# N117DU: 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: 50036
- Year built: 2019
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 25, 2019
- Certificate issued: June 29, 2020
- Expires: June 30, 2027
- Mode S code: A04692
- 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=117DU
- Page: https://openairdocs.org/aircraft/N117DU

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): 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/N117DU/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 N117DU.

## FAA accident and incident reports

None matched to N117DU.

## Service difficulty reports (112, 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 DALA2026082504825](https://openairdocs.org/sdr/DALA2026082504825), Jul 16, 2026: SKIN. CORRODED. ERA 627451-14 REV B: MID FUSELAGE SKIN - FRAME 34-35, S36L-S36R - CORROSION. SUBJECT REPAIR REQUIRES FOLLOW-ON ACTION. ACCOMPLISH SECTION II WITHIN 52,500 FLIGH
- [SDR DALA2026031201742](https://openairdocs.org/sdr/DALA2026031201742), Mar 9, 2026: BATTERY PACK. INOPERATIVE. DURING SVC FOUND R2 DOOR EMERGENCY EXIT SIGN LIGHT INOPERATIVE. CONFIRMED EXIT SIGN ASSEMBLY WORKED NORMAL BY SWAPPING TO DIFFERENT LOCATION IAW AMP 33-54. REMO
- [SDR DALA2026021701093](https://openairdocs.org/sdr/DALA2026021701093), Feb 15, 2026: HYDRAULIC LINE. LEAKING. PERFORMED AN AIR TURN BACK TO MSP DUE TO FUMES IN THE COCKPIT AND CABIN. SUSPECT LEFT ENGINE OVERSERVICED AND FOUND HYD LEAK AT PYLON DISCONNECT WITH EVIDENCE O
- [SDR DALA2025122309354](https://openairdocs.org/sdr/DALA2025122309354), Dec 17, 2025: SEAL. LEAKING. SHIP 8117 RETURNED TO SAT DUE TO ODOR IN CABIN. FOUND OIL IN #2 SPINNER. REPLACED SEAL REF PW1000G-A-72-00-11. WHILE PERFORMING P-TRAK PROCEDURE PER WORK CARD 0
- [SDR DALA2025112508592](https://openairdocs.org/sdr/DALA2025112508592), Nov 21, 2025: HYDRAULIC LINE. LEAKING. ATB- RETURNED TO MSP DUE TO DIRTY SOCK FUME IN CABIN. EMERGENCY WAS DECLARED. LEAK FOUND BETWEEN HPC AND LPC DUE TO HYDRAULIC LINE LOOSE. SAME TIGHTENED. (LP# 7
- [SDR DALA2025110308039](https://openairdocs.org/sdr/DALA2025110308039), Oct 24, 2025: ENGINE. ODOR. FUMES EVENT WHEN APU ON, ALSO WITH ENGINE BLEEDS ON. REPLACED NR 1 ENGINE. (LP 7601408, 1283162).
- [SDR DALA2025080705930](https://openairdocs.org/sdr/DALA2025080705930), Aug 1, 2025: SKIN. DEBONDED. ER/A 601550-14 REV A. A220 / RH HORIZONTAL STABILIZER / UPPER AND LOWER SKINS / @ REAR SPAR / HINGE RIB 2 TO HINGE RIB 3 / DISBOND. SUBJECT REPAIR REQUIRES FOLL
- [SDR DALA2026073004414](https://openairdocs.org/sdr/DALA2026073004414), Jul 31, 2025: SKIN. DEBONDED. DTE / MONITOR INSPECTION LOG REF. ER/A 601550-14 REV A. A220 / HORIZONTAL STABILIZER / UPPER AND LOWER SKINS / @ REAR SPAR / HINGE RIB 2 TO HINGE RIB 3 / DISBON
- [SDR DALA2025080505879](https://openairdocs.org/sdr/DALA2025080505879), Jul 31, 2025: SKIN. CORRODED. LOWER FWD WTBF AT LWR FUSELAGE 6 INCHES AFT OF DRAIN FRAMES 34 - 35, S36R - 36L HAD SIGNS OF CORROSION. REMOVED CORROSION ON LOWER SKIN, FOUND OUT OF LIMITS IAW
- [SDR DALA2025080505878](https://openairdocs.org/sdr/DALA2025080505878), Jul 31, 2025: SKIN. CORRODED. LOWER FWD WTBF AT LWR FUSELAGE 6 INCHES AFT OF DRAIN FRAMES 34 - 35, S36R - 36L HAD SIGNS OF CORROSION. REMOVED CORROSION ON LOWER SKIN, FOUND OUT OF LIMITS IAW
- [SDR DALA2025080505877](https://openairdocs.org/sdr/DALA2025080505877), Jul 31, 2025: SKIN. CORRODED. LOWER FWD WTBF AT LWR FUSELAGE 6 INCHES AFT OF DRAIN FRAMES 34 - 35, S36R - 36L HAD SIGNS OF CORROSION. REMOVED CORROSION ON LOWER SKIN. FOUND OUT OF LIMITS IAW
