JASC 5754
Service difficulty reports · 17,348
Reports filed under 5754 · Leading Edge Devices, 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 = '5754' 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.
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 = '5754' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR MWEA97493Fitting · corrodedDURING D-CK, NR 4 SLAT LT WING INBD/CNTR ATTACH FITTING HOLES CORRODED. MAINT REPAIRED IAW DAC TELEX MISC 3906/PDG.SDR MWEA97492Fittings · corrodedDURING D-CK, NR 1 SLAT INBD/CNTR/OTBD ATTACK FITTING RT WING HOLES CORRODED. MAINT REPAIRED IAW DAC TELEX MISC3906/PDG.SDR MWEA97491Fitting · corrodedDURING D-CK, NR 4 SLAT RT WING INBD/CNTR ATTACH FITTINGS CORRODED HOLES. MAINT REPAIRED IAW DAC TELEX 3906/PDG.SDR MWEA97490Fitting · corrodedDURING D-CK, NR 3 SLAT INBD ATTACH FITTING RT WING 2 HOLES CORRODED. MAINT REPAIRED IAW DAC TELEX MISC3906/PDG.SDR MWEA97489Fitting · corrodedDURING D-CK, NR 3 SLAT LT WING CORRODED HOLE. MAINT REPAIR IAW DAC TELEX MISC3906/PDG.SDR MWEA97488Fittings · corrodedDURING D-CK, LT WING INBRD/CNTR AND OTBD FIT HOLES CORRODED TO EXCESS. MAINT REPAIRED IAW DAC TELEX MISC3906/PDG.SDR CKSA97275Hinge · crackedDURING B-CHECK INSPECTION, FOUND STA 246 LEFT WING LEADING EDGE FLAP HINGE ASSEMBLY CRACKED. REMOVED AND REPLACED FLAP HINGE ASSEMBLY IAW B727 SRM 51-30-2. B-CHECK WORK CARD NUMBER 0115. NON-ROUTINE TASK CARD NUMBER 106257.SDR AU970715Arm · cracked(AUS) LH FOREFLAP SUPPORT ARM CRACKED THROUGH BOLT HOLESDR DL757971180Wedge · dentedA DENT WAS FOUND ON THE NR 9 SLAT TRAILING EDGE WEDGE. THE DENT WAS APPROXIMATELY 3 DIAMETER AND 0.150 DEEP. IT WAS LOCATED 5 FWD FROM THE TRAILING EDGE AND 6 INBOARD FROM THE OUTBOARD END. BECAUSE THE LEADING EDGE SLATS ARE THE SUBJECT OF AD 90-23-06 AND TSDR P5CA9700920Bracket · crackedNR 4 LEFT LEADING EDGE DRIVE UNIT SUPPORT BRACKET CRACKED BY NUT PLATE HOLES, FWD L/R SIDES. STOP DRILL CRACK AND INSTALLED FABRICATED DOUBLER AS PER BOEING SRM 51-40-03.SDR DL767971117Te Wedge · delaminationTHE NR 8 SLAT WAS FOUND TO HAVE THE TRAILING EDGE WEDGE UPPER SKIN DELAMINATED. THE DELAMINATION IS A 1 DIA CIRCLE, APPROX. 4 FROM THE AFT EDGE OF THE TRAILING EDGE WEDGE AND 3 O/B OF THE I/B END. THE TRAILING EDGE WEDGE IS MANUFACTURED WITH 0.016 5052-H38 FSDR DL757971093Wedge · delaminationDELAMINATION WAS FOUND ON THE LEADING EDGE OF THE TRAILING EDGE WEDGE ON THE NR 7 SLAT. THE DAMAGE MEASURED 24 INCHES LONG AND IS LOCATED 6 INCHES FROM THE OUTBOARD EDGE OF THE SLAT AND .75 INCH FROM THE LEADING EDGE. BECAUSE THE LEADING