JASC 5751

Service difficulty reports · 5,081

Reports filed under 5751 · Ailerons, 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 = '5751'
  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 N6WA2026051506Switch · lack of lubeCONFIG AIL WARNING MSG ON TAKE-OFF. CLEANED AND LUBRICATED AIL TRIM SWITCH IAW AMM-27-12-10. OP CHECKS GOOD. AIRCRAFT OK FOR SERVICE.May 12, 2026 · N577GJ · Cndair CL6002C11SDR REXA2026052600607Bushing · damagedFOUND RT AILERON SIDE LUG LABELED -C- TO BE ABOVE 4TH OVER PER GREO 670-57-61-237 BY 0.0225, COMPLIED WITH REPAIR OF BUSHING LUG MARKED C IAW MHIRJ REO 690-57-61-518 REV -- DATED 2026-05-22.May 11, 2026 · N691CA · Cndair CL6002D24SDR SWAA2026061197111Rod End · corrodedTHE RIGHT WING AILERON TAB ATTACH (HINGE) ROD ENDS ALL HAVE EVIDENCE OF EXTERNAL SURFACE CORROSION.. REMOVED RT AILERON TRIM TAB PER AMM 27-11-21. R & R RIGHT WING AILERON TAB ATTACH ROD ENDS IAW CMM 57-50-26. REINSTALLED RT AILERON TRIM TAB IAW AMM 27-11-May 9, 2026 · N8540V · Boeing 7378H4SDR REXA2026060400903Hinge · corrodedAFTER RH AILERON BUSHINGS REMOVAL, CORROSION AND WEAR WAS FOUND ON LUG BORE ON AIL STA 336.4015 ( LUG R1), 337.657 (LUG R2), 338.424 (LUG R3), 342.911 (LUG R5) AND 344.1665 (LUG R6) LUG BORE ON AIL STA 336.4015 ( LUG R1), AND 338.424 (LUG R3) WERE CLEANED PER May 8, 2026 · N909XJ · Cndair CL6002D24SDR FDEA202605080570Skin · damagedLH OUTBOARD AILERON TRAILING EDGE HAS DAMAGE, MARKED WITH TAPE. REPAIRED DAMAGE ON L/H O/B AILERON AT WS 796.26 IN REF TO B757 SRM 57-60-01-2R FIG 201 SH 2 AND B757 SRM 51-70-05-0G FIG 5. CALCULATED NEW BALANCE MOMENT FOR L/H O/B AILERON TO BE -12.30 POUNDMay 8, 2026 · N939FD · Boeing 75723ASDR CALA2026051116132Skin · contaminatedPERFORMING THERMOGRAFIC INSPECTION ON THE LH WING OTBD AILERON IT WAS NOTICED MOISTURE INGRESSION INDICATION IN TWO POINTS OF THE AILERON, ONE AT THE INBD END OF THE AILERON AND ANOTHER ABOUT 15 INCHES FROM OF THE OTBD END. ALL THE STEPS WERE ACCOMPLISHED WITMay 8, 2026 · N649UA · Boeing 767322SDR REXA2026070301058Fitting · corrodedCORROSION AND WEAR WAS FOUND ON LUG BORE ON AIL STA .336.4015 (LUG L1) AND 337.657 (LUG L2) AT LH AILERON. LUG BORE L 1=(STA=336.4015), L2=(STA=337.657), L5=(STA=342.911) & L6=(STA=344.1665) ON CENTTER FITTING AT LH AILERON WERE REPAIRED PER REO 670-57-61-237 May 7, 2026 · N927XJ · Cndair CL6002D24SDR REXA2026070301057Lug · corrodedCORROSION AND WEAR WAS FOUND ON LUG BORE ON AIL STA 336.4015 (LUG R1), 337.657 (LUG R2), 342.123 (LUG R4), 342.911 (LUG R5), 344.1665 (LUG R6) AND CORROSION ON LUG FACE ON AIL STA 337.657 (LUG R2) AT RH AILERON LUG BORE STA 336.4015 (LUG R1), STA 337.657 (LUG May 5, 2026 · N927XJ · Cndair CL6002D24SDR 1Q2R2026070100004Aileron · nickedTEMPORARY TO PERMANENT REPAIR (TRFKE00BS7ND) TO LEFT-HAND AILERON ASSEMBLY. REPAIR PERFORMED IAW REO 670-57-61-484 REV--.May 4, 2026 · N545PB · Cndair CL6002C10SDR SWIA2026041277775Skin · chafedLEFT AILERON LEADING EDGE