JASC 5754
Service difficulty reports · 17,344
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 AWXA200501429Skin · debondedMCN - DURING C13 CHECK DISCOVERED DISBOND AREA ON THE LOWER SURFACE OF THE LEFT WING, NR 2 SLAT, OUTBOARD END OF SLAT. MAINTENANCE REMOVED DISBOND SKIN AND CORE ON THE NR 2 SLAT IAW BOEING 737-300 SRM 51-70-10-2R4. FABRICATED REPLACEMENT CORE AND DOUBLER IAWSDR AWXA200501428Wedge · debondedMCN - DURING C13 CHECK DISCOVERED DISBOND AREA ON THE UPPER AND LOWER SURFACE OF THE NR 1 SLAT WEDGE, INBOARD END. MAINTENANCE REMOVED THE DISBOND SKIN AND CORE ON THE NR 1 SLATE WEDGE IAW BOEING 737-300 SRM 51-70-10-2R4 REPAIR 4. FABRICATED DOUBLER AND CORESDR EIA2005241Skin · repairedPER CUSTOMER REQUEST CHECK, NR 3 L/E FLAP BULLNOSE FAIRING FOUND PREVIOUSLY REPAIRED. DEFECTIVE BULLNOSE FAIRING SKIN REPAIRED PER SRM 57-50-03, FIG 3.SDR AWXA200501413Skin · crackedMCN - DURING C13 CHECK DISCOVERED 7 CRACKS, 1.0 INCHES IN LENGTH, ON THE BOTTOM OF THE NR 1 SLAT FROM SS 247L TO SS 263.5L. MAINTENANCE CUT OUT DAMAGED SKIN ON NR 1 SLAT IAW BOEING 737-300 SRM 57-43-01-2R6. FABRICATED FILLER AND SPLICE PLATE IAW BOEING 737-3SDR AWXA200501412Skin · crackedMCN - DURING C13 CHECK DISCOVERED 5 CRACKS, 1.0 INCHES IN LENGTH, AROUND RIVETS ON THE RT WING, NR 6 SLAT FROM SS 330R TO SS 341R. MAINTENANCE CUT OUT DAMAGED SKIN ON THE RT WING, NR 6 SLAT IAW BOEING 737-300 SRM 57-43-01-2R6. FABRICATED FILLER AND SPLICE PLSDR SWAA053337Skin · crackedDURING SCHEDULED C2 CHECK, FOUND NR 1 L/E SLAT SKIN CRACKED NEAR INBOARD END. REPAIRED SLAT PER SRM.SDR SWAA053318Skin · crackedDURING SCHEDULED SPECIAL VISIT, FOUND NR 2 L/E SLAT LOWER SKIN CRACKED AT OUTBD END. REPAIRED SKIN PER SRM.SDR 2005UALA01214Wedge · delaminatedT/E WEDGE DELAMINATED. WEDGE REPLACED.SDR USAA051212Skin · crackedIN LOWER SKIN OF NR 5 SLAT AT RIVET, ADJACENT TO SLAT ACTUATOR CRACKED. INSTALLED A 30.25 X 3.75 INCH REPAIR DOUBLER ON LOWER SKIN AT CENTER OF SLAT, IAW 57-43-01, DEFECT SIZE: .250 INCH.SDR MWEA050118Doubler · crackedRIB CRACKED BY LEADING EDGE SLATE CABLE PULLEY BRACKET, DO TO SLAT MAKING CONTACT WITH WORK STAND. FABRICATED AND INSTALLED DOUBLER.SDR 2005UALA01160Wedge · damagedNR 9 LEADING EDGE SLAT HAS INTERIM REPAIR INSTALLED INBOARD T/E WEDGE ON LWR SKIN. LOCALIZED DELAMINATION ON THE LOWER SKIN AT THE ENDS OF THE TRAILING EDGE WEDGE OR JUCT AFT OF THE ACTUATOR ATTACH POINTS IS COMMONPLACE FOR THE 777 SLATS. THE 777 AMM 57-43-99SDR 2005UALA01159Skin · delaminatedNR 6 SLAT LEADING EDGE HAS DELAMINATION ON UPPER SURFACE. HONEYCOMB EXPOSED. REINSTALLED NEW SLAT.SDR SWAA053202Skin · delaminatedDURING SCHEDULED 1/2D CHECK, FOUND RT WING NR 5 L/E SLAT DELAMINATED & DISBONDED. REPAIRED SLAT PER SRM.SDR SWAA053200Skin · delaminatedDURING SCHEDULED 1/2D CHECK, FOUND LT WING NR 2 L/E SLAT OUTBOARD UPPER CORNER DELAMINATED. REPAIRED SLAT PER SRM.SDR ASAA0540549Skin · delaminatedOKC - NR 5 SLAT INBOARD TRAILING EDGE IS DELAMINATED. REMOVED DAMAGE, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW 737-400 SRM 51-70-10. (M)SDR ASAA0540548Skin · chafedOKC - FOUND NR 1 SLAT LOWER T/E IS CHAFED. REMOVED DAMAGE, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW 737-400 SRM 51-70-10. (M)SDR IXXA05SMN235SSkin · improperDURING C CHECK INSPECTION, RT OTBD FLAP UPPER SKIN HAS NON STANDARD REPAIR, STA XF 230.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 # 05447 DATED 10-05-05, SEMAN DWG # ED 4072 DATED 10-01-05, EO SEMAN # 20051298 DATED 10-05-05. REMOVED EXISTING NON STANDARSDR IXXA05SMN234SSkin · improperDURING C CHECK INSPECTION, RT WING INBD FLAP UPPER SKIN HAS NON STANDARD REPAIR. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-7-1 FIG 1, EO SEMAN NR 20051279 DATED 09-26-05. REMOVED DAMAGED PLATING IAW DC8 SRM 57-1-0 PG 1, DC8 SRM 51-1-21. FABRICATED NEW PLATING (SDR IXXA05SMN233SSkin · improperDURING C CHECK INSPECTION, LT OTBD FLAP UPPER SKIN HAS NON STANDARD REPAIR, XW 435.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-5 FIG 1, EO SEMAN # 20051210 DATED 09-21-05. REMOVED FASTENERS IAW DC8 SRM 51-1-21, DC8 SRM 51-3-0. REMOVED DAMAGED SECTION IAW DSDR AWXA200501298Skin · crackedMCN - DURING C16 CHECK DISCOVERED 4 CRACKS ON THE BOTTOM OF THE NR 2 SLAT SKIN, OUTBOARD OF ACTUATOR FROM SS221 TO SS225. MAINTENANCE CUT OUT DAMAGED SKIN IAW BOEING 737-300 SRM 57-43-01-2R6 FIG 201. FABRICATED FILLER AND SPLICE PLATE IAW BOEING 737-300 SRM SDR AWXA200501297Skin · crackedMCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED 4 CRACKS ON THE BOTTOM OF THE NR 2 SLAT SKIN, INBOARD OF ACTUATOR FROM SS178 TO SS182. MAINTENANCE CUT OUT DAMAGED SKIN IAW BOEING 737-300 SRM 57-43-01-2R6 FIG 201. FABRICATED FILLER AND SPLICE PLATE IAW BOEINSDR AWXA200501283Skin · crackedMCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED 4 CRACKS, 1.0 INCHES IN LENGTH, ON THE NR 1 LOWER SLAT SKIN BELOW THE CENTER AUXILIARY TRACK FROM SS 298L TO SS 302L. MAINTENANCE CUT OUT DAMAGED AREA ON THE NR 1 LOWER SLAT SKIN IAW BOEING 737-300 SRM 57-43-01SDR AWXA200501282Skin · crackedMCN - MAJOR REPAIR - DURING C16 CHECK,DISCOVERED 4 CRACKS, 1.0 INCHES IN LENGTH, ON THE NO. 1 LOWER SLAT SKIN BELOW THE INBOARD AUXILIARY TRACK FROM SS 274L TO SS 278L. MAINTENANCE CUT OUT DAMAGED AREA ON THE NO. 1 LOWER SLAT SKIN IAW BOEING 737-300 SRM 57-43SDR AWXA200501281Skin · delaminatedMCN - MAJOR REPAIR - DURING C16 CHECK, DISCOVERED