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 2005FA0000016Fitting · damagedFOLLOWING DAMAGE WAS FOUND WHILE LT IB SLAT (PN F50B133B8, SN 133000 WAS AT THIS FACILITY FOR REPAIR. MILLED FITTING, (PN F50B133014) IS ATTACH POINT FOR NR 4 (OB) RAIL. SIX FASTENERS WERE IMPROPERLY INSTALLED THROUGH INNER SKIN OF SLAT. FOUR BLIND FASTENESDR AWXA200500024Wedge · delaminatedMCN - MAJOR REPAIR - DURING C-17 CHECK A DISBOND AREA WAS FOUND IN NR 5 SLAT WEDGE AT LOWER INBOARD END BETWEEN SS 124.53 AND SS 128.03. MAINTENANCE CUT OUT DAMAGE IN NR 5 SLAT WEDGE AT LOWER INBOARD END; FABRICATED A FILLER AND DOUBLER; BONDED REPAIR PARTS TSDR AWXA200500027Skin · delaminatedMCN - MAJOR REPAIR - DURING C-17 CHECK A DISBOND AREA WAS FOUND IN NR 5 SLAT WEDGE ON UPPER AND LOWER SURFACE AT OUTBOARD END BETWEEN SS 248.87 AND SS 254.27. MAINTENANCE REMOVED DAMAGE IN NR 5 SLAT WEDGE ON UPPER AND LOWER SURFACE AT OUTBOARD END; FABRICATEDSDR ASAA0410690Rib · crackedANC - NR 5 LEADING EDGE SLAT OUTBOARD MAIN TRACK RIB ATTACH ANGLE CRACKED. REPLACED STIFFENER. (M)SDR AWXA200500033Skin · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK 6 CRACKS WERE FOUND EMANATING FROM FASTENER HOLES ON LOWER SURFACE OF NR 3 SLAT BETWEEN OUTBOARD AUXILIARY TRACK AND TELESCOPING DUCT WBL 36.50 - 100.27 LT. MAINTENANCE CUT OUT DAMAGE IN LOWER SURFACE OF NR 3 SLAT; FABRISDR 04FDEA03433Web · chafedLT WING NR 3 L/E FLAP INBD ANTI-ICE DUCT CHAFING FLAP. REMOVED & REPLACED WEB IAW SRM 51-30-2, NEW WEB FABBED FROM 2024-T3 .050, BATCH 814135, FOUND INNER SKIN DAMAGED, CUT OUT AREA IAW SRM 57-30-4 FIG 5. FABBED & INSTALLED COVER & FILLER FROM 2024-T3 .016 BSDR 04FDEA03432Web · chafedLT WING NR 3 L/E FLAP INBD ANTI-ICE DUCT CHAFING FLAP. REMOVED & REPLACED WEB IAW SRM 51-30-2, NEW WEB FABBED FROM 2024-T3 .050, BATCH 814135, FOUND INNER SKIN DAMAGED, CUT OUT AREA IAW SRM 57-30-4 FIG 5. FABBED & INSTALLED COVER & FILLER FROM 2024-T3 .016 BSDR 04FDEA03421Rib · damagedDURING AIRPLANE'S CONVERSION FROM P-F/ACF FOUND AT LT SLAT NR 5 OUTBOARD SIDE, RIB WITH HOLES IN RADIUS ANGLE. REPLACE RIB ASSY PER SRM 51-35-01 PAGE 1-12 SRM 51-35-02 PAGE 3-9. P/N ARB1766-501.SDR UPS05M43893Rib · crackedNR 16 LEADING EDGE SLAT TRACK INBOARD FITTING FOUND WITH SIGN OF CRACK AS MARKED. HFEC C/O IAW DAC NDT SPM R.11 PART 06-10-01.001 AND CRACK CONFIRM APPROX 1/2 INCH LONG. LT NR 16 L/E SLAT TRACK AND DOOR REMOVED PER 57-40-01 REV 47 CRACKED. RIB REMOVED PER SSDR MWEA040220Doubler · crackedLEFT WING LEADING EDGE INTERNAL UPPER SURFACE DOUBLER HAS FOUR CRACKS AT THE EDGE OF THE STIFFENING INDENTATIONS, LOCATED APPROXIMATELY 5-14 INCHES INBOARD OF THE NUMBER TWO SLAT OUTBOARD TRACK. STOPPED DRILLED FOUR CRACKS.SDR ASA0440321Skin · scratchedOKC - FOUND RIGHT OUTBOARD FLAP UPPER SURFACE IS SCRATCHED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR CORE PLUG AND DOUBLER IAW SRM. (M)SDR UPS05M43894Rib · crackedRT WING NR 16 LEADING EDGE SLAT TRACK SUPPORT BRACKET FOUND WITH SIGN OF CRACK AS MARKED. HFEC C/O IAW DAC SPM R.11 PT.06-10-01.001 AND CRACK CONFIRM APPROX 5/8 INCH LONG. RT NR 16 SEAT TRACK AND DOOR REMOVED PER AMM 57-40-01 R.47. CRACKED RIB REMOVED AS PSDR SWAA043592Skin · crackedDURING SCHEDULED C3 CHECK, FOUND RT WING NR 6 L/E SLAT SKIN CRACKED. REPAIRED SLAT SKIN PER EA.SDR IXXA0500109SRepair · temporaryDURING A C CHECK INSPECTION, FOUND LT WING EXTENDED L/E OUTBOARD VANE FORWARD OUTER PLATING INTERIM REPAIR AROUND STA XOLDI 6.224. MAJOR REPAIR ACCOMPLISHED REMOVAL OF INTERIM REPAIR IAW DWG SEMON EO 3784, DC8 SRM 51-1-21 PG 1, DC7 SNR 51-1-20D PG 21, AND 51-SDR ASA0440262Wedge · dentedPAE - NR 1 SLAT T/E WEDGE UPPER SURFACE HAS TWO DENTS. REPAIRED DENTS PER SRM. (M)SDR ASA0440261Wedge · dentedPAE - NR 1 SLAT T/E WEDGE UPPER SURFACE HAS TWO DENTS. REPAIRED DENTS PER SRM. (M)SDR 04FDEA03377Skin · dentedACCOMPLISH MAINTENANCE "C" CHECK, NR 003 ENT BY: 067708, PLND: ORIGINAL PLAN DATE WAS ENTERED ON: 29SEP04 14:53:57:6 BY:067708 S=M PLND: DATE:06NOV04 AT: LIS-VNMX ENT BY: 162248 ON: 29OCT04 12:31:08:0 S=M. LEFT WING, KRUEGER FLAP OUTER SURFACE FOUND DENTED. SDR SWAA043523Skin · crackedDURING SCHEDULED C1 CHECK, FOUND RT WING NR 6 L/E SLAT SKIN CRACKED. REPAIRED RT WING NR 6 L/E SLAT SKIN PER SRM.SDR 04FDEA03339Slat Track · wornDURING AIRPLANE'S CONVERSION FROM P-F/ACF, FOUND AT LT WING FIX L/E NR 6 SLAT TRACK RIB WITH SEVERAL WEAR. REPLACE RIB PER SRM 51-33-01 PAGE 34/47. REPLACED P/N: ARB 1188-1 QTY: 8 ARB 1141-1 QTY: 1 ARB 1143-503 QTY:1 ARB 1147-503 QTY:1.SDR 05FDEA01203Rib · damagedDURING AIRPLANE`S CONVERSION FROM P-F/ACF FOUND AT LT SLAT NR 5 OUTBOARD SIDE RIB WITH HOLE IN RADIUS ANGLE. REPLACE RIB ASSY PER SRM 51-35-01 PG 1-12 SRM 51-35-02 PG 3-9. P/N ARB1766-501.SDR AWXA200401460Skin · delaminatedMCN - MAJOR REPAIR - DURING C-18 CHECK FOUND THE UPPER SURFACE OF THE NR 4 SLAT DELAMINATED AT THE INBOARD CORNER BETWEEN WS 521.30 AND WS 531.25. MAINTENANCE CUTOUT DAMAGED SKIN ON UPPER SURFACE OF NR 4 SLAT; FABRICATED AN INTERNAL & EXTERNAL DOUBLER; INSTALLSDR AWXA200401426Skin · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK 2 EACH CRACKS WERE FOUND IN RIVET HOLES OF NR 4 SLAT LOWER SKIN AT TEE CHORD AFT RIVET ROW SLAT STA 94.00. MAINTENANCE CUT OUT DAMAGED AREA OF NR 4 SLAT LOWER SKIN AT SS 94.00; FABRICATED A REPAIR FILLER AND SPLICE PLATESDR SWAA043467Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND LT WING NR 2 L/E SLAT DELAMINATED. REMOVED AND REPLACED LT NR 2 L/E SLAT PER MM.SDR BJNA041101Support Bracket · corrodedDURING A SCHEDULED C-CHECK INSPECTION, LEVEL TWO CORROSION WAS DISCOVERED ON A LEADING EDGE SLAT ACTUATOR SUPPORT BRACKET ON THE LEFT WING SPAR AT WING STATION 421. REMOVED AND REPLACED