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.

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 MJan 12, 2024 · N115DU · Airbus BD5001A10SDR 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)Jan 12, 2024 · N115DU · Airbus BD5001A10SDR 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 REWOJan 12, 2024 · N115DU · Airbus BD5001A10SDR 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 BLENJan 12, 2024 · N115DU · Airbus BD5001A10SDR 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 Jan 12, 2024 · N115DU · Airbus BD5001A10SDR 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 Jan 12, 2024 · N115DU · Airbus BD5001A10SDR 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 MJan 12, 2024 · N115DU · Airbus BD5001A10SDR 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 Jan 12, 2024 · N115DU · Airbus BD5001A10SDR 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 FURTHJan 12, 2024 · N115DU · Airbus BD5001A10SDR 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). CORROJan 12, 2024 · N115DU · Airbus BD5001A10SDR 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)Jan 12, 2024 · N115DU · Airbus BD5001A10SDR 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 007Jan 12, 2024 · N115DU · Airbus BD5001A10SDR 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 BLENDJan 12, 2024 · N115DU · Airbus BD5001A10SDR 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. Jan 11, 2024 · N122UP · Airbus A300F4622RSDR 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 TJan 11, 2024 · N115DU · Airbus BD5001A10SDR 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 FURTJan 11, 2024 · N115DU · Airbus BD5001A10SDR 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 FJan 11, 2024 · N115DU · Airbus BD5001A10SDR 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 CJan 11, 2024 · N115DU · Airbus BD5001A10SDR 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 FURTHJan 11, 2024 · N115DU · Airbus BD5001A10SDR 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 NJan 11, 2024 · N115DU · Airbus BD5001A10SDR 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 FURTHERJan 11, 2024 · N115DU · Airbus BD5001A10SDR 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 FJan 11, 2024 · N115DU · Airbus BD5001A10SDR 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 MEEJan 11, 2024 · N115DU · Airbus BD5001A10SDR 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 CRITERIAJan 11, 2024 · N115DU · Airbus BD5001A10SDR 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 RJan 11, 2024 · N115DU · Airbus BD5001A10SDR 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 CRITERIJan 11, 2024 · N115DU · Airbus BD5001A10SDR 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 MEETSJan 11, 2024 · N115DU · Airbus BD5001A10SDR 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 FUJan 11, 2024 · N115DU · Airbus BD5001A10SDR 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 REWOJan 11, 2024 · N115DU · Airbus BD5001A10SDR 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. NJan 11, 2024 · N115DU · Airbus BD5001A10SDR IPXA2024011295267Unknown · unknown*SDR FILED OPEN* FAULT:AA014 -LT WING #1 SLAT INBD SLAT DRIVE RETRACTABLE DOOR IS CRACK. APPROVEDJan 11, 2024 · N122UP · Airbus A300F4622RSDR 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.Jan 11, 2024 · N661AW · Airbus A320232SDR 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.Jan 11, 2024 · N661AW · Airbus A320232SDR 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.Jan 11, 2024 · N661AW · Airbus A320232SDR 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.Jan 11, 2024 · N661AW · Airbus A320232SDR 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.Jan 11, 2024 · N661AW · Airbus A320232SDR 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 CURREJan 11, 2024 · N810NW · Airbus A330323SDR 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 Jan 10, 2024 · N7726A · Boeing 7377BDSDR 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 FIJan 10, 2024 · N326UP · Boeing 76734AFSDR 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 Jan 9, 2024 · N180FE · Boeing 7673S2FSDR IPXA2024012943096Skin · damaged*** SUPPLEMENTAL SDR *** FAULT : # 8 SLAT NOSE SKIN EXISTING REPAIR HAS A VOID SEALANT REPAIRED SEALANT IAW SOPM 20-50-19 STEP 20.Jan 9, 2024 · N410UP · Boeing 75724APFSDR 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.Jan 9, 2024 · N747UW · Airbus A319112SDR 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.Jan 8, 2024 · N288UP · Doug MD11FSDR 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.Jan 8, 2024 · N819FX · Aerosp ATR72212SDR 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.Jan 8, 2024 · N807AW · Airbus A319132SDR 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.Jan 8, 2024 · N807AW · Airbus A319132SDR 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.Jan 8, 2024 · N807AW · Airbus A319132SDR 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# 01Jan 8, 2024 · N118DU · Bombdr BD1001A10SDR 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 5742-0Jan 8, 2024 · N118DU · Bombdr BD1001A10SDR 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 PERJan 8, 2024 · N118DU · Bombdr BD1001A10
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