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 FDEA202405220716Wedge · wornLH WING, OUTBOARD SLAT 5, TRAILING EDGE WEDGE, LOWER SKIN AT OSS 514.75, PREVIOUS REPAIR WITH WEAR LH WING, OUTBOARD SLAT 5 TRAILING EDGE WEDGE, LOWER SKIN AT OSS 514.75 WAS REPAIRED IAW B767 SRM 57-43-02-2R FIG 201 SHEET 1-2 PAGE 1-2, AND SRM 51-70-10-2RSDR DALA2024052205419Skin · damagedSHIP 1801 FOUND LHW SLAT NO.3 IB INNER SURFACE WORN. CORRECTIVE ACTION: LHW SLAT NO.3 IB INNER SURFACE REPAIRED AS PER B767-400 SRM 57- 43-02-2R-1 & SRM 51-70-10-2R-4. FIG202(SHEET8) & SRM 51-70-10-2R (0351205)SDR DALA2024052205418Skin · damagedSHIP 1818 L/H WING NO.4 SLAT TE LOWER SURFACE FOUND WORN. CORRECTIVE ACTION: L/H WING NO.4 SLAT TE LOWER SURFACE REPAIRED AS PER B767-400 SRM57-43-02-2R-1&SRM51-70-10-2R-4. FIG202(SHEET8) & SRM51-70-10- 2R-0. (0351195)SDR DALA2024052105380Skin · scratchedSCRATCH ON LOWER SKIN, SLAT PANEL #1 LH WS 168.0. SUMMARY OF NRC 00610: SCRATCH ON LOWER SKIN, SLAT PANEL #1 LH WS 168.0 WAS REPAIRED PER ER/A 618009-14 REV ORIG. SECTION I PERMANENT REPAIR AND PER PRI 618009-14 REV 1. ASSOCIATED ER/A 14-618009 ADDED FOR AC 95SDR IXXA20240520001Skin · cracked#3 SLAT LE IN CENTER HAS DAMAGED FASTENER.SDR IPXA2024061321915Skin · crackedFIXED LEADING EDGE BEHIND SLAT #3 IS CRACKED. DOT 142-29 COMPLIED WITH EO: EO-90539-REQ1 AND VTMAE FINAL EA#757-5741-27-A3612 REV.SDR IXXA2024051604Fastener · damaged#3 SLAT LE HAS DAMAGED FASTENER.SDR SWAA2024061885990Skin · crackedCRACK AROUND THE FASTENER AT NO.7 SLAT LOWER SURFACE OF THE L/E SLAT NOSE SKIN AT ACTUATOR RIBS. MARKED<[01] REMOVED DAMAGE AND REPAIRED NO.7 SLAT LOWER SURFACE OF L/E SLAT NOSE SKIN AT ACTUATOR RIBS IAW SRM 57-42-01-2R-8.SDR DALA2024051605287Cover Plate · bentSHIP 3114 SLAT TRACK CLOSING PLATE WING COVER BENT. CORRECTIVE ACTION: INSTALLED NEW SLAT COVER AT SLAT TRACK #5 R/H WING IAW A319 AMM 27-84-69-400-001-A. (5461655)SDR VNAA20240619017Skin · erodedEROSION ON LEADING EDGE AT SLAT 3 OF THE RH WING. LEADING EDGE AT SLAT 3 OF THE RH WING WAS REPAIRED PER REO 690-57-42-1066 REV. --SDR SWIA20240715513Slat Track · corrodedRIGHT WING SLAT TRACK ASSY NUMBER 1, TRACK ASSY 1-2 HAS EVIDENCE OF CORROSION AS MARKED (C-CHECK RO 7/17/2024) REPAIRED RH WING SLAT TRACK 1-2 PER REO 670-57-42-1559 REV-A, DATED 2024-07-03. RIG CHECK GOOD. CLEARANCE CHECK GOOD. COMPLIED WITH TASK CARD SDR SWIA20240512Slat Track · gougedLEFT WING SLAT TRACK 1-1 SLAT TRACK SIDE GOUGED AS MARKED (C-CHECK RO 7/17/2024) REPAIRED LEFT WING SLAT TRACK 1-1 SLAT TRACK PER REO 670-57-42-1556 REV -- DATED 2024-05-30. RIG CHECK GOOD. CLEARANCE CHECK GOOD. COMPLIED WITH SKY WEST TC 51-900-1002-SKYSDR DALA2024051405208Slat Track · corrodedLH SLAT TRACK NBR 4 LOWER AFT SURFACE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. MEASURED WEAR LH SLAT TRACK NBR 4 LOWER AFT SURFACE IAW ER/A 608983-14AD REV D AND PRI 60898SDR DALA2024051405207Slat Track · corrodedLH SLAT TRACK NBR 5 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED LH SLAT TRACK NBR 5 UPPER AFT SURFACE IAW ER/A 608983- 14AD REV D AND PRI 6089SDR DALA2024051405206Slat Track · corrodedLH SLAT TRACK NBR 4 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED LH SLAT TRACK NBR 4 UPPER FWD SURFACE IAW ERA 608983- 14AD REV D AND PRI 60898SDR DALA2024051405205Slat Track · corrodedLH SLAT TRACK NBR 4 RACK TEETH (2 EA) HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED LH SLAT TRACK NBR 4 RACK TEETH IAW ER/A 608983-14AD REV D AND PRI 608983-14AD SDR DALA2024051405204Slat Track · corrodedLH SLAT TRACK NBR 4 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED LH SLAT TRACK NBR 4 UPPER AFT SURFACE IAW ERA 608983- 14AD REV D AND PRI 60898SDR AALA202405148929Skin · crackedAIRCRAFT IN BASE MAINTENANCE: NUMBER 4 SLAT NOSE AND WEDGE SKIN HAS EXPOSED COMPOSITE AND MUD CRACKING. ACCOMPLISHED PERMANENT REPAIR ON NUMBER 4 SLAT NOSE AND WEDGE. PER 787-8 AMM DMC B787-A-57-00-00-02A-257A-A.SDR DALA2024051405203Pinion Gear · corrodedLH SLAT TRACK NBR 4 PINION TEETH (2 EA) HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED LH SLAT TRACK NBR 4 PINION TEETH IAW ERA 608983-14AD REV D AND PRI 608983-14SDR DALA2024051405202Slat Track · corrodedRH SLAT TRACK NBR 5 UPPER AFT HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF 5742-01028-028. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED RH SLAT TRACK NBR 5 UPPER AFT SURFACE IAW ER/A608979- 14AD REV C AND PRI 608979-14AD RSDR DALA2024051405201Slat Track · corrodedRH SLAT TRACK NBR 6 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED RH SLAT TRACK NBR 6 UPPER AFT SURFACE IAW ER/A 608979- 14AD REV C AND PRI 6089SDR FDEA202405090620Rib · crackedLEFT WING - NUMBER 6 SLAT LOWER SURFACE INNER RIB AT STATION XOS 837.572 FOUND CRACK ABOUT 0.2 INCHES. LEFT WING NUMBER 6 SLAT LOWER SURFACE INNER CRACKED RIB AT STATION XOS 837.572 REPAIR CARRIED OUT AS PER EA 1-5750-T0379098 PART 1. TITLE: WINGS-FLIGHT SSDR FDEA202405090619Rib · crackedLEFT WING - NUMBER 6 SLAT LOWER SURFACE INNER RIB AT STATION XOS 842.722 FOUND CRACK ABOUT 0.3 INCHES. LEFT WING NUMBER 6 SLAT LOWER SURFACE INNER CRACKED RIB AT STATION XOS 842.722 REPAIR CARRIED OUT AS PER EA 1-5750-T0379098 PART 1. TITLE: WINGS-FLIGHT SSDR FDEA202405090618Rib · crackedLEFT WING - NUMBER 6 SLAT LOWER SURFACE INNER RIB AT STATION XOS 863.325 FOUND CRACK ABOUT 0.3 INCHES. LEFT WING NUMBER 6 SLAT LOWER SURFACE INNER CRACKED RIB AT STATION XOS 863.325 REPAIR CARRIED OUT AS PER EA 1-5750-T0379098 PART 1. TITLE: WINGS-FLIGHT SSDR FDEA202405090617Rib · crackedLEFT WING - NUMBER 6 SLAT LOWER SURFACE INNER RIB AT STATION XOS 811.623 FOUND CRACK ABOUT 0.4 INCHES. LEFT WING NUMBER 6 SLAT LOWER SURFACE INNER CRACKED RIB AT STATION XOS 811.623 REPAIR CARRIED OUT AS PER EA 1-5750-T0379098 PART 1. TITLE: WINGS-FLIGHT SSDR DALA2024051305157Wedge · debondedSHIP 676 #3 SLAT UPPER T/E WEDGE IS DISBONDED IN 2 AREAS ON 2ND REPAIR FROM OUTBD END + IN BETWEEN 1ST + 2ND REPAIR FROM OUTBD END OF SLAT. CORRECTIVE ACITON: REMOVED #3 SLAT PER AMDS W/C 2781-4380-03 AND ROUTED TO SHOP FOR REPAIR. REPAIRED PER B757 SRM 57-43-SDR FDEA202405060592Rib · crackedLEFT WING - NUMBER 6 SLAT LOWER SURFACE INNER RIB AT STATION XOS 816.823 FOUND CRACK ABOUT 0.4 INCHES. LEFT WING NUMBER 6 SLAT LOWER SURFACE INNER CRACKED RIB AT STATION XOS 816.823 REPAIR CARRIED OUT AS PER EA 1-5750-T0379098 PART 1. TITLE: WINGS-FLIGHT SSDR SWAA2024053182339Wedge · delaminated#8 SLAT WEDGE UPPER O/B CORNER IS DELAMINATED.<[01] ACCOMPLISHED DAMAGE REMOVAL IAW SRM 51-70-10-2R-0; AND SRM 51-70-10-2R-4 REPAIR #4. OK TO INSTALL REPAIR PLIES.;[02] 02 - INSPECTED PER SRM 51-70-10-2R-0;[03] APPLIED REPAIR IAW SRM 51-70-10-2R-0; AND SRM 51-SDR SWAA2024052982549Skin · crackedCRACK LEADING EDGE SKIN SLAT 2 LOWER SURFACE AT LT WING 2024-286837<[01] ON STEP 3. TOOL USED: ET INSTRUMENT. P/N: NORTEC 600D. S/N: 210136503. DUE DATE: 23-MAY-24.;[02] EQUIPMENT USED P/N: NORTEC 600D; S/N: 220272512; DUE DATE: 08-JAN-25;[03] PERFORMRD REPAIRSDR SWAA2024050682378Skin · delaminated#8 SLAT REQUIRES REMOVAL DUE TO DELAMINATION<[01] REMOVED #8 LEADING EDGE SLAT IAW AMM 27-81-21.;[02] ACCOMPLISHED BORESCOPE INSPECTION OF #8 INBD SLAT CAN. OK TO INSTALL #8 SLAT;[03] REMOVED AND REPLACED #8 WING SLAT IAW AMM 27-81-21.;[04] C/W INSPECTION;[05]SDR AALA202405070757Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON SLAT TRACK 5 FORWARD BOLT ON RIGHT-HAND WING. REPLACED BOLT PER AMM 27-84-64-400-002-A.SDR AALA202405072994Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON SLAT TRACK 5 UPPER BOLT ON RIGHT-HAND WING. REPLACED BOLT PER AMM 27-84-64-400-002-A.SDR AALA202405061365Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK #9 FORWARD BOLT AT WS 10204 AND RIB 19. REPLACED BOLT PER TASK CARD 26C51057005.SDR DALA2024050304919Skin · dentedAIRCRAFT 1020, DURING WALK AROUND, FOUND RIGHT WING I/B SLAT DENTED ON L/E. CORRECTIVE ACTION: FABRICATED 2 (EA) INTERNAL DOUBLER AND 1 EX EXTERNAL FILLER. ALODINED AND PRIMED AREAS THAT REQUIRED. INSTALLED PERMANENT REPAIR IAW A321 SRM 57-40-00-300-076. (LP 0SDR DALA2024050104851Skin · debondedSHIP 6700 AD - 01 DISBOND WAS FOUND ON UPPER SKIN AT TRAILING EDGE WEDGE OF LE SLAT 6 OF 12.1IN LENGTH AND 1.2IN WIDTH AT WS 200. IN REFERENCE TO JOB 059-0001. CARD. CORRECTIVE ACTION: SUMMARY OF NRC 00089: TRAILING EDGE WEDGE OF LE SLAT 6 WAS REPAIRED PER B75SDR R61A2024050600197Support Plate · crackedRH WING SLAT #1, NUMBER 2 RAIL I/B SUPPORT PLATE CRACKED. RH WING, SLAT #1, NUMBER 2 RAIL I/B SUPPORT PLATE WAS REPLACED WITH LOCAL MAN / MADE REPAIR PART IAW DWG 170-36422-401 AND SRM 51-42-01.SDR DALA2024050104853Skin · debondedSHIP 6700 AD - 01 DISBOND WAS FOUND ON UPPER SKIN AT TRAILING EDGE WEDGE OF LE SLAT 4 OF 2.3IN LENGTH AND 1.1IN WIDTH AT WS 340. IN REFERENCE TO JOB 057-0001. CARD 5740-01145-05D. CORRECTIVE ACTION: SUMMARY OF NRC 00088: UPPER SKIN AT TRAILING EDGE WEDGE OF LESDR AALA202405076986Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON BOLT ATTACHMENT SLAT TRACK 2 (MID