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 96ZZZX5480Spar Assy · crackedFOUND THE SPAR CRACKED ON LT AILERON AT CENTER HORN AND HINGE ASSY AT THE SPAR ATTACH. SUSPECT FAULT LIES IN DESIGN AS THE AILERON SPAR WAS CUT OUT ON THE OTBD EDGES OF THE 'U' CHANNEL SPAR TO ACCOMODATE THE AILERON ASSY. THIS WEAKENS THE SPAR AND CONTRIBUTESep 5, 1996 · N2561N · Piper PA18150SDR 96ZZZX5479Spar Assy · crackedFOUND THE SPAR CRACKED ON RT AILERON PN 60 714-03 AT CENTER HORN AND HINGE ASSY AT THE SPAR ATTACH. SUSPECT FAULT LIES IN DESIGN AS THE AILERON SPAR WAS CUT OUT BY FACTORY ON THE OTBD EDGES OF THE 'U' CHANNGEL SPAR TO ACCOMMODATE THE AILERON HORN ASSY. THIS Sep 5, 1996 · N2561N · Piper PA18150SDR DL72S962432Spar · crackedREAR SPAR WAS FOUND CRACKED. REPAIRED SPAR PER SRM 51-40-3 FIG 1.Sep 3, 1996 · N492DA · Boeing 727232SDR DHL9670825CSkin · damagedAT C-CHECK, EFFECT PERMANANT REPAIR ON LT OUTBOARD AILERON TRAILING EDGE. INSTALLED BONDING REPAIR PER SRM 51-40-6 AND REPLACED SKIN LOWER SURFACE, SIZE 43.5 INCHES BY 7 INCHES. CHECK BALANCE PER SRM 51-80-4.Aug 31, 1996 · N708DH · Boeing 72725SDR IXXA96151Skin · corrodedDURING ROUTINE C-CHECK INSPECTION, THE RIGHT INBOARD AILERON LOWER PLATING WAS FOUND TO BE CORRODED. REPAIR TO THE PLATING WAS ACCOMPLISHED IAW FAA DER APPROVED REPAIR B12-R09. (M)Aug 27, 1996 · N735PL · Doug DC862SDR CKSA96083Skin · damagedDURING C-2 CHECK, INSPECTION FOUND OUTBOARD AILERON INBOARD LOWER SKIN DAMAGED. REPAIRED LOWER SKIN IAW AIA EA DWG 22486161 SKETCH NR AIA/E/2249, TASK NR 80134, CORROSION CARD NR 111R-0551.Aug 27, 1996 · N6161C · Doug DC8F55SDR UPS96520951Skin · delaminatedINSPECTION TYPE-3C, WHILE WORKING EO B757-5760-6676B FOUND AREA OF DELAM AT INBOARD FORWARD CORNER OF RIGHT WING AILERON LOWER CONDUCTIVE FRAME. REPAIRED RT AILERON LWR SURFACE IAW SRM 51-31-01.Aug 22, 1996 · N408UP · Boeing 75724APFSDR 96ZZZX4787Rib · crackedRIB WAS FOUND CRACKED FROM NUTPLATE RIVET. AFTER REMOVING HINGE FITTING 86392-02, A 1.25 INCH CRACK WAS FOUND RUNNING ALONG THE BOTTOM OF THE NUTPLATE. USING A BORESCOPE, THE INBOARD NOSE RIB WAS ALSO FOUND TO HAVE A 1 INCH CRACK RUNNING THROUGH THE LOWER BOAug 20, 1996 · N886JH · Piper PA32R301SDR P5CA9601231Angle · crackedLT INBOARD AILERON L/E ANGLE INBOARD TO INBOARD HINGE CRACKED. FAB NEW ANGLE PER SRM 57-12-00 AND INSTALLED PER SRM 51-30-02.Aug 12, 1996 · N832FT · Boeing 747121SDR P5CA9601135Hinge Cutout · crackedRT OUTBD AILERON OUTBD HINGE UPPER CUTOUT