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 DALA2022111407338Skin · debondedDISBOND WAS FOUND ON LE SLAT 7 TRAILING EDGE WEDGE LOWER SKIN OF 2.0IN LENGTH AND 2.375IN WIDTH AT OSS 305 APPROX. LE SLAT 7 TRAILING EDGE WEDGE LOWER SKIN WAS REPAIRED PER B757-200 SRM.SDR AALA202211227043Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND WING SLAT 3 BOLT OF TRACK 7. REPLACED BOLT PER AMM 27-84-65-400-002-A.SDR AALA202211154050Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK #6 LOWER MID BOLT. MAINTENANCE REPLACED BOLT PER AMM 27-84-64.SDR DALA2022111407345Skin · delaminatedFOUND RT WING NR 10 SLAT UPPER SKIN FROM IB EDGE 01 INCH AND FROM TE 4 INCH DELAMINATION. RT WING NR 10 SLAT UPPER SKIN REPAIRED FROM IB EDGE 01 INCH AND FROM TE 4 INCH IAW SRM 57-43-02-2R-1, SRM 51-70-10- 2R-4, FIG 202, & SRM 51-70-10-2R-0. DEBOND SIZE: LSDR DALA2022111407343Skin · delaminatedTHE L/H WING NO.4 SLAT UPPER SURFACE FOUND DELAMINATION FROM O/B EDGE 13 INCHES UPPER T/E 5.5 INCHES. THE L/H WING NO.4 SLAT UPPER SURFACE FROM O/B EDGE 13 INCHES, UPPER T/E 5.5 INCHES REPAIRED AS PER B767-400 SRM 57-43-02-2R-1 AND SRM 51-70-10-2R-0.SDR DALA2022111407342Skin · dentedSHIP 1805 FOUND DENT ON LH WING #4 SLAT UPPER SURFACE AT 23 INCHES FROM O/B EDGE AND 4 INCHES FROM UPPER EDGE. LH WING #4 SLAT UPPER SURFACE AT 23 INCHED FROM O/B EDGE AND 4 INCHES FROM UPPER EDGE REPAIRED AS PER B767-400 SRM 57-43-02-2R- 1 AND SRM 51-70-10-SDR DALA2022111407334Skin · debondedDISBOND WAS FOUND ON LE SLAT 10 TRAILING EDGE WEDGE UPPER SKIN OF 8.0IN LENGTH AND 8.0IN WIDTH BTW OSS 803-811. CORRECTIVE ACTION: SUMMARY OF NRC 00167: SLAT 10 WAS REPAIRED ON UPPER SKIN BTW OSS 803-811 PER B757-200 SRM.SDR FDEA202211112759Skin · gougedR/H WING SLAT #8 HAS GOUGE DAMAGE REPAIRED USING 767 SRM 51-70-10-2R; EA H-5750-T0371624 CREATED FOR TRACKING ONLYSDR DALA2022111407333Skin · debondedSHIP 659 AD - AA - DISBOND WAS FOUND ON LE SLAT 4 TRAILING EDGE WEDGE LOWER SKIN OF 2.0IN LENGTH AND 0.75IN WIDTH AT OSS 305 APPROX. CORRECTIVE ACTION: SUMMARY OF NRC: 00069 LE SLAT 4 TRAILING EDGE WEDGE LOWER SKIN AT OSS 305 APPROX. WAS REPAIRED PER B757-200 SDR FDEA202211102763Skin · damagedLH WING - OUTBOARD FLAP ASSY LEADING EDGE STRUCTURE IS DAMAGED AT LOCATION ADJACENT TO THE INBOARD SIDE OF THE OUTBOARD FLAP TRACK FAIRING,MWT. REPAIRED BIRD STRIKE DAMAGE TO LH OB FLAP LEADING EDGE PER EA H-5750-T0371632 P1SDR SWAA2022121368338Repair · debondedDEBONDED EXISTING REPAIR ON SLAT 3 OUTBOARD SIDE, LT WING. REPAIRED THE SLAT IAW SRM 57-42-01-2R-4, REPAIR 4, SRM 51-70-10-2R-4, REPAIR 4, AND SRM 51-70-10-2R-0, REPAIR GENERAL.SDR SWAA2022120968339Skin · debondedDEBONDED SLAT 2 UPPER SKIN LOCATED OUTBOARD SIDE AT LT WING 2022-632171 / [01] TOOL USED; CALIPER PN: 500-197-30; SN: A18135078; DUE DATE: 31/AUG/23.;[02] TOOL USED: HOTBONDER P/N: HCS9200B S/N: 15102320 DUE DATE: 16-JAN-23; POSITECTOR P/N: NS2 S/N: 138341 DUESDR IPXA2022110687872Bracket · crackedINSPECTION TYPE:CLT WING KRUEGER FLAP BOX LOWER CHORD SUPPORT STRUCTURE HAS 3 EACH BRACKETS CRACKED.REMOVED,FABRICATED, AND INSTALLED 3 EACH BRACKETS IAW SRM 51-40-21.SDR AALA202211110026Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING SLAT TRACK 4 FORWARD BOLT AT WS 2580. MAINTENANCE REPLACED BOLT PER TASK CARD 26C51057005.SDR FDEA202211032725Wedge · delaminated#6 SLAT T/E WEDGE IS DISBONDED REMOVED AND REPLACED PER B757 AMM 81-01-4SDR FDEA202211032724Wedge · delaminated#4 SLAT T/E WEDGE IS DISBONDED REMOVED AND REPLACED PER B757 AMM 27-81-02-4SDR FDEA202211032723Wedge · delaminated#3 SLAT T/E WEDGE IS DISBONDED REMOVED AND REPLACED PER B757 AMM 27-81-02-4SDR FDEA202211032722Wedge · delaminated#5 SLAT T/E WEDGE IS DISBONDED REMOVED AND REPLACED PER B757 AMM 27-81-01-4SDR AALA202212015694Bracket · corrodedAIRCRAFT IN BASE MAINTENANCE: RIGHT WING ON FRONT SPAR NUMBER 7 SLAT OUTBOARD SEQUENCE TRACK TORSION ROD ATTACH BRACKET CORRODED ON FACE OG T BOLT HOLES. WING STAT 564 AND FRONT SPAR. INSTALLED NUMBER 7 SLAT OUT BOARD SEQUENCE TRACK TORSION ROD ATTACH BRACKET SDR AALA202212018346Bracket · corrodedAIRCRAFT IN BASE MAINTENANCE, RIGHT WING FRONT SPAR NUMBER 6 SLAT OUT BOARD SEQUENCE TRACK TORSION ROD ATTACH BRACKET CORRODED ON FACE OF T BOLT HOLES. INSTALLED TRACK TORSION ROD ATTACH BRACKET ON FRONT SPAR NUMBER 6 SLAT OUTBOARD SEQUENCE TRACK PER SRM 57-1SDR DALA2022110307126None · noneSHIP 5638 DISBONDED AREA OF 9.25IN LENGTH AND 2.0IN WIDTH WAS FOUND ON LOWER SKIN OF SLAT #2 AT OSS 580 APPROX. CORRECTIVE ACTION: SUMMARY OF NRC 00013; DISBONDED AREA AT OSS 580 APPROX OF SLAT #2 WAS REPAIRED PER B757-200 S.R.M. (2479555)SDR IPXA2022110988014Angle · crackedINSPECTION TYPE:SEGLH OB KRUEGER GLAP WEB HAS CRACKANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-21SDR AALA202301138109Skin · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT WING LEADING EDGE SLAT #2 LOWER SKIN HAS WEAR AT SLAT TRACK 6. MAINTENANCE REPAIRED SLAT LOWER SKIN PER EA 341000.SDR SWAA2022110166292Panel · delaminatedLEFT LOWER WING PANEL 521CB IS DELAMINATED AT INBD FWD EDGE / [01] COMPLIED WITH EA 22-157-03231SDR SWAA2022110166293Panel · crackedLEFT LOWER WING PANEL 521ZB IS CRACKED AT FWD OUTBOARD HOLE. / [01] COMPLIED WITH EA 22-157-03232SDR FDEA202210302853Skin · dentedSLAT 7 R/H WING HAS