JASC 5751

Service difficulty reports · 5,082

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 GLBA96090Aileron · damagedORD -CREW FOUND DAMAGE ON TRAILING EDGE OF LEFT AILERON DURING WALK AROUND INSPECTION. MAINTENANCE REMOVED AND REPLACED LEFT AILERON. FLIGHT TEST WAS GOOD. (M)May 12, 1996 · N122GL · Beech 1900CSDR UPS96220588Spar Web · crackedINSPECTION TYPE-C, LT O/B AILERON SPAR WEB IS CRACKED AT O/B TAB ROD AREA THROUGH HOLE. TRIMMED OUT DAMAGED AREA, FABRICATED REPAIR AND INSTALLED IAW SRM 51-40-2 FIG 1.May 9, 1996 · N946UP · Boeing 72725CSDR 96ZZZX5487Hinge Assy · crackedINSPECTION FOUND CRACKS AT LOWER OTBD AILERON HINGE ANGLES, CRACKS RADIATE UPWARD. RIGHT WING HAS 2 CRACKS, LEFT WING HAS 1 CRACK ON SIDE.May 9, 1996 · N5065U · Cessna 206CESSNASDR 96ZZZX5486Hinge · crackedINSPECTION FOUND CRACKS AT LOWER OTBD AILERON HINGE ANGLES, CRACKS RADIATE UPWARD. RIGHT WING HAS 2 CRACKS, LEFT WING HAS 1 CRACK ON SIDE.May 9, 1996 · N5065U · Cessna 206CESSNASDR UPS96220587Spar · crackedINSPECTION TYPE-C, LT O/B AILERON SPAR UPPER CHORD IS CRACKED O/B OF NR 2 HINGE. REMOVED AND REPLACED UPPER CHORD IAW SRM 51-10-1, 51-30-2 AND BOEING DWG 65-21723.May 8, 1996 · N946UP · Boeing 72725CSDR UPS96220067Nose · corrodedINSPECTION TYPE 'C' AILERON SERVO HOUSING IN FWD NOSE COMP IS CORRODED. REMOVED CORRODED HOUSING, INSTALLED NEW HOUSING PER MM 22-11-11.May 6, 1996 · N937UP · Boeing 72725CSDR AALA960741Fitting · corrodedTUL - FOUND INBOARD AILERON QUADRANT HAS HEAVY CORROSION. REMOVED AND INSTALLED NEW QUANDRANT MOUNT CASTING. (M)May 6, 1996 · N882AA · Boeing 727223SDR CALA9600715Skin · delaminatedINSPECTION FOUND THE LT WING AILERON TAB SKIN DELAMINATING. THE DELAMINATED AREA WAS REMOVED AND A FIBERGLASS OVERLAY REPAIR WAS INSTALLED IAW SRM 51-40-9.May 5, 1996 · N12230 · Boeing 737217SDR DHL9670913CSkin · damagedAT C-CHECK, OB AILERON OF LEFT WING IB TRAILING EDGE CORNER IS BENT AND OIL CANNING. CUT OUT DAMAGED AREA, FABRICATED NEW SKIN, 14 BY 18 PER SRM 57-50-5. REBALANCED AILERON PER SRM 51-80-4.May 2, 1996 · N709DH · Boeing 72782CSDR CALA9600754Skin · crackedINSPECTION FOUND A 1 INCH CRACK AT FASTENER HOLE OF LT OUTBOARD AILERON SKIN. A DOUBLER AND FILLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 57-50-5.Apr 30, 1996 · N16784 · Boeing 727232SDR AALA960684Skin · delaminatedTUL - DURING C-CHECK, FOUND TWO PLACES OF DELAMINATION ON UPPER SURFACE OF T/E ON RIGHT OUTBOARD AILERON. REPAIRED DELAMINATION PER ESO 41000 DATED 4-26-96. (M)Apr 26, 1996 · N1755 · Doug MD11SDR 96ZZZX2685Skin · corrodedDURING C-CHECK, FOUND RT OUTBOARD AILERON SKIN BULGING. CUT OUT DAMAGED AREA, REPAIRED IAW DER DRAWING ARW 950082-0289.Apr 26, 1996 · N8969U · Doug DC862SDR 96ZZZX2669Skin · corrodedDURING C-CHECK, FOUND LEFT WING OUTBOARD AILERON, INBOARD LOWER SURFACE SKIN BULGED. REPAIRED AILERON IAW DER DRW 950082-4066.Apr 26, 1996 · N8969U · Doug DC862SDR UPS96805979Skin · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT WING BOTTOM I/B AILERON, SKIN AT MIDDLE FWD GOUGED CRACKED AND DENTED. STOP DRILLED CRACKS, FAB REPAIR DOUBLERS AND INSTALLED IAW DC8-SRM 57-2-1 AND 57-8-0.Apr 12, 1996 · N803UP · Doug DC873FSDR 96ZZZM1302Bearings · wornDURING ROUTINE MAINTENANCE, BOTH AILERONS WERE DISCOVERED AS HAVING EXCESSIVE FREE PLAY. UPON INSPECTION OF COMPONENTS, ALL THREE ATTACHMENT BEARINGS AND MOUNTING HARDWARE WAS FOUND WORN AND LOOSE. BEARINGS AND HARDWARE REPLACED WITH NEW. (M)Apr 2, 1996 · N840CA · Beech 1900DSDR UPS96806029Aileron · corrosionWHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT I/B AILERON HAS INTERNAL CORROSION. REPLACED AILERON ASSY PER MM 27-11-01.Apr 1, 1996 · N840UP · Doug DC873FSDR CAL960483Skin · delaminatedGSO - INSPECTION FOUND RT AILERON UPPER SURFACE DELAMINATED AT OUTBOARD END OF TRIM TAB CUT-OUT. THE DELAMINATED AREA WAS REMOVED. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-6, SRM 51-10-2, AND SRM 51-20-21. (X)Mar 25, 1996 · N77215 · Boeing 737130SDR AU960385Bracket · corroded(AUS) LH AILERON CENTRE AND INBOARD HINGE BRACKETS CORRODED - RH AILERON CENTRE HINGE BRACKET CORRODEDMar 25, 1996 · Piper PA34200TSDR 96FDEA00700Hinge Fitting · crackedNR0348 AND 030, RT WING O/B AILERON NR 3 HINGE FITTING IS CRACKED.Mar 25, 1996 · N154FE · Boeing 72725SDR MWEA96065Skin · chafedDURING INSPECTION, FOUND RT AILERON SKIN CHAFED FROM FAIRING SKIN ON WING TRAILING EDGE. INSTALLED STAINLESS STEEL DOUBLER REPAIR IAW SRM 57-01 FIG 2 SHEET 2. REBALANCED.Mar 23, 1996 · N600ME · Doug DC914SDR CA960325001Pin · corroded(CAN)RIGHT AILERON OUTBOARD HINGE INBOARD HOLE AND HINGE PIN SEVERELY PITTED. PIN AND FITTING REPLACED.Mar 21, 1996 · Dhav DHC8102SDR UPS96205738Fitting · corrodedWHILE IN FOR SI CHECK, MAINTENANCE REPORTED LT WING, INBOARD AILERON CENTER HINGE FITTING IS CORRODED, AILERON SIDE. REPLACED FITTING IAW SRM 51-30-2, AND OHM 57-50-1.Mar 15, 1996 · N907UP · Boeing 72727CSDR 96FDEA00566Hinge Fitting · corrodedNR0196 AND 002, LEFT O/B AILERON NR 1 HINGE FITTING IS CORRODED ON LOWER SURFACE.Mar 15, 1996 · N154FE · Boeing 72725SDR 96ZZZX3630Aileron Skin · crackedFOUND RIGHT AILERON TOP SKIN CRACKED AT OUTBOARD END. CRACK EXTENDED OUT FROM TWO SIDES OF A RIVET HEAD, APPROXIMATELY .1875 INCH IN BOTH DIRECTIONS. AILERON WAS REPAIRED AND WILL BE MONITORED FOR FURTHER CRACKING.Mar 13, 1996 · N551TP · Israel 1124ASDR 96ZZZX1371Spar · crackedDURING DISASSEMBLY OF AILERON TO REPLACE CRACKED AILERON SKINS, SPAR FOUND TO HAVE 3 CRACKS. THERE ARE TWO, 1.5 INCH CRACKS IN AREA OF OUTBOARD HINGE FITTING ATTACH HOLES AND ONE, .5 INCH CRACK IN AREA OF CENTER HINGE FITTING ATTACH HOLE. CRACKS ARE SUSPECTEMar 11, 1996 · N361AE · Swrngn SA227ACSDR CA960327001Bracket · cracked(CAN)DURING INSPECTION THE AILERON BRACKET WAS FOUND CRACKED WHERE IT ATTACHES TO THE WING TRAILING EDGE STRUCTURE.Mar 8, 1996 · Cessna U206GSDR 