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 IPXA10560118Skin · chafedINSPECTION TYPE:C3, NR 3 SLAT T/E WEDGE INNER SKIN IS CHAFED. NR 3 SLAT T/E WEDGE WAS REPAIRED IAW SRM 51-70-10-2R-4 REPAIR 4 AND SRM 51-70-10-2R REPAIR GENERAL.SDR SWAA102948Wedge · delaminatedDURING SCHEDULED 18Y CHECK, FOUND LT WING NR 2 SLAT O/B WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.SDR SWAA102890Skin · delaminatedDURING SCHEDULED 16Y CHECK, FOUND RT WING NR 6 SLAT T/E OUTBOARD END UPPER SURFACE DELAMINATED. REPAIRED SLAT PER SRM.SDR AALA20100518TUL03Skin · damagedLEFT HIGH LIFT OUTBOARD NUMBER 4 SLAT DAMAGED UNDER GAP SEAL AT CENTER TRACK. CUT OUT DAMAGED SKIN, MANUFACTURED AND INSTALLED FLUSH PATCH PER SRM 57-09-00.SDR SWAA102870Wedge · delaminatedDURING SCHEDULED 14Y CHECK, FOUND LT WING NR 2 SLAT UPPER T/E WEDGE I/B EDGE DELAMINATED. REMOVED AND REPLACED NR 2 SLAT PER MM.SDR UALA2010051901699Skin · dentedLT NR 1 SLAT HAS DENT BEYOND LIMITS. NR 1 SLAT REPAIRED.SDR 2010FA0000582Rib · cracked((OF1R)) DURING AN ANNUAL INSP, THE RT FLAP RIB WAS FOUND CRACKED THROUGH THE L/E RELIEF CUTOUT, IN THE UPPER FANGE BEND RADIUS, AND THROUGH THE ACTUATOR ATTACH BRACKET NUTPLATE RIVET HOLES. THIS COULD ONLY BE VIEWED THROUGH THE INBD ROLLER BOLT ACCESS HOLE. SDR 2010FA0000581Rib · cracked((OF1R)) DURING AN INSP, PRIOR TO PURCHASE, THE LT FLAP NOSE RIB WAS FOUND CRACKED THROUGH THE L/E RELIEF CUTOUT, IN THE UPPER FLANGE BEND RADIUS, AND THROUGH THE ACTUATOR ATTACH BRACKET NUTPLATE RIVET HOLES. THIS IS A VERY DIFFICULT AREA TO ACCESS AND INSPECSDR 2010FA0000580Rib · cracked((OF1R)) DURING AN ANNUAL INSP, 1 RT FLAP NOSE RIB WAS FOUND CRACKED. IT IS THE RIB LOCATED DIRECTLY BENEATH THE ACTUATOR ATTACH BRACKET. IT WAS CRACKED IN THE RELIEF CUTOUT FOR THE FLANGES AND THROUGH THE MOST FWD NUTPLATE RIVET HOLES. VERY INACCESSABLE ASDR IPXA10560089Wedge · chafedINSPECTION TYPE:C4, RT WING NR 8 SLAT T/E WEDGE LOWER SURFACE HAS CHAFING JUST ABOVE OTBD MAIN TRACK (FOUND TO BE OUT OF LIMITS ON CARD NR 861178) REPAIRED RT WING NR 8 SLAT T/E WEDGE LOWER SURFACE IAW SRM 51-70-10-2R
REPAIR 4.SDR ABXA201005200079Support · corrodedLT WING LE NR 3 SLAT INBD AUX TRACK HAS CORROSION ON INBD & OUTBD SUPPORTS. REMOVED CORROSION ON I/B SUPPORT IAW SRM51-10-02. REMOVED AND REPLACED SUPPORT IAW SRM 51-47-02SDR UALA2010051701664Skin · scratchedSLAT NR 14 HAS A LONG SCRATCH. ON ARRIVAL FOUND SLAT NR 14 L/E WITH A 46 INCH LONG SCRATCH. SCRATCH IS 46 INCH LONG. DEEPEST SECTION IS 5.5 INCH LONG AND 0.016 DEEP. BLENDED OUT IAW SRM 57-43-01. HFEC INSP ACP. NO CRACKS NOTED. SPEED TAPE APPLIED. NR 14 SDR USAA2010051890984Skin · delaminatedCLT - Q3 - MAJOR REPAIR - NR 03C40257009/006 - DELAMINATION ON NR 4 SLAT AT INBOARD END ON LOWER