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 SWAA100888Slat · crackedDURING SCHEDULED SPV CHECK, FOUND LT WING NR 3 SLAT CRACKED. REMOVED AND REPLACED NR 3 SLAT PER MM.SDR IPXA10558510Skin · dentedINSPECTION TYPE:C2 NR 8 SLAT UPPER TE SURFACE HAS A CREASED DENT 3 INCH FROM TE AND 29 INCH FROM INBD END NR 8 SLAT UPPER T/E SURFACE OF THE T/E WEDGE WAS REPAIRED IAW BOEING 757-200PF SRM 51-70-10-2R REPAIR 4 AND BOEING 757-200PF SRM 51-70-10-2R-OG REPAIR GENSDR SWAA100821Skin · crackedDURING SCHEDULED 8Y CHECK, FOUND RT WING L/E NR 6 SLAT SKIN I/B LOWER SURFACE CRACKED. REPAIRED SLAT SKIN PER SRM.SDR IPXA10558643Skin · delaminatedINSPECTION TYPE:C3, WHILE PERFORMING THE REPAIR ASSESSMENT FOUND THE NR7 SLAT T/E WEDGE TO HAVE A DELAM AT THE PREVIOUS REPAIR AT OSS 377.45-383.15 AND 4.5" FWD OF THE T/E EDGE (456-W4-03). NR 7 SLAT T/E WEDGE UPPER SURFACE WAS REPAIRED IAW SRM 51-70-10-2R.SDR IPXA10558493Structure · damagedLEFT WING NR 3 SLAT DAMAGED. REPAIRED PER EO B757-5750-35415-B.SDR IPXA10558488Skin · dentedNR 5 LE SLAT UPPER SKIN DENTED 7.75 INCH OTBD OF INNER EDGE. REPAIRED IAW EO B757-5750-36659-A.SDR IPXA10558487Skin · dentedNR 5 L/E SLAT WEDE DENTED 43.25 INCH OTBD OF INNER EDGE. REPAIRED PER EO B757-5750-36660A.SDR USAA20100215EM003Slat · damagedFLIGHT 1161, PHL-CLT - DURING CLIMB FLEW THROUGH A FLOCK OF 12 GEESE AND ONE STRUCK THE WING. THE CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. THE FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE ACCOMPLISHED A BIRD STRIKE INSPECTION AND DAMAGE TO LEFT SDR USAA2010030490496Slat · debondedCLT - C2 - MAJOR REPAIR - NR 6 SLAT HAS DISBOND ON THE OUTBOARD END OF WEDGE. REPLACED NR 6 SLAT IAW JOB CARD 19L51027001.SDR FDEA201002120402Skin · wornLT WING, SLAT NR 2 FOUND DEEP WEAR ON LOWER SKIN. REPAIRED SKIN IAW SRM 57-10-00, FIG 31, VOL I.SDR AALA20100211TUL16Attach Fitting · crackedHIGHT FREQUENCY EDDY CURRENT INDICATES CRACK ON LEFT WING LEADING EDGE NUMBER 5 SLAT AT 2ND FROM OUTBOARD RIB, INBOARD LEG. REMOVED 2ND FROM OUTBOARD ATTACH FITTING; LOCATED, DRILLED, AND INSTALLED NEW ATTACH FITTING PER / ESO 80117. CLEARANCE TO INSTALL LOWESDR AALA20100211TUL03Rib · crackedHIGH FREQUENCY EDDY CURRENT INDICATES CRACK ON RIGHT WING LEADING EDGE NUMBER 5 SLAT AT OUTBOARD RIB INBOARD LEG MARKED. REMOVED AND REPLACED RIB PER SRM 57-50-13.SDR FDEA201002110392Skin · crackedNR 8 SLAT L/E UPPER FACE CTR SECTION HAS CRACK REMOVED CORROSION IAW SRM 51-10-02. BLENDED AREA L=1.5" W=1.2" D=.023 ORIG. MAT .063 OUT OF LIMITS IAW SRM 57-43-01 FIG 101, DET VII. REPAIRED IAW SRM 57-43-01 FIG 201 R NR 