THE SUPPORT BRACKET AT THE CENTER OF THE NUMBER TWO LEADING EDGE SLAT ACTSDR DHL2004873520Door · crackedLEFT INBOARD SLOT UPPER DOOR CRACKED 1.000. REMOVED AND REPLACED INBOARD SLOT UPPER DOOR IAW SRM 51-3-0 PG 1.SDR 04FDEA03180Slat Track · wornLT WING FIXED L/E WORN FROM NR 1 SLAT TRACK INBD TO FUSELAGE IN SEVERAL PLACES, CAUSED FROM NR 1 SLAT LWR LIP. CUT OUT DAMAGED AREA FAB REPAIR DOUBLER PER SRM 57-10-00 FIG 40. INSTALLED REPAIR DOUBLER PER SRM 57-10-00 PAGE 129 FIG 40. N/R 64 GENERATED TO SUSDR 04FDEA03179Skin · crackedLT, INBD SIDE, NR 1 SLAT HAS APPROX. 56 INCH LONG CRACK ON INNER SURFACE, BOTTOM EDGE BELOW CLOSEOUT WEB. FASTENERS MISSING/PULLED. INSTALLED NEW NR 1 SLAT LT S/N MAC86 PER AMM 27-80-01-4 PARA 3(B) 1-13. RIGGED AND ADJUSTED LT NR 1 SLAT PER MM 27-80-01-4 3(BSDR UPS04843578Doubler · crackedRT WING L/E INTERNAL DOUBLER CRACKED AT DRAN HOLE, STA XFS329. FABRICATED REPLACEMENT DOUBLER FROM SHT7075T6/.090 PER SRM 57-3-0 FIG 12. TREATED AND PRIMED REF SRM 51-1-8. REMOVED AND REPLACED PART PER SRM 51-1-20D, 51-1-21.SDR USAA040979Skin · crackedPIT - Q5 - NR 3 SLAT, 6 INCH X 6 INCH AREA, CRACKED AND DISBONDED AT IB LOWER T/E. REMOVED SKIN AND CORE, REPLACED CORE AND REPAIR PLYS IAW SRM 51-70-10 AND EA 70537.SDR USAA040978Skin · bulgedPIT - Q5 - NR 3 SLAT, 1 INCH X 2 INCH BUBBLE IN SKIN, T/E AT SKIN JOINT 12 INCHES FROM IB END. REMOVED DAMAGE, INSTALLED FILLER AND REPAIR PLYS IAW SRM 51-70-10, EA 79537.SDR 0402039866Duct · lack of lubeWHEN SLATS WERE SELECTED TO EXTEND, THE AIRCRAFT ROLLED TO THE LEFT AND THE 'SLAT DISAGREE' LIGHT ILLUMINATED. COMPLIED WITH COM PROCEDURES AND THE SECOND ATTEMPT HAD THE SAME RESULTS. THE SLAT DISAGREE LIGHT DID NOT EXTINGUISH. FLIGHT LANDED UNEVENTFULLY ASDR 04FDEA03165Hinge · corrodedCORROSION ON LT WING NR 1 K-FLAP O/B BULLNOSE HINGE LUG AROUND FASTENERS UPPER SURFACE.SDR USAA040977Skin · crackedPIT - Q5 - NR 6 SLAT SKIN, .1250 TO 4 INCH CRACKS- NUMEROUS; LOWER SURFACE AFT ROW RIVETS - NUMEROUS AREAS ENTIRE LENGTH. REMOVED DAMAGE, INSTALLED DOUBLER IAW SRM 57-43-01, FIG 206.SDR UIEA200400196Spar · crackedD-CHECK, DURING SCHEDULED MAINTENANCE INSPECTION, CRACKS WERE FOUND AT ENDS OF THE NR 15 KRUEGER FLAP FRONT SPAR. TRIMMED OUT CRACKED REGION OF SPAR ATTACHED FLANGES. NDT INSPECTED TRIMMED EDGES TO ENSURE CRACK AND DEFECT FREE CONDITION. INSTALLED REPAIR FISDR UIEA200400197Spar · crackedD-CHECK, DURING SCHEDULED MAINTENANCE INSPECTION, CRACKS WERE FOUND AT ENDS OF THE NR 16 KRUEGER FLAP FRONT SPAR. TRIMMED OUT CRACKED REGION OF SPAR ATTACHED FLANGES. NDT INSPECTED TRIMMED EDGES TO ENSURE CRACK AND DEFECT FREE CONDITION. INSTALLED REPAIR FISDR SWAA043344Skin · delaminatedRIGHT WING NR 5 L/E SLAT DELAMINATED. REMOVED AND REPLACED NR 5 L/E SLAT PER MM.SDR 04FDEA03100Structure · crackedLT WING I/B MID FLAP TRAILING EDGE CHORD CRACKED