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 C2XA09SH185Hinge Fitting · damagedSHV - DURING C-CHECK LT AILERON O/B HINGE FITTING (ON AILERON) I/B HAT BUSHING HOUSING WAS FOUND DAMAGED. MAINTENANCE REMOVED AND REPLACED LT AILERON O/B HINGE FITTING IAW SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Jul 5, 2009 · N13958 · Emb EMB145LRSDR HSYA2009061809Attach Fitting · crackedFOUND BOTH THE LT AND RT AILERON BALANCE WEIGHT CLIPS CRACKED IN HALF. REMOVED AND REPLACED BALANCE WEIGHT CLIPS IAW KIT NR 129-4036-001.Jul 2, 2009 · N101UE · Beech 1900CSDR IPXA09M56705Skin · damagedINSPECTION TYPE: 1C REPAIR SURVEY SEQ NR 281-W4-03 RT INBD AILERON LWR SKIN EXTERNAL DOUBLER BETWEEN STA XIH329.911 TO XIH335.767, 2 EA FASTENER HEADS PULLED. REMOVED EXISTING REPAIR FROM RT WING INBD AILERON LWR SKIN BETWEEN STA XIH 329.911 TO XIH 335.767. Jul 1, 2009 · N281UP · Doug MD11FSDR ERAA200900002Fitting · crackedWHILE INSPECTING IAW SB27-3928, FLIGHT CONTROLS- AILERON BALANCE WEIGHT CLIP INSPECTION; FOUND ONE CLIP CRACKED ON THE RT AILERON.Jun 22, 2009 · N972EA · Beech 1900DSDR ERAA200900001Fitting · crackedWHILE INSPECTING IAW SB27-3928 FLIGHT CONTROLS- AILERON BALANCE WEIGHT CLIP INSPECTION; FOUND ONE CLIP CRACKED ON LT AILERON.Jun 22, 2009 · N972EA · Beech 1900DSDR MALA090092Skin · debondedDURING 6Y/4Y INSPECTION IN CWA, LY AILERON HAS DISBONDED DENT LOCATED AT WS 340.82 AND 9.5 FROM TRAILING EDGE. REPAIRED IAW S51031.Jun 21, 2009 · N422XJ · Saab 340BSDR Y9PAN610SM609Aileron · delaminatedDURING PRE-FLIGHT OF AIRCRAFT BEFORE DEPARTURE, FOUND RT AILERON WITH SEVERE DELAMINATION, APPROX 6 X 24 INCHES.Jun 15, 2009 · N610SM · Israel ASTRASPXSDR UIEA201000128Aileron · damagedTHE PURPOSE OF THIS EO IS TO RECORD A MAJOR REPAIR. DURING C CHECK INSPECTION BEING PERFORMED AT HKG; DAMAGE WAS FOUND TO THE RIGHT I/B AILERON, O/B AFT CORNER DELAMINATION / DAMAGE. PERMANENT REPAIR PERFORMED IN ACCORDANCE WITH THE 747-400 SRM 51-70-07 FIGUJun 8, 2009 · N498MC · Boeing 74747UFSDR C8GA20090167Skin · delaminatedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE RT OTBD AILERON T/E IS DELAMINATED ON INBD END. DAMAGED AREA WAS REMOVED DIM 3 INCH X 3 INCH, FABRICATED FILLER FROM 2024 T3 .012 INCH DIM 3 INCH X 3 INCH, DOUBLER FROM 2024 T3 .012 INCH DIM 5 INCH X 5 IJun 8, 2009 · N801EA · Boeing 727225SDR C8GA20090166Skin · delaminatedWHILE IN HEAVY MX PERFORMING INSP, IT WAS NOTED THAT THE LT OTBD AILERON T/E IS DELAMINATED ON OTBD END. DAMAGED AREA WAS REMOVED DIM. 8 INCH X 3 INCH, FABRICATED FILLER FROM 2024 T3 .012 INCH DIM 8 INCH X 3INCH, DOUBLER FROM 2024 T3 .012 INCH DIM 8INCH X 5 IJun 8, 2009 · N801EA · Boeing 727225SDR C8GA20090146Skin · delaminatedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE LEFT WING O/B AILERON T/E WEDGE IS DELAMINATED AT THE I/B END. DAMAGED AREA WAS REMOVED DIM 7" X 