FORWARD BOLT) ON LEFT-HAND WING. REPLACED BOLT PER JOB CARD 26C51057005.SDR AALA202404309312Skin · crackedAIRCRAFT IN BASE MAINTENANCE: RIGHT WING NUMBER 9 SLAT UPPER SURFACE CRACKED. ACCOMPLISHED REPAIR. PER SRM 57-41-01.SDR SWAA2024061780048Skin · crackedCRACK LEADING EDGE SKIN SLAT 4 LOWER SURFACE AT LT WING. PERFORMED REPAIR ON LEADING EDGE SKIN SLAT 4 LOWER SURFACE AT LT WING IAW B737-700 SRM 57-42-01-2R-8 REPAIR 8.SDR SWAA2024061780049Skin · crackedCRACK LEADING EDGE SKIN SLAT 5 LOWER SURFACE AT RT WING. PERFORMED REPAIR ON LEADING EDGE SKIN SLAT 5 LOWER SURFACE AT RT WING IAW SRM 57-42-01-2R-8 REPAIR 8.SDR AALA202404306890Skin · crackedAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND WING FLAPERON LEADING EDGE HAS CRACK AT MID SECTION APPROXIMATELY 2" LONG. ACCOMPLISHED A PERMANENT REPAIR ON RIGHT HAND WING FLAPERON LEADING EDGE. PER B777-200SRM 57-65-01-2R-1 TABLE 203.SDR UIEA2024042400310Skin · delaminatedLH WING, SLAT #4 SURFACE INNERSIDE AREA UPPER INSIDE CORNER WITH DELAMINATION.(<P>DELAMINATIONS (2 EA) ON LH WING SLAT #4 T/E WEDGE WERE REPAIRED PER SRM 57-43-02-2R-1. NO FURTHER DEFECTS NOTED. </P>)SDR UIEA2024042400311Skin · delaminatedDELAMINATED UPPER CORNER OF SLAT 9 AT RH WING(<P>DELAMINATION ON RH WING SLAT# 9 T/E WEDGE UPPER SKIN INBD CORNER WAS REPAIRED PER SRM 57-43-02-2R-1. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024042400312Skin · delaminatedDELAMINATED UPPER CORNER (UPPER SURFACE) OF SLAT 12 AT RH WING(<P>DELAMINATION ON RH WING SLAT #12 T/E WEDGE UPPER SURFACE WAS REPAIRED PER SRM 57-43-02-2R-1. NO FURTHER DEFECTS NOTED.</P>)SDR DALA2024042904778Wedge · damagedSHIP 666 AD2017-22-12WORK CRD 5740-01145-05E DURING SLAT WEDGE INSP. FOUND NBR 5 SLAT TOP OUTBOARD CORNER FAILED TAP TEST. CORRECTIVE ACTION: -APPLIED SPEED TAPE PER B757 SRM 57-43-02-1A-1 FIGURE 101 PG3 BLOCK G. CAT D TOPP 40-60-05 SECONDARY STRUCTURE WITHIN SDR SWAA2024051679747Skin · delaminated#1 SLAT HAS AREA ON DELAMINATION ON O/B LOWER SURFACE.<[01] REMOVED #1 SLAT PER MM 27-81-21.;[02] REPLACED #1 SLAT PER AMM 27-81-21;[03] OK TO INSTALL #1 SLAT (RII);[04] INSPECTED WORK ACCOMPLISHED IN C/A #3 (RII);[05] (RII) INSPECTION C/W REPLACED #1 SLAT PERSDR SWIA2024051500426Skin · scratchedRH WING #3 SLAT INBOARD END UPPER SKIN HAS TWO SCRATCHES. (C-CHECK RO 5/14/2024) DAMAGE ACCEPTED AS PERMANENTLY ALLOOWABLE WITH NO ADDITIONAL REPAIR REQUIRED PER ETD2024-170-012219 THE REWORKED AREAS MUST BE DETAILED VISUAL INSPECTED EVERY 24 MONTHS FOR CSDR GTIA2024042938100Skin · scratchedREF SPIRIT W/O 293812 T/C ZL-500-03-1-L-NKS. SCRATCH LEADING EDGE SKIN SLAT 1 ON L/H WING. SEVEN SCRATCHES MEASURING LENGTH 5.017 IN DEPTH 0.002 IN, LENGTH 6.141 IN DEPTH 0.003 IN, LEGTH 7.663 IN DEPTH 0.005 IN, LENGTH 22.017 IN DEPTH 0.005 IN, LENGTH 3.462 SDR AALA202407102060Skin Panel · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT WING LEADING EDGE #1 SLAT UPPER SURFACE BOTTOM SKIN WORN AT SLAT TRACK #2. REPAIRED SLAT SKIN PER EA 355439
Back to JASC 5754