# N115DU: 2019 Airbus Canada Ltd Ptnrsp BD-500-1A10

- Status: Valid registration
- Airframe: [Airbus Canada Ltd Ptnrsp BD-500-1A10](https://openairdocs.org/model/airbus-canada-ltd-ptnrsp-bd-500-1a10) (registry code 1400010, 133 seats)
- Engine: [Pratt & Whitney PW1519G](https://openairdocs.org/engine/pratt-whitney-pw1519g) (registry code 52315)
- Data sheets: [TCDS T00008NY](https://openairdocs.org/tcds/T00008NY) (Airbus Canada Limited Partnership), [TCDS E00090EN](https://openairdocs.org/tcds/E00090EN) (Pratt & Whitney) (OpenAirDocs)
- Serial number: 50034
- Year built: 2019
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 18, 2019
- Certificate issued: June 29, 2020
- Expires: June 30, 2027
- Mode S code: A03F24
- Registered owner: [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE)
- Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)
- Owner type: Corporation
- Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=115DU
- Page: https://openairdocs.org/aircraft/N115DU

From the FAA registry file of October 21, 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): 75 in force

### Matched by airframe (Airbus Canada Ltd Ptnrsp BD-500-1A10)

- [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 2025-09-02](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 2025-06-06](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 2024-10-11](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 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 2023-07-05](https://openairdocs.org/ad/2023-07-05): Equipment/furnishings · Airbus Canada Limited Partnership BD-500-1A10. Effective May 30, 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
- [AD 2022-21-03](https://openairdocs.org/ad/2022-21-03): Fuel · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Dec 14, 2022
- [AD 2022-16-02](https://openairdocs.org/ad/2022-16-02): Doors · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Nov 25, 2022
- [AD 2022-16-08](https://openairdocs.org/ad/2022-16-08): Turbine/turboprop engine · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Sep 1, 2022
- [AD 2022-11-21](https://openairdocs.org/ad/2022-11-21): Equipment/furnishings · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jun 15, 2022

### Matched by engine (Pratt & Whitney PW1519G)

- [AD 2025-04-13](https://openairdocs.org/ad/2025-04-13): Turbine Engine Compressor Section · Pratt & Whitney PW1519G, PW1521G, PW1521G-3 and 10 more. Effective Apr 8, 2025
- [AD 2024-06-04](https://openairdocs.org/ad/2024-06-04): Turbine Engine Compressor Section; Turbine Section · Pratt & Whitney PW1519G, PW1521G, PW1521G-3 and 10 more. Effective Apr 11, 2024
- [AD 2022-27-04](https://openairdocs.org/ad/2022-27-04): Engine Controls · Pratt & Whitney PW1519G, PW1521G, PW1521G-3 and 5 more. Effective Jan 31, 2023
- [AD 2022-15-03](https://openairdocs.org/ad/2022-15-03): Turbine Engine Compressor Section · Pratt & Whitney PW1519G, PW1521G, PW1521G-3 and 10 more. Effective Aug 19, 2022
- [AD 2022-02-05](https://openairdocs.org/ad/2022-02-05): Turbine Section · Pratt & Whitney PW1519G, PW1521G, PW1521G-3 and 10 more. Effective Jan 27, 2022
- [AD 2021-20-01](https://openairdocs.org/ad/2021-20-01): Turbine Section · Pratt & Whitney PW1519G, PW1521G, PW1521G-3 and 10 more. Effective Oct 27, 2021
- [AD 2021-17-09](https://openairdocs.org/ad/2021-17-09): Turbine Engine Compressor Section · Pratt & Whitney PW1519G, PW1521G, PW1521G-3 and 10 more. Effective Sep 22, 2021
- [AD 2020-04-01](https://openairdocs.org/ad/2020-04-01): Turbine Engine Oil System · Pratt & Whitney PW1519G, PW1521G, PW1521G-3 and 10 more. Effective Mar 27, 2020
- [AD 2019-16-15](https://openairdocs.org/ad/2019-16-15): Turbine Engine Compressor Section · Pratt & Whitney PW1519G, PW1521G, PW1521G-3 and 10 more. Effective Oct 1, 2019

