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 AUS20021397Bracket · corroded(AUS) LH AILERON CENTRE HINGE BEARING SUPPORT BRACKET CONTAINED EXFOLIATION CORROSION. AREA OF CORROSION APPROXIMATELY 20MM (0.78IN) BY 5MM (0.196IN) AND 0.5MM (0.019IN) DEEP. AIRCRAFT IS A FLOATPLANE.Nov 28, 2002 · Dhav DHC2*SDR CA021115024Spar · cracked(CAN) FOUND RT AILERON INBOARD TRAILING EDGE RIB CRACKED AROUND BOTTOM MOUNTING HOLE.UPON REMOVAL OF RIB, FOUND SPAR IS ALSO HAS A 1/2 INCH CRACKED BESIDE BOTTOM MOUNTING HOLE.Nov 15, 2002 · Piper PA23250SDR CA021115023Rib · cracked(CAN) DURING 100 HOURS INSPECTION, FOUND RT AILERON INBOARD TRAILING EDGE RIB CRACKED AROUND BOTTOM MOUNTING NUT. UPON REMOVAL OF RIB, THE AILERON SPAR IS ALSO CRACKED AT SAME LOCATION.Nov 15, 2002 · Piper PA23250SDR C2XA02TY167Fitting · bentTYS. During a scheduled inspection, the left aileron PCA fitting attach lug was found bent. Maintenance removed and replaced the fitting. I/A/W-EC5750-01177. The repair was satisfactory and the aircraft will be released upon complection of the check.Nov 8, 2002 · N13975 · Emb EMB145LRSDR AUS20021307Aileron · out of balance(AUS) RH AILERON OUT OF BALANCE. ACCESS PANELS (3OFF) IN LOWER SKIN AND A QUANTITY OF EPOXY RESIN IN THE TRAILING EDGE CAUSED THE AILERON TO BE APPROXIMATELY 700 GRAMS OUT OF BALANCE. PERSONNEL/MAINTENANCE ERROR.Oct 31, 2002 · Cessna 402CSDR C2XA02TY154Structure · gougedDURING A SCHEDULED 2-C INSPECTION, THE RT AILERON PCA ATTACH POINT WAS FOUND WITH TOOLING MARKS. MAINT MEASURED THE DAMAGE AND BLENDED TOOLING MARKS, PRIMED AND PAINTED IAW GST-3000/02,CPM-51-21-05,06. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETOct 21, 2002 · N16976 · Emb EMB145LRSDR CA030228009Hinge · seized(CAN) DURING INSPECTION AILERONS WERE ACTUATED FROM THE CONTROL COLUMN AND AILERON MOVEMENT WAS FOUND TO BE SPRINGY. VISUAL INSPECTION OF BOTH AILERONS CONFIRMED HINGE PINS WERE SEIZED AND NOT ALLOWING THE HINGE TO MOVE. NEW HINGES INSTALLED.Oct 15, 2002 · Cessna 180SDR A6WA200260036Tab · dentedDENTS RIGHT AILERON INBOARD AND OUTBOARD TABS X 32 RECEIVED CONCESSION.Oct 4, 2002 · N612AW · Bac 146300ASDR A6WA200260035Tab · dentedDENTS LEFT AILERON TABS X 9 RECEIVED CONCESSION.Oct 4, 2002 · N612AW · Bac 146300ASDR DHL2002803501Structure · dentedLT WING OUTBOARD AILERON TRAILING EDGE, SHOWS 3 DENTS (1/2 IN) BETWEEN XRS 624.000 AND XRS 693.000. REMOVED DAMAGED O/B AILERON T/E PER SRM 51-1-21 PG 1.FABRICATED NEW T/E (2024T3AL 0.030) PER SRM 57-8-1 PG 8.CLEANED TERATED AND PRIMED PER SRM 51-1-8B.INSTASep 26, 2002 · N803DH · Doug DC873SDR 2002FA0001117Fitting · looseDURING INSPECTION FOUND LT INBOARD AILERON HINGE LOOSE. CONDITION FOUND BY FEELING A CLUNK WHILE MOVING TRAILING EDGE OF AILERON UP AND DOWN SLOWLY. TRAILING EDGE OF AILERON HINGE ABLE TO BE MOVED 1/8" UP AND DOWN. FOUND EVIDENCE OF "TORQUE-SEAL" ON ATTACH Sep 25, 2002 · N929R · Cirrus SR22SDR USAA020367Skin · crackedRIGHT AILERON, CRACKED 2 LOCATIONS. LOWER SKIN FLANGE AT NR 3 HINGE AND NR 2 HINGE. REMOVED