# Service difficulty reports: N137DU

A list on [N137DU](https://openairdocs.org/aircraft/N137DU.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 · 56 reports

- [SDR DALA2026061503583](https://openairdocs.org/sdr/DALA2026061503583.md): Longeron · corroded · Jun 10, 2026 · N137DU · Airbus BD5001A10 · Aerodynamic Fairings
  > ER/A 634632-14; A220-100, MID FUSELAGE WING TO BODY FAIRING LONGERONS BTWN FR36-38, FR42-FR45, & FR48-FR52 CORRODED. SUBJECT REPAIR REQUIRES FOLLOW-ON ACTION. ACCOMPLISH 634632-14, SECTION II REPETITIVE INSPECTION WITHIN EVERY 1,000 FLIGHT HOURS FROM 14,712
- [SDR DALA2026061503582](https://openairdocs.org/sdr/DALA2026061503582.md): Skin · corroded · Jun 10, 2026 · N137DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > CORROSION FOUND ON EXTERNAL FUSELAGE SKIN AT FR57-61 STR36-L. C/W ER/A 634830-14AD REV ORIGINAL. (LP# 1639893; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026061503581](https://openairdocs.org/sdr/DALA2026061503581.md): Structure · corroded · Jun 9, 2026 · N137DU · Airbus BD5001A10 · Fuselage Main, Structure
  > WHILE WORKING NRC 00177 FOR REMOVAL OF WASTE SERVICE INTERNL SKIN DOUBLER, FOUND ADDITIONAL CORROSION ON WASTE BOX INTERNAL AREA AT AFT RT SENSOR. C/W DELTA ER/A 635012-14, REV: O SECTION I, WITHIN EVERY 1,000 FLT HRS FROM 14,712 TOTAL ACFT FLT HRS AS OF 05JU
- [SDR DALA2026061103541](https://openairdocs.org/sdr/DALA2026061103541.md): Doubler · corroded · Jun 9, 2026 · N137DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > ER/A 635012-14; A220-100 FUSELAGE REAR BARREL SKIN DOUBLER, WASTE ACCESS AND WASTE BOX ASSY / BTW FR75 - FR76, STR 32L - STR 36L / CORROSION. SUBJECT REPAIR REQUIRES FOLLOW-ON ACTION. ACCOMPLISH 635012-14, SECTION II REPETITIVE INSPECTION WITHIN EVERY 1,000
- [SDR DALA2026060903491](https://openairdocs.org/sdr/DALA2026060903491.md): Frame · corroded · Jun 5, 2026 · N137DU · Airbus BD5001A10 · Fuselage Main, Frame
  > CORROSION ON FR81 INNER AND OUTER SURFACES APPROX. 4 IN FROM STRINGER 19L TOWARD RT (INTERCOASTAL LOWER FR80-81) AT AFT EQUIPMENT COMPARTMENT DOOR CUTOUT SURROUND STRUCTURE (MARKED). REMOVED AND REPLACED FRAME AT FR 81 BETWEEN STRINGER 17R TO STRINGER 18L PER
- [SDR DALA2026060903490](https://openairdocs.org/sdr/DALA2026060903490.md): Frame · corroded · Jun 5, 2026 · N137DU · Airbus BD5001A10 · Fuselage Main, Frame
  > WHILE WORKING ON FR81 INNER AND OUTER SURFACES DAMAGE ON CC# 00187, FOUND FR80 WITH CORROSION BETWEEN LBL 7 AND RBL7. REMOVED AND REPLACED FRAMES AT FR 80 L/H AND R/H SIDE OF BELLY PER A220 ASRP BD500-A-J51-42-20-00AAA-078A-A AND BOMBARDIER DWG C01401201 REV R
- [SDR DALA2026060303375](https://openairdocs.org/sdr/DALA2026060303375.md): Floor Panel · corroded · Jun 1, 2026 · N137DU · Airbus BD5001A10 · Fuselage Floor Panel
  > AFT SERVICE ENTRY FLOOR PANEL WITH CORROSION. REMOVED AND REPLACED AFT SERVICE ENTRY FLOOR PANEL IAW A220 AM BD500-A-J53-00-47-14AAA-720A-A. (LP# 1624367; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026053003278](https://openairdocs.org/sdr/DALA2026053003278.md): Floor Support · corroded · May 29, 2026 · N137DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > CORROSION LEVEL 2 ON FLOOR EDGE SUPPORT AT FR-76, RBL-51, WL-151. REMOVED SILL WEB DAMAGED AND INSTALLED NEW SILL WEB AT FR 76 RBL 51 WL 151 IAW PL C01342700 REV-T. (LP 1619490 - AIRCRAFT WAS GROUNDED)