SURFACE. REPAIRED NR 4 SLAT AT INBOARD END ON LOWER SURFACE IAW B737 SRM 51-70-10 REPAIR 4.SDR UALA2010051701657Skin · damagedNR 5 SLAT HAS DAMAGE. NR 5 SLAT DAMAGED DUE TO LAV DOOR DEPARTING ACFT. DRESSED OUT DAMAGE ON NOSE SKIN OF NR 5 SLAT, POTTED DAMAGE ON TOP SKIN AND PREPPED FOR METAL BOND REPAIR. SKIN SURFACE ETCHED AND PRIMER APPLIED, NEEDS PATCH LAID UP AND CURED (REPAIR NRSDR SWAA102807Skin · crackedDURING SCHEDULED HC2 CHECK, FOUND LT WING NR 1 SLAT CRACKED AT LOWER SKIN. R&R NR 1 SLAT PER MM.SDR IPXA10560158Skin · chafedINSPECTION TYPE:C1, NR 8 SLAT INBD END RIB LWR AFT IS CHAFED AFT OF TAI DUCT CUTOUT, BLEND AREA, HFEC NO CRACKS NOTED, & REFINISHED FLAP PEENED IAW ER NR 10-2853, DATED 5-26-10.SDR SWAA102764Wedge · delaminatedDURING SCHEDULED 14Y CHECK, FOUND LT WING NR 2 SLAT T/E WEDGE DELAMINATED AT O/B END. REPAIRED WEDGE PER SRM.SDR SWAA102756Skin · crackedDURING SCHEDULED 16Y CHECK, FOUND LT WING NR 1 SLAT LOWER SKIN CRACKED AT O/B END. REPAIRED NR 1 SLAT PER MM.SDR SWAA102723Slat · damagedDURING SCHEDULED MV2 CHECK, FOUND RT WING NR 4 SLAT O/B OF NR 1 ENG DAMAGED. REMOVED AND REPLACED SLAT PER MM.SDR FDEA201005131535Rib · crackedLT WING NR 2 L/E SLAT INBD & OTBD RIBS ARE CRACKED WHERE ACTUATOR ROD END MOUNTS. R & R INBD & OTBD ACTUATOR RIBS PN 65-17310-3 & 65-17310-4, FABRICATED 1 EA OTBD RIB APPROX WS 251 FROM 7075-O .040 DIM: 16.25" X 6" & FABRICATED NEW ACTUATOR RIB CHANNEL FROSDR AALA20100512TUL02Slat · corrodedCORROSION AROUND BLIND FASTENER AT OUTBOARD BOTTOM BLIND FASTENER. BLENDED CORRODED AREA AND INSTALLED STRAP-DOUBLER PER EA B757-27-010644.SDR AALA20100512TUL01Skin · corrodedNUMBER 9 SLAT, CORROSION ON SKIN AT DRIVE-TRACK. INSTALLED A FLUSH-DOUBLER PER SRM-57-43-01-2R.SDR USAA2010060191052Skin · delaminatedCLT - Q3 - MAJOR REPAIR - DELAMINATION ON NR 4 SLAT UPPER SURFACE AT OUTBOARD END. REPAIRED NR 4 SLAT UPPER SURFACE AT OUTBOARD END IAW B737 SRM 51-70-10.SDR SWAA102704Slat · delaminatedDURING SCHEDULED 16Y CHECK, FOUND RT WING NR 5 SLAT AT I/B EDGE DELAMINATED. REPAIRED SLAT PER SRM.SDR AALA20100507TUL23Skin · dentedNUMBER 10 SLAT HAS DENT BELOW SRM LIMITS ABOUT 9.5 INCHES FROM OUTBOARD END ON LEADING EDGE SKIN. INSTALLED FLUSH REPAIR DOUBLER PER AARD 57-43-00-1.SDR AALA20100507TUL22Skin · dentedNUMBER 10 SLAT HAS DENT BELOW SRM LIMITS ABOUT 1.5 INCHES FROM OUTBOARD END ON LEADING EDGE. CUT OUT DAMAGED AREA AND FABRICATED DOUBLERS PER AARD 57-43-00-1.SDR FDEA201005071485Angle · crackedSPLICE DOUBLER CRACKED - NR 7 SLAT T/E CHORD ANGLE BENEATH TAI DUCT, APPROXIMATE WING STA 619. REMOVED T/E CHORD ANGLE OF NR 7 SLAT IAW SRM, REV 102, 51-30-2. LOCATED, DRILLED, DEBURRED AND TRIMMED CHORD ANGLE, 114" LONG, IAW SRM 57-50-2 FIG 2 AND 51-30-5. SDR