHL2003805548Frame · crackedLEFT OUTER WING OUTBD L/E FORMER 0.500 CRACKED, STA XFS 753.750. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP HOLE CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER (2024-T3 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. Jul 23, 2003 · N805DH · Doug DC873FSDR AUS20030764Spar · cracked(AUS) CARRY THROUGH SPAR FORWARD AND AFT SPAR WEBS PN 00243001811 (FORWARD) AND PN 00243001813 (AFT) CRACKED IN LOWER RADIUS ON LT SIDE.Jul 23, 2003 · Beech 58SDR DL73S030680Spar · gougedRT WING / MLG AFT SUPPORT FITTING / WBL 157, TOOLING DAMAGE. THE MLG AFT SUPPORT FITTING ON THE RT WING SUFFERED TOOLING DAMAGE DURING REMOVAL OF FASTENERS FOR INSPECTION. THE BORE OF ONE OF THE FASTENERS WAS DAMAGED IN THE AFT FITTING, REAR SPAR UPPER CHORDJul 18, 2003 · N331DL · Boeing 737232SDR KQ72003F00000Spar · corrodedDURING C1 AND C2 CHECK, CPCP GENERAL VISUAL INSP OF WING REAR SPAR FOR CORROSION, DISCOVERED SEVERAL AREAS OF CORROSION AND CRACKING. PERFORMED A NDT INSP HFEC AND CONFIRMED DAMAGE FOUND BY VISUAL INSP. REMOVED WING FUEL PANELS, INSPECTED INTERIOR OF FUEL CEJul 13, 2003 · N727WF · Boeing 72723SDR QXEA200300825Spar · chafedPDX - FLANGES ON FORWARD SPAR UNDER PANELS 261CT, 261FT, 261HT AND 261LT ARE CHAFED APPROXIMATELY YW58.00 RIGHT TO YW58.00 LEFT. REPAIRED IAW RD 8/4-53-451.Jul 11, 2003 · N410QX · Bombdr DHC8401SDR AUS20030691Spar · damaged(AUS) LT WING SPAR DAMAGED. LOOSE RIBS FOUND DURING PERIODIC INSPECTION WHEN SECTION OF FABRIC WAS REMVD TO CARRY OUT RIBREPAIRS REMOVED FABRIC REVEALED NONAPPROVED REPAIR TO REAR SPAR TOP FACE & REPAIRED AREA COVERED BY PAINT. FURTHER FABRIC REMOVAL FOUND SEVJul 3, 2003 · Dhavxx DH82AROBRTSNSDR AUS20030663Spar · corroded(AUS) RT WING AFT SPAR LOWER SECTION CONTAINED LEVEL 2 CORROSION IN AREAOF RH WING VENT TANK LOCATED BETWEEN WS557 AND WS583. FOUND DURING INSPECTION IAW A-B73-5791-51.Jul 3, 2003 · Boeing 73733ASDR AUS20030677Spar · cracked(AUS) LT WING MAIN SPAR WEB CRACKED. CRACK LOCATED AT THE TOP OF THE MAIN LANDING GEAR LEG ATTACHMENT AREA. CRACK LENGTH 100MM (4IN).Jul 1, 2003 · Piper PA28140SDR 2003FA0000852Spar · crackedDURING REPAIRS TO BOTH WINGS FOR DAMAGED RIBS AT WING STA B9.24. FOUND THE RT MAIN SPAR CRACKED AT WEB TO LOWER SPAR CAP JUNCTION UNDER THE MAIN GEAR TRUSS BRACKET(PN95642-5P). THE HORIZONTAL CRACK IS APPROX 1.5 INCH LONG, ABOUT .25 INCH OF THE CRACK IS PASTJul 1, 2003 · N75153 · Piper PA28R200SDR AUS20030651Angle · corroded(AUS) LT WING FRONT SPAR CAP ANGLE CORRODED.Jun 30, 2003 · Cessna 182FSDR AUS20030650Plate · corroded(AUS) LT WING FRONT SPAR CAP DOUBLER PLATE CONTAINED INTERGRANULAR CORROSION.Jun 30, 2003 · Cessna 182FSDR AUS20030799Spar · cracked(AUS) LT WING REAR SPAR CONTAINED A NUMBER OF LENGTH WISE CRACKS. FOUND DURING INSPECTION IAW AD/CHA/23.Jun 10, 2003 · Bbavia 8KCABSDR DHL2003604585Frame · crackedLT. WING CENTER L/E FORMER CRACKED 3.000 AT STA. XOLDI 6.225. STOP DRILLED CRACK AT STA. XOLDI 6.225 AND FABRICATED REINFORCEMENT ANGLE (301 0.250H 0.032) IAW SRM 57-2-0 PG.9-10. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED REINFORCEMENT ANGLE Jun 9, 2003 · N604AL · Doug DC873FSDR AUS20030542Spar · cracked(AUS) WING CARRY THROUGH ASSEMBLY PNO 002-430013-9 CRACKED ON LOWER FACES OF FORWARD WEB PNO 002-430018-1. CRACKS ARE BETWEEN HUCKBOLTS AND JOIN THREE HUCK BOLTS ON EACH SIDE. CRACKS ALSO FOUND IN WEB RADIUS ON BOTH SIDES. CRACKING IS IAW MFG SB2360 FIGURE 1. May 29, 2003 · Beech A36SDR NACA20030088Spar · corrodedDISCREPANCY: REAR SPAR CORRODED L351 TO 399 UPPER AND LOWER CAPS AND WEB. SPLICED IN NEW SECTION OF AFT SPAR WEB FROM LT WING STA. 361 TO STA. 393 IAW O/H MANUAL 13-10 FIG. 13-4.May 29, 2003 · N2907F · Doug DC6SDR 2003FA0000691Spar · crackedCRACK UNDER PLYWOOD PLATE, BOTH CRACKS FLOW THE GRAIN.May 27, 2003 · N6346N · Bbavia 7ECASDR DHL2003604560Frame · crackedRT WING CENTER L/E FRAME CRACKED 1.000, XFS.366.500 (UPPER INNER). STOP DRILLED CRACK AT XFS.366.500 AND FABRICATED ANGLE DOUBLER (2024-T3 0.040) IAW SRM 57-2-0 PG.9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBMay 20, 2003 · N604AL · Doug DC873F
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