# N133DU: 2020 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: 50052
- Year built: 2020
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 23, 2020
- Certificate issued: October 22, 2020
- Expires: October 31, 2027
- Mode S code: A086B4
- 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=133DU
- Page: https://openairdocs.org/aircraft/N133DU

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/N133DU/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 N133DU.

## FAA accident and incident reports

None matched to N133DU.

## Service difficulty reports (53, 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 DALA2026090805029](https://openairdocs.org/sdr/DALA2026090805029), Sep 3, 2026: LIGHT. INOPERATIVE. AFT L2 DOOR EXTERIOR EMERGENCY LIGHT INOP. EXTERIOR EMERGENCY LIGHTS SYSTEMS - DOOR EMERGENCY LIGHTS. R/R AFT LH EMERGENCY LIGHT REF A220 AMP 33-55. OPS CHECK G
- [SDR DALA2026071604188](https://openairdocs.org/sdr/DALA2026071604188), Jul 14, 2026: LIGHT. INOPERATIVE. RIGHT FWD FUSELAGE EXTERNAL EMERGENCY LIGHT INOP. REMOVED AND REPLACED RH EMERGENCY LIGHT PER AMP 33-55-02. OPS CHECK GOOD. (LP# 8640192; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026011400343](https://openairdocs.org/sdr/DALA2026011400343), Jan 10, 2026: OIL SYSTEM. LEAKING. AFTER STARTING BOTH ENGINES AND APU OFF REAR FA CALLED AND REPORTED DIRTY SOCKS SMELL. SMELL REMAINED AFTER SHUTTING RIGHT ENGINE DOWN. C/W SMOKE/FUME WC 0550-2
- [SDR DALA2025112108506](https://openairdocs.org/sdr/DALA2025112108506), Nov 20, 2025: FRAME. CORRODED. THE FOLLOWING HOLES ON FRAME FR76 HAVE CORROSION: HOLE 7 STR 13 (M) (P). REPAIRED PER ER/A PRI 629432-14 REV. 0, REV 1, REV. 2 AND FINAL ER/A 629432-14 REV. ORI
- [SDR DALA2025112108505](https://openairdocs.org/sdr/DALA2025112108505), Nov 20, 2025: FRAME. DAMAGED. THE FOLLOWING HOLES ON FRAME FR76 HAVE CORROSION: HOLE 1 AT STR 9, HOLE 2 AT STR 9, HOLE 3 AT STR 10, HOLE 5 AT STR12, HOLE 6 AT STR 12, HOLE 11 AT STR 18 AND H
- [SDR DALA2025112108504](https://openairdocs.org/sdr/DALA2025112108504), Nov 19, 2025: SKIN. DAMAGED. NOTED DAMAGE TO SKIN AFT OF RUDDER (M)(P). SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0233:2721-2001/001 00405 CO
- [SDR DALA2025111908452](https://openairdocs.org/sdr/DALA2025111908452), Nov 17, 2025: SKIN. CORRODED. WASTE WATER ACCESS PANEL FWD EDGE EXTERNAL SKIN HAS CORROSION. COMPLIED WITH PRI 629290-14 REV 0, 1, 2, AND SECTION I TIME-LIMITED REPAIR OF ERA 629290-14 REV 0
- [SDR DALA2025111908451](https://openairdocs.org/sdr/DALA2025111908451), Nov 17, 2025: SKIN. CORRODED. WASTE BOX- FWD DOUBLER R/H CORNER HAS CORROSION INTERNAL AND EXTERNAL COMPLIED WITH PRI 629290-14 REV 0, 1, 2, AND SECTION I TIME-LIMITED REPAIR OF ERA 629290-1
- [SDR DALA2025111908450](https://openairdocs.org/sdr/DALA2025111908450), Nov 17, 2025: SKIN. CORRODED. WASTE BOX- AFT CUTOUT FLANGE SKIN HAS CORROSION. COMPLIED WITH PRI 629290-14 REV 0, 1, 2, AND SECTION I TIME-LIMITED REPAIR OF ERA 629290-14 REV 0. MAX MATERIAL