ALL DAMAGE PLUS COMPLETED WET LAYUP REPAIR IAW SRM AND EA.Sep 17, 2002 · N300AU · Boeing 737301SDR UPS02239723Hinge Fitting · crackedSUSPECT CRACK ON LEFT O/B AILERON NR 3 HINGE FITTING ON WING. LEFT O/B AILERON REMOVED IAW MM 27-10-10. HINGE FITTING NR 3 REMOVED IAW SRM 51-30-02. NEW HINGE FITTING INSTALLED IAW DRAWING 65-19275.Sep 17, 2002 · N930UP · Boeing 72722CSDR AUS20021050Doubler · cracked(AUS) RH AILERON SPAR DOUBLER CRACKED IN AREA LOCATED IMMEDIATELY BELOW THE INBOARD HINGE ATTACHMENT PLATE LOWER BOLT HOLE. CRACK LENGTH18MM (0.71IN). FOUND DURING DYE PENETRANT INSPECTION IAWAD/PA31/118 AMDT 1.Sep 16, 2002 · Piper PA31350SDR MALA020535Hinge · lack of lubeDURING FLIGHT 3321, WITH AUTO-PILOT OFF, A/C HARD TO TURN TO THE LEFT. MAINTENANCE PERFORMED REQUIRED AILERON CHECKS, ALL CHECKS GOOD. LUBRICATED AILERON HINGE POINTS, FREEDOM FORCE CHECK OF PILOTS AND F/O'S CONTROL COLUMN IS GOOD.Sep 4, 2002 · N110XJ · Saab SF340ASDR AUS20021128Bracket · misrepaired(AUS) LT AILERON INCORRECTLY SECURED TO THE HINGE BRACKET ASSEMBLY. ATTACHMENT HOLE DRILLED OVERSIZE AND A RIVNUT FITTED. UNAPPROVED PART / REPAIR. PERSONNEL / MAINTENANCE ERROR.Sep 1, 2002 · Beech 95C55SDR 2002FA0001056Hinge · misalignedDURING ROUTINE MAINTENANCE, TECH NOTICED LT AILERON MISALIGNED WITH TRAILING EDGE OF WING AT AILERON WELL. FOUND THAT OUTBOARD AILERON HINGE BOTTOM ATTACH SCREWS NOT IN HINGE ATTACH HOLES BUT CAUGHT BETWEEN AFT PORTION OF HINGE AND AILERON ATTACH HOLES. SCREAug 22, 2002 · N793DW · Beech 58SDR 2002F01003Structure · lightning strikeLIGHTNING STRIKE DISCHARGE AT RT OUTBD AILERON TOP SURFACE. REPAIRED AILERON IAW SRM 51-50-01. WING STATION OWS 502 TO OWS 502.Aug 19, 2002 · N195AT · Lkheed 1011SDR WRLA200220Structure · damagedRT INBOARD AILERON IS DAMAGED. TRAILING EDGE IS MISSING FOUND ON WALK AROUND. REMOVED AND REPLACED RT INBOARD AILERON.Aug 16, 2002 · N279WA · Doug MD11SDR COOSDR020217Skin · delaminatedLEFT WING OUTBOARD AILERON TRAILING EDGE DELAMINATED.Aug 1, 2002 · N511PE · Boeing 727232SDR AUS20020776Aileron · damaged(AUS) RH AILERON DAMAGED IN AREA OF LH TRAILING EDGE. DAMAGE WAS THEEXIT POINT OF A LIGHTNING STRIKE. THE AREA OF DAMAGE WASAPPROXIMATELY 193.5SQUAREMM (3SQIN) THROUGH SEVEN RIVET HEADS WITH A HOLE OF APPROXIMATELY 25.4MM (1IN). SEE MDR 02/0777 FORINFORMATION Jul 29, 2002 · Dhav DHC8202SDR AWXA200200814Rib · crackedYVR - MAJOR REPAIR - DURING C-20 CHECK CRACKS WERE FOUND ON THE LT AILERON LEADING EDGE RIBS AT THE OUTBOARD END, AND INBOARD OF THE NR 2 HINGE FITTING. MAINTENANCE REMOVED OUTBOARD RIB OF LT AILERON, FABRICATED A NEW RIB, AND INSTALLED REPAIR PER DWG 65-4645Jul 25, 2002 · N182AW · Boeing 737277SDR AWXA200200816Skin · delaminatedYVR - MAJOR REPAIR - DURING C-20 CHECK DELAMINATION WAS FOUND ON THE LOWER OUTBOARD END OF THE RT AILERON. MAINTENANCE REMOVED AND REPLACED THE RT AILERON PER T/C R3M27015.Jul 24, 2002 · N182AW · Boeing 737277SDR C7WA200200027Skin Panel · delaminatedDURING C-CHECK INSPECTION, FOUND LT WING OUTBOARD AILERON TRAILING