96ZZZX1372Skin · crackedFOUND DURING INSPECTION. SKIN CRACKED APPROXIMATELY 6 INCHES FROM OUTBOARD END WHERE LEADING SKIN AND UPPER SKIN ARE ATTACHED TO SPAR. SUBMITTER STATES THIS IS FOURTH B100 AIRCRAFT WITH CRACKS ON UPPER SKIN. HAVE NOT HAD ANY PROBLEMS ON LT AILERONS.Mar 8, 1996 · N2025S · Beech B100SDR 96ZZZX1363Skin · crackedFOUND DURING INSPECTION. SKIN CRACKED APPROXIMATELY 12 INCHES FROM INBOARD END WHERE LEADING EDGE SKIN AND UPPER SKIN ARE ATTACHED TO SPAR. SUBMITTER STATED THIS IS THE THIRD AIRCRAFT WITH CRACKS IN THE SAME PLACE.Mar 8, 1996 · N771S · Beech B100SDR 96FDEA00646Casting · corrodedRIGHT WING PIVOT BOLT HOLE FOR OUTBOARD AILERON QUAD CORRODED AT BOTTOM. REPLACED OUTBOARD AILERON LOCK-OUT SUPPORT CASTING PER 51-10-1.Mar 8, 1996 · N119FE · Boeing 72725CSDR UPS96805898Skin · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT O/B AILERON SKIN AND LOWER DOUBLER CRACKED AT THE I/B CLOSURE RIB. REPAIRED PER UPS EO DC8-57-0652.Mar 5, 1996 · N797UP · Doug DC871FSDR CA960311014Skin · corrosion(CAN)AILERON DEVELOPED A CRACK. DURING THE REPAIR, NEW SKINS WERE ORDERED AFTER FINDING HEAVY CORROSION AFTER REMOVING THE SKIN. SUBMITTER STATES THAT THIS COULD NOT BE SEEN FROM THE OUTSIDE.Mar 4, 1996 · Beech B100SDR AU960235Spar · cracked(AUS) RH AILERON SPAR CRACKED IN AREA BEHIND INBOARD HINGE ARM ATTACHMENT POINT - FOUND DURING INSPECTION IAW AD/PA31/118Mar 3, 1996 · Piper PA31350SDR 96ZZZX1775Doubler · crackedOUTBOARD DOUBLER HOLDING AILERON TO WING (REINFORCES MOUNT) HAS CRACKS. FOUND ON THREE CONSECUTIVE AIRCRAFT DURING ANNUAL INSPECTION. THREE RIGHT OUTBOARD AND ONE LEFT OUTBOARD. SUBMITTER SUGGESTS COUNTERWEIGHTS FOR THE AILERON MAY BE CAUSING STRESS FRACTURMar 1, 1996 · N3258W · Piper PA32260SDR 96ZZZX1774Doubler · crackedOUTBOARD DOUBLER HOLDING AILERON TO WING (REINFORCES MOUNT) HAS CRACKS. FOUND ON THREE CONSECUTIVE AIRCRAFT DURING ANNUAL INSPECTION. THREE RIGHT OUTBOARD AND ONE LEFT OUTBOARD. SUBMITTER SUGGESTS COUNTERWEIGHTS FOR THE AILERON MAY BE CAUSING STRESS FRACTURMar 1, 1996 · N5517J · Piper PA32260SDR 96ZZZX1773Doubler · crackedOUTBOARD DOUBLER HOLDING AILERON TO WING (REINFORCES MOUNT) HAS CRACKS. FOUND ON THREE CONSECUTIVE AIRCRAFT DURING ANNUAL INSPECTION. THREE RIGHT OUTBOARD AND ONE LEFT OUTBOARD. SUBMITTER SUGGESTS COUNTERWEIGHTS FOR THE AILERON MAY BE CAUSING STRESS FRACTURMar 1, 1996 · N3855W · Piper PA32260SDR DL72S960453Skin · wornLOWER SKIN WAS FOUND WITH OVERSIZED HOLES. SPLICED SKIN SECTION PER M/M 57-51-0 FIG 801. FOUND DURING SHOP INSPECTION OF AILERON ASSEMBLY.Feb 28, 1996 · N467DA · Boeing 727232SDR DL72S960452Spar · crackedSPAR WAS FOUND CRACKED NEAR TAB FITTING. SPLICED SPAR SECTION PER SRM 51-40-3 FIG 1. FOUND DURING SHOP INSPECTION OF AILERON ASSEMBLY.Feb 28, 1996 · N467DA · Boeing 727232SDR 96ZZZM1303Bearings · wornDURING ROUTINE MAINTENANCE, BOTH AILERONS WERE DISCOVERED AS HAVING EXCESSIVE FREE PLAY. UPON