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 SWAA2023030693637Skin · crackedCRACK AROUND THE FASTENER AT NO.1 SLAT LOWER SURFACE OF THE L/E SLAT NOSE SKIN AT ACTUATOR RIBS. MARKED<[01] NDI VERIFY CRACK AROUND THE FASTENER AT NO.1 SLAT LOWER SURFACE OF THE L/E SLAT NOSE SKIN AT ACTUATOR RIBS AND MARK ENDS PER SRM 51-10-02-0G-0;[10] FABSDR DALA2023011900402Skin · dentedTHE NR 1 SLAT, WAS FOUNDED DENTED A AND SCRATCHED ON THE TOP SKIN. REPAIRED IAW ERA 602677-14.SDR FDEA202301160113Rib · crackedWHILE CARRYING OUT INTERNAL BORESCOPE INSPECTION ON LEFT HAND NUMBER 7 SLAT LOOSE RIVETS AREA (SNRM N00517) , FOUND THE SLAT INTERNAL RIB CRACK AT STATION XOS 963.009. RIB AT LEFT HAND NUMBER 7 SLAT INTERNAL AT STATION XOS 963.009 AREA REPAIRED AS PER ESDR FDEA202301160112Rib · crackedWHILE CARRYING OUT INTERNAL BORESCOPE INSPECTION ON LEFT HAND NUMBER 7 SLAT LOOSE RIVETS AREA (SNRM N00517) , FOUND THE SLAT INTERNAL RIB CRACK AT STATION XOS 983.612. RIB AT LEFT HAND NUMBER 7 SLAT INTERNAL AT STATION XOS 983.612 AREA REPAIRED AS PER ESDR FDEA202301160111Rib · crackedWHILE CARRYING OUT INTERNAL BORESCOPE INSPECTION ON LEFT HAND NUMBER 7 SLAT LOOSE RIVETS AREA (SNRM N00517) , FOUND THE SLAT INTERNAL RIB CRACK AT STATION XOS 968.159. RIB AT LEFT HAND NUMBER 7 SLAT INTERNAL AT STATION XOS 968.159 AREA REPAIRED AS PER ESDR DALA2023011800367Wedge · debondedDISBOND OF 1.500IN LENGTH X 1.000IN WIDTH ON ISS109 UPPER SURFACE, LE SLAT 5 TRAILING EDGE WEDGE, LH WING. DISBOND ON ISS109 UPPER SURFACE, LE SLAT 5 TRAILING EDGE WEDGE, LH WING WAS REPAIRED PER B757-200 SRM.SDR DALA2023011800366Wedge · debondedDISBOND OF 1.500IN LENGTH X 1.200IN WIDTH ON OSS410 UPPER SURFACE, LE SLAT 7 TRAILING EDGE WEDGE, RT WING. DISBOND ON OSS410 UPPER SURFACE, LE SLAT 7 TRAILING EDGE WEDGE, RH WING WAS REPAIRED IAW SRM.SDR IXXA2023011501Structure · crackedNR 1 SLAT LWR TRAILING EDGE IS CRACKED, INBOARD END.SDR SWAA2023021491563Web · corrodedCORROSION FRONT SPAR ON INDICATOR FUEL TANK WEB AT RT WING 2023-38015<[01] REPLACED REFUEL PANEL P15 IAW B737-700 AMM 28-21-00-000-801; AMM 28-41-61-000-801; AMM 28-21-00-400-801 AND 28-41-61-400-801; TEST IS OK; TOOL USED: MILLIOHMETTER; P/N: M1 MILLIOHM METESDR DALA2023011800385Skin · corrodedDURING INSPECTION FOUND #3 SLAT T/E WEDGE LOWER SURFACE CORRODED MULTIPLE PLACES. FOUND TO BE OUT OF LIMITS ( OVER 50 INCHES LONG ) IAW B737-900ER SRM 57-42-01-2R-12 AND SRM 51-70-10-2R. R&R #3 SLAT ASSY IAW AMDS T/C: 2780-4522-02.SDR DALA2023011700335Wedge · debondedNR 5 SLAT T/E WEDGE UPPER SURFACE IS DISBONDED AT PREVIOUS REPAIR IN CENTER OF SLAT T/E WEDGE. REF AMDS CARD. REMOVED DISBONDED DOUBLER, FABRICATED REPLACEMENT DOUBLER & INSTALLED PERMANENT REPAIR IAW SRM.SDR SWAA2023021796806Slat · pulledSLAT #7 LOWER L/E SKIN AT ACTUATOR SUPPORT RIB ATTACH POINT HAS PROTRUDING FASTENER HEADS.