EDGE SLATS ARE THE SSDR W8PA971022Skin · crackedNR 6 SLAT, LOWER SURFACE SKIN (JUST BELOW INBOARD AUX TRACT) 3 FASTENERS EXHIBIT EVIDENCE OF CRACKS EMERGING FROM FASTENER HOLES. REMOVED DAMAGED AREA FROM NR 6 SLAT LOWER SURFACE SKIN AND REPAIRED AND INSTALLED DOUBLER PER EWO-100 97-0533, SB 57-1175, DRAWINSDR CALA9700902Skin · crackedINSPECTION FOUND A .3125 INCH CRACK IN NR 3 SLAT LOWER TRAILING EDGE EXTERIOR SKIN AT RIVET BELOW ACTUATOR PISTON. THE CRACK WAS STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-50-3.SDR SWAA970511Slat · damagedDURING SCHEDULED D-CHECK, FOUND NR 6 SLAT CRACKED IN LOWER T/E SKIN NEAR O/B UPSTOP. REPAIRED PER BOEING SRM AND BOEING DRAWING 65C30133.SDR SWAA970496Skin · crackedDURING SCHEDULED D-CHECK, FOUND NR 2 SLAT T/E SKIN CRACKED BELOW ACTUATOR ATTACH POINT. REPAIRED PER BOEING SRM AND DRAWING 65C30133.SDR P5CA9700897Skin · crackedRHW NR 17 VC FLAP FOLDING NOSE O/B PORTION CRACKED AND DEFORMED. REPAIRED NOSE FAIRING PER BOEING SRM 57-50-03. REMOVAL/INSTALLATION PER MM 27-81-02 DWP C/N 012 RAISED.SDR AU970959Brake · faulty(AUS) SLAT SYSTEM WING TIP BRAKE FAULTYSDR EISA97122Slat · dentedDURING ROUTINE C-CHECK, FOUND NR 8 SLAT DENTED FROM SLAT STATION 391-401. REMOVED SLAT AND INSTALLED SERVICEABLE UNIT PER MM 27-81-11. (M)SDR CALA9700790Fitting · brokenINSPECTION FOUND THE RT WING LEADING EDGE NR 3 SLAT OUTBOARD TRACK ATTACH FITTING BROKEN. A NEW FITTING WAS INSTALLED IAW SRM 51-00.SDR AALA970903Track Door · corrodedTUL - NR 3 L/E SLAT OUTBOARD TRACK DOOR HAS CORROSION. REMOVED CORROSION AND INSTALLED DOUBLER (PER 57-50-1 SRM). TST: 42,252. CYCLES: 22,908. (X)SDR AALA970902Track Door · corrodedTUL - NR 3 LEADING EDGE SLAT INBOARD TRACK DOOR IS CRACKED. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 57-50-1. TST: 42,252. CYCLES: 22,908. (X)SDR CKSA97195Skin · chafedDURING C-CHECK INSPECTION, FOUND NR 5 SLAT CHAFED AND DAMAGED ON AFT FACE MARKED B26. CUT OUT DAMAGED AREA, INSTALLED DOUBLER REPAIR IAW L1011 SRM 57-51-00 PAGE 813. TREATED AS PER 51-21-02, PRIMED IAW MM 20-51-09. C-CHECK WORK CARD NUMBER 06-00-1000. NON-SDR CKSA97194Skin · crackedDURING C-CHECK INSPECTION, FOUND NR 2 RIGHT HAND SLAT CRACKED ON AFT FACE AT PREVIOUS REPAIR (B6). REMOVED PREVIOUS REPAIR, STOP DRILLED CRACK AND INSTALLED NEW REPAIR (2024-T3) IAW L1011 SRM 57-51-00 AND SRM 51-50-1. C-CHECK WORK CARD NUMBER 06-27-1000. NOSDR AALA970880Skin · corrodedTUL - CORROSION ON CENTER TORQUE BOX. REPAIRED DOUBLER. FABRICATED AND INSTALLED PER ESO 11697 DATED 1-18-97. TST: 42,464.54. CYCLES, 23,190. (X)SDR