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 CA010108020Seal · contaminated(CAN) PILOT REPORTED OF FROZEN AILERONS AT CRUISE ALTITUDE. AIRCRAFT RETURNED TO BASE. DURING DESCENT PILOT WAS ABLE TO REGAIN CONTROL. INVESTIGATION FOUND EXCESIVE AMOUNT OF WATER IN AILERON BRUSH SEALS. BRUSH SEALS CLEANED, DRIED AND RE-LUBRICTED PER M.M. 27Dec 2, 2000 · Lear 35ASDR SWAA002529Aileron · delaminatedFOUND RT AILERON DELAMINATED. R&R AILERON PER MM.Dec 2, 2000 · Boeing 7372H4SDR CA010118012Stop · bent(CAN) LEFT AND RIGHT AILERON STOPS FOUND SEVERELY BENT. POSSIBLE WING DAMAGE.Dec 1, 2000 · Amrgen AA5BSDR RRXA003553Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LT WING T/E FWD OF I/B AILERON O/B PANEL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////OPEN/////Nov 28, 2000 · N795FT · Doug DC873FSDR ASAA0040133Fitting · gougedPAE - DURING SI CHECK, FOUND LEFT AILERON INBOARD HINGE FITTING A/C SIDE WAS GOUGED ON INBOARD LUG OUTBOARD SIDE. REPAIRED IAW ASA EA5750-01491. (M)Nov 17, 2000 · N775AS · Boeing 7374Q8SDR UPS00234489Fitting · brokenINSPECTION TYPE:C, AFTER RIGHT O/B AILERON TAB REMOVAL FOUND O/B FITTING FOR TAB HINGE B-RING BROKEN. REPLACED FITTING IAW DRG 65-21766.Nov 17, 2000 · N937UP · Boeing 72725CSDR L1GA200000468Aileron · nickedTWO NICKS ON AILERON RT AILERON LEADING EDGE TOP SURFACE. INSTALLED FILLER AND DOUBLER AND REBALANCED SURFACE AFTER REPAIR.Nov 14, 2000 · N12510 · Doug DC932SDR F3LA200000257Hinge · crackedDURING C-5 CHECK, INSPECTION REPORTED CENTER HINGE FOR RT AILERON CASTING CRACKED AT WING FIXED TRAILING EDGE PANEL SCREW HOLE. MAINTENANCE REMOVED CASTING PER SRM 51-30-2, LOCATED AND DRILLED NEW CASTING PER SRM 51-10-1 AND INSTALLED PER SRM 51-30-2.Oct 30, 2000 · N237TR · Boeing 737228SDR RRXA003239Access Panel · delaminatedDURING A MAINTENANCE VISIT FOUND DELAMINATION TO THE LT UPPER AILERON ACCESS PANEL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 19, 2000 · N500MH · Doug DC871FSDR 20001109SH009Aileron · crackedDURING INSPECTION, 3 EACH .25 INCH LONG CRACKS WERE FOUND ON THE LEADING EDGE AT THE FASTENERS USED TO SECURE THE AILERON BALANCE WEIGHT. AFTER THE LEADING EDGE WAS REMOVED FROM THE AILERON AS PART OF THE REPAIR, A .75 INCH LONG CRACK WAS FOUND IN THE LOWER IOct 13, 2000 · Gulstm 690BSDR 20001012SH008Hinge Bracket · crackedFOUND BOTH INBOARD AILERON HINGE BRACKETS CRACKED COMPLETELY THROUGH THE BEARING BOSS. THESE BRACKETS WERE MADE FROM MAGNESIUM AND SUFFER CORROSION PROBLEMS. APPROXIMATELY 40 POUNDS OF PRESSURE SEPARATED THE AILERON FROM ITS HINGE/ATTACH ON THE INBOARD END. Oct 12, 2000 · N4339V · Cessna 190SDR 20001012SH007Hinge Bracket · crackedFOUND BOTH INBOARD AILERON HINGE BRACKETS CRACKED COMPLETELY THROUGH THE BEARING BOSS. THESE BRACKETS WERE MADE FROM MAGNESIUM AND SUFFER CORROSION PROBLEMS. APPROXIMATELY 40 POUNDS OF PRESSURE SEPARATED THE AILERON FROM ITS HINGE/ATTACH ON THE INBOARD END. Oct 12, 2000 · N4339V · Cessna 190SDR RRXA003278Fitting · crackedDURING A MAINTENANCE VISIT FOUND A GOUGE AND POSSIBLE CRACK TO THE O/B AILERON