# N310DU: 2021 Airbus Canada LP BD-500-1A11

- Status: Valid registration
- Airframe: [Airbus Canada LP BD-500-1A11](https://openairdocs.org/model/airbus-canada-lp-bd-500-1a11) (registry code 1400015, 153 seats)
- Engine: [Pratt & Whitney PW1521G SERIE](https://openairdocs.org/engine/pratt-whitney-pw1521g-serie) (registry code 51763)
- Data sheets: [TCDS T00008NY](https://openairdocs.org/tcds/T00008NY) (Airbus Canada Limited Partnership) (OpenAirDocs)
- Serial number: 55142
- Year built: 2021
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 16, 2021
- Certificate issued: December 15, 2021
- Expires: December 31, 2028
- Mode S code: A3472F
- Registered owner: [Delta Air Lines Inc](https://openairdocs.org/faa-owner/DELTA%20AIR%20LINES%20INC)
- Location: [Atlanta, GA](https://openairdocs.org/faa-place/GA/Atlanta)
- Owner type: Corporation
- Owner's area on the map: 33.6604° N, 84.3865° W: Placed by OpenAirDocs at the center of ZIP code 30354, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=310DU
- Page: https://openairdocs.org/aircraft/N310DU

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 71 in force

### Matched by airframe (Airbus Canada LP BD-500-1A11)

- [AD 2026-15-14](https://openairdocs.org/ad/2026-15-14): Engine fuel and control · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Sep 3, 2026
- [AD 2026-13-52](https://openairdocs.org/ad/2026-13-52): Pneumatic · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jul 7, 2026
- [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026
- [AD 2026-10-12](https://openairdocs.org/ad/2026-10-12): Fuel · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jul 1, 2026
- [AD 2026-10-10](https://openairdocs.org/ad/2026-10-10): Equipment/furnishings · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jul 1, 2026
- [AD 2026-10-07](https://openairdocs.org/ad/2026-10-07): Wings · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jul 1, 2026
- [AD 2026-07-04](https://openairdocs.org/ad/2026-07-04): Equipment/Furnishings · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective May 11, 2026
- [AD 2026-06-06](https://openairdocs.org/ad/2026-06-06): Electrical system installation · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective May 1, 2026
- [AD 2026-07-07](https://openairdocs.org/ad/2026-07-07): Air conditioning system · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Apr 17, 2026
- [AD 2026-04-04](https://openairdocs.org/ad/2026-04-04): Fuel · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Apr 8, 2026
- [AD 2025-20-08](https://openairdocs.org/ad/2025-20-08): Fire protection · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Dec 30, 2025
- [AD 2025-19-07](https://openairdocs.org/ad/2025-19-07): Electrical system installation · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Nov 6, 2025
- [AD 2025-19-01](https://openairdocs.org/ad/2025-19-01): Autoflight · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Oct 23, 2025
- [AD 2025-17-01](https://openairdocs.org/ad/2025-17-01): Flight controls · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Sep 29, 2025
- [AD 2025-16-01](https://openairdocs.org/ad/2025-16-01): Fuel · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Sep 18, 2025
- [AD 2025-12-04](https://openairdocs.org/ad/2025-12-04): Hydraulic Power · Airbus Canada Limited Partnership BD-500-1A11. Effective Jul 25, 2025
- [AD 2025-09-02](https://openairdocs.org/ad/2025-09-02): Landing Gear · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jun 18, 2025
- [AD 2025-11-06](https://openairdocs.org/ad/2025-11-06): Standard practices/structures · Airbus Canada Limited Partnership BD-500-1A11. Effective Jun 16, 2025
- [AD 2025-07-04](https://openairdocs.org/ad/2025-07-04): Standard practices/structures · Airbus Canada Limited Partnership BD-500-1A11. Effective May 27, 2025
- [AD 2025-06-06](https://openairdocs.org/ad/2025-06-06): Fuselage · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective May 2, 2025
- [AD 2025-05-07](https://openairdocs.org/ad/2025-05-07): Standard practices/structures · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Apr 15, 2025
- [AD 2025-02-06](https://openairdocs.org/ad/2025-02-06): Fuselage · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Apr 9, 2025
- [AD 2025-03-05](https://openairdocs.org/ad/2025-03-05): Stabilizers · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Mar 21, 2025
- [AD 2024-24-08](https://openairdocs.org/ad/2024-24-08): Equipment/Furnishings · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jan 13, 2025
- [AD 2024-23-05](https://openairdocs.org/ad/2024-23-05): Fuel · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jan 6, 2025
- [AD 2024-22-01](https://openairdocs.org/ad/2024-22-01): Time Limits/Maintenance Checks · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Dec 31, 2024
- [AD 2024-22-04](https://openairdocs.org/ad/2024-22-04): Fuselage · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Dec 17, 2024
- [AD 2024-22-03](https://openairdocs.org/ad/2024-22-03): Electrical Power · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Nov 14, 2024
- [AD 2024-15-06](https://openairdocs.org/ad/2024-15-06): Equipment/furnishings · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Oct 15, 2024
- [AD 2024-17-04](https://openairdocs.org/ad/2024-17-04): Landing Gear · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Sep 20, 2024
- [AD 2024-12-02](https://openairdocs.org/ad/2024-12-02): Portable Oxygen System · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Aug 13, 2024
- [AD 2024-09-01](https://openairdocs.org/ad/2024-09-01): Equipment/Furnishings · Airbus Canada Limited Partnership BD-500-1A11. Effective Jul 2, 2024
- [AD 2024-10-11](https://openairdocs.org/ad/2024-10-11): Doors · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jul 1, 2024
- [AD 2024-10-03](https://openairdocs.org/ad/2024-10-03): Flight Controls · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jun 28, 2024
- [AD 2024-07-11](https://openairdocs.org/ad/2024-07-11): Equipment/furnishings · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jun 6, 2024
- [AD 2024-05-10](https://openairdocs.org/ad/2024-05-10): Electrical Power · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective May 22, 2024
- [AD 2024-05-08](https://openairdocs.org/ad/2024-05-08): Flight Controls · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective May 22, 2024
- [AD 2024-04-08](https://openairdocs.org/ad/2024-04-08): Electrical power · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Apr 23, 2024
- [AD 2024-03-09](https://openairdocs.org/ad/2024-03-09): Equipment/furnishings · Airbus Canada Limited Partnership BD-500-1A11. Effective Apr 16, 2024
- [AD 2023-24-01](https://openairdocs.org/ad/2023-24-01): Fuel · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jan 2, 2024
- [AD 2023-20-01](https://openairdocs.org/ad/2023-20-01): Fire protection · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Nov 9, 2023
- [AD 2023-16-03](https://openairdocs.org/ad/2023-16-03): Pneumatic · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Sep 25, 2023
- [AD 2023-16-02](https://openairdocs.org/ad/2023-16-02): Fuel · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Sep 22, 2023
- [AD 2023-12-09](https://openairdocs.org/ad/2023-12-09): Flight control system · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Aug 7, 2023
- [AD 2023-14-02](https://openairdocs.org/ad/2023-14-02): Navigation · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jul 27, 2023
- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 2023-07-01](https://openairdocs.org/ad/2023-07-01): Turbine/turboprop engine · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Apr 19, 2023
- [AD 2022-26-06](https://openairdocs.org/ad/2022-26-06): Placards and markings · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Feb 2, 2023
- [AD 2022-25-19](https://openairdocs.org/ad/2022-25-19): Hardware, Engine Exhaust · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jan 23, 2023
- [AD 2022-25-05](https://openairdocs.org/ad/2022-25-05): Wings · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jan 23, 2023

### Matched by engine (Pratt & Whitney PW1521G SERIE)

None in force.