- [SDR DALA2025080505876](https://openairdocs.org/sdr/DALA2025080505876), Jul 31, 2025: SKIN. CORRODED. LOWER FWD WTBF AT LWR FUSELAGE 6 INCHES AFT OF DRAIN FR 34 - 35, S36R - 36L HAD SIGNS OF CORROSION. REMOVED CORROSION ON LOWER SKIN & FOUND OUT OF LIMITS IAW AS
- [SDR DALA2025080505875](https://openairdocs.org/sdr/DALA2025080505875), Jul 31, 2025: SKIN. CORRODED. LOWER FWD WTBF AT LWR FUSELAGE 6 INCHES AFT OF DRAIN FR 34 - 35, S36R - 36L HAD SIGNS OF CORROSION. REMOVED CORROSION ON LOWER SKIN FR 34 - 35, S36R-36L, FOUND 
- [SDR DALA2025080505874](https://openairdocs.org/sdr/DALA2025080505874), Jul 31, 2025: SKIN. CORRODED. LOWER FWD WTBF AT LWR FUSELAGE 6 INCHES AFT OF DRAIN FR 34 - 35. S36R - 36L. SIGNS OF CORROSION. REMOVED CORROSION ON LOWER SKIN FR 34 - 35, S36R-36L, FOUND OUT
- [SDR DALA2025080505873](https://openairdocs.org/sdr/DALA2025080505873), Jul 31, 2025: SKIN. CORRODED. LOWER FWD WTBF AT LWR FUSELAGE, 6 INCHES AFT OF DRAIN FR 34 - 35, S36R - 36L SIGNS OF CORROSION. REMOVED CORROSION ON LOWER SKIN FR 34 - 35, S36R -36L, FOUND OU
- [SDR DALA2025072905699](https://openairdocs.org/sdr/DALA2025072905699), Jul 24, 2025: SKIN. CORRODED. CORROSION FOUND ON EXTERNAL SKIN FR79, AFT LAP JOINT, STRINGER 36 TO 37L. BLENDED CORROSION ON EXTERNAL SKIN @ LAP JOINT FR 79, STGR 36R- 36L IAW A220 ASRP 31-2
- [SDR DALA2025072905698](https://openairdocs.org/sdr/DALA2025072905698), Jul 24, 2025: SKIN. CORRODED. CORROSION FOUND ON EXTERNAL SKIN FR77 TO FR78 AROUND STRINGER 36. BLENDED OUT CORROSION ON EXTERNAL SKIN @ FR 77-78 @ STGR 36 IAW A220 ASRP 51-21-06-01AAA. FOUN
- [SDR DALA2025072105449](https://openairdocs.org/sdr/DALA2025072105449), Jul 17, 2025: SKIN. CORRODED. CORROSION FOUND ON EXTERNAL SKIN FR79, AFT LAP JOINT, STRINGER 36 TO 37L. BLENDED CORROSION ON EXTERNAL SKIN @ LAP JOINT FR 79, STGR 36R- 36L IAW A220 ASRP 31-2
- [SDR DALA2025072105448](https://openairdocs.org/sdr/DALA2025072105448), Jul 17, 2025: SKIN. CORRODED. CORROSION FOUND ON EXTERNAL SKIN FR77 TO FR78 AROUND STRINGER 36. BLENDED OUT CORROSION ON EXTERNAL SKIN @ FR 77-78 @ STGR 36 IAW A220 ASRP 51-21-06-01AAA. FOUN
- [SDR DALA2026031101705](https://openairdocs.org/sdr/DALA2026031101705), Jul 9, 2025: SCUFF PLATE. CORRODED. DOOR LOWER SCUFF PLATE FASTENER HOLES 20OL, 19OL, 18OL AND 16OL HAVE CORROSION. REMOVED CORROSION, EVALUATED AREA ON FWD CARGO DOOR LOWER SCUFF PLATE, FOUND OUT
- [SDR DALA2026031101704](https://openairdocs.org/sdr/DALA2026031101704), Jul 8, 2025: DOOR SILL. CORRODED. DOOR LOWER SILL HAS CORROSION AS MARKED AT FASTENER HOLES. REMOVED CORROSION, AFFECTED AREA OF FWD CARGO DOOR LWR SILL FOUND OUT OF LIMITS IAW A220 ASRP J51-21-
- [SDR DALA2026031101703](https://openairdocs.org/sdr/DALA2026031101703), Jul 8, 2025: DOOR SILL. CORRODED. DOOR LOWER SILL HAS CORROSION AS MARKED AT FASTENER HOLES. REMOVED CORROSION, AFFECTED AREA ON AFT CARGO DOOR LOWER SILL FOUND OUT OF LIMITS IAW A220 ASRP J51-2
- [SDR DALA2026031101700](https://openairdocs.org/sdr/DALA2026031101700), Jul 3, 2025: SCUFF PLATE. CORRODED. L1 DOOR SCUFF PLATE FASTENER HOLES 15OL, 14OL, 11OL, 5OL, 4OL, 3OL, 2OL, AND 1OL HAVE CORROSION. REMOVED CORROSION, EVALUATED AREA ON FWD PAX DOOR LWR SCUFF PLA
- [SDR DALA2026031101702](https://openairdocs.org/sdr/DALA2026031101702), Jun 26, 2025: SCUFF PLATE. CORRODED. AFT CARGO DOOR, LOWER SCUFF PLATE FASTENER HOLES 11OL, 10OL, 9OL, 8OL, 7OL, 6OL, 5OL, 4OL, 3OL, 2OL, AND 1OL HAVE CORROSION. REMOVED CORROSION, EVALUATED AREA O
