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 DALA2023030701692None · noneLH WING: SLAT TRACK #4 HAS CORROSION ON UPPER AND LOWER SURFACES . NO EVIDENCE OF PREVIOUS RE-WORK. AA# 5742-01028. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 056-0001:5742-01028-02A/005 00029 CLEANED AND REPAIRED CORSDR DALA2023030701691None · noneLH WING: SLAT TRACK #1 HAS CORROSION ON UPPER AND LOWER SURFACES . NO EVIDENCE OF PREVIOUS RE-WORK. AA# 5742-01028. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 056-0001:5742-01028-02A/002 00026 CLEANED AND REPAIRED CORSDR DALA2023030701690None · noneLH WING: SLAT TRACK #2 HAS CORROSION ON UPPER AND LOWER SURFACES . NO EVIDENCE OF PREVIOUS RE-WORK. AA# 5742-01028. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 056-0001:5742-01028-02A/003 00027 CLEANED AND REPAIRED CORSDR DALA2023030701689None · noneLH WING: SLAT TRACK #3 HAS CORROSION ON UPPER AND LOWER SURFACES . NO EVIDENCE OF PREVIOUS RE-WORK. AA# 5742-01028. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 056-0001:5742-01028-02A/004 00028 CLEANED AND REPAIRED CORSDR DALA2023030701688None · noneLH WING: SLAT TRACK #8 HAS CORROSION ON UPPER AND LOWER SURFACES . NO EVIDENCE OF PREVIOUS RE-WORK. AA# 5742-01028. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 056-0001:5742-01028-02A/009 00033 CLEANED AND REPAIRED CORSDR DALA2023030701687None · noneLH WING: SLAT TRACK #10 HAS CORROSION ON UPPER AND LOWER SURFACES. NO EVIDENCE OF PREVIOUS RE-WORK. AA# 5742-01028. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 056-0001:5742-01028-02A/011 00035 CLEANED AND REPAIRED CORSDR DALA2023030701686None · noneLH WING: SLAT TRACK #11 HAS CORROSION ON UPPER AND LOWER SURFACES. NO EVIDENCE OF PREVIOUS RE-WORK. AA# 5742-01028. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 056-0001:5742-01028-02A/012 00036 CLEANED AND REPAIRED CORSDR SWAA2023041211693Panel · delaminatedLEFT WING LOWER LEADING EDGE PANEL #521GB; CORNER EDGE DELAMINATED (DOT 223-LW521GB).<[01] MEASUREMENTS;[02] COMPLIED WITH MEASUREMENTS OF DAMAGESDR SWAA2023041211692Panel · delaminatedLEFT WING LOWER LEADING EDGE PANEL #521PB; CORNER EDGE DELAMINATED (DOT 223-LW521PB).<[01] PREPARED DAMAGED AREA FOR REPAIR ON LEFT WING LOWER LEADING EDGE PANEL#521PB PER B737 SRM 51-70-04-2R-13;[02] MEASUREMENTS;[03] REPAIRED DAMAGED AREA ON LEFT WING LOWER SDR SWAA2023041211515Slat System · crackedLOWER SKIN OF #7 SLAT APPEARS TO BE CRACKED AT FASTENER HOLE SS 322.26. 8-17<[01] FABRICATED AND INSTALLED DOUBLER AND FILLER AT LEADING EDGE SLAT #7 NOSE SKIN EXTERNAL SS 322.26 MATERIAL USED 7075T6.071 AND 7075T6.063 IN AS PER B 737-700 SRM 57-42-01-2R-8 FIGSDR SWAA2023032411458Slat · crackedCRACK ON EXTERNAL SKIN LEADING EDGE LOCATED SLAT 6 ON SLAT STATION 202.45 AT RT WING 2023-164956<[01] EDDY CURRENT EQUIPMENT USED P/N: NORTEC 600D; S/N: 200053402 AND DUE DATE: 13-MAY-23.;[02] REMOVED AND REPLACED L/E SLAT 6 RT WING IAW B737-700 AMM 27-81-21-0SDR IXXA2023030101Fitting · crackedCRACKED RW LE FITTINGSDR DALA2023022701470None · noneSHIP 3327 DURING H CHECK, A PERMANENT REPAIR WAS MEANT TO BE ACCOMPLISHED IN TRACKED DAMAGES (2 