JASC 5740

Service difficulty reports · 3,003

Reports filed under 5740 · Wing, Attach Fittings, 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 = '5740'
  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 SWIA2025120200821Attach Angle · corrodedL/H TIRE BURST PANEL FWD ATTACHING ANGLE HAS SIGNS OF CORROSION. REMOVED AND INSTALLED NEW ATTACH ANGLE, IAW DWG CC670-10320, REV F, SRM 51-42-21-001-001-A01, AND SRM 51-23-00-001-001-A01. LEAK CHECK GOOD.Aug 21, 2025 · N897SK · Cndair CL6002D24SDR SWAA2025092606896Nut Plate · corrodedCORROSION ON RAIL NUT-PLATE LOCATED TRAILING EDGE INTERNAL CAVITY UPPER POSITION ORSS 375 AT LT WING. REPLACED RAIL NUT-PLATE LOCATED TRAILING EDGE INTERNAL CAVITY UPPER POSITION BTW ORSS 350 TO ORSS 379 APPROX AT LT WING IAW SRM 51-10-02 ITEM 9 AND DWG 115A3Aug 21, 2025 · N8615E · Boeing 7378H4SDR SWAA2025092607116Nut Plate · corrodedCORROSION ON RAIL NUT-PLATE LOCATED TRAILING EDGE INTERNAL CAVITY UPPER POSITION ORSS 404 AT RT WING. REPLACED RAIL NUT-PLATE LOCATED TRAILING EDGE INTERNAL CAVITY UPPER POSITION ORSS 404 AT RT WING IAW SRM 51-40-02.Aug 21, 2025 · N8615E · Boeing 7378H4SDR SWAA2025092607110Nut Plate · corrodedCORROSION ON RAIL NUT-PLATE LOCATED TRAILING EDGE INTERNAL CAVITY UPPER POSITION ORSS 375 AT RT WING. REPLACED RAIL NUT-PLATE LOCATED TRAILING EDGE INTERNAL CAVITY UPPER POSITION ORSS 375 AT RT WING IAW SRM 51-40-0 AND DWG 115A3513 SHEET 5 REV. -.Aug 21, 2025 · N8615E · Boeing 7378H4SDR 2026FA0000153Attach Fitting · crackedLEFT WING FORWARD SPAR, OUTBOARD UPPER AFT-FACING WING ATTACH FITTING WAS FOUND TO BE CRACKED WITHIN GEAR WELL. THE PART IS SHOWN IN THE 421C IPC, SECTION 03-50, PAGE 16, ITEM 6. THE CRACK MEASURES ROUGHLY 5-1/8" AND RUNS HORIZONTALLY ACROSS SEVEN RIVET HOLES.Aug 20, 2025 · N421KM · Cessna 421CSDR JR2R20250820803Nut Plate · brokenRIGHT WING OTBD AFT FLAP LOWER INBD SKIN HAS A BROKEN NUTPLATE.Aug 20, 2025 · N82338 · Emb ERJ170200LRSDR SWAA2025081803829Attach Fitting · damagedNUMBER 6 LEADING EDGE SLAT, HAS 4EA PULLED FASTENERS AT ACTUATOR ATTACH FITTING. PERFORMED SLAT CAN INSP. #6 SLAT TRACKS PER AMM 27-81-21. NO DEFECTS NOTED. OK TO INSTALL NR 6 SLAT IAW AMM 27-81-21. REMOVED SLAT IAW AMM 27-81-21. C/W INSP.REMOVED SLAT IAAug 13, 2025 · N424WN · Boeing 7377H4SDR GRTA20250822001Fitting · damagedDURING WING BOLT INSPECTION, FOUND RH OUTBD LOWER WING BOLT OUTBD FITTING HAS WASHER IMPRESSION. REPAIRED IN ACCORDANCE WITH TEXTRON FIELD REPAIR FR-LJ-1397-15621.Aug 12, 2025 · N591AW · Beech C90ASDR SWAA2025091098731Nut Plate · corrodedCORROSION ON RAIL NUT-PLATE LOCATED LEADING EDGE INTERNAL CAVITY ORSS 406 AT LT WING. REPLACED RAIL NUT-PLATE LOCATED LEADING EDGE INTERNAL CAVITY ORSS 406 AT LT WING IAW B737-800 SRM 51-10-02-0G-0 ITEM 9 SRM 51-40-02 AND DWG 112A4402 SHEET 40 REV A.Aug 5, 2025 · N8617E · Boeing 7378H4SDR JJBA20250806011Nut Plate · brokenLH LEADING EDGE #2 OUTBD RIB, X2 NUT PLATE FOUND BROKEN. LH WING LEADING EDGE #2, LOWER SKIN CUT-OUT AND FILLER INSTALLED INBD OF STA YS=6405.Aug 4, 2025 · N11199 · Emb EMB145XRSDR JJBA20250808018Bracket · crackedINSIDE RH FUEL PANEL 631DB, 2 BRACKETS FOUND CRACKED. RH WING LOWER SKIN AT RIB 8 PAINT REMOVED. RH FUEL PANEL 631DB RIB 8, 2 BRACKETS REPLACED.Aug 1, 2025 · N11199 · Emb EMB145XRSDR SWAA2025090397098Nut Plate · crackedCRACK RAIL NUT PLATE OTBD FRONT SPAR OFSS 465 AT RT WING. REPLACED RAIL NUT PLATE O/B FRONT SPAR OFSS 465 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 112A4402 SHEET:13 REV:-.Jul 31, 2025 · N903WN · Boeing 7377H4SDR SWAA2025082795601Nut Plate · crackedCRACK O/B FIXED LEADING EDGE RAIL NUT PLATE OFSS 576 AT RT WING. REPLACED FIXED LEADING EDGE RAIL NUT PLATE OFSS 576 AT RT WING IAW B737-800 SRM 51-10-02 ITEM 9 AND DWG 112A4402 SHEET 41 REV A.Jul 26, 2025 · N8616C · Boeing 7378H4SDR SWAA2025082795533Nut Plate · crackedCRACK O/B FIXED LEADING EDGE RAIL NUT PLATE OFSS 369 AT LT WING. REPLACED RAIL NUT PLATE LOCATED O/B FIXED LEADING EDGE OFSS 369 AT LT WING IAW SRM 51-10-02-0G-0 ITEM 9; SRM 51-40-02-0G-0 AND DWG 112A4402 SHEET: 40 REV: A.Jul 26, 2025 · N8616C · Boeing 7378H4SDR SWAA2025082795532Nut Plate · corrodedCORROSION O/B FIXED LEADING EDGE RAIL NUT PLATE OFSS 449 AT LT WING. REPLACED O/B FIXED LEADING EDGE RAIL NUT PLATE OFSS 449 AT LT WING IAW B737-800 SRM 51-40-02-0G AND DWG: 112A4402; SHEET: 40; REV: A.Jul 26, 2025 · N8616C · Boeing 7378H4SDR AALA202508079012Attach Fitting · wornAIRCRAFT IN BASE MAINTENANCE: NUMBER 2 TRANSMISSION ATTACH FITTING MOUNTING BOLTS ARE WORN AT TRACK MOUNTS. INSTALLED AND REAMED NUMBER 2 AFT TRACK FORWARD AND AFT TRANSMISSION ATTACH SUPPORT FITTING BUSHINGS. PER SOPM 20-50-03.Jul 17, 2025 · N934NN · Boeing 737823SDR IPXA2025080808894Bracket · crackedRH WING, KRUEGER BOX AREA, LOWER AREA, 1ST ANGLE BRACKET IS CRACKED. STAMP23. INSTALLED ANGLE RH WING, KRUEGER BOX AREA, BY RIB 2, IAW A300-600 SRM 51-40-21.Jul 13, 2025 · N172UP · Airbus A300F4622RSDR IPXA2025080808862Bracket · crackedRIGHT WING, KRUEGER