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 AWXA200501529Skin · crackedMCN - DURING C19 CHECK DISCOVERED 2 CRACKS, .5 AND .75 INCHES IN LENGTH, ON THE BOTTOM OF THE NR 4 SLAT INBOARD OF ACTUATOR FROM SS 50R TO SS 65R. MAINTENANCE TRIMMED OUT DAMAGED AREA ON THE NR 4 SLAT IAW BOEING 737-300 SRM 57-43-01-2R6. FABRICATED FILLER ANSDR AWXA200501527Skin · crackedMCN - DURING C19 CHECK DISCOVERED 6 CRACKS ON THE BOTTOM OF THE NR 6 SLAT BELOW ACTUATOR FROM SS 318R TO SS 324R. MAINTENANCE TRIMMED OUT DAMAGED AREA ON THE NR 6 SLAT IAW BOEING 737-300 SRM 57-43-01-2R6. FABRICATED FILLER AND SPLICE PLATE IAW BOEING 737-300SDR 05FDEA03863Repair · properRT WING, SLAT 1 FOUND FLUSH DOUBLER REPAIR ON LOWER SKIN, DIMENS 11.5 X 8.5 INCHES. PERFORMED A GVI OF REPAIR IAW EA 8.5710-90122 AND FOUND IN COMPLIANCE WITH REQUEST BY EO 83500.7.5001.SDR SWAA053695Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND NR 2 L/E SLAT DELAMINATED. REMOVED AND REPLACED SLAT PER MM.SDR AWXA200501541Wedge · debondedMCN - DURING C19 CHECK DISCOVERED DISBOND AREA ON THE LOWER SURFACE OF THE NR 3 SLAT WEDGE, FROM SS 102L TO SS 111L. MAINTENANCE CUT OUT DISBOND AREA IAW BOEING 737-300 SRM 51-70-10-2R4. FABRICATED DOUBLER AND REPAIR CORE IAW BOEING 737-300 SRM 51-70-10-2R4.SDR AWXA200501540Wedge · debondedMCN - DURING C19 CHECK DISCOVERED DISBOND AREA ON THE UPPER AND LOWER SURFACE OF THE NR 2 SLAT WEDGE, OUTBOARD END FROM SS 250.27L TO SS 254.27L. MAINTENANCE CUT OUT DISBOND AREA IAW BOEING 737-300 SRM 51-70-10-2R4. FABRICATED DOUBLER AND REPAIR CORE FOR UPPSDR AWXA200501531Skin · crackedMCN - DURING C19 CHECK DISCOVERED 2 CRACKS, 1.0 INCH, AT FASTENERS LOCATED ON THE NR 2 SLAT BELOW THE INBOARD AUXILIARY TRACK FROM SS 163L TO SS 165L. MAINTENANCE TRIMMED OUT DAMAGED AREA ON THE NR 2 SLAT IAW BOEING 737-300 SRM 57-43-01-2R6. FABRICATED FILLESDR AWXA200501530Skin · crackedMCN - DURING C19 CHECK DISCOVERED 3 CRACKS AT FASTENERS LOCATED ON THE NR 2 SLAT BELOW OUTBOARD AUXILIARY TRACK FROM SS 211L TO SS 214L. MAINTENANCE TRIMMED OUT DAMAGED AREA ON THE NR 2 SLAT IAW BOEING 737-300 SRM 57-43-01-2R6. FABRICATED FILLER AND SPLICE PLSDR AWXA200501528Skin · crackedMCN - DURING C19 CHECK DISCOVERED 6 CRACKS ON THE BOTTOM OF THE NR 3 SLAT OUTBOARD OF ACTUATOR FROM SS 51L TO SS 76L. MAINTENANCE TRIMMED OUT DAMAGED AREA ON THE NR 3 SLAT IAW BOEING 737-300 SRM 57-43-01-2R6. FABRICATED FILLER AND SPLICE PLATE IAW BOEING 737SDR AWXA200501475Pin · corrodedSAL - DURING BC4 CHECK DISCOVERED CORROSION ON THE HINGE PIN FOR THE OUTBOARD SIDE OF THE NR 4 SPOILER. MAINTENANCE REMOVED AND REPLACED THE HINGE PIN, ON THE NR 4 SPOILER IAW AIRBUS 320 AMM 27-64-44-04.SDR USAA051406Skin · puncturedRIGHT WING LEADING EDGE ABOVE NR 4 