JASC 5710

Service difficulty reports · 4,456

Reports filed under 5710 · Wing Main, Frame 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 = '5710'
  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 CALA2025040703587Cap · wornL/W INB FIXED L/E FAIRING I/B OF # 1 PYLON END CAP DEEP WEAR MARKS. REMOVED AND REPLACED AT L/W INBD FIXED L/E INBD OF NO.1 PYLON AS PER B737-800 SRM 51-40-02-0G-0 AND DWG 116A4008.Apr 4, 2025 · N86534 · Boeing 737824SDR CALA2025040703586Cap · gougedR/W INB FIXED L/E FAIRING I/B PYLON # 2 END CAP DEEP GOUGES, REF AAR N/R 9948446 REMOVED AND REPLACED AT R/W INBD FIXED L/E INBD OF #2 PYLON AS PER B737-800 SRM 51-40-02-0G-0 AND DWG# 116A4008.Apr 4, 2025 · N86534 · Boeing 737824SDR SWAA2025042421441Angle · crackedRAISED FAULT TO DOCUMENT INSPECTION BUYOFF OF REPAIR AT RH A/C BAY STA 663 RBL 9' VAPOR BARRIER CLOSE OUT ANGLE CRACKED REF FAULT BARCODE# TTG8Q00ZD6K0 <[01] REMOVED AND REPLACED RH A/C BAY STA 663 RBL 9' VAPOR BARRIER CLOSE OUT ANGLE PER SRM 51-40-02 AND 57-1Apr 3, 2025 · N8688J · Boeing 7378H4SDR WRXR20250403002Structure · corrodedCORROSION UNDER PANEL 621AT IN FORWARD OUTBOARD CORNER AROUND FASTENER HOLE. WS45. REMOVED CORROSION TO AREA UNDER PANEL 621AT IN FORWARD OUTBOARD CORNER AROUND FASTENER HOLE AT WS45 AND CREATED GRID FOR NDT TO DETERMINE MATERIAL THICKNESS IAW CRJ 900 SRM 51-2Apr 3, 2025 · N638NN · Cndair CL6002D24SDR YENA2025040300363Structure · within limitsDURING HEAVY MAINTENANCE: CORROSION T/E OVERHANG BTW RIB 8 AND RIB 9 ON LH WING (CPCP FINDING); (RESOLVED ON W/O: 1381650 TASKCARD: NR-00004) REFERENCE AEROMAN NR 2025-221712.PERFORMED REWORK ON RIB 7A (WX 4013) PLUS 7.800 IN ON LH WING AND FOUND WITHIN THE ALApr 1, 2025 · N554JB · Airbus A320232SDR SWAA2025050554034Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE IRSS 216 AT LT WING 2025-232329 CORRECTED FAULT NAME: CRACK CORRUGATED PLATE TRAILING EDGE ORSS 216 AT LT WING<[01] REPLACED CORRUGATED PLATE TRAILING EDGE IRSS 216 AT LT WING IAW B737-700 SRM-51-40-02; SRM-51-10-02 ITEM 9 Mar 31, 2025 · N290WN · Boeing 7377H4SDR 9WGA20250428015Mount · corrodedPNL 513AT MOUNT FLANGE HAS SURFACE CORROSION.Mar 31, 2025 · N546JN · Doug MD11FSDR AALA202504020616Plate · wornAIRCRAFT IN BASE MAINTENANCE: LEFT WING SKIN LOWER SURFACE PYLON MOUNTING PLATE BETWEEN RIBS 7 AND 8 HAS ELONGATED / WORN SYSTEM TUBING FEED-THROUGH HOLES. REPLACED MOUNTING PLATE PER SRM 57-21-11-300-005.Mar 30, 2025 · N173US · Airbus A321211SDR SWAA2025033119417Panel · delaminatedLH WING OUTD FIXED TRAILING EDGE LOWER PANEL DENT WITH DELAMINATION 571DB (P/N 115A4710-201)<[01] REMOVED DAMAGE AND APPLIED 250DEG. REPAIR PER SRM 57-51-01-2R-1 AND SRM 51-70-05.;[02] REMOVED DAMAGE AND APPLIED 250DEG. PERMANENT REPAIR PER SRM 57-51-01-2R-1 AMar 29, 2025 · N8544Z · Boeing 7378H4SDR SWIA202506240328Structure · damagedTEMPORARY REPAIR OF THE RH & LH LOWER WING PLANK AT BL45.00 BETWEEN R/SPAR & STR 6 (C-CHECK RO 06/23/2025)PERFORMED TEMPORARY REPAIR OF THE RH AND LH LOWER WING PLANK AT BL45.00 BETWEEN R/SPAR AND STR 6. REF K- REO 601R-21-3893 REV -- DATED 2025-03-08. COMPLIMar 28, 2025 · N919EV · Cndair CL6002B19SDR SWAA2025033119087Plate · crackedLT WING; UPPER WING FIXED T/E PANEL STRUCTURE THAT SERRATED PLATE ATTES TO IS CRACKED; PANEL JUST O/B OF 551CT<[01] REPAIRED LEFT WING INBOARD FIXED TRAILING EDGE DEFLECTION CONTROL RIB UPPER TAB PER SRM 57-51-02-2R-3 REPAIR 3. THIS IS A PERMANENT REPAIR.;[02]Mar 28, 2025 · N7857B · Boeing 73779PSDR SWI2025F01166Beam · chafedRIGHT INBD FLAP VANE ACTUATOR BEAM AT WS65 (NO.2) IS CHAFED. REPAIRED RT INBD FLAP VANE ACTUATOR BEAM AT WS65 (NO.2) AND COMPLIED WITH ALL STEPS OF REO 670-57-52-257 REV - A DATED 2024-08-20. COMPLIED WITH TASK CARD 51-900-1002-SKY.Mar 21, 2025 · N614SK · Cndair CL6002C10SDR SWI2025F01165Beam · chafedRIGHT INBD FLAP VANE ACTUATOR BEAM AT WS24 (NO.1) IS CHAFED. REPAIRED RH IB FLAP VANE ACTUATOR BEAM AT WS24 (NO.1) AND COMPLIED WITH ALL STEPS OF REO 670-57-52-257 REV-A DATED 2024-08-20. COMPLIED WITH TASK CARD 51-900-1002-SKY.Mar 21, 2025 · N614SK · Cndair CL6002C10SDR SWI2025F01164Beam · chafedRIGHT INBD FLAP VANE ACTUATOR BEAM AT WS140 (NO.4) IS CHAFED. REPAIRED RT INBD FLAP VANE ACTUATOR BEAM AT WS140 (NR 4) AND COMPLIED WITH ALL STEPS REO 670-57-52-257 REV-A. COMPLIED WITH TASK CARD 51-900-1002-SKY..Mar 21, 2025 · N614SK · Cndair CL6002C10SDR SWIA2025090200014Beam · chafedRIGHT INBD FLAP VANE ACTUATOR BEAM AT WS102 (NO.3) IS CHAFED. REPAIRED RT INBD FLAP VANE ACTUATOR BEAM AT WS102 (NR 3) AND COMPLIED WITH ALL STEPS OF REO 670-57-52-257 REV - A. COMPLIED WITH TASK CARD 51-900-1002-SKY.Mar 21, 2025 · N614SK · Cndair CL6002C10SDR SWI2025F01181Beam · chafedLEFT INBOARD FLAP VANE ACTUATOR BEAM AT WS65.50 CHAFED. REPAIRED LH I/B FLAP VANE ACTUATOR BEAM AT WS65.50 IAW REO 670-57-52-257 REV -A DATE 2024-08-20. OPS TESTED GOOD. COMPLIED WITH TASK 