JASC 5720

Service difficulty reports · 13,629

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 SWAA2026070609990Support Angle · crackedCRACKED SUPPORT ANGLE LOCATED ORSS 279 TRAILING EDGE AT RT WING. REPLACED SUPPORT ANGLE LOCATED ORSS 279 TRAILING EDGE AT RT WING IAW SRM 51-10-02 ITEM 9 AND DRAWING 115A6200 SHEET 17 REV A.Jun 7, 2026 · N8641B · Boeing 7378H4SDR REXA2026073001316Support Angle · crackedCRACK ON LH WING BRACKET SUPPORT ANGLE SS 15.50, LOWER INNER AREA. CRACK ON LH WING BRACKET SUPPORT ANGLE SS 15.50, LOWER INNER AREA WAS REPAIRED PER EA NO: CRJ957-22519 EA REV IRJun 6, 2026 · N925XJ · Cndair CL6002D24SDR AALA202606159820Strap · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING ATTACH STRAP AT OSS 216, WBL 268.16. REPAIRED STRAP IAW SRM 57-20-00, SRM 51-20-01 AND EA 375886.Jun 6, 2026 · N876NN · Boeing 737823SDR IXXA20260606001Strut · crackedLEFT WING L/E UPPER SUPPORT STRUCTURE HAS CRACKAT LOCK FASTENER AFT END, VERIFIED BY EDDY CURRENT AROUND LES 506Jun 6, 2026 · N503AZ · Boeing 767338SDR 2026FA0000713Stiffener · crackedR/H WING FWD LWR I/B SKIN, FWD STIFFENER CRACKED. REPLACED WITH NEWJun 4, 2026 · N612G · Piper PA28181SDR IPXA2026060804787Bracket · crackedCRACKED R/H WING L/E INBD PANEL. 611KB BRACKET AREA TORQUE TUBE SUPPORT LES 281. INSTALLED NEW BRACKET IAW SRM 51-40-02-0G REV.55 AND BOEING DWG NO.114T1240 SH.6 REV.-Jun 4, 2026 · N397UP · Boeing 767300SDR REXA2026080401442Angle · corrodedSECONDARY NRC FROM NRC 00099 AND 00100: AFTER REMOVAL, CORROSION ON ANGLE SUPPORTS (2EA) OF ACCESS PANELS 542AZ AND 642AZ. CORROSION ON ANGLE SUPPORTS (2EA) OF ACCESS PANELS 542AZ AND 642AZ WAS REMOVED PER SRM 51-21-06-001-001-A01 AND ANGLE SUPPORT (1EA) OF ACJun 3, 2026 · N146PQ · Cndair CL6002D24SDR SWAA2026062308953Angle · crackedCRACKED ANGLE TRAILING EDGE LOCATED ORSS 271 RT WING. REPLACED ANGLE T/E LOCATED ORSS 271 RT WING IAW SRM 51-40-02-0G-0, DWG 115A2930, SHEET 6, REV-.Jun 3, 2026 · N476WN · Boeing 7377H4SDR CALA2026060516839Support · corrodedLEFT WING T/E PANEL 571CB, PANEL SUPPORT IS CORRODED. REMOVED BEAM,FABRICATED NEW BEAM AND INSTALLED PER B737-800 SRM 51-40-02 AND BAC DWG 115A4711 REV B.Jun 3, 2026 · N14240 · Boeing 737824SDR IPXA2026061562566Fitting · crackedCRACKED BRACKET, LT WING T/E INBD SECTION UPPER FIXED PANEL LOWER SUPPORT AT WBL 255.692, ADJACENT NR 6 SPOILER INBD SIDE. IAW SRM 51-40-02-0G REV 106, AND DWG:65B11544, SHEET 1, REV G. INSTALL NEW FITTING ASSY.Jun 2, 2026 · N577UP · Boeing 74744AFSDR SWIA2026060176918Support Angle · crackedRIGHT WING BATT RIB