8". FABRICATED FILLER DIM. 7" X 8" FROM 2024 T3 .012", FABRICATED DOUBLER FROM 2024 T3 .012Jun 8, 2009 · N801EA · Boeing 727225SDR C8GA20090139ASkin · dented"SUPPLEMENTAL INFORMATION" WHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE RIGHT WING O/B AILERON IS DENTED ON THE UPPER T/E WEDGE. DAMAGED AREA WAS REMOVED, FABRICATED DOUBLER FROM 2024 T3 .012" DIM 4" DIA. INSTALLED HOT BOND REPAIR. NOJun 8, 2009 · N801EA · Boeing 727225SDR FDEA200906041912Hinge Bracket · wornFOUND WORN BORES IN HINGE BRACKET A576-61024-201 OF RT ASA. REPAIR PERFORMED BY OVERSIZING THE BORE AND BUSH INSTALLATION IAW RAS/FOK/132/2009 ISS B, APPROVED BY EA 6-5760-131211.Jun 4, 2009 · N746FD · Airbus A300B4622RSDR FDEA200906041911Hinge Bracket · wornFOUND WORN BORES IN HINGE BRACKET A576-61024-200 OF LT ASA. REPAIR PERFORMED BY OVERSIZING THE BORE AND BUSH INSTALLATION IAW RAS/FOK/134/2009 ISS B, APPROVED BY EA 6-5760-131210.Jun 4, 2009 · N746FD · Airbus A300B4622RSDR USAA2009060191360Aileron · delaminatedPHX - RON - MAJOR REPAIR - LOG 4521789 - DELAMINATION WITH PARTIAL SEPARATION ON RIGHT HAND AILERON LOWER LEADING EDGE JUST INBOARD OF OUTBOARD PCA. REPAIRED RIGHT HAND AILERON LOWER LEADING EDGE IAW B757 SRM 57-60-01, 51-70-04, & 51-70-17.May 31, 2009 · N909AW · Boeing 7572G7SDR CA090515002Aileron · obstructed(CAN) INSP OF THE CONTROL SURFACES FOUND THAT AILERONS DO NOT MAKE TRAVEL LIMITS AND PUSH RODS ARE HITTING FWD SPARS OF THE LWR WINGS. ELEVATOR TAB IS UNABLE TO MAKE LIMITS AS STATED. BOTH TRAVEL LIMITS AS STATED IN MM 70206-001 DATED 5-20-1998 PAGE 6 STATE TRMay 15, 2009 · Pitts S2BSDR IPXA09855858Skin · misrepairedINSPECTION TYPE:SVC SURVEY SEQ 852-W3-31 REPAIR DOUBLER AT LT INBD AILERON UPPER EDGE DOES NOT CORRELATE TO SRM REPAIR. REPAIR ACCOMPLISHED PER TIMCO REO-G12538 REV C AND UPS EO DC8-5720-33337-AMay 13, 2009 · N852UP · Doug DC873FSDR M2L2009F00000Hinge Bracket · brokenTHIS PART HAS 2 SMALL 90 DEGREE ANGLES AT EITHER SIDE BOTTOM. THEY HAVE LITTLE OR NO ACTUAL STRENGTH OTHER THAN TO PREVENT THE LOWER WING SKIN FROM NOT BEING SECURED. RT AILERON OTBD HINGE BRACKET. (K)May 11, 2009 · N7520N · Cessna TU206GSDR IPXA09M55886Aileron · misrepairedINSPECTION TYPE:2C REPAIR SURVEY SEQ NR 286-W3-05, EXISTING REPAIR DOUBLER ON LT WING INBD AILERON UPPER LE SKIN AT XIA 318-324 IS INCORRECT MATERIAL GAUGE. REMOVED EXISTING REPAIR DOUBLER, FABRICATED AND INSTALLED REPAIR DOUBLER REF MD11 SRM 57-10-00 FIG 38.May 7, 2009 · N286UP · Doug MD11FSDR C2XA09TY087Bracket · wornRT AILERON DAMPNER LUG MISSING HAT BUSHING. REMOVED AND REPLACED DAMPNER BRACKET IAW EMB 145 SRM 51-40-02.May 6, 2009 · N14543 · Emb EMB145LRSDR C2XA09SH157Support Bracket · damagedSHV - DURING C-CHECK RT AILERON MOST O/B HINGE BRACKET I/B HOUSING DAMAGED. MAINTENANCE REMOVED AND REPLACED RT AILERON MOST O/B HINGE SUPPORT BRACKET ASSY IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.May 4, 2009 · N14930 · Emb EMB145EPSDR QXEA2009050500303Structure · chafedLEFT WING AILERON LEADING EDGE IS CHAFED ON CENTER AND OTBD EDGE. BLENDED DAMAGED AREA REF SRM 57-61-01-101-001-A01. HFEC INSPECTED BLENDED AREA FOR CRACKS IAW NDTM PART 6, 53-00-000-250-A01. NO CRACKS NOTED. UT THICKNESS CHECK IAW NDTM PART 1, 51-20-004 HMay 2, 2009 · N600QX · Cndair CL6002C10SDR C2XA09SH137Attach Fitting · damagedSHV - DURING C-CHECK RT PCA ACTUATOR-TO-AILERON ATTACHMENT FITTING O/B HAT BUSHING MIGRATED. MAINTENANCE REMOVED AND INSTALLED NEW RT PCA ACTUATOR-TO-AILERON ATTACHMENT FITTING IAW EMB-145 SRM 51-40-02 AND IAW EC 5750-01177 REV B. THE AIRCRAFT WAS APPROVED FMay 2, 2009 · N11535 · Emb EMB145LRSDR C2XA09SH136Attach Fitting · damagedSHV - DURING C-CHECK RT PCA ACTUATOR-TO-AILERON ATTACHMENT FITTING O/B ATTACHMENT POINT HAS TOOLING MARKS. MAINTENANCE REMOVED AND INSTALLED NEW RT PCA ACTUATOR-TO-AILERON ATTACHMENT FITTING IAW EMB-145 SRM 51-40-02 AND EC5750-01177 REV B. THE AIRCRAFT WAS AMay 2, 2009 · N11535 · Emb EMB145LRSDR IPXA09M55865Wedge · misrepairedINSPECTION TYPE:C REPAIR SEQUENCE NBR 285-W4-015, RT WING, INBD AILERON INBD T/E, NEEDS VALIDATION FOR REPAIR. BASED UPON COLLECTED INFO, REPAIR SEQ NBR 285-W4-015 DOES NOT CORRELATE TO SRM 57-20-00, FIG3, VOLI, REV40. EXISTING REPAIR WEDGE REMOVED PER SRM 5Apr 23, 2009 · N285UP · Doug MD11FSDR CA090423006Balance Weight · corroded(CAN) AILERON INSP COMPLETED IAW ANNUAL INSP REQUIREMENTS. CORROSION DISCOVERED ON BALANCE WEIGHTS. BALANCE WEIGHTS REMOVED FOR FURTHER INVESTIGATION REVEALED CORROSION ON EACH ATTACH SCREW. CORROSION REMOVED FROM EACH BALANCE WEIGHT, NEW SCREWS INSTALLED AND Apr 23, 2009 · Pilats PC1245SDR C2XA09TY063Bracket · damagedTYS - DURING C-CHECK INSPECTION THE LT AILERON PCA BRACKET OUTBOARD FITTING WAS FOUND DAMAGED/ELONGATED. THE PCA BRACKET WAS REMOVED AND REPLACED IAW EC 5750-0117 AND SRM 57-60-02. A/C STILL IN C-CHECK.Apr 20, 2009 · N12934 · Emb EMB145EPSDR USAA2009042190943Skin · delaminatedBFM - C1 - MAJOR REPAIR - DELAMINATION ON RIGHT OUTBOARD AILERON LOWER SURFACE 12 INCHES INBOARD FROM OUTBOARD END. REPAIRED RIGHT OUTBOARD AILERON LOWER SURFACE IAW B767 SRM 51-60-01.Apr 18, 2009 · N256AY · Boeing 7672B7ERSDR C2XA09SH126Attach Bracket · migratedSHC - DURING C-CHECK RT PCA TO AILERON O/B ROD O/B HAT BUSHING MIGRATED. MAINTENANCE REMOVED AND REPLACED RT PCA TO AILERON ATTACHMENT BRACKET IAW EMB-145 SRM 51-40-02 AND EC5750-01177 REV B. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 16, 2009 · N11106 · Emb EMB145XRSDR C2XA09SH125Attach Bracket · wornSHV - DURING C-CHECK LT PCA TO AILERON ATTACHMENT HAS MIGRATED BUSHING. MAINTENANCE REMOVED AND REPLACED LT PCA TO AILERON ATTACHMENT BRACKET IAW EMB-145 EC5750-01177 REV B. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 16, 2009 · N11106 · Emb EMB145XRSDR C2XA09SH124Attach Bracket · gougedSHV - DURING C-CHECK LT AILERON PCA ATTACH POINT BRACKET O/B ROD ATTACHMENT I/B AND O/B HAT BUSHING HOUSINGS ARE GOUGED. MAINTENANCE REMOVED AND REPLACED LT PCA TO AILERON ATTACHMENT BRACKET IAW EMB-145 EC5750-01177 REV B. THE AIRCRAFT WAS APPROVED FOR RETURApr 16, 2009 · N11106 · Emb EMB145XRSDR C2XA09SH123Attach Bracket · gougedSHV - DURING C-CHECK BRACKET ON THE RT AILERON THAT GOES TO THE PCA IS GOUGED. MAINTENANCE REMOVED AND REPLACED RT PCA TO AILERON ATTACHMENT BRACKET IAW EMB-145 SRM 51-40-02 AND EC5750-01177 REV B. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 16, 2009 · N11106 · Emb EMB145XRSDR C2XA09SH122Attach Bracket · wornSHV - DURING C-CHECK RT AILERON TO PCA BRACKET MOST I/B HAT BUSHING MIGRATED. MAINTENANCE REMOVED AND REPLACED RT AILERON TO PCA ATTACHMENT BRACKET IAW EMB-145 SRM 51-40-02 AND EC5750-01177 REV B. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 16, 2009 · N11106 · Emb EMB145XRSDR C2XA09SH121Attach Bracket · wornSHV - DURING C-CHECK RT PCA TO AILERON I/B ROD O/B HAT BUSHING MIGRATED. MAINTENANCE REMOVED AND REPLACED RT AILERON TO PCA ATTACHMENT BRACKET IAW EMB-145 SRM 51-40-02 AND EC5750-01177 REV B. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 16, 2009 · N11106 · Emb EMB145XRSDR C2XA09SH120Attach Bracket · wornSHV - DURING C-CHECK RT PCA TO AILERON I/B ROD I/B HAT BUSHING MIGRATED. MAINTENANCE REMOVED AND REPLACED RT PCA TO AILERON ATTACHMENT BRACKET IAW EMB-145 SRM 51-40-02 AND EC5750-01177 REV B. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 16, 2009 · N11106 · Emb EMB145XRSDR C2XA09SH119Bracket · wornSHV - DURING C-CHECK LT AILERON DAMPNER BRACKET I/B HAT BUSHING MIGRATED. MAINTENANCE REMOVED AND REPLACED LT AILERON DAMPNER BRACKET IAW SRM 51-40-02. MAINTENANCE PREPPED, PRIMED AND PAINTED LT AILERON DAMPNER BRACKET IAW EMB-145 CPM 51-21-06. THE AIRCRAFTApr 16, 2009 · N11106 · Emb EMB145XRSDR UIEA201000117Skin · damagedTHE PURPOSE OF THIS EO IS TO RECORD A MAJOR REPAIR. DURING C-CHECK INSP; DAMAGE WAS FOUND TO THE RT INBD AILERON UPPER SURFACE OTBD T/E CORNER MEASURING 0.5 IN. X 1.0 IN. (REF FIG 1). PERMANENT REPAIR PERFORMED IAW THE SRM 51-70-06 FIG 5.1. ACCOMPLISH REPAIApr 15, 2009 · N496MC · Boeing 74747UFSDR 2009FA0000327Hinge Bracket · brokenLOWER SUPPORTING ANGLE CRACKED FROM MANY YEARS AND HOURS OF FATIGUE. THIS ACFT HAS BEEN OPERATED ON UNIMPROVED BACK COUNTRY DIRT LANDING STRIPS WHICH POUND AND SHAKE THESE ACFT EXTREMLY. THIS TYPE OF PART FAILURE IS TO BE EXPECTED UNDER THE CONDITIONS THIS AApr 15, 2009 · N206KL · Cessna U206FSDR FDEA200904111267Hinge · corrodedRT AILERON NR 1 HINGE BEARING BORE HAS PITTING CORROSION REMOVED CORROSION FOUND TO BE OUT OF LIMITS. REPAIRED BEARING BORE PER FED EX EA 6-5750-12450 AND