# Service difficulty reports: N127DU

A list on [N127DU](https://openairdocs.org/aircraft/N127DU.md).

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

- [SDR DALA2025080705927](https://openairdocs.org/sdr/DALA2025080705927.md): Skin · gouged · Aug 4, 2025 · N127DU · Airbus BD5001A10 · Service Doors
  > AFT SERVICE DOOR- EXTERIOR SKIN HAS 2 SMALL GOUGES AT THE DOOR HANDLE CUTOUT FROM THE HANDLE CONTACTING THE SKIN. "M" SEE PIC. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0819:5246-2004/002 00275 REPAIRED PER PRIS
- [SDR DALA2025072905701](https://openairdocs.org/sdr/DALA2025072905701.md): Door Sill · corroded · Jul 29, 2025 · N127DU · Airbus BD5001A10 · Fuselage Main, Structure
  > AIRCRAFT AFT SERVICE DOOR SILL, BOLT HOLE #4 HAS CORROSION EMITTING FROM IT. (P)(M). SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0546:5360-2024/002 00539 REMOVED AND REPLACED FORWARD CORNER STRIKER REF A220 ASRP 52-42-21. (LP# 1112326)
- [SDR DALA2025072905697](https://openairdocs.org/sdr/DALA2025072905697.md): Duct · damaged · Jul 24, 2025 · N127DU · Airbus BD5001A10 · APU Bleed Air System
  > APU HIGH PRESSURE BLEED DUCT HAS PLY SEPARATION AT FIRE LOOP STANDOFF, 10 INCHES FWD OF FRAME 85. PER AMDS, REQUIRES CUSTOMER RESPONSE CENTER NOTIFICATION. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 066-0001:3610-2002
- [SDR DALA2025072205496](https://openairdocs.org/sdr/DALA2025072205496.md): Seat Track · corroded · Jul 20, 2025 · N127DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > REAR BARREL SEAT TRACKS. AT LH FR 71 IB MULTIPLE AREAS OF CORROSION ON THE SEAT TRACK. REPLACED SEAT TRACK REF. A220 ASRP 51-42-00 AND A220 DWG C01342700. (LP# 1095019)
- [SDR DALA2025072205495](https://openairdocs.org/sdr/DALA2025072205495.md): Seat Track · corroded · Jul 20, 2025 · N127DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > REAR BARREL SEAT TRACKS. AT LH FR 71 OB MULTIPLE AREAS OF CORROSION ON THE SEAT TRACK (M). REPLACED SEAT TRACK REF. A220 DWG C01342700 AND A220 ASRP 51-42-00. (LP# 1095032)
- [SDR DALA2025072205494](https://openairdocs.org/sdr/DALA2025072205494.md): Seat Track · corroded · Jul 20, 2025 · N127DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > REAR BARREL SEAT TRACKS. AT RH FR 71 OB MULTIPLE AREAS OF CORROSION ON THE SEAT TRACK (M). REPLACED SEAT TRACK REF. A220 ASRP 51-42-00 AND A220 DWG C01342700.
- [SDR DALA2025072205493](https://openairdocs.org/sdr/DALA2025072205493.md): Seat Track · corroded · Jul 19, 2025 · N127DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > REAR BARREL SEAT TRACKS. AT RH FR 71 IB MULTIPLE AREAS OF CORROSION ON THE SEAT TRACK (M). SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0584:5300-2015/002 00502 REPLACED SEAT TRACK REF. A220 DWG C01342700 AND A220 A
- [SDR DALA2025070104903](https://openairdocs.org/sdr/DALA2025070104903.md): Slide · no discrepancy · Jun 26, 2025 · N127DU · Airbus BD5001A10 · Escape Slide
  > LH OWEED SLIDE REQUIRES DEPLOYMENT REF AMDS 2561-9101. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0402:2561-9101/001 00003 DEPLOYED SLIDE PER AMDS 2561-9005 STEP 1-4. SLIDE INSTALL WILL BE COMPLETED ON THE REMAIND
- [SDR DALA2025070104895](https://openairdocs.org/sdr/DALA2025070104895.md): Slide · no discrepancy · Jun 26, 2025 · N127DU · Airbus BD5001A10 · Escape Slide
  > RH OWEED SLIDE REQUIRES DEPLOYMENT REF AMDS 2561-9101. DEPLOYED SLIDE PER AMDS 2561-9006 STEP 1-4. SLIDE INSTALL WILL BE COMPLETED ON THE REMAINDER OF AMDS 2561-9006. (LP# 1047913)
- [SDR DALA2024121111657](https://openairdocs.org/sdr/DALA2024121111657.md): Light · inoperative · Dec 8, 2024 · N127DU · Airbus BD5001A10 · Emergency Lighting
  > RT EXTERNAL REAR EMERGENCY LIGHT INOP. REMOVED AND REPLACED R/H AFT EXTERNAL LIGHT ASSEMBLY. OPS CHECKS GOOD REF A220 AMP 33-55.
