# Service difficulty reports: N133DU

A list on [N133DU](https://openairdocs.org/aircraft/N133DU.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 2 · 53 reports

- [SDR DALA2026090805029](https://openairdocs.org/sdr/DALA2026090805029.md): Light · inoperative · Sep 3, 2026 · N133DU · Airbus BD5001A10 · Emergency Lighting
  > AFT 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)
- [SDR DALA2026071604188](https://openairdocs.org/sdr/DALA2026071604188.md): Light · inoperative · Jul 14, 2026 · N133DU · Airbus BD5001A10 · Emergency Lighting
  > RIGHT 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)
- [SDR DALA2026011400343](https://openairdocs.org/sdr/DALA2026011400343.md): Oil System · leaking · Jan 10, 2026 · N133DU · Airbus BD5001A10 · APU Oil System
  > AFTER 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. INSPECT
- [SDR DALA2025112108506](https://openairdocs.org/sdr/DALA2025112108506.md): Frame · corroded · Nov 20, 2025 · N133DU · Airbus BD5001A10 · Fuselage Main, Frame
  > THE 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.11
- [SDR DALA2025112108505](https://openairdocs.org/sdr/DALA2025112108505.md): Frame · damaged · Nov 20, 2025 · N133DU · Airbus BD5001A10 · Fuselage Main, Frame
  > THE 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 A
- [SDR DALA2025112108504](https://openairdocs.org/sdr/DALA2025112108504.md): Skin · damaged · Nov 19, 2025 · N133DU · Airbus BD5001A10 · Fuselage, Stabilizer Attach Fittings
  > NOTED 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.
- [SDR DALA2025111908452](https://openairdocs.org/sdr/DALA2025111908452.md): Skin · corroded · Nov 17, 2025 · N133DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > WASTE 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# 1308921
- [SDR DALA2025111908451](https://openairdocs.org/sdr/DALA2025111908451.md): Skin · corroded · Nov 17, 2025 · N133DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > WASTE 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#
- [SDR DALA2025111908450](https://openairdocs.org/sdr/DALA2025111908450.md): Skin · corroded · Nov 17, 2025 · N133DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > WASTE 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)
- [SDR DALA2025111908449](https://openairdocs.org/sdr/DALA2025111908449.md): Skin · corroded · Nov 17, 2025 · N133DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > WASTE 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)
- [SDR DALA2025111908448](https://openairdocs.org/sdr/DALA2025111908448.md): Skin · corroded · Nov 17, 2025 · N133DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > WASTE 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)
- [SDR DALA2025111908447](https://openairdocs.org/sdr/DALA2025111908447.md): Access Panel · corroded · Nov 17, 2025 · N133DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > WASTE 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)
- [SDR DALA2025121009035](https://openairdocs.org/sdr/DALA2025121009035.md): Skin · damaged · Nov 11, 2025 · N133DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > ER/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 SECTION
- [SDR DALA2025110508077](https://openairdocs.org/sdr/DALA2025110508077.md): Scuff Plate · corroded · Nov 5, 2025 · N133DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > SCUFF 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 B
- [SDR DALA2025110508076](https://openairdocs.org/sdr/DALA2025110508076.md): Skin · damaged · Nov 5, 2025 · N133DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > PREVIOUS 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
- [SDR DALA2025110207998](https://openairdocs.org/sdr/DALA2025110207998.md): Seat Track · corroded · Nov 1, 2025 · N133DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > DURING 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)
- [SDR DALA2025110608105](https://openairdocs.org/sdr/DALA2025110608105.md): Skin · dented · Oct 28, 2025 · N133DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > FUSELAGE 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 6
- [SDR DALA2025102907932](https://openairdocs.org/sdr/DALA2025102907932.md): Frame · corroded · Oct 26, 2025 · N133DU · Airbus BD5001A10 · Fuselage Main, Structure
  > WING 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)
- [SDR DALA2025102407820](https://openairdocs.org/sdr/DALA2025102407820.md): Pin · binding · Oct 21, 2025 · N133DU · Airbus BD5001A10 · Escape Slide
  > UNABLE 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)
- [SDR DALA2026101905730](https://openairdocs.org/sdr/DALA2026101905730.md): Skin · damaged · Oct 20, 2025 · N133DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > DAMAGE 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
- [SDR DALA2026091105092](https://openairdocs.org/sdr/DALA2026091105092.md): Seat Track · corroded · Oct 20, 2025 · N133DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > REMOVED 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)
- [SDR DALA2025102407818](https://openairdocs.org/sdr/DALA2025102407818.md): Seat Track · corroded · Oct 20, 2025 · N133DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT 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 F
- [SDR DALA2025102407817](https://openairdocs.org/sdr/DALA2025102407817.md): Seat Track · corroded · Oct 20, 2025 · N133DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT 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 I
- [SDR DALA2025102407816](https://openairdocs.org/sdr/DALA2025102407816.md): Seat Track · corroded · Oct 20, 2025 · N133DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT 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 IN
- [SDR DALA2025102407815](https://openairdocs.org/sdr/DALA2025102407815.md): Seat Track · corroded · Oct 20, 2025 · N133DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT 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 INF