RAS/BAE 1009828/2009.Apr 11, 2009 · N814FD · Airbus A310324SDR FDEA200904111266Hinge · corrodedRT AILERON NR 4 HINGE BEARING BORE HAS PITTING CORROSION WITH EXFOLIATION REMOVED CORROSION FROM BORE FOUND TO OUT OF LIMITS. REPAIRED BEARING BORE PER FED EX EA 6-5750-12450 RAS/BAE/1009828/2009.Apr 11, 2009 · N814FD · Airbus A310324SDR IPXA09M55671Skin · gougedINSPECTION TYPE:1C REPAIR SURVEY SEQ 291-W4-07, EXISTING REPAIR DOUBLER ON RT WING I/B AILERON UPPER SKIN BETWEEN XIZ 372.607-375.061 HAS A GOUGE. REMOVED DOUBLER, FABRICATED AND INSTALLED REPAIR DOUBLER IAW IPXA EO MD11-5750-33254-A. ALL WORK ACCOMPLISHED OApr 9, 2009 · N291UP · Doug MD11FSDR SWIA200922031Skin · chafedRIGHT AILERON LEADING EDGE SKIN CHAFED. (C CHECK) REPLACED PER SRM.Apr 8, 2009 · N703SK · Cndair CL6002C10SDR ASAA0945256Aileron · delaminatedLT AILERON LWR BOTTOM I/B EDGE DISBONDED. PREPPED DELAMINATED AREA, BONDED REPAIR IAW B737 400 SRM 51 70 03.Apr 7, 2009 · N793AS · Boeing 737490SDR FDEA200904031167Hinge Fitting · corrodedFOUND CORROSION AND SCRATCHES ON LT AILERON HINGE FITTING. REPAIR PERFORMED BY REAM UP THE HOLE UNTIL DAMAGE REMOVAL AND INSTALLING A BUSHING IAW RAS/FOK/032/2009 ISS A , APPROVED BY EA 6-5750-120232.Apr 3, 2009 · N750FD · Airbus A300B4622RSDR CA090415001Screw · corroded(CAN) AILERONS REMOVED AT ANNUAL INSP. MASS BALANCE WEIGHT SCREWS MS35207-XXX REMOVED ON BOTH AILERONS AND FOUND CORRODED. AREA INSPECTED FOR CORROSION AND NEW SCREWS INSTALLED.Apr 2, 2009 · Pilats PC1245SDR IPXA09655421Fairing · chafedINSPECTION TYPE:C LT WING - I/B AILERON FWD UPPER L/E FAIRING CHAFE DAMAGED. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-17 PARA 4G FIG 18.Mar 31, 2009 · N323UP · Boeing 76734AFSDR C2XA09TY056Fitting · wornRT AILERON OUTBOARD PCA ROD BRACKET OUTBOARD BUSHING HOLE IS OUT OF LIMITS. REMOVED AND REPLACED PCA FITTING IAW EC 5750-01177. AIRCRAFT IS STILL IN C-CHECK.Mar 29, 2009 · N27962 · Emb EMB145SDR AMCR200902Bushing · missingDURING ROUTINE INSP, FOUND TRAIL OF BLACK SOOT STREAMING FROM RT AILERON OTBD HINGE POINT. DISCOVERED BUSH MISSING IN AILERON SIDE OF HINGE WHEN CHECKING FOR PLAY. THE ARE (2) BUSHINGS REQUIRED, BUT ONLY ONE WAS INSTALLED ON AIRFRAME SIDE. OTHER FLIGHT CONTROLMar 26, 2009 · N255DV · Raythn HAWKER800SDR IPXA09B55520Skin · misrepairedINSPECTION TYPE:C REPAIR SEQUENCE NUMBER 259-W4-006 NEEDS VALIDATION FOR REPAIR DUE TO NO CORRELATION WITH SRM. REPAIR DOUBLER & FILLER AT RT WING, INBOARD AILERON TOP FWD O/B SURFACE AT STA XIA 295, REMOVED PER SRM 51-35-01 & 51-31-01 VOL II REV 40 & EN115 2Mar 25, 2009 · N575UP · Boeing 74744AFSDR CA090326010Structure · damaged(CAN) ACFT STRUCK BY LIGHTNING ON APPROACH. LT AILERON TIP REPLACED. P/N-35740407-007.REF:DEF: 836797,836938 AND WO-185137,NR-00001Mar 25, 2009 · Dhav DHC8311
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