INSPECTION OF COMPONENTS, ALL THREE ATTACHMENT BEARINGS AND MOUNTING HARDWARE WERE FOUND WORN AND LOOSE. BEARINGS AND HARDWARE REPLACED WITH NEW. (M)Feb 28, 1996 · N858CA · Beech 1900DSDR AU960224Rib · cracked(AUS) AILERON NOSE RIBS PNO 86397-02 AND PNO 86397-03 CRACKED - FOUND DURING INSPECTION IAW AD/PA44/16Feb 27, 1996 · Piper PA44180SDR 96FDEA00302Hinge Fitting · elongated holesO/B LT WING AILERON HINGE FITTING MOST I/B ON AILERON SIDE BOLT HOLES ARE ELONGATED. REMOVED AND REPLACED O/B LT WING AILERON I/B HINGE FITTING. REINSTALLED AND TORQUED ATTACH BOLTS IAW FEDEX MM 27-10-31.Feb 22, 1996 · N194FE · Boeing 72722SDR AU960211Rib · cracked(AUS) RH AILERON NOSE RIBS CRACKED - FOUND DURING INSPECTION IAW AD/PA44/16Feb 21, 1996 · Piper PA44180SDR DL72L960390Skin · crackedDURING INSPECTION, LEFT WING O/B AILERON WAS FOUND WITH LOWER OUTBOARD SKIN CRACKED. REPAIRED PER MM 57-51-0 PG 801.Feb 20, 1996 · N511DA · Boeing 727232SDR UPS405530Fittings · elongated holesWHILE IN AMS FOR C-CHECK MAINTENANCE REPORTED, LT WING O/B AILERON, 4 ATTACHMENT FITTINGS HOLES ARE ELONGATED AT WS 1308, 1423, 1485 AND 1548. REPLACED HINGE FITTINGS IAW SRM 51-30-02.Feb 16, 1996 · N691UP · Boeing 747121SDR UPS205562Fitting · corrodedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, RT WING O/B AILERON I/B CENTER HINGE FITTING AILERON SIDE IS CORRODED AND BEARING BLOCK HAS BLOWN DUST COVER. REPLACED CENTER HINGE FITTING IAW UPS OHM 57-50-111 AND MM 27-10-41.Feb 16, 1996 · N931UP · Boeing 72725CSDR 96FDEA00263Te Wedge · delaminatedLT WING O/B AILERON T/E WEDGE HAS AN AREA OF DELAMINATION ON I/B LOWER SURFACE 6 INCHES BY 4 INCHES. REPAIRED LT WING O/B AILERON T/E WEDGE PER FEDEX SRM 51-80-04 SRM 51-40-06.Feb 16, 1996 · N194FE · Boeing 72722SDR UPS405463Fitting · elongatedWHILE IN AMS FOR C CHECK, MAINTENANCE REPORTED LT WING O/B AILERON ATTACH FITTINGS HAVE ELONGATED HOLES AT W/S 1308, 1423, 1485, AND 1548. REPLACED FITTINGS PER SRM 51-30-02.Feb 14, 1996 · N691UP · Boeing 747121SDR UPS205543Center Hinge · corrodedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, LT I/B AILERON CENTER HINGE IS CORRODED AT PANEL ATTACH POINT. REPLACED HINGE FITTING IAW MM 27-10-01.Feb 14, 1996 · N931UP · Boeing 72725CSDR DL72W960321Skin · wornDURING INSPECTION, LEFT WING AILERON LOWER OUTBOARD SKIN HAD SEVERAL OVERSIZED AND WORN FASTENER HOLES DUE TO FATIGUE. SPLICED IN NEW SECTION OF SKIN PER MM 57-51-00, FIG 801.Feb 13, 1996 · N2809W · Boeing 727247SDR AALA960273Support · corrodedAFW - LEFT WING AILERON HINGE SUPPORT, RIB NR 1 AT STA 817.27, HAS CORROSION REMOVED AROUND NUTPLATE BEYOND SRM LIMITS, PER MRB 757-726. (X)Feb 13, 1996 · N641AA · Boeing 757223SDR UPS205495Fitting · corrodedWHILE IN FOR C CHECK, MAINTENANCE REPORTED CORROSION LT O/B AILERON HINGE FITTING. REPLACED FITTING PER SRM 51-30-2.Feb 9, 1996 · N931UP · Boeing 72725C
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