CRACKED. CUTOUT REWORKED PER SRM 57-10-01, DAMAGE WITHIN THE LIMIT PER SRM 57-10-01.Aug 12, 1996 · N832FT · Boeing 747121SDR P5CA9601076Strip · tornLEFT OUTBOARD AILERON UPPER OUTBOARD STRIP IS TORN. TORN STRIP REPLACED PER MM 57-51-00.Aug 12, 1996 · N832FT · Boeing 747121SDR CA960916009Balance Weight · loose(CAN) DURING DAILY INSPECTION THE RIGHT HAND AILERON BALANCE WEIGHT WAS FOUND LOOSE, BENT AND HANGING BY THE OUTBOARD BOLTWEIGHT HAD BEEN LOOSE FOR SOME TIME TWO HOLES HAD BEEN SWAGED COMPLETELY THROUGH AND THE LAST HOLE WAS 1/2 WAY THROUGH. WEIGHT WAS BENT AAug 12, 1996 · Swrngn SA226TCSDR DHL9671538DSkin · dentedAT D-CHECK, OUTBOARD AILERON EXTERIOR LOWER SKIN DAMAGED ON RIGHT WING. CUT OUT DAMAGED AREA, INSTALLED FLUSH REPAIR PER SRM 57-50-5, PLUG, 2.75 INCHES BY 1.5 INCHES, FILLER, 4 INCHES BY 5 INCHES. NO RE-BALANCE REQUIRED PER SRM 51-80-4.Aug 11, 1996 · N715DH · Boeing 727155CSDR 96ZZZM1299Bearings · 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)Aug 7, 1996 · N845CA · Beech 1900DSDR IXXA96136Skin · corrodedDURING ROUTINE C-CHECK INSPECTION, THE LEFT OUTBOARD AILERON LOWER PLATING SURFACE WAS FOUND TO BE CORRODED BETWEEN STATIONS XW500 AND 577. THE PLATING WAS REPLACED IAW THE STRUCTURAL REPAIR MANUAL 51-1-21 AND FAA DER APPROVED SKETCH A89-R05. (M)Aug 6, 1996 · N61CX · Doug DC862SDR MWEA96359Skin · corrodedDURING D-CHECK, LT AILERON UPPER SKIN FOUND WITH NUMEROUS AREAS OF LIGHT CORROSION. FABRICATED NEW SKIN AND DOUBLER IAW ME EA 57-002, TREATED AND PRIMED IAW SRM 51-10-3 AND INSTALLED IAW EA 57-002.Jul 31, 1996 · N501ME · Doug DC932SDR AALA961147Rib · corrodedAFW - AILERON SUPPORT RIB WITH CORROSION REMOVED. MATERIAL REMAINING IS BEYOND SRM LIMITS. REPAIR PER MRB 757-894. TST: 15,172 HOURS. CYCLES: 5,361. (X)Jul 28, 1996 · N654A · Boeing 757223SDR IXXA96144Plating · corrodedDURING ROUTINE C-CHECK INSPECTION, THE RIGHT OUTBOARD AILERON LOWER PLATING ON THE INBOARD SIDE WAS FOUND TO BE CORRODED. REPAIR TO THE AREA WAS ACCOMPLISHED IAW THE STRUCTURAL REPAIR MANUAL 57-10-0. (M)Jul 23, 1996 · N61CX · Doug DC862SDR 96ZZZM1298Bearings · 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)Jul 14, 1996 · N833CA · Beech 1900DSDR 96ZZZX3718Spar · crackedDURING DISASSEMBLY OF AILERON FOR SKIN CHANGE, THE SPAR WAS FOUND CRACKED IN TWO PLACES AROUND OUTBOARD HINGE BRACKET. THE CRACKS WERE THE FULL WIDTH OF THE SPAR WEB AND INTO THE RADIUS OF THE FLANGES. THIS IS THE SECOND SPAR FOUND CRACKED LIKE THIS RECENTLY.Jul 10, 