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 DALA2024011800775Slat Track · corrodedRH SLAT TRACK #2 LWR AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF. AA5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. C/W PRI ERA 607388-14AD STEP 3. [1832863]. C/W PRI ERA 607388- 14AD STEP 9. [5333]. CORROSION BLEND MSDR DALA2024011800773Roller · wornRH OUTBOARD LWR SIDE OF SLAT TRACK #4 HAS EVIDENCE OF ROLLER WEAR AND PREVIOUS REWORK REF AA5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FLIGHT. WEAR MARKS MEETS PRI STEP 9 CRITERIA. NO FURTHER REWORK REQUIRED. (LP# 0151210)SDR DALA2024011800772Slat Track · corrodedRH SLAT TRACK #5 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA 5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. C/W PRI ERA 607388-14AD STEP 9. [5333]. CORROSION BLEND MEETS PRI STEP 8. CRITERIA. NO FURTHER REWOSDR DALA2024011800771Slat Track · corrodedRH SLAT TRACK #10 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF. AA5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. C/W PRI ERA 607388-14AD STEP 3. [1832863]. C/W PRI ERA 607388- 14AD STEP 9. [5333]. CORROSION BLENSDR DALA2024011800769Slat Track · corrodedRH SLAT TRACK #9 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA 5742-01028-02B LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. C/W PRI ERA 607388-14AD STEP 3. [1832863]. C/W PRI ERA 607388- 14AD STEP 9. [5333]. CORROSION BLEND SDR DALA2024011800768Slat Track · corrodedL/H SLAT TRACK NBR 4 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. C/W PRI ER/A 607387-14AD STEP 9 [QC 5333] CORROSION BLEND MEETS CRITERIA NO FURTHER SDR DALA2024011800767Slat Track · corrodedRH SLAT TRACK #9 LWR AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. C/W PRI ERA 607388-14AD STEP 3. [1832863]. C/W PRI ERA. 607388- 14AD STEP 9. [5333]. CORROSION BLEND MSDR DALA2024011800766Slat Track · unknownL/H SLAT TRACK NBR 5 LOWER AFT HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA5742-01028-02A. LIAISON ENGINEERING WILL BE REQUIRED BEFORE FURTHER FLIGHT. C/W PRI ER/A 607387-14AD STEP 9[QC 5333] CORROSION BLEND MEETS PRI STEP 8 CRITERIA NO FURTHER REWORK SDR DALA2024011600673Slat Track · unknownLH SLAT TRACK #2 LWR AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. C/W PRI ERA 607388-14AD STEP 9. [5333]. CORROSION BLEND MEETS PRI STEP 8 CRITERIA. NO FURTHSDR DALA2024011600671Unknown · unknownRH SLAT TRACK #4 LOWER AFT SURFACE HAS EVIDENCE OF ROLLER WEAR AND PREVIOUS REWORK REF AA5742-01028-02B LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. 0748182 W C/W PRI ERA 607388-14AD STEP 3. (1832863). C/W PRI ERA 607388- 14AD STEP 9. (5333). CORROSDR DALA2024011600670Unknown · unknownCOPY OF NRT #25 DUE TO LOST PAPERWORK. RH SLAT TRACK #4 PINION TEETH HAS EVIDENCE OF CORROSION. REF. AA5742-01028-02B. LIAISONENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. C/W PRI ERA 607388-14AD REV B STEP 1-16. (LP# 0151121)SDR DALA2024011600669Slat Track · unknownRH SLAT TRACK #5 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF. AA5742-01028-02B LIAISONENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 12JAN24 0907 UTC 02 CORR BY DAVIS 00748182 IAH 12JAN24 ATA 5742 RII: N ENTR 007SDR DALA2024011600665Unknown · unknownRH SLAT TRACK #2 LOWER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF. AA5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. C/W PRI ERA 607388-14AD STEP 3. [1832863]. C/W PRI ERA 607388- 14AD STEP 9. [5333]. CORROSION BLENDSDR IPXA2024021295267Door · crackedLT WING #1 SLAT INBD SLAT DRIVE RETRACTABLE DOOR IS CRACK. PERFORMED SURFACE HFEC INSP OF THE L/H WING #1 SLAT INBD DRIVE RETRACTABLE DOOR IAW A300 NTM PART 6 51-10-08. THE SURFACE AREA OF THE DOOR IS CRACK / DEFECT FREE AT THIS TIME. NDT COMPLETE. INSP ONLY. SDR DALA2024012901254Slat Track · corrodedL/H SLAT TRACK NBR 5 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA5742-01028. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. C/W PRI ER/A 607387-14AD STEP 8 CRITERIA, NO FURTHER REWORK REQUIRED ; REPAIRED LH SLAT TSDR DALA2024011800786Slat Track · corrodedL/H SLAT TRACK NBR 8 UPPER FORWARD HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. C/W PRI ER/A 607387-14AD STEP 9[QC5333] CORROSION BLEND MEETS PRI STEP 8 CRITERIA NO FURTSDR DALA2024011800784Slat Track · corrodedL/H SLAT TRACK NBR 5 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT.C/W PRI ER/A 607387-14AD STEP 9[QC5333] CORROSION BLEND MEETS PRI STEP 8 CRITERIA NO FSDR DALA2024011800783Slat Track · corrodedL/H SLAT TRACK NBR 4 UPPER FORWARD OUTBOARD SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. C/W PRI ER/A 607387-14AD STEP 9 [QC5333] CORROSION BLEND MEETS PRI STEP 8 CSDR DALA2024011800782Slat Track · corrodedL/H SLAT TRACK NBR 4 UPPER FORWARD HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. C/W PRI ER/A 607387-14AD STEP 9 [QC5333] CORROSION BLEND MEETS PRI STEP 8 CRITERIA NO FURTHSDR DALA2024011800780Slat Track · corrodedL/H SLAT TRACK NBR 6 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. C/W PRI ER/A 607387-14AD STEP 9 [QC5333] CORROSION BLEND MEETS PRI STEP 8 CRITERIA NSDR DALA2024011800779Slat Track · corrodedL/H SLAT TRACK NBR 10 LOWER AFT HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT.C/W PRI ER/A 607387-14AD STEP 9 [QC5333] CORROSION BLEND MEETS PRI STEP 8 CRITERIA NO FURTHERSDR DALA2024011800776Slat Track · corrodedL/H SLAT TRACK NBR 7 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. C/W PRI ER/A 607387-14AD STEP 9 [QC5333] CORROSION BLEND MEETS PRI STEP 8 CRITERIA NO FSDR DALA2024011800774Slat Track · corrodedL/H SLAT TRACK NBR 1 UPPER AFT HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA5742-01028-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT.L/H PRI ER/A 607387-14AD STEP 3 [QC 5333] C/W PRI ER/A 607387- 14AD STEP 9. CORROSION BLEND MEESDR DALA2024011800770Slat Track · corrodedL/H SLAT TRACK NBR 1 LOWER FORWARD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA 5742-01028-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. C/W PRI ER/A 607387-14AD STEP 9[QC5333] CORROSION BLEND MEETS PRI STEP 8 CRITERIASDR DALA2024011600676Slat Track · unknownL/H SLAT TRACK NBR 8 UPPER AFT HAS EVIDENCE OF CORROSIN AND PREVIOUS REWORK REF AA5742-01028-02A. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLIGHT. C/W PRI ER/A 607387-14AD STEP 9 [QC5333] CORROSION BLEND MEETS PRI STEP 8 CRITERIA NO FURTHER REWORK RSDR DALA2024011600675Slat Track · unknownL/H SLAT TRACK NBR 6 UPPER FORWARD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. C/W PRI ER/A 607387-14AD STEP 9 [QC5333] CORROSION BLEND MEETS PRI STEP 8 CRITERISDR DALA2024011600674Slat Track · unknownL/H SLAT TRACK NBR 7 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. RII: N ENTR 00748182 W C/W PRI ER/A 607387-14AD STEP 9 [QC5333] CORROSION BLEND MEETSSDR DALA2024011600672Slat Track · unknownL/H SLAT TRACK NBR 5 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA5742-01028. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. C/W PRI ER/A 607387-14AD STEP 9 [QC5333] CORROSION BLEND MEETS PRI STEP 8 CRITERIA, NO FUSDR DALA2024011600668Slat Track · corrodedL/H SLAT TRACK NBR 8 LWR FWD HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF AA5742-01028-02A LIASON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. C/W PRI ER/A 607387-14AD STEP 9 QC 5333. CORROSION BLEND MEETS PRI STEP 8 CRITERIA, NO FURTHER REWOSDR DALA2024011600664Unknown · unknownL/H SLAT TRACK NUMBER 5 LOWER FORWARD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. C/W PRI ER/A 607387-14AD STEP 9. CORROSION BLEND MEETS PRI STEP 8 CRITERIA. NSDR IPXA2024011295267Unknown · unknown*SDR FILED OPEN* FAULT:AA014 -LT WING #1 SLAT INBD SLAT DRIVE RETRACTABLE DOOR IS CRACK. APPROVEDSDR AALA202401123711Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK# 8 LOWER AFT BOLT BETWEEN WS 7316 AND WS 8744, BETWEEN RIBS 13 AND 16. REPLACED BOLT PER TASK CARD 26C61057005.SDR AALA202401129617Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK# 8 LOWER MID BOLT BETWEEN WS 7316 AND WS 8744, BETWEEN RIBS 13 AND 16. REPLACED BOLT PER TASK CARD 26C61057005.SDR AALA202401126944Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK# 8 UPPER AFT BOLT BETWEEN WS 7316 AND WS 8744, BETWEEN RIBS 13 AND 16. REPLACED BOLT PER TASK CARD 26C61057005.SDR AALA202401121450Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK# 8 UPPER FORWARD BOLT BETWEEN WS 7316 AND WS 8744, BETWEEN RIBS 13 AND 16. REPLACED BOLT PER TASK CARD 26C61057005.SDR AALA202401125033Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK# 7 UPPER BOLT BETWEEN WS 7316 AND WS 8744, BETWEEN RIBS 13 AND 16. REPLACED BOLT PER TASK CARD 26C61057005.SDR DALA2024011100513Unknown · unknownAHIP 3310 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR SLAT 2 EXTERNAL SKIN ON RH WING. CORRECTIVE ACTION: COMPLIED WITH PRI 614061-14, VALIDATED ER/A 614061-14 MATCHES PRI 614061-14. EXISTING REPAIR INSTALLED PER A330 SRM 57-40-00, FIGURE 203, WHICH IS CURRESDR SWAA2024020939725Angle · crackedCRACK ANGLE ON AUXILIARY TRACK SLAT 8 INBOARD POSITION RT WING 2023-786223<[01] REPLACED ANGLE ON AUXILIARY TRACK SLAT 8 INBOARD POSITION