- [SDR DALA2024120511474](https://openairdocs.org/sdr/DALA2024120511474.md): Fan · abnormal · Dec 1, 2024 · N127DU · Airbus BD5001A10 · Air Distribution Fan
  > RECIRC AIR FAIL MSG DURING ENG START FA IN AFT GALLEY REPORTED ELECTRICAL SMELL AT SAME TIME. R/R BOTH RECIRC FILTERS PER A220 AMP 21-22-03. REMOVED RECIRC FAN PER A220 AMP 21-22-01. INSTALLED PER A220 AMP 21-22. NO HELP. T/S PER EFIM INSTALLED DCM 1A SLOT 567
- [SDR DALA2024082208371](https://openairdocs.org/sdr/DALA2024082208371.md): Slat Track · corroded · Aug 21, 2024 · N127DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NUMBER 4 PINION TEETH (2EA) HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-010287-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 21AUG24 2157 UTC 02 CORR BY MUNOZ 02379974 IAH 21AUG24 ATA 5742
- [SDR DALA2024082208370](https://openairdocs.org/sdr/DALA2024082208370.md): Slat Track · corroded · Aug 21, 2024 · N127DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 4 UPPER AFT I/B SIDE HAS EVIDENCE OF A ROLLER WEAR MARK WITH REWORK REF 5742-01028-02B. MEASUREMENT DEPTH IS 0.011", OUTSIDE OF SPECIFIED RESTRICTIONS. LIAISON ENGINEERING WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED RH SLAT TRACK #4 UPPE
- [SDR DALA2024082208369](https://openairdocs.org/sdr/DALA2024082208369.md): Slat Track · corroded · Aug 21, 2024 · N127DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NUMBER 4 RACK TEETH (2EA) HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 21AUG24 2204 UTC 02 CORR BY MUNOZ 02379974 IAH 21AUG24 ATA 5742 RII
- [SDR DALA2025070204956](https://openairdocs.org/sdr/DALA2025070204956.md): Tape · peeling · Aug 19, 2024 · N127DU · Airbus BD5001A10 · Wing Miscellaneous Structure
  > LH WINGLET TIP LEADING EDGE EROSION TAPE FOUND PEELED UP. REQUIRES REPAIR. INSPECTED LH WINGLET TIP L E WHERE EROSION TAPE WAS DAMAGED & FOUND NO UNDERLYING DAMAGE. TRIMMED OFF EXCESS EROSION BOOT MATERIAL TO MEET AERODYNAMIC SMOOTHNESS IAW ASRP 55-32-01-01AAA
- [SDR DALA2024052805555](https://openairdocs.org/sdr/DALA2024052805555.md): Landing Gear · faulted · May 23, 2024 · N127DU · Airbus BD5001A10 · Landing Gear Retraction/Extension System
  > SHIP 8127 - MISC/DE - DECLARED EMERGENCY DUE TO GEAR FAIL MSG. CREW DID RECEIVE ALL 3 GEARS DOWN AND LOCKED INDICATING GREEN. FLIGHT LANDED SAFELY. CORRECTIVE ACTION: R/R LGCL PER A220 AMP 32-31-07. PERFORMED ALTERNATE GEAR EXTENSION CHECK ON LGSCU 1A AND 2A P
- [SDR DALA2025070805079](https://openairdocs.org/sdr/DALA2025070805079.md): Tape · peeling · Mar 10, 2024 · N127DU · Airbus BD5001A10 · Vertical Stabilizer