BOX AREA, LOWER AREA, 3ER ANGLE BRACKET IS CRACKED. STAMP23. INSTALLED ANGLE RH WING, KRUEGER BOX AREA, BY RIB 2, IAW A300-600 SRM 51-40-21. REVIEWEDJul 13, 2025 · N172UP · Airbus A300F4622RSDR SWAA2025071787663Bracket · crackedRIGHT WING HAS A BRACKET INBOARD OF SHELF PANEL SUPPORT WEB CRACKED. REMOVED AND REPLACED RH WING BRACKET IB OF SHELF PANEL SUPPORT WEB IAW SRM 51-40-02.Jul 3, 2025 · N8696E · Boeing 7378H4SDR SWAA2025071787664Bracket · crackedLEFT WING HAS A BRACKET INBOARD OF SHELF PANEL SUPPORT WEB CRACKED. REMOVED AND REPLACED BRACKET IAW SRM 51-40-02..Jul 3, 2025 · N8696E · Boeing 7378H4SDR SWAA2025081187765Angle · crackedCRACK ON INBOARD AND OUTBOARD ANGLE LOCATED INBOARD AUXILIARY TRACK SLAT 1 AT LT WING (2E/A). REPLACED INBOARD AND OUTBOARD ANGLE LOCATED INBOARD AUXILIARY TRACK SLAT 1 AT LT WING (2E/A) IAW B737-700 CMM-57-43-01 PAGE 702 STEP 3 C ITEM (9).Jul 2, 2025 · N7886A · Boeing 737752SDR VNAA20250629019Attach Bracket · corrodedCORROSION FOUND ON OTBD/FWD ATTACHMENT BRACKET OF 586BB. REMOVED CORROSION FROM THE WS 128 HINGE ARM OUTBOARD / FORWARD BRACKET COMMON TO PANEL 586BB IAW CRJ-900 SRM 51-21-06-001-001-A01 & FOUND TO BE OUT OF LIMITS DUE TO THERE BEING NO ALLOWABLE LIMITS PROVJun 29, 2025 · N636NN · Cndair CL6002D24SDR SWAA2025071784707Attach Angle · crackedLEFT WING TRAILING EDGE; ATTACH ANGLE FROM DEFLECTION CONTROL RIB TO INTERCOSTAL WEB IS CRACKED. REMOVED CRACKED ANGLE PER SRM 51-40-02.;[02] ANGLE HAS BEEN REMOVED. LOCATED; DRILLED AND DEBURRED REPLACEMENT ANGLE PER SRM 51-40-05. INSTALLED REPLACEMENT ANGJun 24, 2025 · N8693A · Boeing 7378H4SDR AALA202507179413Attach Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING ATTACH FITTING INTERCONNECTING STRUT LOWER POSITION LH WING. MAINTENANCE REPLACED ATTACH FITTING INTERCONNECTING STRUT LOCATED LOWER POSITION LH WING IAW A319 SRM 51-42-11-801 AND DWG D57570280.Jun 22, 2025 · N770UW · Airbus A319112SDR SWAA2025072183181Nut Plate · corrodedCORROSION ON RAIL NUT PLATES LOCATED OFSS697 INTERNAL CAVITY TRAILING EDGE AT RT WING REPLACED RAIL NUT PLATES LOCATED OFSS697 INTERNAL CAVITY TRAILING EDGE AT RT WING IAW B737-700 SRM 51-40-02 AND DWG 112A4402 SHEET 13; REV-.Jun 18, 2025 · N294WN · Boeing 7377H4SDR SWAA2025071580438Nut Plate · crackedCRACK RAIL NUTPLATE LEADING EDGE INTERNAL CAVITY FRONT SPAR LOCATED BETWEEN OFSS 565 TO OFSS 580 AT LT WING. REPLACED RAIL NUTPLATE LEADING EDGE INTERNAL CAVITY FRONT SPAR LOCATED BETWEEN OFSS 565 TO OFSS 580 AT LT WING IAW SRM 