- [SDR DALA2025111908449](https://openairdocs.org/sdr/DALA2025111908449), Nov 17, 2025: SKIN. CORRODED. WASTE BOX- INSIDE THE BOX FWD RT CORNER SKIN HAS CORROSION. COMPLIED WITH PRI 629290-14 REV 0, 1, 2, AND SECTION I TIME-LIMITED REPAIR OF ERA 629290-14 REV 0. M
- [SDR DALA2025111908448](https://openairdocs.org/sdr/DALA2025111908448), Nov 17, 2025: SKIN. CORRODED. WASTE BOX CUT-OUT FWD RT CORNER SKIN HAS CORROSION. COMPLIED WITH PRI 629290-14 REV 0, 1, 2, AND SECTION I TIME-LIMITED REPAIR OF ERA 629290-14 REV 0. MAX MATER
- [SDR DALA2025111908447](https://openairdocs.org/sdr/DALA2025111908447), Nov 17, 2025: ACCESS PANEL. CORRODED. WASTE WATER ACCESS PANEL FWD EDGE INTERNAL SKIN HAS CORROSION. COMPLIED WITH PRI 629290-14 REV 0, 1, 2, AND SECTION I TIME-LIMITED REPAIR OF ERA 629290-14 REV 0
- [SDR DALA2025121009035](https://openairdocs.org/sdr/DALA2025121009035), Nov 11, 2025: SKIN. DAMAGED. ER/A 629290-14 ISSUED FOR DOUBLER REPAIR TO THE WASTE BOX AREA. FOLLOW-ON ACTION REQUIRED. ER/A 629290-14 SECTION I ACCOMPLISHED IN MSP NOV 2025. SECTION II REP
- [SDR DALA2025110508077](https://openairdocs.org/sdr/DALA2025110508077), Nov 5, 2025: SCUFF PLATE. CORRODED. SCUFF PLATE FASTENERS AFT CARGO COMPARTMENT DOOR. COUNTERSINK AT HOLE 4 AND HOLE 11 HAVE CORROSION IN THE COUNTERSINK. BLEND THE CORROSION ON THE SKIN AND LOWER
- [SDR DALA2025110508076](https://openairdocs.org/sdr/DALA2025110508076), Nov 5, 2025: SKIN. DAMAGED. PREVIOUS SKIN BLEND-OUT REWORK HAS DIAMETER LARGER THAN .346 INCHES SEE AMDS CARD 5331-01297-02C STEP 5. ACCOMPLISH DVI OF THE FUSELAGE BOTTOM SKIN BEHIND THE S
- [SDR DALA2025110207998](https://openairdocs.org/sdr/DALA2025110207998), Nov 1, 2025: SEAT TRACK. CORRODED. DURING C2 + 6 YEAR (HEAVY) CHECK VISIT IN MSP, EXTENSIVE CORROSION WAS FOUND AT FR20 ON THE FWD END OF RBL 23 CABIN SEAT TRACK P/N C02312798-003 WHICH EXCEEDS P
- [SDR DALA2025110608105](https://openairdocs.org/sdr/DALA2025110608105), Oct 28, 2025: SKIN. DENTED. FUSELAGE SKIN DENT LOCATED JUST FWD OF FR 26 JUST AFT OF L1 DOOR AT FLOOR LINE HAS DENT STICKER CAN NOT FIND LOG PAGE ON STICKER. SCEPTRE LOG PAGE ENTERED FOR S
- [SDR DALA2025102907932](https://openairdocs.org/sdr/DALA2025102907932), Oct 26, 2025: FRAME. CORRODED. WING TO BODY FAIRING FRAME 48, BOTH LEFT AND RIGHT FRAMES SHOW SIGNS OF CORROSION AND ELONGATED FASTENER HOLES. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 053-00
- [SDR DALA2025102407820](https://openairdocs.org/sdr/DALA2025102407820), Oct 21, 2025: PIN. BINDING. UNABLE TO INSERT DISARM PIN IN THE LH OWEED ESCAPE SLIDE. SEE NR FOR ADDITIONAL INFORMATION 001-0400:2561-9101/001 00142 REMOVAL STOCK NUMBER:81-2563-9-0007 SER
- [SDR DALA2026101905730](https://openairdocs.org/sdr/DALA2026101905730), Oct 20, 2025: SKIN. DAMAGED. DAMAGE TOLERANCE EVALUATION (DTE) REQUIRED. ERA 629805-14 SECTION I ACCOMPLISHED IN MSP DURING CHK. FOLLOW ON ACTION IS REQUIRED ON FUSELAGE SKIN AT FR26, STR. 