LEADING EDGE FLAP, APPROX L/E STA 205 DENTED. REMOVED EXISTING REPAIR, CUT OUT DAMAGE, INSTALLED FILLER & DOUBLER PER EA 96961. DEFECT SIZE: .6"L X .4"W X .080"D, 2.5"L X 1"W X .100"D DENT & PUNCTURE, .75"L X .3"W.SDR ASAA0540653Skin · crackedPAE- NR 3 SLAT LWR T/E SKIN AT OB END CRACKED THROUGH FASTENER HOLE. REPAIRED IAW SRM 57-43-01. (M)SDR 05FDEA03807Repair · properLT WING SLAT NR 1 ON INT SKIN FOUND 1EA FLUSH DOUBLER 22'' BY 22'' AT STA XORS 80. PERFORMED INSPECTION ON SLAT NR 1 REPAIR DOUBLER IAW EA NR 8-5710-90122. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 E3 P2.SDR AWXA200501525Skin · crackedA 5.25 INCH CRACK WAS DISCOVERED ON THE NR 1 SLAT LOWER SKIN FROM SS254.75R TO SS 260R. DAMAGE WAS PLACED ON MONITOR TO BE REPAIRED WITHIN 24 MONTHS. MAINTENANCE TRIMMED OUT DAMAGED AREA ON THE NR 1 SLAT LOWER SKIN IAW BOEING 737-300 SRM 57-43-01-2R6. FABRISDR SWAA053608Skin · crackedDURING SCHEDULED C4 CHECK, FOUND NR 1 L/E SLAT LOWER SKIN CRACKED OTBD OF ACTUATOR. REPAIRED SLAT PER SWA EA.SDR 05FDEA03785Attach Angle · crackedLT WING IB FIXED L/E PNL IB SUPPORT WEB LWR ATTACH ANGLE HAS CRACK AT JUNCTION OF KRUEGER AND NR 1 SLAT.SDR AWXA200501601Skin · delaminatedMCN - DURING C20 CHECK DISCOVERED, THE RT WING, NR 5 SLAT, OUTBOARD TRAILING EDGE LOWER SKIN DELAMINATED. MAINTENANCE REMOVED DISBONDED SKIN IAW BOEING 737-300 SRM 51-70-10-2R4. FABRICATED REPAIR FILLER AND REPAIR DOUBLER IAW BOEING 737-300 SRM 51-70-10-2R4.SDR 05FDEA03776Repair · undamagedFOUND REPAIR ON RT NR 5 SLAT UPPER SURFACE. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT NR 5 RT SLAT WAS DETERMINED TO BE IAW SRM 57-50-3 FIG 1 SHT 6 AND 7, BSDR CALA0500400Skin · crackedINSPECTION FOUND A 1" CRACK AROUND FASTENER HOLE IN RT WING NR 6 SLAT SKIN AT LOWER SURFACE 23 INCHES FROM O/B END. THE SLAT WAS REPAIRED IAW SRM 57-43-01.SDR 05FDEA03758Repair · undamagedFOUND REPAIR TOP SIDE NR 3 L/E KRUGER FLAP LT WING. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT NR 3 L/E KRUGER FLAP, TOP SIDE ON LT WING WAS DETERMINED TSDR SWAA053566Skin · crackedDURING SCHEDULED C2 CHECK, FOUND NR 4 L/E SLAT LOWER T/E SKIN CRACKED. REPAIRED SLAT PER SRM.SDR SWAA053553Skin · crackedDURING SCHEDULED C3 CHECK, FOUND NR 2 L/E SLAT OUTBOARD LOWER SKIN CRACKED. REPAIRED SLAT PER SWA EA.SDR 05FDEA03739Skin · unknownEXISTING EXTERNAL REPAIRS ON NR 5 K-FLAP INNER TAI SKIN, 14 EACH 2" ROUND REPAIRS. REPAIRS REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIRS WERE ACCOMPLISHED USING FAA APPROVED DATA. REMOVED FASTENERS, INSTALLED WASHERS AND INSTALLED FASTENSDR 05FDEA03729Skin · dentedRT WING O/B FLAP LOWER O/B SURFACES HAS DENTS. FOUND DENTS AT X0F 775-781 TO BE WITHIN ALLOWABLE LIMITS IAW DC10 SRM 57-10-00 FIG 48 VOL 1. FOUND