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 P5CA9801257Skin · puncturedHOLE IN LOWER SURFACE OF LEFT INBOARD AILERON. CLEANED AREA, REMOVED DAMAGED MATERIAL, AND REPAIRED WITH FIBERGLASS OVERLAYS IAW SRM 51-40-06.Aug 11, 1998 · N857FT · Boeing 747132SDR 99ZZZX713Rib · crackedPRE-FLIGHT DISCLOSED 'CLICKING' NOISE (LIKE OIL CANNING). NOISE ISOLATED AT HINGE ATTACH AREA AT INBOARD END OF LT AILERON. REMOVED HINGE ATTACH HARDWARE TO FACILITATE INSPECTION. RIB CRACKED IN RADIUS OF SPAR ATTACH FLANGE, OTBD OF LOWER ATTACH BOLT FOR HIJul 28, 1998 · N40510 · Piper PA23250SDR 99ZZZX712Spar · crackedPRE-FLIGHT DISCLOSED 'CLICKING' NOISE (LIKE OIL CANNING). NOISE ISOLATED AT HINGE ATTACH AREA AT INBOARD END OF LT AILERON. REMOVED HINGE ATTACH HARDWARE TO FACILITATE INSPECTION. RIB CRACKED IN RADIUS OF SPAR ATTACH FLANGE, OTBD OF LOWER ATTACH BOLT FOR HIJul 28, 1998 · N40510 · Piper PA23250SDR DL72L981530Skin · delaminatedON T/C, FOUND LEFT O/B AILERON DELAMINATED BEYOND SRM LIMITS. REPLACED LT O/B AILERON TRAILING EDGE WEDGE.Jul 22, 1998 · N507DA · Boeing 727232SDR IXXA9800096Plating · corrodedDURING ROUTINE C CHECK INSPECTION, A CORROSION BULGE AND POPPED RIVET HEADS WERE DETECTED ON THE RIGHT AILERON LOWER PLATING BETWEEN STATIONS XA 605 AND XA 622. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED PLATING, FABRICATION AND INSTALLATION OF A NEW LOWER PLATINJul 14, 1998 · N21CX · Doug DC862SDR AU980863Fitting · corroded(AUS) LT AND RT AILERON BALANCE WEIGHT ATTACHMENT AREA CORRODED. ALL BALANCE WEIGHT ATTACHMENT RIVETS WERE REMOVED AND 'AN' NUTS AND BOLTS INSTALLED. PART TOTAL CYCLES: 5,343.Jul 14, 1998 · Cessna 172FSDR MWEA98783Skin · chafedFOUND RIGHT AILERON LOWER SKIN INBOARD EDGE CHAFED. MTC FABRICATED AND INSTALLED REPAIR DOUBLER.Jul 13, 1998 · N809ME · Doug DC982SDR UPS98827115Doubler · crackedRT I/B AILERON INTERNAL DOUBLER IS CRACKED AT ACCESS PNL NR 541. REPAIRED IAW DHC SK 708-207.Jun 26, 1998 · N708UP · Doug DC871FSDR TWAA9810706Aileron · contaminatedLAX - DURING C-CHECK, MAINTENANCE FOUND ON RT WING TOP OF OUTBOARD AILERON WITH INDICATION OF WATER ON THE WHOLE SURFACE. AFTER WATER REMOVED, INSTALLED WET LAYUP PER SRM 51-70-17, PAGE 67 AND PAINTED AREAS. (M)Jun 25, 1998 · N602TW · Boeing 767231SDR TWAA9810205Aileron · contaminatedLAX - DURING CHECK-C, MAINTENANCE FOUND ON TOP OF RT WING, THE OTBD AILERON HAD INDICATION OF WATER ON WHOLE SURFACE. AFTER WATER REMOVED, INSTALLED WET LAYUP PER SRM 51-70-17, PAGE 