- [SDR DALA2026091105092](https://openairdocs.org/sdr/DALA2026091105092), Oct 20, 2025: SEAT TRACK. CORRODED. REMOVED AND INSTALLED SEAT TRACK PER A220 ASRP 51-77-00- 000AAA-028A-1. 001-0585:5300-2016/002 00428 REMOVED AND INSTALLED SEAT TRACK PER A220 ASRP 51-77-00-000
- [SDR DALA2025102407818](https://openairdocs.org/sdr/DALA2025102407818), Oct 20, 2025: SEAT TRACK. CORRODED. SEAT TRACK RBL 43.5 NEAR FR22 AT FRONT END HAS CORROSION. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0571:5321-20
- [SDR DALA2025102407817](https://openairdocs.org/sdr/DALA2025102407817), Oct 20, 2025: SEAT TRACK. CORRODED. SEAT TRACK CORROSION LBL.23 AT FRAME 74-72. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0585:5300-2016/004 00430 R
- [SDR DALA2025102407816](https://openairdocs.org/sdr/DALA2025102407816), Oct 20, 2025: SEAT TRACK. CORRODED. SEAT TRACK CORROSION LBL.43.5 AT FRAME 74-72. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0585:5300-2016/001 00427
- [SDR DALA2025102407815](https://openairdocs.org/sdr/DALA2025102407815), Oct 20, 2025: SEAT TRACK. CORRODED. SEAT TRACK CORROSION RBL.23 AT FRAME 74-72. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0585:5300-2016/003 00429 R
- [SDR DALA2025093007122](https://openairdocs.org/sdr/DALA2025093007122), Sep 25, 2025: SLAT TRACK. DAMAGED. RIGHT WING SLAT TRACK #10 REQUIRES NDT TO BLENDED AREA. PERFORMED NDT INSPECTION PER ANDTP BD500-AJ51-10-02-00AAA-352A-A OR ANDTP BD500-AJ51-01-20-01AAA-353A-A 
- [SDR DALA2025093007121](https://openairdocs.org/sdr/DALA2025093007121), Sep 25, 2025: SLAT TRACK. DAMAGED. RIGHT WING SLAT TRACK #8 REQUIRES NDT TO BLENDED AREA. PERFORMED NDT INSPECTION PER ANDTP BD500-AJ51-10-02-00AAA-352A-A OR ANDTP BD500-AJ51-01-20-01AAA-353A-A T
- [SDR DALA2025093007120](https://openairdocs.org/sdr/DALA2025093007120), Sep 25, 2025: SLAT TRACK. DAMAGED. RIGHT WING SLAT TRACK #7 REQUIRES NDT TO BLENDED AREA. PERFORMED NDT INSPECTION PER ANDTP BD500-AJ51-10-02-00AAA-352A-A OR ANDTP BD500-AJ51-01-20-01AAA-353A-A T
- [SDR DALA2025093007119](https://openairdocs.org/sdr/DALA2025093007119), Sep 25, 2025: SLAT TRACK. DAMAGED. RIGHT WING SLAT TRACK #6 REQUIRES NDT TO BLENDED AREA. PERFORMED NDT INSPECTION PER ANDTP BD500-AJ51-10-02-00AAA-352A-A OR ANDTP BD500-AJ51-01-20-01AAA-353A-A T
- [SDR DALA2025093007118](https://openairdocs.org/sdr/DALA2025093007118), Sep 25, 2025: SLAT TRACK. DAMAGED. RIGHT WING SLAT TRACK NR 5 REQUIRES NDT TO BLENDED AREA. PERFORMED NDT INSPECTION PER ANDTP BD500-AJ51-10-02-00AAA-352A-A OR ANDTP BD500-AJ51-01-20-01AAA-353A-A
- [SDR DALA2025093007117](https://openairdocs.org/sdr/DALA2025093007117), Sep 25, 2025: SLAT TRACK. DAMAGED. RIGHT WING SLAT TRACK #3 REQUIRES NDT TO BLENDED AREA. PERFORMED NDT INSPECTION PER ANDTP BD500-AJ51-10-02-00AAA-352A-A OR ANDTP BD500-AJ51-01-20-01AAA-353A-A T
- [SDR DALA2025093007116](https://openairdocs.org/sdr/DALA2025093007116), Sep 24, 2025: SLAT TRACK. DAMAGED. LEFT WING SLAT TRACK #11 REQUIRES NDT TO BLENDED AREA. PERFORMED NDT INSPECTION PER ANDTP BD500-A-J51-10-02-00AAA- 352A-A OR ANDTP BD500-A-J51-01-20-01AAA-353A-
- [SDR DALA2025093007115](https://openairdocs.org/sdr/DALA2025093007115), Sep 24, 2025: SLAT TRACK. DAMAGED. LEFT WING SLAT TRACK #10 REQUIRES NDT TO BLENDED AREA. PERFORMED NDT INSPECTION PER ANDTP BD500-A-J51-10-02-00AAA- 352A-A OR ANDTP BD500-A-J51-01-20-01AAA-353A-
- [SDR DALA2025093007114](https://openairdocs.org/sdr/DALA2025093007114), Sep 24, 2025: SLAT TRACK. DAMAGED. LEFT WING SLAT TRACK #9 REQUIRES NDT TO BLENDED AREA. PERFORMED NDT INSPECTION PER ANDTP BD500-A-J51-10-02-00AAA- 352A-A OR ANDTP BD500-A-J51-01-20-01AAA-353A-A
- [SDR DALA2025093007113](https://openairdocs.org/sdr/DALA2025093007113), Sep 24, 2025: SLAT TRACK. DAMAGED. LEFT WING SLAT TRACK #7 REQUIRES NDT TO BLENDED AREA. PERFORMED NDT INSPECTION PER ANDTP BD500-A-J51-10-02-00AAA- 352A-A OR ANDTP BD500-A-J51-01-20-01AAA-353A-A