51-900-1002-SKY.Mar 20, 2025 · N614SK · Cndair CL6002C10SDR SWI2025F01180Beam · chafedLEFT INBD FLAP VANE ACTUATOR BEAM AT WS140 CHAFED. REPAIRED LT INBD FLAP VANE ACTUATOR BEAM AT WS140 IAW REO 670-57-52-257 REV-A DATED: 2024-08-20 OPS TEST GOOD. COMPLIED WITH TASK 51-900-1002-SKY.Mar 20, 2025 · N614SK · Cndair CL6002C10SDR SWI2025F01179Beam · chafedLH IB FLAP VANE ACTUATOR BEAM AT WS102 CHAFED. REPAIRED LH I/B FLAP VANE ACTUATOR AT WS102 REF-CRJ-700 REO 670-57-52-257 REV -B DATE 2024-08-20. SEE CONTINUATION CARD FOR DETAILS. OPS TEST GOOD.COMPLIED WITH TASK 51-900-1002-SKYMar 20, 2025 · N614SK · Cndair CL6002C10SDR SWIA202509020025Beam · chafedLEFT INBOARD FLAP VANE ACTUATOR BEAM AT WS24.00 CHAFED. REPAIRED LT INBOARD FLAP VANE ACTUATOR BEAM AT WS24.00 IAW REO 670-57-52-257 REV-A. OPS TEST GOOD. COMPLIED WITH TASK CARD 51-900-1002-SKY.Mar 20, 2025 · N614SK · Cndair CL6002C10SDR SWAA2025042407806Angle · crackedRH A/C BAY STA 663 RBL 9' VAPOR BARRIER CLOSE OUT ANGLE CRACKED <[01] RH A/C BAY STA 663 VAPOR BARRIER CLOSE OUT ANGLE HAS ADDITIONAL CRACK DAMAGE AT RBL31. ANGLE REQUIRES REPLACEMENT REFERENCE SRM 57-10-10-2R-5.;[02] BEGAN REMOVING FASTENERS PER SRM 51-40-02.Mar 20, 2025 · N8688J · Boeing 7378H4SDR SWAA2025042407792Angle · crackedLH A/C BAY STA 663 LBL 9' VAPOR BARRIER CLOSE OUT ANGLE CRACKED <[01]. LH A/C BAY STA 663 VAPOR BARRIER CLOSE OUT ANGLE HAS ADDITIONAL CRACK DAMAGE AT LBL42. ANGLE REQUIRES REPLACEMENT REFERENCE SRM 57-10-10-2R-5.; [02] BEGAN REMOVAL OF FASTENERS PER SRM 51-4Mar 20, 2025 · N8688J · Boeing 7378H4SDR AALA202504018365Panel · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND WING LOWER TRANSLATE PANEL JUST INBOARD OF PYLON INBOARD FORWARD SUPPORT ROD HAS PLAY AT LOWER ATTACH POINT TO PANEL. REMOVED AND INSTALLED NEW SUPPORT ROD SUPPORT BEAM AT RIGHT HAND WING LOWER TRANSLATE PANEL JUST INBOMar 20, 2025 · N844NN · Boeing 737823SDR AALA202504018797Support Angle · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND WING LOWER TRANSLATE PANEL JUST INBOARD OF PYLON MIDDLE AFT SUPPORT ROD HAS PLAY AT LOWER ATTACH POINT TO PANEL. REMOVED AND INSTALLED NEW ANGLE SUPPORT BEAM AT RIGHT HAND WING LOWER TEPANEL JUST INBOARD OF PYLON MIDDLEMar 20, 2025 · N844NN · Boeing 737823SDR IXXA20250424005Beam · crackedRIGHT WING LEADING EDGE BULL NOSE BEAM IS CRACKED AT OSS 664.58. REF HAECO WO 320011 NR 35285Mar 19, 2025 · N229AZ · Boeing 767323SDR VNAA20250320014Link · corrodedHN00204547 SN: 00683DISCREPANCY:WHILE REPLACING THE LH AILERON FLUTTER DAMPER LINK SHEAR PIN FOUND THE LINK TO BE INTERNALLY CORRODED, AND, FROZEN. REQUIRES REPLACEMENTCORRECTIVE ACTION: FWD HALF OF NEW SERVICEABLE LINK PART NO.600-10177-7 AND AFT HALF PART NOMar 19, 2025 · N509AE · Cndair CL6002C10SDR AALA202505196170Plate · wornAIRCRAFT IN BASE MAINTENANCE: LEFT WING TRAILING EDGE PANEL #3 LOWER SURFACE PYLON MOUNTING PLATE SYSTEM FEED THRU HOLES WORN BETWEEN RIB 7 AND RIB 8. REPLACED MOUNTING PLATE PER SRM 57-21-11-300-005.Mar 18, 2025 · N176UW · Airbus A321211SDR SWIA202507170317Beam · gougedLH INBD FLAP MIDDLE FLAP VANE ACTUATOR BEAM IS GOUGED. (MARKED) (C-CHECK RO 07/16/2025)COMPLIED WITH REO 670-57-52-257 REV A DATE 2024-08-20 OPS CHECKS GOOD. COMPLIED WITH TASK CARD 51-900-1002-SKYMar 17, 2025 · N805SK · Cndair CL6002D24SDR UIEA2025031000251Support · corrodedRIGHT WING TRAILING EDGE INBOARD FLAP #5 SUPPORT MECHANISM 6-6 OUTER PIN WITH SEVERAL CORROSION IN THE INNER BORE.(<P>RIGHT WING TRAILING EDGE INBOARD FLAP #5 SUPPORT MECHANISM 6-6 OUTER PIN WAS REPLACED IAW AMM TASK 27-51-04-402-135 REV 144. NO FUTHER DEFECTSMar 15, 2025 · N1373A · Boeing 76731KSDR NACA2025031400001Former · crackedCRACK- FORMER R/H WING OUTBD L/E CAVITY CURTAUN SUPPORT BRACKEWT OSS 565.Mar 14, 2025 · N321CM · Boeing 767323SDR SWAA2025031705359Bulkhead · crackedL/H WHEEL WELL FWD BULKHEAD; CRACKED BEHIND THE HYDRAULIC SYSTEM A PRESSURE MODULE. <[01] C/W WITH SRM 57-10-10-2R-2.; [02] C/W WITH SRM 57-10-10-2R-2 PAR. 6.; [03] PERFORMED REVIEW OF THIS FAULT IAW SRM 57-10-10-2R-2 PAR. 6.Mar 14, 2025 · N284WN · Boeing 7377H4SDR SWIA20250808313Structure · crackedRH WING SLAT #1, #3 SLAT TRACK BOX CRACKED. (C-CHECK RO 05/08/2025)PERFORMED REPAIR ON R/H WING SLAT # 1, # 3 SLAT TRACK BOX PER BOMBARDIER REO 670-57-42-577. REV. --. DATE: 2016-12-02. NDT PERFORMED BY BARON NDT,LLC FAA CRS# 5NDR545D. REPORT # S040125-3. P.O.Mar 13, 2025 · N604SK · Cndair CL6002C10SDR NACA2025031300003Beam · crackedCRACKED BEAM , LOWER SIDE OF L/H WING OUTBD L/E NOSE BEAM , OSS 679.82.Mar 13, 2025 · N321CM · Boeing 767323SDR NACA2025031100006Former · crackedCRACK - FORMER, FWD SIDE OF L/H WING OUTBD L/E NOSE BEAM, OSS 648.6.Mar 11, 2025 · N321CM · Boeing 767323SDR NACA2025031100003Seal · tornRH WING O/B EXHAUST GATE I/B UPPER AND LOWER SEALS TORN. REMOVE RH WING O/B EXHAUST GATE I/B UPPER AND LOWER SEAL. INSTALL NEW SEAL REF BOEING 