67, AND PAINTED AREAS. TOTAL TIME: 63,613 HOURS. TOTAL CYCLES: 14,886. (Jun 25, 1998 · N602TW · Boeing 767231SDR UPS98827116Aileron · corrodedINSPECTION TYPE:D, THE LT INBD AILERON HAS AREAS OF LIGHT SURFACE CORROSION THROUGHOUT ENTIRE INNER SURFACE OF FORWARD SPAR AREA. REMOVED AND REPACED THE LT INBD AILERON PER MM 27-11-01.Jun 9, 1998 · N772UP · Doug DC871FSDR DHL9870906CSkin · disbondedAT C CHECK, RIGHT OUTBD AILERON UPPER SURFACE HAS PREVIOUS REPAIR, DISBONDING ATOUTBD END. INSTALLED BONDED REPAIR UPPER AND LOWER PER SRM 51-40-6. NO BALANCE REQ'D PER SRM 51-80-4, N/R 2177.Jun 9, 1998 · N709DH · Boeing 72782CSDR ARWA980705Skin · corrodedLEVEL I CORROSION, ON LT AILERON LOWER SURFACE. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW DC-8 SRM 57-2-0. REMOVED DAMAGED AREA CLEANED SURROUNDING AREA IAW DC-8 SRM 51-1-8. FABRICATED NEW PLATING IAW EO NR CF-N345JW - 12/98 IRDTD 04/24/98. TREATED,Jun 9, 1998 · N345JW · Doug DC863SDR UPS98827470Web · crackedINSPECTION TYPE-C/CK, LEFT HAND INBOARD AILERON, INBOARD WEB, CENTER ACCESS PANEL MATING SURFACE OF THE WEB IS TORN AND CRACKED. FABRICATED REPAIR DOUBLERS AND ALODINED AND PRIMED IAW REO 04825 AND DC8 SRM 51-1-8. INSTALLED REPAIR IAW REO 04825 AND DC8 SRM 5May 29, 1998 · N812UP · Doug DC873FSDR AU980597Fitting · corroded(AUS) RT AILERON HINGE FITTINGS CONTAINED INTERGRANNULAR CORROSION. PART TC: 7,910.May 27, 1998 · Cessna S550SDR 98ZZZX2119Skin · debondedDURING CESSNA PROGRESSIVE CARE INSPECTION, NR 3, NR 4, FOUND STIFFENERS IN BOTH AILERONS. DEBONDED AND AILERON SKIN LOOSE. NO REPAIR POSSIBLE BECAUSE OF NO ACCESS DUE TO SKIN BEING BONDED TO RIBS. EXHANGE OVERHAULED AILERONS WERE INSTALLED DUE TO THE FACT TMay 26, 1998 · N104TP · Cessna 421CSDR AU980598Hinge · broken(AUS) LT AILERON HINGE FLANGE BROKEN. INTERGRANNULAR CORROSION WAS ALSO FOUND IN THE HINGES. PART TC: 7,910.May 25, 1998 · Cessna S550SDR QXEA9800774Skin · damagedLEFTHAND AILERON LOWER SKIN DAMAGED AT INBOARD HINGE ARM OPENING. REPAIRED IAW HORIZON AIR EA 4-27-45.May 22, 1998 · N478US · Fokker F28MK4000SDR QXEA9800809Skin · damagedDAMAGED SKIN, TRAILING EDGE OF LEFTHAND AILERON AT OUTBOARD HINGE OF SPRING TAB. REPAIRED IAW HORIZON AIR EA 9-27-84.May 21, 1998 · N820PH · Dhav DHC8102SDR UPS98226734Aileron · corrodedINSPECTION TYPE:C, R/W O/B AILERON I/B FITTING ON AILERON CORRODED AT ACTUATOR MOUNT ATTACHMENT. REMOVED AND REPLACED AILERON IAW MM 27-10-31.May 15, 1998 · N950UP · Boeing 72725CSDR MALA976460Skin · puncturedDURING REPAIRS IN FFV, RIGHT AILERON HAS PUNCTURE DAMAGE TO UPPER SURFACE COMPOSITE SKIN. MAINTENANCE REPAIRED WITH IAW SRM PRACTICES.May 15, 1998 · N404XJ · Saab 340BSDR AU980827Rib · cracked(AUS) AILERON NOSE RIBS CRACKED. FOUND DURING INSPECTION IAW PIPER SB 1011. PART TOTAL CYCLES: 1,879.May 15, 1998 · Piper PA32R301SDR AU980826Rib · cracked(AUS) AILERON NOSE RIBS CRACKED. FOUND DURING INSPECTION IAW PIPER SB 1011. PART TOTAL CYCLES: 1,879.May 15, 1998 · Piper PA32R301SDR UPS98226737Hinge Fitting · corrodedINSPECTION TYPE:C, CORROSION ON RIGHT WING OUTBD AILERON CENTER OUTBD FIXED TRAILING EDGE HINGE FITTING. REMOVED AND REPLACED HINGE FITTING IAW SRM 51-30-2.May 14, 1998 · N950UP · Boeing 72725CSDR UPS98226736Fitting · corrodedINSPECTION TYPE:C, CORROSION ON RIGHT WING OUTBD AILERON CENTER INBD FIXED TRAILING EDGE HINGE FITTING. REMOVED AND REPLACED HINGE FITTING IAW SRM 51-30-2.May 14, 1998 · N950UP · Boeing 72725CSDR CA980526004Support · cracked(CAN) BOTH LT AND RT LOWER AILERON BELLCRANKS BADLY DAMAGED WHERE THEY ARE BOLTED TO THE RIB. REPAIRED.May 14, 1998 · Piper PA28R200SDR P5CA9800767Fitting · gougedLEFT I/B AILERON I/B PRIMARY HINGE WING FITTING LT SIDE IS GOUGED BY RETAINER BOLT HOLE AREA. BLENDED GOUGE LESS THAN 10 PERCENT MATERIAL LOSS PER SRM 57-50-01.Apr 30, 1998 · N857FT · Boeing 747132SDR 98ZZZX2199Balance Weight · burnedDURING THE UNPACKING PROCEDURE OF THE AILERON BALANCE WEIGHT WHICH IS MADE OF DEPLETED URANIUM MATERIAL, IN ORDER TO BE INSTALLED IN THE AIRCRAFT DURING C-CHECK, IT STARTED TO BURN. THIS PART WAS PROVIDED BY THE AIRCRAFT OPERATOR IN OVERHAULED CONDITION.Apr 30, 1998 · N834LA · Doug DC1010SDR P5CA9800882Skin · corrosionLEVEL 1 CORROSION ON LT WING OUTBD AILERON OUTBD LOWER T/E AREA. CORROSION REMOVED PER SRM 51-10-01 AND SRM 51-10-02.Apr 24, 1998 · N851FT · Boeing 747122SDR 98ZZZX1987Aileron · out of balanceAIRCRAFT WAS STRIPPED AND RE-PAINTED. CONTROL SURFACE BALANCE WAS CHECKED. AILERONS FOUND OUT OF LIMITS AS WELL AS ANOTHER FACTORY PAINTED AILERON. NOTE: AILERON BALANCE LIMITS - 0.0 TO 8.5 INCH/POUND. TRAILING EDGE HEAVY (UNDERBALANCE).Apr 23, 1998 · N2582C · Piper PA38112SDR UPS98826681Skin · crackedINSPECTION TYPE:C/CK, RIGHT AILERON UPPER SKIN OUTBOARD END CRACKED. ROUTED OUT CRACK, FABBED PRIMED AND INSTALLED DOUBLER IAW REO 04658.Apr 16, 1998 · N700UP · Doug DC871FSDR UPS98826673Skin · crackedINSPECTION TYPE:C/CK, RIGHT OUTBOARD AILERON TOP LEADING EDGE AREA AND SKIN