- [SDR DALA2026031101701](https://openairdocs.org/sdr/DALA2026031101701), Jun 26, 2025: SCUFF PLATE. CORRODED. FWD CARGO DOOR, LOWER SCUFF PLATE FASTENER HOLES 11OU AND 10OU HAVE CORROSION. REMOVED CORROSION, EVALUATED AREA ON FWD CARGO DOOR UPPER SCUFF PLATE, FOUND OUT 
- [SDR DALA2026031101699](https://openairdocs.org/sdr/DALA2026031101699), Jun 26, 2025: SCUFF PLATE. CORRODED. R1 DOOR SCUFF PLATE FASTENER HOLES 15OL, 14OL, 13OL, 12OL, 11OL, 5OL, 3OL, AND 1OL HAVE CORROSION. REMOVED CORROSION, EVALUATED AREA ON R1 DOOR SCUFF PLATE, FOU
- [SDR DALA2025062504761](https://openairdocs.org/sdr/DALA2025062504761), Jun 21, 2025: SEAT TRACK. CORRODED. AFT RH, I/B SEAT TRACK HAS EVIDENCE OF CORROSION FROM FR72 TO FR74. REMOVED CORROSION, FOUND OUT OF LIMITS, REMOVED AND REPLACED DAMAGED AFT L/H I/B SEAT TRACK 
- [SDR DALA2025062504760](https://openairdocs.org/sdr/DALA2025062504760), Jun 21, 2025: SEAT TRACK. CORRODED. AFT LH, O/B SEAT TRACK HAS EVIDENCE OF CORROSION FROM FR72 TO FR74. REMOVED CORROSION, FOUND OUT OF LIMITS, REMOVED AND REPLACED DAMAGED AFT L/H O/B SEAT TRACK 
- [SDR DALA2025062504759](https://openairdocs.org/sdr/DALA2025062504759), Jun 21, 2025: SEAT TRACK. CORRODED. FWD LH, I/B SEAT TRACK HAS EVIDENCE OF CORROSION FROM FR22 TO FR24. REMOVED CORROSION FOUND WITH OUT LIMITS, REMOVED AND REPLACED FWD LH I/B SEAT TRACK IAW A220
- [SDR DALA2025062504758](https://openairdocs.org/sdr/DALA2025062504758), Jun 21, 2025: SEAT TRACK. CORRODED. FWD RH, O/B SEAT TRACK HAS EVIDENCE OF CORROSION FROM FR22 TO FR24. REMOVED CORROSION, FOUND OUT OF LIMITS, REMOVED AND REPLACED FWD R/H O/B SEAT TRACK IAW A220
- [SDR DALA2025062404721](https://openairdocs.org/sdr/DALA2025062404721), Jun 20, 2025: SEAT TRACK. CORRODED. AFT RH, O/B SEAT TRACK HAS EVIDENCE OF CORROSION FROM FR72 TO FR74. REMOVED CORROSION, FOUND OUT OF LIMITS, REMOVED AND REPLACED AFT R/H O/B SEAT TRACK IAW A220
- [SDR DALA2025062404720](https://openairdocs.org/sdr/DALA2025062404720), Jun 20, 2025: SEAT TRACK. CORRODED. AFT LH, I/B SEAT TRACK HAS EVIDENCE OF CORROSION FROM FR72 TO FR74. REMOVED CORROSION, FOUND OUT OF LIMITS, REMOVED AND REPLACED AFT L/H I/B SEAT TRACK IAW A220
- [SDR DALA2025062404719](https://openairdocs.org/sdr/DALA2025062404719), Jun 20, 2025: SEAT TRACK. CORRODED. FWD LH, O/B SEAT TRACK HAS EVIDENCE OF CORROSION FROM FR22 TO FR24. REMOVED AND REPLACED SEAT TRACK AT FWD L/H O/B IAW A220 ASRP J51 -42-21, J51-21-06, J51-40-1
- [SDR DALA2025062404718](https://openairdocs.org/sdr/DALA2025062404718), Jun 20, 2025: SEAT TRACK. CORRODED. FWD RH, I/B SEAT TRACK HAS EVIDENCE OF CORROSION FROM FR22 TO FR24. REMOVED CORROSION AND FOUND FWD R/H I/B SEAT TRACK OUT OF LIMITS IAW A220 ASRP J51-21-06, J5
- [SDR DALA2025031201906](https://openairdocs.org/sdr/DALA2025031201906), Mar 12, 2025: LIGHT. INOPERATIVE. R2 EXTERNAL EMERGENCY LIGHT INOP. R/R R2 EXTERNAL EMERGENCY LIGHT IAW A220 AMP 33-55. OPS CHECK OK. (LP# 7248522)
- [SDR DALA2024120311423](https://openairdocs.org/sdr/DALA2024120311423), Nov 26, 2024: LIGHT. INOPERATIVE. DURING TEST OF EMERGENCY LIGHTS, AISLE LIGHTS FOUND INOP. INSPECTED INTERNAL EMERGENCY LIGHTS PER A220 AMP 33-52-00. NO FAULTS FOUND. (LP# 5724699)
- [SDR DALA2024102310334](https://openairdocs.org/sdr/DALA2024102310334), Oct 19, 2024: COVER. MISSING. EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE. OVER HEAD EMERGENCY FLOODLIGHT IS MISSING COVER / INTERIOR. RE-SECURED OVERHEAD EMERGENCY FLOOD LIGHT COVER AS 