### Historical (superseded or no longer in force)

- [AD 2025-06-01](https://openairdocs.org/ad/2025-06-01) (historical): Turbine/turboprop engine · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Apr 22, 2025
- [AD 2024-04-11](https://openairdocs.org/ad/2024-04-11) (historical): Electrical Power · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective May 1, 2024
- [AD 2024-04-06](https://openairdocs.org/ad/2024-04-06) (historical): Fuel · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Apr 22, 2024
- [AD 2023-05-08](https://openairdocs.org/ad/2023-05-08) (historical): Time Limits/Maintenance Checks · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective May 12, 2023
- [AD 2022-25-51](https://openairdocs.org/ad/2022-25-51) (historical): Autoflight · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Dec 27, 2022
- [AD 2022-19-09](https://openairdocs.org/ad/2022-19-09) (historical): Landing Gear · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Oct 27, 2022
- [AD 2021-09-03](https://openairdocs.org/ad/2021-09-03) (historical): Equipment/furnishings · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective May 4, 2021
- [AD 2021-04-05](https://openairdocs.org/ad/2021-04-05) (historical): Time Limits/Maintenance Checks · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Mar 30, 2021
- [AD 2019-23-15](https://openairdocs.org/ad/2019-23-15) (historical): Time Limits/ Maintenance Checks · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jan 16, 2020
- [AD 2018-25-04](https://openairdocs.org/ad/2018-25-04) (historical): Cargo and accessory compartment · C Series Aircraft Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jan 14, 2019

All 81: https://openairdocs.org/aircraft/N310DU/ads.md

## Information bulletins (advisory) (1 in force)

- [SAIB NE-19-03](https://openairdocs.org/saib/NE-19-03): Escape Slide Maintenance Tasks and Intervals - JASC 2565. Issued Feb 19, 2019

## NTSB investigations

None matched to N310DU.

## FAA accident and incident reports

None matched to N310DU.