CRACKED ON OUTBOARD END. REPAIRED SKIN IAW REO 04658 REO ATTACHED TO UPS NR 542301.Apr 16, 1998 · N700UP · Doug DC871FSDR CALA9800640Hinges · damagedINSPECTION FOUND LEFT OUTBOARD AILERON HINGES DAMAGED. THE HINGES WERE REMOVED AND REPLACED IAW SRM 51-30-2.Apr 7, 1998 · N15774 · Boeing 727227SDR ASAA9840059Skin · delaminatedSEA - DURING C-CHECK, THE RT AILERON LOWER SKIN WAS FOUND TO BE DELAMINATED. REPAIRED PER EA 5760-01010 AND BOEING TELEX ASA-SEA-98-0063RR. (M)Mar 31, 1998 · N762AS · Boeing 7374Q8SDR TWAA9807301Skin · corrodedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND UPPER TE PANEL FORWARD OF RT WING AILERON UPPER SURFACE, OUTBOARD AREA HAD SEVERAL FASTENER HEADS STRESSED AND ALL SKIN PILLOWING. REPLACED TE SKIN PANEL, NEW PANEL INSTALLED PER SRM 51-01. (M)Mar 27, 1998 · N997Z · Doug DC932SDR 98ZZZX1541Spar · crackedINSPECTION FOUND AILERON SPARS CRACKED. LOCATION: INBOARD HINGE BRACKET ATTACH POINT. LT AILERON HAD .75 INCH CRACK. RT AILERON HAD 2.25 INCH CRACK. CAUSE COULD BE RELATED TO TOTAL TIME.Mar 27, 1998 · N307CL · Gulstm 690BSDR 98ZZZX1540Spar · crackedINSPECTION FOUND AILERON SPARS CRACKED. LOCATION: INBOARD HINGE BRACKET ATTACH POINT. LT AILERON HAD .75 INCH CRACK. RT AILERON HAD 2.25 INCH CRACK. CAUSE COULD BE RELATED TO TOTAL TIME.Mar 27, 1998 · N307CL · Gulstm 690BSDR CA980402021Spar · cracked(CAN) AILERON FRONT SPAR FOUND CRACKED. FOUND DURING REBUILD. AD 96-21-03 MANDATED SB 974 THE INSTALLATION OF BRACKET WHICH TERMINATED REPEAT INSPECTION. REPAIRED.Mar 25, 1998 · Piper PA31SDR CA980402020Spar · cracked(CAN) AILERON FRONT SPAR FOUND CRACKED. FOUND DURING REBUILD. AD 96-21-03 MANDATED SB 974 THE INSTALLATION OF BRACKET WHICH TERMINATED REPEAT INSPECTION. REPAIRED.Mar 25, 1998 · Piper PA31350SDR CA980402019Spar · cracked(CAN) AILERON FRONT SPAR FOUND CRACKED. FOUND DURING REBUILD. AD 96-21-03 MANDATED SB 974 INSTALLATION OF BRACKET WHICH TERMINATED REPEAT INSPECTION. REPAIRED.Mar 25, 1998 · Piper PA31350SDR CA980330023Spar · cracked(CAN) SB 974 HAD BEEN COMPLIED WITH AS TERMINATING ACTION FOR AWD 96-21-03. NEW PARTS WERE INSTALLED. CRACK WAS FOUND AS A RESULT OF A FLEET INSPECTION AFTER CRACKS FOUND ON ANOTHER AIRCRAFT. REF: SDR CA98033021, SDR CA98033022. AIRCRAFT TT: 8,362 HOURSMar 25, 1998 · Piper PA31350SDR CA980330022Spar · cracked(CAN) PIPER SB 974 HAD BEEN COMPLETED AND HINGE P/N 74461-02 HAD BEEN INSTALLED. THIS WAS TERMINATING ACTION FOR AWD 96-21-03. THE CRACK WAS FOUND DURING A