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 DLM11991113Skin · delaminatedLEFT O/B AILERON / FRONT SPAR / LWR FLANGE / XDA 928: TOOLING DAMAGE TO LOWER SPAR FLANGE. SPAR IS M/F SOLID GRAPHITE LAMINATE, APPROX .208 THICK. LOWER FLANGE IS DELAMINATED THROUGH THICKNESS OVER APPROX 1 INCH DEPTH (CHORD-WISE) X 2 WIDTH (SPAN-WISE). RMay 13, 1999 · N809DE · Doug MD11SDR AU990919Bracket · corroded(AUS) RIGHT AILERON CONTROL UNIT LOWER MOUNT BRACKET CORRODED.May 10, 1999 · Fokker F28MK4000SDR UF6A990539Stringer · crackedSBN - RIGHT AILERON UPPER STRINGER NR 2 AT STATION 342.696 WAS FOUND TO BE CRACKED. MAINTENANCE FABRICATED NEW STRINGER FROM RIB 333.454 TO 359.216. AREA WAS ALODINED, PRIMED AND FINISHED PER FACTORY SPECIFICATIONS. ALL WORK WAS DONE IAW BAE ATP SRM 51-10-0May 9, 1999 · N857AW · Bag ATPSDR UPS99229647Casting · corrodedINSPECTION TYPE:C, RIGHT O/B AILERON TAB ROD HINGE CASTING CORRODED. HINGE CASTINGS REMOVED AND REPLACED IAW MM 27-10-41.May 5, 1999 · N921UP · Boeing 727180CSDR UPS99229628Hinge · corrodedINSPECTION TYPE:C, RIGHT I/B AILERON CENTER HINGE FITTING CORRODED. REPLACED HINGE FITTING IAW MM 27-10-01.May 5, 1999 · N921UP · Boeing 727180CSDR UF6A990518Skin · tearSBN - RIGHT AILERON HAS A SMALL TEAR IN THE OUTER SKIN AT THE RADIUS OF THE CENTER HINGE. MAINTENANCE BURNISHED TEAR AND WAS FOUND WITHIN IAW BAE ATP SRM 51-10-01. AREA WAS ALODINED AND PRIMED. (M)May 5, 1999 · N857AW · Bag ATPSDR TWAA9906302Rib · crackedDURING OP 16 MAINT CHECK, FOUND RT AILERON RIB WITH DENT AND .25 INCH IN LONG CRACK, APPROX 10 IN FROM OTBD END AND 5 IN FROM LE. ACCOMPLISHED HFEC TO LOCATE ENDS OF CRACK. REPAIRED PER SRM 53-01, PAGE 10 FIG 2 SHEET 4.Apr 28, 1999 · N986Z · Doug DC931SDR 99FDEA00152Hinge · corrodedNR 417 76C030-00 RT WING OUTBD AILERON-HINGE CASTING HAS DEEP PITTED CORROSION IN MAGNESIUM CASTING. REMOVED AND REPLACED CASTING WITH NEW SAND CASTED ALUM CASTING PER DRW BOEING NR 65-12959 AND FASTENERS IAW SRM 51-30-2 AND STANDARD PRACTICE.Apr 21, 1999 · N150FE · Boeing 72722SDR 99FDEA00151Hinge · corrodedNR 415 76C030-00, RT WING-OUTBD AILERON 2ND AILERON HINGE OB HING CASTING HAS DEEP PITTED CORROSION TO MAGNESIUM CASTING. REMOVED AND REPLACED CASTING WITH NEW TYPE SANDCAST ALUM IAW BOEING INSTALL DRAW NR 65-19260 AND FASTENERS WITH SRM 51-30-2 AND STANDARD Apr 21, 1999 · N150FE · Boeing 72722SDR ABXA9900363Skin · crackedDURING C-CHECK, FOUND RIGHT AILERON SKIN TRAILING EDGE CRACKED. REPLACED RIGHT AILERON SKIN TRAILING EDGE IAW DC9 SRM 51-30-08.Apr 20, 1999 · N952AX · Doug DC941SDR DHL9970153DFitting · crackedAT D-CHECK, LEFT WING O/B AILERON O/B HINGE FITTING CRACKED AT AFT UPPER END AT SKIN ATTACH FLANGE. REMOVED O/B HINGE FITTING AT LEFT WING PER SRM 51-30-2. REPLACED O/B HINGE FITTING PER SRM 57-30-2.Apr 16, 1999 · N701DH · Boeing 72730CSDR CALA9900407Skin · crackedINSPECTION FOUND A .5 AND .375 INCH CRACK IN LT O/B AILERON LOWER SKIN WITH A BEND AT I/B EDGE. THE AILERON WAS REMOVED