AALA20100506TUL03Skin · corrodedRIGHT WING NUMBER 9 SLAT SKIN HAS NEW AREA OF CORROSION FORWARD OF OUTBOARD MAIN TRACK. CUT OUT CORRODED AREA, FABRICATED AND INSTALLED DOUBLERS AND FILLER PER AARD 57-43-00-1.SDR AALA20100506TUL01Rib · crackedNUMBER 5 BRACKET CRACKED IN RADIUS. REMOVED AND REPLACED RIB ASSEMBLY PER ESO 27-80-1.SDR USAA2010052491011Skin · crackedCLT - MAJOR REPAIR - Q3 CHECK - CRACKED NR 1 SLAT, LEFT WING, LOWER SKIN OUTBOARD END. REPAIRED CRACKED NR 1 SLAT, LEFT WING, LOWER SKIN OUTBOARD END IAW B737 SRM 57-40-01 REPAIR 6.SDR USAA2010052491010Skin · crackedCLT - MAJOR REPAIR - Q3 CHECK - CRACKED NR 1 SLAT, LEFT WING, LOWER SKIN 69 INCHES FROM INBOARD END. REPAIRED CRACKED LEFT WING NR 1 SLAT LOWER SKIN 69 INCHES FROM INBOARD END IAW B737 SRM 57-40-01, REPAIR 6.SDR USAA2010051190938Skin · crackedCLT - Q3 - MAJOR REPAIR - CRACK ON NR 3 SLAT LOWER SKIN 34 INCHES FROM INBOARD END. REPAIRED NR 3 SLAT LOWER SKIN 34 INCHES FROM INBOARD END IAW B737 SRM 57-40-01 REPAIR 6.SDR FDEA201005061476Structure · crackedUPON REMOVAL OF T/E ACCESS PANELS, FOUND NR 4 SLAT T/E STRUCTURE CRACKED NEAR TAI DUCT CUTOUT. REMOVED T/E STRUCTURE IAW SRM 51-30-2. FABRICATED NEW STRUCTURE USING EXTRUSION, BAC1514-1559 2024 T3511, DIMENSIONS 120", IAW SRM 57-50-2 FIG 2, 51-30-5, AND 51-30-SDR AALA20100505TUL08Rib · damagedRIGHT WING NUMBER 9 SLAT AT FORWARD OF OUTBOUND MAIN TRACK HAS DAMAGED RIB. INSTALLED FABRICATED RIB. UNDER ESO 90249, AARD 57-43-00-1, AARD 51-20-00-1.SDR FDEA201005051461Skin · misrepairedAGING INSP - EXISTING REPAIR ON RT WING SLAT ASSY NR 6 LOWER SURFACE. EXISTING REPAIR ON RT WING SLAT ASSY NR 6 LOWER SURFACE EVALUATED, FOUND NOT IAW SRM. SLAT ASSY NR 6 R & R IAW AMM 27-80-30. OPERATION TEST CARRIED IAW AMM 27-80-30 FOUND SATISFACTORY. EOSDR USAA2010050790923Skin · delaminatedPHX - B3 - MAJOR REPAIR - NR 4 SLAT IS DELAMINATED AT TRAILING EDGE UPPER SURFACE. REPLACED NR 4 SLAT IAW B737 AMM 27-81-00 & 27-81-21.SDR FDEA201005051460Rib · crackedRT WING - SLAT ASSY NR6, XOS 868 RIB FOUND CRACKED. RT WING SLAT ASSY NR 6, R & R IAW AMM 27-80-30-4, REVISION 64. SLAT ADJUSTMENT AND TEST CARRIED OUT IAW AMM 27-80-30-4, REV 64. FOUND SATISFACTORY.SDR FDEA201005051459Rib · crackedRT WING - SLAT ASSEMBLY NR 6, XOS 858 RIB FOUND CRACKED. RT WING SLAT ASSY NR 6 R & R IAW AMM 27-80-30-4, REV 64. SLAT ADJUSTMENT AND TEST CARRIED OUT IAW AMM 27-80-30-4, REV 64 FOUND SATISFACTORY.SDR FDEA201005051457Rib · crackedRT WING - SLAT ASSY NR 6, XOS 863 RIB FOUND CRACKED. AFTER REMOVAL OF EXISTING REPAIR DOUBLER. RT WING - SLAT ASSY NR 6 R & R IAW AMM 27-80-30-4, REV 64. SLAT ADJUSTMENT AND TEST CARRIED OUT IAW AMM 27-80-30-4 REV 64. FOUND SATISFACTORY.SDR AALA20100504TUL05Rib · damagedRIGHT WING NUMBER 9 SLAT HAS