### 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
- [AD 2021-14-06](https://openairdocs.org/ad/2021-14-06) (historical): Turbine Engine Compressor Section · Pratt & Whitney PW1519G, PW1521G, PW1521G-3 and 10 more. Effective Aug 12, 2021
- [AD 2020-07-02](https://openairdocs.org/ad/2020-07-02) (historical): Turbine Engine Compressor Section · Pratt & Whitney PW1519G, PW1521G, PW1521G-3 and 5 more. Effective Apr 15, 2020
- [AD 2019-21-11](https://openairdocs.org/ad/2019-21-11) (historical): Turbine Engine Compressor Section · Pratt & Whitney PW1519G, PW1521G, PW1521G-3 and 10 more. Effective Oct 29, 2019
- [AD 2019-19-11](https://openairdocs.org/ad/2019-19-11) (historical): Turbine Engine Compressor Section · Pratt & Whitney PW1519G, PW1521G, PW1521G-3 and 10 more. Effective Sep 26, 2019

All 89: https://openairdocs.org/aircraft/N115DU/ads.md

## Information bulletins (advisory) (2 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
- [SAIB NE-20-09](https://openairdocs.org/saib/NE-20-09): TURBINE ENGINE COMPRESSOR SECTION. Issued Apr 30, 2020

## NTSB investigations

None matched to N115DU.

## FAA accident and incident reports

None matched to N115DU.

## Service difficulty reports (81, newest 50)

As reported by operators and repair stations.