RE-SKINNING OF THE AILERON. FOUR OTHER AILERONS ON THE FLEET WERE INSPECTED AND THREE WERE FOUND CRACMar 25, 1998 · Piper PA31350SDR CA980330021Spar · cracked(CAN) PIPER SB 974 HAD BEEN COMPLETED AS TERMINATING ACTION FOR AWD 92-21-03. NEW HINGE INSTALLED. CRACK WAS FOUND AS A RESULT OF A FLEET INSPECTION DUE TO CRACKING OF ANOTHER AIRCRAFT IN THE FLEET. REF: SDR CA980330022, SDR CA980330023. AIRCRAFT TT: 12,Mar 25, 1998 · Piper PA31SDR 98FDEA00215Skin · damagedRT OUTBD AILERON HAS .25 INCH DIAMETER CHERRY MAX IN UPPER SKIN, COUNTER SINK IS TOO DEEP, IN SKIN .040 THICK. REMOVED DAMAGE AND INSTALLED FLUSH DOUBLER PER SRM 57-50-5 AND CUT OUT RIB AREA TO FACILITATE DOUBLER AND INSTALLED TYPICAL FORMED SECTION REPAIR TOMar 18, 1998 · N268FE · Boeing 727233SDR 98FDEA00214Rivets · looseNR 0324, RT WING OUTBOARD AILERON HAS APPROX 70 RIVETS WORKING AND LOOSE ALONG UPPER SKIN FRONT SPAR ATTACHMENT. REMOVED AND REPLACED RIVETS PER EA 7-5750-29411, SRM 57-50-5 SRM 51-30-2.Mar 18, 1998 · N268FE · Boeing 727233SDR 98FDEA00211Skin · damagedNR 0905, RT OUTBD AILERON HAS .25 INCH DIAMETER CHERRY MAX FASTENER IN UPPER SKIN, RIB IS .600 WIDE, ORIGINAL FASTENERS WERE .125 INCH DIAMETER, COUNTER SINK INTO RIB WILL HAVE DAMAGED RIB AND MINIMUM ED IS LOST IN RIB. REMOVED AND REPLACED RIB PER SRM 51-10-Mar 18, 1998 · N268FE · Boeing 727233SDR 98FDEA00210Spar Web · crackedNR 0901, RT AILERON, OUTBOARD HAS CRACK IN SPAR WEB AT FASTENER HOLE. THIS REPAIR TIED TO REPAIR BEING PERFORMED ON NR0324. STOP DRILLED CRACK AND FABRICATED DOUBLER AND INSTALLED REPAIR PER EA 7-5750-29411.Mar 18, 1998 · N268FE · Boeing 727233SDR CALA9800442Skin · dentedINSPECTION FOUND LT OUTBOARD AILERON OUTBOARD UPPER TRAILING EDGE HAD A PREVIOUSLY FILLED SMALL DENT WITH FILLER BREAKING OUT. THE DENTED AREA WAS CUT OUT AND A HOT BONDED REPAIR WAS INSTALLED IAW SRM 51-40-6.Mar 13, 1998 · N17410 · Boeing 727243SDR 98FDEA00186Rib · damagedNR 0905 RT OUTBD AILERON HAS .25 DIA CHERRY MAX FASTENER IN UPPER SKIN, RIB IS .600 WIDE, ORIGINAL FASTENERS WERE .125 DIA COUNTER SINK INTO RIB WILL HAVE DAMAGED RIB AND MINIMUM ED IS LOST IN RIB. REMOVED AND REPLACED RIB PER SRM 51-10-1. SKIN REPAIR ACCOMPMar 12, 1998 · N268FE · Boeing 727233SDR UPS98226075Casting · crackedINSPECTION TYPE-C, CRACK ON RIGHT HAND AILERON LOCKOUT CASTING. CASTING REPLACED IAW DRAWING 65-21779 AND SRS ENGINEERING ORDER 98-0 6-005.Mar 9, 1998 · N926UP · Boeing 72731C
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