ACCESS PANEL SUPPORT ANGLE AT APPROX. WS 50 HAD A POSSIBLE CRACK. REPLACED BATT RIB SUPPORT ANGLE. IAW DWG 601R10203, REV G. COMPLETED SKYWEST TASK CARD 51-900-1003-SKY.Jun 1, 2026 · N936EV · Cndair CL6002B19SDR SWIA2026060176917Intercostal · crackedLEFT WING BATT RIB INTERCOSTAL AT APPROX. WS 50 HAS POSSIBLE CRACK. INSTALLED NEW LT WING AFT BATT RIB WS 53.60. IAW SRM 51-42-06, SRM 51-42-21, REO 601R-57-21-4117, REV -. & DWG 601R10203, REV -G. COMPLETED SKYWEST TASK CARD 51-900-1003-SKY.Jun 1, 2026 · N936EV · Cndair CL6002B19SDR SWAA2026062408446Bracket · crackedCRACKED DEFLECTION CONTROL RIB TRAILING EDGE BRACKET LOCATED ORSS 272 LT WING. REPLACED DEFLECTION CONTROL RIB TRAILING EDGE BRACKET LOCATED ORSS 272 LT WING IAW SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 115A2930 SHEET 7 REV.Jun 1, 2026 · N7876A · Boeing 7377Q8SDR AALA202606030211Strap · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND WING OUTBOARD LOWER ATTACH STRAP FROM OSS 207.75 TO OSS 282.95, RIB 1 TO 2. REPAIRED STRAP PER SRM 57-20-01-2R REPAIR 3 AND EA 375720.Jun 1, 2026 · N853NN · Boeing 737823SDR SWAA2026062308094Angle · crackedCRACKED ANGLE ACCESS PANEL 551FB AT LT WING. REPLACED ANGLE ON ACCESS PANEL 551FB AT LT WING IAW SRM 51-10-02-0G-0, PARAGRAPH 9, SRM 51-40-02-0G-0, AND DWG 115A2710, SHEET 6, REV B.May 31, 2026 · N476WN · Boeing 7377H4SDR SWAA2026061707881Support Angle · crackedCRACKED OTBD TRAILING EDGE SUPPORT ANGLE ON ORSS 287 AT LT WING. REPLACED OTBD TE SUPPORT ANGLE AT ORSS 287, LT WING IAW SRM 51-40-02-0G-0, DWG 115A3700, SHEET 31, REV-, & DWG 115A3712, SHEET 12, REV- .May 30, 2026 · N482WN · Boeing 7377H4SDR SWAA2026061707882Support Bracket · crackedCRACKED TRAILING EDGE SUPPORT BRACKET LOCATED ON IRSS 268 AT LT WING. REPLACED SUPPORT BRACKET LOCATED TRAILING EDGE IRSS 268 AT LT WING IAW SRM 51-10-02-0G-0, PARAGRAPH 9, SRM 51-40-02-0G-0, AND DWG 115A2930, SHEET 7, REV -.May 30, 2026 · N482WN · Boeing 7377H4SDR IPXA2026060823951Bracket · brokenBROKEN BRACKET, LT WING L/E CAVITY PLATE ATTACH ON AIR TUBE CLAMP OVER NR 2 PYLON AT ILES 630 . 720. I.A.W SRM 51-40-02-0G REV. 106 REMOVED DAMAGE BRACKET. I.A.W SRM 51-40-02-0G REV. 106 AND DWG 65B15696 SH. 7 REV. D. INSTALLED NEW BRACKET.May 30, 2026 · N577UP · Boeing 74744AFSDR IPXA2026061620751Support Bracket · corrodedRH WING LOWER SURFACE SIDE OF BODY SPLICE INTERNAL TRIANGULAR SHAPE PANEL 194CR MID SUPPORT BRACKET ANGLE CORRODED/ DOT.139.032. INSTALLED 1EA FRAME, 1EA BRACKET, 1EA FITTING AND 2EA ANGLES IAW B757-200PF SRM 51-40-02-0G-0.May 29, 2026 · N413UP · Boeing 75724APFSDR IPXA2026060206488Angle · crackedCRACKED CLIP, RT WING T/E GEAR AREA PANEL 672EB INBD AFT CONDITION CHECK NORMAL. INSTALLED NEW CLIP I.A.W SRM 51-40-02-0G REV.106 AND BOEING DWG:65B07738 SHEET 06 REV U.May 29, 2026 · N577UP · Boeing 74744AFSDR 2026FA0000722Stiffener · crackedR/H WING FWD LWR I/B SKIN, AFT STIFFENER CRACKED. REPLACED WITH NEWMay 26, 2026 · N328G · Piper PA28181SDR 2026FA0000711Stiffener · crackedR/H WING FWD LWR I/B SKIN, FWD STIFFENER CRACKED. REPLACED WITH NEWMay 26, 2026 · N328G · Piper PA28181SDR SWAA2026062206809Bracket · crackedRIGHT WING T/E LOCATED INBD OF DEFLECTION CONTROL RIB, OVERHANG PANEL SUPPORT BULKHEAD ATTACH BULB SEAL RETAINER CRACKED. REMOVED AND REPLACED DEFLECTOR PANEL SEAL; RETAINER; AND BRACKET IAW SRM 51-40-02, REF AIPC 57-50-00-25. REINSTALLED DEFLECTOR PANEL IAWMay 26, 2026 · N478WN · Boeing 7377H4SDR SWAA2026062206811Bracket · crackedLEFT WING T/E LOCATED INBD OF DEFLECTION CONTROL RIB, OVERHANG PANEL SUPPORT BULKHEAD ATTACH BULB SEAL RETAINER CRACKED. REMOVED AND REPLACED SEAL REAINER AND BRACKET IAW SRM 51-40-02, REF AIPC AIPC 57-50-00-25 & REINSTALLED PANEL IAW SRM 51-40-02, REF AIPC AMay 26, 2026 · N478WN · Boeing 7377H4SDR UIEA2026050100284Strap · corrodedRHW L/E D-BEAM LOWER STRAP AT ILES 665 FOUND HEAVY CORROSION(<P>CORROSION STRAP FABRICATED AS PER BOEING DWG 65B12246 AND PL, AND NEW STRAP REPLACED AS PER SRM 51-10-02, AND NEW STRAP HOLES TRANSFERRED AS PER SRM 51-40-05, AND STRAP INSTALLED AS PER SRM 51-40-May 23, 2026 · N477MC · Boeing 74747UFSDR IPXA2026052424821Stiffener · crackedCRACKED STIFFENER, FLOOR SUPPORT STRUCTURE STA 785.9 RBL 11. ACCOMPLISH THE REPAIR I.A.W SRM 57-10-10-2R-2 REV. 95 AND EGAT WORK SHEET NO: 60431 AND EO-58151-REQ001 REV1.May 23, 2026 · N341UP · Boeing 76734AFSDR CALA2026052716554Support · crackedPANEL 671 BT WITH CRACK ON SUPPORT STRUCTURE. REMOVED PANEL 671BT & BEAM SPRT RH WING, EVAUATED FOUND TO BE OUT OF LIMITS, VERIFIED MATERIAL, FABRICATED NEW SUPPORT, LOCATED AND DRILL NEW SUPPORT, APPLIED ALODINE, APPLIED PRIMER, APPLIED TOP COAT ON SUPPORT, IMay 22, 2026 · N14249 · Boeing 737824SDR 2026FA0000728Stiffener · crackedL/H WING FWD LWR I/B SKIN, TOP AFT STIFFENER CRACKED. REPLACED WITH NEWMay 21, 2026 · N374G · Piper PA28181SDR VNAA202607300012Bracket · corrodedCORROSION ON SUPPORTS (2EAS) OF ELECTRICAL HARNESS BTW WS=0.00 AND WS=29.00 THROUGH ACCEES PANL 542AZ, 642AZ AT LH/RH WING AUXILIARY INTERNAL REAR SPAR. SUPPORTS (2EAS) OF ELECTRICAL HARNESS BTW WS=0.00 AND WS=29.00 THROUGH ACCEES PANL 542AZ, 