- [SDR DALA2026090805026](https://openairdocs.org/sdr/DALA2026090805026), Sep 5, 2026: ROLLER. WORN. RIGHT NR 4 SLAT TRACK BOTH INBD ROLLER WORN, EXCEED MAXIMUM DEPTH OF .010" AT .018" PER WC 5742-01028-02B. REPAIRED PER PRI 620677-14AD REV 0 ER/A REV C, AND FI
- [SDR DALA2026053103308](https://openairdocs.org/sdr/DALA2026053103308), May 31, 2026: LIGHT. INOPERATIVE. LEFT FWD FUSELAGE EXTERNAL EMERGENCY LIGHT AND L/H OVERWING EXTERNAL EMERGENCY LIGHT INOP. REPLACED LIGHTS REF A220 AMP 33-55. OPS CHECKS GOOD. (LP 8901899 - AI
- [SDR DALA2025061004417](https://openairdocs.org/sdr/DALA2025061004417), Jun 5, 2025: LIGHT. DAMAGED. LEFT AND RIGHT OVERWING EMERGENCY LIGHTS WITH WATER DAMAGE (4) NEED REPLACE. REMOVED AND REPLACED LEFT AND RIGHT OVERWING EMERGENCY LIGHTS. PERFORMED EXTERNAL E
- [SDR DALA2025052704039](https://openairdocs.org/sdr/DALA2025052704039), May 21, 2025: FLOOR PANEL. CORRODED. CORROSION ALONG FWD AND INBOARD EDGES OF FSD ENTRY FLOOR PANEL 222KRF. REMOVED AND REPLACED APD ENTRY FLOOR PANEL 222KRF IAW A220 AMP BD500-A-J53-00-47-13AAA-52
- [SDR DALA2025052704038](https://openairdocs.org/sdr/DALA2025052704038), May 21, 2025: FLOOR PANEL. CORRODED. CORROSION ON AFT INBOARD CORNER OF APD ENTRY FLOOR PANEL 241MLF. REMOVED AND REPLACED APD ENTRY FLOOR PANEL 241MLF IAW A220 AMP BD500-A-J53-00-47-13AAA-520A-A A
- [SDR DALA2025052003865](https://openairdocs.org/sdr/DALA2025052003865), May 15, 2025: SEAT TRACK. CORRODED. ***CORROSION*** ON LOWER AREA SEAT TRACK BETWEEN FRAME 47 AND 48 , AT RBL 43, WL 151. REMOVED AND REPLACED SEAT TRACK FROM FR 43-51 + 10" RBL 43 IAW BOMBARDIER 
- [SDR DALA2025050603475](https://openairdocs.org/sdr/DALA2025050603475), May 5, 2025: FLOOR PANEL. CORRODED. ***CORROSION*** ALONG FWD EDGE, AFT INBOARD CORNER AND AFT EDGE OF ASD ENTRY FLOOR PANEL 242MRF. REMOVED AND REPLACED FLOOR PANEL 242MRF IAW A220 AMP BD500- A-J
- [SDR DALA2025050103372](https://openairdocs.org/sdr/DALA2025050103372), Apr 29, 2025: SEAT TRACK. CORRODED. ***CORROSION*** ON SEAT TRACK @ 22 INCHES FWD OF FR74 TO 2 INCHES AFT OF FR74, LBL23, WL151.5. REMOVED AND REPLACE SEAT TRACK BETWEEN FR 61 TO FR 74 +8" LBL 23 
- [SDR DALA2025050603470](https://openairdocs.org/sdr/DALA2025050603470), Apr 24, 2025: CARGO TRACK. CORRODED. ***CORROSION*** ON SEAT TRACK @ 12.5 INCHES FWD OF FR74 TO 2 INCHES AFT OF FR74, RBL23, WL151.5. REMOVED AND REPLACED SEAT TRACK BETWEEN FR 61 TO FR 74, RBL23, 
- [SDR DALA2025042403231](https://openairdocs.org/sdr/DALA2025042403231), Apr 23, 2025: SEAT TRACK. CORRODED. CORRODED SEAT TRACK @ 4 INCHES FWD OF FR20 TO FR20, RBL43, WL151.5. REMOVED AND REPLACED SEAT TRACK BETWEEN FR20 TO FR30 RBL43 WL 151.5 IAW A220 ASRP BD500-A-J5
- [SDR DALA2025042203162](https://openairdocs.org/sdr/DALA2025042203162), Apr 16, 2025: SEAT TRACK. CORRODED. ***CORROSION*** ON SEAT TRACK @ 4 INCHES FWD OF FR20 TO 1.5 INCHES AFT OF FR20, RBL23, WL151.5. REMOVED AND REPLACED SEAT TRACK FROM FR 20 TO FR 34 RBL 23 WL 15
- [SDR DALA2025042103103](https://openairdocs.org/sdr/DALA2025042103103), Apr 15, 2025: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACK @ 4 INCHES FWD OF FR74 TO 2 INCHES AFT OF FR74, LBL43, WL151.5. REMOVED SEAT TRACK DAMAGED FROM FR 74 TO FR61 LBL 43 WL 151.5 AND INSTAL
- [SDR DALA2025041002787](https://openairdocs.org/sdr/DALA2025041002787), Apr 7, 2025: SEAT TRACK. CORRODED. ***CORROSION*** ON SEAT TRACK @ 12.5 INCHES FWD OF FR74 TO 2 INCHES AFT OF FR74, RBL43, WL151.5. REMOVED AND REPLACE SEAT TRACK BETWEEN FR57+13" TO 74+6" RBL43,
- [SDR DALA2025041002786](https://openairdocs.org/sdr/DALA2025041002786), Apr 7, 2025: SEAT TRACK. CORRODED. ***CORROSION*** ON SEAT TRACK @ 5 INCHES FWD OF FR22 TO 15 INCHES AFT OF FR22, LBL43, WL151.5. REMOVED AND REPLACED SEAT TRACK LBL43 FR 20 TO FR 30 IAW A220 ASR
- [SDR DALA2025060904386](https://openairdocs.org/sdr/DALA2025060904386), Apr 1, 2025: ORIFICE. BLOCKED. THE VALVE PIN HOLE IS PARTIALLY OR FULLY BLOCKED AND THE SAFETY PIN CAN'T BE INSTALLED ON RH OWEE DOOR SLIDE. THE SLIDE WILL NEED TO BE DEPLOYED. REMOVED AND IN
- [SDR DALA2025031001817](https://openairdocs.org/sdr/DALA2025031001817), Mar 8, 2025: CONTROL LEVER. FAULTY. SHIP 8115 - DIV - TO LAX DUE TO "NORM BRAKE FAIL MESSAGE". REPLACED LANDING GEAR CONTROL LEVER. (LP# 6875590)
- [SDR DALA2024091208951](https://openairdocs.org/sdr/DALA2024091208951), Sep 7, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR5 HAS EVIDENCE OF CORROSION ON UPPER AFT AND HAS PREVIOUS REWORK, BLEND PER AMDS W/C 5742-010280-02B AND REQUIRES NDT INSPECTION FOR SIGNS OF C