## Service difficulty reports (59, newest 50)

As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR DALA2026100705542](https://openairdocs.org/sdr/DALA2026100705542), Oct 5, 2026: FLOOR PANEL. CORRODED. R1 DOOR FLOOR PANEL# 222KRF HAS CORROSION. REMOVED AND REPLACED R1 DOOR FLOOR PANEL# 222KRF IAW A220 AMP BD500-A-J53-00-47-12AAA-520A-A AND A220 AMP BD500-A-J53
- [SDR DALA2026100705539](https://openairdocs.org/sdr/DALA2026100705539), Oct 3, 2026: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT AT FR20, RBL 33 HAS CORROSION. REPLACED FLOOR SUPPORT AT PASSENGER CABIN FR20 , RBL33 FOR A SERVICEABLE PART PER ASRP BD500-A-J51-42-21- 00AAA-078
- [SDR DALA2026100505498](https://openairdocs.org/sdr/DALA2026100505498), Sep 30, 2026: BRACKET. CORRODED. CORROSION G4 BRACKET AT LBL 1, FR 76-78 HAS CORROSION (MARKED). C/W ER/A 637185-14 REV ORIGINAL ASSOCIATED ER/A 14-637185 ADDED FOR AC 8310. (LP# 1840747; AIRCR
- [SDR DALA2026100505497](https://openairdocs.org/sdr/DALA2026100505497), Sep 29, 2026: FRAME. CORRODED. CORROSION, SECTION 48 FRAME HAS EVIDENCE OF CORROSION AT FR 81 STGR 19L. REMOVED AND REPLACED CENTER SECTION FRAME AT FR 81 PER A220 ASRP BD500-A-J51-42-20-00AA
- [SDR DALA2026093005435](https://openairdocs.org/sdr/DALA2026093005435), Sep 28, 2026: WEB. CORRODED. AFT OF R2 DOOR, FLOOR STRUCTURE WEB HAS CORROSION AT FR 76-79. REMOVED AND REPLACED FLOOR STRUCTURE WEB AFT OF R2 DOOR BETWEEN FR 76-79 IAW A220 ASRP BD500-A-J5
- [SDR DALA2026093005433](https://openairdocs.org/sdr/DALA2026093005433), Sep 26, 2026: SEAT TRACK. CORRODED. RT INBOARD SEAT TRACK AT RBL 23, FR74 CORRODED. REMOVED AND REPLACED RT INBD SEAT TRACK AT RBL 23 BETWEEN FR 61 TO FR 74 PER DWG PL C01342701 REV-G AND ASRP BD5
- [SDR DALA2026092805392](https://openairdocs.org/sdr/DALA2026092805392), Sep 25, 2026: SEAT TRACK. CORRODED. OUTBOARD RT SEAT TRACK AT FR 20, RBL 43.5 WAS CORRODED. REMOVED AND REPLACED THE FWD RT SEAT TRACK, FR 20 - 30 IAW DWG PL C02312600, REV K, AND ASRP BD500-A-51-
- [SDR DALA2026092805389](https://openairdocs.org/sdr/DALA2026092805389), Sep 25, 2026: SEAT TRACK. CORRODED. RIGHT OTBD SEAT TRACK CORRODED. RBL 43.5, FR 74. R & R THE RT SEAT TRACK, FR 61 - 74 IAW DWG PL C01342701, REV G AND ASRP BD500-A-J51-42-20-00AAA-078A-A. (LP 18
- [SDR DALA2026092805388](https://openairdocs.org/sdr/DALA2026092805388), Sep 24, 2026: SUPPORT. CORRODED. SUPPORT, LAV E HAD CORROSION IN FASTENER HOLES, LBL 11, FR 76-79, WL147. REMOVED AND REPLACED THE LAV SUPPORT IAW ASRP BD500-J51-42-21-00AAA-078A-A, & DWG PL C0
- [SDR DALA2026092805387](https://openairdocs.org/sdr/DALA2026092805387), Sep 24, 2026: SEAT TRACK. CORRODED. LEFT OTBD SEAT TRACK CORRODED, LBL 43.50, FR 74. FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED THE SEAT TRACK IAW ASRP BD500-A-J53-61-49-00AAA -661A-A, ASRP B
- [SDR DALA2026092805385](https://openairdocs.org/sdr/DALA2026092805385), Sep 24, 2026: WEB. CORRODED. AFT OF L2 DOOR, FLOOR WEB WAS CORRODED, FR 76 - 79. EVALUATED DAMAGE ON FLOOR WEB AND FOUND OUT OF LIMITS, NO DAMAGE PERMITTED IAW ASRP BD500-A-J51-10-06- 00AAA
- [SDR DALA2026092805384](https://openairdocs.org/sdr/DALA2026092805384), Sep 23, 2026: SEAT TRACK. CORRODED. INBOARD RT SEAT TRACK AT FR20, RBL 23 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW ASRP BD500-A-J51-42-20-00AAA-078A-A, AND DWG PL C02312600, REV K. (LP 18