- [SDR DALA2025093007112](https://openairdocs.org/sdr/DALA2025093007112), Sep 24, 2025: SLAT TRACK. DAMAGED. LEFT WING SLAT TRACK #4 REQUIRES NDT TO BLENDED AREA. PERFORMED NDT INSPECTION PER ANDTP BD500-A-J51-10-02-00AAA- 352A-A OR ANDTP BD500-A-J51-01-20-01AAA-353A-A
- [SDR DALA2025010600118](https://openairdocs.org/sdr/DALA2025010600118), Jan 3, 2025: SLAT TRACK. CORRODED. RH SLAT TRACK #5 HAS CORROSION AND MUST BE INSPECTED WITH EDDY CURRENT. ACCOMPLISHED EDDY CURRENT INSPECTION OF THE BLENDED AREA REF ANDTP 51-01-20-01AAA-353A-3
- [SDR DALA2025010600117](https://openairdocs.org/sdr/DALA2025010600117), Jan 3, 2025: SLAT TRACK. CORRODED. LH SLAT TRACK #1 HAS CORROSION AND MUST BE INSPECTED WITH EDDY CURRENT. ACCOMPLISHED EDDY CURRENT INSPECTION OF THE BLENDED AREA REF A22 ANDTP 51-01-20-01AAA-35
- [SDR DALA2025010600116](https://openairdocs.org/sdr/DALA2025010600116), Jan 3, 2025: SLAT TRACK. CORRODED. LH SLAT TRACK #4 HAS CORROSION AND MUST BE INSPECTED WITH EDDY CURRENT. ACCOMPLISHED EDDY CURRENT INSPECTION OF THE BLENDED AREA REF A220 ANDTP 51-01-20-01AAA-3
- [SDR DALA2024061106024](https://openairdocs.org/sdr/DALA2024061106024), Jun 7, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 4 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 4 UPPER AFT SURFACE IAW ER/A
- [SDR DALA2024061106023](https://openairdocs.org/sdr/DALA2024061106023), Jun 7, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK #5 LOWER FWD INBOARD SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 5 LOWER FWD INBOARD SIDE I
- [SDR DALA2024061106022](https://openairdocs.org/sdr/DALA2024061106022), Jun 7, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK #5 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 5 UPPER AFT SURFACE IAW ER/A 60
- [SDR DALA2024061106021](https://openairdocs.org/sdr/DALA2024061106021), Jun 7, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK #8 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 8 LOWER AFT SURFACE IAW ER/A 60
- [SDR DALA2024061106020](https://openairdocs.org/sdr/DALA2024061106020), Jun 7, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK #9 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 9 LOWER AFT SURFACE IAW ER/A 60
- [SDR DALA2024061106019](https://openairdocs.org/sdr/DALA2024061106019), Jun 7, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 2 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 2 UPPER AFT SURFACE IAW ER/A
- [SDR DALA2024061106018](https://openairdocs.org/sdr/DALA2024061106018), Jun 7, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 7 LOWER FWD I/B SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 7 LOWER FWD I/B SIDE IAW ER
- [SDR DALA2024061106017](https://openairdocs.org/sdr/DALA2024061106017), Jun 7, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 6 LOWER FWD I/B SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 6 LOWER FWD I/B SIDE IAW ER
- [SDR DALA2024061106016](https://openairdocs.org/sdr/DALA2024061106016), Jun 7, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 5 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 5 UPPER AFT SURFACE IAW ER/A
- [SDR DALA2023121910379](https://openairdocs.org/sdr/DALA2023121910379), Dec 18, 2023: UNKNOWN. UNKNOWN. EMERGENCY EXIT SIGNS DO NOT ILLUMINATE WHEN LANDING GEARS ARE LOWERED. ENTIRE CABIN. / INTERIOR. PERFORMED OPS CK OF EMERGENCY LIGHTS, ALL LIGHTS ILLUMINATED. N
- [SDR DALA2023091507598](https://openairdocs.org/sdr/DALA2023091507598), Sep 11, 2023: UNKNOWN. UNKNOWN. SHIP 8133 - MISC/DE - DUE TO "FUEL IMBALANCE AND R FUEL LO QTY" CAUTION MESSAGES ON APPROACH. CORRECTIVE ACTION: FUEL/OIL HEAT EXCHANGER AND RT REFUEL SOV REPLA

All 53: https://openairdocs.org/aircraft/N133DU/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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