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 DHL2007751503Skin · dentedA/C IN "C" CHECK, NR 7 SLAT UPPER SKIN IS DENTED AT RIVET WS 601. REMOVED FASTENERS IN AFFECTED AREA IAW B727 SRM 51-30-2. CUTOUT DAMAGED AREA (DIM.1" BY 1") IAW B727 SRM 57-50-3 FIG 1. FAB REPAIR DOUBLER FROM 2024T3 0.080 PO NR 9004617 (DIM.5 1/4" BY 4 1/4SDR AWXA200700385Skin · wornSAL - WORN AREA ON RIGHT WING NR 2 SLAT, LOWER SURFACE TRAILING EDGE, WS 4862. REPAIRED RIGHT WING NR 2 SLAT, LOWER SURFACE TRAILING EDGE, WS 4862 IAW AWA ER 26-5743-07072-SS1.SDR ABXA070066Panel · missingRIGHT WING SLAT ANTI-ICE DUCT PANEL MISSING. REPLACED RIGHT WING ANTI-ICE DUCT SEAL DOOR IAW BOEING S/B 767-57-0045 AND AMM 57-41-58.SDR 2007FA0000192Skin · corrodedRT WING LEADING EDGE(S) HAD SEVERE CORROSION WHERE THE TKS PANELS ATTACH. AFTER COMPLETE DISASSEMBLY, IT WAS DETERMNED TO BE BEYOND ECONOMICAL REPAIR. RT WING LEADING EDGE HAD BEEN INSPECTED AT MFG 2.5 YEARS PRIOR TO THIS DISCOVERY. (K)SDR SWAA071146Skin · crackedDURING SCHEDULED 18Y CHECK, FOUND RT WING NR 5 L/E SLAT SKIN CRACKED INBOARD OF ACTUATOR. REPAIRED SLAT SKIN PER SRM.SDR ASAA0741500Skin · chafedNR 4 SLAT CHAFED AT O/B TRAILING EDGE BOTTOM SURFACE. PREPPED CHAFED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 51-70-10 REPAIR 4.SDR 07FDEA00595Rib · damagedRT WING L/E TRACK SUPPORT RIB AT STA XOS 1005 EXISTING REPAIR ANGLE. REMOVED SLAT TRACK DOOR FOR ACCESS IAW MM 57-21-01-2. REPLACED DAMAGED RIB IAW DWG ARB1096. REINSTALLED SLAT TRACK DOOR IAW MM 57-21-01-2.SDR USAA070128Skin · delaminatedNR 9 SLAT, WEDGE UPPER SURFACE OSS 643.74-648.74 DELAMINATED. CUT OUT DELAMINATED SKIN, BONDED REPAIR DOUBLER PER SRM 51-70-10, PAR 20, DEFECT SIZE: 2.5L X 1.5W INCHES.SDR USAA070127Skin · delaminatedNR 8 SLAT, WEDGE UPPER SURFACE OSS 319.71-324.71 DELAMINATED. CUT OUT DELAMINATED SKIN, BONDED REPAIR DOUBLER PER SRM 51-70-10, PARA 20, DEFECT SIZE: 1 INCH DIA.SDR 07FDEA00576Angle · crackedLT WING L/E DURING INSPECTION FOUND 1 CRACK 2" LONG ON ANGLE OF SLAT NR 2 AT STA XORS 264. REPAIRED ANGLE IAW SRM 57-00-01 FIG 3 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER I035530-3/N00530-3 AND IAW SRM 57-00-01 FIG 3 VOL 1.SDR ASAA0741485Wedge · dentedNR 3 SLAT DENTED ON T/E WEDGE ASSY LOCATED 28 INCHES I/B OF O B E.D. NR 3 SLAT REPAIRED IAW SRM 51-70-10.SDR EIA2007038Seal · unknownREQUIRE ADDITION OF ADDITIONAL FLAP SEAL MATERIAL FOR LT WING LEADING EDGE KRUEGER FLAP SEALS (RAIN EROSION SHIELDS) REPAIR. REPAIRED NR 11-13 KRUEGER FLAPS MOLDING SEALS PER BOEING DOC D6-13625.SDR SWAA071075Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND RIGHT WING NR 4 L/E SLAT T/E WEDGE UPPER SURFACE DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED SLAT PER MM.SDR SWAA071076Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND RT WING NR 5 L/E SLAT T/E WEDGE UPPER SURFACE DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED SLAT PER MM.SDR USAA070118Wedge · debondedNR 5 SLAT ON O/B END OF WEDGE DISBONDED. REPAIRED DISBOND AREA & INSTALLED EXTERNAL DOUBLER PER SRM 51-70-10, DEFECT SIZE: .5 X .75 INCH.SDR NWAA071069941Skin · crackedDURING "H" CHECK, FOUND CRACKS IN LT FLAP NOSE SKIN AT XFS 235 AND 252. REPAIRED PER EA 99-208467.SDR SWAA071017Skin · crackedDURING SCHEDULED BRDG CHECK, FOUND RT WING NR 6 L/E SLAT SKIN LOWER SURFACE CRACKED. REPAIRED SLAT PER SRM.SDR ASAA0741470Skin · delaminatedNR 4 SLAT I/B TRAILING EDGE DELAMINATED. PREPPED DAMAGED AREA FABRICATED AND BONDED REPAIR CORE AND DOUBLER IAW SRM 51-70-10 REPAIR 4.SDR AWXA200700332Wedge · debondedMCN - FOUND LEFT WING NR 1 SLAT WEDGE DEBONDED, SS 269. REPAIRED LEFT WING NR 1 SLAT WEDGE, SS 254.53 - SS 272.78 IAW B737-300 SRM 51-70-10-2R4.SDR AWXA200700331Wedge · delaminatedMCN - FOUND LEFT WING NR 2 SLAT TRAILING EDGE WEDGE DELAMINATED, SS 139.65. REPAIRED LEFT WING NR 2 SLAT TRAILING EDGE WEDGE, SS 139.65 IAW B737-300 SRM 51-70-10-2R4.SDR USAA070107Skin · delaminatedTHREE AREAS, 7 INCHES DIA DELAMINATED, NR 10 SLAT, UPPER SURFACE, 0SS 798.74-815.74. CUT OUT DELAMINATION, BONDED REPAIR DOUBLER PER SRM 51-20-10, 57-43-02, DEFECT SIZE: 7 INCHES DIA.SDR 07FDEA00486Skin · corrodedOLD REPAIR ON LT SLAT NR 3 LEADING EDGE, BY AN EXTERNAL PATCH, FASTENERS WERE CORRODED AND SOME HOLE DIAMETERS ARE OVERSIZE. REPAIR WAS PERFORMED IAW TD FOK/308/2006 ISSUE A BY EA 6-5744-106357.SDR QXEA200700226Skin · chafedC2 OKC - FOUND PANEL 522CB LEADING EDGE IS CHAFED. REPAIRED IAW SRM 57-00-01, 51-12-00.SDR QXEA200700217Skin · chafedC2 OKC - FLAP LEADING EDGE PANEL 684LB IS CHAFED ON LEADING EDGE. REPAIRED IAW SRM 57-52-01, 51-21-11.SDR QXEA200700228Skin · chafedC2 OKC - FOUND PANEL 584GB LEADING EDGE IS CHAFED. REPAIRED IAW SRM 51-12-00, 57-52-01.SDR QXEA200700224Skin · chafedC2 OKC - FOUND LEFT WING MID SLAT OUTBOARD HAS CHAFING. REPAIRED IAW SRM 51-12-00, 57-42-01.SDR QXEA200700227Skin · chafedC2 OKC - FOUND PANEL 584AB LEADING EDGE IS CHAFED. REPAIRED IAW SRM 51-12-00, 57-52-01.SDR IXXA07SMN105SVane · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING CENTER LEADING EDGE SLOT VANE HAS A NON STANDARD REPAIR, BETWEEN STATION XS 515.720 AND XS 520.168. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK OR CORROSSDR IXXA07SMN097SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING CENTER LEADING EDGE SLOT VANE UPPER SKIN HAD NON STANDARD REPAIR AT STATION XOLDI 6.225. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION NO CRACKS OR CORROSION FOUND. SDR QXEA200700229Skin · chafedC2 OKC - FOUND PANEL 584EB LEADING EDGE IS CHAFED. REPAIRED IAW SRM 51-12-00, 57-61-01.SDR I5HA0758004Slat · bird strikeON APPROACH, THE CREW FELT A VIBRATION AND A SEVERE PULL TO THE LEFT. THEY DECLARED AN EMERGENCY. AFTER LANDING AND GOING TO THE PARKING SPOT, THE CREW DETERMINED THAT THEY HAD BEEN STRUCK BY A BIRD ON THE LT IB WING (LEADING EDGE). MAINTENANCE WAS CALLED ASDR I5HA0658016Skin · damagedON APPROACH, THE CREW FELT A VIBRATION AND A SEVERE PULL TO THE LT. THEY DECLARED AND EMERGENCY. AFTER LANDING AND GOING TO THE PARKING SPOT, THE CREW DETERMINED THAT THEY HAD A BIRD STRIKE ON THE LT IB WING (LEADING EDGE). MAINTENANCE WAS CALLED AND THEY MASDR 07FDEA00346Stiffener · crackedLEFT WING LEADING EDGE STIFFENER AROUND XORS 690 FOUND CRACKED. LEFT HAND WING LEADING