1996 · N359AE · Swrngn SA227ACSDR 96ZZZX3626Spar · crackedDURING DISASSEMBLY OF AILERON FOR SKIN CHANGE, THE SPAR WAS FOUND CRACKED IN TWO PLACES AROUND OUTBOARD HINGE BRACKET. THE CRACKS WERE THE FULL WIDTH OF THE SPAR WEB AND INTO THE RADIUS OF THE FLANGES. THIS IS THE SECOND SPAR FOUND CRACKED LIKE THIS RECENTLY.Jul 10, 1996 · N359AE · Swrngn SA227ACSDR UPS96220959Spar Chord · crackedINSPECTION TYPE-C, RT O/B AILERON AT CENTER I/B HINGE, LWR SPAR CHORD IS CRACKED. REMOVED, FABRICATED AND INSTALLED LWR SPAR CHORD PER BOEING DWG 65-21766, SRM 51-30-02.Jul 8, 1996 · N951UP · Boeing 72725CSDR UPS96420593Web · damagedINSPECTION TYPE-C, RT INB AILERON, TWO FASTENERS OF OUTBD WEB MISSING AND TWO FASTENERS ARE LOSE. REPAIRED WEB OF INB AILERON IAW SRM 51-40-02.Jul 4, 1996 · N677UP · Boeing 747123FSDR UPS96220756Skin · corrodedINSPECTION TYPE-C, LT O/B AILERON HAS SKIN BULGE ON TOP SKIN I/B END. RIVETS REMOVED FROM AILERON SKIN I/B END IAW SRM 51-30-2, AILERON HINGE ASSM FOUND CORRODED. REPLACED HINGE ASSM IAW DWG 65-2176 AILERON RIGGED IAW 27-10-00.Jul 4, 1996 · N941UP · Boeing 72722CSDR 96FDEA01218Te Skin · disbondedNR 0464, 016, RIGHT WING O/B AILERON IS DELAMINATED AT O/B TRAILING EDGE. *S/D* REPAIRED O/B AILERON AT O/B TRAILING EDGE IAW FEDEX SRM 51-40-06.Jul 2, 1996 · N195FE · Boeing 72722SDR UPS96820608Spar · crackedINSPECTION TYPE N/A, RT INB AILERON, INB AILERON ATTACH HINGE, INB SET OF HOLES 2 HAVE CRACK INDICATIONS. INB HOLES ALL LAYERS CRACKED, 1ST 3 LAYERS INDICATIONS ON INB SIDE, AFT LAYER OUTB SIDE. OUTB HOLE FIRST 2 LAYERS HAVE CRACK INDICATIONS INB SIDE OF HOLJul 1, 1996 · N798UP · Doug DC871FSDR CA960708004Bracket · cracked(CAN) BOTH LEFT AND RIGHT AILERON TERMINAL QUADRANT BRACKETS FOUND CRACKED AT LOWER ATTACHMENTS WHERE QUADRANT ATTACHES. ALSO P/N 85711596056.Jul 1, 1996 · Dhav DHC8301SDR 9615301161Skin · crackedDURING LINE CHECK, FOUND A CRACK IN THE LEFT OUTBOARD AILERON UPPER SKIN AT THE NR 5 RIB. REPAIRED PER EA 11-105126.Jun 27, 1996 · N161US · Doug DC1040SDR UPS96220497Rod Fitting · corrodedINSPECTION TYPE: C. RT O/B AILERON BUSS ROD FITTING ON AILERON L/E IS CRACKED. INSTALLED REPLACEMENT FITTING IAW SRM 51-30-2.Jun 21, 1996 · N903UP · Boeing 72751CSDR UPS96220487Hinge Ftg · corrodedINSPECTION TYPE SI, L/W O/B AILERON O/B CENTER HINGE SUPPORT FITTING IS CORRODED. REMOVED CORRODED HINGE FITTING, DRILLED NEW FITTING AND INSTALLED IAW SRM 51-30-02.Jun 19, 1996 · N929UP · Boeing 72722CSDR UPS96220483Fitting · corrodedINSPECTION TYPE SI, R/W O/B AILERON O/B WING SIDE HINGE FITTING IS CORRODED. FOUND R/W O/B AILERON O/B WING SIDE HINGE FITTING OUT OF LIMITS PER SRM 57-40-00. REMOVED AND REPLACED R/W O/B AILERON O/B WING SIDE HINGE FITTING PER SRM 51-30-02.Jun 19, 1996 · N929UP · Boeing 72722CSDR 96ZZZX3388Support Assy · crackedDURING ANNUAL INSPECTION ON GRUMMAN TIGER AA5B, FOUND LEFT AILERON OUTBOARD BEARING SUPPORT ASSY CRACKED APPROXIMATELY .25 INCH INBOARD OF LOWER BOLT HOLE.Jun 12, 1996 · N4533Q · Gulstm AA5BSDR UPS96220548Hinge Fttng · corrodedINSPECTION TYPE SI, L/W I/B AILERON TAB HAS ALL THREE HINGE FITTINGS CORRODED ON THE AILERON SIDE. REMOVED CORRODED HINGE FITTINGS, INSTALLED NEW HINGE FITTINGS IAW SRM 51-30-2, MM 27-10-11.Jun 11, 1996 · N929UP · Boeing 72722CSDR CA960625017Support · cracked(CAN) RIGHT AILERON BRACKET, CENTRE SUPPORT CRACKED ON CENTRE AILERON SPAR.Jun 6, 1996 · Emb EMB110P1SDR CA960620024Support · cracked(CAN) LEFT AILERON BRACKET, CENTRE SUPPORT CRACKED, ON CENTRE AILERON SPAR.Jun 6, 1996 · Emb EMB110P1SDR 96ZZZX5106Rib · crackedDURING A ROUTINE INSPECTION (100 HOUR), EXCESSIVE LATERIAL PLAY WAS DISCOVERED AT RT AILERON TO THE POINT OF CONTACTING WING TIP. FURTHER INVESIGATION FOUND ALL 3 LEADING EDGE RIBS WHICH SUPPORT THE HINGES CRACKED. THESE RIBS ARE DIFFICULT TO INSPECT DUE TO Jun 4, 1996 · N2199Z · Piper PA44180SDR 96ZZZX5105Rib · crackedDURING A ROUTINE INSPECTION (100 HOUR), EXCESSIVE LATERIAL PLAY WAS DISCOVERED AT RT AILERON TO THE POINT OF CONTACTING WING TIP. FURTHER INVESIGATION FOUND ALL 3 LEADING EDGE RIBS WHICH SUPPORT THE HINGES CRACKED. THESE RIBS ARE DIFFICULT TO INSPECT DUE TO Jun 4, 1996 · N2199Z · Piper PA44180SDR 96ZZZX5104Rib · crackedDURING A ROUTINE INSPECTION (100 HOUR), EXCESSIVE LATERIAL PLAY WAS DISCOVERED AT RT AILERON TO THE POINT OF CONTACTING WING TIP. FURTHER INVESIGATION FOUND ALL 3 LEADING EDGE RIBS WHICH SUPPORT THE HINGES CRACKED. THESE RIBS ARE DIFFICULT TO INSPECT DUE TO Jun 4, 1996 · N2199Z · Piper PA44180SDR UPS96220482Support Fitting · corrodedINSPECTION TYPE SI, L/W O/B AILERON, O/B SUPPORT FITTING ON WING IS PITTED AND CORRODED ON LOWER SURFACE AND AROUND BUSHINGS. REMOVED CORRODED PART, ORDERED NEW PART, RECEIVED DRILLED UP FITTING AND INSTALLED NEW FITTING IAW SRM 51-30-2, SRM 51-30-05.May 31, 1996 · N929UP · Boeing 72722CSDR UPS96220413Hinge Fitting · corrodedINSPECTION TYPE SI, RT I/B AILERON CENTER WING SIDE HINGE FITTING IS CORRODED. REMOVED