1 & EA F-5740-131175. WINGS- L/E DEVICSDR IPXA10658538Skin · crackedINSPECTION TYPE:6C, LT WING - NR 4 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR 4 SLAT INBD NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2, FIG 201, REV 46 JUST AT OSS572.5, ORIGINAL MATERIAL IS 7075T6-0063IN, CRACK LENGTH IS 0.07", DAMAGED CUTOUT SIZE ISDR IPXA10658537Skin · crackedINSP TYPE:6C, LT WING - NR 4 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR4 SLAT OTBD NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2 FIG 201 REV 46, JUST AT OSS641.9, ORIGINAL MATERIAL IS 7075T6-0063IN, CRACK LENGTH IS 0.09", DAMAGED CUTOUT SIZE IS 8.8SDR IPXA10658514Skin · crackedINSP TYPE:C, LT WING - NR 3 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED LT WING NR 3 SLAT INBD NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2 FIG 201 REV 46 JUST AT OSS723.9, ORG MATL IS 7075T6-0063IN, CRACK LENGTH 0.12" DAMAGED CUTOUT SIZE IS 8.875" X 7.125" TSDR IPXA10658513Skin · crackedINSP TYPE:C, LT WING - NR 3 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED LT WING NR3 SLAT OTBD NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2 FIG 201 REV 46 JUST AT OSS792.5, ORG MATL IS 7075T6-0063IN, CRACK LENGTH 0.13" DAMAGED CUTOUT SIZE IS 8.875" X 7.125" THSDR IPXA10658512Skin · crackedINSPECTION TYPE:C RHW - NR 9 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED RHW 9 SLAT INBD NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV46 JUST AT OSS572.5, ORG MATL IS 7075T6-0063IN, CRACK LENGTH 0.08 INCH DAMAGED CUTOUT SIZE IS 8.875 INCH BY 7.37SDR IPXA10658511Skin · crackedINSPECTION TYPE:C RHW - NR 9 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED RT WING NR 9 SLAT OTBD NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 46 JUST AT OSS641.9, ORG MATL IS 7075T6-0063IN, CRACK LENGTH IS 0.15 INCH, DAMAGED CUTOUT SIZE IS 8.875"SDR SWAA100860Skin · crackedDURING SCHEDULED HC2 CHECK, FOUND LT WING NR 1 SLAT OUTER SKIN CRACKED. REPAIRED SKIN PER SRM.SDR FDEA201002110391Skin · corrodedNR 2 SLAT ASSY LOWER FACE T/E OF LOWER AREA SKIN IS CORRODED.SDR USAA2010021590374Wedge · debondedCLT - MAJOR REPAIR - Q1 CHECK - RIGHT WING NR 6 SLAT INBOARD TRAILING EDGE WEDGE HAS A 4 INCH AREA OF DISBOND. REPAIRED RIGHT WING NR 6 SLAT INBOARD TRAILING EDGE WEDGE IAW B737 SRM 51-70-10 & 51-30-03.SDR SWAA100861Wedge · delaminatedDURING SCHEDULED HC2 CHECK, FOUND LT WING NR 2 SLAT UPPER T/E WEDGE DELAMINATED. REMOVED AND REPLACED NR 2 SLAT PER MM.SDR SWAA100794Skin · crackedDURING SCHEDULED 8Y CHECK, FOUND LT WING L/E NR 3 SLAT LOWER SURFACE CRACKED. REPAIRED