51-10-02-0G AND 51-40-02-0G-0 Jun 10, 2025 · N292WN · Boeing 7377H4SDR SWAA2025071178755Nut Plate · crackedCRACK ON RAIL NUTPLATE LOCATED LEADING EDGE INTERNAL CAVITY ON ORSS 449 AT RT WING. REPLACED RAIL NUTPLATE LOCATED LEADING EDGE INTERNAL CAVITY ON ORSS 449 AT RT WING IAW SRM 51-40-02-0G AND DWG: 112A4402 SHEET: 13 REV: -. MEASURE OF CRACK: 0.448.Jun 6, 2025 · N7721E · Boeing 7377BDSDR SWAA2025071178757Nut Plate · crackedCRACK ON RAIL NUTPLATE LOCATED LEADING EDGE INTERNAL CAVITY ON ORSS 385 AT LT WING CRACK ON RAIL NUTPLATE LOCATED LEADING EDGE INTERNAL CAVITY ON OFSS 385 AT LT WING. REPLACED RAIL NUTPLATE LOCATED LEADING EDGE INTERNAL CAVITY ON OFSS 385 AT LT WING IAW 51-4Jun 6, 2025 · N7721E · Boeing 7377BDSDR SWAA2025071178758Nut Plate · crackedCRACK ON RAIL NUTPLATE LOCATED LEADING EDGE INTERNAL CAVITY ON ORSS 575 AT LT WING MEASURE OF CRACK: 0.448'. REPLACED RAIL NUTPLATE LOCATED LEADING EDGE INTERNAL CAVITY ON ORSS 575 AT LT WING IAW SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 112A4402 SHEET: 13 RJun 6, 2025 · N7721E · Boeing 7377BDSDR SWAA2025071178759Nut Plate · crackedCRACK ON RAIL NUTPLATE LOCATED LEADING EDGE INTERNAL CAVITY ON ORSS 483 AT LT WING 2025-363338<[01] REPLACED RAIL NUTPLATE LOCATED LEADING EDGE INTERNAL CAVITY ON ORSS 483 AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 112A4402 SHEET: 13 REJun 6, 2025 · N7721E · Boeing 7377BDSDR SWAA2025071078756Nut Plate · crackedCRACK ON RAIL NUTPLATE LOCATED LEADING EDGE INTERNAL CAVITY ON ORSS 575 AT RT WING. EPLACED RAIL NUTPLATE LOCATED LEADING EDGE INTERNAL CAVITY ON ORSS 575 AT RT WING IAW SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 112A4402 SHEET: 14 REV -.Jun 6, 2025 · N7721E · Boeing 7377BDSDR SWIA2025100700603Attach Fitting · corrodedRH WING FWD ATTACHMENT FITTING FOR HINGE BOX AT WS80.5 IS CORRODED. (C-CHECK RO 10/06/2025) REMOVED CORROSION AT RH WING FWD ATTACHMENT FITTING FOR HINGE BOX AT WS80.5 PER CRJ200 SRM 51-21-06 AND PERFORMED REPAIR PER REO 601R-57-21-3951 REV -- DATED 2025-07-Jun 3, 2025 · N917EV · Cndair CL6002B19SDR SWAA2025062578653Fitting · looseLEFT WING TRAILING EDGE - DEFLECTION CONTROL RIB SUPPORT BEAM ATTACHMENT FASTENERS ARE LOOSE AT SERRATED PLATE.<[01] REMOVED INBD AND OUTBD SERRATED PLATES FOR REPLACEMENT IAW SRM 51-40-02.;;[12] INSTALLED TEE FITTING AND UPPER AND LOWER O.B. RADIUS FILLERS PEMay 28, 2025 · N8692F · Boeing 7378H4SDR SWAA2025061072596Attach Angle · crackedLT WING DEFLECTION CONTROL RIB UPPER PANEL ATTACHMENT CRACKED.