DENT AT X0F 783-787 TO BE OUT OF LIMITS IAW DC10 SRM 57-10-00 FIG 48 VOL1. REMOVED DAMAGE AND INSTALLED REPAIR SDR SWAA053544Skin · crackedDURING SCHEDULED C2 CHECK, FOUND NR 6 L/E SLAT LOWER SKIN CRACKED. REPAIRED SLAT PER SRM.SDR 05FDEA03698Doubler · crackedRIGHT FIXED LEADING EDGE INTERIOR BEADED DOUBLER FOUND CRACKED AT XORS663. REPAIRED AS PER FEDEX EA 1-5730-90044SDR UPS05145730Access Panel · crackedACCESS PANEL REMOVED IN RIGHT KRUEGER FLAP BOX AREA. INSTALLED ACCESS PANEL IN RIGHT KRUEGER FLAP BOX AREA PER 57000.SDR 05FDEA03667Skin · damagedFOUND A SPLICE DOUBLER REPAIR AT RIGHT WING NR 1 SLAT LOWER SURFACE ON SLAT SKIN WING STATION XIS247 AT NR 3 SLAT TRACK AREA. PERFORMED A GVI OF EXISTING REPAIR IAW EO8-5100-7-5001 CRITERIA REQUEST AND FOUND IN COMPLIANCE WITH SRM 57-10-00 FIG 29.SDR SWAA053514Skin · crackedDURING SCHEDULED 1/4D CHECK, FOUND NR 4 L/E SLAT SKIN CRACKED AT ACTUATOR OUTBOARD STOP FITTING. REPAIRED SLAT PER SRM.SDR 05FDEA03672Doubler · unknownLT WING FOUND AN EXTERNAL DOUBLER REPAIR AT FIXED L/E LOWER SURFACE AT CUT OUT FOR SLAT TRACK LEFT SIDE STATION XOS 775. PERFORMED A GVI OF EXISTING DOUBLER IAW EO8-5100-7-5001 CRITERIA REQUEST FOUND IN COMPLIANCE WITH SRM 57-10-00 PAGE 215.SDR 05FDEA03669Doubler · unknownFOUND EXTERNAL DOUBLER REPAIR AT LEFT WING NR 1 SLAT UPPER SURFACE L/E AREA BETWEEN WING STATIONS XIS129 TO XIS133. PERFORMED A GVI OF EXISTING REPAIR IAW SRM 57-10-00 FIG 84 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO8-5100-7-5001.SDR 05FDEA03668Doubler · unknownLEFT WING NR 1 SLAT L/E UPPER SURFACE FOUND A FLUSH DOUBLER REPAIR BETWEEN WING STATION XIS152 AND XIS157. PERFORMED A GVI OF EXISTING DOUBLER IAW EO8-5100-7-5001 CRITERIA REQUEST FOUND IN COMPLIANCE WITH SRM 57-10-00 FIG 11.SDR AWXA200501444Skin · delaminatedPHX - DURING A07 CHECK DISCOVERED THE NR 6 SLAT DELAMINATED AT THE INBOARD END AFT WEDGE. MAINTENANCE REMOVED AND REPLACED THE NR 6 SLAT IAW BOEING 757-200 AMM 27-81-01-4. OPERATION AND RIG CHECKS WERE GOOD.SDR SWAA053496Skin · crackedDURING SCHEDULED 1/4D CHECK, FOUND NR 5 L/E SLAT SKIN CRACKED INBOARD OF ACTUATOR. REPAIRED SLAT PER SRM.SDR SWAA053495Skin · crackedDURING SCHEDULED 1/4D CHECK, FOUND NR 6 L/E SLAT SKIN CRACKED AT ACTUATOR INBOARD STOP FITTING. REPAIRED SLAT PER SRM.SDR AWXA200501465Skin · crackedMAJOR REPAIR - DURING C19 CHECK DISCOVERED CRACKS ON THE BOTTOM OF THE NR 1 SLAT SKIN AT 10 FASTENERS BELOW ACTUATOR FROM SLAT STATION (SS) 317L TO SS 327L. MAINTENANCE CUTOUT DAMAGED PART OF SKIN IAW SRM 57-43-01-2R6 FIG 201. FABRICATED FILLER AND SPLICE PLSDR 2005UALA01223Skin · delaminatedNR 2 SLAT LWR SURFACE DELAMINATED AT INBOARD END 3 INCHES FROM THE TRAILING EDGE. INTERIM REPAIR PER 777 AMM 57-43-99. ACP AN