- [SDR DALA2026092805383](https://openairdocs.org/sdr/DALA2026092805383), Sep 23, 2026: SUPPORT BEAM. CORRODED. RIGHT OTBD SUPPORT BEAM CORRODED AT FR 76-78, RBL 36.5, WL 147 IN THE NUT PLATE HOLE. REMOVED AND REPLACED THE SUPPORT BEAM IAW ASRP BD500-A-J51-42-21-00AAA-078
- [SDR DALA2026100705541](https://openairdocs.org/sdr/DALA2026100705541), Sep 22, 2026: FLOOR PANEL. CORRODED. L1 DOOR FLOOR PANEL# 221KLF HAS CORROSION. REMOVED AND REPLACED L1 DOOR FLOOR PANEL #221KLF IAW A220 AMP BD500-A-J53-00-47-11AAA-720A-A. (LP# 1849920; AIRCRAFT 
- [SDR DALA2026092805382](https://openairdocs.org/sdr/DALA2026092805382), Sep 22, 2026: SEAT TRACK. CORRODED. LEFT INBD SEAT TRACK AT LBL 23, FR74, CORRODED. REMOVED AND REPLACED THE SEAT TRACK BTWN LBL 23, FR 74 - 61 IAW ASRP BD500-A-J51-42-20-00AAA-078A-A, & DWG C0134
- [SDR DALA2026080904592](https://openairdocs.org/sdr/DALA2026080904592), Aug 8, 2026: SKIN. CORRODED. DURING CCK IN MSP, MAINTENANCE WAS ACCOMPLISHING ROUTINE CARD 2021-2025 AND FOUND CORROSION COMMON TO THE AFT WASTE SERVICE DOOR AREA. CORROSION IS COMMON TO TH
- [SDR DALA2026082504824](https://openairdocs.org/sdr/DALA2026082504824), Aug 7, 2026: SKIN. CORRODED. ER/A 618056-14 REV A ISSUED FOR CORROSION REPAIR TO THE LOWER AF T FUSELAGE SKIN AND WASTE BOX AREA. FOLLOW ON ACTION IS REQUIRED. ERA 618056-14 REV A SECT. IV 
- [SDR DALA2025122909486](https://openairdocs.org/sdr/DALA2025122909486), Dec 28, 2025: O-RING. CONTAMINATED. AIRCRAFT 8310, FA'S REPORTED A CHEMICAL SMELLING SMOKE IN AFT GALLEY. THE SMOKE AND SMELL WENT TO THE EMERGENCY ROW AND EVENTUALLY THE CABIN. FA'S DONNED MASK. 
- [SDR DALA2025091806866](https://openairdocs.org/sdr/DALA2025091806866), Sep 13, 2025: TRANSCEIVER. FAILED. ATB DUE TO WEATHER RADAR FAIL ADVISORY. REMOVED AND REPLACED WEATHER RADAR ANTENNA, OPS CHECK GOOD ACFT OK FOR SERVICE. (LP 7876389)
- [SDR DALA2025081906210](https://openairdocs.org/sdr/DALA2025081906210), Aug 13, 2025: LEVER. OVERROTATED. DUE TO DELAY TAKEN FOR AFT LEFT DOOR EOAM MODE SELECT LEVER BEING FOUND IN THE OVER-CENTERED POSITION PLZ SETUP TO CHECK THE RIGGING OF THE EOAM TRIGGER PER A22
- [SDR DALA2025042403238](https://openairdocs.org/sdr/DALA2025042403238), Apr 22, 2025: ENGINE. FAULTED. 75 R ENGINE FAULT - BAV INOP IN FLIGHT BETWEEN 11,000 AND LANDING. BRIEF OILY SMELL @ 11,000FT, MSG CONTINUED TILL AFTER LANDING. T/S PER A220 EFIM FAULT CODE 7
- [SDR DALA2024121711790](https://openairdocs.org/sdr/DALA2024121711790), Dec 11, 2024: SLAT TRACK. NO DISCREPANCY. RH SLAT TRACK NBR 8 UPPER FWD SURFACE REQUIRES NDT INSPECTION PER AMDS W/C 5742-01029-02B. PERFORMED EDDY CURRENT INSPECTION R/H SLAT TRACK #8 UPPER FWD SURFACE
- [SDR DALA2024121711787](https://openairdocs.org/sdr/DALA2024121711787), Dec 11, 2024: SLAT TRACK. NO DISCREPANCY. LH SLAT TRACK NBR 1 UPPER AFT SURFACE REQUIRES NDT INSPECTION PER AMDS W/C 5742-01029-02A. PERFORMED EDDY CURRENT INSPECTION L/H #1 SLAT TRACK UPPER AFT SURFACE
- [SDR DALA2024121711791](https://openairdocs.org/sdr/DALA2024121711791), Dec 10, 2024: SLAT TRACK. NO DISCREPANCY. RH SLAT TRACK NBR 2 UPPER FWD SURFACE REQUIRES NDT INSPECTION PER AMDS W/C 5742-01029-02B. PERFORMED EDDY CURRENT INSPECTION R/H #2 SLAT TRACK UPPER SURFACE PER