- [SDR DALA2024080707862](https://openairdocs.org/sdr/DALA2024080707862), Aug 3, 2024: CABLE. FAILED. SHIP 8117 - SMK - RETURNED TO GATE DUE TO SMOKE FROM ROW 17 IN-SEAT MONITOR USB. CORRECTIVE ACTION: PLACED IN-SEAT POWER MASTER CONTROL RELAY ON MEL 44-20-01. R
- [SDR DALA2024032803890](https://openairdocs.org/sdr/DALA2024032803890), Mar 26, 2024: SKIN. DAMAGED. FUSELAGE SKIN / FR 49-50, S8L-S9L / LIGHTNING STRIKES / EXTERNAL DOUBLER REPAIR AT FR49 AND STGR8L. THIS IS A DTA MONITOR LOG FOR ERA 607631-14AD REV A WHICH RE
- [SDR DALA2024032803889](https://openairdocs.org/sdr/DALA2024032803889), Mar 26, 2024: SKIN. DAMAGED. FUSELAGE SKIN / FR 49-50, S8L-S9L / LIGHTNING STRIKES / REPAIRED FASTENER AT FR50 AND ABOVE STGR7L. THIS IS A DTA MONITOR LOG FOR ERA 607631-14AD REV A WHICH RE
- [SDR DALA2024011900871](https://openairdocs.org/sdr/DALA2024011900871), Jan 15, 2024: SLAT TRACK. CORRODED. R/H SLAT TRACK NBR 10 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF 5742-01028-02B, REPAIRED R/H SLAT TRACK #10 UPPER FORWARD SURFACE PER
- [SDR DALA2024011900870](https://openairdocs.org/sdr/DALA2024011900870), Jan 15, 2024: SLAT TRACK. CORRODED. R/H SLAT TRACK NBR 10 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF 5742-01028-02B, REPAIRED R/H SLAT TRACK #10 LOWER AFT SURFACE PER SUM
- [SDR DALA2024011900869](https://openairdocs.org/sdr/DALA2024011900869), Jan 15, 2024: SLAT TRACK. CORRODED. R/H SLAT TRACK NBR 8 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF 5742-01028-02B, REPAIRED R/H SLAT TRACK #8 LOWER AFT SURFACE PER SUMMA
- [SDR DALA2024011900868](https://openairdocs.org/sdr/DALA2024011900868), Jan 15, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK #10 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF AA 5742-01028-02A. REPAIRED L/H SLAT TRACK NBR#10 UPPER FWD SURFACE PER S
- [SDR DALA2024011900867](https://openairdocs.org/sdr/DALA2024011900867), Jan 15, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 8 LOWER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 8 LOWER FWD SURFACE PER SU
- [SDR DALA2024011900866](https://openairdocs.org/sdr/DALA2024011900866), Jan 15, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK #9 IB LOWER FWD SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF AA 5742-01028-02A. REPAIRED L/H SLAT TRACK NBR #9 IB LOWER FWD SIDE PER SU
- [SDR DALA2024011900865](https://openairdocs.org/sdr/DALA2024011900865), Jan 15, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 7 OUTBOARD LOWER FWD SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 7 OUTBOARD LOWER FWD
- [SDR DALA2024011900864](https://openairdocs.org/sdr/DALA2024011900864), Jan 15, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK #9 OB LOWER FWD SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF AA 5742-01028-02A. REPAIRED L/H SLAT TRACK NBR #9 OB LOWER FWD SIDE PER SU
- [SDR DALA2024011900863](https://openairdocs.org/sdr/DALA2024011900863), Jan 15, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 7 INBOARD LOWER FWD SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 7 INBOARD LOWER FWD S
- [SDR DALA2024011900862](https://openairdocs.org/sdr/DALA2024011900862), Jan 15, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 7 OUTBOARD UPPER AFT SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 7 OUTBOARD UPPER AFT