DENTS) AFFECTING THE LEADING-EDGE SKIN BETWEEN FSX865-FSX1062.6 AND FSX3714-FSX3978, SLAT #1, LH WING. REFER TO FIGURE 1 FOR FURTHER DETAILS. AS PER LP 8584973, THESDR DALA2023022701455None · noneSHIP 1808 FOUND DELAMINATION ON RH WING NO.11 SLAT UPPER SURFACE AT O/B T/E AREA. CORRECTIVE ACTION: REPAIRED DELAMINATION ON RH WING NO.11 SLAT UPPER SURFACE AT O/B T/E AREA AS PER B767-400 SRM 57-43-02-2R-1 AND SRM 51-70 (2642789)SDR A6WA202302238519Hinge Arm · gougedRH INBD FLAP HINGE ARM ASSY. AT WS 80.50 IS GOUGED ON LOWER MOUNT LUGS. *****AIRCRAFT REMOVED FROM SERVICE*********** REPAIRED RH IB FLAP HINGE ARM ASSY IAW MHIRJ REO 601R-57-54-358 REV -- DATED 2023-03-08SDR SWAA2023040505767Slat · crackedCRACK LOWER SURFACE SLAT 8 EXTERNAL SKIN AT LEVEL SLAT STATION 451.97 RT WING 2023-142481<[01] TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC 600D; SN:210138103; DUE DATE: 11-APR-23;[02] TOOL USED PN NORTEC 600D SN 220272712 DUE DATE 17-DEC-23;[03] EDDY CURRENT ESDR DALA2023022301356None · noneSHIP 5635 A.A. - A.D. DISBOND 3.000IN LENGTH X 2.000IN WIDTH AT OSS306 LOWER SURFACE, LE SLAT 7, TRAILING EDGE WEDGE, RH WING. CORRECTIVE ACTION: SUMMARY OF NRC 00044: AREA ON OSS 306 LOWER SURFACE LE SLAT 7 OF TRAILING EDGE WEDGE (RH WING) WAS REPAIRED PER B7SDR DALA2023022201334None · noneSHIP 5635 A.A. - A.D. DISBOND 2.100IN LENGTH X 0.900IN WIDTH AT OSS307 UPPER SURFACE, LE SLAT 7, TRAILING EDGE WEDGE, RH WING. CORRECTIVE ACTION: SUMMARY OF NRC 00042: AREA ON OSS307 UPPER SURFACE, LE SLAT 7 OF TRAILING EDGE WEDGE (RH WING) WAS REPAIRED PER B7SDR SWAA2023021603648Panel · crackedRT WING PANEL #621PB HAS HAS A 2' CRACK EMANATING FROM THE FWD I/B FASTENER HOLE.<[01] REMOVED AND REPLACED PNL 621PB REF SRM 51-40-02SDR DALA2023021701240None · noneSHIP 5635 A.A. - A.D.TWO DISBONDED AREAS: 1) 1.500IN LENGTH X 1.000IN WIDTH AT ISS171 UPPER SURFACE AND 2) 1.000IN LENGTH X 1.000IN WIDTH AT ISS188 UPPER SURFACE, LE SLAT 6, TRAILING EDGE WEDGE, RH WING. CORRECTIVE ACTION: SUMMARY OF NRC 00029: THE SLAT PANEL SDR DALA2023021701239None · noneSHIP 5635 A.A. - A.D. DISBOND 1.500IN LENGTH X 1.000IN WIDTH AT ISS156 UPPER SURFACE, LE SLAT 6, TRAILING EDGE WEDGE, RH WING. CORRECTIVE ACTION: SUMMARY OF NRC 00028: THE SLAT PANEL NO.6 WAS REPLACED BY SERVICIABLE SLAT PANEL REFER TO AMDS 2781-4128-02 FOR INSDR DALA2023021601217None · noneSHIP 5635 A.A. - A.D. DISBOND 1.500IN LENGTH X 1.100IN WIDTH AT ISS217 UPPER SURFACE, LE SLAT 5 TRAILING EDGE WEDGE. LH WING. CORRECTIVE ACTION: SUMMARY OF NRC 00025: DISBOND AT ISS217 UPPER SURFACE, LE SLAT 5 TRAILING EDGE WEDGE. LH WING WAS REPAIRED PER B-75SDR DALA2023021601216None · noneSHIP 5635 A.A. - A.D. DISBOND 1.500IN LENGTH X 1.200IN WIDTH AT OSS481 UPPER SURFACE, LE SLAT 8, TRAILING EDGE WEDGE, RH WING. CORRECTIVE ACTION: SUMMARY OF NRC 00046: AREA ON OSS481 UPPER SURFACE, LE SLAT 8, TRAILING EDGE WEDGE, RH WING WAS REPAIRED PER B757-SDR DALA2023021601215None · noneSHIP 5635 A.A. - A.D. DISBOND 2.200IN LENGTH X 1.100IN WIDTH AT OSS795 UPPER SURFACE, LE SLAT 10, TRAILING EDGE WEDGE, RH WING. CORRECTIVE ACTION: SUMMARY OF NRC 00049: DISBOND AT OSS795 UPPER SURFACE, LE SLAT 