O/B HINGE POINT FITTING, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. BLENDED DAMAGE AREA AND RETURNED TO SERVICE IAW EOOct 10, 2000 · N500MH · Doug DC871FSDR RRXA003276Fitting · gougedDURING A MAINTENANCE VISIT FOUND A GOUGED PULLEY CLUSTER FITTING ON O/B SIDE I/B AILERON, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. DLENDED DAMAGED AREA AND RETURNED TO SERVICE IAW EO#00-257 WITH AOct 10, 2000 · N500MH · Doug DC871FSDR 20010112SG020Structure · damagedLOWER SURFACE OF INBOARD AILERON, STATION XW 060 HAS 24 INCHES CHORDWISE TEAR IN SKIN DUE TO ENGINE FAILURE. REMOVED AND REPLACED LEFT INBOARD AILERON IAW 27-10-01. (M)Oct 5, 2000 · N601GC · Doug DC1030FSDR 00FDEA00702Support Fitting · crackedDURING ROUTINE INSP, LEFT O/B AILERON NR 3 ATTACHMENT SUPPORT FOUND CRACKED. REMOVED AND REPLACED PER IAW BAC 727 SRM 51-30-2.Oct 4, 2000 · N188FE · Boeing 72722SDR RRXA003094Skin · puncturedDURING A MAINTENANCE VISIT FOUND A PUNCTURE TO THE LEFT WING CONTROL TAB ON I/B AILERON T/E, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Sep 22, 2000 · N957R · Doug DC863FSDR TWAA0015004Skin · damagedDURING OP 16 MAINT CHECK ON THE LT WING, TOP T/E 24 INCHES FROM O/B END OF O/B AILERON HAD BURNED/DAMAGED SPOT. REWORKED PER SRM 57-60-02, FIG 201, SHEET 2, AND SRM 51-70-03, FIG 1.Sep 22, 2000 · N650TW · Boeing 767205SDR RRXA003102Access Panel · crackedDURING A MAINTENANCE VISIT FOUND A CRACK AND DEFORMED ON THE I/B AILERON BOTTOM SIDE ACCESS PANEL FOR CONTROL TAB/POWER PACK TIE-IN, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Sep 21, 2000 · N957R · Doug DC863FSDR RRXA003116Skin · crackedDURING A MAINTENANCE VISIT FOUND A CRACK ON THE CORNER OF THE I/B AILERON I/B TAB T/E, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Sep 20, 2000 · N957R · Doug DC863FSDR SWAA001794Skin · crackedDURING SCHEDULED D-CHECK, FOUND LT AILERON UPPER SKIN CRACKED ALONG INBOARD END 4.5 FROM L/E. REPAIRED AILERON SKIN PER SRM.Sep 20, 2000 · N352SW · Boeing 7373H4SDR 20001026SH012Skin · crackedON 5-15-00, LEFT AILERON SKIN FOUND CRACKED AT OUTBOARD AFT EDGE UNDERSIDE. UPON FURTHER INSPECTION, FOUND THE SKIN TO BE VERY BRITTLE. ON 9-10-00, FOUND RIGHT AILERON SKIN CRACKED AT SKIN LAP AFT OF CENTER ATTACH POINT BOTH UPPER AND LOWER. SKIN FOUND TO BSep 15, 2000 · N901JA · Beech C90SDR QXEA0002550Structure · damagedYXX- LEFT HAND AILERON COMPOSITE TIP DAMAGED. REPAIRED IAW DHC-8 SRM 51-40-00.Sep 15, 2000 · N824PH · Dhav DHC8102SDR QXEA0002551Structure · damagedYXX- LEFT HAND AILERON TIP, UNDERLYING STRUCTURE FOR COMPOSITE TIP HAS DAMAGE TO MOUNTING FLANGE. REPAIRED IAW DHC-8 SRM 51-40-00 AND SRM 51-22-00, PAGE 5.Sep 14, 2000 · N824PH · Dhav DHC8102SDR 20000920SH007Hinge · misinstalledOUTER HINGE ATTACHMENT SCREWS ON THE LOWER SIDE WERE HOT. INSTALLED THROUGH THE HINGE ASSEMBLY, BUT THROUGH THE SKIN ONLY. SCREWS WERE HELD IN BY THE SKIN AND BACKSIDE OF COCKED HINGE. PROBLEM WAS DISCOVERED FROM RESPONSE TO BEECH MAINTENANCE ALERT MA00-03,Sep 8, 2000 · N249CR · Beech 58PSDR EISA20000160Skin · separatedLEFT WING O/B