- [SDR DALA2024121711789](https://openairdocs.org/sdr/DALA2024121711789), Dec 10, 2024: SLAT TRACK. NO DISCREPANCY. LH SLAT TRACK NBR 4 UPPER AFT SURFACE REQUIRES NDT INSPECTION PER AMDS W/C 5742-01029-02A. PERFORMED EDDY CURRENT INSPECTION L/H #4 SLAT TRACK UPPER AFT SURFACE
- [SDR DALA2024121711788](https://openairdocs.org/sdr/DALA2024121711788), Dec 10, 2024: SLAT TRACK. NO DISCREPANCY. RH SLAT TRACK NBR 5 UPPER FWD SURFACE REQUIRES NDT INSPECTION PER AMDS W/C 5742-01029-02A. PERFORMED EDDY CURRENT INSPECTION R/H #5 SLAT TRACK UPPER SURFACE PER
- [SDR DALA2024090408719](https://openairdocs.org/sdr/DALA2024090408719), Aug 30, 2024: COFFEEMAKER. ODOR. GALLEY AND LAST 4 ROWS OF CABIN. TURNED OFF GALLEY HEATER/FAN, OVENS AND ELECTRICAL OUTLETS. SMELL DID NOT DISSIPATE. REMOVED SCREWS FOR AFT GALLEY CEILING PANE
- [SDR DALA2024082808516](https://openairdocs.org/sdr/DALA2024082808516), Aug 24, 2024: THROTTLE. FAILED. DIV - TO LAX DUE TO "AUTOBRAKE FAIL" MESSAGE ON APPROACH. CORRECTIVE ACTION: DEFERRED AUTOBRAKE SYSTEM TO MEL 32-43-15; R/R THROTTLE QUADRANT ASSEMBLY.
- [SDR DALA2024052805554](https://openairdocs.org/sdr/DALA2024052805554), May 24, 2024: DOOR. CORRODED. LAV SERVICE PANEL - ACCESS DOOR HAS CORROSION AT INBD HINGE ATTACHMENT AREA. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATI
- [SDR DALA2024052805553](https://openairdocs.org/sdr/DALA2024052805553), May 24, 2024: WASTE BOX. CORRODED. LAV SERVICE PANEL - WASTE BOX HAS CORROSION ON LOWER FLANGE AREA AT AFT INBD CORNER. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL I
- [SDR DALA2024052805552](https://openairdocs.org/sdr/DALA2024052805552), May 24, 2024: WASTE BOX. CORRODED. LAV SERVICE PANEL - WASTE BOX HAS CORROSION ON LOWER AND UPPER FLANGE AREAS AT FWD INBD CORNER. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR A
- [SDR DALA2024051505239](https://openairdocs.org/sdr/DALA2024051505239), May 15, 2024: ISOLATOR. WORN. WORN ISOLATOR ITEM #11 WORN TO LIMITS ON LH WING RIB 6. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 100-0001:2820-0128
- [SDR DALA2024051505238](https://openairdocs.org/sdr/DALA2024051505238), May 14, 2024: CANISTER. GOUGED. RH WING FUEL TANK - AC BOOST PUMP CANISTER (P/N 9C207-1) IS GOUGED ON PIPE CONNECTION FLANGE. SEE PICS. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE 
- [SDR DALA2024051505237](https://openairdocs.org/sdr/DALA2024051505237), May 14, 2024: TEE FITTING. WORN. ON TEE ASSEMBLY LC1325-01AE (ITEM 9) CHECK VALVES WERE WORN BEYOND LIMITS. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION
- [SDR DALA2024051505236](https://openairdocs.org/sdr/DALA2024051505236), May 14, 2024: TEE FITTING. GOUGED. TEE ASSEMBLY LC1325-01AE (ITEM 9) GOUGED AT FLANGE END BEYOND LIMITS. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 101-
- [SDR DALA2024020701652](https://openairdocs.org/sdr/DALA2024020701652), Feb 3, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 5 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED RH SLAT TRACK NBR 5 LOWER AFT SURFACE IAW PRI 6
- [SDR DALA2024020701651](https://openairdocs.org/sdr/DALA2024020701651), Feb 3, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 4 LOWER OB SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED RH SLAT TRACK NBR 4 LOWER OB SIDE IAW PRI 608198-14