- [SDR DALA2024091208950](https://openairdocs.org/sdr/DALA2024091208950), Sep 7, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 5 HAS EVIDENCE OF CORROSION ON UPPER FWD AND HAS PREVIOUS REWORK, BLEND PER AMDS W/C 5742-010280-02B AND REQUIRES NDT INSPECTION FOR SIGNS OF 
- [SDR DALA2024091208949](https://openairdocs.org/sdr/DALA2024091208949), Sep 7, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 6 HAS EVIDENCE OF CORROSION ON UPPER FWD AND HAS PREVIOUS REWORK, BLEND PER AMDS W/C 5742-010280-02B AND REQUIRES NDT INSPECTION FOR SIGNS OF 
- [SDR DALA2024091208948](https://openairdocs.org/sdr/DALA2024091208948), Sep 7, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR4 HAS EVIDENCE OF CORROSION ON UPPER FWD AND HAS PREVIOUS REWORK, BLEND PER AMDS W/C 5742-010280-02B AND REQUIRES NDT INSPECTION FOR SIGNS OF C
- [SDR DALA2024091208947](https://openairdocs.org/sdr/DALA2024091208947), Sep 7, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 5 HAS EVIDENCE OF CORROSION ON UPPER AFT AND HAS PREVIOUS REWORK, BLEND PER AMDS W/C 5742-010280-02B AND REQUIRES NDT INSPECTION FOR SIGNS OF 
- [SDR DALA2024091208946](https://openairdocs.org/sdr/DALA2024091208946), Sep 7, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 1 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND HAS PREVIOUS REWORK BLEND PER AMDS W/C 5742-01280 AND REQUIRED NDT INSPECTION FOR SIGNS OF C
- [SDR DALA2024091208945](https://openairdocs.org/sdr/DALA2024091208945), Sep 7, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 1 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND HAS PREVIOUS REWORK BLEND PER AMDS W/C 5742-01280 AND REQUIRED NDT INSPECTION FOR SIGNS OF C
- [SDR DALA2024090908864](https://openairdocs.org/sdr/DALA2024090908864), Sep 6, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 4 PINION TEETH (2EA) HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FUR
- [SDR DALA2024051505240](https://openairdocs.org/sdr/DALA2024051505240), May 15, 2024: NONE. NONE. THIS IS BEING CREATED TO ACCOMPLISH ONE-TIME INSPECTION FOR ER/A 618031-14. ACCOMPLISH ER/A SECTION III ONE-TIME INSPECTION AFTER ACCOMPLISHMENT OF SECTION I TI
- [SDR DALA2024020901832](https://openairdocs.org/sdr/DALA2024020901832), Feb 7, 2024: PACKING. LEAKING. WHEN APU FIRST STARTS STRONG DIRTY SOCKS FEET SMELL IN CABIN/ COCKPIT. UPON STARTING APU AFTER LANDING BURNT TOAST SMELL IN CABIN/COCKPIT. AS PER NO GO ODI PERF
- [SDR DALA2024011800789](https://openairdocs.org/sdr/DALA2024011800789), Jan 12, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK #9 UPPER INBOARD AFT SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF. AA5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFOR
- [SDR DALA2024011800788](https://openairdocs.org/sdr/DALA2024011800788), Jan 12, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK #8 LWR AFT HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. C/
- [SDR DALA2024011800787](https://openairdocs.org/sdr/DALA2024011800787), Jan 12, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK #4 HAS WORN SPOT ON UPPER INBOARD AFT SIDE AND PREVIOUS REWORK. REF AA5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER 
- [SDR DALA2024011800785](https://openairdocs.org/sdr/DALA2024011800785), Jan 12, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK #8 LWR FWD HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF AA5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. C
- [SDR DALA2024011800781](https://openairdocs.org/sdr/DALA2024011800781), Jan 12, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK #1 LWR AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF. AA5742-01028-02B. LIAISON ENGINEERING SUPPORTING REQUIRED BEFORE FURTHER FLT
- [SDR DALA2024011800778](https://openairdocs.org/sdr/DALA2024011800778), Jan 12, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK #4 LWR FWD HAS EVIDENCE OF CORROSION REF AA5742- 01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLIGHT. C/W PRI ERA 607388-14AD ST
- [SDR DALA2024011800777](https://openairdocs.org/sdr/DALA2024011800777), Jan 12, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK #3 LWR AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. C/