SKIN CHAFED AT MULTIPLE SPOTS. INSTALLED NEW LEADING EDGE SKIN IAW DWG CC670-13000, REV D, SRM 51-42-06, SRM 51-42-21, AND SRM 51-42-22.Apr 12, 2026 · N917SW · Cndair CL6002B19SDR DALA2026041302314Hinge Pin · corrodedCORROSION PINS HINGE AILERON ON LH AND RH WING (6E/A). OBTAINED PINS HINGE AILERON ON LH AND RH WING (6E/A) AS PER AIPC 27-14-05-31A AND AIPC 27-14-05-32. THE INSTALLATION IS TO BE ACCOMPLISHED ON AMDS CARD 5760-1010S-LT AND AMDS CARD 5760- 1010S-RT. RII INSPApr 10, 2026 · N336NW · Airbus A320212SDR VNAA202606120058Lug · corrodedSCRATCH FOUND ON LT AILERON HINGE LUG BORE L5 INNER AREA 6. SCRATCH ON LUG BORE L5 AT CENTER FITTING ON LT AILERON WAS REPAIRED PERREO 670-57-61-237 REV-.Apr 7, 2026 · N649NN · Cndair CL6002D24SDR VNAA202606120057Lug · corrodedDAMAGE FOUND LH AILERON CENTRAL HINGES LUG BORES L1, L2 AND L6. LUGS BORE L1, L2 & L6 AT CENTER FITTING AT LH AILERON WERE REPAIRED PERREO 670-57-61-237 REV--.Apr 7, 2026 · N649NN · Cndair CL6002D24SDR VNAA202604010023Spar · damagedFOUND RH AILERON WING AFT SPAR MOST I/B BUSHING LUG BORE TO BE PREVIOUSLY OVERSIZED. CORRECTIVE ACTION: PERFORMED REPAIR BY COMPLYING WITH MHIRJ REO 670-57-51-632, REV -- DATED 2025-08-29 - REPAIR FOR DAMAGE TO BORE OF RH AILERON HINGE FITTING NO 1, INBD LUG, Apr 1, 2026 · N500AE · Cndair CL6002C10SDR VNAA2026040950046Skin · chafedTEMP TO PERM DISPOSITION FOR BLENDED CHAFE DAMAGE TO THE LH IBD TRAILING EDGE LOWER SKIN PANEL EDGE MEMEBER.Mar 30, 2026 · N516AE · Cndair CL6002D24SDR REXA2026040800280Hinge · damagedRH AILERON CENTER HINGE FITTING FOUND ALL 4 PCU LUGS MARKED B, C, F AND G BUSHINGS TO BE O/S UPON REMOVAL. REPAIRED RH AILERON CENTER LUGS IAW MHIRJ REO 690-57-61-503 REV -- DATED 2026-03-19 AND BOMBARDIER REO 670-57-61-107 REV B DATED 2019-01-14. AILERON P/N Mar 30, 2026 · N920XJ · Cndair CL6002D24SDR REXA2026042300319Lug · corrodedCORROSION ON CENTER FITTING LUG L1, L2, L3, L4, L5, L6 AT AILERON WAS FOUND. LUGS BORE L3 & L4 AT CENTER FITTING OF LH AILERON WERE CLEANED PER CRJ 900 SRM 51-26-00-001-001-A01 AND LUGS BORE L1, L2, L5 & L6 WAS REPAIRED PER REO 670-57-61-107 REV:-BMar 29, 2026 · N913XJ · Cndair CL6002D24SDR REXA2026042300318Lug · corrodedCORROSION WAS FOUND ON LUG BORE R2, R5 AND SCRATCHES ON BORE LUG R4(CENTER FITTING) AT RH AILERON. LUG BORE R4 AT CENTTER FITTING WAS CLEANED PER CRJ 900 SRM 51-26-00-001-001-A01 AND LUG BORE R2 AND R5 WERE REPAIRED PER REO 690-57-61-237 REV:-- & REO 690-57-61Mar 29, 2026 · N913XJ · Cndair CL6002D24SDR REXA2026080301386Fitting · damagedBUSHINGS IN AILERON LH, OVERSIZED WAS FOUND ON INBD LUG BORE TO WING TRAILING EDGE AILERON HINGE FITTING #1 AT WS294.50, LHS FOR OVERSIZED LUG BORE TO WING TRAILING EDGE AILERON HINGE FITTING #1 ASSEMBLY AT WS294.50, LHS WAS REPAIRED PER REO 670-57-51-697 REV Mar 26, 2026 · N398CA · Cndair CL6002C10SDR UATA2026032602701Rivet · shearedFLIGHT CONTROL STUCK FULL LEFT AILERON. REPLACED SHEARED RIVETS FROM AILERON TO