- [SDR DALA2026052803247](https://openairdocs.org/sdr/DALA2026052803247.md): Support Angle · corroded · May 27, 2026 · N137DU · Airbus BD5001A10 · Aerodynamic Fairings
  > CORROSION LEVEL 2, WTB ANGLE SUPPORT BETWEEN FR57 AND FR58, STR33-L AND STR33-R. REMOVED DAMAGED WTB ANGLE SUPPORT BETWEEN FR57 AND FR58, STR 33-L AND STR 33-R AND REPLACED PER A220 ASRP BD500-A-J51-42-06-00AAA-0780A-A AND DWG# PL C01731500 REV-E. (LP 16158
- [SDR DALA2026052403143](https://openairdocs.org/sdr/DALA2026052403143.md): Floor Panel · corroded · May 23, 2026 · N137DU · Airbus BD5001A10 · Fuselage Floor Panel
  > AIRCRAFT 8137, FWD SERVICE ENTRY FLOOR PANEL WITH CORROSION LEVEL 2. REPLACED FWD SERVICE DOOR FLOOR PANEL IAW A220 AMP BD500-J53-00-47-12AAA-720A-A. (LP 1609049 - AIRCRAFT WAS GROUNDED)
- [SDR DALA2026052303126](https://openairdocs.org/sdr/DALA2026052303126.md): Seat Track · corroded · May 22, 2026 · N137DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > AIRCRAFT 8137, CORROSION LEVEL 2 FORWARD CABIN RIGHT O/B SEAT TRACK CORROSION ON FORWARD END RBL 43.5 FR20 WL 151.5. REPLACED SEAT TRACK RBL 43.5 FR20 TO FR30 IAW A220 ASRP BD500-A-J51-42-20-00AAA-078A-A AND DWG C02312600 REV: K. (LP 1606885 - AIRCRAFT WAS G
- [SDR DALA2026052203124](https://openairdocs.org/sdr/DALA2026052203124.md): Seat Track · corroded · May 21, 2026 · N137DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION LEVEL 2 RIGHT OTBD SEAT TRACK AFT END CORRODED AT FR 74 RBL 43.5 WL 151.5. REPLACED SEAT TRACK RT OTBD RBL 43.5, FR 74 - 61 IAW ASRP BD500-A-J51-40-11-01AAA-652A-A, DWG PL C0134422701 REV: G AND ASRP BD500-A-J51-42-21-00AAA-078A-A. (LP 1605266 - A
- [SDR DALA2026051903060](https://openairdocs.org/sdr/DALA2026051903060.md): Seat Track · corroded · May 18, 2026 · N137DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT INBD SEAT TRACK AFT END CORRODED AT FR74 LBL 23 WL 151.5. REMOVED AND REPLACED SEAT TRACK L/H / I/B FROM FR 61 TO FR 74 LBL 23 WL 151.5 I.A.W A220 ASRP BD500-A-J51-42-20-00AAA-078A-A, BOMBARDIER PL C01342701 REV-G. (LP# 1600284; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026051903059](https://openairdocs.org/sdr/DALA2026051903059.md): Seat Track · corroded · May 18, 2026 · N137DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT INBD SEAT TRACK AFT END CORRODED AT FR 74 RBL 23 WL151.5. REMOVED DAMAGED SEAT TRACK FROM FR 61 TO FR 74 RBL 23 WL 151.5 AND INSTALLED NEW SEAT TRACK I.A.W A220 ASRP BD500-A-J51-42-20- 00AAA-078A-A AND BOMBARDIER PL C01342701 REV-G. (LP# 1600261; AIRCRAF
- [SDR DALA2026051803051](https://openairdocs.org/sdr/DALA2026051803051.md): Seat Track · corroded · May 15, 2026 · N137DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > LEVEL 2 CORROSION, FORWARD CABIN RIGHT I/B SEAT TRACK CORROSION ON FORWARD END RBL 23 FR20 WL151.5. REPLACED FWD CABIN R/H I/B SEAT TRACK AT RBL 23, BTW FR=20 TO FR=30 PER BOMBARDIER C0231600 REV: K AND ASRP BD500-A-J51-42-20-00AAA-078A-A. (LP 1594928 - AIRC
- [SDR DALA2026051803050](https://openairdocs.org/sdr/DALA2026051803050.md): Seat Track · corroded · May 14, 2026 · N137DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > LEVEL 2 CORROSION, L/H O/B SEAT TRACK AFT END CORRODED AT FR74 LBL 43.5 WL 151.5. REPLACED L/H O/B SEAT TRACK FROM FR60 TO FR74 LBL 43.5 WL 151.5 PER BOMBARDIER DWG PL C01342701 REV-G AND A220 ASRP BD500-A-J51-42-20-00AAA-078A-A. (LP 1593828 - AIRCRAFT WAS G