AND REPLACED IAW MM 27-10-31.Apr 14, 1999 · N17402 · Boeing 727243SDR UPS99229439Hinge · corrodedINSPECTION TYPE:C+SI, RT I/B AILERON CENTERING HINGE CORRODED. CENTERING HINGE REMOVED AND REPLACED IAW 27-10-01.Apr 13, 1999 · N922UP · Boeing 72731CSDR 99FDEA00187Hinge · corrodedNR 417 RT WING, OTBD AILERON HINGE CASTING HAS DEEP PITTED CORROSION IN MAGNESIUM CASTING. REMOVED AND REPLACED CASTING WITH NEW SAND CASTED ALUM CAST PER DRW BOEING NR 65-15959 AND FASTENERS IAW SRM 51-30-2 AND STANDARD PRACTICES.Apr 9, 1999 · N150FE · Boeing 72722SDR 99FDEA00186Hinge · corrodedNR 415, RT, WING OTBD AILERON 2ND HINGE O/B HINGE CASTING HAS DEEP PITTIED CORROSION TO MAGNESIUM CASTING. REMOVED AND REPLACED CASTING WITH NEW TYPE SANDCASTING ALUMINUM IAW BOEING INSTALL DRW NR 65-19260 AND FASTENERS IAW SRM 51-30-2 AND STANDARD PRACTICES.Apr 9, 1999 · N150FE · Boeing 72722SDR 99ZZZX2102Rib · crackedDURING THE NORMAL INSPECTION INTERVAL, CRACKS WERE FOUND IN THE WING RIBS WHERE THE INBOARD AILERON HINGE PLATES (PN 105-100011-51) AND THE OUTBOARD AILERON HINGE PLATES (P/N 105-100011-51) ATTACH. THE SAME PROBLEM HAS BEEN FOUND ON OTHER AIRCRAFT OF SAME MODApr 5, 1999 · N6717Y · Beech 76SDR UPS99229224Fitting · corrodedINSPECTION TYPE:C, LEFT WING OUTBOARD AILERON CENTER OUTBOARD HINGE FITTING CORROED (AILERON SIDE). REPLACED PER SRM 51-30-2.Apr 2, 1999 · N915UP · Boeing 72727CSDR UPS99229210Fitting · corrodedINSPECTION TYPE:C LEFT WING OUTBOARD AILERON CENTER INBOARD HINGE FITTING CORRODED AILERON SIDE. REPLACED HINGE FITTING PER SRM 51-30-2.Apr 2, 1999 · N915UP · Boeing 72727CSDR DHL9970103DCasting · corrodedAT D-CHECK, LEFT WING I/B AILERON LOWER INPUT CASTING IS CORRODED. REMOVED AND REPLACED CASTING PER SRM 59-50-1. REBALANCE NOT REQD PER SRM 51-80-1. RERIGGED PER MM 27-10-0.Mar 29, 1999 · N701DH · Boeing 72730CSDR DHL9970154DCasting · corrodedAT D-CHECK, LEFT AILERON LOCKOUT SUPPORT CASTING IS PITTED AT ALL THRU BOLT ATTACH POINTS. REMOVED AND REPLACED SUPPORT CASTING PER SRM 51-30-2.Mar 28, 1999 · N701DH · Boeing 72730CSDR CALA9900333Skin · corrodedINSPECTION FOUND RT WING O/B AILERON LOWER SKIN CORRODED. THE AILERON WAS REMOVED AND REPLACED IAW MM 27-10-02.Mar 27, 1999 · N12061 · Doug DC1030SDR UPS99229353Skin · damagedINSPECTION TYPE:C+SI, LT I/B AILERON HAS DAMAGE ON UPPER SKIN AT FWD O/B END. DAMAGED AREA TRIMMED IAW SRM 57-50-5.Mar 24, 1999 · N922UP · Boeing 72731CSDR DHL9980748CHinge · crackedAT C CHECK, LT WING AILERON HINGE NR 6 HAS CRACK ON AILERON MOUNT FLANGE. REMOVED HINGE AND INSTALLED NEW HINGE PER MM 27-10-1. N/R 896Mar 15, 1999 · N807DH · Doug DC873FSDR DHL9980708CPanel · crackedAT C-CHECK, LT I/B AILERON I/B LOWER SURFACE ON ACCESS PANEL HAS CRACKED PLATE. FABRICATED REPAIR DOUBLER AND INSTALLED PER SRM 51-1-21, 5 X 4.Mar 14, 1999 · N807DH · Doug DC873FSDR ABXA9900326Fitting · crackedRIGHT WING INBOARD AILERON, INBOARD ATTACH FITTING IS BROKEN OFF ON AILERON SIDE. REPLACED FITTING IAW DC8 SRM 27-10-00.Mar 14, 1999 · N813AX · Doug DC863SDR UPS99228977Skin · corrodedINSPECTION TYPE-C, RT OUTBOARD AILERON HAS CORROSION ON LOWER SKIN AFT OF NR 2 HINGE AREA. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REPLACED RT OUTBOARD AILERON IAW MM 27-10-31.Mar 12, 1999 · N940UP · Boeing 727185CSDR UPS99228917Fitting · corrodedINSPECTION TYPE-C, CORROSION RT WING O/B AILERON CENTER O/B HINGE FITTING. REMOVED AND REPLACED PER SRM 51-30-2.Mar 8, 1999 · N938UP · Boeing 727173CSDR AU990501Bracket · cracked(AUS) AILERON MASS BALANCE ATTACHMENT BRACKET CRACKED.Mar 7, 1999 · Amtr MUSTANG2SDR 20000714SH016Bracket · crackedTHIS AIRCRAFT IS EQUIPPED WITH A ROBERTSON STOL KIT. BOTH OUTBOARD AILERON ATTACH BRACKETS WERE FOUND CRACKED AND BROKEN. THE ADDITIONAL STRESSES RELATED TO THE ROBERTSON CAUSED THIS CONDITON. ALL ROBERTSON STOL EQUIPPED AIRCRAFT SHOULD HAVE THIS BRACKET INMar 5, 1999 · N682RC · Cessna TU206GSDR 20000714SH015Bracket · crackedTHIS AIRCRAFT IS EQUIPPED WITH A ROBERTSON STOL KIT. BOTH OUTBOARD AILERON ATTACH BRACKETS WERE FOUND CRACKED AND BROKEN. THE ADDITIONAL STRESSES RELATED TO THE ROTATION CAUSED THIS CONDITION. THESE PARTS SHOULD BE INSPECTED ON ALL ROBERTSON EQUPPED AIRCRAFMar 5, 1999 · N682RC · Cessna TU206GSDR UPS99828926Skin · crackedINSPECTION TYPE-C3, RT I/B AILERON IS CRACKED, TOP O/B END UNDER THE WEIGHT COVER. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 57-2-0 FIG 2A.Feb 25, 1999 · N808UP · Doug DC873FSDR P2EA99111Skin · delaminatedSJO - DURIGN Q-CHECK RIGHT AILERON WAS FOUND WITH DELAMINATION. AILERON WAS REPAIRED AS PER COOPESA NR COO-CMP-3-57-151-99. (M)Feb 24, 1999 · N208AU · Boeing 737222SDR P2EA99106Skin · delaminatedSJO - DURING Q-CHECK, DELAMINATION WAS FOUND ON THE LEFT AILERON. THE AILERON WAS REPAIRED PER COOPESA EO COO-CMP-3-57-127-99. (M)Feb 23, 1999 · N208AU · Boeing 737222SDR F3LA99022Fitting · brokenPHX - DURING C-CHECK INSPECTION, REPORTED LEFT WING CENTER AILERON HINGE FITTING AFT END BROKEN. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED ATTACH ANGLE AND REPAIRED PER SRM 51-30-2, 51-20-3, AND 51-20-1 AND 51-40-4. (M)Feb 21, 1999 · N214AU · Boeing 737201SDR UPS99829087Skin · dentedINSPECTION TYPE-C, RT WING AILERON DENTED IN UPPER SKIN. CUT OUT DAMAGE, FABBED REPAIR DOUBLER IAW DC8 SRM 57-2-1- FIG 2, INSTALLED DOUBLER IAW DC8 SRM 51-1-21A (W & B DONE ON UPS NR 876762).Feb 20, 1999 · N810UP · Doug DC873FSDR UPS99228967Casting · corrodedINSPECTION TYPE-D, LT I/B AILERON I/B HINGE CASTING CORRODED. CASTING REPLACED IAW DWG 65-21765 AND SRM 51-30-02.Feb 18, 1999 · N923UP · Boeing 72731CSDR UPS99228966Support · corrodedINSPECTION TYPE-D, LT I/B AILERON CENTRE HINGE SUPPORT CORRODED. CENTER HINGE SUPPORT REPLACED IAW MM 27-10-01.Feb 18, 1999 · N923UP · Boeing 72731CSDR UPS99228965Casting · corrodedINSPECTION TYPE-D, RT I/B AILERON ACTUATING ROD ATTACH CASTING HAS SEVERAL AREAS OF PITTING CORROSION. CASTING REPLACED IAW DRAWING 65-21765 AND SRM 51-30-02.Feb 