NR 3 SLAT PER SRM.SDR AALA20100209TUL07Skin · crackedTHE NUMBER 9 SLAT BACK SKIN IS CRACKED AT THE INBOARD DRIVE TRACK FITTING AREA. REPAIRED SLAT PER AARD 57-43-00-4.SDR AALA20100209TUL06Skin · crackedTHE NUMBER 9 SLAT BACK SKIN IS CRACKED AT THE OUTBOARD DRIVE TRACK FITTING AREA. REPAIRED SLAT PER AARD 57-43-00-4.SDR AALA20100209TUL05Skin · crackedTHE NUMBER 8 SLAT BACK SKIN HAS TWO CRACKS AT THE INBOARD DRIVE TRACK FITTING AREA. REPAIRED SLAT PER AARD 57-43-00-4.SDR FDEA201002090540Skin · gougedRT WING NR 7 SLAT T/E BOTTOM SIDE GOUGED INBD OF SLAT HOOK WS 639. BLENDED OUT GOUGE AT NR 7 SLAT T/E WS 639, FOUND BLEND OUT OF LIMITS, FABRICATED REPAIR DOUBLER & INSTALLED REPAIR DOUBLER IAW SRM 51-30-2, SRM 57-50-1 FIG 2, SRM 57-50-3 FIG 10 & SRM 51-1SDR IPXA10558506Wedge · dentedNR 4 SLAT UPPER T/E WEDGE DENTED 49.5 INCHES FROM INBD, 4.6 INCHES FROM AFT. DENT FOUND TO BE OUT OF LIMITS ON TASK CARD 837228. NR 4 SLAT T/E WEDGE WAS REPAIRED IAW SRM 51-70-10-2R REPAIR 4.SDR SWAA100808Slat · crackedDURING SCHEDULED 2HC2 CHECK, FOUND LT WING L/E NR 2 SLAT CRACKED. REPAIRED SLAT PER SRM.SDR USAA2010021290350Slat · debondedPHX - B4 - MAJOR REPAIR - NR 4 SLAT DISBONDED AT INBOARD CORNER BETWEEN SLAT STA 12 TO SLAT STA 16. REPAIRED NR 4 SLAT AT INBOARD CORNER BETWEEN SLAT STA 12 TO SLAT STA 16 IAW B737 SRM 57-43-02 & 51-70-10.SDR USAA2010021290349Wedge · debondedPHX - B4 - MAJOR REPAIR - NR 3 SLAT DISBONDED ON THE TRAILING EDGE WEDGE END CAP AFT CORNER BETWEEN SLAT STA 115 TO SLAT STA 124.4. REPAIRED NR 3 SLAT SKIN IAW B737 SRM 57-43-02 & 51-70-10.SDR FDEA201002090375Skin · dentedRT WING SLAT NR 6 L/E SKIN HAS A DENT WS-179.SDR FOTR20006NR2016Skin · gougedLT WING NR 4 SLAT OTBD END GOUGED. REPAIRED ON W/O NR 20006, N/R 02016- R & R LT WING NR4 SLAT OTBD RIB IAW SRM 51-30-2, REV 102 WITH PN 65-17286-13.SDR FDEA201002060408Structure · crackedRT WING NR 5 SLAT T/E CRACKED, WS 400. ROUTED OUT DAMAGED EDGE AT RT WING NR 5 SLAT T/E IAW SRM 51-10-1, COMPLIED WITH HFEC INSP IAW NDTM 51-00-00 WITH NO CRACK NOTED, AREA FOUND TO BE WITHIN LIMITS IAW DWG SR27-57-046 AND SRM 57-50-1.SDR FDEA201002060407Skin · crackedRT WING NR 8 SLAT OTBD STOP PAD INBD SIDE SKIN CRACKED IN RADIUS OF SLAT SKIN, SLAT STA 760. REMOVED LOWER CHORD FROM NR 8 SLAT IAW SRM, REV 102, 51-30-2. FABRICATED NEW LOWER CHORD IAW SRM 57-50-2 FIG. 2, AND 51-30-5. INSTALLED LOWER CHORD IAW SRM 51-30-2SDR ASAA1047351Skin · debondedNR 2 SLAT T/E WEDGE LWR SURFACE DISBONDED OUT OF LIMITS. REMOVED DAMAGE AND PREVIOUS REPAIR AND INSTALLED DOUBLER REPAIR.SDR IPXA10M58517Skin · gougedINSP TYPE:C1, REPAIR