THE UPPER AND LOWER SURFACE OF THE NR 3 SLAT DELAMINATED FROM SS 116.27L TO SS 124.27L. MAINTENANCE REMOVED DAMAGED AREA FROM THE UPPER AND LOWER SURFACE OF THE NR 3 SLAT IAW BOEING 737-300 SRM 51-70-10-2R4. SDR AWXA200501274Skin · debondedMCN - MAJOR REPAIR - DURING C16 CHECK, DISCOVERED THE UPPER AND LOWER SURFACE OF THE NR 3 SLAT WEDGE DISBONDED FROM SS 12.25L TO SS 18.25L. MAINTENANCE REMOVED DAMAGED AREA FROM THE NR 3 SLAT WEDGE IAW BOEING 737-300 SRM 51-70-10-2R4. FABRICATED REPAIR CORE SDR SWAA053147Structure · crackedDURING SCHEDULED C3 CHECK, FOUND LT WING NR1 L/E SLAT CRACKED. REPAIRED SLAT PER SWA EA.SDR 05FDEA03362Skin · crackedLT WING NR 8 SLAT INNER SURFACE FOUND CRACKED AT SLAT TRACK NR 18 AREA. CARRIED OUT REPAIRED AS PER SRM 57-10-00 FIG 10, VOL I. REPAIR CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.SDR 05FDEA03358Skin · crackedRIGHT WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACKED AT XORS 536. FASTENERS AT CRACKED INTERNAL BEADED DOUBLER AT RIGHT HAND WING FIXED LEADING EDGE XORS 536 REMOVED AS PER SRM 51-31-01 VOLUME II. REPAIR DOUBLER FABRICATED AS PER SRM 57-SDR 05FDEA03356Skin · crackedRIGHT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACKED AT XORS 590. TRIMMED OUT AS PER FEDEX EA 1-5710-89998. REPAIR DOUBLER AND ANGLE FABRICATED AND INSTALLED AS PER FEDEX EA 1-5710-89998. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.SDR 05FDEA03354Skin · crackedRIGHT WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACKED AT XORS 680. TRIMMED OUT AS PER FEDEX EA 1-5710-89997. REPAIR DOUBLER AND ANGLE FABRICATED AND INSTALLED AS PER FEDEX EA 1-5710-89997. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2- 100.SDR 05FDEA03353Skin · crackedLEFT WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACKED AT XORS 635. REPAIR CARRIED OUT AS PER SRM 57-10-00.SDR SWAA053111Skin · crackedRIGHT WING NR 5 L/E SLAT CRACKED. REMOVED AND REPLACED SLAT PER MM.SDR AWXA200501259Wedge · delaminatedMCN - MAJOR REPAIR - DURING C18 CHECK DISCOVERED DISBOND AREA ON OUTBOARD END OF THE RIGHT WING NR 4 SLAT WEDGE. MAINTENANCE REMOVED DISBOND AREA FROM THE NR 4 SLAT WEDGE IAW BOEING 737-300 SRM 51-70-10-2R. FABRICATED AND BONDED REPAIR FILLER AND DOUBLER TO SDR USAA051188Skin · delaminatedFOUND NR 2 SLAT T/E WEDGE O/B END DELAMINATED. REMOVED DAMAGE INSTALLED REPAIR PIECES IAW SRM 51-70-10, DEFECT SIZE: 3" X 6" DELAMINATION.SDR USAA051189Skin · delaminatedNR 2 SLAT T/E WEDGE INBOARD END DELAMINATED. REMOVED DAMAGE, INSTALLED REPAIR PIECES IAW SRM 51-70-10, DEFECT SIZE: 3" BY 5" DELAMINATION.SDR ASMF200510005Structure · damagedCAPTAIN REPORTED THAT DURING SLATS EXTENSION, AIRPLANE TURNED TO LT 5 AND