10, TRAILING EDGE WEDGE, RH WING. WAS REPAIRED PERSDR DALA2023021601214None · noneSHIP 5635 A.A. - A.D. DISBOND 1.500IN LENGTH X 1.500IN WIDTH AT ISS195 UPPER SURFACE, LE SLAT 5 TRAILING EDGE WEDGE. LH WING. CORRECTIVE ACTION: SUMMARY OF NRC 00026: DISBOND AT ISS195 UPPER SURFACE, LE SLAT 5 TRAILING EDGE WEDGE. LH WING WAS REPAIRED PER B-75SDR DALA2023021601213None · noneSHIP 5635 A.A. - A.D. DISBOND 1.600IN LENGTH X 1.200IN WIDTH AT OSS673 UPPER SURFACE, LE SLAT 9, TRAILING EDGE WEDGE, RH WING. CORRECTIVE ACTION: SUMMARY OF NRC 00048: DISBOND AT OSS673 UPPER SURFACE, LE SLAT 9, TRAILING EDGE WEDGE, RH WING WAS REPAIRED PER B7SDR DALA2023021601212None · noneSHIP 5635 A.A. - A.D. DISBOND 4.500IN LENGTH X 3.000IN WIDTH ON PREVIOUS REPAIR AT OSS439 UPPER SURFACE, LE SLAT 8, TRAILING EDGE WEDGE, RH WING. CORRECTIVE ACTION: SUMMARY OF NRC 00045: DISBOND ON PREVIOUS REPAIR AT OSS439 UPPER SURFACE, LE SLAT 8, TRAILING ESDR DALA2023021401169None · noneSHIP 5635 A.A. - A.D. DISBOND 2.800IN LENGTH X 1.500IN WIDTH AT OSS740 UPPER SURFACE, LE SLAT 1 TRAILING EDGE WEDGE. LH WING. CORRECTIVE ACTION: SUMMARY OF NRC 00021: DISBOND AT OSS740 UPPER SURFACE, LE SLAT 1 TRAILING EDGE WEDGE. LH WING WAS REPAIRED PER B757SDR DALA2023021401168None · noneSHIP 5635 A.A. - A.D. DISBOND 1.600IN LENGTH X 1.100IN WIDTH AT OSS731 UPPER SURFACE, LE SLAT 10, TRAILING EDGE WEDGE, RH WING. CORRECTIVE ACTION: SUMMARY OF NRC 00050: DISBOND AT OSS731 UPPER SURFACE, LE SLAT 10, TRAILING EDGE WEDGE, RH WING. WAS REPAIRED PERSDR DALA2023021401167None · noneSHIP 5635 A.A. - A.D. DISBOND 1.200IN LENGTH X 1.200IN WIDTH AT OSS355 UPPER SURFACE, LE SLAT 4 TRAILING EDGE WEDGE. LH WING. CORRECTIVE ACITON: SUMMARY OF NRC 00024: DISBOND AT OSS355 UPPER SURFACE, LE SLAT 4 TRAILING EDGE WEDGE. LH WING. WAS REPAIRED PER B75SDR SWAA2023032001651Panel · crackedCRACK ACCESS PANEL 623GB LOCATED SLAT 6 AT RT WING 2023-106320<[01] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-24; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-24.;[02] TOOL USED: POSDR SWAA2023030600174Fitting · crackedSLAT #5 LOWER L/E SKIN HAS CRACK INDICATION AT ACTUATOR FITTING FASTENER. (MARKED)<[01] ACCOMPLISHED HFEC SURFACE SCAN IAW 737 NDTM PART 6 CHAPTER 51-00-00 PROCEDURE 23. <BR>CRACK NOTED AROUND FASTENER HOLE ON LOWER SKIN; DIMENSIONS 0.1' X 0.1'<BR><BR>ACCOMPLISDR DALA2023020700915Not Reported · not reportedSHIP 1200 FOUND RH WING NO.10 SLAT UPPER NOSE SKIN FROM INBOARD SIDE 40 IHCH 01EA FASTENER AROUND CUTOUT CRACK. CORRECTIVE ACTION: CARRIED OUT THE REPAIR AT RHW NO.10 SLAT UPR NOSE SKIN FROM I/B SIDE 40'' AREA AS PER B767-300 SRM 57-43 (2612329)SDR AALA202302210432Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK 2 MID AFT BOLT BETWEEN WS 1406 AND WS 1957, BETWEEN RIBS 3 AND 4.. MAINTENANCE REPLACED BOLT PER AMM 27-84-63.SDR IPXA2023021190885Angle · crackedINSPECTION TYPE:C1R/H WING FIXED L/E LOWER ANGLE LOCATED AT STA 832.421 IS CRACKED.REMOVED, FABRICATED AND REPLACED CRACKED ANGLE ON THE R/H WING FIXED L/E AT STA 832.421 IAW SRM 51-31-01. (MINOR)SDR SWAA2023032097614Skin · crackedCRACK EXTERNAL SKIN SLAT 8 AROUND THE FASTENERS THAT