AILERON O/B TRAILING EDGE CORNER METAL SEPARATED. REMOVED, FABRICATED SKIN DOUBLERS AND FILLERS, BONDED, ALODINED, AND PRIMED SKIN DOUBLERS AND FILLERS IAW B727-200 SRM 51-10-, 51-20-1, 51-40-5, 51-40-6, 57-50-2 AND B727-200 MM 51-20-151.Aug 31, 2000 · N12305 · Boeing 727231SDR EISA20000159Skin · gougedLT WING O/B AILERON T/E LOWER SURFACE HAS GOUGE. REMOVED, FABRICATED REPAIR DOUBLERS AND FILLERS, BONDED, ALODINED, PRIMED IAW B727-200 SRM 51-10-2, 51-20-1, 51-40-5, 51-40-6, 57-50-2, AND B727-200 MM 51-20-151.Aug 31, 2000 · N12305 · Boeing 727231SDR C2XA00IA262Skin · delaminatedIAH - DURING C-CHECK INSPECTION, THE RIGHT AILERON WAS FOUND TO HAVE LIGHTNING STRIKE DAMAGE OUTBOARD OF THE OUTBOARD STATIC WICK. MAINTENANCE REMOVED AND REPLACED THE AFFECTED AILERON, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Aug 23, 2000 · N13929 · Emb EMB145ERSDR CALA0001454Skin · gougedRIGHT AILERON LOWER SURFACE SKIN IS GOUGED (.5 INCH) AT LEADING EDGE 18 INCHES OUTBOARD OF DAMPERS. REMOVED AILERON IAW MD-80 MM 27-10-01, REPAIRED AILERON IAW MD-80 SRM 57-01 FIG 5 SHEET 2, PERFORMED WEIGHT AND BALANCE IAW SRM 57-50-01, WEIGHT AND BALANCE ISAug 15, 2000 · N13891 · Doug DC982SDR CALA0001445Skin · gougedRT AILERON LWR SURFACE SKIN IS GOUGED AT L/E APPROX 18 INCHES O/B OF DAMPERS. REMOVED AILERON IAW MD-80 MM 27-10-01. REPAIRED AILERON IAW MD-80 SRM 57-01 FIG 5 SHEET 2, PERFORMED WEIGHT AND BALANCE IAW SRM 57-50-01, WEIGHT AND BALANCE IS WITHIN LIMITS. INSAug 15, 2000 · N13891 · Doug DC982SDR EISA20000109Bracket · crackedDURING ROUTINE C-CHECK INSPECTION, RIGHT O/B AILERON LOCKOUT MECHANISM ATTACHING BRACKET IS CRACKED. REMOVED AND REPLACED AILERON LOCKOUT BRACKET. RIGGED RT AILERON LOCKOUT IAW B727 SRM 51-30-2, MM 27-10-121 AND 27-10-131.Aug 9, 2000 · N6815 · Boeing 727223SDR SWAA001484Skin · crackedDURING SCHEDULED 1/2D CHECK, FOUND LT AILERON UPPER SKIN CRACKED. REMOVED AND REPLACED LT AILERON PER MM.Aug 6, 2000 · Boeing 7372H4SDR 20000828SH030Hinge · crackedRIGHT AILERON CENTER HINGE CRACKED FROM CORROSION INSIDE THE RIGHT AILERON. (X)Aug 3, 2000 · N304CW · Piper PA34200TSDR DHL200080580CSkin · deformedRIGHT WING O/B AILERON LOWER SKIN COVERS DEFORMED AT XW 420.000. REMOVED DEFORMED COVER PER SRM 57-2-0. FABRICATED COVER PER SRM 57-2-1. CLEANED, TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED NEW COVER PER SRM 57-2-1.Jul 28, 2000 · N805DH · Doug DC873FSDR F3LA00159Skin · delaminatedDEN - DURING C-2 CHECK, INSPECTION REPORTED LEFT AILERON INBOARD BOTTOM CORNER IN HINGE AREA DELAMINATED IN THREE PLACES. MAINTENANCE REPLACED LEFT AILERON PER MM 27-11-11. (X)Jul 26, 2000 · N578US · Boeing 737301SDR RRXA003771Structure · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE R/H UPPER TRAILING EDGE I/B AILERON PANEL 565G, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW PANEL AND INSTALLED IAW DC-8 SRM 51-3Jul 19, 2000 · N811AL · Doug DC871SDR RRXA002864Structure · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AND SHEARED FASTENERS ON THE LWR SURFACE AT THE I/B SIDE ON THE LT WING O/B