INITIAL INSP AT 50 CYCLE AND EVERY 500 FLT CYCLE UNTIL PERMANENT REPAIR ACPL AT NEXT HMV (5JUNE06). OK TO CF PER AMM AND SFOIQ WALSDR 2005UALA01222Skin · delaminatedNR 3 SLAT LWR SURFACE DELAMINATED AT OUTBOARD END 4 INCHES FROM TRAILING EDGE. INTERIM REPAIR PER 777 AMM 57-43-99. ACP AN INITIAL INSP AT 50 CYCLE AND EVERY 500 FLT CYCLE UNTIL PERMANENT REPAIR ACPL AT NEXT HMV (5JUNE06). OK TO CF PER AMM AND SFOIQ WALSH.SDR 2005UALA01221Skin · delaminatedNR 5 SLAT LWR SURFACE DELAMINATED AT INBOARD END NEAR TRAILING EDGE. INTERIM REPAIR PER 777 AMM 57-43-99. ACP AN INITIAL INSP AT 50 CYCLE AND EVERY 500 FLT CYCLE UNTIL PERMANENT REPAIR ACPL AT NEXT HMV (5JUNE06). OK TO CF PER AMM AND SFOIQ WALSH.SDR USAA051326Skin · crackedIN LOWER SKIN OF NR 5 SLAT AT RIVET, ADJACENT TO SLAT ACTUATOR ATTACH. A 30.25 X 3.75 INCH REPAIR DOUBLER ON LOWER SKIN AT CTR OF SLAT ADJ TO ACTUATOR ATTACH IAW SRM 57-43-01. DEFECT SIZE: .250 INCH LONG CRACK AT RIVET.SDR USAA051331Skin · crackedLOWER SKIN T/E CRACKED. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-43-01 FIG 201, DEFECT SIZE: 6 INCH CRACK.SDR DHL2005749016Bracket · crackedLT WING NR 2 SLAT ACT MOUNT BRACKET IB SIDE HAS INSIDE PLATE CRACKED. REMOVED FABBED NEW AND INSTALLED NR 2 SLAT ACT I/B MOUNT BRACKET MAT USED BAC 1503-10045 PO 9001801 DIM 9.15" BY 3.25" BY 1.25" IAW S/B 727-57-0130 REV 3 FIG 1. REMOVED ALUMINUM DOUBLERS FSDR USAA051322Skin · damagedNR 1 SLAT WITH FLUSH PATCH. MAJOR REPAIR IAW SRM 57-43-01, DEFECT SIZE: 5.5" BY 3.5".SDR 05FDEA03596Skin · gougedRT WING NR 2 SLAT IB TE HAS DENT AND GOUGE APPROX 4.7" LONG UPPER END (HURRICANE RITA NR 31) REF N00081. COMPLIED WITH EA 6-5750-93420SDR SWAA053428Skin · crackedDURING SCHEDULED 1/4D CHECK, FOUND NR 1 L/E SLAT LOWER T/E SKIN CRACKED. REPAIRED SLAT PER SRM.SDR USAA051294Skin · debondedFOUND DISBOND O/B END OF T/E WEDGE. REMOVED DAMAGE, FAB AND INSTALLED REPAIR PARTS IAW TR 51-30-03, DEFECT SIZE: 2" BY 5" DISBOND.SDR USAA051295Skin · debondedFOUND SLAT DISBOND, T/E WEDGE O/B END. REMOVED DAMAGE, FAB AND INSTALLED REPAIR PARTS IAW TR 57-42-04, DEFECT SIZE: 3" X 5" DISBOND.SDR QXEA200501644Anchor · brokenYYC - RIGHT WING SLAT NR 1 INBOARD OF SLAT TRACK PANEL 622BZ HAS A BROKEN ANCHOR UNIT. MAINTENANCE REPLACED WITH A NEW NUT ASSEMBLY IAW CRJ-700 SRM 51-42-06-001-001-A01.SDR QXEA200501625Skin · corrodedYYC - DURING C3 CHECK, RIGHT SLAT INTERIOR SKIN HAS FRETTING CORROSION. MAINTENANCE BLENDED OUT CORROSION IAW CRJ-700 SRM 57-42-01-101-D01-A01. TREATED AREA.SDR ASAA0540592Skin · chafedOKC - NR 1 SLAT T/E LOWER SURFACE IS CHAFED AND CRACKED AT O/B CORNER. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW B737-400 SRM 51-70-10. (M)
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