ATTACH THE ACTUATOR FITTING AT SLAT STATION 451.97 AT RT WING 2023-105954<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR P/N: NORTEC 600D; S/N210138203; DUE DATE: 11-APR-23;[02] EVALUATED SLAT 8 OUT LIMITS; CRACSDR IPXA2023021390955Web · crackedINSPECTION TYPE:2CL/H WING DROOPED L/E HAS A CRACKED WEB.REMOVED, FABRICATED, REPLACED CRACKED WEB ON THE L/H WING DROOPED L/E IAW SRM 51-35-02 AND 51-31-01 (MINOR)SDR SWAA2023030297147Skin · cracked#7 LEADING EDGE SLAT LOWER SKIN AT ACTUATOR ATTACH POINTS HAVE CRACKED SKIN BELOW RIVET.<[01] ACCOMPLISHED HFEC SURFACE SCAN IAW 737 NDTM PART 6 CHAPTER 51-00-00 PROCEDURE 23.<BR>2EA CRACKS NOTED AROUND RIVET HOLE; DIMENSIONS OF CRACKS 0.2' X 0.1' AND 0.1' X 0SDR UIEA2023012400079Skin · delaminatedLHW I/B MID FLAP I/B L/E FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A</P>)SDR AALA202302132862Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE #4 SLAT, #9 SLAT TRACK FORWARD BOLT. MAINTENANCE REPLACED BOLT PER AMM 27-84-66.SDR AALA202302073289Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING #1 LEADING EDGE SLAT TRACK #4 FORWARD BOLT AT WS 3059 AND RIB 6. MAINTENANCE REPLACED BOLT PER AMM 27-84-63.SDR AALA202302213136Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT #4, SLAT TRACK 9 LOWER BOLT BETWEEN WS 10204 AND WS 10729, BETWEEN RIBS 19 AND 20. MAINTENANCE REPLACED BOLT PER AMM 27-84-66.SDR VNAA202301280002Slat Track · corrodedCORROSION ON SLAT TRACKS UPPER/LOWER,1-2 AND 2-2 AT LH WING. TRACK 2 OF SLAT 2 WAS MEASUREMENT AND WAS FOUND WITHIN LIMITS PER REO 690-57-42-950 REV-. TRACK 2 OF SLAT 1 WAS REPLACED PER CRJ-900 AMM27-81-41-000-802-A01 AND AMM 27-81-41-400-802-A01SDR AALA202302218231Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK 8 FORWARD LOWER BOLT BETWEEN WS 8744 AND WS 9235, BETWEEN RIBS 16 AND 17. MAINTENANCE REPLACED BOLT PER AMM 27-84-65.SDR SWAA2023012695500Skin · debonded#8 SLAT T/E #8 SLAT T/E REPAIR DISBOND AND MISSING. REPAIRED #8 SLAT TE PERMANENT REPAIR PER SRM 57-42-01-2R-6.SDR AALA202301310470Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE #11 SLAT TRACK UPPER BOLT. MAINTENANCE REPLACED BOLT PER AMM 27-84-67.SDR CALA2023012500196Wedge · damaged(B757-06-3-0306) #3 SLAT WEDGE T/E PREVIOUS REPAIR SEPARATED 31" FROM INBD EDGE. TRANSCRIBED FROM HAECO NR 9282457. REPAIRED #3 SLAT WEDGE T/E IAW B757 SRM 57-43-02-2R-1, SRM 51-70 -10-2R-0 AND AMM 51-21-001/701. REMOVED HAECO DOT. TRANSCRIBED F ROM HAECO NR 9SDR FDEA202301230158Skin · dentedSLAT 5 WITH DENT AT UPPER SKIN, TRAILING EDGE WEDGE. LH WING SLAT #5 TRAILING EDGE WEDGE WAS REPAIRED IAW B767 SRM 57-43-02-2R PAG. 1-2 FIG. 201 AND B767 SRM 51-70-10-2R FIG. 201 REV. 85 15-DEC-22SDR FDEA2023012320155Skin · wornRH WING, OUTBOARD SLAT (8), TRAILING EDGE, LOWER SURFACE WITH WEAR (TWO POINTS) RH WING, OUTBOARD SLAT 8 TRAILING EDGE, LOWER SURFACE WAS REPAIRED IAW SRM 57-43- 02-2R PAG. 1-2 FIG. 201, AND SRM 51-70-10-2R FIG. 201 REV. 85 15-DEC-22SDR AALA202301316248Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE #5 SLAT TRACK LOWER BOLT. MAINTENANCE REPLACED BOLT PER AMM 27-84-64.
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