N133DU

Service difficulty reports · 53

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. 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 n_number = 'N133DU' AND registry_match = 'registration'
  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 DALA2026090805029Light · inoperativeAFT L2 DOOR EXTERIOR EMERGENCY LIGHT INOP. EXTERIOR EMERGENCY LIGHTS SYSTEMS - DOOR EMERGENCY LIGHTS. R/R AFT LH EMERGENCY LIGHT REF A220 AMP 33-55. OPS CHECK GOOD. (LP# 9622542; AIRCRAFT WAS GROUNDED)Sep 3, 2026 · N133DU · Airbus BD5001A10 · Emergency LightingSDR DALA2026071604188Light · inoperativeRIGHT FWD FUSELAGE EXTERNAL EMERGENCY LIGHT INOP. REMOVED AND REPLACED RH EMERGENCY LIGHT PER AMP 33-55-02. OPS CHECK GOOD. (LP# 8640192; AIRCRAFT WAS GROUNDED)Jul 14, 2026 · N133DU · Airbus BD5001A10 · Emergency LightingSDR DALA2026011400343Oil System · leakingAFTER STARTING BOTH ENGINES AND APU OFF REAR FA CALLED AND REPORTED DIRTY SOCKS SMELL. SMELL REMAINED AFTER SHUTTING RIGHT ENGINE DOWN. C/W SMOKE/FUME WC 0550-2001. P TRAK GRAPH INDICATED APU IS THE SOURCE. CONTINUED WITH WC 0550-2002 WITH NO FINDINGS. INSPECTJan 10, 2026 · N133DU · Airbus BD5001A10 · APU Oil SystemSDR DALA2025112108506Frame · corrodedTHE FOLLOWING HOLES ON FRAME FR76 HAVE CORROSION: HOLE 7 STR 13 (M) (P). REPAIRED PER ER/A PRI 629432-14 REV. 0, REV 1, REV. 2 AND FINAL ER/A 629432-14 REV. ORIGINAL SECTION 1 PERMANENT REPAIR. ORIGINAL THICKNESS WAS .125", MINIMUM REMAINING THICKNESS IS .11Nov 20, 2025 · N133DU · Airbus BD5001A10 · Fuselage Main, FrameSDR DALA2025112108505Frame · damagedTHE FOLLOWING HOLES ON FRAME FR76 HAVE CORROSION: HOLE 1 AT STR 9, HOLE 2 AT STR 9, HOLE 3 AT STR 10, HOLE 5 AT STR12, HOLE 6 AT STR 12, HOLE 11 AT STR 18 AND HOLE 14 AT STR 22. (M) (P) SSI 53-61-23-03. REPAIRED PER ER/A PRI 629432-14 REV. 0, REV 1, REV. 2 ANov 20, 2025 · N133DU · Airbus BD5001A10 · Fuselage Main, FrameSDR DALA2025112108504Skin · damagedNOTED DAMAGE TO SKIN AFT OF RUDDER (M)(P). SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0233:2721-2001/001 00405 COMPLIED WITH PRI 629357 REV 0, 1, AND ERA 629357-14 REV B.Nov 19, 2025 · N133DU · Airbus BD5001A10 · Fuselage, Stabilizer Attach FittingsSDR DALA2025111908452Skin · corrodedWASTE WATER ACCESS PANEL FWD EDGE EXTERNAL SKIN HAS CORROSION. COMPLIED WITH PRI 629290-14 REV 0, 1, 2, AND SECTION I TIME-LIMITED REPAIR OF ERA 629290-14 REV 0. MAX MATERIAL REMOVED 0.059". ORIGINAL THICKNESS 0.125". REMAINING THICKNESS 0.066". (LP# 1308921Nov 17, 2025 · N133DU · Airbus BD5001A10 · Fuselage Main, Plate/SkinSDR DALA2025111908451Skin · corrodedWASTE BOX- FWD DOUBLER R/H CORNER HAS CORROSION INTERNAL AND EXTERNAL COMPLIED WITH PRI 629290-14 REV 0, 1, 2, AND SECTION I TIME-LIMITED REPAIR OF ERA 629290-14 REV 0. MAX MATERIAL REMOVED 0.059". ORIGINAL THICKNESS 0.125". REMAINING THICKNESS 0.066". (LP# Nov 17, 2025 · N133DU · Airbus BD5001A10 · Fuselage Main, Plate/SkinSDR DALA2025111908450Skin · corrodedWASTE BOX- AFT CUTOUT FLANGE SKIN HAS CORROSION. COMPLIED WITH PRI 629290-14 REV 0, 1, 2, AND SECTION I TIME-LIMITED REPAIR OF ERA 629290-14 REV 0. MAX MATERIAL REMOVED 0.059". ORIGINAL THICKNESS 0.125". REMAINING THICKNESS 0.066". (LP# 1308846)Nov 17, 2025 · N133DU · Airbus BD5001A10 · Fuselage Main, Plate/SkinSDR DALA2025111908449Skin · corrodedWASTE BOX- INSIDE THE