SURVEY SEQ NR 282-W3-01 LT WING NR1 SLAT APPROX BETWEEN STA XIS 173-196 FLUSH REPAIR FILLER GOUGED. REMOVED EXISTING REPAIR, CORRECTED OLD DAMAGE CUT-OUT, FABRICATED AND INSTALLED REPAIR IAW SRM 57-40-01, REPAIR 11, FIG 201.SDR SWAA100714Structure · puncturedDURING SCHEDULED MV2 CHECK, FOUND RT WING NR 6 SLAT I/B TRACK CAN PUNCTURED. REMOVED AND REPLACED CAN PER SRM AND EA.SDR AALA20100204TUL13Bushing · wornLEFT WING KNUCKLE BUSHINGS WORN OUTBOARD END OF NUMBER 4 SLAT. REPLACED KNUCKLE RIB ON NUMBER 4 OUTBOARD SLAT WITH NEW ONE IAW AARD 27-80-00-2.SDR AALA20100204TUL17Skin · dentedLEFT WING NUMBER 1 SLAT INBOARD UPPER SURFACE DENTED AND DELAMINATED. REWORKED DENT USING EDR PER SRM 57-70-01-2R1. DENT IS WITHIN LIMITS PER SRM 57-43-02-1A1. TAP TESTED AND NO DELAMINATION FOUND. DYE CHECKED AREA, NO CRACKS FOUND.SDR USAA2010020890308Skin · debondedCLT - MAJOR REPAIR - Q1 CHECK - LEFT WING NR 3 SLAT TRAILING EDGE WEDGE UPPER SURFACE HAS AREA OF DISBOND. REPAIRED LEFT WING NR 3 SLAT TRAILING EDGE WEDGE UPPER SURFACE IAW B737 SRM 51-70-10.SDR ASAA1047341Wedge · delaminatedLEFT WING NR 3 SLAT O/B EDGE OF WEDGE DELAMINATED. INSTALLED FILLER AND DOUBLER.SDR ASAA1047340Skin · delaminatedNR 5 SLAT UPPER SURFACE I/B AFT CORNER DELAMINATED. REPAIRED BY INSTALLING FILLER AND DOUBLER.SDR SWAA100671Slat · delaminatedDURING SCHEDULED SPV CHECK, FOUND RT WING NR 5 SLAT DELAMINATED. REMOVED AND REPLACED NR 5 SLAT PER MM.SDR SWAA100661Skin · crackedDURING SCHEDULED 18Y CHECK, FOUND LT WING NR 1 SLAT SKIN LOWER SURFACED CRACKED. REMOVED AND REPLACED SKIN PER SRM.SDR FDEA201002040323Panel · crackedLT WING NR 1 SLAT IB OF PANEL 525CB INNER COVE PANEL CRACKED. REMOVED COVE PANEL IAW SRM 51-40-02, FABRICATED COVE PANEL ON TRAVELER T10/828657. LOCATED & DRILLED PANEL IAW SRM 51-40-05 TREATED & PRIMED IAW SRM 51-20-01. INSTALLED COVED PANEL TO NR 1 SLATSDR FDEA201002040322Panel · crackedLT WING NR 3 SLAT OB SIDE OF INNER COVE PANEL WITH PANEL 523BB ATTACHED IS CRACKED. REMOVED SEAL RETAINER &GUSSET FOR ACCESS, REMOVED COVE PNL IAW SRM 51-40-02. UPON REMOVAL FOUND GUSSET GOUGED, BLENDED GOUGE ON GUSSET, IAW SRM 51-10-02 ORIG MAT'L .032", MATSDR FDEA201002040321Skin · corrodedLT WING NR 4 SLAT OTBD LOWER SURFACE AFT OF ANTI ICE COVE PANEL CORRODED. ACCOMPLISHED EA F5740-131579. WING LT NR4 SLAT SKIN CORROSION. MAJOR REPAIR.SDR USAA2010020490280Flap · crackedSAL - MAJOR REPAIR - C22 CHECK - RIGHT WING KRUEGER FLAP CRACKED AT LES 189.5- LES 199.5. REPAIRED RIGHT WING KRUEGER FLAP AT LES 189.5- LES 199 IAW EA 132847.
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