AT THE I/B AFT FLAP ACTUATION ROD CUT OUT. REPAIRED PER SRM 51-40-4, 51-30-2, OHM 20-50-01, 20-50-02.SDR IXXA0500088SVane · damagedDURING A ROUTINE C-CHECK INSPECTION, FOUND LEADING WING EXTENDED LEADING EDGE OUTBOARD VANE FORWARD OUTER PLATING INTERIM REPAIR AROUND STATION XOLDO 67.000. MAJOR REPAIR ACCOMPLISHED. REMOVED INTERIM REPAIR, REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION ASDR USAA040983Structure · crackedPIT - Q5 - NR 4 SLAT, SEVERAL .1250 INCH TO .2500 INCH CRACKS, LWR SURFACE, AFT ROW RIVETS AREA OF ACTUATOR. INSTALLED DOUBLER IAW SRM 57-43-01, FIG 206.SDR USAA040843Skin · crackedSKIN, .1250 INCH CRACKS, LOWER SURFACE AFT ROW OF RIVET, NR 5 SLAT IB TRACK AREA. INSTALLED DOUBLER IAW SRM 57-43-01, FIG 206.SDR USAA040937Skin · delaminatedPIT - Q1 - SLAT 15 INCH BY 6 INCH DELAMINATION. NR 3 SLAT IB END. REMOVED TOP SKIN AND CORE, INSTALLED INTERNAL DOUBLER, CORE, TOP SKIN TYP REP 57-42-03, SRM 51-70-10.SDR AWXA200401244Skin · debondedDURING C-15 CHECK, AN AREA OF DISBOND WAS FOUND ON LT WING NR 3 SLAT INBOARD TRAILING EDGE TIP BETWEEN SLAT STA 12.25 AND 15.25 LT. MAINTENANCE REMOVED DISBONED NR 3 SLAT SKIN; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-10,SDR USAA041043Skin · delaminatedPIT - Q1 - TOP SKIN, 3 INCH X 3 INCH AREA AND LOWER SKIN DAMAGE 1 INCH SQUARE, DELAMINATION AND SKIN DAMAGE, NR 4 SLAT TOP SURFACE T/E. INSTALLED FILLER AND INTERNAL DOUBLER, NEW CORE AND TOP DOUBLER IAW SRM.SDR AWXA200401303Skin · crackedMCN - MAJOR REPAIR - DURING C-15 CHECK 3 EACH .125 INCH CRACKS WERE FOUND IN NR 6 SLAT LOWER SKIN AT AFT ROW RIVET HOLES INBOARD OF ACTUATOR ATTACH FITTINGS SLAT STA 291 RT THRU SLAT STA 294 RT. MAINTENANCE CUT OUT DAMAGE IN NR 6 SLAT LOWER SKIN FROM SS 291 RSDR USAA040944Skin · delaminatedPIT - Q5 - NR 2 SLAT SKIN, 3 INCH BY 4 INCH AREA, DELAMINATION, OB END T/E. REMOVED DAMAGE SKIN AND CORE, INSTALLED NEW CORE, TOP DOUBLER IAW SRM 51-70-10.SDR CALA0400688Skin · crackedINSPECTION FOUND A .25 INCH CRACK IN NR 3 SLAT SKIN BELOW ACTUATOR. A DOUBLER WAS INSTALLED ON LOWER SKIN IAW SRM 57-43-01.SDR USAA040900Skin · crackedPIT - Q5 - NR 4 SLAT SKIN, 6 FASTENER HOLES, .1250 INCH TO .2500 INCH CRACK. FASTENER HOLES, LOWER SKIN AREA BELOW ACTUATOR ATTACH POINT. CUT OUT DAMAGE, INSTALLED FILLER AND DOUBLER IAW SRM 57-43-01, FIG 206.SDR USAA040943Skin · delaminatedSKIN AND CORE, 4 INCH BY 4 INCH AREA, IB T/E NR 4 SLAT. REMOVED DELAMINATED SKIN AND CORE, INSTALLED DOUBLER, NEW CORE IAW 51-70-10.SDR SWAA043083Skin · crackedDURING SCHEDULED C3 CHECK, FOUND LT WING NR 1 L/E SLAT SKIN CRACKED. REPAIRED L/E SLAT SKIN PER EA.SDR 04FDEA02974Vane · corrodedLT WING IB FLAP VANE, IB TEE FITTING BORES HAVE CORROSION AND AFT HOLE IS NOT WITHIN EO LIMITS. CORROSION REMOVED AS PER SRM 51-21-01 VOL2 AND REPAIRED AS PER FEDEX EA 1-5750-81571.
Back to JASC 5754