CORRODED CENTER HINGE FITTING, FOUND BEARING BLOCK TO HAVE BLOWN DUST SEAL. REPLACED WITH NEW BEARING BLOCK AND REPLACED HINGE FITTING IAW OHM 57-50-01.May 29, 1996 · N929UP · Boeing 72722CSDR AU960762Rib · cracked(AUS) AILERON RIBS PNO 86399-803 AND PNO 86399-003 CRACKEDMay 28, 1996 · Piper PA44180SDR 96FDEA01048Hinge Casting · brokenLARGE HINGE ASSEMBLY FOR LEFT HAND O/B AILERON HAS BAR BROKEN OFF. REMOVED HINGE CASTING AND INSTALLED A SERVICEABLE CASTING PER DRAWING NR 65-19260 SHEET 1.May 28, 1996 · N136FE · Boeing 72725CSDR GLBA96098Aileron · crackedMSP - CREW REPORTED A CRACK IN RT AILERON END CAP FOUND DURING POST-FLIGHT WALK-AROUND. MAINTENANCE REMOVED, REPAIRED, AND REINSTALLED RT AILERON. TEST FLIGHT CHECKED GOOD. (X)May 23, 1996 · N152GL · Beech 1900CSDR CA960527103Skin · cracked(CAN) CRACKS 1/4 INCH LONG RADIATING FROM 3 HOLES FOR THE ATTACHMENT OF THE STEEL BALANCE WEIGHT ON THE OUTBOARD LEADING EDGE OF RIGHT HAND AILERON.May 18, 1996 · Univar 1083SDR CA960527102Skin · cracked(CAN) CRACK 3/8 INCH LONG RADIATING FROM 3 HOLES FOR THE ATTACHMENT OF THE STEEL BALANCE WEIGHT ON THE OUTBOARD LEADING EDGE OF RIGHT HAND AILERON.May 17, 1996 · Univar 1083SDR UPS96220192Aileron Hinge · corrodedINSPECTION TYPE-C, R/W, O/B AILERON O/B CENTER HINGE FITTING IS CORRODED AILERON SIDE. REMOVED AND REPLACED R/W, O/B AILERON O/B CENTER HINGE FITTING ON AILERON SIDE IAW SRM 51-30-05, 51-30-02 OHM 20-50-03 AND M/M 57-50-11.May 16, 1996 · N922UP · Boeing 72731CSDR UPS96220191Hinge · corrodedINSPECTION TYPE-C, R/W I/B AILERON CENTER AND O/B TAB HINGE FITTINGS ARE CORRODED AILERON SIDE. REMOVED AND REPLACED CENTER AND O/B TAB FITTINGS ON R/W, I/B AILERON IAW SRM 51-30-02.May 16, 1996 · N922UP · Boeing 72731CSDR 96ZZZX3451Doubler · worn holeBUSHINGS 169-110000-347 FELL OUT OF DOUBLER WHEN LOOSE AILERONS REMOVED. NEW PARTS FOR MANUFACTURER FOUND TO HAVE A VERY LOOSE INTERFERENCE FIT BETWEEN BUSHING AND DOUBLER. THIS COULD RESULT IN SAME PROBLEM IN A SHORT TIME.May 16, 1996 · N6996Q · Beech B23SDR 96ZZZM1301Bearings · 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)May 16, 1996 · N847CA · Beech 1900DSDR ARWR961744Skin · crackedDURING C-CHECK, FOUND LT OUTBOARD AILERON UPPER SURFACE AT OUTBOARD ATTACHING FITTING, L/E SKIN HAS A CRACK. CUT DAMAGED SECTION, FABRICATED AND INSTALLED DOUBLER IAW DER NR 950082-1567. TREATED AND PRIMED IAW SRM 51-1-8. (X)May 15, 1996 · N8969U · Doug DC862
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