<[01] REPAIRED LT WING DEFLECTION CONTROL RIB UPPER PANEL ATTACHMENT IAW SRM 57-51-02-2R-3.;[02] CORRECTIVE ACTION COMPLETED.May 19, 2025 · N7823A · Boeing 7377CTSDR SWIA202507140515Attach Fitting · chafedCENTER PCU ATTACH LOBE, ON THE RUDDER, IS CHAFFED ON THE LOBE EDGE (MARKED) (C-CHECK RO 07/11/2025)BLENDED DAMAGE ON CENTER PCU ATTACH LOBE, ON THE RUDDER AND FOUND OUT OF LIMITS. REPAIRED PER MHIRJ REO 601R-55-41-304 REV -- DATE 2025-06-11. COMPLIED WITH ALLMay 15, 2025 · N223JS · Cndair CL6002B19SDR AALA202505279815Attach Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION BOLT ATTACHMENT SLAT TRACK 1 MID FWD POSITION CORRODED AREA IS L= 0.491 IN W=0.195 IN D=0.007 IN. MAINTENANCEMay 10, 2025 · N775XF · Airbus A319112SDR SWAA2025051469258Bracket · crackedRIGHT WING UPR I/B PANEL SUPPORT FWD ATTACH BRACKET (Z BRACKET) CRACKED.<[01] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)]May 10, 2025 · N252WN · Boeing 7377H4SDR IXXA20250521002Attach Bolt · crackedLH WING #6 SLAT AT OUTBD CONTROL ROD LOWER ATTACH L BRACKET IS CRACKEDMay 1, 2025 · N1049A · Boeing 76736NSDR HYIA20250506002Fitting · corrodedDURING SCHEDULED MAINTENANCE A SMALL AREA OF SURFACE CORROSION WAS VISUALLY IDENTIFIED ON THE RIGHT WING LOWER AFT WING FITTING. (OEM PN: 0822550-44). THIS CORROSION MEASURES APPROX. .375" LONG WITH A MAX DEPTH OF APPROX. .030" AND IS CONSISTENT WITH OTHER CORMay 1, 2025 · N747WS · Cessna 402CSDR SWAA2025051957606Attach Angle · crackedCRACKED ATTACH ANGLE AT RT WING T/E JUST IB OF DEFLECTION CONTROL RIB. MARKED<[01] REMOVED AND REPLACED ATTACH ANGLE AT R/W T/E JUST I/B OF DEFLECTION CONTROL RIB IAW SRM 51-40-02-0G-0 PARA. 4.;[02] COMPLETEApr 23, 2025 · N437WN · Boeing 7377H4SDR SWAA2025050751397Attach Bracket · crackedRIGHT WING CONDUIT BRACKET ABOVE AND AFT OF MLG MAIN RETRACT ACTUATOR LOWER ATTACH POINT MOUNT IS CRACKED.<[01] INFO: WORK WITH FAULT ID TTG8Q00ZUZDG AS THIS IS WHERE THE OTHER HALF OF THE SAME BRACKET IS WRITTEN UP.;[02] REFERENCE TASK CARD LINE # 1177; R/H WApr 19, 2025 · N8684F · Boeing 7378H4SDR UATA5606417255702Fitting · damagedUPPER REAR STRUT FITTINGS ON THE RIGHT WING HAVE DAMAGE TO STRUT MOUNTING HOLES AND STRUCTURE. WING LIFT STRUT ATTACH FITTINGS FOUND CORRODED/DAMAGED ON LEFT AND RIGHT WING AND FUSELAGE. WINGS - REMOVED WING LIFT STRUT ATTACH FITTINGS ON BOTH SIDES. TRANSFERREApr 17, 2025 · N708RA · Cessna 208BSDR UATA5606417255701Fitting · damagedUPPER REAR STRUT FITTING ON THE LEFT WING HAS DAMAGE