- [SDR DALA2024020701650](https://openairdocs.org/sdr/DALA2024020701650), Feb 3, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 4 RACK TOOTH NBR 2 SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED RH SLAT TRACK NBR 4 RACK TOOTH NBR 2 IAW
- [SDR DALA2024020701649](https://openairdocs.org/sdr/DALA2024020701649), Feb 3, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 4 PINION TOOTH HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED RH SLAT TRACK NBR 4 PINION TOOTH SURFACE IAW PRI 608
- [SDR DALA2024020701648](https://openairdocs.org/sdr/DALA2024020701648), Feb 3, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 9 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED RH SLAT TRACK NBR 9 UPPER AFT SURFACE IAW PRI 6
- [SDR DALA2024020701647](https://openairdocs.org/sdr/DALA2024020701647), Feb 3, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 8 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED RH SLAT TRACK NBR 8 UPPER AFT SURFACE IAW PRI 6
- [SDR DALA2024020701646](https://openairdocs.org/sdr/DALA2024020701646), Feb 3, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 7 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED RH SLAT TRACK NBR 7 UPPER AFT SURFACE IAW PRI 6
- [SDR DALA2024020701645](https://openairdocs.org/sdr/DALA2024020701645), Feb 3, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 6 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED RH SLAT TRACK NBR 6 UPPER AFT SURFACE IAW PRI 6
- [SDR DALA2024020701644](https://openairdocs.org/sdr/DALA2024020701644), Feb 3, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 5 UPPER FORWARD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED RH SLAT TRACK NBR 5 UPPER FORWARD SURFACE I
- [SDR DALA2024020701643](https://openairdocs.org/sdr/DALA2024020701643), Feb 3, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 4 UPPER OB AFT SIDE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK REF 5742-01028-02A. MEASURED RH SLAT TRACK NBR 4 UPPER AFT OB SIDE IAW PRI 608198
- [SDR DALA2024020701642](https://openairdocs.org/sdr/DALA2024020701642), Feb 3, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 4 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED RH SLAT TRACK NBR 4 UPPER AFT SURFACE IAW PRI 6
- [SDR DALA2024020701641](https://openairdocs.org/sdr/DALA2024020701641), Feb 3, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 4 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED RH SLAT TRACK NBR 4 LOWER AFT SURFACE IAW PRI 6
- [SDR DALA2024020701640](https://openairdocs.org/sdr/DALA2024020701640), Feb 3, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 3 UPPER FORWARD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED RH SLAT TRACK NBR 3 UPPER FORWARD SURFACE I
- [SDR DALA2024020701639](https://openairdocs.org/sdr/DALA2024020701639), Feb 3, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 2 UPPER FORWARD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED RH SLAT TRACK NBR 2 UPPER FORWARD SURFACE I
- [SDR DALA2024020701638](https://openairdocs.org/sdr/DALA2024020701638), Feb 3, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 1 UPPER FORWARD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. L REPAIRED RH SLAT TRACK NBR 1 UPPER FORWARD SURFACE