AALA970879Skin · corrodedTUL - CORROSION OF AFT OUTBOARD TORQUE BOX. REPAIRED DOUBLERS. FABRICATED AND INSTALLED PER ESO 11697 DATED 2-18-97. TST: 42,464.54 HRS. CYCLES, 23,290. (X)SDR DL76S970885Wedge · delaminatedTHE NR 9 LEADING EDGE SLAT TRAILING EDGE WEDGE WAS FOUND TO HAVE THE UPPER SKIN DELAMINATED 4 FROM THE T/E AND 34 FROM THE INB'D END. THE DAMAGE AREA MEASURES 6 FWD-AFT AND 5.5 INBD-OUTBD. THE TRAILING EDGE WEDGE IS M/F 0.016 5052-H38 FACE SHEETS WITH A METASDR ABXA9701058Fitting · corrodedDURING D-INSPECTION, FOUND THE RIGHT WING NR 3 SLAT CENTER ATTACH FITTING CORRODED. *S/D* REPAIRED IAW DC-9 SRM 57-55-00.SDR ABXA9701057Slat · corrodedDURING D-INSPECTION, FOUND THE RIGHT WING NR 4 SLAT CORRODED INBOARD OF CENTER ATTACH FITTING. *S/D* REPAIRED UNIT COMPLETE.SDR ABXA9701056Fitting · chafedDURING D-INSPECTION, FOUND THE RIGHT WING NR 5 SLAT OUTBOARD FITTING CHAFED BEYOND LIMITS. *S/D* REPAIRED IAW DC-9 SRM 57-55-00.SDR ABXA9701055Fitting · corrodedDURING D-INSPECTION, FOUND THE RIGHT WING NR 1 SLAT CENTER ATTACH FITTING CORRODED. *S/D* REPAIRED IAW DC-9 SRM 57-55-00.SDR ABXA9701054Fitting · corrodedDURING D-INSPECTION, FOUND THE RIGHT WING NR 2 SLAT CENTER ATTACH FITTING CORRODED. *S/D* REPAIRED IAW DC-9 SRM 57-55-00.SDR SCNA97127Rib · crackedDURING HEAVY MAINTENANCE VISIT, A CRACK WAS FOUND ON THE NUMBER 5 SLAT ACTUATOR INBOARD AND OUTBOARD ATTACH RIBS. FABRICATED AND INSTALLED REPAIRS PER B727 SRM 57-50-03 AND 51-30-02.SDR CALA9700804Slat · crackedINSPECTION FOUND A .25 INCH CRACK IN RT WING SLAT NR 6 OUTBOARD HOOK AREA. REPAIRED IAW SRM 57-30-4.SDR DL72S970771Rib · crackedNR 3 SLAT RIB NR 3 IS CRACKED IN 2 PLACES LWR FLANGE AT NUTPLATE AND UPPER FLANGE IN RADIUS. REPAIRED AND INSTALLED DOUBLER PER M/M 57-54-00, PG 813A AND SRM 57-50-3 PG 26.SDR UPS97222805Lug · corrodedINSPECTION TYPE:C, NR 6 K-FLAP O/B ATTACH LUG IS CORRODED AT MOUNT BOLT HOLES ON O/B SIDE. REMOVED AND REPLACED NR 6 K-FLAP IAW MM 27-80-01.SDR DHL9770160CFitting · corrodedAT C-CHECK, NR 3 SLAT RIB BULGED AT O/B TRACK ATTACH FITTING. CORROSION FOUND ON FITTING. REPLACED FITTING PER SRM 51-10-1.SDR CALA9700800Angle · crackedINSPECTION FOUND TWO 2 CRACKS IN LT WING RIB TO UPPER SKIN ATTACH ANGLE AT SLAT STA 0 INSIDE LEADING EDGE AREA. THE ANGLE WAS REPLACED IAW SRM 51-10-1.SDR DHL9770161CFitting · corrodedAT C-CHECK, NR 3 SLAT RIB BULGED AT I/B TRACK ATTACH FITTING. REPLACED FITTING PER SRM 51-30-2.SDR 97UAL900326Skin · crackedNR 6 LEADING EDGE SLAT (PN 114W4508-29) CRACKED AT INBOARD TRACK CUTOUT. ONE CRACK THREE INCHES LONG AND THE