BOX FWD RT CORNER SKIN HAS CORROSION. COMPLIED WITH PRI 629290-14 REV 0, 1, 2, AND SECTION I TIME-LIMITED REPAIR OF ERA 629290-14 REV 0. MAX MATERIAL REMOVED 0.059". ORIGINAL THICKNESS 0.125". REMAINING THICKNESS 0.066". (LP# 1308845)Nov 17, 2025 · N133DU · Airbus BD5001A10 · Fuselage Main, Plate/SkinSDR DALA2025111908448Skin · corrodedWASTE BOX CUT-OUT FWD RT CORNER SKIN HAS CORROSION. COMPLIED WITH PRI 629290-14 REV 0, 1, 2, AND SECTION I TIME-LIMITED REPAIR OF ERA 629290-14 REV 0. MAX MATERIAL REMOVED 0.059". ORIGINAL THICKNESS 0.125". REMAINING THICKNESS 0.066". (LP# 1308843)Nov 17, 2025 · N133DU · Airbus BD5001A10 · Fuselage Main, Plate/SkinSDR DALA2025111908447Access Panel · corrodedWASTE WATER ACCESS PANEL FWD EDGE INTERNAL SKIN HAS CORROSION. COMPLIED WITH PRI 629290-14 REV 0, 1, 2, AND SECTION I TIME-LIMITED REPAIR OF ERA 629290-14 REV 0. MAX MATERIAL REMOVED 0.059". (LP# 1308838)Nov 17, 2025 · N133DU · Airbus BD5001A10 · Fuselage Main, Plate/SkinSDR DALA2025121009035Skin · damagedER/A 629290-14 ISSUED FOR DOUBLER REPAIR TO THE WASTE BOX AREA. FOLLOW-ON ACTION REQUIRED. ER/A 629290-14 SECTION I ACCOMPLISHED IN MSP NOV 2025. SECTION II REPEAT INSPECTION REQUIRED EVERY 1,000 FH UNTIL SECTION III IS ACCOMPLISHED WITHIN 10,000 FH OF SECTIONNov 11, 2025 · N133DU · Airbus BD5001A10 · Fuselage Main, Plate/SkinSDR DALA2025110508077Scuff Plate · corrodedSCUFF PLATE FASTENERS AFT CARGO COMPARTMENT DOOR. COUNTERSINK AT HOLE 4 AND HOLE 11 HAVE CORROSION IN THE COUNTERSINK. BLEND THE CORROSION ON THE SKIN AND LOWER SILL OUTER SURFACE AT LOCATIONS 1, 17, 1A, 2A, 3A, 6A, 7A, 8A, 11A TO A SMOOTH CONTOUR PER ASRM BNov 5, 2025 · N133DU · Airbus BD5001A10 · Fuselage Miscellaneous StructureSDR DALA2025110508076Skin · damagedPREVIOUS SKIN BLEND-OUT REWORK HAS DIAMETER LARGER THAN .346 INCHES SEE AMDS CARD 5331-01297-02C STEP 5. ACCOMPLISH DVI OF THE FUSELAGE BOTTOM SKIN BEHIND THE SCUFF PLATE FOOTPRINT PER AND TP BD500-A-J51-00-900-1AAA-018A-A AND VERIFY NO CORROSION REMAINS ON Nov 5, 2025 · N133DU · Airbus BD5001A10 · Fuselage Main, Plate/SkinSDR DALA2025110207998Seat Track · corrodedDURING C2 + 6 YEAR (HEAVY) CHECK VISIT IN MSP, EXTENSIVE CORROSION WAS FOUND AT FR20 ON THE FWD END OF RBL 23 CABIN SEAT TRACK P/N C02312798-003 WHICH EXCEEDS PDL LIMITS. REPLACED SEAT TRACK PER ER/A 629516-14. (LP 1283324)Nov 1, 2025 · N133DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025110608105Skin · dentedFUSELAGE SKIN DENT LOCATED JUST FWD OF FR 26 JUST AFT OF L1 DOOR AT FLOOR LINE HAS DENT STICKER CAN NOT FIND LOG PAGE ON STICKER. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0807:5245-2003/004 00651 COMPLETED PRI 6Oct 28, 2025 · N133DU · Airbus BD5001A10 · Fuselage Main, Plate/SkinSDR DALA2025102907932Frame · corrodedWING TO BODY FAIRING FRAME 48, BOTH LEFT AND RIGHT FRAMES SHOW SIGNS OF CORROSION AND ELONGATED FASTENER HOLES. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 053-0001:5352-01038-09 /001 00626. REMOVED AND REPLACED FRAME REF A220 ASRP 53-82-55. (LP# 1272016)Oct 26, 2025 · N133DU · Airbus BD5001A10 · Fuselage Main, StructureSDR DALA2025102407820Pin · bindingUNABLE TO INSERT DISARM PIN IN THE LH OWEED ESCAPE SLIDE. SEE NR FOR ADDITIONAL INFORMATION 001-0400:2561-9101/001 00142 REMOVAL STOCK NUMBER:81-2563-9-0007 SERIAL NUMBER:28136. (LP# 1264495)Oct 21, 2025 · N133DU · Airbus BD5001A10 · Escape SlideSDR DALA2026101905730Skin · damagedDAMAGE TOLERANCE EVALUATION (DTE) REQUIRED. ERA 629805-14 SECTION I ACCOMPLISHED IN MSP DURING CHK. FOLLOW ON ACTION IS REQUIRED ON FUSELAGE SKIN AT FR26, STR. 21L-STR. 22L. ERA 629805-14 SECTION I REPAIR IS ACCEPTABLE FOR 12 MONTHS FROM 17OCT2025 PENDING DTE Oct 20, 2025 · N133DU · Airbus BD5001A10 · Fuselage Main, Plate/SkinSDR DALA2026091105092Seat Track · corrodedREMOVED AND INSTALLED SEAT TRACK PER A220 ASRP 51-77-00- 000AAA-028A-1. 001-0585:5300-2016/002 00428 REMOVED AND INSTALLED SEAT TRACK PER A220 ASRP 51-77-00-000AAA-028A-1 LOG 1262558 CORROSION LEVEL CHANGED FROM: N TO: 2. (LP# 1262558; AIRCRAFT WAS GROUNDED)Oct 20, 2025 · N133DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025102407818Seat Track · corrodedSEAT TRACK RBL 43.5 NEAR FR22 AT FRONT END HAS CORROSION. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0571:5321-2021/003 00337 REMOVE AND REPLACE TRACK REF A220 ASRP 51-7 7-00. LOG 1262654 CORROSION LEVEL CHANGED FOct 20, 2025 · N133DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025102407817Seat Track · corrodedSEAT TRACK CORROSION LBL.23 AT FRAME 74-72. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0585:5300-2016/004 00430 REMOVED AND REPLACED SEAT TRACK PER A220 ASRP 51-77-00-000AAA-028A-1. SUMMARY SEE NR FOR ADDITIONAL IOct 20, 2025 · N133DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025102407816Seat Track · corrodedSEAT TRACK CORROSION LBL.43.5 AT FRAME 74-72. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0585:5300-2016/001 00427 REMOVED AND REPLACED SEAT TRACK TO FRAME PER AIRBUS DWG C01342701. SUMMARY SEE NR FOR ADDITIONAL INOct 20, 2025 · N133DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025102407815Seat Track · corrodedSEAT TRACK CORROSION RBL.23 AT FRAME 74-72. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0585:5300-2016/003 00429 REMOVED AND REPLACED SEAT TRACK PER A220 ASRP 51-77-00-000AAA-028A-1SUMMARY SEE NR FOR ADDITIONAL INFOct 20, 2025 · N133DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025093007122Slat Track · damagedRIGHT WING SLAT TRACK #10 REQUIRES NDT TO BLENDED AREA. PERFORMED NDT INSPECTION PER ANDTP BD500-AJ51-10-02-00AAA-352A-A OR ANDTP BD500-AJ51-01-20-01AAA-353A-A TO BLENDED AREAS AND CHECK FOR SIGNS OF CRACKS. (1216490)Sep 25, 2025 · N133DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2025093007121Slat Track · damagedRIGHT WING SLAT TRACK #8 REQUIRES NDT TO BLENDED AREA. PERFORMED NDT INSPECTION PER ANDTP BD500-AJ51-10-02-00AAA-352A-A OR ANDTP BD500-AJ51-01-20-01AAA-353A-A TO BLENDED AREAS AND CHECK FOR SIGNS OF CRACKS. (1216489)Sep 25, 2025 · N133DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2025093007120Slat Track · damagedRIGHT WING SLAT TRACK #7 REQUIRES NDT TO BLENDED AREA. PERFORMED NDT INSPECTION PER ANDTP BD500-AJ51-10-02-00AAA-352A-A OR ANDTP BD500-AJ51-01-20-01AAA-353A-A TO BLENDED AREAS AND CHECK FOR SIGNS OF CRACKS. (1216487)Sep 25, 2025 · N133DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2025093007119Slat Track · damagedRIGHT WING SLAT TRACK #6 REQUIRES NDT TO BLENDED AREA. PERFORMED NDT INSPECTION PER ANDTP BD500-AJ51-10-02-00AAA-352A-A OR ANDTP BD500-AJ51-01-20-01AAA-353A-A TO BLENDED AREAS AND CHECK FOR SIGNS OF CRACKS. (1216486)Sep 25, 2025 · N133DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2025093007118Slat Track · damagedRIGHT WING SLAT TRACK NR 5 REQUIRES NDT TO BLENDED AREA. PERFORMED NDT INSPECTION PER ANDTP BD500-AJ51-10-02-00AAA-352A-A OR ANDTP BD500-AJ51-01-20-01AAA-353A-A TO BLENDED AREAS AND CHECK FOR SIGNS OF CRACKS. (1216484)Sep 25, 2025 · N133DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2025093007117Slat Track · damagedRIGHT WING SLAT TRACK #3 REQUIRES NDT TO BLENDED AREA. PERFORMED NDT INSPECTION PER ANDTP BD500-AJ51-10-02-00AAA-352A-A OR ANDTP BD500-AJ51-01-20-01AAA-353A-A TO BLENDED AREAS AND CHECK FOR SIGNS OF CRACKS. (1216480)Sep 25, 2025 · N133DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2025093007116Slat Track · damagedLEFT WING SLAT TRACK #11 REQUIRES NDT TO BLENDED AREA. PERFORMED NDT INSPECTION PER ANDTP BD500-A-J51-10-02-00AAA- 352A-A OR ANDTP BD500-A-J51-01-20-01AAA-353A-A TO BLENDED AREAS AND CHECK FOR SIGNS OF CRACKS. NO CRACKS FOUND. (1216128)Sep 24, 2025 · N133DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2025093007115Slat Track · damagedLEFT WING SLAT TRACK #10 REQUIRES NDT TO BLENDED AREA. PERFORMED NDT INSPECTION PER ANDTP BD500-A-J51-10-02-00AAA- 352A-A OR ANDTP BD500-A-J51-01-20-01AAA-353A-A TO BLENDED AREAS AND CHECK FOR SIGNS OF CRACKS. NO CRACKS FOUND. (1216125)Sep 24, 2025 · N133DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2025093007114Slat Track · damagedLEFT WING SLAT TRACK #9 REQUIRES NDT TO BLENDED AREA. PERFORMED NDT INSPECTION PER ANDTP BD500-A-J51-10-02-00AAA- 352A-A OR ANDTP BD500-A-J51-01-20-01AAA-353A-A TO BLENDED AREAS AND CHECK FOR SIGNS OF CRACKS. NO CRACKS FOUND. (1216123)Sep 24, 2025 · N133DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2025093007113Slat Track · damagedLEFT WING SLAT TRACK #7 REQUIRES NDT TO BLENDED AREA. PERFORMED NDT INSPECTION PER ANDTP BD500-A-J51-10-02-00AAA- 352A-A OR ANDTP BD500-A-J51-01-20-01AAA-353A-A TO BLENDED AREAS AND CHECK FOR SIGNS OF CRACKS. NO CRACKS FOUND. (1216122)Sep 24, 2025 · N133DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2025093007112Slat Track · damagedLEFT WING SLAT TRACK #4 REQUIRES NDT TO BLENDED AREA. PERFORMED NDT INSPECTION PER ANDTP BD500-A-J51-10-02-00AAA- 352A-A OR ANDTP BD500-A-J51-01-20-01AAA-353A-A TO BLENDED AREAS AND CHECK FOR SIGNS OF CRACKS. NO CRACKS FOUND. (1216121)Sep 24, 2025 · N133DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2025010600118Slat Track · corrodedRH SLAT TRACK #5 HAS CORROSION AND MUST BE INSPECTED WITH EDDY CURRENT. ACCOMPLISHED EDDY CURRENT INSPECTION OF THE BLENDED AREA REF ANDTP 51-01-20-01AAA-353A-3. NO CRACK INDICATIONS NOTED. W REFERENCE LP 6955745 FOR SDR RECORD-ABLE EVENT. (LP# 0742846)Jan 3, 2025 · N133DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2025010600117Slat Track · corrodedLH SLAT TRACK #1 HAS CORROSION AND MUST BE INSPECTED WITH EDDY CURRENT. ACCOMPLISHED EDDY CURRENT INSPECTION OF THE BLENDED AREA REF A22 ANDTP 51-01-20-01AAA-353A-A. NO CRACK INDICATIONS NOTED. W REFERENCE LP 6955744 FOR SDR RECORDABLE EVENT. (LP# 0742835)Jan 3, 2025 · N133DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2025010600116Slat Track · corrodedLH SLAT TRACK #4 HAS CORROSION AND MUST BE INSPECTED WITH EDDY CURRENT. ACCOMPLISHED EDDY CURRENT INSPECTION OF THE BLENDED AREA REF A220 ANDTP 