  > ON WALK AROUND FOUND VERT STAB EROSION TAPE PEELED. GVI OF PAINT OK. FWD TO MON IAW A220 ASRP 55-32-01-01AAA-662A-A FOR 8500 FLT HRS. GVI DUE IN 850 FLT HRS. PERFORMED GVI IAW A220 ASRP 51-10-01-01AAA- 018A-A. NO FURTHER DEFECTS FOUND. OK TO CONT. ON MON.REMOV
- [SDR DALA2024010310787](https://openairdocs.org/sdr/DALA2024010310787.md): Unknown · unknown · Dec 30, 2023 · N127DU · Bombdr BD1001A10 · Leading Edge Devices
  > L/H SLAT TRACK NBR 10 LOWER SURFACE HAS EVIDENCE OF CORROSION & PREVIOUS REWORK. REF AA6742-01028-02A. LIAISON ENGINEERING WILL. REPAIRED L/H SLAT TRACK NBR 10 LOWER SURFACE PER ER/A 607781- 14AD REV A AND PRI REV 0. (LP# 0131986)
- [SDR DALA2024010310786](https://openairdocs.org/sdr/DALA2024010310786.md): Unknown · unknown · Dec 30, 2023 · N127DU · Bombdr BD1001A10 · Leading Edge Devices
  > L/H SLAT TRACK NBR 1 UPPER SURFACE HAS EVIDENCE OF CORROSION & NO EVIDENCE OF PREVIOUS REWORK REF AA 5742-01028-02A LIASON ENGINEERING SUPPORT WILL BE REQ'D BEFORE FURTHER FLT. REPAIRED L/H SLAT TRACK NBR 1 UPPER SURFACE PER ER/A 607781-14AD REV A AND PRI REV
- [SDR DALA2024010310785](https://openairdocs.org/sdr/DALA2024010310785.md): Unknown · unknown · Dec 30, 2023 · N127DU · Bombdr BD1001A10 · Leading Edge Devices
  > L/H SLAT TRACK # 7 LOWER AFT SURFACE HAS WEAR AND PREVIOUSLY REWORK. REF AA5742-01028-02A. LIASON ENGINEERING WILL BE REQ'D BEFORE FURTHER FLT. REPAIRED L/H SLAT TRACK NBR 7 LOWER AFT SURFACE PER ER/A 607781- 14AD REV A AND PRI REV 0. (LP# 0131992)
- [SDR DALA2024010310784](https://openairdocs.org/sdr/DALA2024010310784.md): Unknown · unknown · Dec 30, 2023 · N127DU · Bombdr BD1001A10 · Leading Edge Devices
  > L/H SLAT TRACK NBR 8 UPPER SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF AA 5742-01028-02A. LIASON ENGINEERING SUPPORT WILL BE REQ'D BEFORE FURTHER FLT. REPAIRED LH SLAT TRACK NBR 8 UPPER SURFACE PER ER/A 607781-14AD REV A AND PRI REV 0. (LP# 0131
- [SDR DALA2024010310783](https://openairdocs.org/sdr/DALA2024010310783.md): Unknown · unknown · Dec 30, 2023 · N127DU · Bombdr BD1001A10 · Leading Edge Devices
  > L/H SLAT TRACK NBR 7 UPPER SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA 5742-01028-02A. LIASON ENGINEERING SUPPORT WILL BE REQ'D BEFORE FURTHER FLT. REPAIRED L/H SLAT TRACK NBR 7 UPPER SURFACE PER ER/A 607781-14AD REV A AND PRI REV 0. (LP# 0131
- [SDR DALA2024010310782](https://openairdocs.org/sdr/DALA2024010310782.md): Unknown · unknown · Dec 30, 2023 · N127DU · Bombdr BD1001A10 · Leading Edge Devices
  > L/H SLAT TRACK NBR 2 UPPER SURFACE HAS EVIDENCE OF CORROSION NO EVIDENCE OF PREVIOUS REWORK REF AA 5742-01028-02A LIASON ENGINEERING SUPPORT WILL BE REQ'D BEFORE FURTHER FLT. REPAIRED L/H SLAT TRACK NBR 2 UPPER SURFACE PER ER/A 607781-14AD REV A AND PRI REV 0.