AILERON POSITION INDICATING HORN USING MS20470AD RIVETS WITH REFERENCE TO SAAB 340 MM SRM 51-40-21-001 AND 40-30-001B.Mar 25, 2026 · N906RA · Saab SF340ASDR SWIA2026032476345Skin · gougedLEFT AILERON LEADING EDGE GOUGED AND CHAFED IN MULTIPLE LOCATIONS. REPLACED THE LH AILERON LEADING EDGE SKIN IAW DWG CC670-13000, REV-D, SRM 51-42-06, SRM 51-42-21, AND SRM 51-42-22. COMPLIED WITH TASK CARD 51-900-1003-SKY.Mar 24, 2026 · N951SW · Cndair CL6002B19SDR SWIA2026032476342Skin · gougedRIGHT AILERON LEADING EDGE GOUGED AND CHAFED IN MULTIPLE LOCATIONS. REPLACED RT AILERON LEADING EDGE SKIN IAW DWG 601R13031, REV-K , SRM 51-42-06 AND SRM 51-42-13. COMPLIED WITH TASK CARD 51-900-1003-SKY.Mar 24, 2026 · N951SW · Cndair CL6002B19SDR CALA2026032614838Skin · contaminatedLH O/B AILERON LOWER FOUND WATER INGRESSION AT 2ND STATIC DISCHARGER (COUNT FROM I/B), REF. NON-ROUTINE HX NRC WO.6307705 AND ORIGINATED BY EMP NO. V906014 LH OTBD AILERON, WATER CONTAMINATED LHW O/B AILERON LWR SURFACE WATER INGRESSION AREA PERFORMED COMPOSMar 24, 2026 · N654UA · Boeing 767322SDR VNAA20260501016Lug · corrodedAFTER BUSHINGS REMOVAL CORROSION WAS FOUND ON INTERNAL FACE LUGS R1, R2, R3, R4, R5 AND R6 AT CENTER FITTING RH AILERONON. LUGS R3, R4 AND R6 AT CENTER FITTING RH AILERON WERE CLEANED PER CRJ 900 SRM 51-26-00-001-001-A01 AND LUGS R1, R2 AND R5 WERE REPAIRED PMar 22, 2026 · N617NN · Bombdr CL6002D15SDR DALA2026032301945Cover · missing(LOG 8430280) ON WALKAROUND FOUND RIGHT AILERON PCU AERODYNAMIC COVER MISSING. RIGHT AILERON PCU AERODYNAMIC COVER / REMOVABLE FAIRING FOR TRIM ACT. INSTALLED PER B737 IPC 27-11-11-02.Mar 19, 2026 · N924DZ · Boeing 737932ERSDR REXA2026050500490Hinge · corrodedSECONDARY NRC IN REF TO RC 900-27-900-910: CORROSION ON LUG BORES L5 AND L6 IN CENTER FITTING AT LEFT AILERON. LUG BORES L5, L6 AND L1 IN CENTER FITTING AT LEFT AILERON WERE REPAIRED PER REO 670-57-61-237 REV -- & REO 690-57-61-511 REV - AMar 17, 2026 · N279PQ · Cndair CL6002D24SDR REXA2026080501496Hinge Fitting · corrodedAFTER BUSHING AND BEARINGS REMOVAL FOUND CORROSION IN LUG L2 & L5 AT CENTER HINGE FITTING OF FRONT SPAR IN LT AILERON LUG L2 & L5 AT CENTER HINGE FITTING OF FRONT SPAR IN LT AILERON WERE REPAIRED PER REO 670-57-61-107 REV. -B.Mar 12, 2026 · N676CA · Cndair CL6002D24SDR REXA2026080501491Hinge Fitting · corrodedCORROSION IN LUG R2 & R5 AT CENTER HINGE FITTING OF FRONT SPAR IN RH AILERON CORROSION AT CENTER FITTING IN LUGS R2 & R5 WERE REMOVED PER REO 670-57-61-107 REV.-B, REO 690-57-61-504 REV-- AND CRJ 900 SRM 51-26-00-001-001-A01 CLEANING, DEFERRAL NUMBERS WO W907Mar 12, 2026 · N676CA · Cndair CL6002D24SDR REXA2026033000275Intercostal · corrodedFOUND AREAS OF POSSIBLE CORROSION INSIDE OF RH AILERON AT WS 294.50 & 319.50 REMOVED SERVICEABLE RT AILERON LOWER SKIN IAW SRM 51-42-13-001-001-A01, SRM 51-42-22-001-001-A01 & SRM 51-42-21-001-001-A01. AFTER REMOVAL OF RT AILERON LOWER SKIN, PERFORMED A DETMar 10, 2026 · N920XJ · Cndair CL6002D24SDR CALA2026030914445Skin · contaminatedLEFT WING OTBD AILERON DAMAGED. WATER INGRESS AT LOWER SURFACE OF LT LOWER SURFACE OF OTBD AILERON LT WING, PERFORMED COMPOSITE REPAIR IAW SRM 51-70-17 PAR. 4.A.