SECOND IS FIVE INCHES LONG. *S/D* INTERIM REPAIR ACCOMPLISHED AND REPETITIVE INSPECTIONS SCHEDULED AT TEN CYCLE INTERVALS. PERMANENT REPAIR ACCOMPLSDR 97FDEA00245Flap · delaminatedNR 0414 003, RT I/B FOREFLAP ON UPPER SURFACE I/B END IS GOUGED AND DELAMINATED. *S/D* REMOVED RT I/B FOREFLAP AND REPAIRED RUBSTRIPS ON UPPER SURFACE I/B END AND REINSTALLED FOREFLAP AND FUNCTIONAL TESTED WORK DONE IAW FED-EX SRM 51-40-6, FED-EX M/M 27-51-1SDR SCNA97160Skin · chafedDURING HEAVY MAINTENANCE VISIT, THE NUMBER 8 SLAT OUTBOARD EDGE WAS FOUND CHAFED ALONG LEADING EDGE OF SKIN. CUT OUT CHAFED AREA, FABRICATED FILLER DOUBLER REPAIR IAW B727 SRM 57-30-4 AND 51-30-2.SDR RAAA97B2027Rib · damagedDURING SCHEDULED C1 CHECK, FOUND NR 7 LE SLAT, OUTBOARD TRACK, OUTBOARD MOUNT RIB DAMAGED FROM TRACK BOLT REMOVAL AT SLAT STA 330. REPAIRED PER SRM 57-50-2.SDR RAAA97B2023Rib · crackedDURING SCHEDULED C1 CHECK, FOUND NR 2 LE SLAT RIB CRACKED AT SLAT STA 262. REPAIRED PER SRM 57-50-2.SDR DHL9770503CRib · crackedDURING C CHECK, THE NR 1 SLAT ON THE LEFT WING AT THE INBOARD TRACK HAS A CRACK IN RIB SECTION, AT THAT TRACK. STOP DRILLED CRACKS, ACCOMPLISHED HIGH FREQUENCY EDDY CURRENT INSP AND INSTALLED RIB REPAIRS INBOARD AND OUTBOARD PER SRM 57-50-3 FIG 9. SIZE OF RESDR DL757970707Skin · crackedTHE TRAILING EDGE WEDGE ON THE NR 9 SLAT WAS FOUND WITH A .5 INCH CRACK ON THE UPPER SKIN APPROX 3 FROM THE TRAILING EDGE AND 46 FROM THE OUTBOARD EDGE. AS THE LEADING EDGE SLAT TRAILING EDGE WEDGES ARE THE SUBJECT OF AIRWORTHINESS DIRECTIVES, THIS ER/A WILSDR UPS97222584Ribs · crackedINSPECTION TYPE-SI, NR 8 SLAT HAS 2 CRACKS ON RIB AT SLAT STA 365.5. REMOVED AND REPLACED SLAT ASSY IAW MM 27-81-11.SDR UPS97222571Flap · corrodedINSPECTION TYPE-SI, NR 1 K-FLAP LOWER O/B BULLNOSE CONTROL ROD CORRODED AROUND THE LOWER BEARING ATTACH POINT. FOUND OUT OF LIMITS AND REPLACED BULLNOSE WITH NEW ASSEMBLY (P/N 65-21749-5A), (S/N 698551A) IAW MM 27-81-01.SDR UPS97222570Flap · corrodedINSPECTION TYPE-SI, NR 2 K-FLAP BULLNOSE IS CORRODED ON THE UNDERSIDE OF THE FLANGE AT ALL THE LOWER HINGE POINTS. FOUND CORROSION OUT OF LIMITS. REPLACED BULLNOSE WITH NEW ASSEMBLY, (P/N 65-21750-5A), (S/N TAG 00225932) IAW SRM 51-30-5, 51-30-2.SDR 97UAL900296Slat · crackedLEADING EDGE SLAT NR 9 (114W4160-8) CENTER COVER PANEL HAS TWO CRACKS, 2 INCH AND 8 INCH. INTERNALLY FOUND THREE ADDITIONAL CRACKS ON NOSE BEAM WEB 1 INCH TO 3 INCH IN LENGTH UNDER STIFFENERS BETWEEN OUTBOARD MAIN TRACK RIB ASSY AND O/B DEFLECTION CONTROL RIB
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