- [SDR DALA2024010310781](https://openairdocs.org/sdr/DALA2024010310781.md): Unknown · unknown · Dec 30, 2023 · N127DU · Bombdr BD1001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 6 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION WITH PREVIOUS RE-WORK. REF. 5742-01028-02B LIASON ENGINEERING SUPPORT WILL BE REQ'D BEFORE FURTHER FLT. REPAIRED RH SLAT TRACK NDR 6 UPPER AFT SURFACE PER ER/A 607782- 14AD REV B AND PRI REV 0. (
- [SDR DALA2024010310780](https://openairdocs.org/sdr/DALA2024010310780.md): Unknown · unknown · Dec 30, 2023 · N127DU · Bombdr BD1001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 10 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION WITH PREVIOUS REWORK REF. 5742-01028-02B LIASON ENGINEERING SUPPORT WILL BE REQ'D BEFORE FURTHER FLT. REPAIRED RH SLAT TRACK #10 UPPER AFT SURFACE PER ER/A 607782- 14AD REV B AND PRI REV 0. (LP#
- [SDR DALA2023051203780](https://openairdocs.org/sdr/DALA2023051203780.md): Unknown · unknown · May 11, 2023 · N127DU · Bombdr BD1001A10 · Air Conditioning System
  > WET SOCK SMELL NOTICED FROM PAX & CREW. C/W A220 NO-GO ODI 21-72. C/W W/C 0550-2001 +0550-6001. REF LOG 4086590 FOR FINDINGS. WHILE PERFORMING B.S.I. ON #2 ESN 736235 IAW AMDS 0550-6001 STEP (8), FOUND EVIDENCE OF OIL WETNESS @ HPC VARIABLE INLET GUIDE VANES.
- [SDR DALA2023041102849](https://openairdocs.org/sdr/DALA2023041102849.md): Unknown · unknown · Apr 8, 2023 · N127DU · Bombdr BD1001A10 · Leading Edge Devices
  > AIRCRAFT 8127, AD/ERA REQUIRES L/H WING SLAT RIGGING PER AMP 27-81-17, AND THE "SLAT CONTOUR CHECK" AS DESCRIBED IN OPTION #2. CORRECTIVE ACTION: ACCOMPLISHED L/H WING SLAT RIGGING PER A220 AMP 27-81-17, AND THE "SLAT CONTOUR CHECK" AS DESCRIBED IN OPTION #2.
- [SDR DALA2023041102848](https://openairdocs.org/sdr/DALA2023041102848.md): Unknown · unknown · Apr 8, 2023 · N127DU · Bombdr BD1001A10 · Leading Edge Devices
  > AIRCRAFT 8127, AD/ERA REQUIRES R/H WING SLAT RIGGING PER AMP 27-81-17, AND THE "SLAT CONTOUR CHECK" AS DESCRIBED IN OPTION #2. CORRECTIVE ACTION: ACCOMPLISHED L/H WING SLAT RIGGING PER A220 AMP 27-81-17 AND ERA 607782 AND THE "SLAT CONTOUR CHECK" AS DESCRIBED
- [SDR DALA2023041102847](https://openairdocs.org/sdr/DALA2023041102847.md): Unknown · unknown · Apr 8, 2023 · N127DU · Bombdr BD1001A10 · Wing Structure
  > AIRCRAFT 8127, ERA 607781-14AD SECTION I ISSUED FOR REPAIR TO LH SLAT TRACKS FOLLOW ON ACTION REQUIRED. CORRECTIVE ACTION: ERA 607781-14AD REV O SECTION I COMPLETED FOR L/H SLAT TRACK CORROSION REWORK. (TIME LIMITED REPAIR) RII STEP 3 WAS ACCOMPLISHED. (LP 270
- [SDR DALA2023020300859](https://openairdocs.org/sdr/DALA2023020300859.md): Not Entered · not entered · Feb 1, 2023 · N127DU · Bombdr BD1001A10 · Flight Control System
  > SHIP 8127 - DIV - TO LIT DUE TO "R ELEVATOR FAIL" CAUTION MESSAGE. CORRECTIVE ACTION: REPLACED #3 REU. (LP# 9432468)
- [SDR DALA2022110807220](https://openairdocs.org/sdr/DALA2022110807220.md): Hinge Bracket · cracked · Nov 5, 2022 · N127DU · Bombdr BD1001A10 · Horizontal Stabilizer, Spar/Rib