733 AMM 20-50-11 PAGE 201 R100 PME: 005184 DUE DATE: 26 MAR 2025Mar 11, 2025 · N304KH · Boeing 7373Q8SDR FDEA202503080444Plate · looseLH WING I/B FLAP INTERNAL STRUCTURE WAS FOUND 1EA FASTENER HOLE ENLARGED AT RIB25A RS PLUS 5" FABRICATED WEB AND INSTALLED WITH FASTENERS AT LH I/B FLAP RIB25A RS PLUS 5" I.A.W AIRBUS DRAWING NO:A57960114 REV E SHEET 1 & A300-600 SRM 51-40-21-001, PARA7 PMar 8, 2025 · N727FD · Airbus A300F4622RSDR SWAA2025040702889Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE ORSS 297 AT LT WING 2025-172114<[01] REPLACED CORRUGATED PLATE TRAILING EDGE ORSS 297 AT LT WING IAW B737-800 SRM 51-40-02; SRM 51-10-02 AND DWG: 115A3700 SHEET: 71 REV: - .<BR><BR>LENGTH OF CRACK: 0.900 IN <BR>TOOL USED: EMar 7, 2025 · N8614M · Boeing 7378H4SDR SWAA2025040715141Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE ORSS 297 AT LT WING 2025-172114<[01] REPLACED CORRUGATED PLATE TRAILING EDGE ORSS 297 AT LT WING IAW B737-800 SRM 51-40-02; SRM 51-10-02 AND DWG: 115A3700 SHEET: 71 REV: - .<BR><BR>LENGTH OF CRACK: 0.900 IN <BR>TOOL USED: EMar 7, 2025 · N8614M · Boeing 7378H4SDR IPXA2025032415971Beam · crackedLOWER CHORD CRACK OF R/H WING T/E BEAM ASSY AT NO. 7 SPOILER. AREA , WBL 296 AND WBL 303. (REPAIR). REPAIR DAMAGE AREA I.A.W. UPS EO-93195-REQ1 REV.1 JOB COMPLETED.Mar 7, 2025 · N579UP · Boeing 74745ESDR IPXA2025032415924Beam · crackedLOWER CHORD CRACK OF R/H WING T/E BEAM ASSY AT NO. 8 SPOILER. AREA , WBL 382 AND WBL 389. (REPAIR). REPAIR DAMAGE AREA I.A.W. UPS EO-93212-REQ1 REV.1Mar 7, 2025 · N579UP · Boeing 74745ESDR SWAA2025032002743Panel · crackedPANEL 621PB CRACKED AT FWD I/B END. <[01] CRACK AT FWD I/B END OF PANEL 621PB WAS REPAIRED IAW SRM 51-70-05-2R-6.; [02] VERIFIED CORRECTIVE ACTION #1.Mar 7, 2025 · N289CT · Boeing 7377H4SDR SWAA2025031002775Vapor Barrier · crackedCRACK IN RIGHT WHEEL WELL VAPOR BARRIER OF 11 INCHES AT STATION RBL 32.0 TO RBL 54.0 <[01] 01. - REMOVED AND REPLACED PER [SRM 57-10-10-1A-2-A00592 (CRACK - STOP DRILL AND SEAL - DVI EVERY 1200 CYC - INTERIM REPAIR)].Mar 7, 2025 · N256WN · Boeing 7377H4SDR VNAA202503070037Canister · crackedCRACK IN CANISTER WELDED NO.3, ON WS148.01 OF INTERNAL RH MAIN FUEL TANK. CANISTER WELDED NO.3, ON WS148.01 OF INTERNAL RH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577. REV.