642AZ AT LT/RT WMay 21, 2026 · N644NN · Cndair CL6002D24SDR JR2R20260521008Fitting · corrodedRT MLG W/W AILERON QUADRANT FITTING IS CRACKED. REPLACEDMay 21, 2026 · N86316 · Emb ERJ170200LLSDR VNAA202607300015Intercostal · corrodedCORROSION ON INTERCOSTAL BTW WS=29.00 AND WS=48.95 AT RT WING INTERNAL AUXILIARY REAR SPAR. INTERCOSTAL BTW WS 29.00 AND WS 48.95 AT RH WING INTERNAL AUXILIARY REAR SPAR WAS REPLACED IAW SRM 51-42-21-001-001-A01.May 19, 2026 · N644NN · Cndair CL6002D24SDR VNAA202607300014Bracket · corrodedCORROSION ON LIGHT SUPPORT (2EAS) BTW WS 29.00 AND WS 48.00 AT LT & RT WING INTERNAL AUXILIARY REAR SPAR. LIGHT SUPPORT (2EAS) BTW WS=29.00 AND WS=48.00 AT LT & RT WING INTERNAL AUXILIARY REAR SPAR WERE EVALUATE AND FOUND WITH EXCESSIVE CORROSION IAW SRM 51-10May 19, 2026 · N644NN · Cndair CL6002D24SDR VNAA202607300013Angle · corrodedCORROSION ON ANGLE (2EAS) ON BTW WS=0.00 AND WS=29.00 AT LH/RH WING AUXILIARY INTERNAL REAR SPAR. CORROSION ON ANGLE ON BTW WS=0.00 AND WS=29.00 AT RH WING AUXILIARY INTERNAL REAR SPAR WAS REMOVED AND EVALUATED WITHIN OF LIMITS PER SRM 51-21-06-001-001-A01 May 19, 2026 · N644NN · Cndair CL6002D24SDR FXGA2026FA0000410Flange · crackedCRACK INDICATION NR 3 TANK 182C FLANGE, REPAIRED PER EO 2609May 19, 2026 · N747CE · Doug DC6ASDR JR2R20260519023Angle · crackedUPON PREPPING FOR L/H W/W FR52 WEB R/R, FOUND STUB ANGLE CRACKED AT FIRST FASTENER HOLE. REPAIRED PER ETD.May 19, 2026 · N86316 · Emb ERJ170200LLSDR 2026FA0000465Stiffener · crackedR/H WING FWD LWR I/B SKIN, AFT STIFFENER CRACKED. REPLACED WITH NEWMay 18, 2026 · N932G · Piper PA28181SDR 2026FA0000457Stiffener · crackedL/H WING FWD LWR I/B SKIN, TOP FWD STIFFENER CRACKED. REPLACED WITH NEWMay 18, 2026 · N875G · Piper PA28181SDR CALA2026052816581Support Angle · corrodedRT WING TE EDGE AT PANEL 661AB AFT ATTACH SUPPORT ANGLE WITH EVIDENCE OF SURFACE CORROSION. INSTALLED SUPPORT ANGLE (BEAM) AT RT WING TE EDGE PANEL 661AB AFT IAW SRM 51-40-02-0G-0,AND DWG#115A3758,May 16, 2026 · N73270 · Boeing 737824SDR 4VAA202605150038QBracket · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT WING REAR SPAR HYDRAULIC LINE CLAMP BRACKET. THE BRACKET WAS REPLACED IN ACCORDANCE WITH SAAB STATEMENT 2000SDS060710.May 15, 2026 · N749SA · Saab 2000SAABSDR 4VAA202605150037Bracket · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT WING REAR SPAR HYDRAULIC LINE CLAMP BRACKET. THE BRACKET WAS REPLACED IN ACCORDANCE WITH SAAB STATEMENT 2000SDS060710.May 15, 2026 · N749SA · Saab 2000SAABSDR SWAA2026061803395Angle · crackedCRACKED