PREVIOUS BLENDING AT CENTER RIB. CUT OUT DAMAGED AREA AT CENTER RIB. INSTALLED FLUSH DOUBLERS AND FILLER PER AARD 57-43-00-1.SDR IPXA10M60185Fairing · delaminatedINSPECTION TYPE:4C, LT WING INBD SLAT NR1 CRUISE PERFORMANCE FILLET L/E ERODED, DELAMINATED. REPAIRED CRUISE FAIRING REF SRM 51-62-01.SDR IPXA10659798Skin · crackedINSPECTION TYPE:C, RT WING NR 10 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. RT WING NR 10 SLAT L/E OTBD NOSE SKIN AT OSS792.5 AREA SKIN REPAIRED IAW SRM 57-43-01-2R2 FIG 201, ORG MATL IS CLAD7075T6-0.063IN, CRK LENGTH IS 0.1" DAMAGED CUTOUT IS 8.875" X 7" SDR IPXA10659793Skin · crackedINSPECTION TYPE:C, LT WING NR4 SLAT L/E INBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR 4 SLAT L/E INBD NOSE SKIN AT OSS572.5 AREA SKIN REPAIRED IAW SRM 57-43-01-2R2 FIG, 201, ORG MATL IS CLAD7075T6-0.063IN, CRK LENGTH IS 0.11" DAMAGED CUTOUT IS 8.875" X SDR USAA2010050790924Mount · crackedPHX - B3 - MAJOR REPAIR - CRACK ON LEFT OUTBOARD KRUEGER FLAP HINGE MOUNT AT WS 210. REPAIRED LEFT OUTBOARD KRUEGER FLAP HINGE MOUNT AT WS 210 IAW B737 SRM 51-42-11.SDR USAA2010050690892Skin · delaminatedPHX - B03 - MAJOR REPAIR - NR 3 SLAT HAS 2 AREAS OF DELAMINATION AT UPPER TRAILING EDGE SURFACE AT SS12 & SS124. REPLACED NR 3 SLAT IAW AMM 27-81-21-4.SDR AALA20100504TUL01Slat · corrodedRIGHT WING NUMBER 8 SLAT HAS NEW AREA OF CORROSION FORWARD OF OUTBOARD AUXILIARY TRACK ON LOWER SURFACE. REMOVED CORROSION, FABRICATED AND INSTALLED STRAP DOUBLER PER EA B757-27-010445-4-28-10.SDR IPXA10659797Skin · crackedINSPECTION TYPE:C, RT WING NR 10 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED. RT WING NR 10 SLAT L/E INBD NOSE SKIN AT OSS723.9 AREA SKIN REPAIRED IAW SRM 57-43-01-2R2 FIG201, ORG MATL IS CLAD7075T6-0.063IN, CRK LENGTH IS 0.13" DAMAGED CUTOUT IS 8.875" X 7"SDR IPXA10659796Skin · crackedINSPECTION TYPE:C, RT WING NR 9 SLAT OTBD SE SKIN RIVET HOLE FOUND CRACKED RT WING NR9 SLAT L/E OTBD NOSE SKIN AT OSS641.9 AREA SKIN REPAIRED IAW SRM 57-43-01-2R2 FIG 201, ORG MATL IS CLAD7075T6-0.063IN, CRK LENGTH IS 0.2" DAMAGED CUTOUT IS 8.875" X 7.125"SDR IPXA10659795Skin · crackedINSPECTION TYPE:C, RT WING NR 9 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED. RT WING NR 9 SLAT L/E INBD NOSE SKIN AT OSS572.5 AREA SKIN REPAIRED IAW SRM 57-43-01-2R2 FIG201, ORG MATL IS CLAD7075T6-0.063IN, CRK LENGTH IS 0.13" DAMAGED CUTOUT IS 8.875" X 7.125SDR IPXA10659794Skin · crackedINSPECTION TYPE:C, LT WING NR 4 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR 4 SLAT L/E OTBD NOSE SKIN AT OSS641.9 AREA SKIN REPAIRED IAW SRM 57-43-01-2R2 FIG 201, ORG MATL IS CLAD 7075T6-0.063IN, CRK LENGTH IS 0.2" DAMAGED CUTOUT IS 8.875" X 7.1
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