- [SDR DALA2025101307463](https://openairdocs.org/sdr/DALA2025101307463.md): Hinge Fitting · cracked · Oct 8, 2025 · N137DU · Airbus BD5001A10 · Rudder Structure
  > FOUND RUDDER HINGE #1 CRACKED AND RUDDER LOWER CLOSURE RIB CRACKED. REPAIRED PER PRI 629727-14 REV 0 AND ER/A 629727-14 REV ORIGINAL. (LP# 1240208)
- [SDR DALA2025040102431](https://openairdocs.org/sdr/DALA2025040102431.md): Slat Track · corroded · Mar 29, 2025 · N137DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK #9 PINION TEETH (1EA) HAS EVIDENCE OF CORROSION WITH NO PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. COMPLIED WITH ERA 625409-14AD AND PRI 625409-14AD MATCHES. (LP# 0884832)
- [SDR DALA2025040102430](https://openairdocs.org/sdr/DALA2025040102430.md): Slat Track · corroded · Mar 29, 2025 · N137DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK #9 RACK TEETH(1EA) HAS EVIDENCE OF CORROSION WITH NO PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. COMPLIED WITH EAR 625409-14AD AND PRI 625409-14AD MATCHES. (LP# 0884831)
- [SDR DALA2025040102429](https://openairdocs.org/sdr/DALA2025040102429.md): Slat Track · corroded · Mar 29, 2025 · N137DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK #4 PINION TEETH (2EA) HAS EVIDENCE OF CORROSION WITH NO PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. COMPLIED WITH ERA 625409-14AD AND PRI 625409-14AD MATCHES. (LP# 0884825)
- [SDR DALA2025040102428](https://openairdocs.org/sdr/DALA2025040102428.md): Slat Track · corroded · Mar 29, 2025 · N137DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK #4 RACK TEETH (2EA) HAS EVIDENCE OF CORROSION WITH NO PREVIOUS REWORD REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. COMPLIED WITH ERA 625409-14AD AND PRI 625409-14AD MATCHES. (LP# 0884822)
- [SDR DALA2024102110274](https://openairdocs.org/sdr/DALA2024102110274.md): Light · missing · Oct 16, 2024 · N137DU · Airbus BD5001A10 · Emergency Lighting
  > DURING CRV FOUND 2FT REFLECTING ESCAPE PATH MARKING MISSING AT 01B. REPLACED ESCAPE PATH MARKING 01B A220 25-28 AMP. (LP# 6094396)
- [SDR DALA2024082908531](https://openairdocs.org/sdr/DALA2024082908531.md): Slat Track · corroded · Aug 29, 2024 · N137DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 2 UPPER FWD SURFACE FOUND WITH CORROSION AND BLENDED PER AMDS W/C 5742-01028-02A, REQUIRES NDT INSPECTION TO CHECK FOR SIGNS OF CRACKS. REMOVED CORROSION FROM SURFACE BY BLENDING FROM MECHANICAL MEANS. OH 2217529 PERFORMED HFEC ON SLAT TRACK
- [SDR DALA2024082908530](https://openairdocs.org/sdr/DALA2024082908530.md): Slat Track · corroded · Aug 29, 2024 · N137DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 5 UPPER AFT SURFACE FOUND WITH CORROSION AND BLENDED PER AMDS W/C 5742-01028-02B, REQUIRES NDT INSPECTION TO CHECK FOR SIGNS OF CRACKS.REMOVED CORROSION FROM SURFACE BY BLENDING FROM MECHANICAL MEANS. OH 2217529 PREFORMED HFEC ON SLAT TRACK
- [SDR DALA2024081308069](https://openairdocs.org/sdr/DALA2024081308069.md): Longeron · cracked · Aug 11, 2024 · N137DU · Airbus BD5001A10 · Fuselage Main, Longeron/Stringer
  > WHEN PREFORMING WING TO BODY FAIRING SUPPORT STRUCTURE INSPECTION CARD 5353-01038-01B CHECK. FOUND RIGHT LONGERON P/N C02383111-002 CRACKED. STARTED TO REMOVE LONGERON P/N- C02383111-002 PER AMDS 5352-01038-05B. REPLACED LONGERON PER AMDS 5352-0103B-05B NEED