<[01] REMOVED PANEL 624DB AT SLAT #7 IAW SRM 51-40-02.;[02] REMOVED AND REPLACED FASTENERS AT SLAT #7 LOWER L/E SKIN AT ACTUATOR SUPPORT RIB ATTACH POINT IAW SRM 57-42-01SDR SWAA2023021690434Slat · debondedSLAT #5 HAS DISBONDED FILLER MATERIAL AT INNER T/E O/B CORNER.<[01] #5 SLAT WAS REPLACED ON FAULT TTG8Q00H6ZBY;[02] VERIFIED. TASK CARD COMPLETE.SDR SWAA2023021690433Wing · delaminatedRIGHT WING COMPOSITE FIXED LEADING EDGE UPPER SURFACE IS DELAMINATED FROM OFSS 655 TO OFSS 683.<[01] IDENTIFIED R/H O/B UPPER FIXED LEADING EDGE MATERIAL ACCORDING TO SRM 57-41-01-0I-3; FIG. 4; TABLE 4; ITEM 1; AND FIG. 8; TABLE 8. <BR><BR>FOUND DAMAGE TO BE OSDR DALA2023011200252Wedge · debondedSHIP 689 A.A. - A.D. DISBOND OF 4.000IN LENGTH X 1.000IN WIDTH ON OSS343 UPPER SURFACE, LE SLAT 4 TRAILING EDGE WEDGE, LH WING. CORRECTIVE ACTION: SUMMARY OF NRC 00014: AREA AT OSS343 UPPER SURFACE, LE SLAT 4 TRAILING EDGE WEDGE LH WING WAS REPAIRED PER B757-2SDR DALA2023011200251Wedge · debondedSHIP 689 A.A. - A.D. DISBOND OF 1.300IN LENGTH X 1.000IN WIDTH ON OSS315 UPPER SURFACE, LE SLAT 4 TRAILING EDGE WEDGE, LH WING. CORRECTIVE ACITON: SUMMARY OF NRC 00013: AREA AT OSS 315 UPPER SURFACE ON SLAT #4 TRAILING EDGE LH WING WAS REPAIRED PER B757-200 S.SDR DALA2023021401140Slat · corroded(LOG 2576051) DURING INSPECTION FOUND #1 SLAT UPPER T/E HAS MULTIPLE AREAS OF CORROSION. REMOVED AND REPLACED #1 SLAT ASSY DURING HCK IAW AMDS T/C: 2780-4522-01.SDR DALA2023011100222Support Bracket · crackedCRACKED SLAT TRACK NR 1, ANGLE ON RT WING. REPLACED SUPPORT BRACKET ON SLAT TRACK 1 RT WING.SDR SWAA2023011089976Skin · crackedLEFT WING #1 SLAT LOWER SKIN CRACKED AT ACTUATOR MOUNT FITTING CRACK IS APPROX .5 LONG AND 2 FWD OF THE AFT EDGE. REMOVED #1 SLAT PER AMM 27-81-21 THRU STEPS 2G(10);[02] R/R #1 SLAT PER AMM 27-81-21. R/R LEFT WING #1 SLAT PER AMM 27-81-21. R/R LEFT WING #1 SSDR FDEA202301090058Skin · wornRH WING, SLAT # 8, TRAILING EDGE WEDGE, BOTTOM SKIN WITH WEAR. RH WING, SLAT #8, TRAILING EDGE WEDGE BOTTOM SKIN WAS REPAIRED IAW SRM 51-70-10-2R PAG. 163, FIG. 202 REV. 85 DEC15/2022 AND SRM 57-43-02-2R FIG. 201, (SHEET 1) REV. 85 .SDR IPXA2024011592332Panel · dentedNO. 13 KRUEGER FLAP PANEL DENT/DELAMINATION***SM26/LMX6*** ALL JOB DONESDR DALA2023011100223Support Bracket · crackedCRACKED SLAT TRACK NR 1, SUPPORT BRACKET ON LT WING. REMOVED AND REPLACED THE SUPPORT BRACKET.SDR SWAA2023021489046Skin · crackedCRACK LOWER SURFACE SLAT 6 ON EXTERNAL SKIN LOCATED SLAT STA 202.45 APPROX. RT WING 2023-37740<[01] TOOL USED: EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 210138503; DUE DATE: 19-MAY-23;[02] TOOL USED EDDY CURRENT EQUIPMENT PN/ NORTEC 600D; SN/ 210138503; DUSDR FDEA202301060039Rib · crackedRIGHT HAND WING - #8 SLAT ASSEMBLY STATION XOS 1146.814 INTERNAL RIB CRACKED. RIGHT HAND WING #8 SLAT