DENT 2" FROM EDGE A=2.3' Y=0.023' A/Y= 100 PERFORMED HOT BOND REPAIR PER SRM 51-70-10, REF SRM 57-43-02-2R,FIG. 201,DETAIL II,NOTE D. REP. DIM.:DIA. 5.5".REP. LOC.: 46" FROM I/B EDGE AND 0.5" FROM T/E OF SLAT #7. REV.137.0 MAJOR RAPSDR IXXA2022112701Skin · crackedSLAT #8 HAS A DENT AND POSSIBLE CRACK LEADING EDGE UPPER EXTERNAL SURFACE INBD END. REF FAS WO FS220060 NON ROUTINE 00518SDR FDEA202210292695Skin · chafedL/H WING NO. 5 LEADING EDGE SLAT LOWER TRAILING EDGE CHAFFED AT APROX OSS 441 M.W.T. REPAIRED #5 SLAT PER EA H-5750-T0371376SDR IPXA2022110287740Skin · corrodedINSPECTION TYPE:C13, CORROSION WAS FOUND ON SKIN (P/N:114T4103-4) OF NO.10 SLAT BETWEEN OSS 684 AND 693.REPAIR I.A.W 767-300F SRM 57-43-01-1A-1, ALLOWABLE DAMAGE 1 REV 84.01SDR DALA2022103107032Slat · not reported(LOG 9706680) DURING INSPECTION FOUND BIRD STRIKE TO #8 SLAT. REMOVED #8 SLAT PER B737 AMM 27-81. INSTALLED #8 SLAT PER W/C 2780-4522-08. #8 SLAT INSTALLED AND ADJUSTED PER W/C 2780-4522-08.SDR UIEA2022100301074Skin · delaminatedLHW O/B FORE FLAP L/E FOUND DELAMINATION AT (46" FROM I/B )(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A</P>)SDR FDEA202210262674Skin · damagedLEFT WING SLAT NO. 5 TRAILING EDGE WITH MISSING MATERIAL. LEFT WING SLAT NO 5 TRAILING EDGE WAS REPAIRED IAW B767 SRM 57-43-02-2R FIG. 201 SHEET 1-2, PAGE 1-2 AND SRM 51-70-10-2R REP. 4, FIG. 202 SHEET 8, PAGE 149, 162, 163 REV. 82 12-15-21SDR IPXA2022110287741Skin · corrodedINSPECTION TYPE:C13CORROSION WAS FOUND ON SKIN(P/N:114T4104-4) OF NO.9 SLAT BETWEEN OSS 670 AND 682.REPAIR I.A.W 767-300F SRM 57-43-01-1A-1, ALLOWABLE DAMAMGE 1 REV 84.01SDR SIMA20221024001Skin · scratchedLH WING , SLAT #3 HAS SCRATCHES NEAR RIB 16 DURING NDT FOUND .5 IN FLAW (MAJOR REPAIR)-C/A-RECV'D ERS-EJ-57MR-1457 FOR PERMANENT REPAIR IE CUT OUT DAMAGE INSTALL PATCHESSDR FDEA202210222642Skin · damagedRIGHT WING #8 SLAT UPPER TRAILING EDGE LOWER SURFACE HAS AREA OF BARE METAL REPAIRED #8 SLAT UPPER TRAILING EDGE LOWER SURFACE ARE OF BARE METAL IAW FEDEX EA# F-5750-T0370952SDR FDEA202210222641Wedge · delaminated#8 SLAT T/E WEDGE IS DISBONDED REPAIRED #8 SLAT T/E WEDGE DISBOND ON 3EA. AREA IAW FEDEX EA# F-5750-T0370952.SDR IXXA202210220001Skin · cracked#3 SLAT LEADING EDGE SKIN CRACKED.SDR SWAA2022112362524Skin · crackedCRACK SLAT ACTUATOR 7 LOWER SKIN SURFACE AT SLAT STATION 322.71 AT RT WING. SLAT 7 WILL BE REPLACED ON TTG8Q00FQX3A.SDR DALA2022102406847Skin · debondedSHIP 6804 AD - AA - DISBONDED AREA OF 2.375IN LENGTH AND 1.25IN WIDTH WAS FOUND ON LOWER SKIN OF SLAT #2 AT OSS 675 APPROX. CORRECTIVE ACTION: SUMMARY OF NRC 00036:LOWER SKIN OF SLAT #2 AT