(1).Mar 8, 2026 · N643UA · Boeing 767322SDR VNAA202604110022Hinge · corrodedAFTER REMOVAL OF BUSHING WEAR ON LUG R5 WAS FOUND AT RH AILERON. LUG R5 AT RH AILERON WAS REPAIRED PER REO 670-57-61-237 REV --Mar 7, 2026 · N603NN · Cndair CL6002D24SDR VNAA202604110021Hinge · corrodedAFTER REMOVAL OF BUSHING CORROSION ON LUG R2 WAS FOUND AT RH AILERON. LUG R2 AT RH AILERON WAS REPAIRED PER REO 670-57-61-237 REV --Mar 7, 2026 · N603NN · Cndair CL6002D24SDR SWIA2026030575961Hinge · damagedRIGHT AILERON HINGE NR 3 INBD BUSHING HOUSING BORE IS DAMAGED. REMOVED AND REPLACED RT AILERON NR 3 HINGE ASSY IAW SRM 51-42-21. COMPLIED WITH TASK CARD 51-900-1003-SKY.Mar 5, 2026 · N915SW · Cndair CL6002B19SDR SWIA2026030575960Hinge · damagedRIGHT AILERON HINGE NR2 IB BUSHING HOUSING BORE IS DAMAGED. REAMED THE TRAILING EDGE RT NR 2 AILERON HINGE LUGS TO FOURTH OVERSIZE AND INSTALLED THE BUSHINGS IN REFERENCE TO REO 601R-57-51-015, REV NC, COMPLIED WITH TASK CARD 51-900-1003-SKY.Mar 5, 2026 · N915SW · Cndair CL6002B19SDR SWIA2026022775939Shroud · chafedRIGHT AILERON UPPER LEADING EDGE CHAFED. REMOVED AND REPLACED RT AILERON UPPER LEADING EDGE SKIN SHROUD WITH NEW SKIN SHROUD IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, SRM 51-42-22-001-001-A01 & DWG CC670-13000, REV D.Feb 27, 2026 · N732SK · Cndair CL6002C10SDR REXA2026030900233Bushing · abnormalRH AILERON BUSHING LUGS MARKED C AND F FOUND TO BE OVERSIZED UPON BUSHING REMOVAL COMPLIED WITH STEPS F7- F13 AND G IAW REO 670-57-61-237 REV -- 2017-07-25Feb 27, 2026 · N917XJ · Cndair CL6002D24SDR REXA2026030900232Bushing · abnormalLH AILERON BUSHING LUGS MARKED C AND F FOUND TO BE OVERSIZED UPON BUSHING REMOVAL. FABRICATED 2EA O/S BUSHINGS AS REQUIRED USING AMS5659 15-5PH H1000 PO# CP00009965/9662 IAW STEP F.7 OF BOMBARDIER REO 670-57-61-237 REV -- DATED 2017-07-25. C/W LPI ON LH AILEROFeb 27, 2026 · N917XJ · Cndair CL6002D24SDR AALA202603277964Support Frame · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY AILERON HINGE SUPPORT FRAME #1 ON RH WING. MAINTENANCE REPLACED AILERON HINGE SUPPORT FRAME #1 ON RH WING IAW AMM 57-51-31-000-001-A AND 57-51-31-400-001-A.Feb 26, 2026 · N126UW · Airbus A320214SDR AALA202603277596Support Frame · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY AILERON HINGE SUPPORT FRAME #2 ON RH WING. MAINTENANCE REPLACED AILERON HINGE SUPPORT FRAME #2 ON RH WING IAW AMM 57-51-31-000-001-A AND 57-51-31-400-001-A.Feb 26, 2026 · N126UW · Airbus A320214SDR AALA202603278471Support Frame · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY AILERON HINGE SUPPORT FRAME #3 ON RH WING. MAINTENANCE REPLACED AILERON HINGE SUPPORT FRAME #3 ON RH WING IAW AMM 57-51-31-000-001-A AND AMM 57-51-31-400-001-A.Feb 