51-01-20-01AAA-353A-A. NO CRACK INDICATION NOTED. W REFERENCE LP 6955743 FOR SDR RECORDABLE EVENT. (LP# 0742776)Jan 3, 2025 · N133DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024061106024Slat Track · corrodedRH SLAT TRACK NBR 4 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 4 UPPER AFT SURFACE IAW ER/A 607397- 14AD REV C AND PRI 607397-14AD REV O MATCHED. (LP# 0381655)Jun 7, 2024 · N133DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024061106023Slat Track · corrodedRH SLAT TRACK #5 LOWER FWD INBOARD SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 5 LOWER FWD INBOARD SIDE IAW ER/A 607397-14AD REV C AND PRI 607397-14AD REV 0 MATCHED. (LP# 0381641)Jun 7, 2024 · N133DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024061106022Slat Track · corrodedRH SLAT TRACK #5 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 5 UPPER AFT SURFACE IAW ER/A 607397- 14AD REV C AND PRI 607397-14AD REV 0 MATCHED. (LP# 0381634)Jun 7, 2024 · N133DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024061106021Slat Track · corrodedRH SLAT TRACK #8 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 8 LOWER AFT SURFACE IAW ER/A 607397- 14AD REV C AND PRI 607397-14AD REV 0 MATCHED. (LP# 0381627)Jun 7, 2024 · N133DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024061106020Slat Track · corrodedRH SLAT TRACK #9 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 9 LOWER AFT SURFACE IAW ER/A 607397- 14AD REV C AND PRI 607397-14AD REV 0 MATCHED. (LP# 0381620)Jun 7, 2024 · N133DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024061106019Slat Track · corrodedLH SLAT TRACK NBR 2 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 2 UPPER AFT SURFACE IAW ER/A 607396- 14AD REV C AND PRI 607396-14AD REV 0 MATCHED. (LP# 0380625)Jun 7, 2024 · N133DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024061106018Slat Track · corrodedLH SLAT TRACK NBR 7 LOWER FWD I/B SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 7 LOWER FWD I/B SIDE IAW ER/A 607396- 14AD REV C AND PRI 607396-14AD REV 0 MATCHED. (LP# 0380613)Jun 7, 2024 · N133DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024061106017Slat Track · corrodedLH SLAT TRACK NBR 6 LOWER FWD I/B SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 6 LOWER FWD I/B SIDE IAW ER/A 607396- 14AD REV C AND PRI 607396-14AD REV 0 MATCHED. (LP# 0380605)Jun 7, 2024 · N133DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024061106016Slat Track · corrodedLH SLAT TRACK NBR 5 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 5 UPPER AFT SURFACE IAW ER/A 607396- 14AD REV C AND PRI 607396-14AD REV 0 MATCHED. (LP# 0380601)Jun 7, 2024 · N133DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2023121910379Unknown · unknownEMERGENCY EXIT SIGNS DO NOT ILLUMINATE WHEN LANDING GEARS ARE LOWERED. ENTIRE CABIN. / INTERIOR. PERFORMED OPS CK OF EMERGENCY LIGHTS, ALL LIGHTS ILLUMINATED. NO FURTHER DEFECTS. (LP# 0116181)Dec 18, 2023 · N133DU · Bombdr BD1001A10 · Emergency LightingSDR DALA2023091507598Unknown · unknownSHIP 8133 - MISC/DE - DUE TO "FUEL IMBALANCE AND R FUEL LO QTY" CAUTION MESSAGES ON APPROACH. CORRECTIVE ACTION: FUEL/OIL HEAT EXCHANGER AND RT REFUEL SOV REPLACED. (LP# 4927068, 4927074, 2962595)Sep 11, 2023 · N133DU · Bombdr BD1001A10 · Fuel Storage
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