AILERON, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAWJul 12, 2000 · N796FT · Doug DC873FSDR DHL200070914CSkin · delaminatedRIGHT WING T/E LOWER PANEL O/B OF I/B AILERON SHOWS DELAMINATION AREA AT I/B END. REMOVED PANEL FOR COMPOSIT REPAIR PER SRM 51-30-2. INSTALLED COMPOSIT REPAIR PER SRM 51-40-6. INSTALLED REPAIRED PANEL PER SRM 51-30-2.Jul 7, 2000 · N709DH · Boeing 72782CSDR 00FDEA00419Skin · corrodedLEFT WING O/B AILERON LWR SKIN IS CORRODED AFT OF CENTER HINGE POINT. *S/D* REMOVED AND REPLACED PER SRM 51-00-01.Jul 3, 2000 · N377FE · Doug DC1010FSDR 00FDEA00418Skin · corrodedSKIN BULGING AROUND FASTENERS ON LWR SURFACE OF RT O/B AILERON. FOUND CORROSION BETWEEN SKIN AND FINGER DOUBLER. *S/D* REMOVED AND REPLACED LWR SURFACE SKIN OF RT O/B AILERON REF SRM 51-00-01.Jul 1, 2000 · N377FE · Doug DC10*SDR GAIA00372Attach Fitting · crackedDURING ROUTINE C-CHECK, MAINTENANCE FOUND THE LEFT AILERON TAB, OUTBOARD ATTACH HINGE CRACKED. INSTALLED ATTACH HINGE IAW BOEING 727 SRM 57-50-11. DOCUMENTED ON TIMCO NON ROUTINE 23300 W/O 101026. AIRCRAFT WAS RETURNED TO SERVICE. (M)Jun 30, 2000 · N751US · Boeing 727214SDR CA000714032Skin · cracked(CAN) CRACK DISCOVERED ON THE TOP OF THE AILERON SKIN.SKIN REPLACED.AILERON REINSTALLED.Jun 22, 2000 · Beech B100SDR MWEA00494Rib · crackedMKE - NR 4 FROM OUTBOARD SIDE RIB CRACKED ON RIGHT AILERON. FABRICATED AND INSTALLED RIB. (X)Jun 20, 2000 · N700ME · Doug DC914SDR MWEA00517Skin · crackedMKE - OUTBOARD UPPER AFT SECTION OF RIGHT AILERON HAD A .50 INCH CRACK IN THE COMPOSITE MATERIAL. FABRICATED AND INSTALLED NEW TRAILING EDGE. (X)Jun 20, 2000 · N700ME · Doug DC914SDR MWEA00495Panel · gougedMKE - RIGHT AILERON MOST OUTBOARD LEADING EDGE ACCESS PANEL IS GOUGED. FABRICATED AND INSTALLED REPAIR DOUBLER. (X)Jun 20, 2000 · N700ME · Doug DC914SDR CALA0000934Skin · dentedINSPECTION FOUND LT AILERON UPPER SURFACE DENTED. A DOUBLER WAS INSTALLED IAW SRM 57-01. AN ADJUSTMENT TEST OF AILERON TRIM AND CONTROL TABS WAS PERFORMED IAW MM 27-10-05.Jun 20, 2000 · N819NY · Doug DC982SDR CA000706025Aileron · cracked(CAN) DURING REPETITIVE AILERON STRUCTURE INSPECTION, FOUND SKIN CRACKS ALONG FORWARD/AFT UPPER AND LOWER SKIN LAP JOINTS. CRACKS (2 FOUND INITIALLY) RUN LATERALLY ALONG LAP JOINT. ON SKIN REMOVAL, FOUND CORROSION UNDER SKIN AND 5 CRACKS VERYING FROM LESS THJun 17, 2000 · Beech 100BEECHSDR UPS00233159Spar · puncturedINSPECTION TYPE: C+SI. LT IB AILERON REAR SPAR IS PUNCTURED. REMOVED AILERON AND TAB IAW MM 27-10-01. REPAIR CARRIED OUT IAW SRM 5 1-40-2 FIG 1.Jun 9, 2000 · N954UP · Boeing 727185CSDR UPS00233156Fitting · corrodedINSPECTION TYPE: C+SI. LT OB AILERON, IB END FITTING IS BADLY CORRODED AROUND ATTACH LUG FOR AILERON OPERATING ROD. REPLACED AILERON CASTING IAW DRW 65-21766.Jun 9, 2000 · N954UP · Boeing 727185CSDR UPS00233153Fitting · corrodedINSPECTION TYPE:C+SI. LT OB AILERON 2 ND HINGE SUPPORT FITTING FROM IB IS BADLY CORRODED REPLACED FITTING IAW DRW NR 65-21708Jun 9, 2000 · N954UP · Boeing 727185C
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