26, 2026 · N126UW · Airbus A320214SDR CALA2026030314279Aileron · damagedIT WILL BE NECESSARY TO REPAIR THE OUTBOARD AILERON LH AS PER AMM TASK 03-57-60-280-801 PARAGRAPH 2.F(7)(A). CREATED SFR, IT IS NECESSARY QC CHECK AND APPROVAL. ESFR #3049 WAS CHECKED AND APPROVED BY QC. ALL STEPS OF THE ECRA 5760-01139 WERE EXECUTED WITHOUT DFeb 25, 2026 · N69059 · Boeing 767424ERSDR CALA2026030314265Aileron · damagedIT WILL BE NECESSARY TO REPAIR THE RT OTBD AILERON IAW AMM TASK 03-57-60-280-801, PARAGRAPH 2.F(7)(A). PROVIDE DETAILS ABOUT THE REPAIR ACTIONS IT WAS ACCOMPLISHED THERMOGRAPHY INSPECTION ON RT OTBD AILERON IAW NDT MANUAL PART 9 51-00-01. AFTER DAMAGE REMOVALFeb 25, 2026 · N69059 · Boeing 767424ERSDR 2026FA0000144Hinge · detachedAFTER LANDING AND SECURING THE AIRCRAFT, IT WAS OBSERVED THAT THE LEFT AILERON WAS HANGING DOWNWARD FROM THE WING AND WAS NO LONGER PROPERLY ATTACHED ALONG ITS NORMAL HINGE LINEFeb 19, 2026 · N964GV · Tecnam P2006TSDR ASAA2026021964503Skin · nickedLEFT WING AILERON BOTTOM SKIN HAS 4 NICKS ON INBOARD SIDE. SRXR430X. GROUNDED - YES. ACCOMPLISHED A PERMANENT REPAIR ON L/H WING AILERON LOWER SKIN LOCATED AT 27" I/B END 7.5" AFT T/E, REPAIR PATCH IS 5" DIA IAW B737-9 SRM 57-60-01-2R-1 REPAIR 1 TABLE 202. RV Feb 19, 2026 · N710AL · Boeing 7379SDR FDEA202602100163Skin · dentedDENT ON SKIN OF THE OUTBOARD AILERON AT WBL 879 FRON 11" OF TRAILING EDGE, LH WING LH WING OUTBOARD AILERON OF T/E AREA WAS REPAIRED IAW B767 SRM 57-60-02-2R REPAIR 1, FIG 201, SHEET 1 & 2, DETAIL II AND SRM 51-70-03-0G PAR 5L, FIG 16 REV 93 AUG 15/2025.Feb 10, 2026 · N160FE · Boeing 7673S2FSDR VNAA202602090008Panel · chafedFOUND PANEL 699AB TO BE CHAFED, CC670-13000, SHROUD AILERON,Feb 10, 2026 · N510AE · Cndair CL6002C10SDR VNAA202602090007Panel · chafedFOUND PANEL 699CB TO BE CHAFED, CC670-13000, CHAFED, SHROUD AILERONFeb 10, 2026 · N510AE · Cndair CL6002C10SDR VNAA20260328007Hinge Fitting · corrodedCORROSION IN THE INNER AREA OF THE BORE LUGS AT AILERON FITTING 1, CENTRAL FITTING (L1, L2, L3, L4, L5, L6) AND FITTING 4 (UPPER AND LOWER) OF LH WING AILERON. BORE LUGS HINGE FITTING NO. 1 & 4 (LOWER) , CENTER HINGE FITTING BORE LUGS L1, L3, L4, L6 WERE CLEAFeb 8, 2026 · N542EA · Bombdr CL6002D15SDR IPXA2026031399855Skin · corrodedCORROSION, R/H WING OUTBD AILERON TE LOWER SURFACE AROUND DISCHARGER BASE, NR 1 FROM THE INBD (AGING INSPECTION) (NO.5862)(REPAIR) IAW AMM 20-51-01-912-008 REV.115 INSTALL R/H WING OUTBD AILERON TE LOWER PANEL P/N:65B02152-2 AND CONDITION CHECK NORMAL.Feb 8, 2026 · N581UP · Boeing 7474R7FSDR IPXA2026022499855Skin · corroded***SDR FILED OPEN*** FAULT-CORROSION, R/H WING OUTBD AILERON TE LOWER SURFACE AROUND DISCHARGER BASE, #1 FROM THE INBD (AGING INSPECTION) (NO.5862)(REPAIR) I.A.W AMM 20-51-01-912-008 REV.115 INSTALL R/H WING OUTBD AILERON TE LOWER PANEL P/N:65802152-2 AND CONDFeb 8, 2026 · N581UP · Boeing 7474R7F
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