- [SDR DALA2024051505241](https://openairdocs.org/sdr/DALA2024051505241.md): Fuel Line · worn · May 14, 2024 · N137DU · Airbus BD5001A10 · Fuel Storage
  > RH FUEL TANK, DURING ACCOMPLISHMENT OF AMDS 2820-01281-07B STEP 17, ITEM 6 NOTED FUEL TUBE FLANGE WORN BEYOND LIMITS (0.010). REPLACED RH FUEL TANK, ITEM 6 FUEL TUBE P/N C01633386-013 IAW AMDS WC 2820-01281-07B AND A220 AMP BD500-A-J28-21-80-07AAA- 720A-A. CDC
- [SDR DALA2024030603078](https://openairdocs.org/sdr/DALA2024030603078.md): Smoke Detector · failed · Mar 5, 2024 · N137DU · Airbus BD5001A10 · Smoke Detection
  > SHIP 8137 - DIV - TO OMA DUE TO AN EQUIPMENT BAY SMOKE FAIL MESSAGE. CORRECTIVE ACTION: REPLACED AVIONICS AND ELECTRICAL BAY SMOKE DETECTOR SYSTEMS AND TUBING FOR SYSTEM 'A' AND 'B'. (LP# 4344552, 0227027)
- [SDR DALA2024012200962](https://openairdocs.org/sdr/DALA2024012200962.md): Slat Track · corroded · Jan 16, 2024 · N137DU · Airbus BD5001A10 · Leading Edge Devices
  > R/H SLAT TRACK #3 LOW AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA 5742-01028-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED RH #3 LOWER AFT SURFACE IAW ER/A 607445-14AD REV A & PRI 607445 REV 0 MATCH ASSOC
- [SDR DALA2024012200961](https://openairdocs.org/sdr/DALA2024012200961.md): Slat Track · corroded · Jan 16, 2024 · N137DU · Airbus BD5001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 6 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA 5742-01028-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED R/H SLAT TRACK #6 UPPER FWD SURFACE IAW ER/A 607445- 14AD REV A & PRI 607449
- [SDR DALA2024012200960](https://openairdocs.org/sdr/DALA2024012200960.md): Slat Track · corroded · Jan 16, 2024 · N137DU · Airbus BD5001A10 · Leading Edge Devices
  > L/H SLAT TRACK #1 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF AA5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED L/H SLAT TRACK #1 UPPER FWD SURFACE IAW PRI 607449-14AD REV 0 AND ERA 607449-1
- [SDR DALA2024012200959](https://openairdocs.org/sdr/DALA2024012200959.md): Slat Track · corroded · Jan 16, 2024 · N137DU · Airbus BD5001A10 · Leading Edge Devices
  > L/H SLAT TRACK #2 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF AA5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED L/H SLAT TRACK #2 LOWER AFT SURFACE IAW PRI 607449-14AD REV 0 AND ERA 607449-1
- [SDR DALA2024012200958](https://openairdocs.org/sdr/DALA2024012200958.md): Slat Track · corroded · Jan 16, 2024 · N137DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK #2 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, AA 5742-10128-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIREED L/H SLAT TRACK #2 UPPER AFT SURFACE IAW ERA 607449- 14AD REV A AND PRI 607449-14AD
- [SDR DALA2024012200957](https://openairdocs.org/sdr/DALA2024012200957.md): Slat Track · corroded · Jan 16, 2024 · N137DU · Airbus BD5001A10 · Leading Edge Devices
  > L/H SLAT TRACK #4 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF AA5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED L/H SLAT TRACK #4 UPPER FWD SURFACE IAW PRI 607449-14AD REV 0 AND ERA 607449-1