All 59: https://openairdocs.org/aircraft/N310DU/reports.md

## STCs that may be installed (OpenAirDocs) (13)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Airbus Canada LP BD-500-1A11)

- [STC ST04254NY](https://openairdocs.org/stc/ST04254NY): Installation of Viasat Satcom Software. ALOFT AeroArchitects
- [STC ST04818NY](https://openairdocs.org/stc/ST04818NY): Installation of a Passenger Seat Re-Pitch. ALOFT AeroArchitects
- [STC ST00030IB](https://openairdocs.org/stc/ST00030IB): Installation of Test Tech ELT. APTOZ EHF
- [STC ST11389DS](https://openairdocs.org/stc/ST11389DS): Installation of Delta Comfort Passenger Seating Section. Aircraft Systems and Manufacturing Inc
- [STC ST04803NY](https://openairdocs.org/stc/ST04803NY): Installation of a Panasonic Avionics In-Flight Entertainment System. Delta Engineering Coporation
- [STC ST00079IB](https://openairdocs.org/stc/ST00079IB): Integration of Halon-free Portable Fire Extinguisher HAFEX. UMLAUT ENGINEERING GMBH
- [STC ST00215IB](https://openairdocs.org/stc/ST00215IB): Installation of saf-Tglo ECO Photoluminescent Aisle Path Marking Systems. STG AEROSPACE GERMANY GmbH
- [STC ST04792NY](https://openairdocs.org/stc/ST04792NY): Update of Intelsat 2Ku. Delta Engineering Corporation
- [STC ST04562NY](https://openairdocs.org/stc/ST04562NY): Installation of saf-Tglo® SuperSeal UltraLite-X (SSUL-X) Photoluminescent Floor Proximity Emergency Escape Path Marking Systems. STG AEROSPACE GERMANY GmbH
- [STC ST03422NY](https://openairdocs.org/stc/ST03422NY): Update of Intelsat components. Delta Engineering Corporation
- [STC ST04483AT](https://openairdocs.org/stc/ST04483AT): Installation of the Avionics Support Group Constant Friction Mount (cfMount) with Cradle. Avionics Support Group Inc
- [STC ST03972NY](https://openairdocs.org/stc/ST03972NY): Installation of Honeywell Satcom SBB Upgrade and WiFi Network Activation. UMLAUT ENGINEERING GMBH
- [STC ST04073NY](https://openairdocs.org/stc/ST04073NY): Installation of navAero Electronic Flight Bag provisions. Delta Engineering Corporation

## Related

- Other Airbus Canada LP BD-500-1A11 aircraft: https://openairdocs.org/model/airbus-canada-lp-bd-500-1a11/aircraft.md
- The Pratt & Whitney PW1521G SERIE engine: https://openairdocs.org/engine/pratt-whitney-pw1521g-serie.md

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