JASC 5720

Service difficulty reports · 13,638

Reports filed under 5720 · Wing Miscellaneous Structure, 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 = '5720'
  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 EIA2000241Fastener · shearedC1-CHECK, NR 1 NACELLE U/W DIAGONAL BRACE FITTING, 3RD MOST AFT FASTENER ON OUTBOARD ROW FOUND SHEARED. DIAGONAL BRACE FITTING AFT FASTENER REPLACED PER EO57-747-1594-00. (M)Sep 3, 2000 · N480EV · Boeing 747121SDR USAA001524Fitting · crackedPIT - FOUND SUPPORT CRACKED 1.25 INCHES, LEFT WING, LEFT INBOARD GROUND SPOILER PANEL SUPPORT FITTING. INSTALLED TEMPORARY REPAIR PER EO 5788M381 REV D REPAIR 3L. (M)Sep 3, 2000 · N812US · Doug DC981SDR CALA0001375Structure · crackedINSPECTION FOUND A 1 INCH CRACK IN RT WING LEADING EDGE I/B SUPPORT. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-10-4, AND 51-10-3.Sep 3, 2000 · N15841 · Doug DC982SDR AU000857Fitting · corroded(AUS) SPLICE FITTING LOCATED BETWEEN STN 870 FORGING AND HORIZONTAL BEAM LOCATED IN LT WHEEL WELL CORRODED. FOUND DURING CORROSIONINSPECTION.Sep 1, 2000 · Boeing 72777CSDR AU000856Web · corroded(AUS) UPPER WEB LOCATED IN THE LT UPPER WHEEL WELL AT STN 870 BETWEEN WBL 0 AND WBL 24.75 CORRODED. FOUND DURING CORROSION INSPECTION.Sep 1, 2000 · Boeing 72777CSDR UPS00833788Angle · crackedINSPECTION TYPE:C123, LEFT WING L/E VERTICAL ANGLE IS CRACKED AT XS250. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 9753297, AND SRM 51-1-20D.Sep 1, 2000 · N729UP · Doug DC871FSDR UPS00833725Angle · crackedINSPECTION TYPE:C123, LEFT WING CENTER L/E VERTICAL ATTACH ANGLE IS CRACKED AT XS 520. REMOVED, FABRICATED, AND REPLACED ANGLE IAW DWG 9753297, AND SRM 51-1-20D, 51-1-21.Sep 1, 2000 · N729UP · Doug DC871FSDR COMA0010326Angle · crackedDURING A 1C INSPECTION TASK 193-01Z, THE WING TO FUSELAGE FAIRING (193) LOWER ATTACH ANGLE WAS FOUND TO BE CRACKED. THE ANGLE WAS REPLACED WITH A SERVICEABLE ANGLE IAW AERODESIGN REPORT 1226-9.Aug 31, 2000 · N268CA · Emb EMB120RTSDR COMA0010325Angle · crackedDURING A 1C INSPECTION TASK 194-01Z, THE WING TO FUSELAGE FAIRING (194) LOWER ATTACH ANGLE WAS FOUND TO BE CRACKED. THE ANGLE WAS REPLACED WITH A SERVICEABLE ANGLE IAW AERODESIGN REPORT 1226-9.Aug 31, 2000 · N268CA · Emb EMB120RTSDR COMA0010324Angle · crackedDURING A 1C INSPECTION TASK 194-01Z, THE WING TO FUSELAGE FAIRING (194) LOWER ATTCH ANGLE WAS FOUND TO BE CRACKED. THE ANGLE WAS REPLACED WITH A SERVICEABLE ANGLE IAW AERODESIGN REPORT 1226-9.Aug 31, 2000 · N268CA · Emb EMB120RTSDR RRXA002990Fastener · damagedDURING A MAINTENANCE VISIT FOUND A PARTIAL HI-LOK DRILLED AT RT LWR WING I/B NR 4 PYLON, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Aug 29, 2000 · N811AL · Doug DC871SDR RRXA003001Doubler · crackedDURING A MAINTENANCE VISIT FOUND REPAIR DOUBLER INTERFERING WITH NEW SPLICE DOUBLER AT STA XFS 576, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, ALODINED AND PRIMED AREA IAAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED Aug 27, 2000 · N997GE · Doug DC871FSDR UPS00434119Flange · crackedINSPECTION TYPE:C, RT WING UPPER FLANGE CRACKED ON L/E RIB AT OLES 1453. REPAIR CARRIED OUT IAW SRM 57-20-03.Aug 25, 2000 · N691UP · Boeing 747121SDR 00FDEA00593Web · crackedDURING ROUTINE INSP, 4 CRACKS WERE FOUND IN RT WING LEAD EDGE WEB JUST O/B OF BOTTLE BOLT. STOP DRILLED CRACKS, FAB DOUBLERS AND INSTALLED REPAIR PER IAW SRM 51-40-2.Aug 24, 2000 · N499FE · Boeing 727232SDR 00FDEA00591Angle · crackedDURING ROUTINE INSP, THE ANGLE AT RIGHT WING LEAD EDGE WEB JUST O/B OF THE BOTTLE BOLT, FOUND CRACKED. REMOVED AND REPLACED ANGLE PER IAW SRM 51-30-2.Aug 24, 2000 · N499FE · Boeing 727232SDR TWAA0104905Angle · crackedDURING OP 15 MAINTENANCE CHECK ON RIGHT WING LEADING EDGE THE WING LEADING EDGE ANGLE AFT OF DOUBLER OUTBOARD OF LOWER VORTILION, WAS CRACKED. REPLACED ANGLE AND INSTALLED FASTENERS.Aug 22, 2000 · N996Z · Doug DC932SDR QXEA0002405Structure · damagedPDX- RIGHT HAND WING LOWER STRIP JOINT IS DAMAGED. REPAIRED IAW HORIZON AIR EA 4-57-449.Aug 19, 2000 · N479AU · Fokker F28MK4000SDR UPS00233637Angle · corrodedINSPECTION TYPE:C, CRACK ON ANGLE BETWEEN SKIN AND RIB IN RIGHT WING L/E CAVITY AT O/B END OF NR 6 L/E FLAP. REPLACED ANGLE AND INSTALLED FASTENERS IAW SRM 51-30-02 AND BOLTS IAW OHM 20-50-01.Aug 17, 2000 · N925UP · Boeing 72731CSDR RRXA002865Clip · crackedDURING A MAINTENANCE VISIT FOUND CRACKED CAN'T LWR. CLIPS FOR STRINGERS 60-64 AT TOP OF RT WING ACCESS HOLE 505A AT STA XW 508, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-Aug 15, 2000 · N811AL · Doug DC871SDR AT0000396Fitting · corrodedFOUND RIGHT WING AT XRS 160 BUTE DOOR HINGE FITTING CORRODED. REMOVED CORROSION AND INSTALLED REPAIR IAW DC9 SRM 53-01 FIGURE 1.Aug 15, 2000 · N830AT · Doug DC932SDR DL72W001707Angle · crackedFOUND ON MV4 CK, 1 INCH CRACK IN NR 11 SPOILER ACTUATOR FITTING I/B ATTACH ANGLE AT LOWER BOLT. REPLACED ANGLE PER MM 57-42-0.Aug 14, 2000 · N297WA · Boeing 727247SDR 20000828SH032Bracket · crackedBRACKET CRACKED, RIGHT. SIMILAR PROBLEM LEFT TIP ON ANOTHER AIRCRAFT. (X)Aug 14, 2000 · N4FE · Lear 45LEARSDR 20000828SH001Bracket · crackedBRACKET CRACKED LEFT TIP. SAME OPERATOR REPORTED RIGHT BRACKET CRACKED ON OTHER AIRCRAFT. (X)Aug 14, 2000 · N45FE · Lear 45LEARSDR EIA2000036Bracket · brokenFRA - LEFT SIDE WING OVERHEAT LIGHT CAME ON DURING CLIMB-OUT AT FL 240. FOUND DUCT SEAL AT LE MID SECTION BLOWN. REPLACED, REALIGNED AND RETORQUED DUCT ASSY AND SUPPORT MOUNTS. DURING TROUBLESHOOTING FOUND SUPPORT BRACKETS BROKEN. FABRICATED BRACKETS PER EAug 12, 2000 · N481EV · Boeing 747132SDR DHL200080501CAngle · crackedAT C-CHECK, RT WING T/E ANGLE CRACKED 2 INCHES AT XW 5.000. PERFORMED STOP DRILL IAW SRM 57-2-0, FIG 2, CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B, PG 1-2, FABRICATED AND INSTALLED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2.Aug 9, 2000 · N805DH · Doug DC873FSDR DHL200080536CAngle · crackedAT C-CHECK, RT WING T/E ANGLE CRACKED 2 