ASSEMBLY STATION XOS 1146.814 INTERNAL CRACKED RIB REMOVED AND REPLACED AS PER MD-11 SRM 51-31-01-0G. RIB FABRICATED AS PER DOUGLAS DRAWING ARB 1954 REVISSDR FDEA202301060038Rib · crackedLEFT HAND WING - #6 SLAT ASSEMBLY STATION XOS 806.424 INTERNAL RIB CRACKED. LEFT HAND WING #6 SLAT ASSEMBLY STATION XOS 806.424 INTERNAL CRACKED RIB REMOVED AND REPLACED AS PER MD-11 SRM 51-31-01-0G. RIB FABRICATED AS PER DOUGLAS DRAWING ARB 1824 REVISION SDR FDEA2023010960033Rib · crackedRIGHT HAND WING - #6 SLAT ASSEMBLY STATION XOS 822.002 INTERNAL RIB CRACKED. RIGHT HAND WING #6 SLAT ASSEMBLY STATION XOS 822.022 INTERNAL CRACKED RIB REMOVED AND REPLACED AS PER MD-11 SRM 51-31-01-0G. RIB FABRICATED AS PER DOUGLAS DRAWING ARB 1825 REVISIOSDR AALA202301130052Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT #1, SLAT TRACK 3 LOWER BOLT. MAINTENANCE REPLACED BOLT PER TASK CARD 26C51057005 .SDR AALA202301132832Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK 7 LOWER BOLT. MAINTENANCE REPLACED BOLT PER AMM 27-84-65.SDR SWAA2023021387673Bracket · crackedL/H WING L/E #1 SLAT I/B AUXILIARY TRACK LOWER I/B BRACKET CRACKED. (18-006)<[01] REMOVER BRACKET AT L/H WING L/E #1 SLAT I/B AUXILIARY TRACK LOWER I/B PER REF SRM 51-40-02-0G-0.;[02] VERIFIED STEP 1;[03] OK TO INSTALL NEW BRACKET.;[04] REPLACED L/H WING L/E #SDR SWAA2023020887272Panel · delaminatedLT WING L/E PANEL 521CB FWD O/B CORNER IS DELAMINATED<REMOVED DAMAGED PLIES TO FWD O/B CORNER AND CLEANED IAW SRM 51-70-05-2R-6 PAR. 4.A.-D.<BR><BR>UPDATED MEASUREMENTS TABLE. FABRICATED AND INSTALLED REPAIR PLIES TO REPAIR AREA USING BMS8-79 CL3 ST1581 LOT# 1SDR SWAA2023020887278Panel · crackedRT WING L/E PANEL 621PB IS CRACKED AT I/B FWD CORNER (MARKED)<BEGAN FABRICATING REPAIR PLIES USING REPAIR FABRIC BMS 8-79 CL3 ST1581 LOT# 1510611-1; BMS 8-79 CL3 ST120 LOT# 1513772-2; AND ADHESIVE FILM BMS 5-129 TY2 GR05 LOT# 1510001-1 IAW SRM 51-70-05-2R-6 PASDR AALA202301135254Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING-EDGE SLAT #1, SLAT TRACK 2 FORWARD MID BOLT. MAINTENANCE REPLACED BOLT PER AMM 27-84-63.SDR AALA202301138368Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT #3, SLAT TRACK 8 LOWER AFT BOLT. MAINTENANCE REPLACED BOLT PER AMM 27-84-65.SDR AALA202301136927Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT #4, SLAT TRACK 9 FORWARD BOLT. MAINTENANCE REPLACED BOLT PER AMM 27-84-66.SDR AALA202301131427Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT #3, SLAT TRACK 8 LOWER MID BOLT. MAINTENANCE REPLACED BOLT PER AMM 27-84-65.SDR AALA202301132200Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT #3, SLAT TRACK 7 UPPER BOLT. MAINTENANCE REPLACED BOLT PER AMM 27-84-65.SDR AALA202301134218Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT #3, SLAT TRACK 8 UPPER FORWARD BOLT. MAINTENANCE REPLACED BOLT PER AMM 