OSS 675 APPROX WAS REPAIRED PER B757-200 S.R.M. (2459691)SDR SWAA2022111461423Skin · crackedRIGHT WING LOWER SURFACE OF THE EDGE SLAT NOSE SKIN TWO CRACKS AROUND FASTENERS HOLES NEXT TO SS 322 ON SLAT NR 7. CRACK MEASURES 0.600 IAW SRM 51-40-02-0G-0. PERFORMED ROTO INSP ON EXISTING HOLES OF RT WING LOWER SURFACE OF THE EDGE SLAT NOSE SKIN AROUND SDR IPXA2022101787179Skin · chafedINSPECTION TYPE:N/ARIGHT WING NO. 8 SLAT TRAILING WEDGE LOWER SKIN CHAFE REPAIRREPAIRED IAW UPS E.O. B767-5750-84540-B ON NRC 684226SDR IXXA2022101601Skin · delaminated# 11 SLAT HAS DELAM ON UPPER WEDGE. TAP TEST BAD.SDR FDEA202210152571Rib · crackedRIGHT HAND WING NUMBER 6 SLAT RIB FOUND CRACKED AT XOS 868.4 DURING INTERNAL BORESCOPE INSPECTION. RIB REMOVED AND FABRICATED PER DOUGLAS DRAWING ARB1828 REVISION B. INSTALLED FABRICATED RIB AT RIGHT HAND WING NUMBER 6 SLAT AT STATION XOS 868.4 AS PER SDR FDEA202210152570Rib · crackedRIGHT HAND WING NUMBER 6 SLAT RIB FOUND CRACKED AT XOS 858.1 DURING INTERNAL BORESCOPE INSPECTION. RIB REMOVED AND FABRICATED PER DRAWING ARB1827 REVISION C. INSTALLED FABRICATED RIB AT RIGHT HAND WING NUMBER 6 SLAT AT STATION XOS 858.1 AS PER SRM 51-35SDR FDEA202210152569Rib · crackedLEFT HAND WING NUMBER 8 SLAT RIB FOUND CRACKED AT XOS 1025.54 DURING S/M WORK. LEFT WING NUMBER 8 SLAT RIB AT STATION XOS 1025.54 CRACKED RIB REMOVED AND REPLACED WITH FABRICATED RIB IAW SRM 51-35-01-OG. RIB FABRICATED IAW DRAWING ARB1925 REVISION B. AND EA 1SDR FDEA202210152568Rib · crackedLEFT HAND WING NUMBER 8 SLAT RIB FOUND CRACKED AT XOS 1010.49 DURING S/M WORK. LEFT HAND WING NUMBER 8 SLAT RIB AT STATION XOS 1010.49 CRACKED RIB REMOVED AND REPLACED WITH FABRICATED RIB AS PER SRM 51-35-01-OG. RIB FABRICATED AS PER DOUGLAS DRAWING ARB1SDR AALA202210178806Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT #5, SLAT TRACK #12 LOWER FORWARD BOLT AT WS 14057 AND RIB 26. REPLACED BOLT PER AMM 27-84-67.SDR SWAA2022111659758Skin · crackedCRACK SLAT 3 LOWER SURFACE OF THE LEADING EDGE SLAT NOSE SKIN AT THE ACTUATOR RIBS AT LT WING 2022-584338 / [01] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC600D; S/N: 190023010;CAL DUE DATE: 14-FEB-23;[02] REMOVED AND REPLACED LEADING EDGE SLAT 3 IAW B737-7SDR SWAA2022101859471Structure · crackedDOT A-24-100 LH I/B FIXED L/E WTB FAIRING SUPPORT STRUCTURE CRACKED AT FASTENER HOLE AT LOWER FWD EDGE OF PANEL 195AL. / [01] HFEC IAW B737 NDT PART 6; 51-00-00 PROC 23. CRACK VERIFIED MARKED IN BLACK. TOOL#31823; DUE 23DEC22;[02] REMOVED CRACKED FAIRING SUPPOSDR IXXA2022101202Skin · delaminated#4 SLAT DELAMINATED
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