- [SDR DALA2024012200956](https://openairdocs.org/sdr/DALA2024012200956.md): Slat Track · corroded · Jan 16, 2024 · N137DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK #4 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, AA 5742-10128-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED L/H SLAT TRACK #4 UPPER AFT SURFACE IAW ERA 607449-14AD REV A AND PRI 607449-14AD R
- [SDR DALA2024012200955](https://openairdocs.org/sdr/DALA2024012200955.md): Slat Track · corroded · Jan 16, 2024 · N137DU · Airbus BD5001A10 · Leading Edge Devices
  > L/H SLAT TRACK #5 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 02322997 W REPAIRED L/H SLAT TRACK #5 LOWER AFT SURFACE IAW PRI 607449-14AD
- [SDR DALA2024012200954](https://openairdocs.org/sdr/DALA2024012200954.md): Slat Track · corroded · Jan 16, 2024 · N137DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK #8 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, AA 5742-10128-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED LH SLAT TRACK #8 UPPER FWD IAW PRI 607449-14AD REV 0 AND ERA 607449-14AD REV A MATC
- [SDR DALA2024012200953](https://openairdocs.org/sdr/DALA2024012200953.md): Slat Track · corroded · Jan 16, 2024 · N137DU · Airbus BD5001A10 · Leading Edge Devices
  > L/H SLAT TRACK #8 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF AA5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED L/H SLAT TRACK #8 LOWER AFT SURFACE IAW PRI 607449-14AD REV 0 AND ERA 607449-1
- [SDR DALA2024012200952](https://openairdocs.org/sdr/DALA2024012200952.md): Slat Track · corroded · Jan 16, 2024 · N137DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK #6 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, AA 5742-10128-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED L/H SLAT TRACK #6 UPPER SURFACE IAW ERA 607449-14AD REV A AND PRI 607449-14AD REV 0
- [SDR DALA2024012200951](https://openairdocs.org/sdr/DALA2024012200951.md): Slat Track · corroded · Jan 16, 2024 · N137DU · Airbus BD5001A10 · Leading Edge Devices
  > L/H SLAT TRACK #9 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 02322997 W REPAIRED L/H SLAT TRACK #9 LOWER AFT SURFACE IAW PRI 607449-14AD
- [SDR DALA2024012200950](https://openairdocs.org/sdr/DALA2024012200950.md): Slat Track · corroded · Jan 16, 2024 · N137DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK #5 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, AA 5742-10128-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED L/H SLAT TRACK #5 UPPER FWD SURFACE IAW ERA607449-14AD REV A AND PRI 607449-14AD MA
- [SDR DALA2024012200949](https://openairdocs.org/sdr/DALA2024012200949.md): Slat Track · corroded · Jan 16, 2024 · N137DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK #5 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, AA 5742-10128-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. RII: N ENTR 01991231 W REPAIRED L/H SLAT TRACK #5 UPPER AFT SURFACE IAW ERA 607449-14A REV A
- [SDR DALA2024012200948](https://openairdocs.org/sdr/DALA2024012200948.md): Slat Track · corroded · Jan 16, 2024 · N137DU · Airbus BD5001A10 · Leading Edge Devices
  > L/H SLAT TRACK #10 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. AA5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED L/H SLAT TRACK #10 UPPER FWD SURFACE IAW PRI 607449- 14AD REV 0 AND ERA 607449-14