EDGE PANEL DELAMINATED. REPAIRED LEFT WING OUTBOARD AILERON IAW COOPESA EO COO0CMP-2-57-366-02 WITH DER APPROVAL. (M)Jul 13, 2002 · N511PE · Boeing 727232SDR GTIA020915Skin · delaminatedFTW - FOUND RIGHT OUTBOARD AILERON TAB DELAMINATED ON LOWER SURFACE AT INBOARD END AND AT CENTER HINGE. REMOVED RIGHT AILERON OUTBOARD TAB. DAMAGE EXCEEDS MD80 SRM REPAIR LIMITS. INSTALLED RIGHT OUTBOARD AILERON TAB. (M)Jul 13, 2002 · N819NK · Doug DC981SDR 2002FA0000897Angle · separatedCOULD NOT MOVE AILERONS. 90 PERCENT ANGLE, USED TO PREVENT OIL CANNING, BONDED INSIDE AILERON, BROKE LOOSE AND WORKED ITS WAY DOWN TRAILING EDGE OF AILERON AND INTO FLAP TRAILING EDGE, PREVENTING AILERONS FROM MOVING. 90 PERCENT ANGLE IS 8 INCHES LONG AND .3Jul 12, 2002 · N4652N · Cessna 402CSDR LR7A02058Skin · corrodedDURING SCHEDULED C3 INSPECTION PER JOB CARD HC2704 FOUND LH AILERON UPPER SKIN CORRODED AT AS 55, FS 595.REPAIRED SKIN IAW SRM SMP 583 51-140-10. NR 0139.Jul 7, 2002 · N404LC · Lkheed 382GSDR SWAA021453Aileron · delaminatedDURING WALKAROUND INSPECTION, FOUND LT AILERON DELAMINATED. REMOVED AND REPLACED LT AILERON AND TAB PER MM.Jul 2, 2002 · N722WN · Boeing 7372T4SDR COOSDR020214Structure · delaminatedRIGHT WING, OUTBOARD AILERON TRAILING EDGE (PN 65-21766-66)(SN BN-26) WITH DELAMINATION.Jul 1, 2002 · N128NA · Boeing 7272J7SDR COOSDR020187Structure · corrodedRIGHT WING OUTBOARD AILERON TRAILING EDGE (PN 652176634) (SN 226) UPPER, LOWER SKIN AND HONEYCOMB CORE, CORRODED.Jul 1, 2002 · N794AJ · Boeing 727227SDR C2XA02TY106Bracket · damagedTYS DURING A SCHEDULED INSPECTION THE RIGHT HAND AILERON TO PCA BRACKET MOUNT HOLE WAS FOUND TO BE ELONGATED DUE TO WEAR. MAINTENANCE REMOVED AND REPLACED THE THE BRACKET IAW CONTINENTAL EXPRESS EC 5750-01177 AND EMB 145 SRM 57-60-02. THE AIRCRAFT WILL BE RJun 21, 2002 · N15973 · Emb EMB145SDR SWAA021322Aileron · delaminatedDURING WALK AROUND INSPECTION, FOUND LT AILERON DELAMINATED ON BOTTOM SURFACE 1.5 INCHES OTBD OF AILERON TAB CUTOUT SUPPORT BRACE. REMOVED AND REPLACED AILERON PER MM.Jun 15, 2002 · Boeing 7372H4SDR 02FDEA00447Fitting · corrodedLEFT WING O/B AILERON FITTING CORRODED ON TOPSIDE OF FITTING. REMOVED AND REPLACED FITTING PER MM 27-10-131-4.Jun 12, 2002 · N186FE · Boeing 727200SDR CA020607012Skin · cracked(CAN) DURING AN EVENT NR 3 INSPECTION AN APPROXIMATE 1 INCH CRACK WAS FOUND ON THE LOWER SURFACE OF THE LT AILERON. THE CRACK WAS LOCATED NEAR THE INBOARD END OF THE AILERON AT THE TRAILING EDGE OF THE SIXTH STIFFENING BEAD. THE AILERON WAS REMOVED AND REPLACEJun 3, 2002 · Piper PA44180SDR DEM2002F00009Hinge Bracket · crackedFOUND BOTH INBOARD AILERON HINGE BRACKETS CRACKED COMPLETELY THROUGH THE BEARING BOSS.Jun 1, 2002 · N4339V · Cessna 190SDR DEM2002F00008Hinge Bracket · crackedFOUND BOTH INBOARD AILERON HINGE BRACKETS CRACKED COMPLETELY THROUGH THE BEARING BOSS.Jun 1, 2002 · N4339V · Cessna 190SDR COOSDR020169Aileron · delaminatedLEFT WING OUTBOARD AILERON TRAILING EDGE UPPER AND LOWER SKIN DELAMINATED AND HONEYCOMB CORE