27-84-65.SDR AALA202301130749Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT #2, SLAT TRACK 6 UPPER FORWARD BOLT. MAINTENANCE REPLACED BOLT PER AMM 27-84-64.SDR AALA202301138073Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING-EDGE SLAT #3, SLAT TRACK 7 FORWARD BOLT. MAINTENANCE REPLACED BOLT PER AMM 27-84-65.SDR AALA202301136234Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING-EDGE SLAT #2, SLAT TRACK 5 FORWARD BOLT. MAINTENANCE REPLACED BOLT PER AMM 27-84-64.SDR AALA202301131834Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING SLAT 2 , SLAT TRACK 6 LOWER AFT BOLT. MAINTENANCE REPLACED BOLT PER AMM 27-84-64.SDR DALA2023010408528Skin · dentedSHIP 3308 SLAT #1 L/H DENT WITH SCRATCH DAMAGE LOCATED BELOW STR1 BETWEEN WFX4506 AND WFX4770. CORRECTIVE ACTION: PERMANENT REPAIR ACCOMPLISHED IAW ERA 602677-14. (2557631)SDR DALA2022122908490Slat · dentedSHIP 182 FOUND LHW SLAT NO.5 EDGE DENT, CORRECTIVE ACTION: ACCOMPLISHED REPAIRED THE DENT AREA AS PER SRM 51-70-10 (2555113)SDR FDEA202212263017Wedge · delaminated#2 SLAT T/E WEDGE IS DISBONDED. ACCOMPLISHED PERMANENT REPAIR OF DISBONDED SKIN ON #2 SLAT TE WEDGE UPPER SURFACE IAW FED EX EA F-5750-T0372135, SRM 51-70-10-2R-0, AND 51-70-10-2R, REPAIR 4.SDR FDEA202212263016Wedge · delaminated#10 SLAT T/E WEDGE IS DELAMINATED ACCOMPLISHED PERMANENT REPAIR OF DISBONDED SKIN ON #10 SLAT UPPER SURFACE IN 3 AREAS IAW EA F-5750-TO372141-P1, SRM 51-70-10-2R-0, AND 51-70-10-2R REPAIR 4.SDR FDEA202212263015Wedge · delaminated#5 SLAT T/E WEDGE DISBONDED. REPAIRED #5 SLAT T/E WEDGE IAW FED EX EA F-5750-T0372139-P1- WINGS- FLIGHT SURFACES-#5 SLAT, TRAILING EDGE WEDGE, DELAMINATION AND B757 SRM 51-70-10-2R REPAIR 4 AND SRM 57- 43-01SDR AALA202212290908Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE, CORROSION ON RIGHT WING SLAT TRACK 9 FORWARD BOLT. MAINTENANCE REPLACED BOLT PER AMM 27-84-66.SDR SWAA2023020183321Slat · crackedCRACK LOWER SKIN SLAT 1 ON AUXILIARY TRACK AT LT WING (2 EA) 2022-695543<[01] REPLACED BRACKET LOWER SKIN SLAT 1 ON AUXILIARY TRACK AT LT WING IAW B737-700 SRM 51-40-02 SEE INDIVIDUAL SIGN OFF BELOW.;[02] CORRECTED STEP 1 REPLACED BRACKET LOWER SKIN SLAT 1 ON SDR SWAA2023020183323Slat · crackedCRACK SLAT 2 LOWER SKIN ON AUXILIARY TRACK PLATE AT LT WING 2022-695547<[01] REPLACED PLATE LOWER SKIN ON AUXILIARY TRACK PLATE AT LT WING IAW B737-700 SRM 51-40-02 SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED PLATE LOWER SKIN ON AUXILIARY TRACK PLATE AT LT WISDR SWAA2023011783557Skin · crackedCRACK AROUND THE FASTENER AT NR 3 SLAT LOWER SURFACE REMOVED DAMAGE IAW SRM 57-42-01-2R-8 REPAIR 8 PAR 4.F(1). HFEC INSPECTED CUTOUT AREA IAW NDTM PART 6 51-00-00 PROCEDURE 23 FABRICATED, LOCATED, DRILLED, DEBURRED, APPLIED CHEMICAL CONVERSION COAT, PRIME
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