TO STRUT MOUNTING HOLES AND STRUCTURE. WING LIFT STRUT ATTACH FITTINGS FOUND CORRODED OR DAMAGED ON LEFT AND RIGHT WING AND FUSELAGE. WINGS - REMOVED WING LIFT STRUT ATTACH FITTINGS ON BOTH SIDES. TRANSFERREApr 17, 2025 · N708RA · Cessna 208BSDR VNAA202504170107Trunnion · corrodedLH INBD FLAP VANE ACTUATOR AT FLS140.4 FWD TRUNNION IS CORRODED. CORRECTIVE ACTION: REPLACED LH INBD FLAP W.S. 140.4 FLAP VANE ACTUATOR PN: CC670-14300-9-01 IAW CRJ700 AMM 27-52-23-000/400-801 A01. CC670-14002-7Apr 17, 2025 · N508AE · Cndair CL6002C10SDR VNAA202504170106Trunnion · corrodedLH INBD FLAP VANE ACTUATOR AT FLS102.9 FWD TRUNNION IS CORRODED CORRECTIVE ACTION: REPLACED LH INBD FLAP W.S. 102.9 FLAP VANE ACTUATOR PN: CC670-14300-9-01 IAW CRJ700 AMM 27-52-23-000/400-801 A01. CC670-14002-7Apr 17, 2025 · N508AE · Cndair CL6002C10SDR VNAA202504170105Trunnion · corrodedL/H I/B FLAP VANE ACUTATOR FWD TRUNNION AT STATION LS 24.0 IS CORRODED.CORRECTIVE ACTION: REPLACED LH INBD FLAP W.S. 24.0 FLAP VANE ACTUATOR PN: CC670-14300-9-01 IAW CRJ700 AMM 27-52-23-000/400-801 A01. CC670-14002-7Apr 17, 2025 · N508AE · Cndair CL6002C10SDR SWI2025F01153Cradle · gougedRIGHT INBD FLAP VANE ACTUATOR SYSTEM- CRADLE ASSEMBLY AT WS65.50 GOUGED. COMPLIED WITH REPAIR TO RT INBD FLAP VANE ACTUATOR SYSTEM- CRADLE ASSEMBLY AT WS65.50 REF REO 670-57-52-609 REV -- DATED 2025-05-16 AND SRM-51-21-16-001-001-A01. ALL CHECKS GOOD. COMPLApr 15, 2025 · N614SK · Cndair CL6002C10SDR SWI2025F01152Cradle · gougedLEFT INBD FLAP VANE ACTUATOR SYSTEM- CRADLE ASSEMBLY AT WS65.50 GOUGED. REPAIRED LT INBD FLAP VANE ACTUATOR SYSTEM, CRADLE ASSEMBLY AT WS65.50 IAW REO 670-57-52-608 REV -- DATE 2025-05-16 AND SRM 51-12-00-001-001 A01. COMPLIED WITH TASK 51-900-1002-SKY.Apr 15, 2025 · N614SK · Cndair CL6002C10SDR SWIA20250902003Cradle · gougedRIGHT INBD FLAP VANE ACTUATOR SYSTEM, CRADLE ASSEMBLY AT WS24.00 GOUGED. COMPLIED WITH REPAIR TO RH IB FLAP VANE CRADLE ASSY AT WS24 REF REO 670-57-52-609 REV -- AND SRM-51-21-16-001-001-A01. ALL CHECKS GOOD. COMPLIED WITH TASK CARD 51-900-1002-SKY.Apr 15, 2025 · N614SK · Cndair CL6002C10SDR SWI2025F00936Attach Angle · corrodedTHE RH MLG TIRE BURST PANEL 642AZ ATTACHMENT ANGLE IS CORRODED (C-CHECK RO 07/15/2025)INSTALLED NEW RH MLG TIRE BURST PANEL 642AZ ATTACHMENT ANGLE REF. DWG CC670-10320, REV -F, DATE: 2015-11-04 AND CRJ900 SRM 51-42-21-001-001-A01. COMPLETED SKYWEST TASK CAApr 15, 2025 · N802SK · Cndair CL6002D24
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