--.."Mar 7, 2025 · N594NN · Cndair CL6002D24SDR VNAA202503070035Canister · crackedCRACK IN CANISTER WELDED NO.3 IN STA. WS148 OF INTERNAL LH MAIN FUEL TANK. CANISTER WELDED NO.3 IN STA. WS148 OF INTERNAL LH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577. REV-.Mar 7, 2025 · N594NN · Cndair CL6002D24SDR CALA2025031302767Fuel Panel · damagedLEFT WING LOWER FUEL PANEL LAND 540JB HAS IRREGULAR HOLE. ACCOMPLISHED REPAIR OF IRREGULAR HOLE#595 ON FUEL PANEL LAND 540 JB IAW SRM 57-21-11-300-002. REAMED AND COLD WORKED HOLE. FABRIC ATED AND INSTALLED BUSHING OD=.4054IN. FABRICATED AND INSTALLED BRIDGINMar 6, 2025 · N434UA · Airbus A320232SDR IPXA2025032656563Structure · crackedFAULT: CRACK FOUND IN MIDDLE HOLE ON FR40 RH UPPER TENSION FAST. REPAIR PER A300-600F SRM REV 41 CHAP 57-10-24-201 PARA 5.A, FIG 202 AND FIG 206 SHEET 2 (REPAIR WITH BUSH).UPS CONSIDERS THIS A MINOR REPAIR PER GMM 05.04. CAUTION:THE WORK INSTRUCTIONS CONTAINEDMar 4, 2025 · N121UP · Airbus A300F4622RSDR IPXA2025032657484Angle · brokenRH/WING, DEFLECTOR PANEL 672AB, METAL FINGER BROKEN DOT-008 DD5240. REPLACED ANGLE-CONDUCTOR AT RH/WING, DEFLECTOR PANEL 672AB IAW A300-600F SRM 51-40-21. REQUEST OK TO PERFORM BONDING TEST.Mar 4, 2025 · N121UP · Airbus A300F4622RSDR IPXA2025032660192Panel · brokenRH/WING, DEFLECTOR PANEL 672CB, METAL FINGERS BROKEN DOT-009 DD5240. REPLACED ANGLE-CONDUCTOR AT RH WING, DEFLECTOR PANEL 672 CB IAW SRM 51-40-21. REQUEST OK TO PERFORM BONDING TEST.Mar 4, 2025 · N121UP · Airbus A300F4622RSDR SWAA2025032602006Rib · damagedR WING DEFLECTION CONTROL RIB HAS 2EA ELONGATED FASTENER HOLE ON ATTACHMENT TAB.(MARKED)<[01] WEAR DAMAGE ON RIGHT WING I/B FIXED T/E DEFLECTION CONTROL RIB UPPER TAB IS OUT OF LIMITS PER SRM 53-51-02-1A-1. CUT AND REMOVED THE DAMAGED PART OF THE DEFLECTION COMar 4, 2025 · N8689C · Boeing 7378H4SDR SWAA2025032605765Plate · wornLEFT WING I/B FIXED TRAILING EDGE UPPER PANEL TO DEFLECTION RIB WORN AT SERRATED PLATE<[01] LEFT WING I/B FIXED TRAILING EDGE UPPER PANEL TO DEFLECTION RIB TAB FASTENER HOLES WORN DOWN 0.090?; TAB THICKNESS IS 0.100?. TAB IS OUT OF LIMITS PER SRM 57-51-02-1A-1Mar 4, 2025 · N8689C · Boeing 7378H4SDR SWIA202503190004Structure · ground damageTRANSFER FROM EAML 1548503 : TUG WITH NO DRIVER ROLLED ACROSS RAMP AND IMPACTED RIGHT WING DURING BOARDING. LARGE DENT IN LEADING EDGE. (FILED CLOSED - FLIGHT 5449) REMOVED AND REPLACED RIGHT WING LEADING EDGE ASSEMBLY 620JL WITH REFERENCE TO AMM 57-41-0Mar 4, 2025 · N856AS · Cndair CL6002B19
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