EDGE CRACKED STIFFENER AROUND XORS 690 REPAIRED AS PER FEDEX E.A. 1-5710-107779, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR SWAA070585Skin · delaminatedDURING SCHEDULED 20Y CHECK, FOUND RIGHT WING NR 4 L/E SLAT DELAMINATED AT OUTBOARD END. REPAIRED L/E SLAT PER SRM.SDR 07FDEA00299Skin · misrepairedLT WING NR 4 SLAT REPAIR AT O/B TRACK SKIN DOES NOT CONFORM TO FEDX DWG SR 27-57-034 REMOVED AND REPLACED LT NR 4 SLAT REF MM 27-81-011.SDR 07FDEA00278Beam · corrodedDURING KRUEGER FLAP INSTALLATION, RT WING, FOUND BEAM A535-10218-201 CORRODED REPLACEMENT OF CORRODED BEAM IAW SRM 57-45-11.SDR SWAA070520Skin · delaminatedDURING SCHEDULED 10Y CHECK, FOUND LEFT WING NR 2 L/E SLAT OUTBOARD AFT CORNER DELAMINATED. REPAIRED SLAT PER SRM.SDR SWAA070513Skin · crackedDURING SCHEDULED C1 CHECK, FOUND LEFT WING NR 1 L/E SLAT CRACKED AT LOWER AFT CORNER. REPAIRED SLAT PER SWA EA.SDR 07FDEA00224Skin · damagedLT WING SLAT NR 2 SCRATCH ON L/E SKIN FROM STA XIS 247 TO STA XIS 258. REPAIRED CARRIED OUT IAW SRM 57-10-00 VOL 1 FIG 43 AND SRM 57-10-00 VOL 1 FIG 29. FABRICATED PARTS IAW DETAIL PARTS TRAVELER N00269 AND SRM 57-10-00 VOL1 FIG 29.SDR DHL2007802519Rib · crackedLT INBD FLAP RIB HAS FOUR CRACKS OF 1" AND 1.500" STA XW 125.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG 2 PG 6 (SHEET 4). REMOVED CRACKED RIV IAW SRM 57-1-0 PG.1, SRM 51-1-21, SRM 51-1-20D. FABRICATED RIB (AL2024"0" 0.050") IAW SRM 57-7-1SDR AWXA200700318Skin · crackedMCN - FOUND RIGHT WING NR 5 SLAT TRAILING EDGE SKIN CRACKED, SS 219. RIGHT WING NR 5 SLAT TRAILING EDGE SKIN, SS 219 IAW B737-300 SRM 57-43-01-02R6.SDR AWXA200700265Skin · crackedMCN - FOUND LEFT WING NR 1 SLAT LOWER SURFACE HAS 6 CRACKS, SS 291.75 - SS 300.5. REPAIRED LEFT WING NR 1 SLAT LOWER SURFACE, SS 284.4 - SS 333.4 IAW B737-300 SRM 57-43-01.SDR AWXA200700203Skin · debondedMCN - FOUND LEFT WING NR 2 SLAT UPPER SURFACE, INBOARD END HAS AN AREA DISBONDED, SS 126. REPAIRED LEFT WING NR 2 SLAT UPPER SURFACE, INBOARD END, SS124.40 - SS 127.40 IAW B737-300 SRM 51-70-10-2R4.SDR SWAA070424Slat · crackedDURING SCHEDULED C2 CHECK, FOUND RIGHT WING NR 6 L/E SLAT CRACKED AT LOWER INBOARD T/E END. REPAIRED SLAT PER SRM.SDR SWAA070373Slat · crackedDURING SCHEDULED C1 CHECK, FOUND RT WING NR 6 L/E SLAT CRACKED AT OUTBOARD T/E. REPAIRED NR 6 L/E SLAT PER SWA EA.SDR USAA070068Skin · wornLOWER I/B CORNER T/E WEDGE NR 4 SLAT, WORN AREA/CHAFED. INSTALLED DOUBLER PER SRM 57-41-01-1A, DEFECT SIZE: .5 INCH.SDR SWAA070330Skin · delaminatedDURING SCHEDULED 18Y CHECK, FOUND LT WING NR 3 L/E SLAT UPPER SURFACE DELAMINATED. REPAIRED SLAT PER SRM.SDR QXEA200700146Structure · corrodedC3 OKC - FOUND RIGHT NR 1 SLAT HAS PITTING ON EXTERIOR SURFACE FROM SS 57.50 TO SS 199.66. REPAIRED IAW SRM 51-14-06, 51-21-11.SDR QXEA200700145Structure · damagedC3 OKC - FOUND RIGHT SLAT PANEL 622CB HAS DAMAGE AT LEADING EDGE. REPAIRED IAW SRM 53-00-00, 51-20-08 AND 51-21-11.SDR ASAA0741408Wedge · delaminatedNR 2 SLAT INBOARD END TRAILING EDGE WEDGE IS DELAMINATED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 51-70-10.
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