RT WING IAW B737-700 SRM 51-40-02. SEE INDIVIDUAL STEP SIGNOFF BELOW;[02] CORRECTED STEP 1<BR>REPLACED ANGLE ON AUXILIARY SDR IPXA2024012355631Skin · eroded*SUPPLEMENTAL SDR* FAULT - EROSION, LH WING NO.4 SLAT OUTBD CLOSURE PNL (REPAIR). REMOVE THE DAMAGE MATERIALS AND CLEAN.MEASURE THE DAMAGE AREA(LENGTH:0.5", WIDTH:0.3",DEPTH:1 PLY , 0.7" FROM TRAILING EDGE , 1" FROM OUTBOARD EDGE).BOND THE REPAIR PLIES WITH FISDR FDEA202401090156Skin · dentedFOUND DENT ON #11 SLAT AFT EDGE AT APPROX WS 887, MEASURING 14" X 5.5". COMPLIED WITH (EA# H-5740-T 0378114 P 1 REPAIRED LH WING L/E # 11 SLAT TRAINLING EDGE WEDGE AT WS OSS 887 IN REF TO 767 SRM 57-43-02-2R, PG 1-2 DETAIL I & III, FIG.201 SHEETS 1 & 2, AND SDR IPXA2024012943096Skin · damaged*** SUPPLEMENTAL SDR *** FAULT : # 8 SLAT NOSE SKIN EXISTING REPAIR HAS A VOID SEALANT REPAIRED SEALANT IAW SOPM 20-50-19 STEP 20.SDR AALA202401166412Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK #4 UPPER BOLT BETWEEN RIBS 5 AND 6. REPLACED BOLT PER TASK CARD 26C51057005.SDR IPXA2025030426040Structure · crackedNUMBER 11RT SLAT CAN CRACK REPAIRED #11 RH SLAT CAN BY WELDING I.A.W> MD11 SRM 57-40-02 / DPS 10.225, NDT PER NDTSPM PART 08 AND AGE HARDEN. REF, DPS 7.00 WORK ACCOMPLISHED ON TRAVELER 70028779890001. REVIEWED.SDR COEA2024031905819Strip · chafedWO 251965 NR 400033 HEAVY CHECK COE/MINOR REPAIR: R/H WING FWD SPAR UPPER STRIP SLAT CHAFED. CORRECTIVE ACTION: REPAIRED PER SRAS ES_00231159_01...23063 ISSUE A, DATED 2/28/2024.SDR AALA202401229930Bolt · corrodedAIRCRAT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK #1 LOWER BOLT BETWEEN WS 700 AND WS 1406, BETWEEN RIBS 2 AND 3. REPLACED BOLT PER TASK CARD 26C61057005.SDR AALA202401220320Bolt · corrodedAIRCRAT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK #1 MID AFT BOLT BETWEEN WS 700 AND WS 1406, BETWEEN RIBS 2 AND 3. REPLACED BOLT PER TASK CARD 26C61057005.SDR AALA202401228751Bolt · corrodedAIRCRAT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK #1 MID FORWARD BOLT BETWEEN WS 700 AND WS 1406, BETWEEN RIBS 2 AND 3. REPLACED BOLT PER TASK CARD 26C61057005.SDR DALA2024011100499Unknown · unknownDURING GVI OF #6 L/H SLAT TRACK RACKS AND PINIONS IAW AMDS 5742-01028-2A FOUND # 6 PINION HAVING MINOR SCORING. REPAIRED #6 PINION PER ERA 607567-14AD AND PRI REV 3 ASSOCIATED AA 5742-01028 ADDED FOR AC 8118 ASSOCIATED ER/A 14-607567 ADDED FOR AC 8118. (LP# 01SDR DALA2024011000447Unknown · unknownNEED TO ACCURATELY MEASURE MATERIAL REMOVED ON PINION TEETH. L/H WING PINION 6 AND 11. ACCOMPLISHED A MECHANICAL MEASUREMENT. COMPARED INDEXED MEASUREMENT UTILIZING KNOWN SERVICABLE PINIONS. MEASUREMENT DOCUMENTED ON PRI 607567-14AD REV B. ASSOCIATED AA 5742-0SDR DALA2024011000446Unknown · unknownDURING DVI OF NBR 11 L/H SLAT TRACK RACKS AND PINIONS IAW AMDS 5742-01028-02A. FOUND NBR 11 PINION HAVING MINOR SCORING. ORDERED NBR 11 SLAT TRACK PINION MPN C01612526-001 BRAKE UNLOCK TOOL P/N C01612001-0016500-02. ALSO ORDERED PART NOT REQUIRED. REPAIRED PER
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