  > R/H HORIZONAL /ELEVATOR HINGE BRACKET # 3 CRACKED IN LWR AFT CORNER IN RADIUS.SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0260:2090-2039-RH/ 003 00114 COMPLIED WITH ER/A PRI 603293-14 REV. 1 AND FINAL ERA 603293-14 REV. ORIGINAL. C/W ERA PRI 603293-14 REV OR
- [SDR DALA2022110807219](https://openairdocs.org/sdr/DALA2022110807219.md): Hinge Bracket · cracked · Nov 5, 2022 · N127DU · Bombdr BD1001A10 · Horizontal Stabilizer, Spar/Rib
  > R/H HORIZONAL /ELEVATOR HINGE BRACKET # 2 CRACKED IN LWR AFT CORNER IN RADIUS.SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0260:2090-2039-RH/ 002 00113 COMPLIED WITH ER/A PRI 603292-14 REV. 1 AND FINAL ERA 603292-14 REV. ORIGINAL. C/W PRI 603292-14 REV ORIGIN
- [SDR DALA2022110407168](https://openairdocs.org/sdr/DALA2022110407168.md): Frame · corroded · Nov 3, 2022 · N127DU · Bombdr BD1001A10 · Fuselage Main, Frame
  > AIRCRAFT 8127, UPPER CORNER OF FRAME 75 HAS CORRODED SPOT FORWARD OF WASTE BOX. CORRECTIVE ACTION: REPLACED WASTE BOX PAN, INBD HINGE FITTINGS, INBD HINGE ARM FITTINGS, AND REMOVED CORROSION ON WASTE B=DOOR DOUBLER PER ER/A 603257-14. LP 2481206
- [SDR DALA2022110407167](https://openairdocs.org/sdr/DALA2022110407167.md): Pan · corroded · Nov 3, 2022 · N127DU · Bombdr BD1001A10 · Fuselage Miscellaneous Structure
  > AIRCRAFT 8127, CORROSION FOUND ON FORWARD EDGE OF LAV PAN, 2 LOCATIONS. CORRECTIVE ACTION: REPLACED WASTE BOX PAN, INBD HINGE FITTINGS, INBD HINGE ARM FITTINGS, AND REMOVED CORROSION ON WASTE B=DOOR DOUBLER PER ER/A 603257-14. LP 2481199
- [SDR DALA2022110407166](https://openairdocs.org/sdr/DALA2022110407166.md): Access Door · corroded · Nov 3, 2022 · N127DU · Bombdr BD1001A10 · Fluid Service Doors
  > AIRCRAFT 8127, CORROSION FOUND ON FWD EDGE OF LAV WASTE SERVICE DOOR (146 BR). CORRECTIVE ACTION: REPLACED WASTE BOX PAN, INBD HINGE FITTINGS, INBD HINGE ARM FITTINGS, AND REMOVED CORROSION ON WASTE B=DOOR DOUBLER PER ER/A 603257-14. LP 2481194
- [SDR DALA2022110407165](https://openairdocs.org/sdr/DALA2022110407165.md): Hinge · corroded · Nov 3, 2022 · N127DU · Bombdr BD1001A10 · Fuselage, Door Hinge
  > AIRCRAFT 8127, BOTH HINGES ON LAV WASTE SERVICE DOOR (146 BR) CORRODED. CORRECTIVE ACTION: REPLACED WASTE BOX PAN, INBD HINGE FITTINGS, INBD HINGE ARM FITTINGS, AND REMOVED CORROSION ON WASTE B=DOOR DOUBLER PER ER/A 603257-14. LP 2481191
- [SDR DALA2022110407164](https://openairdocs.org/sdr/DALA2022110407164.md): Pan · corroded · Nov 3, 2022 · N127DU · Bombdr BD1001A10 · Fuselage Miscellaneous Structure
  > AIRCRAFT 8127, SEVERAL AREAS CORRODED ON LAV PAN WASTE BOX (MARKED). CORRECTIVE ACTION: REPLACED WASTE BOX PAN, INBD HINGE FITTINGS, INBD HINGE ARM FITTINGS, AND REMOVED CORROSION ON WASTE B=DOOR DOUBLER PER ER/A 603257-14. LP 2481177
- [SDR DALA2022110407163](https://openairdocs.org/sdr/DALA2022110407163.md): Doubler · corroded · Nov 3, 2022 · N127DU · Bombdr BD1001A10 · Fluid Service Doors
  > AIRCRAFT 8127, CORROSION FOUND ON FWD SECTION OF THE WASTE ACCESS INTERNAL DOUBLER. CORRECTIVE ACTION: REPLACED WASTE BOX PAN, INBD HINGE FITTINGS, INBD HINGE ARM FITTINGS, AND REMOVED CORROSION ON WASTE B=DOOR DOUBLER PER ER/A 603257-14. LP 2481175
- [SDR DALA2023022801499](https://openairdocs.org/sdr/DALA2023022801499.md): None · none · Nov 1, 2022 · N127DU · Bombdr BD1001A10 · Fuselage Internal Mounting Structure