All 112: https://openairdocs.org/aircraft/N117DU/reports.md

## STCs that may be installed (OpenAirDocs) (15)

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 Ltd Ptnrsp BD-500-1A10)

- [STC ST04254NY](https://openairdocs.org/stc/ST04254NY): Installation of Viasat Satcom Software. ALOFT AeroArchitects
- [STC ST00030IB](https://openairdocs.org/stc/ST00030IB): Installation of Test Tech ELT. APTOZ EHF
- [STC ST02570LA](https://openairdocs.org/stc/ST02570LA): Interior Installations and Modifications. Safran Cabin Inc
- [STC ST11389DS](https://openairdocs.org/stc/ST11389DS): Installation of Delta Comfort Passenger Seating Section. Aircraft Systems and Manufacturing Inc
- [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 ST04425CH](https://openairdocs.org/stc/ST04425CH): Installation of a Honeywell One Aero Edge Node (1AEN) in accordance with StandardAero Master Data List 1037081, Revision (B), dated June 9, 2020 or later FAA approved revision. StandardAero Business Aviation Services LLC
- [STC ST04424CH](https://openairdocs.org/stc/ST04424CH): TPED Compatibility Test in accordance with StandardAero Master Data List 1037140, Revision (B), dated June 1, 2020 or later FAA approved revision. Standard Aero Business Aviation Services LLC
- [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
- [STC ST00149IB](https://openairdocs.org/stc/ST00149IB) (historical): Installation of a Cabin air exhaust muffler, to reduce this noise to a more comfortable level by installing a valve cap and sound damping system. DOA21 LIMITED

## Related

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

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