LT WING DOWN CONDITION, IT ENDS ONCE TAKEOFF LIGHT ILLUMINATED, AFTER SLATS EXTENSION PROCESS. AIRPLANE WAS SENT TO HANGAR AND SLATS / FLAPS SEQUENCE MECHANISM AND BUS CABLE CONDITION WESDR MWEA050109Doubler · dentedSLAT HORN ON THE LEFT WING HAS A DENT. FABRICATED AND INSTALLED DOUBLER.SDR AWXA200501384Skin · gougedGYR - DURING C10 CHECK, DISCOVERED GROOVES WORN INTO PREVIOUS REPAIR DOUBLER ON THE LOWER SURFACE OF THE T/E WEDGE SKIN, FOR THE NR 4 LEADING EDGE SLAT. DAMAGE WAS CAUSED BY CONTACT WITH FIXED LEADING EDGE DURING EXTENSION AND RETRACTION. MAINTENANCE REMOVEDSDR AWXA200501373Skin · delaminatedDURING C10 CHECK DISCOVERED SMALL AREA OF DELAMINATION ON THE LOWER SURFACE OF THE NO. 3 SLAT TRAILING EDGE WEDGE AT WS 460L. MAINTENANCE REMOVED DELAMINATION AREA ON THE NR 3 SLAT IAW BOEING 757-200 SRM 51-70-10-2R. FABRICATED DOUBLER AND FILLER IAW BOEING SDR SWAA053070Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND NR 2 L/E SLAT UPPER T/E WEDGE DELAMINATED AT INBD AND OTBD ENDS. REPAIRED SLAT PER SRM.SDR USAA051179Wedge · delaminatedFOUND NR 2 SLAT T/E WEDGE INBD END DELAMINATED. REMOVED DAMAGE, INSTALLED REPAIR PIECES IAW SRM 51-70-10, DEFECT SIZE: 3" BY 5" DELAMINATION.SDR USAA051178Wedge · delaminatedFOUND NR 2 SLAT T/E WEDGE O/B END DELAMINATED. REMOVED DAMAGE, INSTALLED REPAIR PIECES IAW SRM 51-70-10, DEFECT SIZE: 3" X 6" DELAMINATION.SDR USAA051174Wedge · damagedFOUND NUMBER 5 SLAT WEDGE TOP SURFACE 10 INCHES FROM OUTBOARD END DAMAGED. REMOVED DAMAGE, FABRICATED AND INSTALLED CORE, FABRICATED AND INSTALLED DOUBLER IAW 57-42-02, DEFECT SIZE: 6".SDR SWAA053006Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND RT WING NR 5 L/E SLAT DELAMINATED. REMOVED AND REPLACED SLAT PER MM.SDR SWAA052986Skin · crackedDURING SCHEDULED 1/2D CHECK, FOUND RT WING NR 4 L/E SLAT T/E INBD LOWER SKIN CRACKED. REPAIRED SKIN PER SRM.SDR SWAA052989Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND RT WING NR 5 L/E SLAT T/E WEDGE OTBD UPPER CORNER DELAMINATED. REMOVED AND REPLACED SLAT PER MM.SDR SWAA052955Skin · crackedDURING SCHEDULED 1/2D CHECK, FOUND LT WING NR 3 L/E SLAT T/E LOWER SKIN CRACKED. REMOVED AND REPLACED NR 3 SLAT PER MM.SDR AWXA200501197Skin · crackedMCN - MAJOR REPAIR - DURING C18 CHECK DISCOVERED THE NR 5 SLAT LOWER SKIN CRACKED, .750 INCHES IN LENGTH, APPROXIMATELY 39 INCHES FROM INBOARD SIDE, UNDER THE CENTER AUXILIARY TRACK AT SS 163.53. MAINTENANCE REMOVED DAMAGED PART OF SKIN ON THE NR 5 SLAT IAW BSDR 2005UALA01075Wedge · delaminatedSLAT HAS DAMAGED DELAMINATED T/E WEDGE. WEDGE REPLACED.SDR 0509004Rib · crackedRT WING, SLAT NR 4 RIB CRACKED AT SLAT STA 0.28.
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