- [SDR DALA2024012200947](https://openairdocs.org/sdr/DALA2024012200947.md): Slat Track · corroded · Jan 16, 2024 · N137DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK #1 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, AA 5742-10128-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED L/H SLAT TRACK #1 UPPER AFT SURFACE PER ERA 607449-14A AND PRI 607449-14A REV 0 MAT
- [SDR DALA2024012200946](https://openairdocs.org/sdr/DALA2024012200946.md): Slat Track · corroded · Jan 16, 2024 · N137DU · Airbus BD5001A10 · Leading Edge Devices
  > L/H SLAT TRACK #9 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. AA5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED L/H SLAT TRACK #9 UPPER FWD SURFACE IAW PRI 607449-14AD REV 0 AND ERA 607449-14AD
- [SDR DALA2024012200945](https://openairdocs.org/sdr/DALA2024012200945.md): Slat Track · corroded · Jan 16, 2024 · N137DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK #10 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. AA 5742-10128-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED LH SLAT TRACK #10 LOWER AFT SURFACE IAW PRI 607449-14AD REV 0 AND ERA 607449-14AD
- [SDR DALA2024011100503](https://openairdocs.org/sdr/DALA2024011100503.md): Unknown · unknown · Jan 10, 2024 · N137DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > FOUND WTBF SUPPORT BEAM CLIP CRACKED. REMOVED SUPPORT BEAM + CLIP (R LARSON 437286) INSTALLED LONGERON ASSY REF A220 WORK CARD 5352-01038-05A C022383111-001, REINSTALLED ITEM 430 AND REPLACED CLIP C02383123-001. R/R # 3 RADIO ALTIMETER 5001277 ANTENNAS PER A22
- [SDR DALA2024011100502](https://openairdocs.org/sdr/DALA2024011100502.md): Unknown · unknown · Jan 10, 2024 · N137DU · Airbus BD5001A10 · Aerodynamic Fairings
  > WORKING AD RELATED WORK CARD 5352-01038-01B FOUND LONGERON P/N C02383111-001 AT LBL 4010 CRACKED FROM FRAME C02383123-001 TO FRAME C02383037-001 25" ALONG THE NUT PLATE FLANGE THEN VERTICAL 1.5" FROM FRAME 02383037-001 UP 2.25" FROM NUT PLATE FLANGE. REMOVED S
- [SDR DALA2023110309046](https://openairdocs.org/sdr/DALA2023110309046.md): Unknown · unknown · Nov 2, 2023 · N137DU · Airbus BD5001A10 · Air Distribution System
  > WHEN APU IS STARTED AND TAKES OVER A/C PACKS, WE GET A BAD DIRTY SOCKS SMELL. DURING INSPECTIONS FOUND APU STARTER ORING LEAKING. REPLACED PER A220 AMP 49-41 (AM 322087) LEAK CKS OK. REF LP 0046147 FOR NO GO ODI LOG. (LP# 9136834)
- [SDR DALA2023083007066](https://openairdocs.org/sdr/DALA2023083007066.md): Unknown · unknown · Aug 29, 2023 · N137DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > CORROSION ON WASTE BOX DOUBLER RIGHT SIDE AND AFT SIDE. -M-. 001-0244:2021-2025/001 00020 COMPLIED WITH ER/A 611382-14 PRI REV 0, ER/ A 611382-14 PRI REV 1, ER/A 611382-14 PRI REV 2 AND FINAL ER/A 611382-14 REV OR IGINAL. CLOSING REQUIREMENTS RII: INSPECTOR 00
- [SDR DALA2026061103540](https://openairdocs.org/sdr/DALA2026061103540.md): None · none · Aug 23, 2023 · N137DU · Airbus BD5001A10 · Standard Practices/Structures
  > ERA 611382-14 SECTION I ACCOMPLISHED IN MSP DURING CCK AUG 2023. FOLLOW ON ACTION IS REQUIRED. REPAIR WAS TO WASTE BOX AREA. ACCOMPLISH ERA 611382-14 SECTION II EVERY 850 FH AFTER SECTION I AND SECTION III WITHIN 8000 FH AFTER SECTION I. ASSOCIATED ER/A 14-611

Next page: https://openairdocs.org/aircraft/N137DU/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 = 'N137DU' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N137DU/reports

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