CORRODED.Jun 1, 2002 · N1279E · Boeing 7272Q6SDR COOSDR020167Aileron · delaminatedRIGHT WING OUTBOARD AILERON TRAILING EDGE UPPER AND LOWER SKIN DELAMINATED AND HONEYCOMB CORE CORRODED.Jun 1, 2002 · N1279E · Boeing 7272Q6SDR COOSDR02116Aileron · delaminatedRIGHT WING, OUTBOARD AILERON TRAILING EDGE WITH DELAMINATION.Jun 1, 2002 · N994AJ · Boeing 727233SDR AUS20021467Arm · corroded(AUS) LH OUTBOARD AILERON HINGE ARM CONTAINED EXFOLIATION CORROSION AROUND BOLT HOLE.May 24, 2002 · Dhav DHC6100SDR AUS20021029Hinge · corroded(AUS) RH OUTBOARD AILERON ATTACHMENT HINGE CORRODED. CORROSION IS LOCATED AT ZONE 88 WBL 492.0. FOUND DURING CPCP INSPECTION.May 21, 2002 · Boeing 727277SDR 2002FA0000661Skin · crackedAILERON SKIN CRACKS OBSERVED PROPAGATING LATERALLY IN UPPER AND LOWER AREAS FOWARD OF SPAR AND AFT OF BALLANCE WEIGHTS.May 21, 2002 · N161DP · Beech 95B55SDR AUS20021033Hinge · corroded(AUS) OUTBOARD AILERON INPUT ROD ATTACHMENT FITTING CORRODED. AILERON UPPER SKIN CRACKED AND LOWER SKIN CORRODED. LOCATED IN ZONE 81WBL 492.0. FOUND DURING CPCP INSPECTION.May 17, 2002 · Boeing 727277SDR CA020530010Hinge Bracket · cracked(CAN) AILERON BRACKETS WERE LOOSE ON SPAR AND IN SKIN ATTACH. UPON EXAMINATION FOUND BOTH BRACKETS CRACKED AT REAR AND BOTTOM FLANGES. IT APPEARS THAT THE BRACKETS HAD BEEN LOOSE PREVIOUSLY AND REPAIRED BY SUBSTITUING CHERRY MAX THROUGH BOTTOM SKIN WHICH DID NMay 17, 2002 · Cessna U206BSDR CA020611002Rib · chafed(CAN) RIB LACING THAT SECURES FABRIC ONTO AILERON RIBS FOUND TO BE SERIOUS CHAFED ALONG RIB EDGES WHICH COULD LEAD TO FAILURE OF FABRIC SECURITY ONTO RIBS AND POTENTIAL AILERON FLUTTER, ON BOTH RIGHT AND LEFT AILERON ASSEMBLIES.May 16, 2002 · Helio H395ASDR 2002FA0000801Hinge Bracket · corrodedTHESE BRACKETS ARE MADE OF MAGNESIUM AND ARE CORRODING AND CRACKING TO AN ALARMING DEGREE.May 16, 2002 · N2165C · Cessna 195BSDR 2002FA0000800Hinge Bracket · crackedTHESE BRACKETS ARE MADE OF MAGNESIUM AND ARE CORRODING AND CRACKING TO AN ALARMING DEGREE.May 16, 2002 · N9854A · Cessna 190SDR 2002FA0000748Bracket · corrodedBRACKETS ARE MADE OF MAGNESIUM, CORRODING AND CRACKING. APPROXIMATELY 80 PERCENT OF THE BRACKETS INSPECTED BY BEAD BLASTING ARE UN-AIRWORTHY. PROBLEM OF CORROSION BETWEEN BEARING AND BOSS WHICH EXPANDS AND CRACKS THE BOSS. SEPARATION OF AILERON FROM REAR WIMay 16, 2002 · N4411C · Cessna 190SDR 2002F00637Bracket · corrodedBRACKETS ARE MADE OF MAGNESIUM, CORRODING AND CRACKING. PROBLEM OF CORROSION BETWEEN BEARING AND BOSS WHICH EXPANDS AND CRACKS THE BOSS. REMOVE BRACKETS FROM AIRCRAFT AND BEAD BLAST BODY WHILE PROTECTING BEARING.May 16, 2002 · N3040B · Cessna 195SDR 2002FA0000747Bracket · corrodedBRACKETS ARE MADE OF MAGNESIUM, CORRODING AND CRACKING. APPROXIMATELY 80 PERCENT OF THE BRACKETS INSPECTED BY BEAD BLASTING ARE UN-AIRWORTHY. PROBLEM OF CORROSION BETWEEN BEARING AND BOSS WHICH EXPANDS AND CRACKS THE BOSS. SEPARATION OF AILERON FROM REAR WIMay 16, 2002 · N195WT · Cessna 195B
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