ANGLE TRAILING EDGE LOCATED ORSS 280 RT WING. REPLACED ANGLE TRAILING EDGE LOCATED ORSS 280 RT WING IAW ALLOWABLE DAMAGE 57-51-02-1A-1 ALLOWABLE DAMAGE 1, NOT FOUND ALLOWABLE DAMAGE, SRM 51-10-02-0G-0, ITEM 9, SRM 51-40-02-0G-0, AND DWG 115A6200, SHEEMay 15, 2026 · N500WR · Boeing 7378H4SDR SWAA2026061103387Intercostal · crackedBRACKET INBOARD OF THE INBD RT WING DEFLECTION CONTROL RIB INBD INTERCOSTAL IS CRACKED. REMOVED AND REPLACED THE BRACKET ANGLE IAW SRM 5-40-02.May 15, 2026 · N8540V · Boeing 7378H4SDR SWAA2026061003430Support Beam · corrodedCORROSION SUPPORT BEAM LOCATED TRAILING EDGE BTW ORSS 334 TO ORSS 442 WL 190 AT RT WING. REPLACED SUPPORT BEAM LOCATED TRAILING EDGE BTW ORSS 334 TO ORSS 442 WL 190 AT RT WING IAW SRM 51-10-02 ITEM 9 AND DWG 115A3700 SHEET, 51 REV-.May 15, 2026 · N7749B · Boeing 7377BDSDR CALA2026051716307Support Angle · corrodedLT WING TE EDGE AT PANEL 561AB AFT ATTACH SUPPORT ANGLE WITH EVIDENCE OF SURFACE CORROSION. INSTALLED SUPPORT ANGLE ( BEAM) AT LT WING TE EDGE PANEL 561AB AFT IAW SRM 51-40-02-0G-0,AND DWG 115A3758,PENDING ESFR ENTRY AND NO DIP REQUIRED.May 15, 2026 · N73270 · Boeing 737824SDR 2026FA0000386Stiffener · shearedFLAP TRACK STIFFENERS THAT KEEP THE FLAP TRACKS STRAIGHT AND TRUE WERE FOUND TO BE SHEARED OFF AND/OR CRACKED.May 15, 2026 · N61803 · Cessna 172MSDR 4VAA202605130026Support · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LEFT HAND NACELLE FIRE FLOOR SUPPORT. THE SUPPORT WAS REPAIRED IN ACCORDANCE WITH SAAB STATEMENT 2000SDS060641.May 13, 2026 · N749SA · Saab 2000SAABSDR 4VAA202605130025Angle · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LEFT HAND NACELLE FIRE FLOOR ANGLE. THE ANGLE WAS REPLACED IN ACCORDANCE WITH SAAB STATEMENT 2000SDS060704.May 13, 2026 · N749SA · Saab 2000SAABSDR SWAA2026061098356Angle · crackedCRACKED ANGLE TRAILING EDGE, ORSS 261 PLUS 14 INCHES, RT WING. REPLACED ANGLE AND FASTENERS ON TRAILING EDGE LOC ORSS 261 PLUS 14 INCHES AT RT WING IAW SRM 51-40-02-0G-0 AND DWG 115A2512 SHEET 16, REV-.May 13, 2026 · N7749B · Boeing 7377BDSDR SWAA2026061097912Angle · crackedCRACKED ANGLE LOCATED INBD SIDE OF RT WING INBD AUXILIARY TRACK SLAT 6. REPLACED ANGLE LOCATED INBD SIDE OF INBD AUXILIARY TRACK SLAT 6 AT RT WING SRM 51-40-02, AND DWG 114A5030, SHEET 2 REV:C. MEASUREMENT OF CRACK: L: 2.400'.May 12, 2026 · N7749B · Boeing 7377BDSDR 2026FA0000462Stiffener · crackedR/H WING FWD LWR I/B SKIN, AFT STIFFENER CRACKED. REPLACED WITH NEW.May 12, 2026 · N164G · Piper PA28181
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