  > ERA 603257-14AD SECTION I ACCOMPLISHED IN MSPDURING C CHECK TO THE WASTE BOX AREA. FOLLOW ON ACTION IS REQUIRE. ACCOMPLISH ERA 603257-14AD SECTION II EVERY 850 FH AFTER SECTION I ACCOMPLISHMENT.ERA 603257-14AD SECTION I REPAIR IS ACCEPTABL E FOR 8500 FH. FURTH
- [SDR DALA2021091505503](https://openairdocs.org/sdr/DALA2021091505503.md): Radome · damaged · Sep 10, 2021 · N127DU · Airbus BD5001A10 · Aerodynamic Fairings
  > RADOME REPAIR PER ERA 588183-14. RADOME SKIN/CORE REPAIRED PER ERA 588183-14. REPETITIVE INSPECTION PER ERA 588183-14 SECTION II REQUIRED EVERY 850 HRS UNTIL ACCOMPLISHMENT OF PERMANENT REPAIR PER SECTION III AT 8500 HRS. ASSOCIATED ER/A 14-588183 ADDED. (LP#
- [SDR DALA2020101903384](https://openairdocs.org/sdr/DALA2020101903384.md): Bottle · low pressure · Oct 19, 2020 · N127DU · Bombdr BD1001A10 · Emergency Equipment
  > DURING SVC CK FOUND L2 DOOR EOAM PRESSURE LOW. SERVICED L2 DOOR EOAM PER A220 AMP 52-11. C/W RII VERIFIED DOOR SAFTY PIN STOWED PER A220 AMP 52-11.
- [SDR DALA2020101903385](https://openairdocs.org/sdr/DALA2020101903385.md): Bottle · low pressure · Oct 17, 2020 · N127DU · Bombdr BD1001A10 · Emergency Equipment
  > L1 DOOR EOAM IN YELLOW. SERVICED L1 DOOR EOAM PER A220 AMP 52-11. OK FOR SVC. C/W RII. VERIFIED DOOR SAFTY PIN STOWED PER A220 AMP 52-11.
- [SDR DALA2020020430875](https://openairdocs.org/sdr/DALA2020020430875.md): Bottle · low pressure · Jan 31, 2020 · N127DU · Bombdr BD1001A10 · Emergency Equipment
  > L-1 DOOR EOAM PSI BELOW MINIMUMS. ACTUATOR SAFETY PIN INSTALLED FOR MAINT. SERVICED L-1 DOOR EOAM ACTUATOR PER A220 AMP 52-11. COMPLIED WITH RII REQUIREMENTS PER A220 AMP BD500-A-J52-11-08-01AAA-214A-A. VERIFIED L1 DOOR ASSIST ACTUATOR REARMED AND SAFETY PIN R
- [SDR DALA2020012870629](https://openairdocs.org/sdr/DALA2020012870629.md): Damper · low pressure · Jan 27, 2020 · N127DU · Airbus BD5001A10 · Passenger/Crew Doors
  > L1 DOOR EOAM FORWARD PASSENGER DOOR DAMPER IS IN THE RED BAND REQUIRES RII AND SERVICING. SERVICED PASSENGER ENTRY DOOR L1 EOAM I.A.W CE SERIES AMP TASK BD500-A-J52-12-08-01AAA-21A-A. SERVICED TO GREEN BAND. (LP# 6527185)
- [SDR DALA2020012800631](https://openairdocs.org/sdr/DALA2020012800631.md): Fairing · cracked · Jan 22, 2020 · N127DU · Airbus BD5001A10 · Aerodynamic Fairings
  > DURING A CHECK FOUND BELLY FAIRING CRACKED AT MID E&E ACCESS DOOR. REMOVED LONGERON PER AMP 53-82. INSTALLED LONGERON TO AFT WTBF LH SUPPORT STRUCTURE P/N C02383111-0010DL PER ERA 583461-14 AND ASRP C SERIES 51-42 THIS IS PERMANENT REPAIR. (LP# 6527164)
- [SDR DALA2019110206394](https://openairdocs.org/sdr/DALA2019110206394.md): B-Nut · loose · Nov 2, 2019 · N127DU · Bombdr BD1001A10 · Extinguishing System
  > #2 ENG FIRE EXTINGUISHING HOSE B NUT LOSE AND TORQUE STRIPE BROKEN ON ENGINE CONNECTING SIDE OF THE HOSE. REPLACE HOSE ACCORDING TO AD RELATED TASK CARD 2620-01223-01B. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 024-0

## 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 = 'N127DU' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N127DU/reports

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