- [SDR DALA2024011800775](https://openairdocs.org/sdr/DALA2024011800775), Jan 12, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK #2 LWR AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF. AA5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. C
- [SDR DALA2024011800773](https://openairdocs.org/sdr/DALA2024011800773), Jan 12, 2024: ROLLER. WORN. RH OUTBOARD LWR SIDE OF SLAT TRACK #4 HAS EVIDENCE OF ROLLER WEAR AND PREVIOUS REWORK REF AA5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FLIGHT. 
- [SDR DALA2024011800772](https://openairdocs.org/sdr/DALA2024011800772), Jan 12, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK #5 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA 5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT.
- [SDR DALA2024011800771](https://openairdocs.org/sdr/DALA2024011800771), Jan 12, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK #10 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF. AA5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT
- [SDR DALA2024011800769](https://openairdocs.org/sdr/DALA2024011800769), Jan 12, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK #9 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA 5742-01028-02B LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. 
- [SDR DALA2024011800768](https://openairdocs.org/sdr/DALA2024011800768), Jan 12, 2024: SLAT TRACK. CORRODED. L/H SLAT TRACK NBR 4 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE 
- [SDR DALA2024011800767](https://openairdocs.org/sdr/DALA2024011800767), Jan 12, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK #9 LWR AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. C/
- [SDR DALA2024011800766](https://openairdocs.org/sdr/DALA2024011800766), Jan 12, 2024: SLAT TRACK. UNKNOWN. L/H SLAT TRACK NBR 5 LOWER AFT HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA5742-01028-02A. LIAISON ENGINEERING WILL BE REQUIRED BEFORE FURTHER FLIGHT. C
- [SDR DALA2024011600673](https://openairdocs.org/sdr/DALA2024011600673), Jan 12, 2024: SLAT TRACK. UNKNOWN. LH SLAT TRACK #2 LWR AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER
- [SDR DALA2024011600671](https://openairdocs.org/sdr/DALA2024011600671), Jan 12, 2024: UNKNOWN. UNKNOWN. RH SLAT TRACK #4 LOWER AFT SURFACE HAS EVIDENCE OF ROLLER WEAR AND PREVIOUS REWORK REF AA5742-01028-02B LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT.
- [SDR DALA2024011600670](https://openairdocs.org/sdr/DALA2024011600670), Jan 12, 2024: UNKNOWN. UNKNOWN. COPY OF NRT #25 DUE TO LOST PAPERWORK. RH SLAT TRACK #4 PINION TEETH HAS EVIDENCE OF CORROSION. REF. AA5742-01028-02B. LIAISONENGINEERING SUPPORT REQUIRED BEFOR
- [SDR DALA2024011600669](https://openairdocs.org/sdr/DALA2024011600669), Jan 12, 2024: SLAT TRACK. UNKNOWN. RH SLAT TRACK #5 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF. AA5742-01028-02B LIAISONENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLIGHT
- [SDR DALA2024011600665](https://openairdocs.org/sdr/DALA2024011600665), Jan 12, 2024: UNKNOWN. UNKNOWN. RH SLAT TRACK #2 LOWER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF. AA5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT.
- [SDR DALA2024012901254](https://openairdocs.org/sdr/DALA2024012901254), Jan 11, 2024: SLAT TRACK. CORRODED. L/H SLAT TRACK NBR 5 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA5742-01028. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTH
- [SDR DALA2024011800786](https://openairdocs.org/sdr/DALA2024011800786), Jan 11, 2024: SLAT TRACK. CORRODED. L/H SLAT TRACK NBR 8 UPPER FORWARD HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTH
- [SDR DALA2024011800784](https://openairdocs.org/sdr/DALA2024011800784), Jan 11, 2024: SLAT TRACK. CORRODED. L/H SLAT TRACK NBR 5 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE F
- [SDR DALA2024011800783](https://openairdocs.org/sdr/DALA2024011800783), Jan 11, 2024: SLAT TRACK. CORRODED. L/H SLAT TRACK NBR 4 UPPER FORWARD OUTBOARD SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRE

All 81: https://openairdocs.org/aircraft/N115DU/reports.md

## Related

- Other Airbus Canada Ltd Ptnrsp BD-500-1A10 aircraft: https://openairdocs.org/model/airbus-canada-ltd-ptnrsp-bd-500-1a10/aircraft.md
- STCs for the Airbus Canada Ltd Ptnrsp BD-500-1A10: https://openairdocs.org/model/airbus-canada-ltd-ptnrsp-bd-500-1a10/stcs.md
- The Pratt & Whitney PW1519G engine: https://openairdocs.org/engine/pratt-whitney-pw1519g.md

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