INCHES AT XW 5.000. PERFORMED STOP DRILL IAW SRM 57-2-0 FIG 2, CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B, PG 1-2, FABRICATED AND INSTALLED REINFORCING ANGLE IAW SRM 57-2-0, FIG 2.Aug 9, 2000 · N805DH · Doug DC873FSDR RRXA002798Former · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE FORMER AT T/E AT STA XFS 778, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57-2-2 AND 51-1-21.Aug 3, 2000 · N811AL · Doug DC871SDR COMA0010308Angle · crackedUPON COMPLIANCE OF 1C-CHECK TASK 194-01Z THE RIGHT WING UPPER SKIN ATTACH ANGLE FOR FAIRING 194 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IN ACCORDANCE WITH EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 1226-21, IR,Aug 3, 2000 · N247CA · Emb EMB120RTSDR COMA0010307Angle · crackedUPON COMPLIANCE OF 1C-CHECK TASK 193-01Z, THE LEFT WING UPPER SKIN ATTACH ANGLE FOR FAIRING 193 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IN ACORDANCE WITH EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 1226-21, IR, Aug 3, 2000 · N247CA · Emb EMB120RTSDR DHL200070949DFitting · crackedRT WING UPPER FRONT SPAR CORNER FITTING AT RBL 70.5 IS CRACKED. REMOVED UPPER FRONT FITTING PER SRM 51-30-2. INSTALLED NEW FITTING PER SRM 51-30-2.Aug 1, 2000 · N709DH · Boeing 72782CSDR RRXA002813Frame · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP FORMER AT T/E ON NR 3 STUB WING RT I/B AT STA XS 254, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 57-2-0.Jul 31, 2000 · N811AL · Doug DC871SDR EIA2000221Web · corrodedFOUND REAR SPAR WEB AT BS 1241 BULKHEAD FITTING ATTACH FASTENER SURROUNDING AREA CORRODED ON BOTH RIGHT AND LEFT SIDES. CORROSION REMOVED ON LEFT AND RIGHT REAR SPAR WEB AT BS 1241 BULKHEAD FITTING PER EVR EO-57-747-1544-99. (M)Jul 30, 2000 · N477EV · Boeing 747SR46SDR EIA2000234Fitting · crackedFOUND RIGHT BS 1241 KICK FITTING H-11 BOLT HOLE AREA, HOLE ''D'' CRACKED AT KICK FITTING AND TERMINAL FITTING BOTH CRACKS APPROX .030 INCH IN LENGTH. OVERSIZED FASTENER HOLE ON TERMINAL FITTING AND KICK FITTING ECCENTRICITY TO REMOVE CRACK, NDT INSPECTED, FREJul 30, 2000 · N477EV · Boeing 747SR46SDR EIA2000032Bracket · damagedDURING CLIMB, THE RIGHT WING OVERHEAT LIGHT ILLUMINATED. ISOLATED RIGHT WING AND LIGHT EXTINGUISHED. FOUND DUCTING TO NR 1 RIGHT BRACKET PDU BLOWN. INSPECTED AREA, NO DAMAGE FOUND. REPLACED BRACKET. OPS CHECK OK. (M)Jul 30, 2000 · N481EV · Boeing 747132SDR EIA7552Bracket · damagedNR 1 RIGHT WING LEADING EDGE FLAP FAILED TO RETRACT PNEUMATICALLY. OPERATIONAL CHECK OK ELECTRICALLY. FOUND BRACKET PDU TO DUCTING LET GO. REPLACED WITH NEW BRACKET. OPS CHECK NORMAL. (M)Jul 30, 2000 · N481EV · Boeing 747132SDR RRXA003814Angle · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO NR 2 STUB WING L/E ANGLE INSIDE BOTTOM ACCESS PANEL AT STA. XS250.089, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-Jul 28, 2000 · N811AL · Doug DC871SDR RRXA003813Former · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO NR 2 STUB WING L/E AT STA. XS227.335 