- [SDR DALA2025093007122](https://openairdocs.org/sdr/DALA2025093007122.md): Slat Track · damaged · Sep 25, 2025 · N133DU · Airbus BD5001A10 · Leading Edge Devices
  > RIGHT 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)
- [SDR DALA2025093007121](https://openairdocs.org/sdr/DALA2025093007121.md): Slat Track · damaged · Sep 25, 2025 · N133DU · Airbus BD5001A10 · Leading Edge Devices
  > RIGHT 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)
- [SDR DALA2025093007120](https://openairdocs.org/sdr/DALA2025093007120.md): Slat Track · damaged · Sep 25, 2025 · N133DU · Airbus BD5001A10 · Leading Edge Devices
  > RIGHT 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)
- [SDR DALA2025093007119](https://openairdocs.org/sdr/DALA2025093007119.md): Slat Track · damaged · Sep 25, 2025 · N133DU · Airbus BD5001A10 · Leading Edge Devices
  > RIGHT 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)
- [SDR DALA2025093007118](https://openairdocs.org/sdr/DALA2025093007118.md): Slat Track · damaged · Sep 25, 2025 · N133DU · Airbus BD5001A10 · Leading Edge Devices
  > RIGHT 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)
- [SDR DALA2025093007117](https://openairdocs.org/sdr/DALA2025093007117.md): Slat Track · damaged · Sep 25, 2025 · N133DU · Airbus BD5001A10 · Leading Edge Devices
  > RIGHT 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)
- [SDR DALA2025093007116](https://openairdocs.org/sdr/DALA2025093007116.md): Slat Track · damaged · Sep 24, 2025 · N133DU · Airbus BD5001A10 · Leading Edge Devices
  > LEFT 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)
- [SDR DALA2025093007115](https://openairdocs.org/sdr/DALA2025093007115.md): Slat Track · damaged · Sep 24, 2025 · N133DU · Airbus BD5001A10 · Leading Edge Devices
  > LEFT 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)
- [SDR DALA2025093007114](https://openairdocs.org/sdr/DALA2025093007114.md): Slat Track · damaged · Sep 24, 2025 · N133DU · Airbus BD5001A10 · Leading Edge Devices
  > LEFT 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)
- [SDR DALA2025093007113](https://openairdocs.org/sdr/DALA2025093007113.md): Slat Track · damaged · Sep 24, 2025 · N133DU · Airbus BD5001A10 · Leading Edge Devices
  > LEFT 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)
- [SDR DALA2025093007112](https://openairdocs.org/sdr/DALA2025093007112.md): Slat Track · damaged · Sep 24, 2025 · N133DU · Airbus BD5001A10 · Leading Edge Devices
  > LEFT 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)
- [SDR DALA2025010600118](https://openairdocs.org/sdr/DALA2025010600118.md): Slat Track · corroded · Jan 3, 2025 · N133DU · Airbus BD5001A10 · Leading Edge Devices
  > RH 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)
- [SDR DALA2025010600117](https://openairdocs.org/sdr/DALA2025010600117.md): Slat Track · corroded · Jan 3, 2025 · N133DU · Airbus BD5001A10 · Leading Edge Devices
  > LH 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)
- [SDR DALA2025010600116](https://openairdocs.org/sdr/DALA2025010600116.md): Slat Track · corroded · Jan 3, 2025 · N133DU · Airbus BD5001A10 · Leading Edge Devices
  > LH 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)
- [SDR DALA2024061106024](https://openairdocs.org/sdr/DALA2024061106024.md): Slat Track · corroded · Jun 7, 2024 · N133DU · Airbus BD5001A10 · Leading Edge Devices
  > RH 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)
- [SDR DALA2024061106023](https://openairdocs.org/sdr/DALA2024061106023.md): Slat Track · corroded · Jun 7, 2024 · N133DU · Airbus BD5001A10 · Leading Edge Devices
  > RH 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)
- [SDR DALA2024061106022](https://openairdocs.org/sdr/DALA2024061106022.md): Slat Track · corroded · Jun 7, 2024 · N133DU · Airbus BD5001A10 · Leading Edge Devices
  > RH 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)
- [SDR DALA2024061106021](https://openairdocs.org/sdr/DALA2024061106021.md): Slat Track · corroded · Jun 7, 2024 · N133DU · Airbus BD5001A10 · Leading Edge Devices
  > RH 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)
- [SDR DALA2024061106020](https://openairdocs.org/sdr/DALA2024061106020.md): Slat Track · corroded · Jun 7, 2024 · N133DU · Airbus BD5001A10 · Leading Edge Devices
  > RH 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)
- [SDR DALA2024061106019](https://openairdocs.org/sdr/DALA2024061106019.md): Slat Track · corroded · Jun 7, 2024 · N133DU · Airbus BD5001A10 · Leading Edge Devices
  > LH 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)
- [SDR DALA2024061106018](https://openairdocs.org/sdr/DALA2024061106018.md): Slat Track · corroded · Jun 7, 2024 · N133DU · Airbus BD5001A10 · Leading Edge Devices
  > LH 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)
- [SDR DALA2024061106017](https://openairdocs.org/sdr/DALA2024061106017.md): Slat Track · corroded · Jun 7, 2024 · N133DU · Airbus BD5001A10 · Leading Edge Devices
  > LH 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)
- [SDR DALA2024061106016](https://openairdocs.org/sdr/DALA2024061106016.md): Slat Track · corroded · Jun 7, 2024 · N133DU · Airbus BD5001A10 · Leading Edge Devices
  > LH 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)
- [SDR DALA2023121910379](https://openairdocs.org/sdr/DALA2023121910379.md): Unknown · unknown · Dec 18, 2023 · N133DU · Bombdr BD1001A10 · Emergency Lighting
  > EMERGENCY 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)
- [SDR DALA2023091507598](https://openairdocs.org/sdr/DALA2023091507598.md): Unknown · unknown · Sep 11, 2023 · N133DU · Bombdr BD1001A10 · Fuel Storage
  > SHIP 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)

Next page: https://openairdocs.org/aircraft/N133DU/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/aircraft/N133DU/reports

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