18, 1999 · N923UP · Boeing 72731CSDR UPS99228754Hinge · corrodedINSPECTION TYPE-C, WHILE WORKING CUSTOMER CARD 866785 FOUND LT WING O/B AILERON CENTER O/B FWD HINGE HALF CORRODED. REMOVED CORRODED HINGE AND INSTALLED NEW HINGE IAW SRM 51-30-2.Feb 15, 1999 · N948UP · Boeing 72725CSDR UPS99228751Fitting · corrodedINSPECTION TYPE-C, RT WING O/B AILERON ACTUATOR ROD END FITTING IS CORRODED. REMOVED CORROSION FITTING AND INSTALLED NEW FITTING IAW SRM 51-30-2.Feb 15, 1999 · N948UP · Boeing 72725CSDR UPS99228750Hinge · corrodedINSPECTION TYPE-C, WHILE WORKING CUSTOMER CARD 866785 FOUND LT WING O/B AILERON CENTER I/B FWD HINGE HALF CORRODED. REMOVED CORRODED HINGE AND INSTALLED NEW HINGE IAW SRM 51-30-2.Feb 15, 1999 · N948UP · Boeing 72725CSDR UPS99228749Hinge · corrodedINSPECTION TYPE-C, WHILE WORKING CUSTOMER CARD 866785 FOUND O/B FWD HINGE HALF CORRODED, LT WING O/B AILERON. REMOVED CORRODED HINGE AND INSTALLED NEW HINGE IAW SRM 51-30-2.Feb 15, 1999 · N948UP · Boeing 72725CSDR DHL9974007CSkin · delaminatedAT C CHECK, L/W OUTBD AILERON UPPER SURFACE AT OUTSIDE UPPER SURFACE TRAILING EDGE DELAMINATED. INSTALLED BONDED REPAIR PER SRM 51-40-6, NO BALANCE REQUIRED PER SRM 51-80-4, 7 BY 2 N/R 1108.Feb 3, 1999 · N740DH · Boeing 7272Q9SDR UPS99228629Fitting · corrodedINSPECTION TYPE:SI R/W O/B AILERON, UPPER QUADRANT HINGE HAS PITTING AROUND HINGE BOLT. REMOVED PITTED FITTING, INSTALLED NEW FITTING IAW SRM 51-30-2 PG 14 PARA 7 AND PG 8 PARA A5.Feb 2, 1999 · N949UP · Boeing 72725CSDR 99ZZZX1030Skin · delaminatedAIRCRAFT WAS BEING ANNUALED AND AD 79-22-04 PARA (A)(2) WAS BEING PERFORMED. FOUND THE UPPER SKIN DELAMINATED FROM THE LEADING EDGE AFT FROM 1 INCH TO 4 INCHES AT THE BONDED RIBS.Jan 29, 1999 · N74304 · Gulstm AA5BSDR RRXA991047Skin · damagedDURING A MAINTENANCE VISIT, FOUND DAMAGE, UPPER SKIN, RT O/B AILERON AT STA XW 698. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLERS IAW FAA APPROVED TIMCO DER ENGINEERING SKETCJan 20, 1999 · N105WP · Doug DC873SDR RRXA991045Skin · damagedDURING A MAINTENANCE VISIT, FOUND DAMAGE, SKIN, RT O/B UPPER SKIN RT O/B AILERON AT FWD AREA BETWEEN STA XA 630.250 AND 608.634. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER Jan 20, 1999 · N105WP · Doug DC873SDR P5CA9900035Panel · corrodedLEFT WING UPPER SURFACE OF OUTBOARD AILERON FIX PANEL SMALL AREA OF CORROSION. REPAIRED PER SRM 51-10-01 AND 51-10-02.Jan 20, 1999 · N854FT · Boeing 747122SDR P5CA9900060Link · wornRIGHT INBOARD AILERON/REACTION LINK FOUND WORN. REPAIRED AND REPLACED BEARINGS PER OHM 20-50-03.Jan 18, 1999 · N854FT · Boeing 747122SDR AU990033Balance Weight · corroded(AUS) RIGHT AILERON MASS BALANCE ARM SNAPPED OFF ADJACENT TO ITS CLAMP DURING MEDIUM WIND BUFFETING. INSPECTION OF THE ARM REVEALED CORROSION AROUND 70 PERCENT OF THE CIRCUMFERENCE. THE LEFT ARM ASSEMBLY WAS THEN INSPECTED AND FOUND TO BE CORRODED ON THE REAJan 18, 1999 · Bnorm BN2B26
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