AND UPPER T/E, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-4, 51-1-20D.Jul 28, 2000 · N811AL · Doug DC871SDR RRXA003812Bracket · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO NR 2 STUB WING L/E AT STA. XS255 AND BULKHEAD WEB, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, 51-3-2, 51-1-4.Jul 28, 2000 · N811AL · Doug DC871SDR UPS00434097Flange · crackedINSPECTION TYPE:C, RT WING UPPER FLANGE FOUND CRACKED ON L/E RIB AT OLES 1421.35. REPAIRED RIB IAW SRM 57-20-03 FIG 1.Jul 28, 2000 · N691UP · Boeing 747121SDR DL72S001399Stiffener · crackedFOUND AT A1 LTR CK, VERTICAL SPAR STIFFENER CRACKED O/B OF I/B TRACK AT NR 7 SLAT. REPAIRED PER ERA 377979-14.Jul 25, 2000 · N8873Z · Boeing 727225ASDR UPS00833581Fitting · crackedINSPECTION TYPE:C123, RIGHT WING STA XW 727 STRINGER 3 ATTACH CLIP IS CRACKED. REMOVED, FABRICATED, AND REPLACED FITTING IAW DWG 4614390, AND 8110-3 APPROVED DH SK 806-014, AND SRM 51-1-20D.Jul 22, 2000 · N806UP · Doug DC873FSDR UPS00833577Angle · crackedINSPECTION TYPE:C123, LEFT NR 2 STUB WING VERTICAL ANGLE IS CRACKED AT XS250. REMOVED, FABRICATED, AND REPLACED ANGLE IAW DWG 9753293, AND SRM 51-1-20D.Jul 22, 2000 · N806UP · Doug DC873FSDR UPS00833559Angle · crackedINSPECTION TYPE:C123, RIGHT WING L/E VERTICAL ANGLE IS CRACKED AT XS 520. REMOVED, FABRICATED, AND REPLACED ANGLE IAW DWG 9753297, AND SRM 51-1-20D, 51-1-21.Jul 22, 2000 · N806UP · Doug DC873FSDR UPS00434103Flange · crackedINSPECTION TYPE:C, RT WING UPPER FLANGE CRACKED AT FWD END OF L/E RIB AT OLES 1349.25. REF NRC 44310792.Jul 21, 2000 · N691UP · Boeing 747121SDR UPS00434072Flange · crackedINSPECTION TYPE:C, LT WING UPPER FLANGE CRACKED TWO LOCATIONS ON L/E OLES 1246.35. L/E RIB REPAIRED IAW SRM 57-20-03 FIG 1.Jul 21, 2000 · N691UP · Boeing 747121SDR UPS00833561Angle · crackedINSPECTION TYPE:C123, LEFT WING L/E VERTICAL ANGLE IS CRACKED AT XS 520. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 9753297 AND SRM 51-1-21, 51-1-20D.Jul 21, 2000 · N806UP · Doug DC873FSDR UPS00434098Intercostal · crackedINSPECTION TYPE:C, LT WING T/E INTERCOSTAL TO REAR ANGLE BRACKET CRACKED AT WS 570. NEW INTERCOSTAL TO REAR ANGLE BRACKET INSTALLED IAW 51-30-02.Jul 20, 2000 · N691UP · Boeing 747121SDR UPS00434065Splice · corrodedINSPECTION TYPE:C, LT WING LOWER FALSE WORK SUPPORT BEAM CRACKED AT ILES 813. REPAIR CARRIED OUT IAW SRM, QUERY NOTE 93/2000 SPLICED IN NEW SECTION OF BEAM BS 806 - 818, FAA 8110 ISSUED.Jul 20, 2000 · N691UP · Boeing 747121SDR AALA20001243Stiffener · corrodedTUL - FOUND HEAVY CORROSION ON L/E VERTICAL STIFFENER AT TOP OUTBOARD OF FUEL PRESSURE SWITCHES. INSTALLED NEW STIFFENER AT L/E, OUTBOARD OF FUEL PRESSURE SWITCHES. (M)Jul 19, 2000 · N716AA · Boeing 727227SDR 00FDEA00471Web · crackedDURING ROUTINE INSPECTION, WEB AT LEFT WING LEAD EDGE BS 920 FOUND CRACKED ADJACENT TO BOTTLE BOLT. REMOVED AND REPLACED PER IAW SRM 51-40-2.Jul 17, 2000 · N189FE · Boeing 72722
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